ICAS 2024: TOPICS AND TITLES |
1.1 - Aircraft Design and Integrated System (Basics and Theory) |
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ICAS2024_0042: L. Paletti¹, L. Boggero¹, G. Wende¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany TRANSLATING THE CONCEPT OF SUSTAINABILITY FOR THE DETERMINATION OF REQUIREMENTS FOR THE DESIGN OF FUTURE AIRCRAFT |
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ICAS2024_0059: S. Garg¹, J.H. Bussemaker¹, L. Boggero¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany MDAX : ENHANCEMENTS IN A COLLABORATIVE MDAO WORKFLOW FORMULATION TOOL |
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ICAS2024_0068: S. Hosseini¹, M.A. Vaziry Zanjany¹, H.R. Ovesy¹, E. Lekzian, Semnan University, Iran; ¹Amirkabir University of Technology, Iran APPLICATION OF LAMBDA FRAMEWORK FOR AIRCRAFT MULTIDISCIPLINARY DESIGN, ANALYSIS AND OPTIMIZATION |
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ICAS2024_0080: E.J. Adler¹, A.H.R. Lamkin¹, J.R.R.A. Martins¹; ¹University of Michigan, United States DUCTED HEAT EXCHANGER THERMAL AND AERODYNAMIC SHAPE OPTIMIZATION |
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ICAS2024_0088: A. Filippatos¹, D.N. Markatos¹, A. Theochari¹, S. Malefaki¹, T. Kalampoukas¹, S.G. Pantelakis¹; ¹University of Patras, Greece A PROPOSAL TOWARDS A STEP CHANGE FROM ECO-DRIVEN TO SUSTAINABILITY-DRIVEN DESIGN OF AIRCRAFT COMPONENTS |
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ICAS2024_0097: B.M.H.J. Fröhler¹, A.A. Pohya¹, J. Häßy¹, T. Kilian¹, A.H. Bismark¹, M. Radestock, Germany; D. Cruz Palacios, Aernnova Aerospace, Spain; ¹German Aerospace Center (DLR), Germany PERFORMANCE AND ECONOMIC ASSESSMENT OF A WING-INTEGRATED HYBRID LAMINAR FLOW CONTROL SYSTEM |
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ICAS2024_0141: N. Roh¹, M. Park¹; ¹Hanwha systems, South Korea MAXIMUM SPEED OF BATTERY-POWERED TILT-ROTOR AIRCRAFT |
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ICAS2024_0175: F. Salucci¹, N. Prabhakar¹, D. Karbowski¹; ¹Argonne National Laboratory, United States ANALYZING THE IMPACTS OF SUSTAINABLE POWERTRAINS FOR SHORT-HAUL COMMUTER AIRLINES |
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ICAS2024_0193: G. Licheva¹, S. Liscouët-Hanke¹; ¹Concordia University, Canada CRYOGENIC TANK SIZING MODEL FOR THE CONCEPTUAL DESIGN OF HYDROGEN-POWERED AIRCRAFT |
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ICAS2024_0216: L. Zheng¹, M. Wang², Y. Lu², H. Qiao¹, T. Xiao¹, S. Deng¹; ¹Nanjing University of Aeronautics and Astronautics, China; ²Chinese Aeronautical Establishment, China NUMERICAL AND THEORETICAL INVESTIGATION OF HELICOPTER DITCHING WITH VARIOUS INITIAL VELOCITY AND PITCHING ANGLE |
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ICAS2024_0233: A.S.J. van Heerden, University of Glasgow, United Kingdom; S. Jimeno Altelarrea¹, A. Riaz¹, X. Chen¹, M.D. Guenov¹, A. Molina-Cristóbal, University of Glasgow Singapore, Singapore; ¹Cranfield University, United Kingdom SET-BASED DESIGN TECHNIQUES FOR EVOLVABILITY EXPLORATION DURING CONCEPTUAL AIRCRAFT DESIGN |
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ICAS2024_0254: R. Jan¹, S. Delbecq¹, E. Benard¹; ¹ISAE-Supaero, France EVALUATION OF ASWING FOR OVERALL AIRCRAFT DESIGN OF UNCONVENTIONAL CONFIGURATIONS. APPLICATION TO JOINED WINGS WITH FOLDING WINGTIPS |
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ICAS2024_0273: S. Cacciola¹, C.E.D. Riboldi¹, C. Spitale¹; ¹Politecnico di Milano, Italy STEADY ANALYSIS OF THREE-SURFACE AIRPLANES: IMPROVING THE AERODYNAMIC PERFORMANCE THROUGH REDUNDANT LONGITUDINAL CONTROL |
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ICAS2024_0285: L. Boggero¹, J. Bussemaker¹, G. Donelli¹, F. Torrigiani¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany PROCESSES, METHODS AND TOOLS SUPPORTING THE DEVELOPMENT OF AERONAUTICAL SYSTEMS |
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ICAS2024_0301: R. di Giuseppe, ISAE-Supaero, SafranTech, France; S. Delbecq¹, V. Pauvert, SafranTech, France; V. Pommier-Budinger¹; ¹ISAE-SUPAERO, France INCREMENTAL TRADE-OFF STUDY OF A HYDROGEN FUEL CELL-BASED PROPULSION SYSTEM USING MDAO TECHNIQUES |
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ICAS2024_0303: G. Palaia¹, K. Abu Salem¹; ¹Polytechnic of Turin, Italy POWER MANAGEMENT SUPPLY OPTIMIZATION FOR HYBRID-ELECTRIC REGIONAL AIRCRAFT |
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ICAS2024_0332: Y.-T. Zhang¹, S.-R. Xu¹, Z.-J. Zheng¹, Y. Zheng¹, Y.-L. Liu¹; ¹Zhejiang University, China TILT-DUCT AIRCRAFT WING AERODYNAMIC DESIGN AND OPTIMIZATION BASED ON ADJOINT METHOD |
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ICAS2024_0346: J.L. Lovaco¹, R.C. Munjulury¹, I. Staack, Technische Universität Braunschweig, Germany; P. Krus, Linköping University, Sweden; ¹Saab Aeronautics & Linköping University, Sweden LARGE LANGUAGE MODEL-DRIVEN SIMULATIONS FOR SYSTEM OF SYSTEMS ANALYSIS IN FIREFIGHTING AIRCRAFT CONCEPTUAL DESIGN |
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ICAS2024_0371: L.H. Peristy¹, R.E. Perez¹; ¹Royal Military College of Canada, Canada LONGITUDINAL STABILITY PARAMETERS FOR FLYING BOOM AERIAL REFUELING |
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ICAS2024_0399: S. Wöhler¹, K. Buchtal¹, M. Iwanizki¹, J. Häßy¹, K. Dahlmann¹, C. Lois¹, M. Hepperle¹; ¹DLR, Germany CLIMATE IMPACT AND ECONOMIC ASSESSMENT OF LIQUID HYDROGEN AND SYNTHETIC KEROSENE LONG-RANGE AIRCRAFT CONCEPTS |
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ICAS2024_0415: S. Corcione¹, A. De Marco¹, V. Cusati¹; ¹University of Naples Federico II, Italy A COST-EFFICIENT PREDICTIVE METHOD FOR AERODYNAMIC PERFORMANCE DEGRADATION OF HORIZONTAL TAIL UNDER ICING CONDITIONS |
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ICAS2024_0420: Z. Lu¹, Z.-H. Han¹, W.-P. Song¹, K.-S. Zhang¹, K.-Y. Zhou¹; ¹School of Aeronautics, Northwestern Polytechnical University, China EFFICIENT MULTI-OBJECTIVE DESIGN OPTIMIZATION OF ROTOR AIRFOILS FOR IMPROVING DYNAMIC STALL CHARACTERISTICS |
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ICAS2024_0431: A. Yang¹, J. Zhang, Shanghai Artificial Intelligence Laboratory, China; J. Li, Institute of High Performance Computing, A*STAR, Singapore; R. Liem¹; ¹Hong Kong University of Science and Technology, Hong Kong SAR of China DATA-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION AND MULTI-FIDELITY DESIGN EXPLORATION USING CONDITIONAL DIFFUSION-BASED GEOMETRY SAMPLING METHOD |
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ICAS2024_0439: R. Parello, ONERA/ISAE-SUPAERO, France; S. Defoort, ONERA, France; E. Benard¹, Y. Gourinat¹; ¹ISAE-SUPAERO, France INTEGRATING CRYOGENIC TANKS MODEL IN HYDROGEN AIRCRAFT DESIGN FOR PARAMETRIC PERFORMANCE ANALYSIS |
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ICAS2024_0462: G. Grazioso, University of Naples Federico II, Italy; A. De Marco, University of Naples, Italy STRUT-BRACED WING INDUCED DRAG MODELING FOR REGIONAL TURBOPROP AIRCRAFT DESIGN |
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ICAS2024_0470: M. Tuccillo¹, P. Della Vecchia¹; ¹University of Naples Federico II, Italy MULTIDISCIPLINARY PRELIMINARY DESIGN PROCESS OF HYBRID-ELECTRIC SEAPLANE |
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ICAS2024_0484: K. Swannet¹, C. Varriale¹, N.A.K. Doan¹; ¹Delft University of Technology, Netherlands LATENT SPACE CORRELATION FOR INTERPRETABLE AIRFOIL PARAMETERIZATION USING VARIATIONAL AUTOENCODERS |
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ICAS2024_0488: N. Bhargav¹, V. Elangovan¹, R.C. Munjulury, Linköping University, Sweden; C. Hesse², P. Satwan²; ¹Linköping University/DLR, Germany; ²Institute for System Architectures in Aeronautics, DLR, Germany EXPLORATION AND EVALUATION OF KNOWLEDGE-BASED ENGINEERING APPROACH FOR LIQUID HYDROGEN TANK INTEGRATION IN EXISTING FUSELAGE |
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ICAS2024_0496: T. Goetzendorf-Grabowski¹, A. Kwiek¹, J. Mieloszyk, ?ukasiewicz Research Network – Institute of Aviation, Poland; A. Tarnowski¹; ¹Warsaw University of Technology, Poland RAPID DESIGN OF UNCONVENTIONAL AIRCRAFT USING SOFTWARE TOOLS COUPLED IN OPTIMIZATION LOOP – LESSONS LEARNED |
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ICAS2024_0515: P. De Felipe¹, C. Cumpsty¹, I. Iturriaga¹, H. Dance¹; ¹ZeroAvia, United Kingdom HYDROGEN AIRLINER TANK OPTIMISATION |
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ICAS2024_0561: Y. Tong¹, M. Luo¹, Z. Cui¹, Z. Liu¹, Z. Ji¹; ¹Beihang University, China RESEARCH ON MULTI-ATTRIBUTE DECISION MAKING AND VERIFICATION METHODS FOR SYSTEMS CONFRONTATION |
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ICAS2024_0572: Y.H. Wang¹, W.P. Song¹, H. Nie¹, K.F. Zheng¹, Z.H. Han¹; ¹Northwestern Polytechnical University, China DESIGN OPTIMIZATION OF A WIG CRAFT’S HIGH LIFT DEVICE CONSIDERING GROUND EFFECT |
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ICAS2024_0575: M. Alberti¹, G. Apuleo¹, A. Calia¹, D. Cirio¹, A. Cozzolino¹, F. Gravano¹, M. Mancini¹, F. Nunciato¹, A. Terrile¹; ¹Piaggio Aerospace, Italy AICRAFT-0 SAT D1 FOR GREENER, SAFER AND AFFORDABLE MORE ELECTRIC (MEA) AND FLY-BY-WIRE (FBW) SMALL AIR TRANSPORT (SAT) |
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ICAS2024_0585: C. Jouanet¹, K. Amadori¹, E. Espinoza Juarez¹; ¹Linköpings University, Sweden SUSTAINABLE AVIATION IN NORDIC COUNTRIES |
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ICAS2024_0590: F. Mazzoni¹, G. Accardo², R. Biga², E. Brusa¹, C. Delprete¹, C.A. Manrique-Escobar², V. Vercella²; ¹Politecnico di Torino, Italy; ²Leonardo S.p.A., Italy HYDROGEN STORAGE SYSTEM DESIGN: CASE STUDIES FOR AIRBORNE APPLICATION |
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ICAS2024_0611: L.J. Liu¹, D. Kim, Ecole Nationale de l’Aviation Civile, France; C. Reyner¹, R.P. Liem¹; ¹The Hong Kong University of Science and Technology, Hong Kong SAR of China DATA-DRIVEN MULTI-RANGE MISSION-BASED OVERALL AIRCRAFT CONCEPTUAL DESIGN OPTIMIZATION |
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ICAS2024_0614: Y.-L. Yin¹, K.-S. Zhang¹, H.-L. Qiao¹, A.-L. Che¹, Z.-H. Han¹; ¹School of Aeronautics, Northwestern Polytechnical University, China FAST PARAMETRIC STRUCTURE MODELING FOR VARIETY OF AIRCRAFT CONFIGURATIONS |
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ICAS2024_0625: K.-S. Zhang¹, H.-L. Qiao¹, P.-H. Wang¹, Y.-Q. Du¹, Z.-H. Han¹; ¹School of Aeronautics, Northwestern Polytechnical University, China EXPLORATION OF EFFICIENT HYPERPARAMETERS ADAPTION OF SUPPORT VECTOR REGRESSION FOR AERODYNAMIC DESIGN |
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ICAS2024_0626: Y. Liu¹, C.N. Li¹, C.L. Gong¹; ¹Northwestern Polytechnical University, China A DISTRIBUTED UMDO ARCHITECTURE BASED ON SURROGATE MODELS FOR LAUNCH VEHICLE DESIGN |
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ICAS2024_0643: L.D. Deng¹, W.P. Song¹, J.H. Xu¹; ¹School of Aeronautics, Northwestern Polytechnical University, China INVESTIGATION ON AERODYNAMIC DESIGN OF VTOL AIRCRAFT PROPELLER |
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ICAS2024_0687: M.A.S. Abdul-Kaiyoom¹, A. Yildirim¹, J.R.R.A. Martins¹; ¹University of Michigan, United States ROBUST SCHUR-COMPLEMENT SOLVERS AND LARGE-SCALE MULTIDISCIPLINARY DESIGN OPTIMIZATION |
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ICAS2024_0696: S. Du, China; C. Li, China; Y. Liu, China AN UNCERTAINTY MULTIDISCIPLINARY PROPAGATION ANALYSIS METHOD FOR CORRELATED HIGH-DIMENSIONAL DATA IN AIRCRAFT DESIGN |
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ICAS2024_0721: Z. Dong¹, X. Guo¹, W. Dong¹, P. Wang¹; ¹Shanghai Jiaotong University, China TRANSIENT SIMULATION CALCULATION FOR ELECTRIC THERMAL ANTI-ICING PERFORMANCE OF COMPOSITE WING IN ICING ENVIRONMENT |
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ICAS2024_0723: R.J. Huyssen, CSIR, South Africa; G.R. Spedding, University of Southern California, United States ON THE EXISTENCE OF A FAMILY OF IDEAL AIRCRAFT CONFIGURATIONS |
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ICAS2024_0736: A. Marsano¹, F. Bustos Ortega¹, G. Santarella¹, S.G. Soundararajan¹, F. Giargia¹; ¹Politecnico di Torino, Italy CFD STUDY OF AIR SUPPLY SYSTEM FOR COOLING OF A HYDROGEN POWERED UNMANNED SEAPLANE AND REDUCTION OF THE RESULTING DRAG |
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ICAS2024_0744: B.T.V. Carnielo¹, D.D. Bueno¹; ¹São Paulo State University, Brazil THE INFLUENCE OF DIFFERENT WING MOTIONS ON THE LIFT IN BIO-INSPIRED AERIAL VEHICLES |
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ICAS2024_0825: N.-H. Ye¹, T. Long¹, B. Fu, Xi’an Modern Control Technology Research Institute, China; R.-H. Shi, Beijing Institute of Technology Chongqing Innovation Center, China; ¹Beijing Institute of Technology, China SURROGATE-ASSISTED HIERARCHICAL OPTIMIZATION METHOD FOR VARIABLE SWEEP FLIGHT VEHICLE TRAJECTORY |
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ICAS2024_0862: A. Viviani¹, A. Aprovitola¹, L. Iuspa², G. Pezzella²; ¹Università della Campania Luigi Vanvitelli , Italy; ²Università della Campania Luigi Vanvitelli , Italy OPTIMIZATION PROCEDURE FOR THE WING OF A MARS EXPLORATION DRONE |
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ICAS2024_0943: S. Favre¹, F. Di Fede, Leonardo Labs, Leonardo S.p.A., Italy; E. Brusa¹, C. Delprete¹; ¹Politecnico di Torino, Italy FUEL-BASED THERMAL MANAGEMENT SYSTEM ARCHITECTURES AND TANK TEMPERATURE EVOLUTION MODELS FOR AVIATION |
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ICAS2024_0951: C.P. van Dam, University of California - Davis, United States; S.S. Hosseini¹, S.A. Pandya¹; ¹NASA Ames Research Center, United States SCOPING OF AN AIR SUPPLY CONFIGURATION FOR ACTIVE FLOW CONTROL ON A COMMERCIAL TRANSPORT AIRPLANE HIGH-LIFT SYSTEM |
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ICAS2024_1002: L. Trainelli¹, C.E.D. Riboldi¹, G. Sirtori¹; ¹DAER, Politecnico di Milano, Italy METHODOLOGIES FOR THE PRELIMINARY SIZING OF HYDROGEN-POWERED AIRCRAFT AND SUPPORTING AIRPORT INFRASTRUCTURES |
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ICAS2024_1036: J.Z. Li¹, Y.J. Yang¹, Y.F. Zhang¹; ¹School of Aerospace Engineering, Tsinghua University, China AIRFOIL PRESSURE PREDICTION BASED ON PHYSICS-INFORMED DEEP LEARNING APPROACH |
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ICAS2024_1046: J.L.C. Chan¹, Y. Sun¹, H. Smith, Cranfield University , United Kingdom; ¹Cranfield University, United Kingdom PERFORMANCE ENHANCEMENTS BETWEEN DIFFERENT APPLICATIONS OF ALTERNATIVE FUELS AND NOVEL AIRCRAFT CONFIGURATIONS |
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ICAS2024_1067: R. Cavallaro¹, P. Norczyk Simon¹, A. Cini¹; ¹Universidad Carlos III de Madrid, Spain LOCAL AIR QUALITY AND NOISE OPTIMIZATION OF A LARGE ASPECT RATIO WINGS WITH DISTRIBUTED HYBRID ELECTRIC PROPULSION |
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ICAS2024_1114: P. Shiva Prakasha¹, P. Ratei¹, M. Van Eenige¹, T. Lefebvre, The French Aerospace Lab, France; M. Alder¹, U. Gupta, Cranfield University , United Kingdom; M. Antonio Solazzo, CIRA, Italy; B. Nagel¹; ¹German Aerospace Center - DLR, Germany EU IMPACT MONITOR PROJECT - OVERVIEW AND APPROACH |
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ICAS2024_1134: S. Cacciola¹, L. Bottà¹, C.E.D. Riboldi¹, L. Trainelli¹; ¹Politecnico di Milano, Italy IDENTIFICATION OF THE IMPACT OF BLOWING ON THE AERODYNAMIC MODEL OF AN AIRPLANE WITH DISTRIBUTED ELECTRIC PROPULSION |
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ICAS2024_1169: V.T. Todorov¹, D. Rakov, Blagonravov Institute of Engineering Science, Russia; A. Bardenhagen¹; ¹Technical University of Berlin, Germany A MORPHOLOGICAL ANALYSIS OF METHODS FOR CONCEPTUAL AIRCRAFT DESIGN UNDER UNCERTAINTIES |
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ICAS2024_1292: F. Collier, NASA (LaRC), United States OBJECTIVES OF THE UNITED STATES FULL SCALE BLENDED WING BODY FLIGHT DEMONSTRATION |
1.2 - Aircraft Design and Integrated System (Applications) |
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ICAS2024_0036: D. Teubl¹, T.B. Sissing¹, M. Hornung¹; ¹Chair of Aircraft Design, Technical University of Munich, Germany RETROFITTING A JET DRIVEN UAV TO FORM A MULTI-PURPOSE TEST PLATFORM |
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ICAS2024_0064: R. Habing¹, M.-J. Van der Meulen¹, M. Huet, ONERA / DAAA, France; R. Jaron, DLR, Germany; F. Petrosino², M. Barbarino², O. Zaporozhets, Institute of Aviation, Poland; ¹NLR, Netherlands; ²CIRA, Italy DUAL-STREAM JET NOISE TEST WITH INTERNAL MIXER DESIGN VARIATIONS FOR LTO NOISE OF SUPERSONIC AIRCRAFT |
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ICAS2024_0091: Y.C. Roth¹, R. Herrmann¹, C. Sanchez Santos, Aernnova, Spain; M. Uellendahl, Airbus Aerostructures, Germany; J. Koopman, GKN Fokker Aerospace, Netherlands; A. Henneberg, Diehl Aviation, Germany; J. Kos, Royal Netherlands Aerospace Centre, Netherlands; I.F. Villegas, Delft University of Technology, Netherlands; A. Choudhary, SAMXL, Netherlands; L. Larsen, DLZ Zentrum für Leichtbauproduktionstechnologie, Germany; S. Ferstl, Premium Aerotec, Germany; B. Diehl, Fraunhofer, Germany; F. Emanuelsson, Saab Aerospace Systems, Sweden; J.-B. Sinechal¹, M. Pleth¹, K. Atherton¹; ¹Airbus, Germany CLEANSKY2/ CLEAN AVIATION LARGE PASSENGER AIRCRAFT FOR MORE SUSTAINABLE COMMERCIAL FUSELAGE TECHNOLOGIES – MAJOR ACHIEVEMENTS |
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ICAS2024_0092: T. Burschyk¹, B. Fröhler¹, M. Alder¹, T. Zill¹; ¹DLR, Institute for System Architectures in Aeronautics, Germany GLOBAL SENSITIVITY ANALYSIS OF LIQUID HYDROGEN STORAGE DESIGN PARAMETERS FOR OVERALL AIRCRAFT DESIGN |
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ICAS2024_0103: M. Engelmann¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany GEOMETRIC OPTIMIZATION OF HYDROGEN AIRCRAFT FUSELAGES IN PRELIMINARY DESIGN |
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ICAS2024_0109: H. Mohammadi¹, G. Sirtori¹, L. Trainelli¹; ¹DAER, Politecnico di Milano, Italy PRELIMINARY SIZING OF HYDROGEN-BURNING JETLINER FOR DIRECT OPERATING COST OPTIMIZATION |
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ICAS2024_0121: M. Graebert¹, R. Jaron¹, M. Plohr¹, S. Zenkner¹, C. Richter², C. Stöhr², C. Villena Munoz, Cranfield University, United Kingdom; M.-J. van der Meulen³, R. Habing³, M. Huet, ONERA, France; F. Petrosino*, M. Barbarino*, F. Fischer, MTU, Germany; O. Zaporozhets, Institute of Aviation, Poland; ¹DLR, Germany; ²Rolls-Royce Deutschland, Germany; ³NLR, Netherlands; *CIRA, Italy LANDING AND TAKEOFF NOISE PREDICTION OF CONCEPTUAL SUPERSONIC AIRCRAFT |
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ICAS2024_0129: M. Plohr¹, S. Zenkner¹, S. Bake², D. Zeitz²; ¹DLR Institute of Propulsion Technology, Germany; ²Rolls-Royce Deutschland Ltd & Co KG, Germany THERMODYNAMIC DESIGN AND EMISSIONS MODEL OF A MACH 1.8 SUPERSONIC AIRLINER ENGINE |
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ICAS2024_0151: T. Müller¹, V. Gollnick¹; ¹Institute of Air Transportation Systems, Germany A DESIGN APPROACH FOR A MODEL-SCALE VTOL POWERED BY TWO PIVOTING KEROSENE TURBINES |
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ICAS2024_0166: S.M. Lübbe¹, M. Schäfer¹, O. Bertram¹; ¹German Aerospace Center (DLR), Germany MASS AND POWER ESTIMATIONS IN PRELIMINARY FLIGHT CONTROL SYSTEM DESIGN |
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ICAS2024_0172: N. Prabhakar¹, F. Salucci¹, D. Karbowski¹; ¹Argonne National Laboratory, United States ENERGY AND EMISSION ANALYSIS OF AN AIR-TAXI SERVICE USING DYNAMIC EVTOL SYSTEM MODELS |
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ICAS2024_0179: A. Heidebrecht¹, M. Hoogreef¹, A.T. Isikveren, SAFRAN S.A., Germany; A. Gangoli Rao¹; ¹TU Delft, Netherlands RESULTS FROM THE APPU PROJECT: THE POTENTIAL OF LOW-THRESHOLD HYDROGEN-POWERED BLI PROPULSION |
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ICAS2024_0217: K. Abu Salem¹, G. Palaia¹, A. Frediani, SkyBox Engineering, Italy; ¹Politecnico di Torino, Italy FROM THEORY TO FLIGHT: THE BOX-WING CONFIGURATION IMPLICATIONS FOR THE NEXT-GENERATION AIRCRAFT |
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ICAS2024_0222: K. Abu Salem¹, G. Palaia¹; ¹Politecnico di Torino, Italy ENVIRONMENTAL IMPLICATIONS OF HYBRID-ELECTRIC REGIONAL AIRCRAFT: EMISSIONS AND CLIMATE CHANGE |
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ICAS2024_0251: N. Wood¹, S. Taylor¹, M. Hales¹, M. Joynt¹, S. Chandran¹, D. Sanjeevekumar¹; ¹GKN AEROSPACE, United Kingdom A PERFORMANCE COMPARISON OF HYDROGEN AIRCRAFT CONCEPTS |
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ICAS2024_0267: H. Jentink, Royal Netherlands Aerospace Centre NLR, Netherlands; C. Döll, ONERA, France; P. Iannelli, CIRA, Italy; M. Hoogreef, TU Delft, Netherlands; D. Kierbel, Airbus, France SCALED FLIGHT TESTING FOR EVALUATING DISTRIBUTED ELECTRIC PROPULSION |
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ICAS2024_0284: Z.X. Yao, Shenyang Aircraft Design and Research Institute, China INNOVATIVE UAVS WITH CONFIGURATION OF LIKING BOTH PLANE AND KITE FOR WIND POWER |
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ICAS2024_0352: M. Park¹, N. Roh¹; ¹Hanwha systems, South Korea DETERMINISTIC HYBRID POWER RATIOS CONSIDERING VARIOUS FAILURE CASES FOR QUAD TILTROTOR AIRCRAFT |
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ICAS2024_0358: F. Reimer¹, M. Fuchs¹, J. Herzig¹, S. Cornelje¹, J. Biedermann¹, B. Nagel¹; ¹DLR, Germany INVESTIGATING THE FLEXIBLE HYDROGEN AIRCRAFT SYSTEM INTERFACE DESIGN USING THE XR CO-DESIGN APPROACH |
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ICAS2024_0366: M. Blandino¹, M.M. Molinari¹, J. Liberatori¹, P.P. Ciottoli¹, R. Malpica Galassi¹; ¹Sapienza Università di Roma, Italy IMPACT OF WELL-TO-TANK EFFICIENCY AND EMISSIONS ON HYBRID AIRCRAFT DESIGN OPTIMIZATION |
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ICAS2024_0398: S. Wöhler¹, J. Häßy¹, V. Kriewall, TUHH, Germany; ¹DLR, Germany ESTABLISHING THE DLR-F25 AS A RESEARCH BASELINE AIRCRAFT FOR THE SHORT-MEDIUM RANGE MARKET IN 2035 |
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ICAS2024_0477: E.-H. Lee¹, H.-H. Yang¹, S.-G. Lee¹, J.-H. Han¹; ¹KAIST, South Korea DEVELOPMENT OF A SERVO-DRIVEN FLAPPING-WING AIR VEHICLE WITH FOLDING-WING MECHANISM |
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ICAS2024_0503: M. Kotzem¹, S. Wöhler¹, T. Burschyk¹, C. Hesse¹, S. Hellbrück¹, T. Zill¹; ¹German Aerospace Center (DLR), Germany CONCEPTUAL AIRCRAFT DESIGN OF A RESEARCH BASELINE WITH DIRECT LIQUID HYDROGEN COMBUSTION |
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ICAS2024_0536: V. Youhanna¹, L. Felicetti¹, D. Ignatyev¹; ¹Cranfield University, United Kingdom PRELIMINARY DESIGN EXPLORATION OF PROSPECTIVE MULTIROTOR AEROBOTS FOR MARS |
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ICAS2024_0557: R.Y. Yanev¹, I. Staack¹; ¹Technische Universität Braunschweig, Germany FRAMEWORK DEVELOPMENT FOR CONCEPTUAL DESIGN AND CONFIGURATION ANALYSIS OF EVTOL AIRCRAFT |
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ICAS2024_0564: C. Reyner¹, C. Lee¹, D. Kim, Ecole Nationale de l’Aviation Civile, France; R.P. Liem¹; ¹The Hong Kong University of Science and Technology, Hong Kong SAR of China MISSION-BASED OPTIMAL PROPELLER SELECTION FOR VTOL SUAV CONFIGURATION |
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ICAS2024_0566: Z. Lei, SUWA UNIVERSITY OF SCIENCE, Japan POTENTIAL OF THE RANGE EXTENSION OF SUPERSONIC TRANSPORT |
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ICAS2024_0568: G. Jia, China; D. Hu, China; Z. Guo, China; Y. Lu, China; D. Liu, China ANALYSIS OF STEALTH ENHANCEMENT DESIGN PROCESS AND METHODS FOR UNMANNED AERIAL VEHICLE |
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ICAS2024_0573: Y. Shiratsuchi¹, K. Kaneko, The University of Tokyo, Japan; S. Okada, Tokyo University of Agriculture and Technology, Japan; A. Oyama², K. Yamada², H. Tanaka², M. Sato¹; ¹Kogakuin University, Japan; ²Japan Aerospace Exploration Agency, Japan MICRO-SIZE MARS AIRPLANE FOR THE STEPWISE MARS LANDING EXPLORATION PROGRAM |
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ICAS2024_0597: Q. Chen¹, Z.-H. Han¹, J.-L. Qiao¹, Y.-L. Ding¹, K.-S. Zhang¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China AERODYNAMIC DESIGN OF A SUPERSONIC TRANSPORT CONFIGURATION CONSIDERING AVERAGE LOUDNESS IN THE WHOLE BOOM CARPET |
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ICAS2024_0636: R. de Vries¹, R.E. Wolleswinkel¹, D. Rosen Jacobson¹, M. Bonnema², S. Thiede²; ¹Elysian Aircraft, Netherlands; ²University of Twente, Netherlands BATTERY PERFORMANCE METRICS FOR LARGE ELECTRIC PASSENGER AIRCRAFT |
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ICAS2024_0649: C.E.D. Riboldi¹, M. Belan¹, S. Cacciola¹, R. Terenzi¹, S. Trovato¹, D. Usuelli¹, G. Familiari¹; ¹Dept. of Aerospace Science and Technology, Politecnico di Milano, Italy PRELIMINARY SIZING OF A LOW-ALTITUDE AIRSHIP INCLUDING ION PLASMA THRUSTERS |
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ICAS2024_0758: C. Villena Muñoz¹, C. Lawson¹, A. Riaz¹, A. Sharma¹; ¹Cranfield University, United Kingdom DESIGN OF THE SENECA MACH 1.8 SUPERSONIC AIRLINER WITH MULTI-FIDELITY AERODYNAMIC ANALYSIS FOR NOISE-OPTIMISED TAKE-OFF TRAJECTORIES |
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ICAS2024_0785: H. Kim¹, T. Kim, Seoul Digital University, South Korea; C. Son¹; ¹Cheongju University, South Korea A STUDY ON BATTERY SEPARATION DRONES TO EXTEND ENDURANCE |
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ICAS2024_0813: D. Liu¹, Z. Chen¹, Z. Guo¹, B. Zhu¹, G. Jia¹, X. Yang¹; ¹National University of Defense Technology, China ANALYSIS OF BATTERY WEIGHT REQUIREMENTS IN THE DESIGN OF HYBRID ELECTRIC POWERED AIRCRAFT |
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ICAS2024_0820: R. Jaron, DLR, Germany; N. Viola, Politecnico di Torino, Italy THE FUTURE OF CIVIL SUPERSONIC TRANSPORT IN EUROPE: THE SENECA AND MORE&LESS PROJECTS |
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ICAS2024_0826: E. Nguyen Van¹, J. Gauvrit-Ledogar¹, C. Julien², B. Paluch², J.L. Ruan, ONERA/DMPE, France; F. Moens, ONERA/DAAA, France; ¹ONERA/DTIS, France; ²ONERA/DMAS, France IMPACT OF HYDROGEN FUEL ON OVERALL DESIGN OF TRANSPORT AIRCRAFT |
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ICAS2024_0882: G. Fasulo¹, L. Federico¹, F. Petrosino¹, S. Graziani², N. Viola², S. Hengy³, B. Martinez³, M. Albisser³; ¹Italian Aerospace Research Centre (CIRA), Italy; ²Politecnico di Torino, Italy; ³French-German research institute of Saint-Louis (ISL), France SONIC BOOM COMPARATIVE STUDY BETWEEN MACH 4.7 OUTDOOR EXPERIMENTAL TESTS AND NUMERICAL SIMULATIONS |
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ICAS2024_0910: A. Bierig¹, F. Nikodem¹, D. Rothe¹; ¹DLR, Germany GENERAL DESIGN CONSIDERATIONS FOR SOLAR-ELECTRIC HIGH-ALTITUDE LONG-ENDURANCE AIRCRAFT |
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ICAS2024_0927: E. Sunzeri¹, D. Ferretto¹, N. Viola¹; ¹Politecnico di Torino, Italy CONCEPTUAL DESIGN METHODOLOGY FOR LOW-SUPERSONIC LH2-POWERED PASSENGERS AIRCRAFT |
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ICAS2024_0939: R.K. Nangia, Nangia Aero, United Kingdom; L. Hyde, Consulting, United Kingdom; J.E. Cooper, Bristol University, United Kingdom CONTINUING DEVELOPMENT OF A NOVEL CERTIFIABLE AIRLINER “GONDOLA” USING LIQUID HYDROGEN |
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ICAS2024_0975: E. Terrenoire¹, M. Muller¹, E. Ramirez Correra², P. Leyland², K. Synylo³, A. Krupko³, O. Zaporozhets, ILOT, Poland; D. Lee*, B. Owen*, L. Lim*, A. Skowron*, R. Rodriguez DE Leon*, D. Marsh*, S. Matthes, DLR, Germany; P. Madden, RR UK, United Kingdom; S. Bake, RR DE, Germany; C. Mourouzidis, CU, United Kingdom; ¹ONERA, France; ²AEDS, Switzerland; ³NAU, Ukraine; *MMU, United Kingdom SENECA’S AIRCRAFT EMISSIONS EVALUATION AND THEIRS ENVIRONMENTAL |
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ICAS2024_1021: I. Kopec¹, D. Matyja¹; ¹Polish Air Force University, Poland DESIGN OF REMOTE-CONTROLLED GROUND BASED AIRCRAFT TUG |
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ICAS2024_1032: R. Fusaro¹, G. Piccirillo¹, D. Ferretto¹, G. Saccone, Italian Aerospace Research Center, Italy; D. Bodmer², J. Jäschke², M. Cremaschi, ENVISA, Italy; N. Viola¹; ¹Politecnico di Torino, Italy; ²Hamburg University of Technology, Germany ESATTO: THE HOLISTIC FRAMEWORK TO SUPPORT THE DESIGN OF SUSTAINABLE SUPERSONIC AVIATION |
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ICAS2024_1060: A. Battiston¹, A. Magrini¹, R. Ponza¹, E. Benini¹, B. Türkyilmaz², A. Seitz², A. Heidebrecht, TU Delft, Netherlands; ¹hit09, Italy; ²Bauhaus Luftfahrt, Germany DESIGN OPTIMISATION OF A BOUNDARY LAYER INGESTION PROPULSOR FOR A MULTI-FUEL HYDROGEN AIRCRAFT |
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ICAS2024_1078: C. Svensson¹, P. Miltén¹, T. Grönstedt¹; ¹Chalmers University of Technology, Sweden MODELLING HYDROGEN FUEL CELL AIRCRAFT IN SUAVE |
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ICAS2024_1085: L. Trainelli¹, C.E.D. Riboldi¹, Y.M. Khan¹, F. Salucci, Argonne National Laboratory, United States; G. Sirtori¹; ¹DAER, Politecnico di Milano, Italy CONCEPTUAL DESIGN OF A ZERO-EMISSION REGIONAL AIRCRAFT FOR ENHANCED SHORT-HAUL MOBILITY |
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ICAS2024_1090: B. Rietdijk¹, M. Selier¹; ¹Conscious Aerospace, Netherlands ARCHITECTURE DESIGN FOR A COMMERCIALLY VIABLE HYDROGEN-ELECTRIC POWERED RETROFITTED REGIONAL AIRCRAFT |
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ICAS2024_1156: A. Kalgutkar¹, P. Gupta¹, P. Priyadarshi, Vikram Sarabhai Space Centre, India, India; R.S. Pant¹; ¹Indian Institute of Technology Bombay, India, India CONCEPTUAL DESIGN AND SIZING OF A SOLAR POWERED QUAD-ROTOR FIXED WING HYBRID UAV FOR EXPLORATION OVER MARS |
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ICAS2024_1170: A.A. Mishra¹, B. Kunwar¹, I. Chakraborty¹; ¹Auburn University, United States INTEGRATED SIZING OF AN ELECTRIFIED TILT-WING AIRCRAFT FOR VERTICAL AND CONVENTIONAL TAKEOFF AND LANDING |
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ICAS2024_1207: G. Cafiero¹, P.J. Comunian¹, A. Lerro¹, F. Ponti², A.N. Damiani Ferretti²; ¹Politecnico di Torino, Italy; ²Università di Bologna, Italy PRELIMINARY DESIGN OF A FULL ELECTRIC GENERAL AVIATION AIRCRAFT POWERED WITH FUEL CELL: A CASE STUDY. |
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ICAS2024_1293: M. Page, JetZero, United States TECHNICAL APPROACH FOR A BWB AIRLINER TO MEET MARKET DEMANDS |
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ICAS2024_1294: M. Page, JetZero, United States TECHNICAL FINDINGS TO DATE TO SUPPORT MARKET DEMANDS OF A BWB AIRLINER |
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ICAS2024_1295: M. Page, JetZero, United States GROUND AND SCALED FLIGHT TEST PLANS TO SUPPORT DEVELOPMENT OF A BWB AIRLINER |
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ICAS2024_1296: J. Ahuja¹, C. Perron¹, R.D.B. Rivera¹, J.C. Tai¹, D.N. Mavris¹; ¹Georgia Tech, United States PERFORMANCE COMPARISON OF THE BLENDED WING BODY AND TUBE AND WING CONFIGURATIONS |
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ICAS2024_1303: J.M. Thomassin, Pratt & Whitney Canada, Canada P&W APPROACH TO SUSTAINABILITY |
2 - Systems Engineering and Integration |
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ICAS2024_0041: H. Cao¹, W. Cheng¹, C. Xing, Chinese Aeronautics Establishment (CAE), China; G. Song¹; ¹ Aviation Industry Development Research Center of China (ADR) , China TECHNICAL RISK MANAGEMENT OF SYSTEM OF SYSTEMS BASED ON TECHNOLOGY READINESS ASSESSMENT |
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ICAS2024_0053: N. Kuelper¹, V. Kriewall¹, K. Beschorner¹, F. Thielecke¹; ¹Hamburg University of Technology, Germany TECHMAPS – TECHNOLOGY MANAGEMENT FOR THE ARCHITECTING PROCESS OF AIRCRAFT ON-BOARD SYSTEMS |
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ICAS2024_0076: A. Spinelli¹, A. Sharma, Centre for Aeronautics, Cranfield University, United Kingdom; T. Kipouros¹; ¹Centre for Propulsion and Thermal Power, Cranfield University, United Kingdom REQUIREMENTS UNCERTAINTY PROPAGATION IN CONCEPTUAL DESIGN USING BAYESIAN NETWORKS |
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ICAS2024_0095: A. Sarr¹, J. Jézégou¹, P. de Saqui-Sannes¹; ¹ISAE-SUPAERO, France MODEL-BASED APPROACH FOR HYDROGEN PRELIMINARY AIRCRAFT DESIGN CONSIDERING SAFETY AND OPERABILITY |
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ICAS2024_0148: B. Boden¹, M. Padilha¹, T. Burschyk¹, C. Cabaleiro de la Hoz¹, E. Moerland¹, M. Fioriti, Politecnico di Torino, Germany; ¹DLR, Germany AUTOMATING THE VERIFICATION OF GEOMETRIC REQUIREMENTS FOR AIRCRAFT FUEL SYSTEMS USING KNOWLEDGE-BASED ENGINEERING |
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ICAS2024_0160: V. Voth¹, O. Bertram¹; ¹German Aerospace Center (DLR), Germany AIRCRAFT SYSTEM DESIGN: A MODEL-BASED AND COLLABORATIVE APPROACH |
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ICAS2024_0191: S. Kazula, DLR - Electrified Aero Engines, Germany SAFETY ANALYSIS (CCA) OF THE AIR SUPPLY SYSTEM OF A FUEL CELL-POWERED AERO ENGINE FOR ELECTRIC REGIONAL AIRCRAFT |
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ICAS2024_0211: W. Cheng¹, R. Fan, Aviation Industry Corporation of China, Ltd (AVIC), China; J. Xu¹, H. Zhang¹, Z. Wang¹; ¹Aviation Industry Development Research Center of China (ADR), China RESEARCH ON TECHNOLOGICAL INNOVATION CAPABILITY EVALUATION INDEX FOR AVIATION INDUSTRIES |
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ICAS2024_0318: A. Hechelmann¹, T. Mannchen¹; ¹Baden-Wuerttemberg Cooperative State University (DHBW) Ravensbur, Germany APPLICATION OF SYSML IN THE DEVELOPMENT OF AIRCRAFT CABIN HEALTH MANAGEMENT |
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ICAS2024_0343: M. Yao¹, X. Wang¹, L. Kong, Chinese Aeronautical Establishment, China; G. Fu¹, X. Wang¹, J. Yao¹; ¹School of Reliability and Systems Engineering, Beihang Universit, China RESEARCH ON UNMANNED CLUSTER RECONNECTION DECISION-MAKING METHOD CONSIDERING RESOURCE SUPPLEMENTATION |
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ICAS2024_0357: F. Villas¹, L. Knöös Franzén¹, C. Jouannet², K. Amadori², I. Staack, TU Braunschweig, Germany; ¹Linköping University, Sweden; ²Saab Aeronautics, Sweden CONCEPT OF OPERATIONS IN AN AGENT-BASED SIMULATION: A SYSTEM-OF-SYSTEMS APPROACH |
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ICAS2024_0397: L.D.O. Morais¹, P. Krus, Linköping University, Sweden; L. Pereira¹; ¹UFABC, Brazil A HUMAN-CENTERED SYSTEMS ENGINEERING APPROACH FOR INTEGRATING ARTIFICIAL INTELLIGENCE IN AVIATION: A REVIEW OF AI SYSTEMS |
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ICAS2024_0402: V. Nugnes¹, C. Varriale, TU Delft, Italy; P. Ratei¹, P. Shiva Prakasha¹, B. Nagel¹; ¹DLR, Italy A SYSTEM OF SYSTEMS AIRCRAFT DESIGN FRAMEWORK: DEMONSTRATION USING A SEAPLANE TRANSPORT NETWORK IN THE GREEK ISLANDS |
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ICAS2024_0413: P.W. Jansen¹, R.E. Perez¹, J.C.-H. Wang, Ribbit Inc, Canada; ¹Royal Military College of Canada, Canada SYSTEM OF SYSTEMS ANALYSIS OF AUTONOMOUS AIRCRAFT OPERATIONS IN AIR CARGO FEEDER NETWORKS |
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ICAS2024_0510: F. During¹, R.C. Munjulury¹, R. Hällqvist, System Simulation and Concept Development, Saab Aeronautics, Sweden; ¹FLUMES, Linköping University, Sweden AUTOMATION OF ENGINEERING INTEROPERABILITY FOR AIRCRAFT SYSTEM DESIGN |
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ICAS2024_0514: P. Krus, Linköping University, Sweden LARGE LANGUAGE MODEL IN AIRCRAFT SYSTEM DESIGN |
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ICAS2024_0550: X. Li¹, L. Deng¹, Y. Ge¹, Y. Pei¹, Y. Gu², L. Cao², A. Shi¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China; ²Shanghai Electro-Mechanical Engineering Institute, China RESEARCH ON ROUTE PLANNING METHOD FOR UAV SWARM AREA COVERAGE MISSIONS BASED ON COMPLEX NETWORKS |
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ICAS2024_0554: S. Sinha Roy¹, Y. Huang¹, D. Bekdache¹, T.-Y. Fung¹, B. Beck¹, C. Guariniello¹, D. DeLaurentis¹; ¹Purdue University, United States FROM ONTOLOGY TO SYSTEM ARCHITECTURE: AN MBSE APPROACH TOWARD THE REALIZATION OF URBAN AIR MOBILITY |
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ICAS2024_0603: C. Mirabella¹, M. Tuccillo¹, P. Della Vecchia¹; ¹Università degli Studi Federico II, Italy A MODEL BASED SYSTEM ENGINEERING APPROACH TOWARDS AIRCRAFT DIGITAL CERTIFICATION |
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ICAS2024_0729: M.M. Alexiev¹, R.E. Perez¹, P.W. Jansen¹, J.C.-H. Wang, Ribbit Inc., Canada; ¹Royal Military College of Canada, Canada MODELING CARGO DEMAND FOR REGIONAL AIR TRANSPORT NETWORKS IN CANADA AND THE UNITED STATES |
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ICAS2024_0843: Z. Cui¹, M. Luo¹, J. Lu¹, J. Wang¹; ¹Beihang University, China A SEMANTIC MODEL-BASED SYSTEMS ENGINEERING APPROACH FOR SUPERSONIC BUSINESS JET CONCEPTUAL DESIGN |
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ICAS2024_0860: A. Dagna¹, S. Centomo², E. Brusa¹, C. Delprete¹, R. Gentile²; ¹Politecnico di Torino, Italy; ²Leonardo LABS, Leonardo S.p.A., Italy AUTOMATIC SYSTEM REQUIREMENTS VERIFICATION FOR THE MBSE-ORIENTED AIRCRAFT DESIGN PROCESS |
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ICAS2024_0869: T. Stefani¹, J.M. Christensen¹, E. Hoemann¹, A. Anilkumar Girija¹, F. Köster, DRL, Germany; T. Krüger¹, S. Hallerbach¹; ¹DLR, Germany APPLYING MODEL-BASED SYSTEM ENGINEERING AND DEVOPS ON THE IMPLEMENTATION OF AN AI-BASED COLLISION AVOIDANCE SYSTEM |
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ICAS2024_0962: Y.-Z. Wang¹, B.-L. Shang¹, P.-F. Li¹, W.-Z. Liu¹, R.-X. Lin¹, K.-A. Xing¹, Y.-T. Deng¹; ¹School of Aeronautics, Northwestern Polytechnical University, China EFFECTIVENESS EVALUATION METHOD FOR AVIATION EMERGENCY RESCUE SYSTEM OF SYSTEMS BASED ON EFFECT CHAIN |
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ICAS2024_1116: I. Kute¹, J. Dagli¹, E. Khot¹, R. Verma¹, P. Gupta¹, D. Shukla¹, R. Pant¹; ¹Indian Institute of Technology Bombay, India, India AN AUTONOMOUS SYSTEM FOR DOCKING AND BATTERY SWAPPING IN UAVS |
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ICAS2024_1138: P. Shiva Prakasha¹, N. Naeem¹, K. Amadori, SAAB Aeronautics, Sweden; G. Donelli¹, J. Akbari¹, F. Nicolosi, UNINA, Italy; L. Knöös Franzen, Linkoping University, Sweden; M. Ruocco, Smartup Engineering, Italy; T. Lefebvre, The French Aerospace Lab, France; B. Nagel¹; ¹German Aerospace Center - DLR, Germany COLOSSUS EU PROJECT – COLLABORATIVE SOS EXPLORATION OF AVIATION PRODUCTS, SERVICES AND BUSINESS MODELS: OVERVIEW AND APPROACH |
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ICAS2024_1139: M. Fouda¹, L. Willrodt¹, H. Almeida¹, J. Cortez¹, O. Hussein¹, F. Castaneda¹, H. Dhouib¹, C. Dahik¹, V. Drouet¹, R. Brook¹; ¹Capgemini Engineering, Germany AN MBSE ENABLED MDAO APPROACH FOR THE CONCEPTUAL DEVELOPMENT OF COMPLEX SYSTEMS |
3.1 - Aerodynamics – CFD Methods and Validation |
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ICAS2024_0031: J. Jiménez-Varona¹, G. Liaño¹; ¹INTA, Spain GRID EFFECT ON M823 BOMB AT TRANSONIC REGIME |
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ICAS2024_0035: H. Qiao¹, F. Qin¹, S. Deng¹; ¹Nanjing University of Aeronautics and Astronautics, China A NUMERICAL VIRTUAL FLIGHT PLATFORM DEVELOPMENT AND ITS APPLICATION ON HIGH MANEUVERABILITY FLIGHT VEHICLES |
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ICAS2024_0062: A.-R. Hübner¹, J. Kirz¹, K. Weinman¹; ¹German Aerospace Center (DLR), Germany APPLICATION OF DIFFERENT NUMERICAL TOOLS AND NUMERICAL METHODS FOR PREDICTION OF HEAT EXCHANGER RAMAIR-CONCEPTS FOR HYBRID ELECTRIC PROPULSION AIRCRAFT CONFIGURATIONS |
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ICAS2024_0078: L.V. Rezende Sanches, Universidade Federal do Paraná, Brazil; G.L. Olichevis Halila¹, F. Issamu Kitadani Odaguil¹, J.L.F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil; ¹Embraer, Brazil ADJOINT-BASED TRANSONIC WING AERODYNAMIC SHAPE OPTIMIZATION INVESTIGATIONS |
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ICAS2024_0081: M. Choudhari¹, E. Beyak¹, N. Hildebrand¹, F. Li¹, E. Vogel¹, P. Paredes, National Institute of Aerospace, United States; V. Srivastava², B. Venkatachari²; ¹NASA Langley Research Center, United States; ²Analytical Mechanics Associates, United States TRANSITION MODELING IN SUPPORT OF CFD VISION 2030 - HIGHLIGHTS OF RECENT EFFORTS AT THE NASA LANGLEY RESEARCH CENTER |
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ICAS2024_0104: M. Turner¹, J. Sharpe¹, M. Kopacz¹, D. Standingford¹, C. Sequeira², B. Sanby², C. Rider²; ¹Zenotech, United Kingdom; ²Flare Bright, United Kingdom VALIDATION OF CFD-BASED DATA SERVICE FOR DRONE INSPECTION OF WIND FARMS WITH FLIGHT TEST DATA |
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ICAS2024_0124: S.S. Chauhan¹, G. Padovany da Silva, Universidade Federal do Parana, Brazil; G.L. Olichevis Halila, Embraer, Brazil; J.R.R.A. Martins¹, J.L.F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil; ¹University of Michigan, United States INVESTIGATING THE INFLUENCE OF AN INBOARD PROPELLER’S VERTICAL OFFSET ON A TRAILING WING’S LIFT AND DRAG DISTRIBUTIONS |
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ICAS2024_0181: A.C.N. Carloni, Instituto Tecnológico de Aeronáutica, Brazil; J.L.F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil DATA-DRIVEN UNSTEADY AERODYNAMIC MODELS FOR AEROELASTIC STABILITY ANALYSES |
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ICAS2024_0197: G. Sharma¹, T.H. Tran, Le Quy Don Technical University, Vietnam; J. Tanimoto¹; ¹Kyushu University, Japan APPLICATION OF CONVOLUTIONAL NEURAL NETWORKS IN DETERMINING THE VELOCITY AND PRESSURE FIELDS AROUND AIRFOIL MODELS |
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ICAS2024_0205: Q. Nguyen Dinh¹, H. Tran The¹, G. Sharma², J. Tanimoto²; ¹Le Quy Don Technical University, Vietnam; ²Kyushu University, Japan APPLICATION OF ARTIFICIAL NEURAL NETWORK (ANN) FOR PREDICTION OF DRAG COEFFICIENT OF AXISYMMETRIC BOATTAIL MODELS |
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ICAS2024_0243: Y. Luo, China; L. Wang, China; J. Wang, China; X. Lang, China; X. Yang, China NUMERICAL SIMULATION STUDY ON THE INFLUENCE OF WING SPACING OF DRAGONFLY-INSPIRED FLAPPING WINGS |
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ICAS2024_0247: M. Carlsson¹, P. Eliasson¹, P. Weinerfelt¹; ¹Saab, Sweden ENHANCING EFFICIENCY FOR UNSTEADY CFD COMPUTATIONS IN AERONAUTICS |
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ICAS2024_0276: Q. Li¹, X. Yang², W. Dong¹, Y. Du²; ¹Shanghai Jiao Tong University, China; ²China Aerodynamics Research and Development Center, China KINETIC MONTE CARLO BASED CATALYTIC VISCOUS WALL BOUNDARY MODELING IN CFD SIMULATION OF HIGH-ENTHALPY NON-EQUILIBRIUM FLOW |
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ICAS2024_0283: P. Raj, Virginia Tech, United States EFFECTIVENESS OF CFD FOR AIRCRAFT DESIGN: STATUS AND PROSPECTS |
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ICAS2024_0309: M. De Rosa¹, A. Glorioso¹, G. Pezzella¹, A. Viviani¹; ¹University of Campania, Italy AERODYNAMICS AND AEROACOUSTIC ANALYSIS OF A SUPERSONIC SLENDER-BODY GEOMETRY |
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ICAS2024_0311: B. Guo¹, Y.F. Lu¹, B. Wang, Chinese Academy of Military Science, China; Z. Guo¹, G.W. Jia¹, D.N. Liu¹; ¹National University of Defense Technology, China SEPARATION SAFETY ANALYSIS IN VARIABLE LAUNCH CONDITION OF SMALL AIR-LAUNCHED UAVS BASED ON NUMERICAL SIMULATION AND FLIGHT TEST |
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ICAS2024_0327: S. Shahjahan¹, B. Emmerson¹, D. Verstraete¹; ¹The University of Sydney, Australia ON THE CHOICE OF TURBULENCE MODEL FOR THE SIMULATION OF AIRFOILS AT REYNOLDS NUMBER BELOW 200,000 |
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ICAS2024_0354: N. Verde, Italy; F. Capoluongo, Italy; P. Catalano, CIRA, Italy; G. Pezzella, University of Campania , Italy; A. Viviani, University of Campania, Italy FLUIDODYNAMIC ANALYSIS OF LOW REYNOLDS NUMBER FLOWS |
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ICAS2024_0363: F. Cascone¹, P. Roncioni¹, O. Russo¹, M. Marini¹, S. Di Benedetto¹, M. Albano², R. Bertacin², G. Ranuzzi²; ¹CIRA, Italy; ²ASI, Italy LAUNCH SYSTEM ASSESSMENT OF AN EXPERIMENTAL HYPERSONIC SCRAMJET VEHICLE |
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ICAS2024_0463: M. Panagopoulos¹, N.J. Lawson¹, D.M. D’Alessandro¹, E. Kearns¹; ¹University of Syndey, Australia COMPUTATIONAL FLUID DYNAMICS ANALYSIS OF A DIRECT AIR CAPTURE FILTER SYSTEM |
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ICAS2024_0465: J.R.R.A. Martins¹, M.A.S. Abdul-Kaiyoom¹, E.J. Adler¹, A.C. Gray¹, H. Hajdik¹, E. Jonsson¹, A.H.R. Lamkin¹, B. Pacini¹, A. Yildirim¹; ¹University of Michigan, United States SHAPING SUSTAINABLE AVIATION WITH CFD-BASED DESIGN OPTIMIZATION |
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ICAS2024_0502: J. Pauen¹, S. Unterstrasser¹, A. Stephan¹; ¹DLR, Germany TOWARDS REFINED CONTRAIL SIMULATIONS OF FORMATION FLIGHT SCENARIOS |
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ICAS2024_0506: B. Isnard¹, G. Tanguy¹, D. Farcy¹, E. Garnier¹, J.-M. Foucault, LMFL, France; ¹ONERA, France IDENTIFICATION METHOD OF LONGITUDINAL COEFFICIENTS BASED ON THE NUMERICAL STUDY OF THE FLOW TOPOLOGY AROUND THE SACCON GEOMETRY |
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ICAS2024_0531: M. Jian¹, Y. Xiao¹, X. Cheng¹, W. Dong¹; ¹Shanghai Jiao Tong University, China CONJUGATED HEAT TRANSFER SIMULATION OF BUOYANCY-INDUCED FLOW AND HEAT TRANSFER MECHANISMS IN A COMPRESSOR CAVITY |
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ICAS2024_0537: S. Chen¹, Z. Guo¹, G. Jia¹, D. Liu¹; ¹National University of Defense Technology, China AERODYNAMIC CHARACTERISTICS RESEARCH OF A DISTRIBUTED PROPULSION AIRCRAFT |
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ICAS2024_0556: H.Y. Wang¹, C.T. Mutasa¹, Z.L. Chen¹; ¹Northwestern Polytechnical University, China NUMERICAL STUDIES ON NOISE-SHIELDING EFFECTS OF A BLENDED-WING-BODY AIRCRAFT USING BOUNDARY ELEMENT METHOD |
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ICAS2024_0558: J.M. Kirkness-Duncombe¹, N.J. Lawson¹, G.A. Vio², S.D. Moss², D.J. Munk²; ¹The University of Sydney, Department of Aeronautical Engineering, Australia; ²Defence Science and Technology Group, Aerospace Division, Australia AEROACOUSTIC CAVITY FLOW ENERGY HARVESTING |
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ICAS2024_0576: P. Lu¹, Y. Xi¹, J. Sun¹, S. Fu¹; ¹Tsinghua University, China STABILITY CHARACTERISTICS OF CROSSFLOW MODES IN HYPERSONIC BOUNDARY LAYER WITH EXPANSION CORNER |
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ICAS2024_0579: D.F. Kurtulus¹, B. Anilir¹, D. Raymer, Conceptual Research Corporation, United States; ¹METU, Turkey ON THE AERODYNAMIC CHARACTERISTICS OF CRESCENT WING |
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ICAS2024_0581: D. Di Pasquale¹, T. Tarun, Indian Institute of Technology(BHU) , India; S. Shubham¹, S.A. Prince¹, A. Proenca¹; ¹Cranfield University, United Kingdom COMPUTATIONAL ANALYSIS ON THE EFFECTS OF LEADING EDGE TUBERCLES ON THE PERFORMANCE OF ROTATING PROPELLER |
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ICAS2024_0583: G. Yang, University of Bristol, United Kingdom JET NOISE ABATEMENT VIA SURROGATE MODEL-BASED AEROACOUSTIC OPTIMISATION USING LARGE EDDY SIMULATION |
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ICAS2024_0607: C.-P. Liu¹, W.-P. Song¹, S.-Q. Han, Sichuan University, China; Z.-H. Han¹; ¹Northwestern Polytechnical University, China EFFECTS OF GEOMETRY PARAMETERS ON AERODYNAMIC CHARACTERISTICS OF ROTOR AIRFOIL IN REVERSE FLOW |
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ICAS2024_0618: H. Zeng¹, Z.-H. Han¹, C.-Z. Xu¹, Y. Zhang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China A SEQUENTIAL LOCAL ENUMERATION-BASED IMPROVED LATIN HYPERCUBE SAMPLING METHOD FOR BALLISTIC CONSTRAINT DESIGN SPACE |
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ICAS2024_0641: Q. Li¹, G. Wang¹, M. Qin¹, L. Xu¹; ¹Northwestern Polytechnical University, China NUMERICAL STUDY OF FLOWS OVER LAUNCH VEHICLES WITH VARIOUS FAIRING BY SECOND-MOMENT CLOSURE DETACHED-EDDY SIMULATION |
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ICAS2024_0644: Z. Han¹, Z.-H. Li, National Laboratory for Computational Fluid Dynamics, China; S.-Y. Chu¹, W.-Y. Cheng¹, C.-S. Wang¹; ¹Aviation Industry Development Research Center of China, China ANALYSIS ON COMPLEX HYPERSONIC FLOW DURING THE REENTRY OF EXPIRED SPACECRAFT |
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ICAS2024_0676: E. Levati¹, C. Pasquali¹, G. Bernardini¹, M. Gennaretti¹; ¹Roma Tre University, Italy A BOUNDARY INTEGRAL EQUATION FORMULATION FOR POTENTIAL COMPRESSIBLE FLOWS AROUND DEFORMABLE BODIES |
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ICAS2024_0681: H. Wu¹, W. Song¹, H. Nie¹, Z. Han¹; ¹National Key Laboratory of Aircraft Configuration Design, China BOUNDARY-LAYER SUCTION AND AERODYNAMIC SHAPE OPTIMIZATION FOR HYBRID LAMINAR FLOW CONTROL ON A FIN |
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ICAS2024_0694: C. Wang¹, P. Li¹, L. He¹, G. Li¹, H. Dai¹; ¹Chinese Aeronautical Establishment, China A HIGH-PRECESION PSEUDO ARC-LENGTH METHOD WITH POSITIVE VALUE PRESERVATION PROPERTIES BASED ON TV SPLITTING |
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ICAS2024_0704: L.-Y. Huang¹, X. Zhao¹, X.-C. Li, Nanjing University of Aeronautics and Astronautics, China; ¹School of Aeronautics, Northwestern Polytechnical University, Xi, China ANALYSIS OF AERODYNAMIC INTERFERENCE CHARACTERISTICS AND AEROACOUSTICS FOR HIGH-SPEED COMPOSITE HELICOPTER IN HOVER |
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ICAS2024_0709: L. Jin¹, G. Feng¹, L. Wu¹; ¹Overall Technology R&D Department, AVIC Aerospace Life-support I, China RESEARCH ON AIRSPEED CORRECTION TECHNOLOGY OF EJECTION SEAT BASED ON CFD |
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ICAS2024_0752: Y.-Y. Guo¹, W.-Q. Yang¹, J.-L. Xuan¹, W. Wang¹, D. Xue¹; ¹Northwestern Polytechnical University, China THE EFFECTS OF INITIAL STRESS ON AERODYNAMIC PERFORMANCE OF FLEXIBLE MEMBRANE-SKELETON WINGS WITH FSI SIMULATION |
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ICAS2024_0783: Z.K. Liu¹, Y.L. Liu¹, Q.Z. Li¹, G. Wang¹; ¹Northwestern Polytechnical University, China NUMERICAL INVESTIGATION OF THE INTERACTION OF OPPOSING JETS AND SUPERSONIC FREE FLOWS |
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ICAS2024_0791: J.L. Kurniawan¹, M. Hu¹; ¹Institut Teknologi Bandung, Indonesia SURROGATE MODELING OF VORTEX SHEDDING TURBINE IN LOW REYNOLDS NUMBER |
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ICAS2024_0822: M. Zieher¹, D. Sedlacek¹, C. Breitsamter¹; ¹Technical University of Munich, Germany ASSESSMENT OF AN ADAPTIVE ONE-EQUATION TURBULENCE MODEL FOR LEADING-EDGE VORTEX FLOWS ON MULTIPLE SWEPT DELTA WINGS |
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ICAS2024_0823: C. Sebastia Saez¹, J. Martin Ferres¹, M. Hornung¹; ¹Technical University of Munich, Germany NUMERICAL ANALYSIS OF GENERALIZED AERODYNAMIC FORCES CONSIDERING LAMINAR-TURBULENT TRANSITION ON A NLF WING |
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ICAS2024_0824: A. Lopez¹, G. Magrì², U. Cella¹, G. Urso, RBF Morph srl, Italy; F. Della Barba², M.-E. Biancolini¹; ¹Università di Roma Tor Vergata, Italy; ²Università degli studi di Padova, Italy EFFICIENT SHAPE OPTIMIZATION IN AERONAUTICS: INTEGRATING PARAMETRIC CAD AND MESH MORPHING FOR ENHANCED AERODYNAMIC PERFORMANCE |
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ICAS2024_0863: G. Barbato¹, G. Pezzella¹, A. Viviani¹; ¹Università della Campania Luigi Vanvitelli, Italy PRELIMINARY DESIGN OF A FIXED-WING DRONE FOR MARS EXPLORATION ACTIVITIES |
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ICAS2024_0864: S.M. Giannino¹, G. Pezzella¹, A. Viviani¹; ¹Università della Campania Luigi Vanvitelli, Italy LOW SPEED AERODYNAMICS OF SIX OPTIMISED UNCONVENTIONAL RE-ENTRY VEHICLE AEROSHAPES |
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ICAS2024_0872: D. Ninni¹, F. Bonelli¹, A. Laricchiuta², G. Colonna², G. Pascazio¹; ¹Politecnico di Bari, Italy; ²CNR ISTP Bari, Italy ASSESSMENT OF A MACROSCOPIC MODEL FOR THE AEROTHERMODYNAMICS CHARACTERIZATION OF ICE GIANTS ATMOSPHERIC ENTRY |
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ICAS2024_0877: A. Assonitis¹, R. Paciorri ¹, V. Orlandini¹, A. Neri, ESA ESRIN, Italy; ¹University of Rome La Sapienza , Italy AERO-THERMAL ANALYSIS OF A REUSABLE LAUNCH VEHICLE DURING RE-ENTRY MANOEUVRER |
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ICAS2024_0904: M. Niu, Northwestern Polytechnical University, China; F. Sun, Xi'an Modern Control Technology Research Institute, China; C. Du, AVIC XAC COMMERCIAL AIRCRAFT CO., LTD., China; H. Huang, Northwestern Polytechnical University/Aircraft Strength Reserch , China HYDRODYNAMIC ANALYSIS OF STATIC WATER IMPACT ON WEDGE-SHAPED HULL WATERTIGHT TEST SPECIMEN THROUGH NUMERICAL ANALYSIS |
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ICAS2024_0907: C.-S. Dikmen¹, M.-N. Yüksel¹, M. Yumusak¹; ¹Roketsan, Turkey NUMERICAL INVESTIGATION OF HYPERSONIC FLOWS |
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ICAS2024_0925: H. Zhang¹, J. Chen², F. Wang¹, G. Zhang¹, Z. Shen, Aircraft Strength Research Institute of China, China; Q. Zhu, China Special Vehicle Research Institute, China; G. Wu, Commercial Aircraft Corporation of China Ltd, China; M. Tong²; ¹Jinling Institute of Technology, China; ²Nanjing University of Aeronautics and Astronautics, China SCALE EFFECT ON WATER LANDING PERFORMANCE OF AMPHIBIOUS AIRCRAFT |
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ICAS2024_0929: J.-Y. Li¹, X.-Y. Wang, Shanghai Electro-Mechanical Engineering Institute, China; J.-C. Chen¹, J. Jiao, China Special Vehicle Research Institute, China; M.-B. Tong¹, C.-L. Yan, Beijing University Of Aeronautics And Astronautics, China; ¹Nanjing University Of Aeronautics And Astronautics, China ANALYSIS OF SUCTION FORCE EFFECT ON DIFFERENT FUSELAGE SHAPE DURING THE WATER DITCHING |
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ICAS2024_0930: F. Rossetti¹, L. Pirillo¹, M. Cimini, ENEA, Italy; M. Bernardini¹, F. Stella¹; ¹Sapienza University, Italy NUMERICAL INVESTIGATION ON THE LIQUID SLOSHING DAMPING INSIDE A TANK WITH A FLEXIBLE ANTI-SLOSHING DEVICE |
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ICAS2024_0952: F. Duan¹, J.-Y. Li¹, Z.-D. Li, Aerospace Life-support Industries Ltd, China; M.-B. Tong¹; ¹Nanjing University of Aeronautics and Astronautics, China RESEARCH ON AERODYNAMIC PERFORMANCE OF OVERSIZE MODULAR PARAFOIL IN RANDOM WIND FIELD |
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ICAS2024_1004: M.V.G. Muniz¹, J.A.A. Lyrio, Aeronautics Institute of Technology, Brazil; J.L.F. Azevedo¹; ¹Institute of Aeronautics and Space, Brazil LINEAR SYSTEM TECHNIQUES APPLIED TO NONLINEAR AEROSERVOELASTIC ANALYSES |
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ICAS2024_1009: R. Navarro¹, L.M. García-Cuevas¹, J. García-Tíscar¹, F.N. Ramírez¹; ¹Universitat Politècnica de València, Spain PERFORMANCE AND ACOUSTIC ANALYSIS OF A DISTRIBUTED ELECTRIC PROPULSION UNMANNED AIRCRAFT |
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ICAS2024_1026: P. Roncioni¹, M. Marini¹, R. Fusaro², N. Viola², D. Pepelea, INCAS, Romania; B. Cakir, VKI, Belgium; M. Clay, REL, United Kingdom; ¹CIRA, Italy; ²POLITO, Italy AERODYNAMIC NUMERICAL/EXPERIMENTAL COMPARISON OF A HYPERSONIC TEST VEHICLE IN MORE&LESS PROGRAM |
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ICAS2024_1033: M. Nemati¹, A. Jahangirian¹; ¹amirkabir university of technology, Iran MACHINE LEARNING INTEGRATION IN COMPUTATIONAL FLUID DYNAMICS FOR RAPID FLOW FIELD PREDICTION |
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ICAS2024_1048: L. Pinelli¹, M. Marconcini¹, A. Arnone ¹, D. Bacci, Oxford Thermofluids Institute, University of Oxford, United Kingdom; ¹Department of Industrial Engineering, University of Florence, Italy HIGH FIDELITY MODELING OF ACOUSTIC LINERS FOR AERONAUTICAL APPLICATIONS |
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ICAS2024_1084: J. Parez¹, P. Kovar¹, T. Vampola¹; ¹Czech Technical University in Prague, Czech Republic PREDICTION OF TRANSIENT DEFORMATION BY COUPLING CFD AND FEM ANALYSIS USING MACHINE LEARNING BASED CORRELATION FUNCTION |
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ICAS2024_1112: J.R. Teixeira Da Silva¹, M.E.M.C. Lopes¹, A.P.R. Preguica¹, C.F. Rafael¹, P.C. Souza Villela¹, G.A. Lima da Silva, Aerothermal Solutions and Software Distributor LLC, United States; H. Jasak, Cambridge University, United Kingdom; ¹ATS Aerothermal Solutions, Brazil INITIAL DEVELOPMENT OF A CFD ICING TOOL |
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ICAS2024_1175: R.O. Bura, Republic Indonesia Defense University, Indonesia; A. Riyadl, National Research and Innovation Agency, Indonesia DETACHED EDDY SIMULATION OF HYPERSONIC SHOCK-WAVE/BOUNDARY-LAYER INTERACTIONS ON HIFIRE-1 AXISYMMETRIC CONE-CYLINDER-FLARE |
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ICAS2024_1178: E. Malof¹, J. Bayandor¹; ¹University at Buffalo CRASH Lab, United States FLUID-SOLID INTERACTIVE MODELLING OF FABRIC-BASED ATMOSPHERIC ENTRY SIZED AERODYNAMIC DECELARATORS |
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ICAS2024_1179: J.G. Coder, Pennsylvania State University, United States EVALUATION OF CFD TRANSITION MODELING FOR TRANSONIC, NATURAL-LAMINAR-FLOW DESIGN |
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ICAS2024_1181: F.B. Oliveira, Instituto Tecnologico de Aeronautica, Brazil; J.L.F. Azevedo, Instituto de Aeronautica e Espaco, Brazil; Z.J. Wang, University of Kansas, United States ANALYSIS OF THE R FAMILY OF LIMITERS APPLIED TO HIGH-ORDER FR/CPR SCHEMES FOR THE SIMULATION OF SUPERSONIC FLOWS |
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ICAS2024_1190: T. Chagas Silva, Instituto Tecnológico de Aeronáutica, Brazil; J.L.F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil ASSESSMENT OF EXPLICIT ALGEBRAIC REYNOLDS STRESS MODELS APPLIED TO AERONAUTICAL FLOWS |
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ICAS2024_1197: G. Gori¹, A. Zanotti¹; ¹Department of Aerospace Science and Technology, PoliMI, Italy UNCERTAINTY ANALYSIS OF THE AERODYNAMIC PERFORMANCE OF EVTOL PROPELLERS VIA REYNOLDS STRESS TENSOR PERTURBATION |
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ICAS2024_1198: S.E. Monroe, Clarkson University, United States PARELLEL UNSTEADY REYNOLDS-AVERAGED NAVIER-STOKES (URANS) STUDEIS OF THE PERFORMANCE OF ONR WATERJET AXWJ-2 |
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ICAS2024_1313: P. Raj, United States EFFECTIVENESS OF CFD FOR AIRCRAFT DESIGN: STATUS AND PROSPECTS PART 2 |
3.2 - Experimental Aerodynamics |
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ICAS2024_0023: C.O.L. Hamilton Smith¹, N.J. Lawson¹; ¹The University of Sydney, Australia HOT-WIRE ANEMOMETRY OF THE BOUNDARY LAYER PRIOR TO A CAVITY IN RESPONSE TO VARIED UPSTREAM GEOMETRY |
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ICAS2024_0070: N. Menakath¹, N.J. Lawson¹, G.A. Vio, Defence Science and Technology Group, Australia; ¹The University of Sydney, Australia SURFACE VISUALISATION OF TIME AVERAGED FLOW BEHAVIOUR AROUND RIGID AND FLEXIBLE HEMISPHERES UTILISING UV SENSITIVE OIL |
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ICAS2024_0218: D. Damljanovic¹, D. Vukovic¹, L. Petrovic¹; ¹Military Technical Institute, Serbia REVITALIZATION OF A FLOW-CELL DEVICE FOR AIR INTAKE TESTING AND ITS INTEGRATION WITH WIND TUNNEL SYSTEMS |
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ICAS2024_0219: R. Bardera¹, A.A. Rodríguez-Sevillano², J.C. Matías¹, E. Barroso¹, M. Ojeda², J. Fernández²; ¹Instituto Nacional de Técnica Aeroespacial (INTA)., Spain; ²Escuela Técnica Superior de ingeniería Aeronáutica y del Espacio, Spain EXPLORING WINGTIP COLUMNAR VORTEX GENERATORS FOR UAV PERFORMANCE ENHANCEMENT |
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ICAS2024_0257: R. Bardera¹, J.C. Matias¹, E. Barroso¹; ¹Instituto Nacional de Técnica Aeroespacial, Spain PIV AND AERODYNAMIC FORCES ANALYSIS OF A HELICOPTER OPERATING AROUND A BUILDING BY WIND-TUNNEL EXPERIMENTS |
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ICAS2024_0390: N. Cao Van¹, H. Itoh¹, M. Mizoguchi¹, A. Uenaka¹; ¹National Defense Academy of Japan, Japan ELECTRIC FIELD MEASUREMENT IN GLOW DISCHARGE PLASMA INTERACTING WITH SHOCK WAVE IN HYPERSONIC FLOW |
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ICAS2024_0412: V. Gollnick¹, J. Luehrmann¹, F. Danquah¹, A. Semke¹, T. Mueller¹, J. Thoeben¹; ¹Hamburg University of Technology, Germany ANALYSIS OF AN ELECTRICAL-POWERED-DUCTED-THRUST VECTORING-FLAP |
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ICAS2024_0447: G. Fasulo¹, L. Federico¹; ¹Italian Aerospace Research Centre (CIRA), Italy ASSESSING THE SONIC BOOM OF A FULL-SIZE AIRCRAFT FROM FREE FLIGHT TESTS ON A SUB-SCALE MODEL |
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ICAS2024_0456: B. Ilic¹, G. Ocokoljic¹, M. Samardžic¹, J. Isakovic, Academy of Applied Technical Studies, Serbia; ¹Military Technical Institute, Serbia UPGRADE OF THE VTI T-38 BLOWDOWN TRISONIC TEST FACILITY: WIND TUNNEL CONTROL SYSTEM |
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ICAS2024_0526: Y.-F. Wang¹, B.-F. Song¹, Y. Luo¹, X.-Y. Lang¹, W. Wang¹; ¹Northwestern Polytechnical University, China INFLUENCE OF REINFORCED TRAILING EDGE ON FLAPPING WING AERODYNAMIC FORCE AND DEFORMATION |
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ICAS2024_0540: J. Yuan¹, S. Yu¹, Z. Qian¹; ¹AVIC Aerodynamics Research Institute, China EFFECT OF FREESTREAM DISTURBANCES ON BOUNDARY LAYER TRANSITION IN HYPERSONIC WIND TUNNEL |
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ICAS2024_0549: N. Kishimoto, Kwansei Gakuin University, Japan; D. Wada¹, M. Tamayama¹, Y. Iwami², N. Tomita², T. Ikeda³, Y. Tanahashi³, K. Katagiri, Hiroshima University, Japan; ¹JAXA, Japan; ²Yamashina Institute of Ornithology, Japan; ³Chubu University, Japan EVALUATION OF WIND TUNNEL TEST RESULTS OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) |
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ICAS2024_0710: P. Hartl¹, M. Ritschel¹, M. Braune¹, H. Mai¹; ¹German Aerospace Center (DLR), Germany EXPERIMENTAL INVESTIGATION OF THE DLR-F23 CONFIGURATION AT TRANSONIC SPEEDS USING FAST-RESPONSE PRESSURE-SENSITIVE PAINT |
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ICAS2024_0757: M. Avirovic¹, C. Brunelli¹, K. Wykes², C. Mengdehl², B.G. Marinus¹, J. Degroote, University of Ghent, Belgium; J. Van Beeck, Von Karman Institute for Fluid Dynamics, Belgium; ¹Royal Military Academy, Belgium; ²Stemme Belgium, Belgium DESIGN OF MEASUREMENT SETUP FOR HIGH-ALTITUDE IN-FLIGHT EXPERIMENTS ON DU89-134/14 AIRFOIL AT LOW REYNOLDS NUMBER |
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ICAS2024_0790: Y. Liu¹, J. Xiao¹, N.A. Benai-dara¹, Z. Chen¹, N. Qin, University of Sheffield, United Kingdom; ¹NUAA, China EXPERIMENTAL AND NUMERICAL INVESTIGATION ON AERODYNAMIC PERFORMANCE OF A MARS ROTOR SYSTEM |
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ICAS2024_0812: C.P. Li, China; G. Zhang, China; N. Liu, China; Y. Zhang, China; L. Xu, China; M. Wang, China DESIGN OF DUAL-FUSELAGE FLIGHT PLATFORM FOR JET CONTROL FUNCTION VERIFICATION |
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ICAS2024_0840: S. Takaya¹, K. Shibata¹, D. Numata¹; ¹Tokai University, Japan DEVELOPMENT OF UNSTEADY PRESSURE-SENSITIVE PAINT FOR LOW REYNOLDS NUMBER WIND TUNNEL TESTS IN LOW-PRESSURE ENVIRONMENTS |
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ICAS2024_0853: K. Bantscheff¹, F. Santelli¹, C. Breitsamter¹; ¹Technische Universität München / Lehrstuhl für Aerodynamik, Germany EXPERIMENTAL AND NUMERICAL INVESTIGATION OF A STRUCTURAL-DYNAMICALLY SCALED DELTA WING WITH TRAINING EDGE FLAPS |
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ICAS2024_0894: D. Guida¹, A. Smoraldi¹, A. Schettino, C.I.R.A., Germany; ¹CIRA Italian Aerospace Research Centre, Italy DESIGN OF A HIGH ENTHALPY HYPERSONIC NOZZLE FOR “GHIBLI” PLASMA WIND TUNNEL |
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ICAS2024_0978: C. Moreira¹, C. Breitsamter¹; ¹Technical University of Munich, Germany AERODYNAMIC INTERACTION EFFECTS OF TILTROTOR EVTOL AIRCRAFT |
3.3 - Basic Fluid Dynamics and Flow Control |
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ICAS2024_0034: R. Yamashita, The University of Tokyo, Japan NUMERICAL SIMULATION OF FLOWS AROUND AN AIRFOIL DURING ACCELERATED AND DECELERATED FLIGHT |
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ICAS2024_0067: A. Shi, China; Y. He, China; E.H. Dowell, United States A BRIEF REVIEW OF PANEL AEROELASTICITY WITH SHOCK INTERACTION |
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ICAS2024_0176: M. Khaled¹, B. Faraji-Tajrishi¹, A. Herrgen, MTU Aero Engines AG, Germany; B. Weigand¹; ¹Institute of Aerospace Thermodynamics, University of Stuttgart, Germany VALIDATION OF MULTIPHASE FLOW SIMULATIONS BY EXPERIMENTAL MEASUREMENTS IN A CHANNEL FLOW |
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ICAS2024_0228: C. Brunelli¹, M. Avirovic¹, B. Janssens¹, B.G. Marinus¹, M. Runacres, Vrije Universiteit Brussel, Belgium; G. May, Von Karman Institute for Fluid Dynamics, Belgium; A. Ecorce², A. Dalbera²; ¹Royal Military Academy, Belgium; ²National Polytechnic Institute of Toulouse , France PASSIVE FLOW CONTROL DEVICES ON LOW-REYNOLDS DU89-134 AIRFOIL |
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ICAS2024_0239: X. Bai, China; B. Mi, China; J. Zhang, China RESEARCH ON UNSTEADY AERODYNAMIC MODELING METHOD OF PREPOSITIVE WING - MAIN WING COMPOSITE SYSTEM AT HIGH ATTACK ANGLE |
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ICAS2024_0282: X.-T. Tan¹, H.-Y. Xu¹, Z. Pei¹; ¹Northwest Polytechnic University, China NUMERICAL INVESTIGATION OF THE FLOW FEATURES ON THE TURRET WITH DIFFERENT CYLINDER HEIGHT IN THE TRANSONIC FLOW |
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ICAS2024_0426: S.-T. Peng¹, F.-Z. Chen¹, H. Yan¹, X.-Q. Sun¹; ¹Northwestern Polytechnical University, China NUMERICAL INVESTIGATION ON THE EFFECT OF REYNOLDS NUMBER ON TANDEM DROPLET |
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ICAS2024_0543: P. Li¹, Z. Cao¹, D. Li¹; ¹Northwestern Polytechnical University, China RESEARCH ON EFFICIENT ACTIVE T-S WAVE GENERATION METHOD IN BOUNDARY LAYER |
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ICAS2024_0553: B.Z. Xu¹, Z.L. Chen¹; ¹Northwestern Polytechnical University, China NUMERICAL STUDY ON ACOUSTIC RECEPTIVITY OF COMPRESSIBLE LAMINAR FLOW OVER A FLAT PLATE WITH MODIFIED SUPER-ELLIPSE LEADING EDGE |
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ICAS2024_0569: Z.Y. Tang, China; H.N. Xu, China; X.Y. Li, China; J. Ren, China WALL TEMPERATURE EFFECTS ON AERODYNAMIC HEATING MECHANISMS IN SHOCK WAVE TURBULENT BOUNDARY LAYER INTERACTION |
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ICAS2024_0574: Y. Xi¹, S. Fu¹; ¹School of Aerospace Engineering, Tsinghua University, China CROSSFLOW AND GÖRTLER INSTABILITIES IN HYPERSONIC BOUNDARY LAYERS |
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ICAS2024_0595: E.A.R. Camacho¹, A.R.R. Silva¹, F.D. Marques, Universidade de São Paulo, Brazil; ¹Universidade da Beira Interior, Portugal MITIGATING DYNAMIC STALL WITH A MOVABLE LEADING-EDGE: THE NACA0012-IK30 WING |
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ICAS2024_0655: X.-L. Li¹, J.-H. Xu¹, W.-P. Song¹, S.-Q. Han, Sichuan University, China; Z.-H. Han¹; ¹ Northwestern Polytechnical University, China NUMERICAL INVESTIGATION ON AERODYNAMIC PERFORMANCE OF HOVERING ROTOR IN GROUND EFFECT |
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ICAS2024_0662: Y.-R. Zhao, China; B.-G. Mi, China; H. Zhan, China; H.-Y. Xu, China FAULT DIAGNOSIS AND TOLERANCE SYSTEM OF FLIGHT STATE PERCEPTION MODEL BASED ON MACHINE LEARNING FOR CO-FLOW JET AIRFOIL |
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ICAS2024_0682: Z. Cao¹, P.F. Li¹, D. Li¹; ¹Northwestern Polytechnical University, China MEASUREMENTS OF T-S WAVES DUE TO ACOUSTIC DISTURBANCES IN EXPERIMENTS |
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ICAS2024_0741: C. Cordoni¹, A. Saporiti¹, M. Boffadossi¹; ¹DAER, Politecnico di Milano, Via La Masa 34, 20156 Milano, Italy, Italy A CFD STUDY OF THE ACTIVE FLOW CONTROL SYSTEM BEHAVIOUR ON A VERTICAL TAIL SECTION OF AN AIRPLANE, WITH THE AID OF AI |
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ICAS2024_0788: N. Wu¹, J.-P. Hu¹, Y.-G. Lyu¹, J. Wang¹, Y. Tan¹, Z.-X. Liu¹; ¹Northwestern Polytechnical University, China STUDY OF THE SCAVENGE PUMP PERFORMANCE FOR TWO-PHASE FLOW IN AN AIRCRAFT ENGINE LUBRICATION SYSTEM |
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ICAS2024_0792: C.Q. Gao, China; K. Ren, China; W.W. Zhang, China ACTIVE-PASSIVE HYBRID CONTROL OF SHOCK BUFFET |
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ICAS2024_0817: Y. Xu¹, Y.-G. lLyu¹, J.-P. Hu¹, Z. Liu¹; ¹Northwestern Polytechnical University, China EXPERIMENTAL STUDY ON MULTI-ATTITUDE OIL SUPPLY STRUCTURE |
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ICAS2024_0849: Y. Yang, Civil Aviation Flight University of China, China; H. Zhang¹, W. Lu, Nanjing Tech University, China; C. Zhang¹, C. Xu¹, G. Huang¹; ¹Nanjing University of Aeronautics and Astronautics, China MECHANISM STUDY ON THE IMPACT OF PULSED JET AT THE BLADE TIP LEADING EDGE ON THE FLOW FIELD IN COMPRESSOR |
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ICAS2024_0870: S. Hayböck¹, C. Breitsamter¹; ¹Technical University of Munich, Germany IMPLEMENTATION OF ACTIVE FLOW CONTROL ON A SHORT-INLET UHBR ENGINE NACELLE |
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ICAS2024_0918: Z.-M. Xu¹, Z.-H. Han¹, H. Nie¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China ON THE INFLUENCE OF BASE FLOW CHARACTERISTICS ON CROSSFLOW INSTABILITY IN SWEPT BOUNDARY LAYERS |
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ICAS2024_0934: H. Zhao¹, D. Zhu¹, S. Wang², S. Chang², L. Yu¹, Y. Wu¹; ¹AVIC Aerodynamics Research Institute, China; ²Beihang University, China STUDY OF DROPLET MOTION AND WATER FILM FLOW CHARACTERISTICS ON SUPERHYDROPHOBIC SURFACES UNDER AIRFLOW SHEARING |
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ICAS2024_0944: J. Hassan ¹, R. Marsilio¹, G.M. Di Cicca¹, M. Ferlauto¹; ¹Dept. of Mech. and Aerospace Engineering, Politecnico di Torino, Italy NUMERICAL STUDY OF THE FLOWFIELD IN A DIFFERENTIALLY-THROTTLED LINEAR AEROSPIKE |
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ICAS2024_0969: R. Haidl¹, B. Weigand¹; ¹Institute of Aerospace Thermodynamics, University of Stuttgart, Germany EXPERIMENTAL SETUP FOR THE INVESTIGATION OF WATER SEPARATION IN ANNULAR FLOW WITHIN A CIRCULAR CHANNEL |
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ICAS2024_0987: V. Prieto, ONERA and ISAE-SUPAERO, France; M. Forte, ONERA, France; E.R. Gowree, ISAE-SUPAERO, France ON THE INFLUENCE OF SURFACE ROUGHNESS ON BOUNDARY-LAYER TRANSITION FOR SWEPT WINGS |
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ICAS2024_0995: O. Avni¹, Y. Dagan¹; ¹Technion - Israel Institute of Technology, Israel NONLINEAR DROPLET DYNAMICS IN IDEALIZED TRAILING VORTICES |
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ICAS2024_1053: P. Scavella¹, G. Paolillo¹, T. Astarita¹, G. Cardone¹, C.S. Greco¹; ¹University of Study of Naples Federico II, Italy NUMERICAL STUDY ON ACTIVE FLOW CONTROL SOLUTIONS FOR HIGH LIFT |
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ICAS2024_1123: E. De Bono, France; A.D. Fernandes, Italy; G. Petrone, Italy; M. Ouisse, France; R. Teloli, Italy; S. De Rosa, Italy ON THE OPTIMIZATION OF (GENERALIZED) IMPEDANCE FOR ACOUSTIC LINERS |
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ICAS2024_1153: H.W.M. Hoeijmakers¹, M.P.J Sanders¹, L.H. Groot Koerkamp¹, A. van Garrel¹, C.H. Venner¹; ¹University of Twente, Netherlands FLYING WING CIRCULATION DISTRIBUTIONS, AERODYNAMIC PERFORMANCE AND WAKE ROLL-UP |
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ICAS2024_1208: E. Saccaggi¹, G.M. Di Cicca¹; ¹Politecnico di Torino, Italy GENETIC ALGORITHM OPTIMIZATION OF AN OPPOSITION CONTROL STRATEGY IN A FULLY TURBULENT CHANNEL FLOW |
3.4 - Applied Aerodynamics |
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ICAS2024_0047: G. Abate¹, H.P. Monner¹; ¹German Aerospace Center (DLR), Germany MORPHING LEADING-EDGE TUBERCLES ON CESSNA 172 WING |
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ICAS2024_0069: R.H. Thomas¹, Y. Guo, NASA Langley Reseach Center, United States; E.H. Nesbitt¹, I.A. Clark¹, J.C. June¹; ¹NASA Langley Research Center, United States REFINED PREDICTIONS COMPARED WITH THE PROPULSION AIRFRAME AEROACOUSTICS AND AIRCRAFT SYSTEM NOISE FLIGHT RESEARCH TEST DATA |
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ICAS2024_0102: T. Streit¹, J. Ruberte Bailo¹, A. Büscher, Airbus Operations GmbH, Germany; A. Seitz¹; ¹DLR (GERMAN AEROSPACE CENTER), Germany DESIGN OF A HIGHLY EFFICIENT TRANSPORT NLF AIRCRAFT WITH A BACKWARD SWEPT WING AND A LONG SINGLE-AISLE FUSELAGE |
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ICAS2024_0116: S. Keye¹, O. Brodersen¹, S. Melber-Wilkending¹; ¹German Aerospace Center (DLR), Germany SUMMARY OF DLR RESULTS FROM THE SEVENTH AIAA DRAG PREDICTION WORKSHOP |
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ICAS2024_0134: H. Pantel¹, F. Falissard¹, G. Dufour, ISAE-SUPAERO, France; ¹ONERA, France SIMULATION OF AN INSTALLED PROPELLER BY MEANS OF STEADY AND UNSTEADY BODY-FORCE MODELING |
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ICAS2024_0158: R.H. Morais¹, L.F. Ferreira Marques, ISEC, Portugal; A. Resende Rodrigues da Silva¹, R. Melicio, LAETA-IDMEC, Instituto Superior Técnico, Universidade de Lisboa, Portugal; ¹LAETA-AEROG, Universidade da Beira Interior, Portugal MODELLING ASTEROID TRAJECTORY IN EARTH’S ATMOSPHERE |
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ICAS2024_0189: N. Mthembu¹, H. Ndlovu¹, B. Ndebele¹, K. Jamison¹, L. Zwane¹; ¹CSIR, South Africa DECOUPLING STORE AND PARENT AERODYNAMICS FOR FAST PREDICTION OF SUBSONIC STORE TRAJECTORIES |
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ICAS2024_0227: H.M. Hajdik¹, A. Yildirim¹, J.R.R.A. Martins¹; ¹University of Michigan, United States AERODYNAMIC SHAPE OPTIMIZATION OF FILLETED INTERSECTIONS WITH SURFACE MESH DEFORMATION |
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ICAS2024_0232: M. Nikbay¹, K. Kontis², H. Aleisa², B. Pirlepeli¹; ¹Istanbul Technical University, United Kingdom; ²University of Glasgow, United Kingdom LOW-SUBSONIC AERODYNAMIC ANALYSES OF A NONPLANAR BWB MODEL: AN EXPERIMENTAL AND CFD STUDY |
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ICAS2024_0264: R.R. Duivenvoorden¹, F. do Nascimento Monteiro¹, T. Sinnige¹; ¹Delft University of Technology, Netherlands EXPERIMENTAL MEASUREMENTS OF SLIPSTREAM DEFORMATION FOR AN INSTALLED DISTRIBUTED PROPELLER CONFIGURATION. |
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ICAS2024_0265: M. Nayman¹, R.E. Perez¹; ¹Royal Military College of Canada, Canada LOCALIZED AERODYNAMIC SHAPE OPTIMIZATION FOR AUTOMOTIVE APPLICATIONS |
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ICAS2024_0293: Y. Tamaki¹, Y. Yokoyama¹, T. Imamura¹; ¹The University of Tokyo, Japan EVALUATING INSTALLATION EFFECTS IN SEMI-SPAN WIND TUNNEL EXPERIMENTS USING CARTESIAN-GRID-BASED FLOW SOLVER UTCART |
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ICAS2024_0298: H. Zhao¹, K.-K. Wang¹, Z.-Y. Gong¹, K.Y. Gan¹; ¹Northwestern Polytechnical University, China NOVEL GRADIENT-ENHANCED MULTI-FIDELITY SURROGATE MODEL ASSISTED ROBUST MULTIDISCIPLINARY DESIGN OPTIMIZATION OF TAILLESS FLYING WING |
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ICAS2024_0319: J. Rasines¹, D. Verstraete¹; ¹The University of Sydney, Australia ON THE CHALLENGES OF SURROGATE-BASED AERODYNAMIC SHAPE OPTIMISATION |
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ICAS2024_0333: R. Addo-Akoto¹, S.-G. Lee¹, J.-S. Han, Chungnam National University, South Korea; J.-H. Han¹; ¹KAIST, South Korea ASPECT RATIO AND ADVANCE RATIO EFFECTS ON AERODYNAMIC CHARACTERISTICS OF FLEXIBLE FLAPPING WINGS |
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ICAS2024_0348: N. Montella, University of Campania/ CIRA, Italy; G.A. Vio, The University of Sydney, Australia; L. Iuspa¹, A. Aprovitola¹, G. Pezzella, University of Campania , Italy; A. Viviani¹; ¹University of Campania, Italy WIND TUNNEL ANALYSIS OF A SPACE RE-ENTRY VEHICLE AT LOW-SPEED CONDITIONS |
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ICAS2024_0361: A. Glorioso¹, F. Petrosino², M. Barbarino², G. Pezzella¹, A. Viviani¹; ¹University of Campania, Italy; ²CIRA, Italy SONIC BOOM ANALYSIS OF DIFFERENT SUPERSONIC AIRCRAFT |
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ICAS2024_0370: F. Nicolosi¹, P. Della Vecchia¹; ¹University of Naples Federico II, Italy WIND-TUNNEL TESTS OF INNOVATIVE TAILPLANE CONFIGURATIONS |
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ICAS2024_0373: S. Wang¹, H. Zhao¹, K. Gan¹, Z. Gong¹, Y. Gan¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China SPARSE POLYNOMIAL CHAOS-BASED SONIC BOOM UNCERTAINTY QUANTIFICATION AND AERODYNAMIC/SONIC BOOM ROBUST DESIGN OPTIMIZATION UNDER MULTI-PARAMETER UNCERTAINTIES |
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ICAS2024_0394: G. Beghetto¹, M. Boffadossi¹; ¹Politecnico di Milano, Italy DESIGN AND AERODYNAMIC OPTIMIZATION OF A THIN-HAUL AIRCRAFT WITH DISTRIBUTED ELECTRIC PROPULSION: ZETHA |
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ICAS2024_0401: V. Orlandini¹, R. Paciorri¹, A. Assonitis¹, A. Bonfiglioli, Università degli Studi della Basilicata, Italy; ¹University of Rome La Sapienza, Italy NUMERICAL STUDY ON THE FIRST-STAGE RE-ENTRY TRAJECTORY USING AN INFLATABLE BALLUTE |
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ICAS2024_0411: D. Skrna, Austria; M. de Rosa Jacinto, Brazil; M. Berens, Germany AEROACOUSTICS INVESTIGATION OF PROPELLER LEADING EDGE TUBERCLES APPLIED TO ADVANCED AIR MOBILITY |
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ICAS2024_0414: C. Graham¹, R.E. Perez¹; ¹Royal Military College of Canada, Canada CHARACTERIZATION OF EXTERNAL LIQUID HYDROGEN TANK INTERFERENCE DRAG |
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ICAS2024_0448: S.-Y. Jin¹, Z.-H. Gao¹, S.-S. Chen¹, Y.-Q. Wang, China Aerodynamics Research and Development Center, China; ¹ Northwestern Polytechnical University, China DATA MINING ANALYSIS ON AERODYNAMIC STEALTH DESIGN PRINCIPLES OF AIRFOIL PROFILES |
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ICAS2024_0449: Y. Li¹, X. Xu¹, Z. Zhou¹, Y. Bai¹, H. Wang¹, B. Xu¹; ¹Northwestern Polytechnical University, China SIMULATION STUDY ON AERODYNAMIC CHARACTERISTICS OF COMBINED LOW ASPECT RATIO UAV |
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ICAS2024_0471: T. Ikeda¹, R. Furuya, Ryoyu Systems, Japan; M. Murayama¹; ¹JAXA, Japan NUMERICAL EVALUATION FOR FAN-NOISE SHIELDING EFFECTS ON AFT-FUSELAGE MOUNTED AND EMBEDDED ENGINES |
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ICAS2024_0473: J. Liu¹, D. Xue¹; ¹School of Aeronautics, Northwestern Polytechnical University, China RESEARCH ON OPTIMAL TORSIONAL DEFORMATION OF FLAPPING WING |
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ICAS2024_0501: L. Manfriani¹, X. Liu¹; ¹ZHAW, Switzerland FLIGHT TEST AND CFD STUDY OF THE EFFECT OF WING BOUNDARY LAYER TRANSITION ON AILERON BALANCE |
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ICAS2024_0507: Y.H. Kim, South Korea; J.-H. Shin, South Korea; C.J. Woo, South Korea; C.K. Son, South Korea; K.J. Yee, South Korea OPERATIONAL LIMITS ASSESSMENT FOR HIGH-ALTITUDE LONG-ENDURANCE UAVS CONSIDERING PROPELLER ICING EFFECT |
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ICAS2024_0551: Z. Xu¹, D. Li¹, J. Cai¹, J. Han, N, China; ¹Northwestern Polytechnical University School of Aeronautics, China LONG-WAVE INSTABILITY OF AIRCRAFT WAKE VORTEX UNDER SHEAR CROSSWIND |
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ICAS2024_0605: R.-F. Xu¹, W.-P. Song¹, X.-H. Li², R.-Z. Qian², Y.-J. Zhang², J.-H. Xu¹, X.-L. Li¹; ¹Northwestern Polytechnical University, China; ²AVIC The First Aircraft Institute, China RESEARCH ON AERODYNAMIC DESIGN OF ENGINE NACELLE UNDER THE INFLUENCE OF PROPELLER SLIPSTREAM FOR THE TURBOPROP AIRCRAFT |
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ICAS2024_0632: R. de Vries¹, T. Sinnige¹, L.L.M. Veldhuis¹; ¹Delft University of Technology, Netherlands AERODYNAMIC PERFORMANCE AND INTERACTION EFFECTS OF AN OVER-THE-WING DISTRIBUTED-PROPELLER SYSTEM IN CRUISE CONDITIONS |
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ICAS2024_0634: X. Jia¹, C. Gong¹, C. Li¹; ¹Northwestern Polytechnical University, China SPARSE RECONSTRUCTION OF SURFACE LOADS ON AIRCRAFT USING POD AND RBFNN |
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ICAS2024_0639: C. Wei¹, C. Rao¹, L. Yang¹, T. Zhang¹; ¹Aerodynamics Research Institute, China AERO-KINEMATIC OPTIMIZATION OF HIGH-LIFT DEVICES WITH DOWNWARD DEFLECTION OF SPOILER |
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ICAS2024_0665: D. Guagliardo¹, E. Cestino¹, A. Virdis¹, A. Alfero¹, V. Sapienza¹; ¹Politecnico of Turin, Italy NUMERICAL-THEORETICAL EVALUATION OF THE DITCHING OF A HULL WITH DIHEDRAL ANGLES BETWEEN -5 AND 20 DEGREES |
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ICAS2024_0677: R. Giansante¹, G. Bernardini¹, M. Gennaretti¹; ¹Roma Tre University, Italy FINITE-STATE AEROELASTIC MODELLING OF MORPHING WING THROUGH UNSTEADY LIFTING-LINE THEORY |
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ICAS2024_0679: B.W. Shu, Northwestern Polytechnical University, China; Z.H. Gao, China; J.T. Huang, China; X. Chen, China; W. Zhang, China; H. Zhao, China FAST PREDICTION OF PRESSURE DISTRIBUTION FOR 3D CONFIGURATION BASED ON LARGE LANGRAGE MODEL |
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ICAS2024_0690: K.-Y. Zhou¹, S.-Q. Zhang, Jilin Chongtong Chengfei New Material Co., LTD, China; W.-P. Song¹, J.-H. Xu¹, Z.-H. Han¹; ¹Northwestern Polytechnical University, China RESEARCH ON MULTI-OBJECTIVE AERODYNAMIC/STRUCTURAL DESIGN OPTIMIZATION METHOD FOR LARGE THICKNESS FLATBACK AIRFOILS |
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ICAS2024_0691: M. Marciniuk¹, L. Kiszkowiak², P. Piskur, Polish Naval Academy of the Heroes of Westerplatte, Poland; L. Malicki¹, K. Strzelecka¹, K. Sibilski², S. Kachel²; ¹Wroclaw University of Science and Technology, Poland; ²Military University of Techology, Poland AERODYNAMIC ANALYSIS OF CAMBER MORPHING AIRFOILS USING PARTICLE IMAGE VELOCIMETRY AND COMPUTATIONAL FLUID DYNAMICS METHODS |
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ICAS2024_0852: K. Zuo¹, X. Yuan, China Aerodynamics Research and Development Center, China; W. Zhang¹, Z. Ye¹; ¹Northwestern Polytechnical University, China INTELLIGENT RECONSTRUCTION METHOD OF AIRFOIL FLOW FIELD BASED ON DEEP ATTENTION NETWORK |
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ICAS2024_0857: Q. Zhang, Northwestern Polytechnical University, China; W. Zhang, Northwestern Polytec, China A HYBRID APPROACH FOR RECONSTRUCTION OF TRANSONIC BUFFET AERODYNAMIC NOISE: INTEGRATING RANDOM FOREST AND COMPRESSIVE SENSING ALGORITHM |
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ICAS2024_0859: P.E. Di Nuzzo, Italy; M. Maione¹, G. Pezzella¹, A. Viviani¹; ¹University of Campania, Italy ENGINEERING-BASED TOOL FOR THREE-DIMENSIONAL ESTIMATIONS OF RE-ENTRY VEHICLES AEROTHERMODYNAMICS |
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ICAS2024_0901: Z.-W. Lu¹, Y.-H. Li¹, J.-C. Chen¹, M.-B. Tong¹, B. Wu¹; ¹Nanjing University of Aeronautics and Astronautics, China NUMERICAL SIMULATION OF THE RESPONSE CHARACTERISTICS OF THE WING STRUCTURE OF A SEAPLANE PLANING IN WAVE |
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ICAS2024_0957: W. Wang¹, X. Jia¹, C. Gong¹, C. Li¹; ¹Northwestern Polytechnical University, China MULTI-FIDELITY SURROGATE MODELING BASED ON DATA EXTENSION USING POD AND ANN |
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ICAS2024_0958: S. Zhao¹, W. Zhang¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China CORRELATION MODELLING OF SURFACE INVISCID FLOW CHARACTERISTICS AND FRICTION DISTRIBUTION BASED ON MACHINE LEARNING |
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ICAS2024_1080: W. Zhang¹, X. Wang¹, J. Kou¹, Z. Liu, The China Aerodynamics Research and Development Center, China; ¹ Northwestern Polytechnical University, China DYNAMIC STALL PREDICTION THROUGH COMBINING PHYSICAL MODELS AND MACHINE LEARNING |
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ICAS2024_1110: J. Kou¹, C. Ning¹, W. Zhang¹; ¹Northwestern Polytechnical University, China TRANSFER LEARNING FOR REDUCED-ORDER MODELING OF TRANSONIC FLOWS USING MULTIFIDELITY DATA |
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ICAS2024_1150: P. Kovar, Center of Advanced Aerospace Technology, Czech Republic; J. Fürst, Department of Technical Mathematics, Faculty of Mechanical Engin, Czech Republic ABOUT MODELLING OF EMPIRICAL CORRELATIONS WITHIN AERODYNAMIC PROFILES USING HIGHER ORDER ARTIFICIAL NEURAL NETWORKS |
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ICAS2024_1201: D. Vera Sepúlveda¹, R. Cassineli Palharini¹, E. Gaglio, Scuola Superiore Meridionale, Italy; R. Savino, University of Naples “Federico II”, Italy; ¹Universidad Técnica Federico Santa Marpia, Chile AERODYNAMIC ANALYSIS OF A FLAP-BASED DEPLOYABLE RE-ENTRY SYSTEM UNDER RAREFIED CONDITIONS |
4.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance |
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ICAS2024_0025: C. Matias¹, A. Diskin¹, O. Golan, Afeka- Tel-Aviv Academic College of Engineering, Israel; A. Garkun², E. Strokin²; ¹Israel Aerospace Industries, Israel; ²Technion Research & Development Foundation, Israel SURFACE QUALITY CHALLENGE FOR TI-6AL-4V ADDITIVE MANUFACTURED TOPOLOGIC OPTIMIZED LIGHTWEIGHT STRUCTURE |
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ICAS2024_0032: W.J. Vankan¹, N. van Hoorn¹, A.J. de Wit¹, T.P.A. Koenis¹; ¹NLR, Netherlands ELECTROMAGNETIC INDUCTION HEATING OF TP-CFRP LAMINATES: FEM MODELLING AND VALIDATION |
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ICAS2024_0045: J. Zhou, China; C. Zhang, China STUDY ON LOW-VELOCITY IMPACT BEHAVIOR AND RESIDUAL PERFORMANCE PREDICTION OF CFRP T-JOINTS |
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ICAS2024_0058: G.M. Odegard, Michigan Technological University, United States; M. Maiaru, Columbia University, United States PROCESS MODELLING OF COMPOSITES USING A MULTISCALE FRAMEWORK |
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ICAS2024_0105: N. Monokrousos¹, L. Könözsy¹, V. Pachidis¹, E. Sozio², F. Rossi²; ¹Cranfield University, United Kingdom; ²Pangea Aerospace, Spain NUMERICAL SOLUTION OF LOX FLOW IN A LIQUID ROCKET ENGINE ADDITIVELY MANUFACTURED COOLING CHANNEL |
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ICAS2024_0120: E. Monaco¹, F. Ricci¹; ¹Università di Napoli , Italy CONVOLUTIONAL NEURAL NETWORKS ALGORITHMS FOR STRUCTURAL HEALTH MONITORING OF AIRCRAFTS COMPOSITES PANELS |
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ICAS2024_0169: P. Conen¹, F. Raddatz¹, G. Wende¹; ¹DLR, Germany TRAIN ON SYNTHETIC - TEST ON REAL: DOMAIN ADAPTATION FOR STRAIN-BASED DAMAGE DETECTION ON AN AIRCRAFT WING |
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ICAS2024_0212: H. Wu¹, Y. Bai¹, S.-L. Fang¹, Z.-Q. Zhao¹, C. Zhang¹; ¹Northwestern Polytechnical University, China THE RESISTANCE TO THE HIGH-VELOCITY IMPACT OF THE INTRA-LAYER HYBRID PLAIN WEAVE COMPOSITES |
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ICAS2024_0213: T. Nan¹, G.J. Yun, Seoul National University, North Korea; C. Zhang¹; ¹Northwestern Polytechnical University, China MICROMECHANICAL MODELING OF THE VISCOELASTIC-VISCOPLASTIC RESPONSE OF FIBER-REINFORCED COMPOSITES |
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ICAS2024_0215: C. Zhang¹, P. Liu¹, Y.-L. Li¹; ¹Northwestern Polytechnical University, China MODELING THE TEMPERATURE-RISE BEHAVIOR OF 2D TRIAXIAL BRAIDED COMPOSITES UNDER IMPACT LOADS |
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ICAS2024_0225: S. Zhao¹, J. Huang¹, C. Zhang¹; ¹Northwestern Polytechnical University, China THE EFFECT OF TARGET THICKNESS ON THE BALLISTIC BEHAVIOR OF HYBRID CFRP/KFRP COMPOSITES |
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ICAS2024_0229: I. Rivero¹, A. Palomar¹, M. Rebollo¹, J. Domingo¹, M. Lozano¹, Z. Mujika¹, D. Garijo¹, G. Lara¹, A. Capitan¹, J. Gomez-Escalonilla¹; ¹Airbus, Spain DEMOCRATIZATION OF FATIGUE EVALUATION FOR REALISTIC RIVETING CONFIGURATIONS USING STATE-OF-THE-ART SIMULATIONS |
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ICAS2024_0250: P. Minigher, INEGI / University of Porto / University of Girona, Italy; A. Arteiro¹, A. Turon, University of Girona, Spain; J. Fatemi, Airbus NL, Netherlands; S. Guinard, Airbus SAS, France; L. Barrière, Saint Exupéry, France; P.P. Camanho¹; ¹INEGI / University of Porto, Portugal ON AN EFFICIENT GLOBAL/LOCAL STOCHASTIC METHODOLOGY FOR FAILURE PREDICTION OF AIRCRAFT COMPOSITE STRUCTURES |
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ICAS2024_0252: S. Saputo¹, R. Augello¹, E. Carrera, Germany; ¹Department of Aeronautics and Aerospace Engineering, Politecnico, Italy MACRO, MESO AND MICRO SCALE ENERGY EVALUATION IN LAMINATED AND COMPOSITE STRUCTURES USING THE COMPONENT-WISE APPROACH |
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ICAS2024_0259: Y. Bai¹, P. Liu¹, Z.-Q. Zhao¹, C. Zhang¹; ¹Northwesterm Polytechnical University, China A MESO-SCALED SIMULATION ON THE THICKNESS EFFECT OF TWO-DIMENSIONAL TRIAXIALLY BRAIDED COMPOSITES UNDER TENSILE LOADS |
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ICAS2024_0275: R. Szczepaniak¹, P. Przybylek¹, D. Szczechula¹, A. Krzyzak¹, A. Komorek¹, G. Woroniak, Bialystok University of Technology, Poland; ¹Polish Air Force University, Poland ANALYSIS OF THE POSSIBILITY OF INCREASING THE THERMAL RESISTANCE OF EPOXY RESIN WITH CWNT AND MMT |
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ICAS2024_0290: B. Castanié¹, J.-C. Passieux¹, J.-N. Périé¹, C. Bouvet¹, J.-E. Dufour¹, J. Serra¹; ¹Institut Clément Ader, France MULTIAXIAL TESTING OF AERONAUTIC COMPOSITE STRUCTURES AT INTERMEDIATE SCALE |
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ICAS2024_0296: R. Hu, China; Z. Yuan, China; C. Zhang, China DYNAMIC AND STABILITY ANALYSES OF ROTATING THIN-WALLED FILAMENT WOUND GLASS FIBRE COMPOSITE CYLINDERS WITH METAL LINER |
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ICAS2024_0300: K. Li¹, Y. Ma, Chongqing University of Technology, China; Y. Han¹; ¹AVIC Manufacturing Technology Institute, China STABLE LOCALIZED CORROSION IN A 7075-T6 ALUMINUM ALLOY FSW JOINT: MECHANISM AND MITIGATION |
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ICAS2024_0307: B. Omede'¹, A.M. Grande¹; ¹Politecnico di Milano, Italy MACHINE LEARNING AND NUMERICAL OPTIMIZATION OF BIO-INSPIRED 3D-PRINTABLE SANDWICH CORE CELL |
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ICAS2024_0316: W. Stryczniewicz¹, T. Kwiatkowski¹, I. Kaminska², M. Chojnacki², K. Fronc²; ¹?ukasiewicz Research Network - Institute of Aviation, Poland; ²Institute of Physics Polish Academy of Sciences, Poland THERMAL HISTORY PAINT UNDER HIGH SUBSONIC FLOW |
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ICAS2024_0339: X. Liu¹, D. Gu¹; ¹Nanjing University of Aeronautics and Astronautics, China EFFECT OF LASER PRINTING MODE ON SURFACE TOPOGRAPHY, MICROSTRUCTURE AND CORROSION PROPERTY OF ADDITIVE-MANUFACTURED NITI |
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ICAS2024_0351: B.R. Yang¹, B. Wan¹, G.C. Fu¹, X.H. Wang¹, X.H. Wang¹, J. Yao¹; ¹Beihang University, China A PHASE FIELD BASED DEEP LEARNING APPROACH FOR MECHANICAL PROPERTY PREDICTION OF SINTERED SILVER IN POWER ELECTRONICS |
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ICAS2024_0360: A. Riccio¹, A. Garofano¹, G. Rigliaco¹, M. Boccaccio², F. Acerra²; ¹University of Campania “Luigi Vanvitelli”, Italy; ²Leonardo S.p.A., Italy REDESIGN OF AN AERONAUTICAL COMPOSITE STIFFENED PANEL WITH THE DOUBLE-DOUBLE DESIGN APPROACH |
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ICAS2024_0368: Y. Liu¹, W. Wang¹, J. Zhao¹, Y. Song¹, L. Zou¹; ¹Chongqing University, China WEAR EVOLUTION OF PYRAMID-STRUCTURED ABRASIVE BELTS AND ITS EFFECT ON GRINDING OPERATIONS |
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ICAS2024_0393: Y. Zhang, China; Y. Ning, China; B. Wang, China; H. Peng, China FATIGUE CRACK LIFE PREDICTION BASED ON BAYESIAN DYNAMIC UPDATE |
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ICAS2024_0407: D. Blanco Garde¹, F. Mews¹, J. Jokinen¹, N. Pournoori¹, M. Kanerva¹; ¹Tampere University, Finland HOT-WET CONDITIONING AND THE SENSITIVITY OF MECHANICAL TESTING WITHIN SURFACE TREATMENT QUALIFICATION FOR AIRCRAFT |
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ICAS2024_0422: H. Peng¹, B. Wang¹, Y. Zhang¹, L. Ji¹, S. Li¹; ¹AVIC the First Aircraft Institute, China STUDY ON FATIGUE PROPERTIES OF TITANIUM ALLOY BASE MATERIAL AND WELDED STRUCTURE IN THERMAL COMBINED ENVIRONMENT |
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ICAS2024_0435: W.H. Yuan¹, Y.J. Chai¹, X.W. Yang¹, F. Ripamonti, Politecnico di Milano, Italy; X. Wang¹, Y.M. Li¹; ¹Xi’an Jiaotong University, China FLUID-STRUCTURE INTERACTION OF TWO-PHASE SCATTERER METAMATERIALS FOR VIBRATION SELF-SUPPRESSION |
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ICAS2024_0438: M. Bona¹, A.M. Grande¹; ¹Politecnico di Milano, Italy OPTIMIZATION OF POST-PROCESSING HEAT TREATMENT FOR LPBF MODIFIED 2024 ALUMINIUM ALLOY |
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ICAS2024_0525: E.G. Park, South Korea; S.H. Jeong, South Korea; J.Y. Cho, South Korea; J.H. Kim, South Korea DEVELOPMENT OF A MACHINE LEARNING-BASED STRESS SPECTRUM ESTIMATION TECHNIQUE FOR FATIGUE MONITORING |
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ICAS2024_0538: N.M. Hoang¹, M.D. Ha¹, T.Q. Nguyen¹, P.M. Nguyen¹; ¹Viettel Aerospace Institute, Vietnam INTEGRATIVE ANALYSIS OF LOW-CYCLE FATIGUE AND CRACK PROPAGATION IN TURBINE BLADES |
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ICAS2024_0544: Y. Liu¹, B. Liu¹; ¹Northwestern Polytechnical University, China ELASTIC/PLASTIC SEMI-ANALYTICAL METHOD FOR ARBITRARY CURVED SURFACES OF SCARF REPAIRED COMPOSITES |
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ICAS2024_0584: J. Gu¹, Y. Bai¹, Z. Zhao¹, C. Zhang¹; ¹Northwestern Polytechnical University, China A DYNAMIC TEST METHODOLOGY FOR DETERMINING THE LONGITUDINAL COMPRESSIVE RESPONSE OF CARBON FIBER COMPOSITE TOWS |
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ICAS2024_0633: C.M. Johnston¹, L.C. Tshabalala¹, M. Davids, University of the Witwatersrand, South Africa; ¹CSIR, South Africa FATIGUE PROPERTIES OF ADDITIVELY MANUFACTURED TOOL STEEL |
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ICAS2024_0654: E. Del Priore¹, L. Lampani¹; ¹Sapienza University of Rome, Italy IMPROVING SHAPE SENSING OF AERONAUTICAL STRUCTURES WITH STRAIN PRE-EXTRAPOLATION AND SENSOR PLACEMENT OPTIMIZATION |
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ICAS2024_0739: P.E. Boffa¹, E. Casciaro¹, P. Bettini¹; ¹Politecnico di Milano, Italy FULLY-EMBEDDED PRESSURE SENSOR FOR AERODYNAMICS SURFACES BASED ON FBG TECHNOLOGY |
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ICAS2024_0748: G. Zhang, China; M. Tong, China; B. Yan, China; F. Wang, China; H. Zhang, China DAMAGE AND MECHANICAL REPAIR OF COMPOSITE LAMINATES: EFFECTS OF EMBEDDED DEFECTS AND LOW VELOCITY IMPACTS |
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ICAS2024_0760: M.H. Elalfy¹, R. de Breuker¹, S.G.P. Castro¹; ¹TU Delft, Netherlands TOWARDS EFFICIENT ANALYSIS OF POSTBUCKLING IN AIRCRAFT STIFFENED STRUCTURES |
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ICAS2024_0796: Y. Ma, China; X. Zha, China; P. Cheng, China; J. Xie, China; L. Li, China; X. Liu, China INVESTIGATION ON THE MECHANISM OF THERMAL CYCLING FAILURE IN C/SIC COATING COMPOSITE MATERIALS |
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ICAS2024_0806: M. Mucha¹, D. Sikorski, 41st Training Air Base, Poland; R. Szczepaniak¹, R. Babel¹, A. Krzyzak¹, T. Zahorski¹; ¹Polish Air Force University, Poland EFFECT OF INFILL STYLE AND DENSITY ON SELECTED MECHANICAL PROPERTIES OF THE CARBON FIBRE REINFORCED ABS MFD FILAMENT |
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ICAS2024_0808: Y. Yue¹, R. Zhao¹, B. Wang¹, Y. Li, Shaanxi Key Laboratory of Impact Dynamics and Engineering Applic, China; ¹School of Aeronautics, Northwestern Polytechnical University, China HIGH-VELOCITY DROPLET IMPACT STUDIES ON C/SIC AND C/C COMPOSITES |
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ICAS2024_0818: R. Masia¹, M. Petrolo¹, E. Zappino¹, N. Zobeiry, University of Washingthon, United States; E. Carrera¹; ¹Politecnico di Torino, Italy NUMERICAL ANALYSIS OF PROCESS-INDUCED DEFORMATIONS AND STRESSES IN AERONAUTICAL COMPOSITE COMPONENTS |
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ICAS2024_0830: Z.-X. Liu¹, J. Liu¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China DEVELOPMENT AND ANALYSIS OF THE THEORY OF COMPOSITE EXPANSION RING UNDER ELECTROMAGNETIC LOADING |
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ICAS2024_0841: C. Zhang¹, J. Liu¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China HIGH TEMPERATURE BALLISTIC IMPACT TEST TECHNOLOGY BASED ON ELECTROMAGNETIC LAUNCH |
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ICAS2024_0858: V. Memmolo¹, L.M. Cardone¹, G. Petrone¹, S. De Rosa¹; ¹Università degli Studi di Napoli Federico II, Italy DESIGN OF HYDROGEN STORAGE SYSTEMS IN NEW-GENERATION REGIONAL AIRCRAFT |
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ICAS2024_0878: J.-H. Cha, Chosun Uni., South Korea INFLATABLE SPACE SHIELD STRUCTURE FOR SPACE HABITATION MODULE |
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ICAS2024_0908: N. Tsushima, Japan Aerospace Exploration Agency, Japan; M. Kita¹, I. Matsubara¹, M. Ohishi, Ryoyu Systems Co., Ltd., Japan; R. Higuchi, 2The University of Tokyo, Japan; K. Yamamoto¹; ¹3Cybernet Systems Co., Ltd., Japan EFFICIENT THERMOMECHANICAL SIMULATION FOR METALLIC LATTICE STRUCTURES FABRICATED BY ADDITIVE MANUFACTURING |
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ICAS2024_0923: Y. Elbaz, Technion, I.I.T., Israel; H. Abramovich, Technion, I.I.T., Israel LASER SHEAROGRAPGY-PREDICTION AND OPTIMIZING ITS FLAW DETECTION CAPABILITIES USING AN ADVANCED HYBRID APPROACH |
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ICAS2024_0933: D.-B. Li, China; H.-X. Huang, China; X.-C. Liu, China; P.-Y. Hou, China; H.-H. Liao, China A METHOD FOR OPTIMISING THE ARRANGEMENT OF INTERNAL CHANNELS IN AIRCRAFT HYDRAULIC MANIFOLDS MANUFACTURED BY ADDITIVE MANUFACTURING |
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ICAS2024_1006: Y. Lu¹, W. Wang¹, Y. Zhang, Hangzhou Zhiyuan Research Institute, China; Z. Zhang, Northwest Institute of Mechanical and Electrical Engineering, China; ¹Northwestern Polytechnical University, China IMPACT RESPONSES AND FAILURE MECHANISMS OF ALMGB14 UNDER DYNAMIC LOADS |
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ICAS2024_1052: M.S. Loukil¹, J. Xu¹, E. Marklund², M. Merzkirch², F. Moreau³, F. Ohlsson³; ¹Linköping University, Sweden; ²Research Institutes of Sweden RISE, Sweden; ³Oxeon AB, Sweden THERMAL AND MECHANICAL CYCLING OF THIN-PLY COMPOSITES FOR CRYOGENIC APPLICATIONS |
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ICAS2024_1076: G. Masciopinto¹, E. D'Accardi¹, D. Palumbo¹, U. Galietti¹; ¹Polytechnic University of Bari, Italy STIMULATED THERMOGRAPHY AS NON-DESTRUCTIVE TESTING TO ASSESS THE STRUCTURAL INTEGRITY OF AERONAUTICAL COMPONENT IN CFRP |
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ICAS2024_1081: V.M. Sharma¹, P. Jha¹, V. Samanyusree¹, A. Sharma¹, S. Maheshwari¹, G.S. Mamatha¹; ¹RV College of Engineering, India EMBEDDED SENSORS FOR AIRCRAFT PREDICTIVE MAINTENANCE: SHM SYSTEM INTEGRATION & TRADE-OFF ANALYSIS |
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ICAS2024_1099: Y. Zhao, China; W. Wang, China; X. Wan, China INVESTIGATION ON VARIABLE-HEIGHT PROTRUSION ARRANGEMENT OF METAL–COMPOSITE HYBRID JOINTS UNDER A TENSILE LOAD |
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ICAS2024_1108: S. Kiasat¹, A.S. Nobari, Aeronautics Engineering Department, Imperial College, United Kingdom; M. Filippi¹, E. Carrera¹; ¹POLITECNICO DI TORINO, Italy INVESTIGATING THE EFFECT OF DELAMINATION-INDUCED FRICTIONAL CONTACT ON THE DYNAMIC BEHAVIOR OF LAMINATE STRUCTURES |
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ICAS2024_1111: G. Janszen¹, A.M. Caporale¹, L. Cavalli, Petroceramics S.p.A., Italy; M. De Stefano Fumo, CIRA, Italy; A. Airoldi¹; ¹Politecnico di Milano, Italy IMPACT TOLERANCE OF CERAMIC MATRIX COMPOSITES FOR AEROSPACE APPLICATIONS |
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ICAS2024_1120: M. Sladky¹, M. Machac², J. Papuga², I. Jebacek¹; ¹Faculty of Mechanical Engineering, Brno University of Technology, Czech Republic; ²Faculty of Mechanical Engineering, Czech Technical University, Czech Republic THE FATIGUE LIFE PREDICTION OF THIN-WALLED WELDED JOINTS |
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ICAS2024_1135: R. De Finis, Università del Salento, Italy; D. Palumbo¹, U. Galietti¹; ¹Politecnico di Bari, Italy STRUCTURAL HEALTH MONITORING OF CFRP DURING FATIGUE LOAD VIA THE ASSESSMENT OF CRACK DENSITY BY MEANS OF THERMOGRAPHY |
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ICAS2024_1141: P. Jha¹, V.M. Sharma¹, V. Samanyusree¹, A. Sharma¹, S. Maheshwari¹; ¹R. V. College of Engineering, India USE OF GRAPHENE MATERIAL IN AIRCRAFT STRUCTURE FOR LIGHTNING STRIKE PROTECTION |
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ICAS2024_1146: M. Khella¹, S. Ghiasvand¹, P. Ballarin¹, F. Panzeri¹, S. Piacquadio¹, A. Airoldi¹; ¹Politecnico di Milano, Italy NUMERICAL TOOLS FOR SLOW-GROWTH APPROACHES TO DAMAGE TOLERANT COMPOSITE AERONAUTICAL STRUCTURES |
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ICAS2024_1158: D. Fanteria¹, L. Boni¹, F. Romano, 2CIRA S.C.p.A., Italian Aerospace Research Centre, Italy; ¹University of Pisa, Italy DAMAGE TOLERANCE OF A CURVED COMPOSITE STIFFENED PANEL FABRICATED BY AN OUT OF AUTOCLAVE – LIQUID RESIN INFUSION PROCESS |
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ICAS2024_1203: E. Carrera , Politecnico, Italy; V.V. Zozulya, iMex, Ukraine VIBRATION OF COMPOSITE SHELLS OF REVOLUTION USING EQUIVALENT SINGLE LAYER APPROACH |
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ICAS2024_1206: M.C. Noviello¹, I. Dimino¹, S. Ameduri¹, A. Concilio¹; ¹The Italian Aerospace Research Centre (CIRA), Italy CONCEPTUAL DESIGN AND TOPOLOGY OPTIMIZATION OF A COMPLIANT MORPHING FLAP FOR NEXT GENERATION HYBRID-ELECTRIC REGIONAL AIRCRAFT |
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ICAS2024_1222: J. Jokinen, Tampere University, Finland; T. Thorvaldsen, Norwegian Defence Research Establishment, Norway; P. Nijhuis, Royal Netherlands Aerospace Centre, Netherlands; M. Kadlec¹, R. Ruzek¹, L. Munch, University of Stuttgart, Institute of Aircraft Design, Germany; M. Hoffmann, Airbus Defence and Space GmbH, Germany; T. Viitanen, Technical Research Center of Finland Ltd, Finland; M. Wallin, Patria Aviation, Finland; G. Sagvolden, Light Structures AS, Norway; C. Sbarufatti², L. Martulli², A. Bernasconi²; ¹Czech Aerospace Research Centre, Czech Republic; ²Politecnico di Milano, Department of Mechanical Engineering, Italy PATCHBOND II - CERTIFICATION OF ADHESIVE BONDED REPAIRS FOR PRIMARY AEROSPACE COMPOSITE STRUCTURES |
4.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity |
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ICAS2024_0011: A. Voß¹, J. Baier¹; ¹DLR Institute of Aeroelasticity, Germany CLOSED-LOOP GUST LOADS ANALYSIS OF A SUPERSONIC FIGHTER AIRCRAFT |
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ICAS2024_0012: V. Handojo¹, S. Puelm¹; ¹DLR German Aerospace Center, Germany POTENTIAL LIMITS OF LOAD ALLEVIATION IN REDUCING THE STRUCTURAL MASS OF A LONG-RANGE TRANSPORT CONFIGURATION |
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ICAS2024_0054: J. Cecrdle¹, O. Vich¹, J. Starek¹, J. Vlach¹, M. Kolar¹, M. Smid¹; ¹Czech Aerospace Research Centre (VZLU), Czech Republic W-WING AEROELASTIC DEMONSTRATOR DESIGN MODIFICATION AND UPGRADE |
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ICAS2024_0066: Y. He¹, A. Shi¹; ¹Northwestern Polytechnical University, China EFFECTS OF SHOCK IMPINGEMENT LOCATION ON PANEL AEROELASTIC STABILITY IN MACH REFLECTION |
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ICAS2024_0071: K. Otsuka, Tohoku University, Japan; C.W. Cheng¹, R. Palacios¹; ¹Imperial College London, United Kingdom ABSOLUTE NODAL COORDINATE FORMULATION FOR NONLINEAR MULTIBODY MODELING OF FLARED HINGED WINGS |
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ICAS2024_0072: Z. Guo¹, A. Tang¹, Q. Jing¹; ¹Chinese Flight Test Estsblishment, China FLIGHT LOADS RESEARCH OF TWIN VERTICAL TAIL FOR BLENDED WING-BODY AIRCRAFT BASED ON STRAIN GAUGE CAILBRATION |
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ICAS2024_0111: Y.J. Pan¹, M. Alam¹, A. Spinelli¹, E. Bragado Aldana¹; ¹Cranfield University, United Kingdom STRUCTURAL AND AEROELASTIC OPTIMISATION OF A LARGE AIRCRAFT WING WITH A PASSIVE TWIST WINGTIP |
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ICAS2024_0114: F.M.A. Mitrotta¹, A. Pirrera¹, T. Macquart¹, J.E. Cooper¹, A. Pereira do Prado², P.H. Cabral²; ¹University of Bristol, United Kingdom; ²Embraer, Brazil INFLUENCE OF SKIN CURVATURE ON WINGBOX OPTIMIZATION WITH NONLINEAR STRUCTURAL STABILITY CONSTRAINTS |
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ICAS2024_0115: V. Priasso¹, A. Lannoo¹; ¹DMAS, ONERA, France DEVELOPMENT OF A MASS EVALUATION TOOL FOR CLASSICAL AND DISRUPTIVE AIRCRAFT STRUCTURES |
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ICAS2024_0130: R. Pecora, University of Naples Federico II, Italy TRADE OFF STUDIES ON WING MANEUVER LOAD ALLEVIATION STRATEGIES BASED ON AILERONS AND WINGLETS MOVABLE SURFACES |
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ICAS2024_0140: N.J. Lawson, The University of Sydney, Australia; G. Zhao¹, S.C. Place¹, R.A. Harrison¹; ¹Cranfield University, United Kingdom MEASUREMENT OF WING BENDING IN-FLIGHT FROM A T67 SLINGSBY FIREFLY LIGHT AIRCRAFT |
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ICAS2024_0147: F. Toffol¹, C. Bisagni¹; ¹Politecnico di Milano, Italy GUST LOAD PASSIVE ALLEVIATION BY MEANS ON NONLINEAR, BUCKLING DRIVEN, STRUCTURAL RESPONSE |
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ICAS2024_0150: H.F. Maathuis¹, S.G.P. Castro¹, R. De Breuker¹; ¹Delft University of Technology, Netherlands EXPLORING MULTI-FIDELITY AEROELASTIC TAILORING: PROSPECT AND MODEL ASSESSMENT |
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ICAS2024_0162: A. Crovato¹, P. Dechamps¹, A.P. Prado², P.H. Cabral², V.E. Terrapon¹, G. Dimitriadis¹; ¹University of Liège, Belgium; ²Embraer S.A., Brazil FAST TRANSONIC CORRECTIONS FOR PANEL METHODS USING VISCOUS-INVISCID INTERACTION |
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ICAS2024_0167: P.H. Cabral¹, A.P. do Prado¹, E. Carrera², A. Pagani², A. Racionero Sánchez-Majano², M. Enea²; ¹Embraer S.A., Brazil; ²Politecnico di Torino, Italy AEROELASTIC TAILORING BASED ON VIRTUALLY-GENERATED ALLOWABLES AND HIGH ORDER FINITE ELEMENTS FOR IMPROVED COMPOSITE WING AEROELASTIC TAILORING BASED ON VIRTUALLY-GENERATED ALLOWABLES AND HIGH ORDER FINITE ELEMENTS FOR IMPROVED COMPOSITE WING DESIGN |
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ICAS2024_0170: J.R. Banerjee¹, A. Ananthapuvirajah¹, P.H. Cabral, Embraer S.A., Brazil; ¹City, University of London, United Kingdom THE EFFECTS OF ENGINE MASS AND LOCATION ON THE FLUTTER CHARACTERISTICS OF AIRCRAFT WINGS |
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ICAS2024_0192: L. Zhu¹, J. Shen, University of Exeter, United Kingdom; R.M.J. Groh¹, M. Schenk¹, A. Pirrera¹; ¹University of Bristol, United Kingdom ENHANCING THE PERFORMANCE OF SLENDER STRUCTURES WITH GEOMETRIC CONSTRAINTS: A CASE STUDY WITH THE ROORDA FRAME |
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ICAS2024_0299: J. Docter¹, H. Pijlman¹, D. de Wit², J. Vervliet², J. Katarzynski¹, R. Postma¹, K.-J. Bisschop¹, J. Vroon¹; ¹NLR, Netherlands; ²Asco Industries, Belgium NOVEL TEST RIG TO DEMONSTRATE A MULTI FUNCTIONAL FLAP MECHANISM OFFERING A 2ND DEGREE OF FREEDOM |
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ICAS2024_0322: R.A.S. Cardoso¹, M.S. Reis¹, L.P.S. Ferreira, FEMTO-ST, France; M.P. Alves¹, S.K. Ha, Hanyang University, South Korea; C.A. Cimini Jr.¹; ¹Federal University of Minas Gerais, Brazil A-BASIS AND B-BASIS BUCKLING ALLOWABLES FOR AN AIRCRAFT COMPOSITE WING |
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ICAS2024_0365: S. Xiao¹, L.-Y. Liu¹, H.-M. Xue¹, M.-Q. Wang¹, D.-Y. Chen¹; ¹AVIC Shenyang Aircraft Design and Research Institute, China LARGE-SCALE STRUCTURAL DYNAMIC TOPOLOGY OPTIMIZATION DESIGN FOR AIRCRAFT VIBRATION REDUCTION UNDER RANDOM EXCITING RESPONSE |
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ICAS2024_0375: P. Xu¹, Q.-X. Mu¹, W.-N. Zhang¹; ¹AVIC Shenyang Aircraft Design and Research Institute, China OPTIMIZATION DESIGN OF MULTI-SCALE ACTIVE COOLING STRUCTURE FOR AIRCRAFT |
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ICAS2024_0385: A. De Gaspari¹, V. Cavalieri¹, M. Corti¹, S. Ricci¹; ¹Politecnico di Milano, Italy MULTI-OBJECTIVE DESIGN OPTIMIZATION OF A MORPHING AILERON FOR A HYBRID ELECTRIC REGIONAL AIRCRAFT |
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ICAS2024_0386: F. Healy¹, H. Gu¹, D. Rezgui¹, J. Cooper¹; ¹University of Bristol, United Kingdom CONCEPTUAL DESIGN OF HYDROGEN-POWERED AIRCRAFT: HIGH ASPECT RATIO WINGS AND FLOATING WINGTIPS |
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ICAS2024_0389: H. Qiu¹, Y. Guo¹, Z. Guan¹, H. Zhu¹, Y. Pan¹; ¹Nanjing University of Aeronautics and Astronautics, China DYNAMIC BUCKLING ANALYSIS OF THIN-SHELL COMPOSITE STRUCTURES BASED ON ISOGEOMETRIC ANALYSIS |
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ICAS2024_0403: C.E.S. Cesnik¹, S. Sharqi¹; ¹University of Michigan, United States FINITE ELEMENT MODEL UPDATE OF VERY FLEXIBLE AIRCRAFT BASED ON GROUND VIBRATION TESTS |
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ICAS2024_0405: S.-R. Xu, China; Y.-T. Zhang, China; J.-F. Zhang, China; Y. Zheng, China; Y.-L. Liu, China OPTIMIZATION OF COMPOSITE WING STRUCTURE FOR TILT-DUCT AIRCRAFT CONSIDERING DISCRETE AND CONTINUOUS DESIGN VARIABLES |
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ICAS2024_0418: Z. Yu¹, J. Huang¹, Q. Jiang¹, F. Fan, CHRDI , Germany; S. Huang¹; ¹CHRDI, China ROTOR DYNAMIC LOADS CHARACTERISTIC ANALYSIS WITH BLADE TIP TWIST DISTRIBUTION |
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ICAS2024_0423: J. Liu¹, W. Qian¹, X. Hu¹, X. Ai¹, X. Ran¹; ¹Dalian University of Technology, China NUMERICAL AND EXPERIMENTAL RESEARCH ON AEROELASTICITY OF HIGH-ASPECT-RATIO WINGS |
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ICAS2024_0430: W.-Z. Feng¹, J.-H. Zhang¹, Z.-H. Liang¹, W. Qian¹; ¹Dalian University of Technology, China REDUCED ORDER MODELLING OF UNSTEADY AERODYNAMICS FOR GROUND FLUTTER TEST SYSTEM |
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ICAS2024_0445: Y. Zhang¹, H. Zhan¹, B. Mi¹, M. Zhang¹; ¹Northwestern Polytechnical University, China INVESTIGATION ON INFLUENCE PARAMETER OF AIRCRAFT-MISSILE SEPARATION BY CONSIDERING AEROELASTICITY |
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ICAS2024_0446: M. Zhang¹, H. Zhan¹, B. Mi¹, Y. Zhang¹, Y. Liu¹; ¹Northwestern Polytechnical University, China ANALYSIS AND STUDY ON FLUTTER CHARACTERISTICS OF WINGS UNDER TYPICAL FRAGMENT DAMAGE |
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ICAS2024_0479: Y.M. Meddaikar¹, J.K.S. Dillinger¹, W.R. Krüger¹, R. De Breuker, Delft University of Technology, Netherlands; G.H. Silva¹, P.H. Cabral², A.P. do Prado²; ¹DLR - Institute of Aeroelasticity, Germany; ²Embraer S.A., Brazil SANDWICH COMPOSITES SKIN PANEL OPTIMIZATION FOR THE COMMON RESEARCH MODEL WING |
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ICAS2024_0486: L. Pustina¹, R.M. Galassi¹, M. Blandino¹, F. Mastroddi¹; ¹Sapienza University of Rome, Italy ADVANCED MULTIDISCIPLINARY DESIGN OF NEXT-GENERATION GREEN AIRCRAFT |
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ICAS2024_0495: M.R. Chiarelli¹, S. Bonomo¹, G. Cascinelli¹; ¹Department of Civil and Industrial Engineering, Pisa, Italy ON THE FUTURE OF TRANSONIC FLIGHTS: CURVED PLANFORM WINGS FOR BUFFET-ONSET CONTROL |
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ICAS2024_0513: C.R. Vindigni¹, G. Mantegna¹, A. Esposito¹, C. Orlando¹, A. Alaimo¹; ¹Kore University of Enna, Italy ADAPTIVE WING FLUTTER SUPPRESSION BY MEANS OF MULTIPLE TRAILING EDGE CONTROL SURFACES - A COMPARATIVE STUDY |
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ICAS2024_0530: R. Hou¹, B.T. Wang, Department of Strength Design, The First Aircraft Institute of A, China; Z.X. Zhu¹, W.C. Gao¹; ¹Department of Astronautical Science and Mechanics, HIT, China EXPERIMENTAL INVESTIGATION AND NUMERICAL ANALYSIS OF THE EFFECT OF TEMPERATURE ON THE MECHANICAL PROPERTIES OF AEROSPACE COMPOSITE-METAL HYBRID JOINTS |
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ICAS2024_0565: X. Tian¹, Y. Gu¹, Z. Yang¹; ¹Northwestern Polytechnical University, China DESIGN OF A BODY FREEDOM FLUTTER FLIGHT MODEL WITH CONVENTIONAL CONFIGURATION |
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ICAS2024_0580: A. Herwig¹, M. Haupt¹, T. Brack¹, J. Bustamante¹, S. Heimbs¹; ¹Cluster of Excellence SE²A – Techniche Universität Braunschweig, Germany GUST LOAD ALLEVIATION IN A SCALED UAV DEMONSTRATOR |
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ICAS2024_0588: N. Li¹, H. Wang¹, Z.Q. Li¹, Z.H. Wang¹; ¹Taiyuan University of Technology, China DYNAMIC DROP SIMULATION OF THE MAIN LANDING GEAR OF A GENERAL AVIATION AIRCRAFT |
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ICAS2024_0604: M.R. Ritter¹, M. Schmalz¹, M. Fehrs¹; ¹German Aerospace Center (DLR), Germany PRELIMINARY STRUCTURAL DESIGN OF A HIGH ASPECT RATIO RANSPORT AIRCRAFT WITH LAMINAR WING |
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ICAS2024_0642: W. Wang¹, W. Qian¹, X. Ai¹; ¹Dalian University of Technology, China AEROELASTIC DIVERGENCE AND FLUTTER ANALYSIS OF A WING WITH ALL MOVING WING TIP |
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ICAS2024_0651: H.-J. Guo, China; Z.-H. Han, China; C.-Z. Xu, China; K.-S. Zhang, China; W.-P. Song, China; J.-Q. Luo, China EFFICIENT AEROSTRUCTURAL DESIGN OPTIMIZATION COMBINING GRADIENT-ENHANCED KRIGING WITH COUPLED ADJOINT METHOD |
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ICAS2024_0666: G.M. Gagliardi¹, M.D. Kulkarni, Embry-Riddle Aeronautical University, United States; F. Marulo¹; ¹University of Naples Federico II, Italy SEMI-ANALYTICAL SENSITIVITY METHODS FOR AEROELASTIC SHAPE OPTIMIZATION |
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ICAS2024_0727: S. Stammel¹, C. Bisagni¹; ¹Politecnico di Milano, Italy NUMERICAL METHOD TO DETERMINE STRUCTURAL ELEMENT REDUCED STIFFNESS FOR DESIRED COMPOSITE WING STRUCTURES CONFIGURATIONS |
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ICAS2024_0728: X.-Y. Ai, China; X.-Y. Chen, China; W.-J. Wang, China; J. Liu, China; X.-J. Ran, China; W. Qian, China COMPUTATIONAL/EXPERIMENTAL AEROELASTIC STUDY FOR AN ALL-MOVABLE HORIZONTAL TAIL WITH TORSION FREE-PLAY |
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ICAS2024_0730: F. Lovero¹, G. Biggi¹, S. Lombardi¹, M.A.C. Costa¹, V. Amore¹, E. Cestino¹; ¹Politecnico di Torino, Italy EXPERIMENTAL VALIDATION OF THE DYNAMIC FINITE ELEMENT MODEL OF A 1:8 SCALE SEAPLANE USING A LASER DOPPLER VIBROMETER (LDV) |
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ICAS2024_0740: C.W. Cheng¹, S. Duessler¹, R. Palacios¹, G. Wilson¹; ¹Imperial College London, United Kingdom NUMERICAL INVESTIGATION OF PASSIVE AND ACTIVE ALLEVIATION OF DYNAMIC LOADS ON HIGH-ASPECT-RATIO-WING VEHICLES |
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ICAS2024_0784: W. Qian¹, W.-Z. Feng, Dalian University of Technology, China; C.-X. Han¹, X.-Y. Ai¹; ¹Daian University of Technology, China STUDY OF AEROELASTIC PROBLEM OF RUDDER SYSTEM WITH ELECTRIC ACTUATOR AND STRUCTURAL NONLINEARITIES |
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ICAS2024_0814: F. Nicassio¹, A.P. Fontanella², M. Cinefra², G. Scarselli¹; ¹University of Salento, Italy; ²Politecnico of Bari, Italy DETECTION OF DELAMINATIONS IN DAMAGED COMPOSITE PLATES VIA LOCAL DAMAGE RESONANCE APPROACH |
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ICAS2024_0832: A. Milazzo, University of Palerrmo, Italy; M. Lo Cascio, University of Palermo, Italy FREE VIBRATIONS OF CYLINDRICAL SHELLS WITH CUTOUTS BY A SINGLE-DOMAIN RITZ FORMULATION |
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ICAS2024_0837: G. Di Mauro¹, M. Guida¹, G. Olivares², L.M. Gomez²; ¹University of Naples Federico II, Italy; ²Jerry Moran Center, AVET, NIAR, WSU, United States MULTIPHYSICS MODELING FOR SAFE BATTERIES USING LS-DYNA |
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ICAS2024_0854: M. Filippi¹, R. Azzara¹, M. Santori¹, M. Petrolo¹, E. Carrera¹; ¹Politecnico di Torino, Italy COUPLED THERMOELASTIC ANALYSIS OF BEAM STRUCTURES USING A REFINED 1D FINITE ELEMENT MODEL |
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ICAS2024_0874: E. Roncolini¹, F. Toffol ¹, S. Ricci¹; ¹Politecnico di Milano, Italy AEROELASTIC ISSUES IN THE DESIGN OF HIGH ASPECT RATIO STRUT-BRACED WING AIRCRAFT |
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ICAS2024_0875: A. Mannoosseril¹, S. Adhikari¹, A.P. Prado², P.H. Cabral²; ¹James Watt School of Engineering, University of Glasgow, United Kingdom; ²Embraer S.A., São José dos Campos, Brazil, Brazil RANDOM MATRIX MODELLING FOR UNCERTAINTY QUANTIFICATION IN PRESTRESSED STRUCTURES |
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ICAS2024_0900: X. Wang¹, X. Peng¹, H. Liu¹, J. Kou¹, W. Zhang¹; ¹Northwestern Polytechnical University, China EFFICIENT MULTI-FIDELITY REDUCED-ORDER MODELING FOR FLUTTER PREDICTIONS ACROSS MULTIPLE MACH NUMBERS |
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ICAS2024_0905: F. Sun, Xi'an Modern Control Technology Research Institute, China; Y.-H. Zheng¹, S.-S. Zhu¹; ¹Northwestern Polytechnical University, China ANALYTICAL STUDY ON HYDROSTATIC RESPONSE CHARACTERISTICS DURING WATER LANDINGS OF AMPHIBIOUS AIRCRAFT |
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ICAS2024_0922: Y. Sun¹, Z. Han¹, H. Cao¹, W. Cheng¹, Z. Wu², C. Yang²; ¹Aviation Industry Development Research Center of China, China; ²School of Aeronautic Science and Engineering, Beihang University, China REVIEW ON NONLINEAR AEROELASTIC ANALYSIS WITH FREEPLAY |
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ICAS2024_0954: M. Candon¹, E. Hale¹, M. Balajewicz, Independent Researcher, United States; A. Delgado-Gutierrez¹, V. Muscarello¹, P. Marzocca¹; ¹RMIT University, Australia PARAMETERISATION OF NONLINEAR AEROELASTIC REDUCED ORDER MODELS WITH AERODYNAMIC AND STRUCTURAL NONLINEARITY |
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ICAS2024_1001: E. Zappino¹, M. Santori¹, M. Petrolo¹, E. Carrera¹; ¹Politecnico di Torino, Italy HIGHER-ORDER 1D STICK MODELS FOR THE FLUTTER ANALYSIS OF AIRCRAFT STRUCTURES |
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ICAS2024_1015: S.-Y. Sun¹, H.-Z. Wang¹, R. Yang¹, W. Qian¹; ¹Dalian University of Technology, China MODELING AND VALIDATION OF MORPHING WING TRAILING EDGE BASED ON ZERO POISSON'S RATIO HONEYCOMB |
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ICAS2024_1017: M. Abouhamzeh, University of Wolverhampton, United Kingdom; Y. Ma, Bauhaus Aviation Research Institute, Germany INVESTIGATING AN OPTIMAL AEROELASTIC DESIGN FOR AIRCRAFT WINGS WITH DISTRIBUTED PROPELLERS MADE OF COMPOSITES |
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ICAS2024_1035: L. Pustina¹, F. Mastroddi¹, P. Della Vecchia, University of Naples “Federico II”, Italy; G. Cerino, LEONARDO, Aircraft Division, Italy; ¹Sapienza University of Rome, Italy STRUCTURAL DESIGN OF NEXT-GENERATION REGIONAL GREEN AIRCRAFT |
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ICAS2024_1097: H.E.A.A. Santos, Embraer S.A., Brazil; D.A. Rade, Aeronautics Institute of Technology, Brazil STOCHASTIC BUCKLING ANALYSES OF LAMINATED COMPOSITE PLATES UNDER HYGROTHERMAL, GEOMETRIC AND MATERIAL UNCERTAINTIES MODELED AS NON-GAUSSIAN RANDOM FIELDS |
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ICAS2024_1106: G. Cardellino¹, T. Melz¹, R. Feldmann¹, C. Adams, Technical University of Graz, Austria; F. Franco², G. Petrone², S. De Rosa²; ¹Technical University of Darmstadt, Germany; ²Universitä degli Studi di Napoli Federico II, Italy ACTIVE CONTROL DAMPING WITH THE USE OF VOICE COIL ACTUATORS |
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ICAS2024_1140: F. Montano¹, I. Benedetti¹, V. Gulizzi¹; ¹Università degli Studi di Palermo, Italy A FORMULATION FOR WING AEROELASTIC ANALYSIS BASED ON THE UNSTEADY VLM AND STRUCTURAL DISCONTINUOUS GALERKIN TECHNIQUE |
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ICAS2024_1142: E. Carrera¹, A. Pagani¹, M. Valente¹, G. Palaia¹; ¹Politecnico di Torino, Italy A PRELIMINARY METHODOLOGY TO ASSESS GUST SPECTRA VIA SATELLITE DATA |
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ICAS2024_1162: H. Raza¹, P. Vaghela¹, E. Stumpf, RWTH Aachen, Germany; J. Bayandor¹; ¹University at Buffalo, United States BIRD AND DRONE IMPACT DAMAGE PROGNOSIS OF ON-DEMAND AIR MOBILITY SERVICE AIRCRAFT ENGINE |
5 - Propulsion |
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ICAS2024_0135: J. Häßy¹, A. Görtz¹, M. Schmelcher¹, J. Schmeink¹, M. El-Soueidan¹; ¹DLR, Germany ON THE WATER ENHANCED TURBOFAN CONCEPT: PART B – FLOW PATH AND MASS ASSESSMENT |
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ICAS2024_0143: B. Mi¹, H. Zhan¹, J. Yu, No. 5715 Factory of PLA, China; ¹Northwestern Polytechnical University, China FLOW CHARACTERISTICS OF THE INLET IN TURBOPROP ENGINE WITH THE INFLUENCE OF SANDS |
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ICAS2024_0153: F. Lutz¹, J. Jézégou¹, M. Budinger², A. Reysset²; ¹ISAE-SUPAERO, France; ²INSA Toulouse, France STUDY OF HYBRIDISATION SCENARIOS FOR TURBOPROP AIRCRAFT IN THE GENERAL AVIATION SEGMENT |
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ICAS2024_0157: B.A.T. Noordman¹, W.J. Vankan¹; ¹Royal Netherlands Aerospace Centre, Netherlands DESIGN AND ANALYSIS OF A SCALED COMPOSITE UHBR FAN BLADE FOR WIND TUNNEL TESTS |
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ICAS2024_0161: D. Kierbel¹, T. Neuland¹, P.-E. Roux¹, P. Nehter¹, J. Hollmann², C.N. Dagli², P. Köhler², S. Kabelac², A.G. Rao³, F. de Domenico³, M. Hoogreef³, L. Van Biert³, F. Yin³, C. Rossignol*, L. Dessemond*, M.C. Steil*, P. Maasº, F. Winterº, C. Warschº, S.S. Venturaᵟ, M. Mettenᵟ, M.P. Heddrichᵟ, S.A. Ansarᵟ ; ¹AIRBUS SAS, Germany ;²Leibniz University Hannover, Germany ;³Technische Universiteit Delft, Netherlands ;*Univ. Grenoble Alpes, Univ. Savoie Mont Blanc, France ;ºBauhaus Luftfahrt e.V., Germany ;ᵟGerman Aerospace Center, German HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION |
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ICAS2024_0188: A.T. Hoang¹, N.J. Lawson¹, T. Bykerk, German Aerospace Center (DLR), Germany; ¹The University of Sydney, Australia DESIGN OF A WIND TUNNEL MODEL FOR A REUSABLE LAUNCH VEHICLE DURING ITS LANDING BURN |
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ICAS2024_0195: M. Bhardwaj¹, S. Rajashankar¹, N. Ananthkrishnan¹, A. Sharma¹, W.-D. Ki², H.-J. Namkoung²; ¹Yanxiki Tech, India; ²Hyundai Rotem, South Korea MODEL-BASED CONCEPTUAL DESIGN AND EVALUATION OF A SOLID-FUEL SCRAMJET VEHICLE |
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ICAS2024_0199: A. Görtz¹, J. Häßy¹, M. Nickl², A. Lessis², M. Schmelcher¹, M. El-Soueidan¹; ¹German Aerospace Center, Germany; ²Bauhaus Luftfahrt e.V., Germany ON THE WATER ENHANCED TURBOFAN CONCEPT: PART A - THERMODYNAMICS AND OVERALL ENGINE DESIGN |
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ICAS2024_0235: F. Strauss¹, T. Nilsson, Lund University, Sweden; K. Manassis¹; ¹German Aerospace Center DLR, Germany RAMJET/SCRAMJET TEST BENCH WITH CAVITY INJECTION OF HYDROGEN |
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ICAS2024_0255: O. Russo¹, P. Roncioni¹, M. Marini¹, S. Di Benedetto¹, G. Ranuzzi², S. Pizzurro², M. Albano²; ¹Italian Aerospace Research Centre (CIRA), Italy; ²Italian Space Agency (ASI), Italy PROPULSIVE CFD ANALYSIS OF THE SCRAMJET HYPERSONIC EXPERIMENTAL VEHICLE |
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ICAS2024_0261: M.G. Kolb¹, A. Seitz¹, B. Türkyilmaz¹, Y. Ma¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany MODELLING AND INITIAL ASSESSMENT OF A FUEL CELL AUXILIARY PROPULSION AND POWER UNIT |
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ICAS2024_0263: L. Lobuono¹, D. MacManus¹, R. Christie¹, L. Boscagli¹; ¹Cranfield University, United Kingdom UNSTEADY AERODYNAMICS OF A COUPLED COMPACT INTAKE-FAN IN CROSSWIND |
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ICAS2024_0272: P. Wehrel¹, J. Schmeink¹, J. Häßy¹; ¹German Aerospace Center (DLR), Germany KNOWLEDGE-BASED TURBINE DISK MODELING – A CONCEPTUAL DESIGN PROCESS CALIBRATED TO THE NASA ENERGY EFFICIENT ENGINE |
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ICAS2024_0281: H. Tuo¹, P. Liu¹, S. Ding¹, T. Qiu¹, C. Liu¹, R. Cheng, AECC Shenyang Engine Research Institute, China; ¹Research Institute of Aero-Engine, Beihang University, China A MOMENTUM-INTEGRAL METHOD TO CALCULATE WINDAGE LOSSES ON A ROTATING DRUM WITH SUPERPOSED FLOW |
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ICAS2024_0323: G. Li, Tianmushan Laboratory, China; Y. Zhang¹, G. Zhang, Beihang University Research Institute of Aero-Engine, China; S. Huang¹, S. Ding, Civil Aviation University of China, China; ¹Beihang UniversitySchool of Energy and Power Engineering, China NUMERICAL SIMULATION OF HEAT TRANSFER IN MINIATURE RADIALLY ROTATING SODIUM/POTASSIUM HEAT PIPES |
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ICAS2024_0329: S. Shahjahan¹, D. Verstraete¹; ¹The University of Sydney, Australia INFLUENCE OF MOTOR CHARACTERISTICS ON OPTIMAL PROPROTOR DESIGN |
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ICAS2024_0341: Z. Liu¹, R. Ruan¹, L. Cheng¹, Y. Zhang¹, Z. Liu¹, D. Wu¹; ¹Northwestern Polytechnical University, China AN EXPERIMENTAL SIMULATION ON THE INFLUENCE OF DIFFERENT FILM COOLING HOLE SHAPES ON PARTICLE DEPOSITION ON TURBINE VANE |
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ICAS2024_0342: D. Li¹, Z. Ge¹, R. Cui¹, L. Yang¹, C. Wei¹, W. Song, Northwestern Polytechnical University, China; ¹AVIC Aerodynamics Research Institute, China AERODYNAMIC OPTIMIZATION OF HIGH-ALTITUDE PROPELLER COMBINED WITH MACHINE LEARNING METHOD |
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ICAS2024_0419: K. Han, China; S. Yu, China; J. Huang, China; J. Bai, China; Y. Qiu, China AERODYNAMIC PERFORMANCE OF BLADELESS DUCTED FAN BASED ON EJECTION EFFECT WITH DIFFERENT DESIGN VARIABLES |
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ICAS2024_0432: L. Palanti¹, L. Mazzei¹, C. Bianchini¹, S. Link², K. Dave², F. De Domenico², A.G. Rao²; ¹Ergon Research, Italy; ²TU Delft, Netherlands CFD-BASED SCOUTING FOR THE DESIGN OF A MULTI-FUEL KEROSENE/HYDROGEN ATMOSPHERIC BURNER |
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ICAS2024_0442: J. Hellgren¹, M. Persson¹, H. Alfredsson¹; ¹RISE Research Institutes of Sweden, Sweden AIRPORT CHARGING SYSTEM DESIGNS AND POWER MANAGEMENT FOR MEGAWATT-LEVEL CHARGING OF BATTERY-ELECTRIC AIRCRAFT |
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ICAS2024_0450: Z. Li¹, C. Liu¹, P. Liu¹, Y. Wang¹, X. Jin¹, S. Ding¹; ¹Research Institute of Aero-Engine, Beihang University, China FAST PREDICTION METHOD FOR RADIAL GROWTH OF LABYRINTH SEAL CLEARANCE BASED ON TRANSIENT THERMAL-FLUID COUPLING NETWORK |
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ICAS2024_0512: S. Tsentis¹, I. Goulos¹, S. Prince¹, V. Pachidis¹, V. Zmijanovic, Reaction Engines Ltd, United Kingdom; ¹Cranfield University, United Kingdom BASE FLOW CHARACTERISTICS FOR A SUB-SCALE HIGH-SPEED EXHAUST AT OVER-EXPANDED MODE |
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ICAS2024_0518: B.O. Cakir¹, D. Sanned¹, P. Vauquelin¹, M. Prakash¹, J.-P. Hannappel¹, A. Subash¹, M. Richter¹, X.-S. Bai¹, C. Fureby¹; ¹Lund University, Sweden EXPERIMENTAL AND NUMERICAL INVESTIGATIONS OF A SWIRL-STABILIZED JET ENGINE COMBUSTOR |
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ICAS2024_0622: T. Matuschek¹, J. Häßy¹, M. Schmelcher¹, A. Görtz¹; ¹German Aerospace Center (DLR), Germany PERFORMANCE ASSESSMENT OF AN ENGINE-INTEGRATED CLOSED-AIR COOLING THERMAL MANAGEMENT SYSTEM IN A NEXT GENERATION FIGHTER CONFIGURATION |
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ICAS2024_0708: J. Juracka¹, Z. Hubnerova¹; ¹Brno University of Technology, Czech Republic FUEL CONSUMPTION MONITORING OF TURBOPROP ENGINE |
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ICAS2024_0712: T. Qiu¹, S. Bao¹, S. Ding, Civil Aviation University of China, China; Q. Ma¹, X. Wang¹, C. Gan¹; ¹Beihang University, China SUSTAINABLE FUELS SAFETY BOUNDARIES DEMARCATION METHOD |
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ICAS2024_0720: L.W. Li¹, T.L. Dong¹, W.T. Ji¹, J.M. Wu¹; ¹Xi'an Jiaotong University, China EFFECTS OF SHAPE AND STREAMWISE SPACING OF PIN-FINS ARRAYS ON FLOW AND HEAT TRANSFER |
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ICAS2024_0726: C. Dosne¹, R. Barrier¹, S. Bourasseau¹, M. Carini¹, A. Dumont¹, J. Peter¹; ¹ONERA, France GRADIENT-BASED OPTIMIZATION OF AN AXIAL COMPRESSOR UNDER INLET DISTORTION USING BODY-FORCE MODELING |
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ICAS2024_0738: H. Murphy¹, C. Gallagher¹, C. Stuart¹, S. Spence¹, S. Fitzgerald, Ryanair DAC, Ireland; ¹Dept. of Mechanical Engineering, Trinity College Dublin, Ireland EVALUATION AND SIMULATION OF PARALLEL HYBRID ELECTRIC PROPULSION WITH REAL FLIGHT DATA |
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ICAS2024_0865: M. Zhang¹, J. Jiao¹, J. Zhang¹, Z. Zhang¹; ¹Chinese Academy of Sciences, China LOW ENERGY CONSUMPTION DESIGN METHOD AND STRATEGY FOR HIGH-ALTITUDE PROPELLERS BASED ON FLIGHT PROFILE |
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ICAS2024_0896: J. García-Tíscar¹, P. Quintero¹, F.N. Ramírez¹, A. Cremades, KTH Royal Institute of Technology, Sweden; ¹Universitat Politècnica de València, Spain EFFECT OF POPULAR ADDITIVE MANUFACTURING TECHNOLOGIES ON THE PERFORMANCE AND ACOUSTICS OF UAV PROPELLERS |
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ICAS2024_0919: Q.-L. Li¹, L. Zhou¹, Z.-X. Wang¹, X.-B. Zhang¹, S. Huang¹; ¹Northwestern Polytechnical University, China AERODYNAMIC DEFORMATION EXPERIMENT OF SERPENTINE NOZZLE FOR TURBOFAN AND ANALYSIS OF FLUID-STRUCTURE INTERACTION METHOD |
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ICAS2024_0920: M.-X. Wang¹, L. Zhou¹, J.-W. Shi¹, W.-J. Deng¹, H. Xiao¹; ¹Northwestern Polytechnical University, China EXPERIMENTAL AND NUMERICAL INVESTIGATION ON SEPARATION CHARACTERISTICS OF SERPENTINE CONVERGENT-DIVERGENT NOZZLE |
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ICAS2024_0924: L. Pugliese¹, D. Ferretto¹, R. Fusaro¹, N. Viola¹; ¹Politecnico di Torino, Italy COMPARISON OF LIFE CYCLE COST FOR MACH 8 AND MACH 5 HYPERSONIC PASSENGERS AIRCRAFT |
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ICAS2024_0940: X. Xiong¹, S. Wu¹; ¹International WYNNBEAR Advanced AeroTech Innovation, United States NOVEL SOFTWARE-DRIVEN VARIABLE-PITCH AND LEVEL FLIGHT CONTROL SYSTEM: PRINCIPLES AND APPLICATIONS FOR SMALL AIRCRAFT WITH A QUADROTOR CASE STUDY |
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ICAS2024_0973: J.H. Jeong, Korea Aerospace Research Institute, South Korea; J.W. Ko, Korea Aerospace University, South Korea PSYCHOACOUSTICAL ANALYSIS OF SYNTHESIZED MOTOR-PROPELLER ROTOR SYSTEM NOISE |
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ICAS2024_1003: P. Marocco¹, M.C. Massaro¹, A.H.A. Monteverde¹, M. Santarelli¹; ¹Politecnico di Torino, Italy ASSESSING THE TECHNICAL VIABILITY OF ALL-ELECTRIC HYDROGEN-POWERED AIRCRAFTS |
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ICAS2024_1011: L. Liu¹, L. Zeng¹, T. Wang¹, Z. Gao¹, X. Shao¹; ¹Zhejiang University, China DEEP LEARNING BASED FAST PREDICTION OF AERODYNAMIC PARAMETERS FOR DUCTED PROPELLERS |
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ICAS2024_1012: L. Zhang, China; T.-T. Jing, China; X. Sun, China; T. Gao, China; Z. Xu, China; F. Qin, China MULTI-DIMENTIONAL DESIGN AND THERMAL PROTECTION CAPABILITY OF A REGENERATIVE COOLED RBCC VARIABLE-GEOMETRY COMBUSTOR |
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ICAS2024_1027: K. Fong¹, P. Norman¹, C.E. Jones¹; ¹University of Strathclyde, United Kingdom SAFETY-DRIVEN BASELINING OF HYBRID ELECTRIC AIRCRAFT ELECTRICAL POWER SYSTEM ARCHITECTURES |
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ICAS2024_1054: A. Link¹, S. de Graaf¹; ¹German Aerospace Center (DLR), Germany PROJECTION OF KEY POWERTRAIN COMPONENT FIGURES OF MERIT FOR OVERALL ASSESSMENT OF ELECTRIC FLIGHT SCENARIOS |
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ICAS2024_1069: K. Ziaja¹, D. Lieder², J. Göing², J. Friedrichs², F. di Mare¹; ¹Ruhr University Bochum, Germany; ²Technische Universität Braunschweig, Germany DESIGN APPROACH FOR HYBRID ELECTRIC PROPULSION CONCEPTS OF MID-RANGE AIRCRAFT INCLUDING SUSTAINABLE AVIATION FUELS |
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ICAS2024_1103: A. Johansson¹, P. Miltén¹, A. Lundbladh, GKN Aerospace, Sweden; C. Xisto¹; ¹Chalmers University of Technology, Sweden MODELLING A HYDROGEN FUELLED COMPOSITE CYCLE AEROENGINE |
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ICAS2024_1109: A. Batra¹, R. Raute, Dept. Ind. Elec. Eng. University of Malta, Malta; R. Camilleri¹; ¹INSTITUTE OF AEROSPACE TECHNOLOGIES (IAT), UNIVERSITY OF MALTA, Malta A SENSITIVITY ANALYSIS ON THE ENDURANCE EQUATION FOR HYBRID-ELECTRIC AIRCRAFT |
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ICAS2024_1125: C. Fischer, 1Instituto Federal de São Paulo and Aeronautics Institute of Tec, Germany; M.A.R. Diaz¹, L. Souza¹, R.G.A. da Silva¹, L.C.S. Goes¹; ¹Aeronautics Institute of Technology, Brazil INSTRUMENTATION OF A SUBESCALE GROUND EFFECT VEHICLE, VOLITAN, TO MEASURE FLIGHT PROPULSION EFFICIENCY |
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ICAS2024_1129: F.G. Schiavone¹, M. Durand², M. Torresi¹, S.M. Camporeale¹, T. Schuller², D. Laera¹; ¹Polytechnic University of Bari, Italy; ²Institut de Mécanique des Fluides de Toulouse, France EXPERIMENTAL AND NUMERICAL INVESTIGATION OF NOISE GENERATION IN HYDROGEN AND METHANE-HYDROGEN LAMINAR FLAMES |
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ICAS2024_1132: R. Lopusiewicz¹, N. Ksiazek¹; ¹AGH University of Krakow, Poland CHALLENGES OF INTEGRATING PHOTOVOLTAIC CELLS ONTO THE WINGS OF AN UNMANNED SOLAR-POWERED AIRCRAFT |
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ICAS2024_1147: D. Del Gatto¹, S. Adamidis¹, C. Mourouzidis¹, S. Brown¹, V. Pachidis¹; ¹Cranfield University, United Kingdom DESIGN SPACE EXPLORATION OF NEXT-GENERATION SUPERSONIC BUSINESS JET ENGINE WITH A FOCUS ON LANDING AND TAKE-OFF (LTO) NOISE |
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ICAS2024_1157: M. Crona¹, S. Dinger¹, P. Samuelsson¹, H. Strömfeldt¹, I. Jonsson¹; ¹Chalmers University of Technology, Sweden LOW-SPEED PROPELLER FOR UAV APPLICATIONS, FROM DESIGN TO EXPERIMENTAL EVALUATION |
6.1 - Flight Dynamics and Control (Control & Modelling) |
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ICAS2024_0008: X. Wang¹, M. Yang¹, P. Ma¹, T. Chao¹; ¹Harbin Institute of Technology, China LINEAR QUADRATIC PURSUIT AND EVASION DIFFERENTIAL GAME GUIDANCE STRATEGY WITH OBSTACLE AVOIDANCE |
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ICAS2024_0043: Y. Lee¹, J. Kim¹, Y. Kim¹; ¹Seoul National University, South Korea LEARNING-BASED FULL-ENVELOPE AUTOPILOT DESIGN BASED ON THE KOOPMAN OPERATOR THEORY |
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ICAS2024_0044: P. Piprek¹, P.M. Dias¹, J. Tonti¹, D. Schwalb¹; ¹Airbus Defence and Space GmbH, Germany APPLICATION OF CLUSTERING TECHNIQUES IN OPTIMISATION-BASED FLIGHT CONTROL SYSTEM CLEARANCE |
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ICAS2024_0185: J. Che¹, X. Chen¹, S. Che, Northwestern Polytechnical University, China; J. Li¹, Z. Sun¹; ¹Flight Automatic Control Research Institute, AVIC, China SYSTEM ARCHITECTURE AND EVALUATION METHOD OF HUMAN-MACHINE COLLABORATION IN FLIGHT CONTROL SYSTEM |
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ICAS2024_0223: K.H. Kienitz, Instituto Tecnologico de Aeronautica, Brazil; A. Gonzalez Sorribes¹, R. Sanz Diaz¹, C. Braga de Mendonça, Boeing Brasil, Brazil; P.J. Garcia¹; ¹Universitat Politecnica de Valencia, Spain STRUCTURED H-INFINITY DESIGN OF PREDICTORS FOR THE MONITORING OF AN AIRCRAFT IN ITS FLIGHT ENVELOPE |
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ICAS2024_0317: P. Månsson, Saab AB, Sweden INFLUENCE OF CONTROL POWER RATE ON HIGH-ALPHA ROLL MANOEUVRABILITY |
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ICAS2024_0355: T. Goetzendorf-Grabowski¹, L. Kiszkowiak², A. Kwiek¹, P. Zalewski², K. Chudy², M. Figat¹; ¹Warsaw University of Technology, Poland; ²Military University of Technology, Poland STUDY ON CONFIGURATIONS OF AIRBORNE LAUNCH SYSTEM FOR DELIVERY OF SMALL PAYLOAD TO LOW EARTH ORBIT |
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ICAS2024_0364: J. Gauci, University of Malta, Malta; B. Zammit, Malta; M. Galea, Malta A GENETIC ALGORITHM FOR TRAJECTORY GENERATION IN ENGINE-OUT EMERGENCY LANDING SCENARIOS OF COMMERCIAL AIRCRAFT |
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ICAS2024_0424: H. Lee¹, S. Lee¹; ¹Korea Aerospace University, South Korea A COMPARSION OF TRAJECTORY GENERATION ALGORITHMS FOR A TERRAIN FOLLOWING FLIGHT |
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ICAS2024_0468: C.-G. Jung¹, C.-H. Lee¹, M.-J. Tahk¹; ¹Korea Advanced Institute of Science and Technology(KAIST), South Korea TRAJECTORY OPTIMIZATION FOR LONG-RANGE AIR-LAUNCHED GLIDING VEHICLES USING CONVEX PROGRAMMING |
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ICAS2024_0478: Z.Y. Yuan¹, W.Y. Yang¹, J.X. Xuan¹; ¹nwpu, China ATTITUDE CONTROL DESIGN FOR A FLYING-CRAWLING INTEGRATED FLAPPING-WING MICRO AIR VEHICLE |
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ICAS2024_0491: M. Naruoka¹, T. Ninomiya¹; ¹Japan Aerospace Exploration Agency, Japan DATA ORIENTED EVALUATION OF FLIGHT CHARACTERISTIC MODELS BY USING BAYES FACTOR |
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ICAS2024_0494: C. Santoro¹, S.R. Bassolillo, University of Naples Parthenope, Italy; A. Ferraro, University of Reggio Calabria Mediterranea, Italy; L. Blasi¹, I. Notaro¹; ¹University of Campania L. Vanvitelli, Italy A MODEL PREDICTIVE CONTROL ALGORITHM FOR THE FORMATION CONTROL OF NANOSATELLITES IN LEO ORBIT |
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ICAS2024_0601: J. Diepolder¹, J.Z. Ben-Asher¹; ¹Technion, Israel INTEGRATING POST-OPTIMAL SENSITIVITIES INTO SUPERVISED TRAINING OF NEURAL NETWORKS |
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ICAS2024_0613: H. Wilke¹, G.C. Silva¹, F.J. Silvestre¹; ¹Technische Universität Berlin, Germany AILERON-FLAP-INTEGRATED ROLL CONTROL LAW BY OPTIMIZED CONTROL ALLOCATION FOR FLEXIBLE TRANSPORT AIRCRAFT |
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ICAS2024_0621: C. Zhai¹, B. Song¹, Q. Fu¹, J. Xuan¹, J. Li¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China DYNAMICS ANALYSIS AND CONTROL OF A LARGE WINGSPAN FLAPPING-WING VEHICLE |
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ICAS2024_0627: M.-W. Kang¹, D.-W. Lee², S.-H. Yun¹, H.-C. Bang²; ¹ADD, South Korea; ²KAIST, South Korea DATA-DRIVEN MODEL DISCOVERY AND CONTROL OF HIGH-PERFORMANCE TRAINER AIRCRAFT VIA SPARSE IDENTIFICATION OF NONLINEAR DYNAMICS |
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ICAS2024_0646: Y. Wang¹, M. Sun¹, J. Fu¹; ¹Beihang University, China VALIDATION OF ENERGY CHARACTERISTICS IN FLIGHT CONTROL SYSTEM BASED ON A MULTIDISCIPLINARY VIRTUAL PLATFORM |
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ICAS2024_0647: F.C. Antoniazzi¹, A.G.P. Sarmento¹, E. Villani¹; ¹Aeronautical Institute of Technology, Brazil FAULT DETECTION FOR AN AIRCRAFT ELEVATOR |
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ICAS2024_0805: S. Kolb, CREA, France PILOT INDUCED OSCILLATIONS AND FLIGHT PHASES IDENTIFICATION OF THE SPACE SHUTTLE AND TRANSPORT AIRPLANES |
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ICAS2024_0819: T. Jann¹, N. Fezans¹, A. Koloschin¹, S.-O. Schmidt¹, P. Link¹, J. Ament¹, S. Krause¹; ¹German Aerospace Center (DLR), Institute of Flight Systems, Germany ASSISTED AND AUTOMATED AERIAL REFUELLING – OVERVIEW OF THE CONDUCTED RESEARCH AT THE GERMAN AEROSPACE CENTER (DLR) |
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ICAS2024_0828: M. Shin¹, M.-J. Tahk¹, B. Kim¹, C.-H. Lee¹; ¹Korea Advanced Institute of Science and Technology, South Korea PURSUIT-BASED LONG-RANGE AIR-TO-AIR MISSILE MIDCOURSE GUIDANCE ROBUST TO CHANGES IN THE PREDICTED IMPACT POINT |
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ICAS2024_0839: J.-I. Jang¹, C.-H. Lee¹, S. He, BIT, China; ¹KAIST, South Korea CONVEX PROGRAMMING APPROACH OF ROBUST POWERED DESCENT GUIDANCE THROUGH DYNAMIC TUBE MPC |
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ICAS2024_0861: D.B. Rossato, Faculdade de Tecnologia SENAI, Brazil; K.H. Kienitz, Instituto Tecnológico de Aeronáutica, Brazil SELF-DRIVING AND MODEL-BASED EXTREMUM SEEKING CONTROL IN TIGHT FORMATION FLIGHT FOR FUEL SAVING |
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ICAS2024_0890: J.-Q. Yan, School of Aeronautics, Northwestern Polytechnical University, China ENERGY PREDICTION DURING APPROACH AND LANDING BASED ON LONG SHORT-TERM MEMORY MODEL |
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ICAS2024_0891: T. Giusti Degaspare, Embraer S.A., Brazil; K.H. Kienitz, Instituto Tecnológico de Aeronáutica, Brazil APPLICATION OF A MORE INTEGRATED TOTAL ENERGY CONTROL SYSTEM FOR IMPROVING AIRCRAFT AND ENGINE CONTROL EFFICIENCY |
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ICAS2024_0892: K.-W. Jung¹, C.-H. Lee¹; ¹KAIST, South Korea DOWNRANGE CONTROL GUIDANCE FOR REENTRY BURN OF REUSABLE LAUNCH VEHICLE |
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ICAS2024_0938: R.K. Nangia¹, T. Nangia¹; ¹Nangia, United Kingdom GROUND EFFECT ON A SLENDER 65º DELTA WING WITH SIDESLIP, IMAGE METHOD, USING EULER |
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ICAS2024_0977: Y. Liu¹, Y.-H. Nong², X. Liu, Shanghai Aircraft Airworthiness Certification Center, China; Z.-H. Cheng², M.-X. Zhang¹; ¹Northwestern Polytechnical University, China; ²AVIC General Huanan Aircraft Industry, China MODELING AND FLIGHT CONTROL LAW DESIGN FOR A SEAPLANE DURING WATER SURFACE TAKEOFF |
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ICAS2024_1014: R. Vos¹, N. Johnson¹, S. Nolet¹; ¹TU Delft, Netherlands FLYING V DIRECTIONAL FLIGHT CONTROL: AN EXPERIMENTAL INVESTIGATION |
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ICAS2024_1044: J. Novák ¹, J. Hanák¹, P. Chudý¹; ¹BUT, Czech Republic PREDICTIVE CONTROL DRIVEN TACTICAL MANEUVERING |
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ICAS2024_1070: Z.-F. Luo¹, Y.-J. Lian, National University of Defense Technology, China; C. Zhang, Chinese Academy of Sciences, China; T. Zhang¹; ¹Sun Yat-sen University, China TRAJECTORY DESIGN FOR ASTEROID SAMPLE RETURN COMBINING BALLISTIC CAPTURE AND AEROBRAKING |
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ICAS2024_1087: C.-K. Zhou¹, Z.-F. Luo¹, T. Zhang¹; ¹SUN YAT-SEN UNIVERSITY, China REENTRY TRAJECTORY DESIGN FOR DEFORMABLE HYPERSONIC VEHICLES BASED ON NEURAL NETWORKS |
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ICAS2024_1115: C. Varriale¹, F. Yunus¹, M. Snellen¹; ¹Delft University of Technology, Netherlands OPTIMAL APPROACH AND DEPARTURE TRAJECTORIES WITH ACOUSTIC FOOTPRINT ASSESSMENT FOR AN AIR MOBILITY QUAD-ROTOR |
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ICAS2024_1119: C.R. Li¹, W.Q. Li¹, Y. Li¹, S. Tang¹; ¹Northwestern Polytechnical University, China A NOLINEAR MODEL PREDICTIVE CONTROL METHOD FOR AIRBREATHING HYPERSONIC VEHICLE BASED ON KOOPMAN OPERATOR |
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ICAS2024_1151: P. Schmollgruber¹, C. Toussaint¹, P. Iannelli, CIRA, Italy; H. Jentink, Royal NLR, Netherlands; D. Kierbel, Airbus S.A.S., France; ¹ONERA, France RESULTS OF THE SCALED FLIGHT DEMONSTRATOR FLIGHT TESTS |
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ICAS2024_1166: A. Comer¹, I. Chakraborty¹; ¹Auburn University, United States EXPLICIT MODEL FOLLOWING TRAJECTORY CONTROL SYSTEM FOR MULTIPLE VERTICAL TAKEOFF AND LANDING CONFIGURATIONS |
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ICAS2024_1182: C. Döll¹, S. Waitman¹; ¹ONERA, France CONTROL ALLOCATION FOR A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT USING DIFFERENTIAL THRUST |
6.2 - Flight Dynamics and Control (UAV related) |
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ICAS2024_0013: L.H. Wang¹, A.J. Li¹, C.Q. Wang¹, Z. Yury, Samara National Research University, Russia; ¹Northwestern Polytechnical University, China ROBUST SLIDING MODE CONTROL FOR UAV FORMATION WITH EXTERNAL DISTURBANCES UNDER EVENT-TRIGGERED STRATEGY |
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ICAS2024_0029: J. Novák ¹, J. Hanák¹, P. Chudý¹; ¹BUT, Czech Republic HYBRID MODELING APPROACH FOR OPTIMIZATION BASED CONTROL OF MULTIROTOR UNMANNED AERIAL VEHICLES |
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ICAS2024_0084: B.-Y. Qin¹, D. Zhang¹, S. Tang¹; ¹Northwestern Polytechnical University, China HAWK-INSPIRED COOPERATIVE ENCIRCLEMENT GUIDANCE OF FIXED-WING UAV SWARM WITH LIMITED COMMUNICATION IN THREAT SCENARIO |
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ICAS2024_0231: H. Shi¹, S. Li, AVIC Chengdu Aircraft Industrial (Group) Co., Ltd., China; Z. Huang¹, S. Li¹, A. Li¹, Y. Zhou¹; ¹BEIHANG UNIVERSITY, China MANNED AND UNMANNED AERIAL VEHICLES COOPERATIVE COMBAT FRAMEWORK BASED ON LARGE LANGUAGE MODELS |
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ICAS2024_0271: D.M. Gierszewski¹, P. Piprek¹, F. Holzapfel, Technische Universität München, Germany; ¹ Technische Universität München, Germany ONBOARD TRAJECTORY OPTIMIZATION FOR RADIUS TO FIX TURNS |
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ICAS2024_0294: H.J. Ahn¹, H.C. Bang¹; ¹KAIST, South Korea MEDIAL AXIS TRANSFORMATION-BASED CONVEX MODEL PREDICTIVE CONTROL FOR MULTIROTOR INDOOR AUTONOMOUS FLIGHT WITH FIXED ALTITUDE |
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ICAS2024_0310: Y.J. Hasan¹, N. Fezans¹, A. Voß, DLR Institute of Aeroelasticity, Germany; ¹DLR Institute of Flight Systems, Germany FLIGHT MECHANICAL ANALYSIS OF A VERY FLEXIBLE HIGH-ALTITUDE PLATFORM UNDER UNCERTAINTY CONSIDERATIONS |
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ICAS2024_0459: S.R. Bassolillo¹, G. Raspaolo², L. Blasi², E. D'Amato¹; ¹Università degli Studi di Napoli Parthenope, Italy; ²Università degli Studi della Campania L. Vanvitelli, Italy ENHANCING QUADCOPTER CONTROL: A MODEL REFERENCE ADAPTIVE CONTROL APPROACH WITH NEURAL NETWORKS |
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ICAS2024_0516: R.C. Silva¹, D.D. Bueno¹; ¹UNESP, Brazil DYNAMICS OF THE MECHANISM FOR VENTILATION ACROSS FEATHERS IN FLAPPING WING UAV |
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ICAS2024_0535: J.L. Kurniawan¹, P.B.A. Baylon¹, R.A. Sasongko¹; ¹Institut Teknologi Bandung, Indonesia A NOVEL APPROACH TO AUTOMATED TRACKING CONTROL OF HYBRID TILTING ROTOR UAVS USING LQG CONTROLLER AND STATE MACHINE |
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ICAS2024_0548: K. Miyabe¹, M. Bando¹, S. Hokamoto¹; ¹Kyushu Univercity, Japan STUDY ON CONTROL PERFORMANCE OF A NEW TYPE OF TILT-ROTOR AIRCRAFT |
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ICAS2024_0570: J. Cai¹, M. Lovera¹; ¹Politecnico di Milano, Italy PASSIVE FAULT TOLERANT CONTROL OF A DUAL-SYSTEM UAV IN TRANSITION FLIGHT |
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ICAS2024_0578: L. Wang¹, X. Yang¹, Y. Luo¹, H. Chen¹, J. Li¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China DESIGN OF ATTITUDE CONTROL SYSTEM FOR DRAGONFLY-INSPIRED FLAPPING WING AERIAL VEHICLE |
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ICAS2024_0608: G. Raspaolo, Italy; G. D'Alterio, Italy; I. Notaro, Italy; E. D'Amato, Italy A SIMULINK APPROACH TO MODELING HETEROGENEOUS DRONE FORMATIONS FOR AGENT-BASED SIMULATION |
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ICAS2024_0610: Y. Fan, China; Y. Sun, China; B. Mi, China FLIGHT CONTROL SYSTEM KNOWLEDGE GRAPH CONSTRUCTION BASED ON AERONAUTICAL DOMAIN KNOWLEDGE AUGMENTED LARGE LANGUAGE MODEL |
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ICAS2024_0653: H.-S. Lee¹, D.-W. Lee¹, H.-C. Bang¹; ¹KAIST, South Korea AERODYNAMIC MODEL IDENTIFICATION OF A VTOL TAILSITTER UAV USING SPARSE IDENTIFICATION OF NONLINEAR DYNAMICS |
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ICAS2024_0664: D. Kim¹, H.J. Kim¹; ¹Seoul National University, South Korea AUTONOMOUS LANDING OF A QUADROTOR ON A MOVING TARGET WITH OCCLUSION AVOIDANCE MANEUVER |
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ICAS2024_0713: D.F. Duda¹, H. Fuest¹, J. Müller¹, T. Islam¹, D. Moormann¹; ¹RWTH Aachen Unitversity, Germany INCREMENTAL NONLINEAR DYNAMIC INVERSION CONTROLLER FOR A FLYING WING OPERATED IN AN AIRBORNE WIND ENERGY SYSTEM |
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ICAS2024_0724: X. Zhou¹, M. Dziendzikowski², K. Dragan², M. Giglio³, L. Dong¹, C. Sbarufatti³; ¹Beihang University, China; ²Instytut Techniczny Wojsk Lotniczych, Poland; ³Politecnico di Milano, Italy ON THE DEVELOPMENT OF THE STRUCTURAL DIGITAL TWIN OF AN UNMANNED AERIAL VEHICLE |
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ICAS2024_0778: K. Mall¹, R. Gadre¹, J. Gerardus¹, D.A. DeLaurentis¹; ¹Purdue University, United States TRAJECTORY OPTIMIZATION OF EVTOL VEHICLES FOR URBAN AIR MOBILITY USING INDIRECT METHODS |
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ICAS2024_0794: H. Dai¹, Z. Wang¹, J. Ding¹, G. Li¹, C. Wang¹, L. He¹, H. Liu, Swinburne University of Technology, Australia; ¹Chinese Aeronautical Establishment, China FUZZING ON TARGET DETECTION SYSTEM OF UNMANNED AERIAL VEHICLE |
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ICAS2024_0795: E. D'Amato, Università degli Studi di Napoli Parthenope, Italy ADVANCED SOLUTIONS AND CHALLENGES IN MULTI-DRONE SYSTEMS FOR SEARCH AND RESCUE MISSIONS: TECHNICAL APPROACHES AND UNRESOLVED MATTER |
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ICAS2024_0879: J. Novák ¹, J. Hanák¹, P. Chudý¹; ¹BUT, Czech Republic MODEL PREDICTIVE CONTROL DRIVEN AERIAL GRASPING WITH SOFT OPERATIONAL CONSTRAINTS |
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ICAS2024_0897: D. Pla Guerrero¹, A. Hegde¹, J. Wan, Flanders Make, Belgium; E. Allegaert¹, Y. Lemmens¹; ¹Siemens Digital Industries Software, Belgium HARDWARE-IN-THE-LOOP SIMULATION FRAMEWORK FOR THE EVALUATION OF AUTONOMOUS FLIGHT FUNCTIONS |
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ICAS2024_0947: G. Charruaz¹, A. Borgia¹, A. Braghin¹, T. Bussi¹, A. Esposito¹, A. Pescosolido¹; ¹Politecnico di Torino, Italy FLIGHT PERFORMANCE AND DYNAMICS OF AN UNCONVENTIONAL SOLAR POWERED UAS |
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ICAS2024_0972: H.-X. Huang¹, D.-B. Li¹, P.-Y. Qi¹, Y.-X. Shang¹; ¹beihang university, China ULTRA-LOW-ALTITUDE PENETRATION PATH PLANNING FOR FIXED-WING AIRCRAFT BASED ON NMP ALGORITHM |
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ICAS2024_0980: Y. Hayashi¹, J.-H. Kim¹, T. Tsuchiya¹; ¹The University of Tokyo, Japan IN-FLIGHT MEASUREMENT OF WING SURFACE PRESSURE DISTRIBUTION ON A FIXED-WING UAV AND ITS APPLICATION TO FLIGHT CONTROL |
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ICAS2024_0984: I.A. Iliopoulos¹, J.S. Korolis¹, S.D. Fassois¹, J.S. Sakellariou¹; ¹University of Patras, Greece IN-FLIGHT VIBRATION SIGNAL BASED DETECTION AND LOCALIZATION FOR UAV PROPELLER ANOMALIES UNDER UNCERTAINTY VIA MACHINE LEARNING TYPE METHODS |
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ICAS2024_1020: K. Li¹, K. Zhang¹, H. Liu², Y. Li², Q. Wang¹; ¹Northwestern Polytechnical University, China; ²Shenyang Aircraft Design and Research Institute, China AN UAV MANEUVERING DECISION-MAKING ALGORITHM BASED ON DEEP TRANSFER REINFORCEMENT LEARNING |
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ICAS2024_1100: C. Fischer, Instituto Federal de São Paulo and Aeronautics Institute of Tec, Brazil; A.S. Davi, Lilium GmbH, Germany; R.G.A. da Silva¹, L.C.S. Goes¹; ¹Aeronautics Institute of Technology, Brazil DYNAMIC FREE FLIGHT TESTS WITH A SUB-SCALE AIRPLANE DESIGNED ACCORDING TO THE FROUDE NUMBER |
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ICAS2024_1136: A. Boldrini¹, G. Gozzini¹, D. Invernizzi¹; ¹Politecnico di Milano, Italy ADAPTIVE CONTROL AND MISSION PLANNER DESIGN FOR UAV OPERATIONS WITH BATTERY MANAGEMENT |
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ICAS2024_1176: V.P. Fernandes¹, T.R. Paula¹, R.C. Nascimento¹, R.G.A. Silva¹, L.C.S. Góes¹; ¹ITA - Instituto Tecnológico de Aeronáutica, Brazil FLIGHT PATH RECONSTRUCTION OF A FLEXIBLE WING UAV WITH WING MOUNTED VANES |
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ICAS2024_1209: A. Bagherzadeh¹, F. Saghafi¹; ¹Sharif University of Technology, Iran AN OPTICAL FLOW BASED GUIDANCE ALGORITHM FOR A QUADROTOR UAV MOVING INSIDE CIRCULAR CORRIDORS |
7 - Systems, Subsystems and Equipment |
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ICAS2024_0033: G.-M. Li¹, W.-T. Xie¹; ¹AVIC XI’AN Aeronautics Computing Technique Research Institute, China THE DESIGN FOR TESTABILITY OF CIVIL AIRCRAFT AVIONICS SYSTEMS |
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ICAS2024_0046: C. Deiler, DLR, Germany FLIGHT TEST RESULTS FOR PERFORMANCE-BASED ICE DETECTION |
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ICAS2024_0056: M. Rovelli¹, A. Brandl¹, S. Di Bitonto¹, F. Di Donfrancesco¹, E. Maruccia¹, I. Viglietti¹, D. Marchetti¹; ¹Leonardo, Italy HYBRID AIR DATA SYSTEM ARCHITECTURE: FROM DESIGN TO FLIGHT TEST VERIFICATION |
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ICAS2024_0085: F. Cuomo¹, C. Musto¹, S. Bozhko, University of Nottingham, United Kingdom; B. Guida, Aeromechs srl, Italy; ¹Leonardo Aircraft, Italy SMART ELECTRIC POWER MANAGEMENT ONBOARD FUTURE AIRCRAFT |
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ICAS2024_0123: R. Tirschmann¹, D. Metzler², T. Koch², M. Spieler¹, W. Nendel¹, L. Kroll¹; ¹Technische Universität Chemnitz, Germany; ²Liebherr-Aerospace Lindenberg GmbH, Germany SIMULATION AND VERIFICATION OF HYDRAULIC ROTOR GAP PARAMETERS OF A NOVEL HIGH EFFICIENT WET ELECTRO MOTOR PUMP FOR AEROSPACE APPLICATIONS |
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ICAS2024_0146: M.N. Duval¹, T. Lammering¹; ¹Liebherr-Aerospace Lindenberg GmbH, Germany DEVELOPMENT OF AN ELECTRO-HYDROSTATIC NOSE LANDING GEAR ACTUATION AND STEERING SYSTEM |
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ICAS2024_0149: O. Petrella¹, A. Martucci¹, P. Caruso¹, L. Travascio¹, A. Vozella¹; ¹CIRA, Italy HYDROGEN SAFETY: A COMPARATIVE ANALYSIS OF LEAK DETECTION SENSORS |
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ICAS2024_0156: C. Raab¹, N. Fezans¹; ¹DLR (German Aerospace Center) - Institute for Flight Systems, Germany MEASURING THE ANGLE OF ATTACK – PRACTICAL CONSIDERATIONS FOR THE DEVELOPMENT OF FAULT DETECTION RESIDUALS |
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ICAS2024_0171: M. Schäfer¹, R. Keimer¹, O. Bertram¹; ¹German Aerospace Center (DLR), Germany DEVELOPMENT AND TESTING OF AN ACTUATION SYSTEM FOR A MORPHING CONTROL SURFACE |
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ICAS2024_0178: C.W. Schwarz¹, C. Deiler¹, J. Lucke¹, T. Jurkat-Witschas¹, A. Orazzo², B. Thillays²; ¹DLR, Germany; ²Safran Aerosystems, France SENS4ICE EU PROJECT HYBRID ICE DETECTION ARCHITECTURES DEMONSTRATION RESULTS |
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ICAS2024_0194: H.-C. Ma¹, T. Guo¹, G.-D. Li¹, J.-B. Bai¹; ¹Aviation Industry Corporation of China-The First Aircraft INST, China CONFIGURATION ANALYSIS OF INTEGRATED THERMAL MANAGEMENT BASED ON THE TURBINE-FAN REFRIGERATION SYSTEM |
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ICAS2024_0244: S. Sun¹, H. Wang¹, R. Liu¹, S. Kuang¹, W. Chen¹; ¹Civil Aviation University of China, China INTEGRITY MONITORING OF TIGHTLY INTEGRATED BDS/SINS USING MULTI-HYPOTHESIS SOLUTION SEPARATION (MHSS) ALGORITHM |
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ICAS2024_0270: A. Dell’Amico, Linköping University, Sweden DESIGNING A HARDWARE-IN-THE-LOOP SIMULATION TEST BED FOR AIRCRAFT ENERGY MANAGEMENT APPLICATIONS |
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ICAS2024_0295: E. Revello¹, M. Boccaccio, Leonardo Labs, Italy; F. Acerra, Leonardo SpA, Italy; A. Monteverde¹; ¹Politecnico di Torino, DISAT, Italy POTENTIAL APPLICATION OF PHASE CHANGE MATERIALS FOR THERMAL MANAGEMENT SYSTEM OF NEXT GENERATION AIRCRAFT |
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ICAS2024_0425: H. Lee¹, H. Lee¹, S. Lee¹; ¹Korea Aerospace University, South Korea DEVELOPMENT OF THRUST CONTROL SYSTEM FOR SPACECRAFT’S DOCKING MANEUVER |
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ICAS2024_0440: C. Koopman¹, D. Zammit-Mangion¹; ¹University of Malta, Malta ENHANCED SAFETY THROUGH AI: AN ASSESSMENT OF ADVERSARIAL REINFORCEMENT LEARNING FOR CONTROL OF COMPLEX AIRCRAFT |
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ICAS2024_0467: D. Milz¹, M. May¹, J. Martins¹, R. Kuchar¹, G. Looye¹; ¹German Aerospace Center (DLR), Germany FAILURE HANDLING ON A SPLIT-FLAP ULTRALIGHT GENERAL AVIATION AIRCRAFT WITH HYBRID NONLINEAR DYNAMIC INVERSION |
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ICAS2024_0483: A. Aimasso¹, M. Bertone¹, C. Ferro¹, M.D.L. Dalla Vedova¹, P. Maggiore¹; ¹Politecnico di Torino, Italy PRELIMINARY ANALYSIS OF TEMPERATURE EFFECTS AND MANEUVER-INDUCED DEFORMATIONS ON FBG OPTIC FIBER INTEGRATED SYSTEMS |
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ICAS2024_0504: R. Fallucca¹, A. Iannuzzo¹, S. Gallina¹, E. Cestino¹, V. Sapienza, Aeronautical Engineering Consultant, Italy; ¹Politecnico di Torino, Italy EXPERIMENTAL RESULTS OF ANTENNA PLACEMENT TEST ON A CARBON-FIBER SCALE REPLICA OF THE S55X SEAPLANE |
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ICAS2024_0511: S. Wehrend¹, K. Zumach¹, L. Schwan¹, D. Krause¹; ¹Hamburg University of Technology (TUHH), Germany TOWARDS A HOLISTIC APPROACH TO INCREASE SUSTAINABILITY IN AIRCRAFT CABIN DESIGN |
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ICAS2024_0520: T. Aresi¹, A. Zanoni¹, G. Cassoni¹, P. Masarati¹; ¹Politecnico di Milano, Italy SIMPLIFIED MODELS OF PILOT BIOMECHANICS FOR ROTORCRAFT VERTICAL BOUNCE ANALYSIS |
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ICAS2024_0529: Q. Yin¹, Y. Quan¹, L. Ma¹, J. Liu¹, J. Chai¹, J. Liu¹, L. Zhang¹; ¹Beihang University, China ANGLE AND DISTANCE EFFECT ON PHOSPHOR THERMOMETRY |
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ICAS2024_0674: X. Hu¹, Y. Fu¹, D. Lyu¹, M. Sun¹, S. Zhao, Beijing Institute of Precision Mechatronics and Controls, Labora, China; J. Fu¹, J. Zhao¹; ¹School of Mechanical Engineering and Automation, Beihang Univers, China RESEARCH ON MODELING THE TEMPERATURE FIELD OF A NEW AEROSPACE SERVO ELECTRO-HYDROSTATIC MODULE BASED ON THERMO-MAGNETIC BIDIRECTIONAL COUPLING ANALYSIS |
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ICAS2024_0678: S. Yang¹, S. Huang¹, Y. Wang¹, Y.-P. Huang¹; ¹CHRDI, China VIBRATION ANAYLYSIS AND INFLUENCING FACTOR STUTY OF HELICOPTER HYDRAULIC PIPELINNE |
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ICAS2024_0697: Y. Zhang¹, Y. Yang², Q. Xiao², R. Li¹, Z. Xu¹; ¹Northwestern polytechnical University, China; ²China Academy of Launch Vehicle Technology, China AN IMPROVED END-TO-END STAR MAP RECOGNITION METHOD FOR AEROSPACE VEHICLE |
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ICAS2024_0731: Q.-H. Nghiem¹, T.-G. Nguyen¹, B.-M. Pham¹, P.-M. Nguyen¹; ¹Viettel Aerospace Institute, Vietnam AERODYNAMIC DESIGN METHODOLOGY OF A NON-UNIFORM PERFORATED INVERSE CONICAL FLOW SPREADER IN INTERMITTENT BLOW DOWN WIND TUNNEL |
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ICAS2024_0735: M.-W. Sun¹, J. Fu¹, D.-C. Lyu¹, J.-C. Mare, ICA, INSA-Toulouse, France; ¹Beihang University, China MODEL-BASED DESIGN OF ACTIVE/ACTIVE ELECTRO-HYDROSTATIC ACTUATION FOR HELICOPTER FLIGHT CONTROLS |
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ICAS2024_0737: T.-G. Nguyen¹, Q.-H. Nghiem¹, P.-M. Nguyen¹; ¹Viettel Aerospace Institute, Vietnam NUMERICAL METHOD FOR DESIGNING AND MODELING AN EXHAUST CLUSTER FOR A SMALL TURBOJET ENGINE TEST CELL |
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ICAS2024_0755: C.C.D. Silva¹, Y. Castro¹, A. Sarmento¹, E. Villani¹; ¹ Instituto Tecnológico de Aeronáutica, Brazil MULTIPLATFORM SIMULATION USING ROS |
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ICAS2024_0786: N.L. Ywet¹, A.A. Maw¹, J.W. Han¹, J. Chung, Toronto Metropolitan University, Canada; J.W. Chang, Korea Aerospace University, South Korea; J.-W. Lee¹; ¹Konkuk University, South Korea ENHANCED AIRCRAFT TAKEOFF/LANDING SAFETY USING DEEP LEARNING MODEL IN RUNWAY ASSISTANCE SYSTEM |
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ICAS2024_0866: Y. Ding¹, D. Xu¹, Y. Li¹, Z. Fang¹, T. Chen¹, H. Zhang, Airforce Engineering University, China; B. Chen, Shanghai University, China; ¹Aviation Industry of China (AVIC), China ATTITUDE ESTIMATION USING KALMAN FILTERING FOR SPACEBORNE SAR SYSTEMS |
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ICAS2024_0932: S. Yang¹, Y. Long, School of Energy and Power Engineering, Beihang University, China; Z. Hu¹; ¹Institute for Aero Engine, Tsinghua University, China EXPLORING A CATEGORY OF LIMIT CYCLE OSCILLATIONS IN AIRCRAFT HYDRAULIC SYSTEMS |
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ICAS2024_1010: J.-W. Xie¹, P.-F. Zhu¹, J.-P. Hu¹, Y.-G. Lyv¹, Z.-X. Liu¹; ¹Northwestern Polytechnical University, China VOID FRACTION CALCULATION MODEL BASED ON TWO-PHASE FLOW PATTERNS IN THE SCAVENGE PIPE |
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ICAS2024_1028: B. Yuan¹, S. Zhang¹, B. Wang, School of Electronic and Information, Northwestern Polytechnica, China; K. Zhang, School of Electronic and Information, Northwestern Polytechnical, China; ¹College of Aerospace Science and Engineering, National Universit, China MULTI SENSOR AND MULTI TASK ALLOCATION BASED ON IMPROVED WHALE OPTIMIZATION ALGORITHM |
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ICAS2024_1030: S. Zhang, China; P.-F. Zhu, China; H. Fan, China; Z.-X. Liu, China A STUDY ON THE AIRLOCK MECHANISM OF THE OIL SUPPLY PUMP IN AERO-ENGINE LUBRICATING OIL SYSTEM |
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ICAS2024_1043: C. Jiang¹, Y. Shang¹, T. Yu¹, Z. Liu¹, M. Li¹; ¹Beihang University, China MODELING AND ANALYSIS OF ELECTRO-HYDROSTATIC ACTUATORS EFFICIENCY |
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ICAS2024_1050: G. Di Rito¹, A. Suti¹; ¹University of Pisa - Dept. of Civil and Industrial Engineering, Italy PRELIMINARY DESIGN OF POWER CONTROL STRATEGIES FOR THE HYBRID-ELECTRIC PROPULSION SYSTEM OF A LIGHTWEIGHT FIXED-WING UAV |
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ICAS2024_1072: A. Wise¹, S. Bozhko¹, S. Yeoh¹, S. Sumsurooah¹, C. Manrique, Leonardo S.p.A, Italy; ¹University of Nottingham, United Kingdom DUAL STAGE BATTERY SIZING AND PERFORMANCE ASSESSMENT ON-BOARD HYBRID ELECTRIC AIRCRAFT |
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ICAS2024_1093: J.A. Herrera Velasco, National Autonomous University of Mexico (UNAM), Mexico; H.S. Delgado Guevara, UNAM, Mexico DEVELOPMENT OF UAVS/DRONES EQUIPPED WITH THERMAL SENSORS FOR THE SEARCH OF INDIVIDUALS LOST UNDER RUBBLE DUE TO EARTHQUAKE COLLAPSES OR ANY EVENTUALITY REQUIRING SUCH CAPABILITIES |
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ICAS2024_1187: M.A.D. Di Marzo¹, O.A. Gonzatto Junior¹, H.N. Najafabadi, Linköping University – LiU, Sweden; J.H. Bidinotto¹; ¹University of São Paulo - USP, Brazil NONLINEAR BEHAVIOR IN AIRCRAFT FUEL GAUGE READINGS: AN EXPLORING ANALYSIS |
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ICAS2024_1205: G. di Mauro¹, M. Guida¹, G. Olivares², L.M. Gomez², R. Turco¹, R. Tesser¹, S. Mallardo¹, G. Santagata¹, P. Russo¹; ¹Università degli Studi di Napoli Federico II, Italy; ²Jerry Moran Center for Advanced Virtual Engineering & Testing (A, United States PRELIMINARY ASSESSMENT FOR STRUCTURAL BATTERY COMPONENTS |
8 - Manufacturing and Supply Chain Management |
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ICAS2024_0022: J. Shipley¹, A. Magnusson¹, J. Gårdstam¹, C. Beamer¹, A. Cassese¹; ¹Quintus Technologies, Sweden THE PRODUCTION OF HIGH-PERFORMANCE HEAT EXCHANGERS FOR AEROSPACE APPLICATIONS |
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ICAS2024_0100: F. Martone¹, G. Zazzaro¹, M. Inverno¹, S. De Luca, Atitech S.p.A., Italy; F. Mainieri, Major Bit Consulting s.r.l., Italy; G. Romano¹; ¹C.I.R.A. Italian Aerospace Research Centre, Italy A SUPPORTING FRAMEWORK FOR AIRCRAFT MRO OPERATIONS. CAPACITY PLANNING, TASKS TRACEABILITY AND DISEMBARKED ITEMS TRACKING |
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ICAS2024_0190: S. Merola ¹, M. Guida¹, F. Marulo¹; ¹University of Naples Federico II, Italy COMPUTER VISION ALGORITHMS FOR THE IDENTIFICATION OF DAMAGES ON FULL-SCALE AIRCRAFT COMPONENTS |
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ICAS2024_0248: M.C. Li, China; S. Yan, China; K.F. Zhang, China; W. Wang, China; L. Zou, China; Y. Huang, China THERMAL AND GRINDING PERFORMANCE OF 3D PRINTED COMPLIANCE GRINDING TOOLS WITH ROTARY-ENHANCED HEAT TRANSFER STRUCTURE |
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ICAS2024_0260: H. Li¹, L. Zou¹, W. Wang¹, L. Gui¹; ¹Chongqing University, China REDESIGN AND MACHINING OF LEADING EDGE OF TRANSONIC COMPRESSOR BLADE IN ROBOTIC GRINDING OPERATION |
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ICAS2024_0262: K. Li¹, P. Fu¹, Z. Tang¹, B. Zhang¹, Y. Ma, Chongqing University of Technology, China; ¹AVIC Manufacturing Technology Institute, China SURFACE MORPHOLOGY AND MICROSTRUCTURAL FEATURES OF ELECTRON BEAM SURFI-SCULPTED TI-6AL-4V ALLOY |
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ICAS2024_0306: M. Bartolomei¹, F. Barravecchia¹, L. Mastrogiacomo¹, F. Franceschini¹, F. Acerra², D.M. Gatta², D. Cannizzaro²; ¹Politecnico di Torino, Italy; ²Leonardo S.p.A, Italy PRELIMINARY RESULTS FOR AN INSTRUCTION DESIGN PROCEDURE IN AERONAUTICAL MANUFACTURING |
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ICAS2024_0313: T. Müller¹, V. Gollnick¹; ¹Institute of Air Transportation Systems, Germany BUILDING METHODS FOR A COMPOSITE CONSTRUCTED VTOL USING 3D PRINTING TECHNIQUES |
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ICAS2024_0378: W.-X. Wang¹, H.-L. He¹, T.-Y. Zhou, Cardiff University, United Kingdom; L. Wan¹; ¹Chongqing University, China PRESERVING HUMAN EXPERTISE: EXPLORING MIXED REALITY TRAJECTORY PLANNING FOR ROBOTIC BELT GRINDING |
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ICAS2024_0487: E. Delsol¹, I. Taouil¹, W. Azoti², B. Castanie², P. Olivier², L. Ratsifandrihana, Segula, France; ¹Segula - ICA, France; ²ICA, France A DIGITAL METHOD FOR THE COMPENSATED MOLD DESIGN OF COMPOSITE PARTS |
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ICAS2024_0589: G. Donelli¹, J.M.G.D. Mello², F.I.K. Odaguil², T. Van der Laan, GKN/Fokker, Netherlands; L. Boggero¹, B. Nagel¹; ¹German Aerospace Center DLR, Germany; ²Embraer, Brazil VALUE-DRIVEN TRADESPACE EXPLORATION FOR AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN |
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ICAS2024_0593: T. Wang¹, C. Wang¹, J.-J. Li¹, W.-X. Wang¹; ¹Chongqing University, China EFFECTS OF PROCESSING STRATEGIES ON SURFACE QUALITY AND MECHANICAL PROPERTIES IN HYBRID ADDITIVE MANUFACTURING OF IN718 ALLOY |
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ICAS2024_0672: J. Pesce¹, A. Carini¹, M. Marinacci¹, M. Boscia¹, P. Marzioli¹, M. Pasquali¹, M. Eugeni¹, M. Mecella¹, P. Piergentili¹, P. Gaudenzi¹; ¹Sapienza University of Rome, Italy CYBER-PHYSICAL SYSTEM IMPLEMENTATION FOR THE AR-ASSISTED AIT OF AEROSPACE COMPONENTS |
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ICAS2024_0799: A. Alaimo, Kore Università di Enna, Italy; S. Bagassi¹, E. Carrera, Politecnico di Torino, Italy; T. Fadda¹, M.C. Moruzzi¹; ¹Università di Bologna, Italy DESIGN AND DEVELOPMENT OF THE VISUAL AND AUDITORY LAYER FOR DIFFERENT CABIN/COCKPIT LAYOUT |
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ICAS2024_0804: G. Ascione¹, G. Donelli¹, L. Boggero¹, B. Nagel¹; ¹DLR, Germany UNCERTAINTY PROPAGATION IN VALUE-DRIVEN DECISION-MAKING FOR THE AIRCRAFT, MANUFACTURING AND SUPPLY CHAIN DESIGN |
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ICAS2024_0964: K.J. Lin, China; Y. Xu, China; D.D. Gu, China; J.H. Shan, China; K.Y. Shi, China; W.L. Zhang, China LIGHT WEIGHT DESIGN AND LASER ADDITIVE MANUFACTURING OF METAL BIPOLAR PLATES FOR THE APPLICATION OF AIRCRAFT FUEL CELL |
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ICAS2024_1127: I. Tan¹, G. Cohen¹, A.-C. Araujo¹, A. Daidié¹; ¹Institut Clément Ader, France FRICTION RIVETING OF THERMOPLASTIC COMPOSITE WITH A CNC MACHINE: EXPERIMENTAL WORK |
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ICAS2024_1152: Y. Ghanjaoui¹, J.H. Bussemaker¹, J. Biedermann¹, B. Nagel¹; ¹DLR, Germany AN ONTOLOGY-BASED APPROACH FOR THE CO-DEVELOPMENT AND OPTIMIZATION OF AIRCRAFT CABIN DESIGN AND ASSEMBLY ARCHITECTURES |
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ICAS2024_1194: P. Ottosson¹, E.-L. Westman¹, I. Nygren, Quintus Technologies, Sweden; T. Pettersson, Permanova LaserTool in Blekinge, Sweden; F. Niklasson², L.-E. Brattström²; ¹RISE Research Institutes of Sweden, Sweden; ²GKN Aerospace Engine Systems Sweden, Sweden DESIGN OF A SUSTAINABLE FLEXFORMING PROCEDURE FOR AERO ENGINE COMPONENTS IS ALLOY 718 |
9 - Air Transport System Efficiency |
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ICAS2024_0061: L. Nöhren¹, O. Gluchshenko¹, M.-M. Temme¹, K. Muth¹; ¹DLR, Germany ATM CONTROLLER SUPPORT IN CASE OF SPACIOUS SEVERE WEATHER CONSTELLATIONS ILLUSTRATED USING TWO AIRSPACE EXAMPLES |
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ICAS2024_0096: Z.L. Zengerling¹, M. Mendiguchia Meuser¹, A. Lau¹, V. Gollnick, Hamburg University of Technology (TUHH), Germany; ¹German Aerospace Center (DLR), Germany MITIGATING THE CLIMATE IMPACT OF AVIATION BY OPERATIONAL MEANS - A COMPARATIVE STUDY FOR DIFFERENT WEATHER SITUATIONS |
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ICAS2024_0126: N. Barry¹, C. Gallagher¹, S. Fitzgerald, Ryanair, Ireland; C. Stuart¹; ¹Trinity College Dublin, Ireland CHARACTERISING THE ROLE OF FLEET RENEWAL ON THE PATHWAY TO 2050: A EUROPEAN AIRLINE CASE STUDY |
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ICAS2024_0137: G. Enea¹, T. Reynolds¹, J. Venuti¹, T. Polishchuk², V. Polishchuk², A. Lemetti², A. Lau³, J. Solzer³, T. Bölle³; ¹MIT Lincoln Laboratory, United States; ²Linköping University, Sweden; ³German Aerospace Center (DLR), Germany COMPARING CONVECTIVE WEATHER IMPACTS ON AIR TRAFFIC MANAGEMENT OPERATIONS IN UNITED STATES, CANADA & EUROPE |
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ICAS2024_0142: N.K. Wickramasinghe¹, Y. Nakamura¹, A. Senoguchi¹; ¹Electronic Navigation Research Institute, Japan ESTIMATING THE IMPACT OF NUMERICAL WEATHER PREDICTION DATA MODELS ON SHORT-HAUL MINIMUM COST TRACKS |
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ICAS2024_0155: E. Wille, RWTH Aachen University, Germany COMPARING THE CAPACITY OF DIFFERENT VERTIPORT TOPOLOGIES USING DISCRETE EVENT SIMULATION |
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ICAS2024_0325: T. Iijima¹, N. Matayoshi¹, N. Yokoyama¹, H. Yoshida¹, A. Oosedo¹, S. Kikkawa¹, M. Yawata², S. Nakada², T. Yahata²; ¹JAXA, Japan; ²NEC, Japan DEVELOPMENT OF LOW ALTITUDE 4-DIMENSIONAL OPERATIONS MANAGEMENT SYSTEM FOR ADVANCED AIR-MOBILITY |
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ICAS2024_0326: M. Gomes Araujo¹, C. Conte², F. De Crescenzio¹, D. Accardo²; ¹University of Bologna, Italy; ²University of Naples Federico II, Italy CLASSIFICATION OF EXTENDED REALITY BASED HUMAN MACHINE INTERFACES SCENARIOS FOR URBAN AIR MOBILITY |
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ICAS2024_0347: G. Riccardi¹, L. Brucculeri¹, E. Fornaciari, d-flight, Italy; M. D'Onofrio, Techno Sky, Italy; A. Zilli², D. Leanza², G. Ferrara, Eurocontrol, France; M. Molinario³, G. Esposito³, A. Favier, Pipistrel, Italy; ¹ENAV S.P.A, Italy; ²DTA, Italy; ³NAIS, Italy CORUS-XUAM: TACKLING URBAN AIR MOBILITY AIRSPACE INTEGRATION CHALLENGES |
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ICAS2024_0377: F. Pollet¹, T. Planès¹, S. Delbecq¹; ¹Fédération ENAC ISAE-SUPAERO ONERA, Université de Toulouse, France A COMPREHENSIVE METHODOLOGY FOR PERFORMING PROSPECTIVE LIFE CYCLE ASSESSMENTS OF FUTURE AIR TRANSPORT SCENARIOS |
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ICAS2024_0380: Y. Nakamura¹, A. Senoguchi¹; ¹Electronic Navigation Research Institute, Japan RELATIONSHIPS BETWEEN AIRCRAFT ROUTES AND TURBULENCE-RELATED WEATHER DATA |
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ICAS2024_0406: K.A. Buchtal¹, A. Lau¹, D. Ebert², J. Richters², K. Schneiders²; ¹German Aerospace Center (DLR), Institute of Air Transport, Germany; ²German Weather Service (DWD), Radioactivity Monitoring, Germany ROUTE PLANNING FOR VOLCANIC ASH AND RADIOACTIVITY IN-SITU DRONE MEASUREMENTS USING A GENETIC ALGORITHM AND KRIGING |
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ICAS2024_0410: D. Kacik, Warsaw University of Technology, Poland OVERVIEW OF FACTORS RELATED TO AIRCRAFT OPERATION ASSOCIATED WITH A NEGATIVE IMPACT ON THE ENVIRONMENT |
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ICAS2024_0464: A. Edsel¹, S.D. Biswas¹, M. Kilbourne¹, R. Gadre¹, S. Vashi¹, K. Mall¹, W.A. Crossley¹, D.A. DeLaurentis¹, M.D. Patterson², B.E. Sells²; ¹Purdue University, United States; ²NASA Langley Research Center, United States EXPLORING RIDESHARING IN PASSENGER URBAN AIR MOBILITY: A COMPARATIVE ANALYSIS |
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ICAS2024_0685: T. Welsch¹, M.-M. Temme¹; ¹DLR, Germany SPEED GATED INTERCEPT PROCEDURE STUDY FOR INTEGRATION OF INCREASING DIVERSE OPERATIONS (IDO) AT EUROPEAN AIRPORTS |
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ICAS2024_0686: F. Vehlhaber¹, M. Salazar¹; ¹Eindhoven University of Technology, Netherlands AIRPORT INFRASTRUCTURE SIZING FOR A REGIONAL ELECTRIC AVIATION NETWORK |
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ICAS2024_0745: M. Swaid, German Aerospace Center (DLR), Germany; S. Papakonstantinou¹, D. Kloock-Schreiber¹, V. Gollnick¹; ¹Hamburg University of Technology (TUHH), Germany DESIGN OF A UAM GROUND INFRASTRUCTURE NETWORK WITH RESPECT TO MAINTENANCE CAPACITY REQUIREMENTS |
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ICAS2024_0763: N. Yoshikawa, Mitsubishi Electric Corporation, Japan PAIRWISE SWAPPING SEQUENCE OPTIMIZATION BY METROPOLIS-HASTING ALGORITHM WITH QUANTUM ANNEALING FOR AIR TRAFFIC CONTROL |
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ICAS2024_0782: M. Peng¹, A. Kamat¹, V. Tran, Harvard University, United States; C. Dawson², C. Fan², M.Z. Li¹; ¹University of Michigan, United States; ²Massachusetts Institute of Technology, United States PROBING AND MODELING LARGE-SCALE AIRLINE NETWORK DISRUPTIONS: 2022 SOUTHWEST AIRLINES SCHEDULING CRISIS |
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ICAS2024_0835: A. Andreeva-Mori¹, K. Ohga¹, K. Kobayashi¹; ¹Japan Aerospace Exploration Agency (JAXA), Japan LOW-ALTITUDE INTEGRATED AIRSPACE OPERATIONS OF AIRCRAFT FLYING UNDER VISUAL FLIGHT RULES: THE VERTICAL DIMENSION |
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ICAS2024_0845: M. Viscardi, University of Naples, Italy MODELING TECHNIQUE FOR THE EVALUTAION OF ENVIRONMENTAL EFFECT OF FLIGHT-PATH NEAR AIRPORTS: THE CASE STUDY OF A NEW ROUTE AT NAPLES AIRPORT |
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ICAS2024_0850: J.C. Lee¹, S.K. Kim, Georgia Institute of Technology, South Korea; S.M. Ahn¹, J.H. Kim, Sejong University, South Korea; ¹Handong Global University, South Korea WHAT-IF SCENARIO ANALYSIS OF REGIONAL AIR MOBILITY OPERATIONS IN SOUTH KOREA |
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ICAS2024_0946: M. Spieck, Thelsys, Germany; J.H. Binnebesel¹, J. Mehnen¹; ¹mb+Partner, Germany AUTOMATED OPERATION OF HIGH-PERFORMANCE FIXED-WING DRONES: A POTENTIAL GAME-CHANGER FOR GREEN AERIAL SERVICES |
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ICAS2024_0950: F. Borgna¹, V. Borio¹, R. Fusaro¹, N. Viola¹, G. Saccone, Italian Aerospace Research Centre (CIRA), Italy; ¹Politecnico di Torino, Italy INTEGRATING ECO-EFFICIENT FLIGHT PLANNING IN AIRCRAFT CONCEPTUAL DESIGN: MINIMAL NOX ROUTES FOR HIGH-SPEED AIRCRAFT USING HYDROGEN |
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ICAS2024_0953: G. Sato, Electronic Navigation Research Institute, Japan DEMAND CAPACITY BALANCING FOR URBAN AIR MOBILITY USING MULTIAGENT SIMULATION |
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ICAS2024_0963: D. Iwata, The University of Tokyo, Japan; E. Itoh, The University of Tokyo/Electronic Navigation Research Institute, Japan DEVELOPMENT OF A NEW OPERATIONAL FRAMEWORK TO ACCOMMODATE STOCHASTIC AIR TRAFFIC FLOW AT TOKYO INTERNATIONAL AIRPORT |
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ICAS2024_0966: K. Tominaga¹, N. Inoue¹, M. Schultz, University of the Bundeswehr Munich, Germany; Y. Zeng, Nanyang Technological University Singapore, Singapore; E. Itoh¹; ¹The University of Tokyo, Japan TIME-BASED CONTROL TO REDUCE TRAJECTORY COMPLEXITY IN THE FLOW-CENTRIC AIR TRAFFIC CONTROL PARADIGM |
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ICAS2024_0968: K. Sekine¹, P. Bouchaudon, EUROCONTROL Innovation Hub, France; T. Tatsukawa¹, K. Fujii¹, E. Itoh, The University of Tokyo, Japan; ¹Tokyo University of Science, Japan VALIDATING FLOW-BASED EN ROUTE AMAN COUPLING ESCAPE LIGHT WITH AIRTOP SOFTWARE |
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ICAS2024_0985: T. Finck, German Aerospace Center, Germany A ROADMAP FOR TRANSFORMING TRADITIONAL ATCO TEAMS INTO COLLABORATIVE HUMAN-MACHINE TEAMS |
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ICAS2024_1007: T. Oliveira¹, A. Carvalho¹; ¹The Boeing Company, Brazil STRUCTURED ANALYSIS ESTIMATION FOR ELECTRICAL ENERGY DEMAND ON AIRPORT OPERATIONS FOR HYBRID REGIONAL AND ELECTRIC TOWING PARAMETERIZED BY MOVEMENT METRICS CONSIDERING UPCOMING ELECTRIC INTENSIVE TECHNOLOGIES AND EMISSION REDUCTIONS IN THE UPCOMING DECADE |
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ICAS2024_1016: S. Bagassi¹, M. Corsi¹, T. Fadda¹; ¹University of Bologna, Italy EXTENDED REALITY IN AIRPORT CONTROL TOWERS: FROM CONCEPT DESIGN TO PRELIMINARY ASSESSMENT OF AN INNOVATIVE HUMAN-MACHINE INTERFACE FOR AIR TRAFFIC CONTROL OPERATORS |
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ICAS2024_1038: T. Marks¹, A. Hillebrecht¹, M.A. Bellido-Manganell¹; ¹German Aerospace Center, Germany APPLICATIONS AND CHALLENGES FOR AIRBORNE AD-HOC COMMUNICATION NETWORKS IN ORP AIRSPACES USING THE L-BAND |
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ICAS2024_1059: S. Bagassi¹, T. Fadda¹, M. Corsi¹; ¹University of Bologna, Italy ADVANCED HUMAN MACHINE INTERFACES FOR DRONE MONITORING: ASSESSMENT OF THE TECHNOLOGICAL FRAMEWORK FOR THE DESIGN OF AN AUGMENTED REALITY INTERFACE |
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ICAS2024_1133: A. Avi¹, G. Quaranta¹, A. Valentini, Fondazione Bruno Kessler, Italy; ¹Politecnico di Milano, Italy AI-ASSISTED DESIGN OF UAV DOCKING STATION NETWORK FOR DUAL USE PURPOSES |
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ICAS2024_1137: T. Reynolds¹, K.C. Woodrow¹, H. Iskenderian¹, D. Johnson¹, M. Matthews¹, J. Venuti¹, M. Worris¹, G. Enea¹, B. Crawley, NAV CANADA, Canada; ¹MIT Lincoln Laboratory, United States WEATHER-AWARE INTEGRATED AIRPORT/AIRSPACE CAPACITY PREDICTION TECHNOLOGIES |
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ICAS2024_1177: A. Harada, Kyushu University, Japan; N. Takeichi, Tokyo Metropolitan University, Japan; T. Masuki¹, H. Nakahata¹, S. Inohata¹, N. Nagata¹, A. Yasuda¹; ¹Japan Airlines Co., Ltd., Japan FEASIBILITY STUDY ON OPERATIONAL FLIGHT PLANS ADAPTED FOR TRAJECTORY BASED OPERATION |
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ICAS2024_1281: K. Ellis¹, M. Johnson¹, N. Neogi¹, J. Homola¹; ¹NASA, United States NASA RESEARCH TO EXPAND UAS OPERATIONS FOR DISASTER RESPONSE |
10 - Safety and Security |
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ICAS2024_0027: V. Gomes¹, T. Paiva¹, A. Herculano¹, T. Dias¹, M.M. Cardoso-Junior¹, M.C. Belderrain¹; ¹ITA, Brazil SLEEPINESS IN BRAZILIAN AVIATION: A PROBLEM-SOLVING APPROACH |
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ICAS2024_0049: R. Mori, Kobe University, Japan IDENTIFICATION OF FACTORS CONTRIBUTING TO UNFAVORABLE LANDINGS |
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ICAS2024_0074: T. Hu¹, J. Song¹, N. Yue¹, Z. Zhang², Y. Zhang², T. Chen²; ¹Airworthiness Technology Research & Management Center, China; ²Shanghai Aviation Airworthiness Certification Center, China STUDY ON THE BALLISTIC-RESISTANT AIRWORTHINESS STANDARDS FOR COMMERCIAL AIRCRAFT COCKPIT DOOR |
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ICAS2024_0089: D.M.C. de Lima¹, D.C. Fernandes¹, M.M. Cardoso Junior¹; ¹Aeronautical Institute of Technology, Brazil VALIDATING ASSUMPTIONS ABOUT PILOT RECOGNITION: A PCM-BASED APPROACH FOR AIRCRAFT CERTIFICATION SAFETY ASSESSMENT PROCESS |
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ICAS2024_0099: R.O. Kuchar¹, W. Scholz², B. Dörfler, Rödel Aerospace Systems, Germany; P. Herrmann², P. Jamakatel, University of the Bundeswehr Munich , Germany; J. Karger², J.J. Kiam³, J. Klennert*, M. Klennert*, M. Lindlar, German Aerospace Center (DLR-ME), Germany; M.S. May¹, D. Milz¹, N. Mummº, D. Nospes³, L. Peterº, G. Looye¹, A. Schulte³, P. Stütz³; ¹German Aerospace Center (DLR-SR), Germany; ²SFL GmbH., Germany; ³University of the Bundeswehr Munich, Germany; *STAR Healthcare Management GmbH., Germany; ºAmazilia Aerospace GmbH., Germany MOREALIS – A HOLISTIC APPROACH TO ENHANCE SAFETY FOR MICRO-AIRCRAFT OPERATIONS |
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ICAS2024_0106: J.G. Fowler¹, D.C. Fernandes¹, D.M.C. de Lima¹, G.V. da Rocha¹, M.M. Cardoso Júnior¹; ¹Aeronautic Institute of Technology, Brazil DECODING AN IN-FLIGHT REFUELING INCIDENT: AVIATION COMPLEXITY THROUGH STAMP/CAST AND ACCIMAP METHODS |
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ICAS2024_0127: T.F. Macedo¹, M.M. Cardoso Junior¹; ¹Technological Institute of Aeronautics, Brazil FROM THA TO REAL-TIME MONITORING: INTEGRATING NEW VIEW OF SAFETY INTO FLIGHT TEST PROGRAMS |
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ICAS2024_0131: J.C. Silva, Brazil; A. Barqueira, Portugal; L.B. Magalhães, Portugal; L.F.F.M. Santos, Portugal INSIGHTS INTO HUMAN FATIGUE: STATISTICAL ANALYSIS IN AIRCRAFT MAINTENANCE |
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ICAS2024_0132: I. de Souza Rehder¹, M.M. Cardoso Júnior¹, E. Villani¹; ¹Aeronautical Institute of Technology, Brazil A SYSTEMATIC REVIEW OF HUMAN FACTORS AND AI INFLUENCING OPERATOR PERFORMANCE IN MUM-T ENVIRONMENTS |
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ICAS2024_0183: C.-R. Huang¹, H.-L. Shi¹; ¹AVIC Aerospace Life-Support Industries, Ltd., China PILOT FATIGUE DETECTION USING BP NEUTRAL NETWORKS |
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ICAS2024_0202: A.C. Russo, Universidade de São Paulo, Brazil; A. Sarmento¹, I.S. Rehder¹, M.M. Cardoso-Junior¹, E. Villani¹; ¹Instituto Tecnológico de Aeronáutica, Brazil ASSESSING MENTAL WORKLOAD AND INTERFACE USABILITY IN MILITARY PILOTS: AN ADVANCED EYE-TRACKING METHODOLOGY |
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ICAS2024_0214: H. Inokuchi¹, H. Oikawa¹, G. Morimoto, Metro Weather Co., Ltd, Japan; S. Inaka¹; ¹JAXA, Japan REMOTE OBSERVATION EXPERIMENT OF VOLCANIC ASH USING POLARIZATION LIDAR |
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ICAS2024_0268: P. Jamakatel¹, J.J. Kiam ¹; ¹University of the Bundeswehr Munich, Germany GENERATION AND COMMUNICATION OF STRATEGIC PLANS AT DIFFERENT LEVELS OF ABSTRACTION FOR INTELLIGENT ASSISTANCE SYSTEMS IN GENERAL AVIATION |
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ICAS2024_0279: L. Yuan¹, B. Miao¹, K. Yan¹, C.L. Zhu¹; ¹Nanjing University of Aeronautics and Astronautics, China THE IMPACT OF PIEZOELECTRIC STACK HEATING ON AIRCRAFT DEICING |
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ICAS2024_0287: X. Xu¹, Y. Zhang¹, G. Chen¹, X. Ma, Xi'an Jiaotong UniversityXi'an Jiaotong University, China; ¹Xi'an Jiaotong University, China INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF WINGS UNDER ICING CONDITIONS AT VARIOUS SWEEP ANGLES |
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ICAS2024_0416: F. de Assis da Silva Junior¹, J.M. Vieira da Fonseca¹, I.N.M. da Silva¹, A.V. Gaspar¹, M.M. Cardoso Junior¹; ¹Technological Institute of Aeronautics, Brazil HELICOPTER ACCIDENTS IN BRAZIL: AN ANALYSIS OF MAINTENANCE FROM THE PERSPECTIVE OF HUMAN FACTORS |
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ICAS2024_0460: M. Lindlar¹, J. Klennert, STAR Healthcare Management GmbH, Germany; S. Plath¹; ¹German Aerospace Center, Germany PILOT SAFETY – SUPPORT BY BIOMEDICAL MONITORING IN PILOTS WITH HEALTH RISKS |
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ICAS2024_0517: M. May¹, D. Milz¹, W. Scholz², P. Herrmann², J. Karger², L. Peters³, N. Mumm³, R. Kuchar¹; ¹DLR, Germany; ²SFL GmbH, Germany; ³Amazilia Aerospace GmbH, Germany MIXED FLIGHT CONTROL LAYOUT FOR ULTRALIGHT GENERAL AVIATION AIRCRAFT |
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ICAS2024_0559: S. Morioka, Interstellar Technologies Inc., Japan; S. Obana, Hosei University, Japan; M. Yoshida, NICT, Japan A FAST INFORMATION THEORETICALLY SECURE RADIO COMMUNICATION PROTOCOL BASED ON GNSS POSITIONING |
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ICAS2024_0587: G. Li¹, Y.-D. Teng¹, Z.-L. Wang¹, T.-G. Xu¹, S.-T. Ding, Civil Aviation University of China,, China; ¹Beihang University, China A METHOD FOR AUTOMATIC GENERATING SAFETY ANALYSIS BASED ON AVIATION PISTON ENGINE MODEL |
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ICAS2024_0599: Z. Wang, China; G. Li, China; Y. Teng, China; T. Xu, China; Y. Zhang, China SENSITIVITY ANALYSIS OF SAFETY FACTORS BASED ON MODEL OF AVIATION RECIPROCATING ENGINE TURBOCHARGING SYSTEM |
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ICAS2024_0617: T. Marks, German Aerospace Center, Germany; K. Fuger, Hamburg University of Technology, Germany MUTUAL POSITION PLAUSIBILITY CHECKING IN FLYING AD-HOC NETWORKS USING DISTANCE MEASUREMENTS |
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ICAS2024_0700: D. Angelini¹, E. Cestino¹, D. Cestino², F. Cattel²; ¹Politecnico di Torino, Italy; ²A.O.U. Città della Salute e della Scienza di Torino, Italy COMPARATIVE ANALYSIS OF EVTOL, DRONE AND GROUND TRANSPORTATION SYSTEMS FOR EMERGENCY DELIVERY OF BLOOD-DERIVED MEDICATION |
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ICAS2024_0706: D. Nospes¹, P. Stütz¹; ¹University of the Bundeswehr Munich, Germany SENSOR AND COVERAGE PATH PLANNING FOR THE MONITORING OF AIRCRAFT EMERGENCY LANDING SITES |
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ICAS2024_0707: M. Blecken¹, H. Hintze¹, R. God¹; ¹Hamburg University of Technology, Germany ENABLING AIRWORTHINESS SECURITY BY A HOLISTIC SECURITY ENGINEERING PROCESS AT VARIOUS AIRCRAFT DESIGN LEVELS |
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ICAS2024_0719: H. Hofsäß¹, F. Holzapfel¹; ¹Technical University of Munich, Germany DYNAMIC RESPONSE MONITORING OF FLIGHT CONTROL WITH INCREMENTAL NONLINEAR DYNAMIC INVERSION |
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ICAS2024_0743: A. Esposito¹, G. Iacolino¹, C. Orlando¹, A. Alaimo¹; ¹Kore University of Enna, Italy METAMODELLING OF THE WORKLOAD ASSESSMENT IN SIMULATED FLIGHTS USING THE KRIGING METHOD |
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ICAS2024_0834: V.P. Schultz, NASA Langley Research Center, United States; H. Schlickenmaier, HS Advanced Concepts LLC, United States; L. Daelemans, European Union Aviation Safety Authority, Germany; C. Genster, Diamond Aircraft, Austria; M. Walz, Federal Aviation Administration,, United States; E. Holtz, Harbour Air, Canada; S. Ying, Ampaire, United States A CALL TO ACTION TO ENGAGE THE COMMUNITY TO MEET THE CHALLENGES THAT MUST BE TACKLED TO MAKE ELECTRIFIED AIRCRAFT PROPULSION REAL |
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ICAS2024_0848: M.D. Turazza¹, J.P.C.A Macedo ¹, J.H. Bidinotto¹; ¹EESC/USP, Brazil HANDLING QUALITIES RATING SCALE: THE IMPACT OF THE PILOT SUBJECTIVITY IN WORKLOAD EVALUATION |
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ICAS2024_0955: J. Yao, China; Y. Lu, China; Z. Zhong, China; S. Fu, China CLASSIFICATION OF COGNITIVE LOAD BASED ON THE PILOT’ VISUAL SCAN PATTERNS |
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ICAS2024_1186: T.-J. Jiang¹, Z.-P. Luo¹, Z. Kan¹, J.-W. Xiang¹, X.-C. Liu², C.-Y. Bai², X.-L. Xi²; ¹Beihang University, China; ²Aircraft Strength Research Institute, China IMPROVING DISTRIBUTION OF CRASH ENERGY ABSORPTION FOR CIVIL AIRCRAFT BASED ON PROGRESSIVE BENDING FAILURE MECHANISM |
11 - Operations and Sustainment |
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ICAS2024_0020: A.-K. Koschlik¹, M.J. Scott², T. Keser¹, F. Rauscher¹, H. Meyer¹, W. Verhagen², P. Marzocca², F. Raddatz¹, G. Wende¹; ¹DLR, Germany; ²RMIT, Australia MIXED REALITY FOR AIRCRAFT STRUCTURAL DENT AND BUCKLE NON-DESTRUCTIVE EVALUATION |
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ICAS2024_0065: D.Y. Sabag¹, O. Yakimenko, Naval Postgraduate School, United States; H. Alian¹; ¹Israeli Air Force, Israel DIGITAL TWIN OF AN AIRCRAFT LANDING GEAR TO ENHANCE FAILURE ANALYSIS AND MANAGE PREDICTIVE MAINTENANCE |
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ICAS2024_0083: M.J. Scott¹, O. Kirkpatrick¹, W. Verhagen¹, V. Kekoc, Defence Science and Technology Group, Australia; B. Teunisse, Capability Acquisition and Sustainment Group, Australia; J. Zhang¹, H. Fayek¹, P. Marzocca¹; ¹RMIT University, Australia APPLICATION OF NATURAL LANGUAGE PROCESSING FOR AIRCRAFT DEFECT TRACKING IN MAINTENANCE OPERATIONS |
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ICAS2024_0110: S. Kim¹, O. Park¹, H.-S. Shin¹; ¹Cranfield University, United Kingdom A DESIGN OF VFR APPROACH AND DEPARTURE PROCEDURES OF UAM AT VERTIPORTS ADJACENT TO THE AIRPORT |
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ICAS2024_0125: J. Aigner¹, A.-K. Koschlik¹, H. Meyer¹, F. Raddatz¹, G. Wende¹; ¹German Aerospace Center (DLR), Germany CINNABAR PROJECT – COST-BENEFIT ANALYSIS OF DIGITAL PROCESSES FOR NON-DESTRUCTIVE INSPECTIONS OF AIRCRAFT STRUCTURES |
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ICAS2024_0152: T. Keser¹, R. Schmied-Kowarzik¹, A.-K. Koschlik¹, L. Kaschub², M.J. Scott, RMIT University, Australia; R. Rodeck², G. Wende²; ¹German Aerospace Center (DRL), Germany; ²German Aerospace Center (DLR), Germany CINNABAR PROJECT - AUGMENTED REALITY WORKFLOW FOR AIRCRAFT DENT & BUCKLE INSPECTION |
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ICAS2024_0159: Y. Huang¹, G. Sun¹, J. Tao¹, J. Feng¹; ¹Fudan University, China A NOVEL DEEP MULTIMODAO INFORMATION FUSION MODEL FOR AERO-ENGINE STATE PREDICTION |
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ICAS2024_0164: R. Schmied-Kowarzik¹, T. Keser¹, L. Kaschub¹, A.-K. Koschlik¹, R. Rodeck¹, G. Wende¹; ¹German Aerospace Center (DLR), Germany CINNABAR PROJECT: EXAMINING REQUIREMENTS FOR USER ACCEPTANCE OF AIRCRAFT STRUCTURE INSPECTION IN AUGMENTED REALITY |
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ICAS2024_0165: M.C. Berschik¹, S. Wehrend¹, F.N. Laukotka¹, D. Krause¹; ¹Hamburg University of Technology, Germany DIGITALISATION AND SUSTAINABILITY IN CABIN DESIGN: SYNERGIES AND DEPENDENCIES |
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ICAS2024_0198: L. Baldo¹, A. De Martin¹, M. Terner, Leonardo S.p.A. Aircraft Division, Italy; M. Sorli¹; ¹DIMEAS, Politecnico di Torino, Italy THE JOURNEY TOWARDS CONDITION-BASED MAINTENANCE: A FRAMEWORK FOR THE HORIZONTAL TAIL ACTUATOR OF AN ADVANCED JET TRAINER AIRCRAFT |
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ICAS2024_0292: M. Osund-Ireland¹, B. Elzen¹, W.A. Ireland¹; ¹Susteer AB, Sweden CLIMATE RESILIENCE – THE IMPACT OF EXTREME WEATHER EVENTS - A CASE STUDY: HEATHROW AIRPORT |
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ICAS2024_0350: E. Stefana¹, E. De Paola¹, L. Pustina¹, R. Patriarca¹, F. Mastroddi¹; ¹Sapienza University of Rome, Italy ENSURING THE NEXT GENERATION GREEN AIRCRAFT’ SUSTAINABILITY FROM THE DESIGN PHASE VIA A LIFE-CYCLE COST ANALYSIS |
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ICAS2024_0367: P. Viry¹, T. Planès¹, S. Delbecq¹, L. Joly, ISAE-SUPAERO, Université de Toulouse, France; A. Salgas¹; ¹Fédération ENAC ISAE-SUPAERO ONERA, Université de Toulouse, France AN EMPIRICAL AND CUSTOMISABLE FLEET RENEWAL MODEL FOR PROSPECTIVE SCENARIOS USING OPEN-ACCESS DATA |
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ICAS2024_0379: D.S. Nithya¹, G. Quaranta¹, V. Muscarello², M. Liang²; ¹Politecnico di Milano, Italy; ²RMIT University, Australia ASSESSMENT OF A HIGHLY PARAMETERIZED STEADY-STATE MICROSCALE WIND SIMULATOR FOR URBAN AIR MOBILITY APPLICATIONS |
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ICAS2024_0452: A. Oestreicher¹, A. Rahn¹, J. Ramm¹, J. Städing², C. Keller², K. Wicke¹, G. Wende¹; ¹DLR, Germany; ²MTU Maintenance, Germany SUSTAINABLE ENGINE MAINTENANCE: EVALUATING THE ECOLOGICAL IMPACT OF LIFE LIMITED PART REPLACEMENT |
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ICAS2024_0455: S. Bianchi¹, F. Negroni¹, M. Riganti¹; ¹Leonardo Aircraft Division, Italy FASTVIBE SW TOOL FOR RIDE-ALONG VIBRATION SURVEY ANALYSIS |
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ICAS2024_0500: M. Fioriti¹, M. Borghi¹, G. Pavan¹; ¹Politecnico di Torino, Italy ENVIRONMENTAL AND ECONOMIC ASSESSMENT OF AN EVTOL AIRCRAFT FLEET FOR URBAN AIR MOBILITY |
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ICAS2024_0545: S. Wildermuth¹, W. Veraburenon¹, T. Bellier¹, C. Bil¹; ¹RMIT University, Australia LIFE CYCLE ASSESSMENT OF ALTERNATIVE LAUNCH METHODS |
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ICAS2024_0657: A. Giacotto¹, A.C. Pereira Mesquita¹, H. Costa Marques¹, A. Martinetti, University of Twente, Netherlands; ¹ITA, Brazil HOLISTIC AND SCALABLE SMART OPTIMIZATION FRAMEWORK FOR PRESCRIPTIVE MAINTENANCE |
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ICAS2024_0671: J. Roesing, RWTH Aachen University, Germany FACTORS INFLUENCING THE CLIMATE-RELEVANT ENVIRONMENTAL IMPACT OF AIR TRANSPORT COMPARED TO RAIL AND ROAD TRANSPORT |
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ICAS2024_0680: G. Quaresma¹, L.B. Magalhães, ISEC, ISEC Lisboa, Portugal; A.F. Ferreira, IDMEC-LAETA, Mechanical Engineering Department, IST/UL, Portugal; A. Silva¹; ¹AEROG-LAETA, Aerospace Sciences Department, UBI, Portugal E-KEROSENE POTENTIAL FOR COMMERCIAL AVIATION DECARBONIZATION |
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ICAS2024_0701: D.F. Migliore¹, G. D'Alessio², S. Caggese², A. De Martin², F. Acerra¹, M. Sorli², M. Fioriti²; ¹Leonardo S.p.A., Italy; ²Politecnico di Torino, Italy COMPARATIVE ANALYSIS OF MACHINE LEARNING ALGORITHMS FOR HEAT EXCHANGERS DIAGNOSIS IN ELECTRIFIED AIRCRAFT |
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ICAS2024_0705: S. Papakonstantinou¹, D. Kloock-Schreiber¹, M. Ziegler², A.N. Mishra, Hamburg University of Technology, Germany; P.K. Jaisawal¹, U. Wieczorek², V. Gollnick¹; ¹Hamburg University of Technology, ILT, Germany; ²Airbus Protect, Germany MRO FOR VTOLS IN A FUNCTIONAL SEQUENCES SOLUTION SPACE |
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ICAS2024_0793: A. Apostolidis¹, S. Le Dantec, SIGMA Clermont, France; K.P. Stamoulis¹; ¹Amsterdam University of Applied Sciences, Netherlands TOWARDS TRUSTWORTHY DATA-DRIVEN GAS TURBINE PROGNOSTICS |
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ICAS2024_0993: G. Sirtori¹, L. Trainelli¹, Z. Lahmam¹; ¹DAER, Politecnico di Milano, Italy HYDROGEN TANKERING: TOOLS FOR ECONOMIC AND ENVIRONMENTAL IMPACT SCENARIO STUDIES |
14 - Education and Training |
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ICAS2024_0314: J. Li¹, Y. He, Sichuan Technical Exchange Center, China; X.H. Tang, School of Public Administration, Sichuan University, China; Y.M. Zhou¹, W.F. Huo², J. Zhang², K. Lin², Y. Luo, Mao County Innovation Institute of Intelligent Aircraft Engineer, China; M. Ling, Chenghang Innovation Institute of Intelligent Aerocraft, Chengdu, China; ¹School of Aeronautic Science and Engineering, Beihang University, China; ²Chengdu Xueshang Technology Co., Ltd, China A TIERED CONTINUOUS CULTIVATING SYSTEM FOR AVIATION TECHNOLOGY TALENTS THAT INTEGRATES STEM AND POPULAR SCIENCE EDUCATION |
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ICAS2024_0324: M. Luo¹, H. Liu¹, X. Zhang¹, Z. Cui¹; ¹Beihang University, China TRANSFORMATIVE PEDAGOGY: CO-TEACHING COURSE CLUSTERS THROUGH COMPETITIVE TEAM DESIGNS FOR INNOVATIVE TALENT DEVELOPMENT IN AEROSPACE EDUCATION |
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ICAS2024_0505: F. Prokic¹, C. Eriksson¹, R.C. Munjuluru¹; ¹Linköping University, Sweden DESIGN AND VISUALIZATION OF A KNOWLEDGE-BASED AIRCRAFT CABIN IN VIRTUAL REALITY |
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ICAS2024_0508: E. Gaspari¹, E. Bianchini¹, L. Pezzullo¹, A. Giorgi¹, M. Giannetti¹, D.M. Macchini¹, L. Ferrarini¹, F. Bondanese¹, S. Celli¹, T. Strafforello¹, U. Mignemi¹, A. Arnaldi¹, M. Ferrazzani¹, M. Sanna¹, D. Geraci¹, M.R. Chiarelli¹, A.A. Quarta¹, G. Palaia¹, L. Boni¹; ¹University of Pisa, Department of Civil and Industrial Engineeri, Italy DESIGN BUILD AND FLY: A STUDENT APPROACH TO THE CREATION OF AN RC DRONE FOR UNIVERSITY COMPETITION |
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ICAS2024_0867: I. Jonsson¹, C. Xisto¹, V. Chernoray¹, A. Capitao Patrao¹; ¹Chalmers University Of Technology, Sweden LESSONS LEARNED FROM PROJECT BASED TEACHING IN AEROSPACE AT CHALMERS |
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ICAS2024_1098: G. Kontos¹, O. Lehmann¹; ¹Abu Dhabi University, United Arab Emirates DESIGNING A FRAMEWORK FOR FLIGHT SIMULATOR TRAINING SCENARIOS. AN EVIDENCE BASED TRAINING APPROACH. |
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ICAS2024_1185: O.D. Dantsker, Indiana University, United States INTEGRATING UNMANNED AERIAL SYSTEMS INTO THE INTELLIGENT SYSTEMS ENGINEERING CURRICULUM |
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ICAS2024_1263: M. Kanerva¹, Y. Zhang, Tsinghua University, China; R. Yondo Mine¹, L. Qiu, Beihang University, China; M. Wang, BIT, China; ¹Tampere University, Finland MICKEY MOUSE AND A GIANT: COMPARISON OF AERONAUTICS EDUCATION IN FINLAND AND CHINA |
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ICAS2024_1264: C. Ehrich¹, L. Kriebel¹, T. Schulz¹, M. Tekkel¹, L. Wauer¹, L. Wenz¹, L. Kugler², S. Müller², C. Niro²; ¹Technical University of Berlin, Germany; ²German Aerospace Center (DLR), Germany DLR DESIGN CHALLENGE 2024: DESIGN OF A COST AND ENERGY EFFICIENT REGIONAL AIRCRAFT |
15 - Guest lectures |
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ICAS2024_0057: S. Garg¹, A.M.P. Silva², P.F. Albuquerque², E. Nguyen Van, The French Aerospace Lab (Onera), France; K. Kimura³, Y. Sugioka³, M. Jacinto¹, P. Shiva Prakasha¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany; ²Centre of Engineering and Product Development (CEiiA), Portugal; ³Japan Aerospace Exploration Agency (JAXA), Japan IFAR-X: COLLABORATIVE ENGINEERING FRAMEWORK FOR NEXT GENERATION OF AEROSPACE ENGINEERS WORKING ON AIRCRAFT DESIGN |
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ICAS2024_0079: P.F. Albuquerque¹, A.M.P. Silva¹, A. Pereira¹; ¹CEiiA, Portugal AIRCRAFT WING STRUCTURAL SIZING COMPUTATIONAL TOOL TAILORED FOR A COLLABORATIVE MULTIDISCIPLINARY DESIGN FRAMEWORK |
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ICAS2024_0108: D.P. Wells¹, G.M. Gatlin¹, J.C. June¹, T.V. Marien¹; ¹NASA Langley Research Center, United States NASA TRANSONIC TRUSS-BRACED WING STUDIES |
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ICAS2024_0781: B. Chan, University of Pennsylvania, United States; Y. Deng¹, N. Tran¹, H. Wu¹, M. Ikeda, RTX Research Center, United States; G. Cinar¹, M.Z. Li¹; ¹University of Michigan, United States OPTIMIZING FLEET ASSIGNMENT DECISIONS FOR REGIONAL AIRLINES WITH HYBRID ELECTRIC AIRCRAFT UPTAKE |
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ICAS2024_0836: M. Kazari, Kawasaki Heavy Industries,Ltd., Japan DEVELOPMENT OF CORE TECHNOLOGIES FOR HYDROGEN AIRCRAFT |
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ICAS2024_0855: M. Méheut¹, D. Losada Costoso¹, F. Moens¹, O. Atinault¹, C. Julien¹, L. Vertonghen¹, L. Coelho¹, V. Priasso¹, A. Lannoo¹, S. Defoort¹, E. NGuyen Van¹, C. David¹, D. Glenis¹, J. Sodja², S. de Boer², J. Schwingel³, D. Eisenhut³; ¹ONERA, France; ² Delft University of Technology, Netherlands; ³University of Stuttgart, Germany STRUT-BRACED DRY WING CONCEPT FOR HYDROGEN-POWERED AIRCRAFT |
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ICAS2024_0856: Y. Yamaguchi, Mitsubishi Heavy Industries, Ltd./Commercial Aviation Systems, Japan AIRCRAFT DX IN COMMERCIAL AVIATION SYSTEMS |
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ICAS2024_0884: D.D.V. Pham¹, C. Recine¹, R.H. Jansen, NASA Glenn Research Center, United States; ¹NASA Ames Research Center, United States SIZING AND PERFORMANCE ANALYSIS OF A MW-CLASS ELECTRIFIED AIRCRAFT PROPULSION (EAP) SYSTEM FOR A PARALLEL HYBRID TURBOPROP CONCEPT |
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ICAS2024_0971: N. Seki¹, T. Inoue¹; ¹IHI Corporation, Japan DEVELOPMENT OF AIRCRAFT SYSTEM ELECTRIFICATION AND HYBRID ELECTRIC PROPULSION |
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ICAS2024_1172: J. Gladin¹, E. Aydin¹, J. Kenny¹, A. Burell¹, J. Decroix¹, T. Zaidi¹, R. Gautier¹, D. Mavris¹; ¹ASDL, United States REASSESSMENT OF PARAMETRIC OPTIMIZATION AND PERFORMANCE ANALYSIS METHODOLOGY FOR MILD HYBRID AIRCRAFT PROPULSION SYSTEMS |
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ICAS2024_1188: K.D. James¹, A. Meade¹; ¹NASA Ames Research Center, United States VEHICLE ASSESSMENT AND SYSTEM-WIDE BENEFIT ANALYSES OF HYBRID-ELECTRIC COMMERCIAL AIRCRAFT – ELECTRIFIED POWERTRAIN FLIGHT DEMONSTRATION PROJECT (EPFD) |
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ICAS2024_1210: J.P. Slotnick, Boeing, United States A CFD VALIDATION ECOSYSTEM TO ADVANCE THE PREDICTION OF LOW-SPEED AERODYNAMICS |
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ICAS2024_1212: A.M. Clark¹, D.S. Lacy¹; ¹Boeing Commercial Airplanes, United States CHALLENGES IN GEOMETRY DEVELOPMENT FOR THE CRM-HL ECOSYSTEM |
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ICAS2024_1213: M. Rivers, United States NASA CONTRIBUTIONS TO THE HIGH LIFT COMMON RESEARCH MODEL ECOSYSTEM |
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ICAS2024_1214: R. Rudnik¹, S. Pülm¹, F. Schmidt¹, J. Wild¹, A. Schröder¹, C. Spehr¹, P. Mühlmann¹; ¹DLR, Germany THE CRM-HL ECOSYSTEM - DLR CONTRIBUTIONS |
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ICAS2024_1215: T. Hashioka¹, Y. Murahashi¹, H. Yasuda¹, Y. Sawaki¹, S. Onda¹, Y. Tsuchimoto¹, Y. Nishizaki¹, W. Suzuki¹, T. Kawamura¹; ¹Kawasaki Heavy Industries, Ltd., Japan TEST SUMMARY OF THE FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL |
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ICAS2024_1216: K. Hood, United States BOEING CONTRIBUTIONS TO THE CRM-HL ECOSYSTEM |
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ICAS2024_1217: C.L. Rumsey, NASA Langley Research Center, United States HIGH-LIFT PREDICTION WORKSHOPS: RETROSPECTIVE, LESSONS LEARNED, AND FUTURE PROSPECTS |
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ICAS2024_1218: C. Grabe, DLR, Germany CFD VALIDATION EXPERIMENTS AT DLR: OVERVIEW AND LESSONS-LEARNED |
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ICAS2024_1219: C.J. Roy¹, K.T. Lowe¹, W.J. Devenport¹, A. Borgoltz¹, A. Gargiulo, University of Virginia, United States; ¹Virginia Tech, United States THE BEVERLI HILL EXPERIMENTS FOR SMOOTH-BODY TURBULENT FLOW SEPARATION - RETROSPECTIVE, LESSONS LEARNED, AND FUTURE PROSPECTS |
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ICAS2024_1220: M. Galbraith, United States SYSTEMATIC CFD VERIFICATION - RESULTS FROM THE 2024 HIGH FIDELITY CFD VERIFICATION WORKSHOP |
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ICAS2024_1221: S. Watanabe, Japn Aerospace Exploration Agency, Japan OVERVIEW OF JAPANESE R&D ACTIVITIES ON GREEN TRANSFORMATION AND DIGITAL TRANSFORMATION IN AVIATION |
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ICAS2024_1223: O. Bertram¹, B. Schuchardt¹, A. König¹, K. Wendt¹, P. Shiva Prakasha¹; ¹DLR, Germany ADVANCING URBAN AIR MOBILITY: COLLABORATIVE EXCELLENCE AND INFRASTRUCTURE INITIATIVES BY DLR |
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ICAS2024_1225: T.F. Wunderlich, German Aerospace Center (DLR), Germany OPTIMAL WING ASPECT RATIO OF HIGHLY EFFICIENT LONG-RANGE AIRCRAFT |
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ICAS2024_1226: G. Symeonidis, European Research Council Executive Agency (ERCEA), Belgium EUROPEAN RESEARCH COUNCIL (ERC) - FUNDING OPPORTUNITIES AND REPRESENTATIVE PROJECT HIGHLIGHTS |
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ICAS2024_1227: T. Beezhold, Boeing, United States THE CHALLENGE OF SUSTAINABILITY IN COMMERCIAL AVIATION |
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ICAS2024_1229: A. Orton, Federal Aviation Administration, United States; R. Guerrero, United States Air Force, United States; R. Wahls, National Aeronautics and Space Administration, United States UNITED STATES' AIRCRAFT SUSTAINABILITY RESEARCH & DEVELOPMENT EFFORTS |
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ICAS2024_1230: C. Bisagni, Politecnico di Milano, Italy NABUCCO TAKE-OFF: MULTI-STABLE PANELS FOR AN ADAPTIVE WING |
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ICAS2024_1231: J. Crouch, Boeing, United States APPLICATION OF LAMINAR FLOW CONTROL FOR ENHANCED PERFORMANCE AND REDUCED EMISSIONS |
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ICAS2024_1232: A. Morgans, United Kingdom THERMOACOUSTIC INSTABILITY IN AERO-ENGINE COMBUSTORS |
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ICAS2024_1233: G. Bezos O Connor, NASA (LaRC), United States BARRIERS TO MW CLASS ELECTRIFIED POWERTRAIN AIRCRAFT PROPULSION SYSTEMS |
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ICAS2024_1234: M. Kotsonis, Delft University of Technology, Netherlands METAMATERIALS FOR CONTROL OF FLUID FLOWS |
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ICAS2024_1235: R. Seele, GE Aerospace, United States GE AEROSPACE: RISING TO THE CHALLENGE FOR MORE SUSTAINABLE FLIGHT |
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ICAS2024_1237: R. Young, NASA (LaRC), United States NASA HI-RATE COMPOSITE AIRCRAFT MANUFACTURING (HICAM) PROJECT OVERVIEW |
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ICAS2024_1238: M. Kohzai, Japan ACTIVITY PLANS USING CRM-HL AT JAXA |
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ICAS2024_1239: T.M. Schneider, EPFL, Switzerland TOWARDS A FIRST-PRINCIPLE BASED QUANTITATIVE DESCRIPTION OF TURBULENCE WITHOUT THE NEED FOR ADHOC MODELS |
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ICAS2024_1240: B. Cobleigh, NASA (AFRC), United States; E. Kaduce, Boeing, United States X-66: ACCELERATED LEARNING THROUGH FULL SCALE PROTOTYPING |
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ICAS2024_1241: F. Weiss, DLR, Germany DRIVETRAIN INFLUENCE ON THE LEAD-LAG MOTION OF HELICOPTER ROTORS |
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ICAS2024_1242: J. Ludvik, Honeywell, United States FUEL CELL BASED POWERTRAINS |
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ICAS2024_1244: D. Cuchet, ATR, France ATR COMMERCIAL AVIATION SUSTAINABILITY STRATEGY |
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ICAS2024_1245: A.L. Nerone¹, J.M. Haglage¹, L.M. Nakley¹, R. Tornabene¹; ¹NASA (GRC), United States NASA HYBRID THERMALLY EFFICIENT CORE (HYTEC) PROJECT OVERVIEW |
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ICAS2024_1246: J.U. Müller, Lufthansa, Germany RIBLETS IN AVIATION- FIRST EVER INDUSTRIALIZATION WITH AEROSHARK |
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ICAS2024_1247: W.J. Coupe¹, S. Saxena¹; ¹NASA Ames Research Center, United States TOWARDS SUSTAINABLE AVIATION WITH EFFICIENT AIRSPACE OPERATIONS |
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ICAS2024_1248: M.L. Post, DARPA/TTO, United States AFC FLIGHT-DEMONSTRATOR X-65 PROGRAM OVERVIEW |
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ICAS2024_1251: P. Coen, United States BREAKING THE SOUND BARRIER: ACHIEVING QUIET SUPERSONIC FLIGHT OVER LAND |
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ICAS2024_1252: R. Moore, NASA (LaRC), United States; C. Voigt, DLR, Germany RECENT FLIGHT EXPERIMENTS SHOW THE CLIMATE BENEFITS OF SUSTAINABLE AVIATION FUELS (SAF) AND ADVANCED ENGINE TECHNOLOGIES |
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ICAS2024_1253: A. Krein, Clean Aviation, Germany SUSTAINABLE AVIATION TECHNOLOGY PROGRAMMES IN EUROPE |
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ICAS2024_1254: G. Llewellyn, Airbus, United Kingdom TOWARDS ZERO CLIMATE IMPACT AVIATION |
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ICAS2024_1255: G. Warwick¹, G. Norris¹; ¹Aviation Week, United States A VIEW LOOKING IN - AVIATION WEEK'S ASSESSMENT OF SUSTAINABLE AVIATION R&D IN CHINA AND THE ASIA-PACIFIC REGION |
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ICAS2024_1256: A. Boschen, SESAR Joint Undertaking, Germany HOW CAN EUROPE BECOME THE MOST EFFICIENT AND ENVIRONMENTALLY-FRIENDLY SKY TO FLY IN THE WORLD? |
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ICAS2024_1257: F. Donus, MTU, Germany MTU’S ROADMAP TOWARDS SUSTAINABLE PROPULSION |
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ICAS2024_1258: C. Jouannet, Saab Aeronautics, Sweden NAVIGATING COMPLEXITY: ADAPTING AEROSPACE DEVELOPMENT IN A DYNAMIC WORLD |
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ICAS2024_1259: A. Andreeva-Mori, Japan Aerospace Exploration Agency (JAXA), Japan; D. Sziroczák, Budapest University of Technology and Economics (BME), Hungary; G. Schwoch, German Aerospace Center (DLR), Germany; M.C.R. Murça, Aeronautics Institute of Technology (ITA), Brazil; B. Dziugiel, Lukasiewicz Research Network – Institute of Aviation (ILOT), Poland; J. Homola, National Aeronautics and Space Administration (NASA), United States; V. Kramar, VTT Technical Research Centre of Finland, Finland ENHANCING PUBLIC GOOD MISSIONS AND DISASTER RESPONSE WITH ADVANCED AERIAL TECHNOLOGY: OPPORTUNITIES AND CHALLENGES |
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ICAS2024_1261: S. McCullough, Bombardier, Canada BOMBARDIER ECOJET RESEARCH PROJECT; THE QUEST FOR SUSTAINABLE AVIATION |
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ICAS2024_1262: R. Woszidlo, The Boeing Company, United States THE PATH TO TRANSITION ACTIVE FLOW CONTROL TECHNOLOGY |
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ICAS2024_1265: T. Yamane, Japan Aerospace Exploration Agency, Japan JAXA EN-CORE PROJECT OVERVIEW AND ACHIEVEMENTS |
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ICAS2024_1266: R. Foley, RTX/Collins, United States CLEAN AVIATION HIGH VOLTAGE NETWORK AND DEMONSTRATION |
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ICAS2024_1267: F. Vitiello¹, F. Causa¹, R. Opromolla¹, G. Fasano¹; ¹University of Naples Federico II, Italy RESEARCH RESULTS AND PERSPECTIVES ON NON-COOPERATIVE SENSING FOR SAFE UAM OPERATIONS |
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ICAS2024_1268: E. Theunissen, Netherlands Defence Academy, Netherlands SENSOR UNCERTAINTY MITIGATION FOR DETECT AND AVOID SYSTEMS |
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ICAS2024_1278: L.R. Humphrey¹, C.A. Muñoz¹; ¹NASA, United States PRELIMINARY APPLICATION OF FORMAL VERIFICATION TO AN AUTONOMY ARCHITECTURE FOR UNMANNED AIRCRAFT |
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ICAS2024_1279: C. Most, Lufthansa, Germany AI DRIVEN DECISION SUPPORT IN OPERATIONS STEERING |
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ICAS2024_1280: G. Leblanc¹, G. Ifimov¹, M. Kalacska², O. Lucanus², J.P. Arroyo-Mora¹, J. Gorman¹, M. Wheatley, Ontario Ministry of Natural Resources and Forestry, Canada; C. McFayden, Natural Resources Canada, Canada; ¹National Research Council of Canada (NRC), Canada; ²Applied Remote Sensing Laboratory, McGill University, Canada ON-GOING WILDLAND FIRE WORK AT THE NATIONAL RESEARCH COUNCIL OF CANADA WITH A FOCUS ON THE USE OF COTS RPAS FOR REDUCTION OF NON-FIRE PILOT WORKLOAD |
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ICAS2024_1283: M. Cantrell, Airbus, United Kingdom WING OF TOMORROW - LONGER, LEANER, LIGHTER |
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ICAS2024_1286: D. Sanghi¹, C.E.S. Cesnik¹, C. Riso¹; ¹University of Michigan, United States EXPLORING ROLL MANEUVERABILITY OF FUTURE AIRCRAFT WITH HIGH AR WINGS |
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ICAS2024_1287: H. Maliska, NASA, United States THE NASA X-57 “MAXWELL” DISTRIBUTED ELECTRIC PROPULSION FLIGHT DEMONSTRATOR PROJECT |
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ICAS2024_1288: S. Clarke¹, J. Terry¹, K. Harris¹, D. Avanesian¹; ¹NASA, United States X-57 TRACTION POWER AND COMMAND SYSTEMS DEVELOPMENT |
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ICAS2024_1289: N. Borer, NASA, United States FLIGHT PERFORMANCE ESTIMATES FOR THE NASA X-57 DISTRIBUTED ELECTRIC PROPULSION FLIGHT DEMONSTRATOR |
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ICAS2024_1290: N.K. Borer¹, R.D. Wallace², J.R. Reynolds², D.E. Cox¹, C. Sales², T.L. Williams², W.M. Ringelberg²; ¹NASA Langley Research Center, United States; ²NASA Armstrong Flight Research Center, United States DISTRIBUTED THRUST TAKEOFF FOR THE NASA X-57 MOD IV FLIGHT DEMONSTRATOR |
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ICAS2024_1297: D. Reckzeh, Airbus, Germany PERSPECTIVES ON FLOW CONTROL APPLICATIONS FOR LARGE TRANSPORT AIRCRAFT |
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ICAS2024_1298: P. Schmollgruber, ONERA, France HIGH ASPECT RATION WING CONCEPTS |
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ICAS2024_1299: A. Sultan, NASA (ARMD), United States NASA SUSTAINABLE FLIGHT NATIONAL PARTNERSHIP OPERATIONS RESEARCH |
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ICAS2024_1300: M.J. Logan, NASA, United States APPLICATION OF UAS TECHNOLOGIES TO CREATE RESILIENT RURAL COMMUNITIES |
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ICAS2024_1301: CS. Silva, Embraer, Brazil EMBRAER SUSTAINABILITY STRATEGY |
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ICAS2024_1302: P.C. Crothers, Boeing Aerostructures Australia, Australia SUSTAINABLE HIGH RATE COMPOSITE MANUFACTURE |
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ICAS2024_1305: S.S. Savian, JetZero, United States JETZERO: RESHAPING AVIATION WITH THE BLENDED WING |
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ICAS2024_1306: T. Newby, Rolls-Royce plc, United Kingdom DELIVERING THE ROLLS-ROYCE NET ZERO ROADMAP |
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ICAS2024_1307: A.J. Murphy, Pratt & Whitney, United States PRATT & WHITNEY SUSTAINABILITY STRATEGY & DEMONSTRATORS |
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ICAS2024_1308: D. Dijoud, France SAFRAN PROPULSION STRATEGY AND ROADMAP FOR FUTURE SUSTAINABLE AVIATION |
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ICAS2024_1310: I. Bloy, AIRBUS, France AIRBUS COMMERCIAL AVIATION SUSTAINABILITY STRATEGY |
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ICAS2024_1312: J.F. Langford, Aurora Flight Sciences, A Boeing Company, United States INTEGRATING ACTIVE FLOW CONTROL ON AIRCRAFT |
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ICAS2024_1314: G. Teofili, ZeroAvia, United Kingdom ACCELERATING THE CLEAN FUTURE OF FLIGHT |
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ICAS2024_1315: M.R. Berube, Department of Energy EERE, United States FUTURE LANDSCAPE OF AVIATION ENERGY – US PERSPECTIVE |
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ICAS2024_1318: Y.C. Roth, Airbus, Germany FUSELAGE, CABIN & CARGO AND EMPENNAGE OF TOMORROW @ AIRBUS COMMERCIAL - NEW FUSELAGE DESIGN & MATERIALS |
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ICAS2024_1319: J. Tai, Georgia Tech, United States PERFORMANCE COMPARISON OF THE BLENDED WING BODY AND TUBE AND WING CONFIGURATIONS EXTRA |
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ICAS2024_1322: P.H. Kopardekar, United States NASA’S ADVANCED AIR MOBILITY RESEARCH |
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ICAS2024_1324: K. Mokaddem, AIRBUS, France CLEAN AVIATION SHORT MEDIUM RANGE AIRCRAFT CONCEPT |
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ICAS2024_1325: B. Nagel, Germany PIONEERING THE EXCHANGE OF KNOWLEDGE |
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ICAS2024_1326: A.S.J. van Herden, United Kingdom DIGITAL COLLABORATION FOR SUSTAINABLE AVIATION |
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ICAS2024_1327: K.K. Koschlik, Germany HARNESSING THE POWER OF METAVERSE TO REVOLUTIONIZE AIRCRAFT AND MRO RESEARCH |
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ICAS2024_1328: C. Jouannet, Sweden MANAGING DIGITAL COMPLEXITY |