ICAS 2022: TOPICS AND TITLES |
1.1 - Aircraft Design and Integrated System (Basics and Theory) |
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ICAS2022_0055: I. Berlowitz, IBAero Engineering, Israel TRANSPORT AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM AIR QUALITY IMPROVEMENT |
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ICAS2022_0084: T. Planès¹, S. Delbecq¹, V. Pommier-Budinger¹, V. Palanque¹, E. Bénard¹; ¹ISAE-SUPAERO, France SIZING AND OPTIMIZATION OF A MORE ELECTRIC AIRCRAFT INTEGRATING SHORT-TERM INCREMENTAL TECHNOLOGIES |
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ICAS2022_0102: V. Gollnick¹, B. Muth, TU Braunschweig, Germany; T. Weber¹, K. Scheibe, HAW Hamburg, Germany; M. Grünewald, FH Aachen, Germany; E. Aydin¹; ¹TU Hamburg, Germany CONCEPTUAL DESIGN OF FUTURE MILITARY AIR SYSTEMS - AN EDUCATIONAL APPROACH |
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ICAS2022_0117: S. Delbecq¹, T. Planès¹, M. Delavenne¹, V. Pommier-Budinger¹, A. Joksimovic¹; ¹ISAE-SUPAERO, France AIRCRAFT FLEET MODELS USING A BOTTOM-UP APPROACH FOR SIMULATING AVIATION TECHNOLOGICAL PROSPECTIVE SCENARIOS |
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ICAS2022_0129: D. Reckzeh, Airbus, Germany TECHNOLOGY INTEGRATION FOR FUTURE AIRCRAFT CONFIGURATIONS |
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ICAS2022_0139: N. Ma¹, F.-M. Meng¹, J.-H. Meng¹, L. Liu¹; ¹Beijing Institute of Technology, China STRUCTURAL DESIGN AND FLUTTER ANALYSIS OF SWEPT BAFFLED INFLATABLE WING |
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ICAS2022_0143: Z. Cui¹, M. Luo¹, H. Liu¹, X. Sun¹, Z. Ji¹, Y. Hua, China Academy of Launch Vehicle Technology, China; ¹Beihang University, China DIGITAL COLLABORATIVE DESIGN: AN INNOVATIVE FRAMEWORK IN AERONAUTICAL EDUCATION |
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ICAS2022_0149: T. Effing¹, V. Schmitz¹, F. Schültke¹, F. Peter, Bauhaus Luftfahrt e.V, Germany; E. Stumpf¹; ¹RWTH Aachen University, Germany COMBINED APPLICATION OF HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER IN PRELIMINARY AIRCRAFT DESIGN |
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ICAS2022_0155: T. Streit¹, M. Kruse¹, T. Kilian¹, J. v. Geyr, DLRK, Germany; I. Petropoulos, ONERA, France; ¹DLR, Germany AERODYNAMIC DESIGN AND ANALYSIS OF HLFC WINGS WITHIN THE EUROPEAN PROJECT HLFC-WIN |
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ICAS2022_0186: N. Wu¹, C.A. Mader¹, J.R.R.A. Martins¹; ¹University of Michigan, United States LARGE-SCALE MULTIFIDELITY AEROSTRUCTURAL OPTIMIZATION OF A TRANSPORT AIRCRAFT |
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ICAS2022_0187: M.A. Hariansyah¹, K. Shimoyama¹; ¹Institute of Fluid Science, Tohoku University, Japan DEEP LEARNING TECHNIQUES FOR HIGH-DIMENSIONAL SURROGATE-BASED AERODYNAMIC DESIGN |
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ICAS2022_0192: E. Shima, Japan Aerospace Exploration Agency, Japan; K. Yonezawa, Central Research Institute of Electric Power Industry, Japan; R. Nishida¹, S. Honda¹, M. Sato¹; ¹Kogakuin University, Japan AERODYNAMIC CHARACTERISTICS OF BOX WINGS FOR AN INNOVATIVE EVTOL CONFIGURATION |
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ICAS2022_0199: Y. Zhang¹, F. Qu¹, J.Q. Bai¹, D.S. Jia², E.K. Bontoft², V.V. Toropov²; ¹Northwestern Polytechnical University, China; ²Queen Mary University of London, United Kingdom AN EFFICIENT SOLUTION FOR AERODYNAMIC SHAPE OPTIMIZATION WITHIN THE MID-RANGE APPROXIMATION FRAMEWORK |
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ICAS2022_0214: F. Lutz¹, J. Jézégou¹, A. Reysset, INSA Toulouse, France; A. Busteros-Ramos¹, V. Pommier-Budinger¹; ¹ISAE-SUPAERO, France FAST-OAD-GA: AN OPEN-SOURCE EXTENSION FOR OVERALL AIRCRAFT DESIGN OF GENERAL AVIATION AIRCRAFT |
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ICAS2022_0227: R.C. Llamas-Sandin¹, C.D. Handal-Rivera¹; ¹Airbus OSL, Spain DESIGN OF AN ADVANCED EMPENNAGE AND REAR FUSELAGE CONCEPT FOR A COMMERCIAL AIRCRAFT |
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ICAS2022_0246: T.E. Boogaart¹, M.F.M. Hoogreef¹, A. Gangoli Rao¹; ¹Delft University of Technology, Netherlands INSTALLATION PENALTY OF AERO-ENGINES ON NARROW BODY AIRCRAFT |
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ICAS2022_0304: S. Wöhler¹, J.-N. Walther¹, W. Grimme¹; ¹German Aerospace Center (DLR), Germany DESIGN AND ECO-EFFICIENCY ASSESSMENT OF A PEOPLE-MOVER AIRCRAFT IN COMPARISON TO STATE-OF-THE-ART NARROW BODY AIRCRAFT |
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ICAS2022_0323: M. Mandorino¹, P. Della Vecchia¹, F. Nicolosi¹, S. Corcione¹, V. Trifari¹, G. Cerino, Leonardo Aircraft Division, Italy; M. Fioriti², C. Cabailero², T. Lefebvre, ONERA/DTIS, Université de Toulouse, France; ¹University of Naples Federico II, Italy; ²Politecnico di Torino, Italy REGIONAL JET RETROFITTING DESIGN: FROM STAKEHOLDERS’ NEEDS AND SYSTEM’S REQUIREMENTS TO MDAO WORKFLOW FORMULATION |
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ICAS2022_0334: D. Haldar¹, E. Holmgren¹, A. Johansson¹; ¹KTH Royal Institute of Technology, Sweden IMPLEMENTATION OF WING ICE PROTECTION SYSTEM IN MORE ELECTRIC AIRCRAFT TECHNOLOGIES |
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ICAS2022_0338: S. Tarroc Gil¹, J. Schminder¹, A. Guerrero i Almirall, UptimAI, Czech Republic; J.I. Tarraga Prieto, MAHLE Electronics S.L.U, Slovenia; R. Vaz Linn, Federal University of Rio Grande do Sul, Brazil; ¹Linköping University, Sweden ZONAL MODEL BASED AIRCRAFT PASSENGER THERMAL COMFORT COMPARATIVE STUDY |
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ICAS2022_0350: M. Fioriti, Politecnico di Torino, Italy; C. Cabaleiro, DLR, Germany; T. Lefebvre, ONERA, France; P. Della Vecchia¹, M. Mandorino¹, S. Liscouët-Hanke², A. Jeyarai²; ¹Università di Napoli Federico II, Italy; ²Concordia University, Canada CERTIFICATION DRIVEN DESIGN FROM STAKEHOLDERS’ NEEDS TO MDAO FORMULATION WITHIN AGILE 4.0 PROJECT |
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ICAS2022_0355: F. Valpiani¹, P. Cicolini¹, D. Esposto¹, A. Galletti¹, D. Guagliardo¹; ¹Politecnico di Torino, Italy NUMERICAL MODELING OF FLUID-STRUCTURE INTERACTION OF A 3D WEDGE DURING WATER IMPACT WITH VARIATION OF VELOCITY AND PITCH ANGLE |
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ICAS2022_0359: P. De Felipe¹, D. Yang¹; ¹Imperial College London, United Kingdom ECONOMICS OF SUSTAINABLE REGIONAL AIR MOBILITY |
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ICAS2022_0365: A.K. Jeyaraj¹, J.H. Bussemaker², S. Liscouët-Hanke¹, L. Boggero²; ¹Concordia University, Canada; ²DLR, Germany SYSTEMS ARCHITECTING: A PRACTICAL EXAMPLE OF DESIGN SPACE MODELING AND SAFETY-BASED FILTERING WITHIN THE AGILE 4.0 PROJECT |
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ICAS2022_0369: E. Holmgren¹, D. Haldar¹, L. Bertling Tjernberg, School of Electrical Engineering and Computer Science, KTH Royal, Sweden; A. Johansson, SAAB, Sweden; ¹KTH Royal Institute of Technology, Sweden MORE ELECTRIC AIRCRAFT (MEA) SCALING ASPECTS AND WEIGHT IMPACT |
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ICAS2022_0371: L. Kiszkowiak¹, A. Olejnik¹, A. Dziubinski, Lukasiewicz Research Network – Institute of Aviation, Poland; ¹Military University of Technology, Poland THE USE OF COMPUTATIONAL FLUID DYNAMICS METHODS IN THE PRELIMINARY DESIGN OF A NEW GENERATION LIGHT COMBAT AIRPLANE |
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ICAS2022_0375: P. Schmollgruber¹, C. Toussaint¹, A. Lepage¹, F. Bremmers², H. Jentink², L. Timmermans², N. Genito³, A. Rispoli³, D. Meissner, 5Airbus Operations GmbH, Germany; D. Kierbel, Airbus S.A.S., France; ¹ONERA, France; ²NLR, Netherlands; ³CIRA, Italy VALIDATION OF SCALED FLIGHT TESTING |
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ICAS2022_0413: K. Khankwa¹, T. Phiboon¹, A. Ariyarit¹, R. Kasemsri¹, M. Kanazaki, Tokyo Metropolitan University, Japan; ¹Suranaree University of Technology, Thailand AIRFOIL DESIGN BY MULTI-ADDITIONAL SAMPLING MULTI-FIDELITY EFFICIENT GLOBAL OPTIMIZATION |
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ICAS2022_0435: S. Shin¹, S. Lee¹, C. Son, Cheongju University, South Korea; K. Yee, Seoul National University, South Korea; ¹Korea Institute of Industrial Technology, South Korea AIRCRAFT DESIGN PARAMETER ESTIMATION USING DATA-DRIVEN MACHINE LEARNING MODELS |
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ICAS2022_0459: E. Kobayashi¹, K. Chiba¹; ¹The University of Electro-Communications, Japan INFLUENCES OF CHANGING THE INSTALLING POSITIONS OF MULTIPLE WINGLETS ON AERODYNAMIC CHARACTERISTICS |
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ICAS2022_0464: D. Kierbel, AIRBUS, France CLEAN-SKY 2 LARGE PASSENGER AIRCRAFT PLATFORM 1 ADVANCED ENGINE AND AIRCRAFT CONFIGURATIONS |
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ICAS2022_0478: S. Santhosh¹, M.C. Moruzzi¹, F. De Crescenzio¹, S. Bagassi¹; ¹University of Bologna, Italy AURALIZATION OF NOISE IN A VIRTUAL REALITY AIRCRAFT CABIN FOR PASSENGER WELL-BEING USING HUMAN-CENTRED APPROACH |
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ICAS2022_0484: F. Vidal de Saint Jean, Dassault Aviation, France TOWARD A GREENER AIRCRAFT ARCHITECTURE |
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ICAS2022_0505: D. Kiehn¹, J. Autenrieb¹, N. Fezans¹; ¹German Aerospace Center (DLR), Germany COAST - A SIMULATION AND CONTROL FRAMEWORK TO SUPPORT MULTIDISCIPLINARY OPTIMIZATION AND AIRCRAFT DESIGN WITH CPACS |
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ICAS2022_0521: T. Klaproth¹, M. Hornung¹; ¹Technical University of Munich, Germany SUCCESSIVE KNOWLEDGE BUILDUP AND TRANSFER DURING THE ANALYSIS OF SCALED UAV WINGS BY MEANS OF MACHINE LEARNING |
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ICAS2022_0548: Z. Lu¹, Z.-H. Han¹, Z. Zhou, Science and Technology on Scramjet Laboratory,CARDC, China; W.-P. Song¹, Y. Zhang¹; ¹Northwestern Polytechnical University, China EFFICIENT SURROGATE-BASED MULTI-OBJECTIVE OPTIMIZATION ALGORITHM WITH A NEW ADAPTIVE WEIGHT VECTOR GENERATION |
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ICAS2022_0602: K. Radhakrishnan, 1Institute of Air Transportation Systems, TUHH, Germany; K. Deck¹, P. Proesmans¹, F. Linke², F. Yin¹, V. Grewe¹, R. Vos¹, B. Lührs², M. Niklaß², I. Dedoussi¹; ¹Delft University of Technology, Netherlands; ²Air Transportation Systems, DLR, Germany MINIMIZING THE CLIMATE IMPACT OF THE NEXT GENERATION AIRCRAFT USING NOVEL CLIMATE FUNCTIONS FOR AIRCRAFT DESIGN |
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ICAS2022_0606: M. Desmet¹, J. Vervliet¹, D. De Wit¹, R. Seidler, Deutsches Zentrum Fuer Luft und Raumfahrt E.V., Germany; J. Docter, Netherlands Aerospace Centre, Netherlands; B. Everaert¹; ¹Asco Industries nv/sa, Belgium CS2 – MANTA – MULTI-FUNCTIONAL FLAP MECHANISM OFFERING A SECOND DEGREE OF FREEDOM |
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ICAS2022_0649: V. Marciello¹, M. Ruocco, SmartUp Engineering s.r.l., Italy; F. Nicolosi¹, M. Di Stasio¹; ¹University of Naples Federico II, Italy MARKET ANALYSIS, TLARS SELECTION AND PRELIMINARY DESIGN INVESTIGATIONS FOR A REGIONAL HYBRID-ELECTRIC AIRCRAFT |
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ICAS2022_0659: C. Jouannet¹, K. Amadori¹, M. Emeneth, PACE America Inc., United States; A. Papageorgiou, Linköpings University, Sweden; ¹Saab Aeronautics, Sweden UNMANNED AEW/ISR PLATFORM CONCEPTUAL DESIGN AND TECHNOLOGY ASSESSMENT |
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ICAS2022_0732: E. Moerland¹, A. Mancini¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany TOWARDS A SEAMLESS SIMULATION OF THE AIR TRANSPORT SYSTEM |
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ICAS2022_0764: D.C. Yates, Boeing, United States BOEING/SAAB CO-DEVELOPMENT PROGRAMME OF T-7A TRAINER - A JOINT DIGITAL JOURNEY |
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ICAS2022_0804: C. Jouannet, Saab Aeronautics, Sweden; I. Staack¹, T. Grönstedt², X. Zhao², P. Krus¹, A. Lundbladh, GKN Aerospace, Sweden; B. Nagel, DLR, Germany; ¹Linköpings University, Sweden; ²Chalmers, Sweden SUSTAINABLE AVIATION FOR SWEDEN - TECHNOLOGY & CAPABILITY ASSESSMENT TARGETING 2045 |
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ICAS2022_0819: R. Thijssen¹, P. Proesmans¹, R. Vos¹; ¹Delft University of Technology, Netherlands PROPELLER AIRCRAFT DESIGN OPTIMIZATION FOR CLIMATE IMPACT REDUCTION |
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ICAS2022_0850: N.F.M. Wahler¹, L. Radomsky², L.V. Hanisch², R. Mallwitz², M. Henke², A. Elham¹; ¹University of Southampton, United Kingdom; ²TU Braunschweig, Germany A CREDIBILITY-BASED CRITERION FOR THE ASSESSMENT OF FUTURISTIC AIRCRAFT CONCEPTS |
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ICAS2022_0854: B. Fröhler¹, M. Iwanizki¹, P. Balack¹, J. Häßy¹, D. Silberhorn¹; ¹German Aerospace Center (DLR), Germany IMPACT OF THE NUMBER OF WING STATIONS ON THE TWIST DISTRIBUTION OF A BWB CONCEPTUAL AIRCRAFT DESIGN IN A MDAO ENVIRONMENT TO MATCH TARGET LIFT DISTRIBUTION |
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ICAS2022_0893: L.M.F. Barbosa, Heart Aerospace, Sweden METHODOLOGIES AND EXAMPLE OF CONCEPTUAL DESIGN FOR A FOOT-LAUNCHABLE SPORT SAILPLANE |
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ICAS2022_0895: L.A.S.A Prado¹, T.S.G. Das¹, S. Coskun¹, A. Kötter¹; ¹Capgemini Engineering / Altran Deutschland und SAS KG, Germany DEVELOPMENT OF INNOVATIVE AND ECO-FRIENDLY AIRFRAME TECHNOLOGIES TO IMPROVE AIRCRAFT LIFE CYCLE ENVIRONMENTAL FOOTPRINT – LIFE CYCLE ASSESSMENT ACTIVITIES AT ECOTECH / CLEANSKY 2 |
1.2 - Aircraft Design and Integrated System (Applications) |
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ICAS2022_0050: X. Wang¹, T. Ma, Institude of Unmanned System, Beihang University, China; N. Qiao¹, J. Fu, SchoolofTransportationScienceandEngineering, Beihang University, China; ¹School of Aeronautic Science and Engineering, Beihang University, China AN INVESTIGATION ON THE IMPROVEMENT FOR TANDEM WING PITCHING MOMENT CHARACTERISTICS |
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ICAS2022_0107: C. Ding, School of Aeronautic Science and Engineering,Beihang University, China; T.-L. Ma, Institute of Unmanned System, Beihang University, China; J.-C. Fu, School of Transportation ScienceandEngineering,BeihangUniversity, China; X.-S. Wang, School of Aeronautic Science and Engineering, Beihang University, China RESEARCH ON THE OVERALL DESIGN OF A HIGH-SPEED MORPHING UAV |
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ICAS2022_0148: K. Abu Salem¹, V. Cipolla¹, G. Palaia¹, V. Binante², D. Zanetti²; ¹University of Pisa, Italy; ²SkyBox Engineering, Italy CONCEPTUAL STUDY OF HYBRID-ELECTRIC BOX-WING AIRCRAFT TOWARDS THE REDUCTION OF AVIATION EFFECTS ON LOCAL AIR QUALITY AND CLIMATE CHANGE |
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ICAS2022_0163: A. Batra¹, R. Raute, Dept. Ind. Elec. Power Conv., University of Malta, Malta; R. Camilleri¹; ¹Institute of Aerospace Technologies (IAT), University of Malta , Malta SERIES OR PARALLEL HYBRID-ELECTRIC AIRCRAFT PROPULSION SYSTEMS? CASE STUDIES OF THE ATR42 AND ATR72 |
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ICAS2022_0195: Y. Yue¹, Y. Pei¹, P. Hou¹; ¹School of Aeronautics, Northwestern Polytechnical University, China TASK ALLOCATION METHOD FOR COMPLEX RECONNAISSANCE AREA BY MULTIPLE UAVS |
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ICAS2022_0200: Y.-L. Huang¹, D.-Q. Huang¹, W. Du¹, J. Liu, Beihang University, China; ¹AVIC CHENGDU AIRCRAFT INDUSTRIAL(GROUP) CO.LTD, China RESEARCH ON THE SELECTION METHOD OF TYPICAL RCS BENCHMARK BASED ON AHP |
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ICAS2022_0210: P. Gupta, Manipal Institute of Technology, Manipal, India, India; R.S. Pant, Indian Institute of Technology Bombay, Mumbai, India, India CONCEPTUAL DESIGN AND SIZING FOR A FIXED WING UAV FOR EXPLORATION OVER MARS |
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ICAS2022_0240: L. Babetto¹, B. Kniebel¹, E. Stumpf¹; ¹ILR, RWTH Aachen University, Germany SORA-BASED RISK ASSESSMENT FOR CARGO UNMANNED AERIAL VEHICLES IN THE UAM FRAMEWORK |
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ICAS2022_0241: N. Montella¹, A. Aprovitola¹, L. Iuspa¹, G. Pezzella¹; ¹University of Campania , Italy AEROSHAPE AND TRAJECTORY DESIGN OF NEXT GENERATION RE-ENTRY VEHICLES |
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ICAS2022_0248: M.F.M. Hoogreef¹, V.O. Bonnin¹; ¹Delft University of Technology, Netherlands SCALABILITY ANALYSIS OF RADICAL TECHNOLOGIES TO VARIOUS AIRCRAFT CLASS - PART I: INITIAL DESIGNS |
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ICAS2022_0269: F. Staub¹, T. Tsuchiya¹; ¹The University of Tokyo, Japan DESIGN AND WIND TUNNEL TESTING OF A GENERAL AVIATION BLENDED WING BODY AIRCRAFT |
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ICAS2022_0340: L. Giacomossi¹, J.A. Ricardo Jr¹, J.F.B. Brancalion, EMBRAER, Brazil; M.R.O.A. Maximo¹, D.A. Santos¹; ¹ITA, Brazil COOPERATIVE THREAT ENGAGEMENT WITH HETEROGENEOUS DRONE SWARMS |
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ICAS2022_0342: R. Scigliano¹, V. De Simone¹, R. Fusaro², D. Ferretto², M. Marini¹, N. Viola²; ¹Italian Aerospace Research Center - CIRA scpa, Italy; ²Politecnico di Torino (PoliTo), Italy COOLING SYSTEM OF STRATOFLY HYPERSONIC VEHICLE: CONCEPTUAL DESIGN, NUMERICAL ANALYSIS AND VERIFICATION |
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ICAS2022_0345: M. Borghi¹, G. Clinca¹, F.A. D'Amico¹, F. Fornaseri¹, E. Versino¹; ¹Politecnico di Torino, Italy “CONCORDE-NEO”: A BIOFUEL PROPELLED SUPERSONIC COMMERCIAL AIRCRAFT WITH CONCORDE CONFIGURATION |
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ICAS2022_0358: J. Benad¹, R. Vos¹; ¹Delft University of Technology, Netherlands DESIGN OF A FLYING V SUBSONIC TRANSPORT |
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ICAS2022_0362: X. Zhao¹, C. Xisto¹, S.-H. Peng, Chalmers University of Technology/FOI, Sweden; ¹Chalmers University of Technology, Sweden DEVELOPMENT OF AN AERODYNAMIC ANALYSIS TOOL FOR BOUNDARY LAYER INGESTION CONCEPT DESIGN |
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ICAS2022_0373: R.K. Nangia, Nangia, United Kingdom; L. Hyde, Consulting, United Kingdom ARRIVING AT CERTIFIABLE NOVEL AIRLINER USING LIQUID HYDROGEN & EFFICIENCY METRICS |
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ICAS2022_0383: F. Pollet¹, S. Delbecq¹, M. Budinger, ICA, Université de Toulouse, ISAE-SUPAERO, MINES ALBI, UPS, INSA, France; J.-M. Moschetta¹, J. Liscouët, Concordia University, Canada; ¹ISAE-SUPAERO, France A COMMON FRAMEWORK FOR THE DESIGN OPTIMIZATION OF FIXED-WING, MULTICOPTER AND VTOL UAV CONFIGURATIONS |
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ICAS2022_0408: Y. Fukumine¹, Z. Lei¹; ¹Suwa University of Science, Japan ESTIMATION OF EVTOL FLIGHT PERFORMANCE USING ROTORCRAFT THEORY |
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ICAS2022_0431: P.D. Bravo-Mosquera¹, J.P. Eguea¹, H.D. Cerón-Muñoz¹, F.M. Catalano¹; ¹University of São Paulo, Brazil EXPERIMENTAL INVESTIGATION OF A NEXT-GENERATION AIRLINER WITH BOUNDARY LAYER INGESTION |
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ICAS2022_0444: M. Sugiura¹, Y. Tanabe¹, N. Kobiki¹, H. Sugawara¹, K. Kimura¹; ¹JAXA, Japan HIGH-SPEED COMPOUND HELICOPTER RESEARCH AT JAXA |
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ICAS2022_0446: P.D. Bravo-Mosquera¹, T. Chau², F.M. Catalano¹, D.W. Zingg²; ¹University of São Paulo, Brazil; ²University of Toronto, Canada EXPLORATION OF BOX-WING AIRCRAFT CONCEPT USING HIGH-FIDELITY AERODYNAMIC SHAPE OPTIMIZATION |
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ICAS2022_0447: V. Nan Fernandez-Ayala¹, L. Vimláti¹, A. Matoses Gimenez¹, H. Delmotte¹, M. Ivchenko¹, R. Mariani¹; ¹KTH Royal Institute of Technology, Sweden DESIGN OF A HALE UAV FOR ATMOSPHERIC IMAGING |
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ICAS2022_0462: J. Mieloszyk¹, A. Tarnowski¹, A. Kwiek¹, R. Topolewski¹, T. Goetzendorf-Grabowski¹; ¹Warsaw University of Technology, Poland MEDIUM SIZE UAV AS TEST PLATFORM FOR NEW TECHNOLOGIES |
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ICAS2022_0481: V.O. Bonnin¹, M.F.M. Hoogreef¹; ¹Delft University of Technology, Netherlands SCALABILITY ANALYSIS OF RADICAL TECHNOLOGIES TO VARIOUS AIRCRAFT CLASS - PART II: SENSITIVITY ANALYSIS |
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ICAS2022_0496: C. Xisto, Chalmers University of Technology, Sweden; A. Lundbladh, GKN Aerospace AB, Sweden DESIGN AND PERFORMANCE OF LIQUID HYDROGEN FUELLED AIRCRAFT FOR YEAR 2050 EIS |
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ICAS2022_0498: G. Piccirillo¹, S. Graziani¹, R. Fusaro¹, N. Viola¹; ¹Politecnico di Torino, Italy LTO NOISE AND SONIC BOOM PREDICTIONS IN EARLY CONCEPTUAL DESIGN PHASES |
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ICAS2022_0541: J. Gauvrit-Ledogar¹, N. Berend¹, J. Hermetz¹; ¹ONERA, France FLIGHT EXPERIMENTS FOR THE ALTAIR SEMI-REUSABLE AIR-LAUNCH SYSTEM WITH THE DEMONSTRATOR EOLE |
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ICAS2022_0544: T. Jiang¹, M. Li¹, Y. Liu¹, Y. Zheng¹; ¹School of Aeronautics and Astronautics, Zhejiang University, China MIXED INTEGER NONLINEAR PROGRAMMING FOR EVTOL AIRCRAFT DESIGN AND OPTIMIZATION |
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ICAS2022_0546: J. Gauvrit-Ledogar¹, A. Tremolet¹, F. Moens¹, M. Méheut¹, S. Defoort¹, R. Liaboeuf¹, F. Morel¹, B. Paluch¹; ¹ONERA, France MULTIDISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION PROCESS DEDICATED TO BLENDED WING BODY CONFIGURATIONS |
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ICAS2022_0551: O. Gori, Politecnico di Torino, Italy SIMPLIFIED MODELS FOR THE PRELIMINARY AERODYNAMIC CHARACTERIZATION OF HIGH-SPEED VEHICLES TO SUPPORT MISSION ANALYSIS |
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ICAS2022_0572: N. Viola¹, R. Fusaro¹, D. Ferretto¹, O. Gori¹, M. Marini², P. Roncioni², B.O. Cakir³, A.C. Ispir³, B.H. Saracoglu³; ¹Politecnico di Torino, Italy; ²CIRA, Italy; ³VKI, Belgium HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONS |
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ICAS2022_0584: L.-W. Zhang¹, Z.-H. Han¹, J.-L. Qiao¹, Y.-L. Ding¹, Q. Chen¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China A RAPID DESIGN METHOD FOR QUIET SPIKE OF SUPERSONIC TRANSPORT AIRCRAFT |
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ICAS2022_0593: M. Fouda¹, E.J. Adler², J.H. Bussemaker¹, J.R.R.A. Martins², D.F. Kurtulus, Middle East Technical University, Turkey; L. Boggero¹, B. Nagel¹; ¹DLR, Germany; ²University of Michigan, United States AUTOMATED HYBRID PROPULSION MODEL CONSTRUCTION FOR CONCEPTUAL AIRCRAFT DESIGN AND OPTIMIZATION |
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ICAS2022_0609: V. Polepeddi¹, P. Raj¹, M. Emeneth, PACE America, United States; ¹Virginia Tech, United States REGIONAL TRANSPORT AIRCRAFT DESIGN USING TURBO-ELECTRIC DISTRIBUTED PROPULSION (TEDIP) SYSTEM |
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ICAS2022_0622: A. Heidebrecht¹, K. Burger¹, M. Hoogreef¹, R. Vos¹, A.T. Isikveren, SAFRAN S.A. c/o Aerospace Embedded Solutions GmbH, Munich, Germany; A. Gangoli Rao¹; ¹TU Delft, Netherlands DEVELOPMENT OF A HYDROGEN-POWERED FUSELAGE-MOUNTED BLI PROPULSOR ADD-ON FOR PASSENGER AIRCRAFT |
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ICAS2022_0641: F. Nicolosi¹, V. Marciello¹, V. Cusati¹, F. Orefice¹; ¹University of Naples Federico II, Italy TECHNOLOGY ROADMAP AND CONCEPTUAL DESIGN OF HYBRID AND ELECTRIC CONFIGURATIONS IN THE COMMUTER CLASS |
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ICAS2022_0674: S. Song¹, S. Deng¹, Q. Li, AVIC General Aircraft Research Institute, China; H. Qiao¹, Y. Lu¹; ¹Nanjing University of Aeronautics and Astronautics, China NUMERICAL INVESTIGATION ON THE AERO-PROPULSION EFFECT OF DISTRIBUTED PROPULSION FOR V/VTOL APPLICATION |
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ICAS2022_0699: R. Kalra¹, P. Flores-Peña, Drone Hopper S.L., Spain; A. Sanchez-Carmona¹, C. Cuerno-Rejado¹; ¹Universidad Politécnica de Madrid, Spain ENHANCING UAS DESIGN PROCESS FOR SPECIFIC CATEGORY OPERATIONS USING SORA |
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ICAS2022_0703: A.S.J. van Heerden¹, S. Sasi¹, R. Ghelani¹, D. Sanders¹, I. Roumeliotis¹; ¹Cranfield University, United Kingdom A SCALABLE HYDROGEN PROPULSION SYSTEM FOR CIVIL TRANSPORT AIRCRAFT |
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ICAS2022_0729: E.T. da Silva¹, A.G.P. Sarmento¹, T.R. de Paula¹, A.S. Oliveira¹, J. Possamai¹, H.C. Marques¹, M.M. Cardoso¹, E. Villani¹; ¹Aeronautics Institute of Technology, Brazil UNMANNED AERIAL VEHICLE – HUMAN PERFORMANCE EVALUTION UNDER CRITICAL OPERATIONAL SCENARIO |
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ICAS2022_0760: Z.-K. Li¹, S.-G. Su, Aerospace Times Feihong Technology Co., Ltd. , China; Z.-Y. Li¹, F.-R. Li¹, G. Chao¹; ¹Northwestern Polytechnical University, China RESEARCH ON THE DESIGN OF UNMANNED AERIAL VERICLE FOR MINE INSPECTION |
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ICAS2022_0762: S. Horinouchi, SuperSonic Jet Planning Inc., Japan CONCEPT DESIGN OF A LOW BOOM SSBJ TO SATISFY SOCIAL ACCEPTANCE |
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ICAS2022_0778: J.-J. Lee¹, J.-H. Lee¹; ¹Korea Aerospace Research Institute, South Korea DESIGN STUDY OF BRAKE MECHANICAL CONTROL SYSTEM OF UAV |
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ICAS2022_0840: D. Kloock-Schreiber¹, M. Swaid², V. Gollnick¹, A. Fay, HSU, Institute of Automation Technology, Germany; M. Niklaß²; ¹TUHH, Institute of Air Transportation Systems, Germany; ²DLR, Institute of Air Transportation Systems, Germany INNOVATIVE URBAN AIR MOBILITY FROM THE PERSPECTIVE OF THE HAMBURG METROPOLITAN REGION |
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ICAS2022_0858: J. Kim¹, T. Tsuchiya¹; ¹The University of Tokyo, Japan OPENVSP BASED AERODYNAMIC DESIGN OPTIMIZATION TOOL BUILDING METHOD AND ITS APPLICATION TO TAILLESS UAV |
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ICAS2022_0947: S.-K. Paek, Korea Aerospace Research Institute, South Korea KARI-DLR DIGITAL COLLABORATION TO BUILD A MDAO SYSTEM FOR THE PRELIMINARY DESIGN OF HYBRID EVTOL AIRCRAFT |
2 - Systems Engineering and Integration |
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ICAS2022_0011: J. La¹, C. Bil¹, I. Heiets¹, K.A. Lau, Qatar Airways, Qatar; ¹RMIT University, Australia DOOR-TO-DOOR TRAVEL PLANNER FOR IMPROVED TRAVELER EXPERIENCE USING DIGITAL TWIN CONCEPT |
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ICAS2022_0063: M. Fuchs¹, F. Beckert¹, F. Rauscher¹, C. Goetz¹, J. Biedermann¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany VIRTUAL RECONFIGURATION AND ASSESSMENT OF AIRCRAFT CABINS USING MODEL-BASED SYSTEMS ENGINEERING |
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ICAS2022_0079: S.J. Wright¹, J. Aaltonen¹; ¹Tampere University, Finland FUEL CELLS AND NOVEL THERMAL MANAGEMENT ADVANCEMENTS REQUIRED FOR AVIATION |
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ICAS2022_0082: S.M. Lübbe¹, M. Schäfer¹, O. Bertram¹; ¹German Aerospace Center (DLR), Germany COUPLING OF MODEL-BASED SYSTEMS ENGINEERING AND SAFETY ANALYSIS IN CONCEPTUAL AIRCRAFT SYSTEM DESIGN |
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ICAS2022_0142: X. Sun¹, M. Luo¹, Z. Cui¹, Z. Ji¹, H. Liu¹; ¹Beihang University, China A COLLABORATIVE DESIGN METHOD FOR CIVIL AIRCRAFT BASED ON AN ENDURING AND EVOLUTIONARY AUTHORITATIVE SOURCE OF TRUTH |
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ICAS2022_0352: L. Knöös Franzén¹, R. Chaitanya Munjulury¹, P. Krus¹; ¹Linköping University, Sweden ONTOLOGY-ASSISTED AIRCRAFT CONCEPT GENERATION |
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ICAS2022_0434: R. Hällqvist¹, J. Naeser¹, J. Wallén Axehill¹, E. Herzog¹; ¹Saab AB, Sweden HETEROGENEOUS SYSTEMS MODELLING IN SUPPORT OF INCREMENTAL DEVELOPMENT |
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ICAS2022_0453: D. Kim¹, F. Karagoz¹, S. Datta¹, M. Balchanos¹, D.H. Anvid¹, E.D. Harrison¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States A MODEL BASED SYSTEMS ENGINEERING APPROACH TO STREAMLINED NOISE CERTIFICATION OF TRANSPORT-TYPE AIRCRAFT |
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ICAS2022_0467: L. Debschütz¹, A. Seefried², T. Westermeier¹, R. Kuchar², D. Schwalb¹; ¹Airbus Defence and Space, Germany; ²German Aerospace Center, Germany EXPERIMENTAL INVESTIGATION OF FUEL SLOSH IN A GENERIC FIGHTER WING TANK CONFIGURATION |
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ICAS2022_0472: M.E.A. Enes¹, E. Tugrul¹, M. Yuce¹, N. Sever¹, E. Yigit¹, T. Inal¹; ¹Turkish Aerospace, Turkey A FAULT INTEGRATOR BASED VOTE&MONITOR DESIGN FOR GRACEFULL DEGRADATION IN MULTIPLE REDUNDANT SAFETY CRITICAL SYSTEMS |
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ICAS2022_0477: A. Oprea¹, R. Hällqvist¹, I. Staack, Linköping University, Sweden; M. Eek, Swedish National Road and Transport Research Institute, Sweden; H. Gavel¹; ¹Saab Aeronautics, Sweden MODEL FIDELITY AND ITS INFLUENCE ON AIRCRAFT CONCEPTUAL DESIGN |
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ICAS2022_0493: B. Wenhao¹, L. Yuhui¹, W. Weixiang¹, Z. An¹; ¹Northwestern Polytechnical University, China HUMAN-MACHINE FUNCTION ALLOCATION METHOD FOR SINGLE PILOT OPERATION USING HESITANT FUZZY 2-TUPLE LINGUISTIC INFORMATION |
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ICAS2022_0506: A. Johansson, Saab Aeronautics, Sweden; M. Yildiz¹, L. Bertling-Tjernberg¹; ¹Royal Institute of Technology (KTH), Sweden MORE ELECTRIC AIRPLANE: CASE STUDY STOCKHOLM - COPENHAGEN |
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ICAS2022_0526: A.G. Slongo¹, C. Jochims Lau¹, T.B. Volkmann¹, G. de Oliveirra¹, G. Heberle¹, B.M. Ramos¹; ¹AEL Sistemas, Brazil EXTRACTING MODEL-BASED SYSTEMS ENGINEERING VALUE THROUGH A MINIMUM VIABLE PRODUCT CASE STUDY AT AEL SISTEMAS |
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ICAS2022_0604: I. Sander¹, I. Söderquist², M. Ekman², R. Jordao¹, F. Bahrami¹, R. Chen¹, A. Åhlander²; ¹KTH Royal Institute of Technology, Sweden; ²Saab AB, Sweden TOWARDS CORRECT-BY-CONSTRUCTION DESIGN OF SAFETY-CRITICAL EMBEDDED AVIONICS SYSTEMS |
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ICAS2022_0615: L. Boggero¹, T. Lefèbvre, ONERA/DTIS, France; J. Vankan, Royal Netherlands Aerospace Centre (NLR), Netherlands; B. Beijer, KE-works, Netherlands; V. Saluzzi, Bombardier Aviation, Canada; B. Nagel¹; ¹German Aerospace Center (DLR), Germany THE AGILE 4.0 MBSE-MDAO DEVELOPMENT FRAMEWORK: OVERVIEW AND ASSESSMENT |
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ICAS2022_0645: J.L. Lovaco¹, I. Staack¹, P. Krus¹; ¹Linköpings Universitet, Sweden ENVIRONMENTAL AGENT-BASED MODELLING FOR A FIREFIGHTING SYSTEM OF SYSTEMS |
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ICAS2022_0655: E. Razafimahazo¹, P. de Saqui-Sannes¹, R.A. Vingerhoeds¹, J. Soula², R. Mège², C. Baron, LAAS-CNRS, France; ¹ISAE-SUPAERO, France; ²CSTB, France TOWARDS A CUSTOMIZABLE ARCHITECTURE FOR INDOOR MULTI-USAGES DRONES |
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ICAS2022_0660: R. Saar de Moraes¹, S. Nadjm-Tehrani¹; ¹Linköping University, Sweden CONCEPT LEVEL EXPLORATION OF IMA-BASED NETWORKED PLATFORMS WITH MIXED TIME-SENSITIVE COMMUNICATION REQUIREMENTS |
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ICAS2022_0661: P. Andersson¹, M. Lejon¹, A. Pradas¹, M. Jacobson¹; ¹GKN Aerospace Sweden, Sweden DEMONSTRATING AN APPROACH FOR MULTIDISCIPLINARY SET BASED DESIGN WITHIN AN AEROSPACE RESEARCH PROJECT - DEFAINE |
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ICAS2022_0665: N. Kuelper¹, J. Broehan¹, T. Bielsky¹, F. Thielecke¹; ¹Hamburg University of Technology, Germany SYSTEMS ARCHITECTING ASSISTANT (SARA) - ENABLING A SEAMLESS PROCESS CHAIN FROM REQUIREMENTS TO OVERALL SYSTEMS DESIGN |
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ICAS2022_0700: J. Zamboni¹, A. Zamfir¹, E. Moerland¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany A SEMANTIC KNOWLEDGE BASED ENGINEERING FRAMEWORK FOR THE RAPID GENERATION OF NOVEL AIR VEHICLE CONFIGURATIONS |
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ICAS2022_0702: B. Boden¹, Y. Cabac¹, T. Burschyk¹, B. Nagel¹; ¹DLR, Germany RULE-BASED VERIFICATION OF A GEOMETRIC DESIGN USING THE CODEX FRAMEWORK |
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ICAS2022_0707: E. Villani¹, J. Alfredsson², M. Bång³, B. Johansson³, U. Anderini², D. Arjoni¹; ¹Aeronautics Institute of Technology (ITA), Brazil; ²SAAB AB, Sweden; ³Linköping University, Sweden HMI-HUFLAB – A BRAZILIAN - SWEDISH INITIATIVE IN HUMAN FACTORS FOR AERONAUTICS |
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ICAS2022_0724: E. Allegaert¹, Y. Lemmens¹, E. Ongut¹; ¹Siemens Digital Industries Software, Belgium TEMPLATE-BASED SYNTHESIS OF 3D SYSTEMS FOR MBSE |
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ICAS2022_0791: M.C. Berschik¹, M. Blecken¹, H. Kumawat¹, J.-E. Rath¹, D. Krause¹, R. God¹, T. Schüppstuhl¹; ¹Hamburg University of Technology, Germany A HOLISTIC AIRCRAFT CABIN METAMODEL AS AN APPROACH TOWARDS AN INTERCONNECTED DIGITISED CABIN LIFECYCLE |
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ICAS2022_0797: C. Krammer, Germany; F. Schweighofer, Germany; D. Gierszewski, Germany; S.P. Scherer, Germany; T. Akman, Germany; H. Hong, Germany; F. Holzapfel, Germany REQUIREMENTS-BASED GENERATION OF OPTIMAL VERTICAL TAKEOFF AND LANDING TRAJECTORIES FOR ELECTRIC AIRCRAFT |
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ICAS2022_0874: P. Krus¹, I. Staack¹, A.A.M. Oliveira, Federal University of Santa Catharina, Brazil; ¹Linköping University, Sweden HYBRID ELECTRIC PROPULSION SYSTEM OPTIMIZATION FOR A COMMUTER AIRCRAFT |
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ICAS2022_0875: L. Pereira, Federal University of ABC, Brazil; P. Krus, Linköping University, Sweden CRITICALITY AND COMFORT ZONE SUPPORTING DESIGN CHOICES TO ACHIEVE SUSTAINABLE REQUIREMENTS: THE CASE OF ELECTRIC AIRCRAFT |
3.1 - Aerodynamics – CFD Methods and Validation |
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ICAS2022_0020: R. Castellanos¹, J. Bowen Varela¹, A. Gorgues¹, E. Andrés¹; ¹INTA, Spain AN ASSESSMENT OF REDUCED-ORDER AND MACHINE LEARNING MODELS FOR STEADY TRANSONIC FLOW PREDICTION ON WINGS |
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ICAS2022_0029: D. Mo¹, H. Lin¹, C. Liang¹, S. Shang¹, J. Xia, Aero Engine Academy of China, China; Y. Liu¹; ¹AECC Shenyang Engine Research Institute, China TWO-PHASE NUMERICAL SIMULATION INVESTIGATION ON THE EFFECTS OF TURBULENCE MODEL AND OPERATING CONDITIONS ON THE CENTRIFUGAL NOZZLE PERFROMANCE |
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ICAS2022_0033: K.-L. Wang¹, Z. Zhou¹; ¹Northwestern Polytechnical University, China INVESTIGATION ON CRUISE PERFORMANCE OF A HAND-LAUNCHED SOLAR-POWERED UAV FOR ENVIRONMENTAL MONITORING IN TIBET |
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ICAS2022_0043: R. Zahn¹, A. Weiner, Technical University of Braunschweig, Germany; C. Breitsamter¹; ¹Technical University of Munich (TUM), Germany WING BUFFET PRESSURE LOAD PREDICTION BASED ON A HYBRID DEEP LEARNING MODEL |
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ICAS2022_0051: A. Porcarelli, KTH - Royal Institute of Technology, Sweden DEVELOPMENT OF A CFD MODEL AND METHODOLOGY FOR THE INTERNAL FLOW SIMULATION IN A HYDROGEN-POWERED UAV |
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ICAS2022_0104: A. Rizzi¹, D. Henningson¹; ¹KTH, Sweden AERONAUTICAL CFD AND TURBULENCE - PROGRESS AND CHALLENGES |
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ICAS2022_0124: D. Standingford¹, C. Sequeira², M. Allan¹, C. Rider², G. Furse², J. Sharpe¹; ¹Zenotech, United Kingdom; ²Flare Bright, United Kingdom VALIDATING AIRSPACE CFD MODELS FOR DRONE OPERATION WITH FLIGHT TEST DATA |
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ICAS2022_0147: E.K.T. Carias¹, S.A. Prince¹; ¹Cranfield University, United Kingdom VALIDATION STUDY OF BLUNTED AND SHARP CONES AT HYPERSONIC SPEED |
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ICAS2022_0157: S.-Q. Han, Sichuan University, China; W.-P. Song¹, Z.-H. Han¹; ¹Northwestern Polytechnical University, China A COMPUTATIONAL STUDY ON BLADE-VORTEX INTERACTION FOR COAXIAL ROTORS IN HOVER USING A NOVEL HIGH-ORDER SCHEME |
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ICAS2022_0173: K. Rajkumar¹, J. Radtke¹, E. Tangermann¹, M. Klein¹; ¹University of the Bundeswehr Munich, Germany OPEN CAVITY SIMULATIONS UNDER SIDESLIP FLOW CONDITIONS |
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ICAS2022_0191: F.B. Oliveira, Instituto Tecnológico de Aeronáutica, Brazil; J.L.F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil ON THE INFLUENCE OF GRADIENT RECONSTRUCTION PROCEDURES OVER THE ACCURACY OF FINITE VOLUME BASED SCHEMES |
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ICAS2022_0204: Y. Zhao¹, Y. Liu¹, S. Zhu¹, H. Xu¹, D. Wang¹; ¹Department of Aeronautics and Astronautics, Fudan University, China INVESTIGATION OF TWO-DIMENSIONAL VORTEX DYNAMICS IN THE V103 CASCADE |
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ICAS2022_0236: A. Capitao Patrao¹, B. González Lozano¹, I. Jonsson¹, C. Xisto¹; ¹Chalmers University of Technology, Sweden NUMERICAL MODELING OF LAMINAR-TURBULENT TRANSITION IN AN INTERCONNECTING COMPRESSOR DUCT |
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ICAS2022_0242: P. Eliasson¹, P. Weinerfelt¹, F. Bramkamp, NSC, Sweden; ¹Saab, Sweden ENHANCING CFD PREDICTIONS FOR THE GRIPEN AIRCRAFT |
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ICAS2022_0260: L.P. Velandia Luis¹, P. Celso Greco Junior¹; ¹University of Sao Paulo, Brazil VISCOUS CORRECTION FOR HIGH ORDER IMMERSED INTERFACE METHOD FOR COMPRESSIBLE TRANSONIC FLOWS |
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ICAS2022_0286: R. Moretti¹, J. Decours¹; ¹ONERA, France EXTERNAL-INTERNAL AERODYNAMIC COUPLING ON A TURBOPROP ENGINE USING THE BODY-FORCE METHOD |
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ICAS2022_0317: R. Spencer, CFMS Ltd, United Kingdom; M. Allan, Zenotech Ltd, United Kingdom COMPUTATIONALLY ECONOMICAL METHODS FOR LANDING GEAR NOISE SIMULATIONS |
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ICAS2022_0330: Y. Wang, China; S.-Q. Zhang, China; W.-P. Song, China; Z.-H. Han, China UNSTEADY SIMULATIONS OF MASSIVELY SEPARATED FLOW AROUND NACA0021 AIRFOIL USING A TRANSITIONAL IDDES MODEL |
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ICAS2022_0341: M. Sinisi¹, G. Cantanna¹, G. Occhipinti¹, A. Caramazza¹, G. Dilonardo¹, E. Cestino¹; ¹Politecnico di Torino, Italy CFD TAKE-OFF ANALYSIS OF A SEAPLANE HULL THROUGH A DYNAMIC MULTIPHASE MODEL |
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ICAS2022_0349: D. Passiatore¹, L. Sciacovelli, ENSAM Paris, France; P. Cinnela , Sorbonne Université, France; G. Pascazio¹; ¹Politecnico di Bari, Italy NUMERICAL INVESTIGATION OF HYPERSONIC TURBULENT BOUNDARY LAYERS WITH HIGH-TEMPERATURE EFFECTS |
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ICAS2022_0351: C. Tavera Guerrero¹, N. Glodic¹, H. Mårtensson, GKN Aerospace Sweden AB, Sweden; ¹KTH, Sweden STEADY-STATE AERODYNAMICS TIP GAP INFLUENCE IN A TRANSONIC LINEAR CASCADE AT NEAR STALL |
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ICAS2022_0353: G. Muchla¹, A. Kwiecien¹; ¹Faculty of Power and Aeronautical Engineering, WUT, Poland COMPARATIVE ANALYSIS OF AERODYNAMIC CHARACTERISTICS OBTAINED BY ANALYTICAL, PANEL AND CFD METHOD |
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ICAS2022_0357: A.-O. Sezer¹, M. Elfarra, Ankara Y?ld?r?m Beyaz?t University, Turkey; H.-I. Ünlü¹; ¹Turkish Aerospace, Turkey NUMERICAL INVESTIGATION OF ROTORCRAFT PRESSURE ERROR CORRECTION BY UTILIZATION OF AIR DAMS |
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ICAS2022_0376: S.-H. Peng, Swedish Defence Research Agency, FOI, Sweden HYBRID RANS-LES MODELLING: SOME RECENT DEVELOPMENT AND AERODYNAMIC APPLICATIONS |
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ICAS2022_0384: L.K. Fitzgerald¹, A.J. Niven¹, P.C. Griffin¹; ¹University of Limerick, Ireland A STATIC STABILITY COMPARISON OF WIND TUNNEL AND COMPUTATIONAL FLUID DYNAMICS METHODS |
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ICAS2022_0410: S. Han¹, Y. Xu¹; ¹Chinese Aeronautical Establishment, China NUMERICAL PREDICTION OF FOCUS BOOM GENERATED BY MANEUVERS |
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ICAS2022_0414: B. Kierulf, Northeastern University, United States CRITICAL REVIEW OF SOUNDING ROCKET FLIGHT DATA AND COMPUTATIONAL FLUID DYNAMICS EFFORTS |
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ICAS2022_0416: K. Abe¹, S. Miyazaki¹, D. Sasaki¹, S. Takahashi², G. Yamada²; ¹Kanazawa Institute of Technology, Japan; ²Tokai University, Japan COMPUTATIONAL ANALYSIS OF SUPERSONIC FLOW AROUND A WEDGE AND A CYLINDER USING BUILDING-CUBE METHOD |
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ICAS2022_0421: L. Qu, China; S. Han, China; Y. Song, China; Y. Xu, China; Y. Zhang, China; Y. Wang, China IN-FLIGHT MEASUREMENTS AND ESTIMATION OF SONIC BOOM SIGNATURE OF SUPERSONIC AIRCRAFT |
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ICAS2022_0422: H.-Y. Li¹, X. Zhao¹, Z.-X. Xia¹; ¹School of Aeronautics, Northwestern Polytechnical University, China A FAST PREDICTION METHOD FOR DROPPING WATER OF FIRE FIGHTING AIRCRAFT BASED ON EXTERNAL BALLISTICS OF PARTICLES |
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ICAS2022_0487: Z.-P. Li, AECC Shenyang Engine Research Institute, China REDESIGNING AND SIMULATION EVALUATION ON LARGE-FLOW HIGH-TEMPERATURE HIGH-PRESSURE BYPASS SURGE-OUT SYSTEM |
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ICAS2022_0528: T. Di Fabbio¹, E. Tangermann¹, M. Klein¹; ¹Universität der Bundeswehr München, Germany INVESTIGATION OF LEADING-EDGE VORTICES ON A TRIPLE-DELTA-WING CONFIGURATION USING SCALE-ADAPTIVE SIMULATION |
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ICAS2022_0555: C.-H. Gao¹, W.-P. Song¹, S.-Q. Han¹, K. Lu¹, Y. Wang¹, Z.-H. Han¹, B. Wu, Shanghai Electro-mechanical Engineering Institute, China; ¹Northwestern Polytechnical University, China HIGH-ACCURATE NUMERICAL SIMULATION FOR VORTEX FLOW OVER A SLENDER MISSILE AT HIGH ANGLE OF ATTACK |
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ICAS2022_0557: P. Wegener¹, S. Keye¹; ¹DLR, Germany CAD DEFORMATION FOR THE CONSIDERATION OF AEROELASTIC EFFECTS |
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ICAS2022_0571: J.S. Kern¹, A. Hanifi¹, D.S. Henningson¹; ¹FLOW, Department of Engineering Mechanics, KTH Royal Institute o, Sweden ANALYSIS OF A LAMINAR SEPARATION BUBBLE ON A NACA0009 AIRFOIL AT DIFFERENT BACKGROUND DISTURBANCE LEVELS |
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ICAS2022_0596: P. Roncioni¹, M. Marini¹, R. Fusaro², N. Viola²; ¹CIRA, Italy; ²POLITO, Italy AERODATABASE DEVELOPMENT AND INTEGRATION OF SUPERSONIC/HYPERSONIC CRUISER VEHICLES IN MORE&LESS PROJECT |
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ICAS2022_0630: M. Dhake¹, C. Thantanapally¹, S. Arcidiacono¹, S. Ansumali¹; ¹SankhyaSutra Labs Ltd, India TRANSONIC FLOW OVER DELTA WING USING ENTROPIC LATTICE BOLTZMANN METHOD |
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ICAS2022_0643: V. Gryazev, United Kingdom; U. Armani, United Kingdom; A.R. Murali, France; A.P. Markesteijn, United Kingdom; S.A. Karabasov, United Kingdom; V. Toropov, United Kingdom; S.E. Naghibi, United Kingdom; V. Riabov, Japan APPLICATION OF GENETIC PROGRAMMING AND ARTIFICIAL NEURAL NETWORK APPROACHES FOR RECONSTRUCTION OF TURBULENT JET FLOW FIELDS |
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ICAS2022_0672: A.R.S. Righi, ITA, Brazil; G.L.O. Halila¹, J.L.F. Azevedo¹; ¹IAE, Brazil A STUDY ON THE NUMERICAL SIMULATION OF FLOW TRANSITION INCLUDING CROSSFLOW EFFECTS |
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ICAS2022_0676: D.S. Tonon¹, J.T. Tomita¹, C. Bringhenti¹, D.F.C. Barbosa¹, L.H.L. Whitacker¹, L.E.N. Almeida, AVIBRAS, Brazil; ¹Aeronautics Institute of Technology , Brazil EFFECTS OF TWO WINGLET TIP GEOMETRIES ON THE FLOW AND AERODYNAMIC PERFORMANCE OF A HYDRAULIC AXIAL TURBINE |
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ICAS2022_0684: S. Arvidson¹, M. Carlsson, Chalmers University of Technology, Sweden; S. Nilsson¹; ¹Saab Aeronautics, Sweden EFFECT OF LES LENGTH SCALE AND NUMERICAL SCHEME IN HYBRID RANS-LES OF FREE SHEAR LAYER FLOWS |
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ICAS2022_0710: W. Klimczyk¹, A. Sieradzki¹; ¹Lukasiewicz Research Network - Institute of Aviation, Poland PROPELLER AEROACOUSTIC MODELS IN VARIABLE-FIDELITY DESIGN OPTIMIZATION |
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ICAS2022_0711: H.R. Zandi Pour¹, M. Iovieno¹; ¹Politecnico di Torino, Italy HEAT TRANSFER ENHANCEMENT BY SUSPENDED PARTICLES IN A TURBULENT SHEARLESS FLOW |
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ICAS2022_0726: J.A.A. Lyrio¹, J.L.F. Azevedo², D.A. Rade¹, R.G. da Silva², C. Breviglieri, Embraer, S. A., Brazil; ¹Instituto Tecnologico de Aeronautica, DCTA/ITA, Brazil; ²Instituto de Aeronautica e Espaço, DCTA/IAE/ALA, Brazil STUDY OF THE EFFECTS OF NUMERICAL MODEL ENHANCEMENTS FOR AEROSTRUCTURAL ANALYSIS IN TRANSONIC FLOWS |
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ICAS2022_0735: V. Gulizzi, University of Palermo, Italy HIGH-ORDER ACCURATE EMBEDDED-BOUNDARY DISCONTINUOUS GALERKIN METHODS FOR INVISCID GAS DYNAMICS |
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ICAS2022_0746: R.O. Bura, Republic of Indonesia Defense University, Indonesia; F.A. Maulana, Indonesia TURBULENCE MODELLING STUDIES OF SHOCK-WAVE/BOUNDARY-LAYER INTERACTIONS ON HIFIRE-1 AXISYMMETRIC CONE CYLINDER FLARE IN HYPERSONIC FLOWS |
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ICAS2022_0749: M.A.L. Matunaga, ITA - Instituto Tecnológico de Aeronáutica, Brazil; J.L.F Azevedo, IAE - Instituto de Aeronáutica e Espaço, Brazil AUTOMATIC FREE-FORM DEFORMATION AS GEOMETRIC PARAMETERIZATION FOR AERODYNAMIC DESIGN |
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ICAS2022_0790: K. Sugaya¹, T. Imamura¹; ¹The University of Tokyo, Japan UNSTEADY TURBULENT FLOW SIMULATION OF ROTOR BLADES ON MOVING CARTESIAN GRIDS USING RECURSIVE FITTING APPROACH |
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ICAS2022_0869: D.M. Pio¹, C.F. Rafael¹, P.S.C. Villela¹, G.A.L. da Silva¹, M. Ferro, Laboratorio Nacional de Computacao Cientifica -, Brazil; M.J.M. Guedes, Marinha do Brasil, Brazil; ¹Aerothermal Solutions - ATS, Brazil LARGE EDDY SIMULATION OF A LYNX HELICOPTER LANDING IN THE BARROSO CORVETTE SHIP |
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ICAS2022_0887: R. Santos¹, L. Alves¹, N. Cerulus², H. Quintanilha Jr², V. Theofilis²; ¹UFF, Brazil; ²UoL, United Kingdom ACCURATE TWO-DIMENSIONAL STEADY-STATES FOR THE SUPERSONIC FLOW OVER A COMPRESSION CORNER |
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ICAS2022_0914: K.J. Fidkowski, University of Michigan, United States DATA-DRIVEN ADAPTATION AND OPTIMIZATION OF TURBULENT FLOWS |
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ICAS2022_0946: A. Rizzi¹, D. Henningson¹; ¹KTH, Sweden AERONAUTICAL CFD AND TURBULENCE - PROGRESS AND CHALLENGES PART 2 |
3.2 - Experimental Aerodynamics |
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ICAS2022_0024: J. Pereira, National Research Council Canada, Canada OPTIMIZATION OF AN ACTIVE DAMPING SYSTEM FOR USE WITH A SINGLE STRUT MOUNT |
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ICAS2022_0045: C. Bu¹, Z. Ma¹, Y. Zhang¹, L. Li¹; ¹AVIC Aerodynamics Research Institute, China DEVELOPMENT AND VERIFICATION OF OSCILLATING BLADE GUST GENERATOR IN LOW-SPEED WIND TUNNEL |
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ICAS2022_0061: J.H. You¹, M.C.N. Wright¹, H. Quix¹; ¹European Transonic Windtunnel GmbH, Germany RECENT ACTIVITIES ON FLOW QUALITY ASSESSMENT AT THE EUROPEAN TRANSONIC WINDTUNNEL |
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ICAS2022_0075: D. Sedlacek¹, C. Breitamter¹; ¹Technical University of Munich, Germany STRAKE SECTION IMPACT ON HYBRID-DELTA-WING AERODYNAMICS |
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ICAS2022_0078: Y. Shen¹, S. Feng¹, Y. Wang¹, C. Bu¹, H. Tan¹, W. Mu¹, H. Chen¹; ¹AVIC Aerodynamics Research Institute, China EXPERIMENTAL STUDY ON NON-COMMAND MOTION CHARACTERISTICS OF SMALL ASPECT RATIO FLYING WING |
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ICAS2022_0083: D. Schröder¹, T. Leweke, CNRS, Aix-Marseille Université, Centrale Marseille, France; R. Hörnschemeyer¹, E. Stumpf¹; ¹Institute of Aerospace Systems, RWTH Aachen University, Germany VOLUMETRIC VELOCITY MEASUREMENTS OF A HELICAL VORTEX PAIR |
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ICAS2022_0128: F.L. dos Santos¹, L. Botero-Bolivar¹, C.H. Venner¹, L.D. de Santana¹; ¹University of Twente, Netherlands AERODYNAMIC AND AEROACOUSTIC CHARACTERISTICS OF THE NACA 0008 AIRFOIL |
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ICAS2022_0145: T.D. Nguyen¹, M. Taguchi¹, M. Kashitani¹, K. Kusunose, Formerly Japan Aerospace Exploration Agency, Japan; ¹National Defense Academy of Japan, Japan ANALYSIS OF LOW-SPEED AERODYNAMIC CHARACTERISTICS OF BUSEMANN BIPLANE AIRFOIL INSTALLED HIGH LIFT DEVICES |
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ICAS2022_0154: J.-S. Han¹, C. Breitsamter¹; ¹Technical University of Munich, Germany WIND-TUNNEL TEST ON LEADING-EDGE VORTEX OF LOW-ASPECT-RATIO FLAPPING PLATES |
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ICAS2022_0215: R. Mariani¹, S. Suewatanakul¹, S. Ghika¹, L.A. Penela¹, P. Wennhage¹, B. Zang, University of Bristol, United Kingdom; ¹KTH Royal Institute of Technology, Sweden WIND TUNNEL TEST OF A BLENDED WING BODY UNMANNED AERIAL VEHICLE |
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ICAS2022_0243: A. Inasawa¹, R. Taniguchi¹, M. Asai¹, M. Sasamori², M. Kurita²; ¹Tokyo Metropolitan University, Japan; ²JAXA, Japan EXPERIMENTAL INVESTIGATION OF THE EFFECT OF THE YAW ANGLE ON THE DRAG REDUCTION RATE FOR TRAPEZOIDAL RIBLETS |
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ICAS2022_0250: J. Stegmüller¹, S. Hayböck¹, P. Hartl¹, C. Breitsamter¹; ¹Technical University of Munich, Germany EXPERIMENTAL INVESTIGATIONS OF AN AEROELASTIC WIND TUNNEL MODEL FOR TAIL BUFFETING ANALYSIS |
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ICAS2022_0256: X. Jiang¹, G. Liu¹, J. Zhou¹, Q. Jia¹; ¹AECC Shenyang Engine Research Institute, China EXPERIMENTAL INVESTIGATION ON JET IMPINGEMENT HEAT TRANSFER WITH CROSS FLOW FOR AERO-ENGINE INLET CONE |
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ICAS2022_0262: G.P.G. Silva¹, M.V.R.J. Silva¹, J.P. Eguea¹, F.M. Catalano¹; ¹Department of Aeronautical Engineering, University of Sao Paulo, Brazil EXPERIMENTAL STUDIES ON THE INTERACTION BETWEEN PROPELLERS AND WING |
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ICAS2022_0270: L. Fan¹, T. Guo¹, L. Zhang¹, H. Zhang¹; ¹CARDC, China EXPERIMENTAL INVESTIGATION ON TRANSPORT AIRPLANE LONGITUDINAL STABILITY ENHANCEMENT IN CRITICAL ICING CONDITION |
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ICAS2022_0347: D. Steiling¹, P. Aschwanden¹, J. Müller¹, T. Jax¹; ¹RUAG AG, Switzerland POWERED WIND TUNNEL TESTING WITH HYDRAULIC MOTORS |
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ICAS2022_0378: S. Noel¹, D.M. Birch², J.J. Doherty², T. Tipnis¹; ¹QinetiQ, United Kingdom; ²University of Surrey, United Kingdom WALL INTERFERENCE CORRECTIONS USING NONLINEAR LEAST-SQUARES OPTIMISATION |
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ICAS2022_0411: Z. Guocheng¹, B. Anyu ¹, C. Bao¹, L. Xiangnan¹; ¹AVIC ARI, China AN OVERVIEW OF AERO-ACOUSTIC EXPERIMENTAL TECHNOLOGY IN AVIC FL-10 WIND TUNNEL |
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ICAS2022_0417: M.-H. Kang¹, X. Zhao¹, R. Yao¹, H.-Y. Li¹; ¹Norhwestern Polytechnical University, China INFLUENCE OF TIP DIHEDRAL ON ROTOR AERODYNAMIC PERFORMANCE AND TIP VOTEX |
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ICAS2022_0437: A. Esposito, DEPT.OF INDUSTRIAL ENGINEERING UNIVERSITY OF NAPLES FEDERICO II, Italy; C. Allouis, STEMS-CNR, Italy; M. Lappa, Dept of Mech. and Aer.Engineering, University of Strathclyde, United Kingdom A NEW FACILITY FOR HYPERSONIC FLOW SIMULATION DRIVEN BY A HIGH VELOCITY OXYGEN FUEL GUN |
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ICAS2022_0547: Y. Jiao, China; H. Zou, China; B. Chen, China; C. Xiao, China INVESTIGATION ON CORRECTION OF TUNNEL WALL INTERFERENCE FOR DYNAMIC AIRFOIL TEST IN LOW-SPEED WIND TUNNEL |
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ICAS2022_0583: T. Jaroslawski¹, O. Vermeersch¹, J.-M. Moschetta², M. Forte¹, E. Gowree²; ¹ONERA, France; ²ISAE-SUPAERO, France STABILTY AND TRANSITION OF A LAMINAR SEPARATION BUBBLE SUBJECTED TO FREESTREAM TURBULENCE |
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ICAS2022_0589: B.-B. Jia¹, Z.-B. Zhang¹, H.-X. Li, AECC, China; ¹AECC Shenyang Engine Institute, China SURGE CHARACTERISTICS IN FRONT OF EACH STAGE FOR A HIGH PRESSURE FIVE STAGE COMPRESSOR |
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ICAS2022_0611: F. Scarano¹, M.C. Jacob, Université de Lyon, France; X. Carbonneau¹, E.R. Gowree¹; ¹ISAE - SUPAERO, France UNIFORM MOMENTUM ZONES IN A TURBULENT BOUNDARY LAYER OVER PERFORATED WALLS |
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ICAS2022_0625: N. Taymourtash¹, A. Zanotti¹, G. Gibertini¹, G. Quaranta¹; ¹Politecnico di Milano, Italy EXPERIMENTING ROTORCRAFT FLIGHT IN COMPLEX ENVIRONMENTAL CONDITIONS USING THE WIND TUNNEL: HELICOPTER SHIP LANDING CASE |
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ICAS2022_0696: S. Hammer¹, J. Fridh¹, M. Billson, GKN Aerospace Sweden, Sweden; ¹KTH Royal Institute of Technology, Sweden IDENTIFICATION OF CRITICAL ACOUSTIC MODES FOR AN OPEN BOX CAVITY WITH ADJUSTABLE DEPTH |
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ICAS2022_0720: J. Zastrow¹, F. Oberdieck¹, U. Henne¹, C. Klein¹; ¹DLR - German Aerospace Center, Germany NUMERICAL AND EXPERIMENTAL INVESTIGATIONS ON THE DLR-F23 COMBAT AIRCRAFT WIND TUNNEL MODEL |
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ICAS2022_0814: N. Kishimoto, Setsunan University, Japan; D. Wada¹, M. Tamayama¹, Y. Iwami², N. Tomita², T. Ikeda³, Y. Tanahashi³, K. Katagiri, Osaka Research Institute of Science and Technology, Japan; ¹JAXA, Japan; ²Yamashina Institute for Ornithology, Japan; ³Chubu University, Japan WIND TUNNEL EXPERIMENT OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) AND BLACK KITE (MILVUS MIGRANS) |
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ICAS2022_0834: B.-B. XU¹, C.J. Wu¹, F.Z. Sun¹, J.P. Tang¹, W.T. Xiong¹; ¹China Aerodynamics Research and Development Center, China INFLUENCE OF MANEUVERING PROCESS ON PERFORMANCE CHARACTERISTICS OF BELLY INLET OF AIRCRAFT |
3.3 - Basic Fluid Dynamics and Flow Control |
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ICAS2022_0037: M.M. Jentys¹, C. Breitsamter¹; ¹Technical University of Munich, Germany TRANSITIONAL FLOW MODELLING OF A HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER TRANSONIC TRANSPORT AIRCRAFT WING |
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ICAS2022_0156: L. Wang, Beihang University, China; C.W. Wong¹, Y. Zhou¹; ¹Harbin Institute of Technology, China OPTIMIZATION STUDY ON THE FLOW SEPARATION CONTROL USING A SAWTOOTH PLASMA ACTUATOR |
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ICAS2022_0238: P. Eliasson, Saab, Sweden; A. Rizzi¹, J. Oppelstrup¹, M. Zhang, Airinnova AB, Sweden; ¹KTH, Sweden IMPROVING STALL CHARACTERISTICS OF UCAV WING WITH VORTEX GENERATORS |
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ICAS2022_0302: H. Li¹, X. Wang¹, D. Yu¹, F. Liu¹; ¹Shenyang Aircraft Design and Research Institute, China RESEARCH ON PRESSURE LOAD OF AN EMBEDDED JET NOZZLE |
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ICAS2022_0403: W. Stalewski, Lukasiewicz Research Network- Institute of Aviation, Poland PRELIMINARY STUDY ON A FLUIDIC DEVICE SUPPORTING AIRCRAFT-FLIGHT CONTROL |
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ICAS2022_0530: A.R. Proenca¹, S.A. Prince¹, L. Banks-Davies¹, K.P. Garry¹; ¹Cranfield University, United Kingdom EXPERIMENTAL EVALUATION OF A PASSIVE FLOW-CONTROL DEVICE FOR A TILTROTOR AIRCRAFT |
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ICAS2022_0605: J.M. Faúndez Alarcón¹, K. Sasaki¹, A. Hanifi¹, R. Larsson, Saab Aeronautics, Sweden; D.S. Henningson¹; ¹KTH Royal Institute of Technology, Linné FLOW Centre, Sweden REACTIVE CONTROL OF BYPASS TRANSITION IN A WING BOUNDARY LAYER |
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ICAS2022_0635: V.G. Kleine, ITA, Brazil; A. Hanifi¹, D.S. Henningson¹; ¹KTH, Sweden ANALYSIS OF THE STABILITY OF MULTIPLE HELICAL VORTICES USING COMPLEX-STEP LINEARIZATION |
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ICAS2022_0680: T. Coelho Leite Fava¹, D. Henningson¹, A. Hanifi¹; ¹KTH, Sweden DIRECT NUMERICAL SIMULATIONS OF A THICK, ROTATING AIRFOIL AT A LOW REYNOLDS NUMBER |
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ICAS2022_0697: E.R. Gowree, ISAE-SUPAERO, France; C.J. Atkin, University of East Anglia, United Kingdom STABILITY OF A LAMINAR BOUNDARY LAYER OVER LOCALISED SURFACE INDENTATION |
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ICAS2022_0780: M. Bremm¹, R. Hörnschemeyer¹, E. Stumpf¹; ¹RWTH Aachen University, Germany EXPERIMENTS TO INVESTIGATE LIFT PRODUCTION MECHANISMS ON OSCILLATING TRAILING-EDGE FLAPS |
3.4 - Applied Aerodynamics |
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ICAS2022_0092: P. Yan, Shenyang Aircraft Design and Research Institute, China; F. Liu, Shenyang Aircraft Design and Research Institute, Chinese Aeronau, China A NOVEL EMBEDDED INLET BASED ON THE INTEGRATED DESIGN CONCEPT OF FUSELAGE AND INLET |
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ICAS2022_0126: R. Jesudasan¹, R. Mariani¹, A. Hanifi¹; ¹KTH Royal Institute of Technololgy, Stockholm, Sweden PRELIMINARY AERODYNAMIC WING DESIGN OPTIMISATION FOR WING-IN-GROUND EFFECT AIRCRAFT |
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ICAS2022_0150: R. Larsson, Saab Aeronautics, Sweden ANALYSIS OF THE EFFECT OF FLOW TRANSITION OVER THE WINGS OF THE BLADE DEMONSTRATOR |
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ICAS2022_0165: W.-Y. Zhou¹, G.-Q. Yang¹, X. Gao¹, X.-Y. Zhu¹, B.-X. Zhou¹; ¹AVIC Xi’an Flight Automatic Control Research Institute, China NUMERICAL SIMULATION OF MISSILE AIR-LAUNCHED DYNAMIC PROCESS UNDER DOWNWASH FLOW OF HELICOPTER ROTOR |
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ICAS2022_0219: J.-H. Dai¹, P.-Q. Liu¹, L. Li¹; ¹Beihang University, China MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF 2D HIGH-LIFT DEVICE BASED ON DISTRIBUTED DEEP REINFORCEMENT LEARNING |
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ICAS2022_0232: P. D'Alesio¹, G. Travostino¹, P. Planquart², G. Glabeke²; ¹Piaggio Aerospace, Italy; ²von Karman Institute, Belgium WIND TUNNEL TESTS RESULTS AND PERFORMANCE OF THE MOTHIF BLOWN FLAP |
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ICAS2022_0251: J.B. Vos¹, A. Gehri¹, H. Truong², A. Marouf², Y. Hoarau²; ¹CFS Engineering, Switzerland; ²University of Strasbourg, ICUBE Research Institute, France USING ACTIVE FLOW CONTROL TO IMPROVE THE AERODYNAMIC PERFORMANCE OF THE NEXT GENERATION CIVIL TILT ROTOR AIRCRAFT |
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ICAS2022_0259: A. Aprovitola¹, N. Montella¹, L. Iuspa¹, G. Pezzella¹, A. Viviani¹; ¹University of Campania , Italy AERODYNAMIC AND AEROTHERMODYNAMIC ASSESSMENT OF A LIFTING-BODY RE-ENTRY VEHICLE |
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ICAS2022_0312: Y. Leng¹, K. Fayez, DELAIR, France; J.-M. Moschetta¹, M. Bronz, ENAC, France; ¹ISAE-SUPAÉRO, France A STUDY OF HIGH-LIFT DEVICES FOR LOW REYNOLDS NUMBER APPLICATIONS |
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ICAS2022_0318: R. Jan¹, J.-M. Moschetta¹, J.-P. Condomines, ENAC, France; ¹ISAE-SUPAERO, France PREDICTING STEADY LIFT AND DRAG COEFFICIENT OF TANDEM AIRCRAFT USING PRANDTL’S EXTENDED LIFTING-LINE THEORY IMPLEMENTED UNDER ASWING |
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ICAS2022_0319: Z. Wei, China RESEARCH ON THE INFLUENCE OF FLIGHT ATTITUDE ON UNILATERAL MISSILE SEPARATION FROM EMBEDDED BAY |
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ICAS2022_0329: C.H. Ge¹, P.Q. Liu¹, Q.L. Qu¹; ¹Beihang University, China NUMERICAL STUDY ON WATER DISPLACEMENT DRAG CHARACTERISTICS OF AIRCRAFT ELASTIC TIRE ON CONTAMINATED RUNWAYS |
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ICAS2022_0335: R. Boisard¹, L. Lefevre¹, T. Zhang², G. Barakos², A. Visingardi, CIRA, Italy; F. Lößle³, A. Kostek³, T. Andronikos, NTUA, Greece; M. Keßler*, R. Wickersheim*, A. Colliº, G. Gibertiniº, A. Zanottiº; ¹ONERA, France; ²University Of Glasgow, United Kingdom; ³DLR, Germany; *University of Stuttgart, Germany; ºPolitecnico di Milano, Italy ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUP |
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ICAS2022_0367: F. Yu¹, J. Bartasevicius¹, M. Hornung¹; ¹Technical University of Munich, Germany COMPARING POTENTIAL FLOW SOLVERS FOR AERODYNAMIC CHARACTERISTICS ESTIMATION OF THE T-FLEX UAV |
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ICAS2022_0380: B.D.J. Schreiner¹, D.G. MacManus¹, F. Tejero¹, F. Sanchez-Moreno¹, C. Sheaf, Rolls Royce, United Kingdom; ¹Cranfield University, United Kingdom TRANSONIC NACELLE DESIGN FOR FUTURE MEDIUM RANGE AERO-ENGINES |
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ICAS2022_0385: Y. Lu, China; A. Del Buono, Italy; T. Xiao, China; A. Iafrati, Italy; J. Xu, China ON THE APPLICABILITY ASSESSMENT OF VON KARMAN’S MOMENTUM THEORY IN PREDICTING THE WATER-ENTER LOAD OF V-SHAPED BODY |
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ICAS2022_0570: M. Hackström¹, F. Kållberg¹, P. Nordström¹; ¹Saab Aeronautics, Sweden AERODYNAMIC DEVELOPMENT OF SAAB FCAS UNMANNED SUPERSONIC COMBAT AIRCRAFT |
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ICAS2022_0653: H.W.M. Hoeijmakers¹, L.H. Groot Koerkamp¹, L.D. de Santana¹, C.H. Venner¹, S. Stramigioli¹, J.L. Mulder¹, A. Brentjes¹, F. Gijsman¹, S.A. Hartman¹; ¹University of Twente, Netherlands INVESTIGATION FLAPPING-FLIGHT AERODYNAMICS OF A ROBOTIC BIRD |
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ICAS2022_0678: J.P. Eguea¹, G.P.G. Silva¹, F.M. Catalano¹; ¹USP, Brazil PUSHER PROPELLER INFLUENCE ON A LAMINAR WING TRANSITION LOCATION USING INFRARED THERMOGRAPHY |
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ICAS2022_0860: D. Perdolt¹, D. Milz¹, M. May¹, M. Thiele, Technical University of Munich, Germany; ¹German Aerospace Center, Germany EFFICIENT MID-FIDELITY AERODYNAMIC MODELING OF A TILT-WING EVTOL FOR CONTROL APPLICATIONS |
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ICAS2022_0889: G.J. Resende¹, V. Malatesta¹, M.C. Savio², B.M. Castro²; ¹ITA - Aeronautics Institute of Technology, Brazil; ²EMBRAER, Brazil STUDY OF EFFECTS ON THE WING'S AERODYNAMIC CHARACTERISTICS DUE TO DISTRIBUTED PROPULSION OVER WINGSPAN |
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ICAS2022_0905: E.J. Adler¹, A.C. Gray¹, J.R.R.A. Martins¹; ¹University of Michigan, United States TO CFD OR NOT TO CFD? COMPARING RANS AND VISCOUS PANEL METHODS FOR AIRFOIL SHAPE OPTIMIZATION |
4.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance |
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ICAS2022_0005: D. Desgaches, AIRBUS, France USE OF FRICTION STIR WELDING ON PRIMARY STRUCTURES OF AIRCRAFTS INSTEAD OF RIVETED JUNCTION |
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ICAS2022_0012: I. Rivero¹, A. Palomar¹, N. Martin¹, M. Lozano¹, J. Romero¹, B. De Nicolas¹, M. Rebollo¹, J. Gomez-Escalonilla¹; ¹Airbus, Spain TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES AEROSTRUCTURES |
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ICAS2022_0028: S. Olsson¹, B. Carlsson¹, B. Helgesen¹; ¹Quintus Technologies AB, Sweden FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSURE |
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ICAS2022_0036: C. Matias¹, A. Diskin¹, O. Golan, Afeka- Tel-Aviv Academic College of Engineering, Israel; A. Garkun², E. Strokin²; ¹Israel Aerospace Industries (IAI), Israel; ²The Israel Institute of Metals,, Israel TI-6AL-4V ADDITIVE MANUFACTURING MEASURE OF QUALITY ACCORDING TO FATIGUE CRACK INITIATION VS. CRACK PROPAGATION |
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ICAS2022_0052: Y. Yang¹, S. Lyu¹; ¹Aircraft Strength Research Institute, China A DAMAGE RECOGNITION METHOD OF COMPOSITE STRUCTURES USING ARTIFICIAL DEFECTIONS |
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ICAS2022_0101: J.-H. Cha¹, C.-G. Kim¹; ¹KAIST, South Korea DOPAMINE-COATED UHMWPE/HYDROGEN-RICH BENZOXAZINE COMPOSITES FOR SPACE RADIATION SHIELDING |
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ICAS2022_0111: Z. Kapidzic¹, S.B. Lindström, Linköping University, Sweden; J. Lundgren¹; ¹Saab AB, Sweden INCREMENTAL FATIGUE DAMAGE MODEL: APPLICATION TO PLANE PROBLEMS WITH NON-PROPORTIONAL LOADING |
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ICAS2022_0206: A. Ariaseta, Sweden; N. Sadeghinia, Sweden; J. Andersson, Sweden INFLUENCE OF KEYHOLE TIG WELDING PARAMETERS ON WELD GEOMETRY OF NEWLY-DEVELOPED SUPERALLOY VDM ALLOY 780 |
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ICAS2022_0207: Y. Nishijima¹, H. Tanaka¹, A. Biron, Special Military School of Saint-Cyr, France; T. Miura¹; ¹National Defense Academy, Japan VARIATIONS IN STRUCTURAL PROPERTIES OF LATTICE STRUCTURES DEPENDING ON UNIT CELL SHAPE FOR MORPHING WINGS |
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ICAS2022_0218: A. Alaimo¹, G. Mantegna¹, C. Orlando¹, D. Tumino¹, C.R. Vindigni¹; ¹Faculty of Engineering and Architecture Kore University of Enna, Italy RVE-BASED HOMOGENIZATION OF ADDITIVELY MANUFACTURED POROUS METALS |
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ICAS2022_0253: R. Augello¹, E. Carrera¹, A. Pagani¹, M. Petrolo¹; ¹Politecnico di Torino, Italy A GLOBAL/LOCAL ELEMENT-WISE APPROACH FOR THE BUCKLING AND POST-BUCKLING ANALYSIS OF THIN MULTILAYERED STRUCTURES |
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ICAS2022_0278: D. Wang, School of Aeronautics, Northwestern Polytechnical University, Xi, China; G.W. Li, School of civil aviation, Northwestern Polytechnical University, China; H.Y. Huang, School of Aeronautics, Northwestern Polytechnical University, China STUDY ON MECHANICAL PROPERTIES OF CARBON FIBER RESIN MATRIX COMPOSITE BOLTED JOINT STRUCTURE AT HIGH TEMPERATURE |
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ICAS2022_0280: G. Nicolosi¹, A. Lunghitano ¹, S. Lombardi ¹, T. Talamucci¹, A. Caivano¹, N. Simone¹, E. Cestino¹, V. Sapienza, Aeronautical Engineering Consultant, Italy; ¹Politecnico di Torino, Italy WING STATIC STRUCTURAL ANALYSIS AND EXPERIMENTAL TESTING OF A COMPOSITE 1:8 S55-X REPLICA |
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ICAS2022_0289: G. Gastaldo, France; Y. Rafik, France; M. Budinger, France; V. Pommier-Budinger, France; P. Olivier, France; P. Navarro, France PROPOSITION OF A NEW QUALIFICATION IMPACT TEST FOR AEROSPACE SMART STRUCTURES |
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ICAS2022_0343: A.R. de Faria, ITA, Brazil ASSESSMENT OF FAILURE UNDER LONGITUDINAL COMPRESSION OF UNIDIRECTIONAL COMPOSITES WITH IN-PLANE FIBER MISALIGNMENT |
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ICAS2022_0393: H. Rahman¹, R. De Breuker¹, S.G.P. Castro¹; ¹Delft University of Technology, Netherlands OPTIMAL DESIGN OF STIFFENED PANELS UNDER BUCKLING CONSTRAINTS: A DESIGN METHODOLOGY CONSIDERING CAD-BASED PARAMETERIZATION WITH SIMULTANEOUS LAYOUT AND SIZING OPTIMIZATION |
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ICAS2022_0396: A. Polla, Politecnico di Torino; Royal Melbourne Institute of Technology, Italy; G. Frulla¹, E. Cestino¹, R. Das², P. Marzocca²; ¹Politecnico di Torino, Italy; ²Royal Melbourne Institute of Technology, Australia NUMERICAL AND EXPERIMENTAL STRUCTURAL CHARACTERIZATION OF COMPOSITE ADVANCED JOINT FOR ULTRA LIGHT AEROSPACE PLATFORMS |
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ICAS2022_0561: S. Sieberer¹, J. Homan, Fatec Engineering, Netherlands; M. Schagerl¹; ¹Johannes Kepler University Linz, Austria FATIGUE OF NOTCHED STANDARD SPECIMENS – THE INFLUENCE OF THE STRESS GRADIENT ON THE S-N CURVE IN AL2024 |
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ICAS2022_0607: S. Stekovic¹, R. Romero-Ramirez¹, L. Selegård, Saab Aeronautics, Sweden; ¹Linköping University, Sweden EFFECT OF NITRIDING ON MICROSTRUCTURE AND MECHANICAL PROPERTIES ON A TI64 ALLOY FOR AEROSPACE APPLICATIONS |
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ICAS2022_0608: X. Jia¹, H. Du¹, L. Zhang¹, X. Zhang¹, Z. Zhong¹; ¹AVIC The first Aircraft Institute, China ELECTROMAGNETIC INTERFERENCE SHIELDING EFFECTIVENESS OF THE THIN CARBON NANOFIBERS/ SILICON CARBIDE FABRICS COMPOSITES |
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ICAS2022_0632: B. Yan¹, G. Zhang¹, M. Tong¹, L. Li¹, D. Yu¹, S. Zhu¹, Z. Wu², H. Wang², T. Jin, China Special Vehicle Research Institute, China; ¹Nanjing University of Aeronautics & Astronautics, China; ²Nanjing University of Aeronautics and Astronautics, China EXPERIMENTAL INVESTIGATIONS ON TENSILE PROPERTIES OF ALUMINUM HONEYCOMB SANDWICH STRUCTURES WITH SINGLE-SIDED REPAIRING |
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ICAS2022_0685: C. Bisagni¹, E. Labans¹; ¹Delft University of Technology, Netherlands INVESTIGATION OF BUCKLING RESPONSE OF CYLINDRICAL SHELLS USING 3D-PRINTING TECHNOLOGY |
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ICAS2022_0690: G. Di Mauro¹, P. Russo, Institute for Polymers, Composites and Biomaterials, C.N.R., Italy; M. Guida¹; ¹University of Naples Federico II – Department of Industrial Eng., Italy MECHANICAL CHARACTERIZATION OF A COMPOSITE STRUCTURAL BATTERY LAMINATE |
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ICAS2022_0692: D. Fanteria¹, L. Boni ¹, F. Bovecchi¹, D.O. Busse, IRBUS Operations GmbH, Germany; D. Furfari, AIRBUS Operations GmbH, Germany; ¹University of Pisa, Italy FATIGUE LIFE ENHANCEMENT OF TYPICAL AERONAUTICAL JOINTS BY MEANS OF ENGINEERED RESIDUAL STRESSES |
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ICAS2022_0705: L.P.S. Ferreira¹, M.O. Yano², S. Silva², C.A. Cimini¹; ¹UFMG, Brazil; ²UNESP, Brazil DAMAGE QUANTIFICATION ON COMPOSITE STRUCTURES USING NEURAL NETWORKS AND HYBRID DATA |
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ICAS2022_0754: O. Orell¹, J. Jokinen¹, M. Kanerva¹; ¹Tampere University, Finland FATIGUE CHARACTERIZATION OF ADHESIVE JOINTS IN AEROPLANES-THE DEVELOPMENT OF A NEGATIVE LOAD RATIO (R<0) TESTING METHOD |
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ICAS2022_0777: H. El Fazani¹, J. Coil¹, J. Laliberté¹; ¹Carleton University , Canada FATIGUE CRACK PROPAGATION IN ADDITIVELY MANUFACTURED POLYMER PARTS |
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ICAS2022_0799: W.R.P. Mendonca¹, M.R.B. Rodrigues¹; ¹Embraer S.A., Brazil APPLICATION OF THE VIRTUAL CRACK CLOSURE TECHNIQUE FOR CRACKS IN BUILT-UP PANELS |
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ICAS2022_0820: C. Willberg¹, J.-T. Hesse¹, D. Krause¹; ¹German Aerospace Center, Germany PERIDYNAMIC SIMULATION PLATTFORM TO DETERMINE VIRTUAL ALLOWABLES OF MANUFACTURING DEVIATIONS |
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ICAS2022_0822: G.C. Cristea¹, A. Stefan¹, K. Krawczyk, Joanneum Research, Austria; C.-E. Pelin¹, S. Ilina¹; ¹INCAS, Romania TRIBOLOGICAL AND STRUCTURAL EVALUATION OF 3D PRINTED EPOXY RESINS |
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ICAS2022_0831: V.R. Pakkam Gabriel¹, P. Fernberg¹; ¹Luleå University of Technology, Sweden FATIGUE DAMAGE MODEL OF HIGH TEMPERATURE POLYMER COMPOSITES IN AERO-ENGINES |
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ICAS2022_0862: Y.J. Liu, AVIC the First Aircraft Institute, China RESEARCH ON THE DUCTILE FRACTURE OF AL7085 AND TC11 UNDER COMPLEX STRESS STATE |
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ICAS2022_0894: M. Atif¹, X.Z. Shi¹, M.A. Raza¹, M.Z. Sheikh¹, J. Shen, Joint International Research Center of Impact Dynamics and Its E, China; Y. Li, School of Civil Aviation, Northwestern Polytechnical University, China; ¹Northwestern Polytechnical University, China HIGH IMPACT AND DAMAGE TOLERANT MULTICOMPONENT ALLOY FOR HIGH STRAIN RATE APPLICATIONS |
4.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity |
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ICAS2022_0016: J. Lübker, Germany SOME EXPERIMENTAL RESULTS ON DYNAMIC AEROELASTICITY OF PLATES AND SHELLS IN SUBSONIC AND SUPERSONIC FLOW. |
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ICAS2022_0030: F. Franke¹, U. Burger¹, C. Hühne, German Aerospace Center, Germany; ¹Technische Hochschule Ingolstadt, Germany A REDUCED ORDER MODEL FOR FULL-SCALE DRONE COLLISIONS |
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ICAS2022_0032: Y. Liu¹, K. Xu, Aero Engine Academy of China, China; Y. Chen¹, Y. Wu¹, Q. Du¹, D. Mo¹; ¹AECC Shenyang Engine Research Institute, China DYNAMIC STRESS SIMULATION AND ASYMMETRY STATOR DESIGN FOR A FAN BLISK |
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ICAS2022_0038: V.A.S. Paiva¹, L.H.S. Teixeira¹, J.H. Izuka¹, P.G. Ramos¹, P.R.G. Kurka¹; ¹UNICAMP, Brazil EXPERIMENTAL AND NUMERICAL ANALYSIS OF A PRE-STRESSED TENSEGRITY MEMBRANE |
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ICAS2022_0044: J. Cecrdle, Czech Aerospace Research Centre (VZLU), Czech Republic UPDATING OF JET TRAINER AIRCRAFT DYNAMIC MODEL TO RESULTS OF GROUND VIBRATION TEST |
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ICAS2022_0059: G.C. Fonseca, Embraer Minas Gerais, Brazil; S.F.M. Almeida, Instituto Tecnológico de Aeronáutica, Brazil NUMERICAL ANALYSIS AND COMPARISON WITH RESULTS OF FRACTURE TESTS OF LUG MANUFACTURED IN COMPOSITE MATERIAL |
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ICAS2022_0158: V. Handojo¹, T. Klimmek¹, T. Streit, DLR - Institute of Aerodynamics and Flow Technology, Germany; ¹DLR - Institute of Aeroelasticity, Germany LOADS ANALYSIS AND STRUCTURAL OPTIMIZATION OF A LONG-RANGE TRANSPORT CONFIGURATION WITH HYBRID LAMINAR FLOW CONTROL |
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ICAS2022_0161: A. Voß¹, T. Klimmek¹; ¹DLR Institute of Aeroelasticity , Germany AEROELASTIC MODELING, LOADS ANALYSIS AND STRUCTURAL DESIGN OF A FIGHTER AIRCRAFT |
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ICAS2022_0178: F. Sturm¹, M. Hornung¹; ¹Technical University of Munich, Germany MORPHING FORWARD WING SECTION SKIN DESIGN FOR A SAILPLANE CONSIDERING WING BENDING |
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ICAS2022_0220: R. Azzara¹, M. Filippi¹, A. Pagani¹, E. Carrera¹; ¹Politecnico di Torino, Italy NONLINEAR VIBRATION-BUCKLING INVESTIGATION OF UNSTIFFENED AND STIFFENED STRUCTURES SUBJECTED TO MECHANICAL AND THERMAL LOADINGS |
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ICAS2022_0228: S. Pülm¹, V. Handojo¹, R.B. Seidler¹; ¹German Aerospace Center (DLR) e.V., Germany XRF1 HIGH LIFT LOAD ANALYSIS OF WING AND HIGH LIFT SYSTEM |
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ICAS2022_0247: M.C. Moruzzi¹, M. Cinefra, Poliecnico di Bari, Italy; S. Bagassi¹, E. Zappino, Politecnico di Torino, Italy; ¹Università di Bologna, Italy VIBRO-ACOUSTIC ANALYSIS OF MULTI-LAYER CYLINDRICAL SHELL-CAVITY SYSTEMS VIA CUF FINITE ELEMENTS |
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ICAS2022_0290: X.J. Zhang¹, D. Guo¹, H.Y. Huang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China DESIGN AND STUDY ON NOISE REDUCTION PROPERTIES OF A MULTISTAGE BIONIC MEMBRANE-TYPE ACOUSTIC METAMATERIAL |
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ICAS2022_0295: E. Carrera, Politecnico di Torino, Italy; U. Galvanetto, University of Padova, Italy; S. De Rosa, Università degli Studi di Napoli, Italy; P. Gardonio, University of Udine, Italy; A. Milazzo, Università degli Studi di Palermo, Italy; R. Vescovini, Politecnico di Milano, Italy; M. Zaccariotto, University of Padua, Italy DEVELOPMENT AND APPLICATIONS OF A VIRTUAL HYBRID PLATFORM FOR MULTISCALE ANALYSIS OF ADVANCED STRUCTURES OF AIRCRAFT (DEVISU) |
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ICAS2022_0311: K. Lu¹, W.-P. Song¹, K. Ye¹, C.-H. Gao¹, S.-Q. Han, Sichuan University, China; ¹Northwestern Polytechnical University, China A NUMERICAL METHOD FOR STUDY ON THE AERO-ELASTICITY OF AIR-TO-AIR MISSILES IN OVER-THE-SHOULDER LAUNCH |
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ICAS2022_0316: G.-W. Li¹, T.-H. Luo¹, H.-Y. Hang¹; ¹Northwestern Polytechnical University, China RESEARCH ON THE EFFECT OF THE PROCESS FIRST SHOT PEENING STRENGTHENING THEN SHOT PEENING FORMING ON FATIGUE STRENGTH OF 7050 HIGH-STRENGTH ALUMINUM ALLOY |
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ICAS2022_0372: X. Chen¹, A. Riaz¹, M.D. Guenov¹; ¹Cranfield University, United Kingdom SET-BASED DESIGN COORDINATION BETWEEN COUPLED SYSTEMS: A WING AERO-STRUCTURAL DESIGN PERSPECTIVE |
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ICAS2022_0399: D. Massegur¹, D. Clifford¹, A. Da Ronch¹, S. Symon¹; ¹University of Southampton, United Kingdom COMPARING REDUCED ORDER MODEL FORMS FOR NONLINEAR DYNAMICAL SYSTEMS |
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ICAS2022_0427: G. Guarino¹, V. Gulizzi¹, A. Milazzo¹; ¹1University of Palermo, Department of Engineering, Italy TRANSIENT AND FREE-VIBRATION ANALYSIS OF LAMINATED SHELLS THROUGH THE DISCONTINUOUS GALERKIN METHOD |
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ICAS2022_0436: F. Toffol¹, F. Fonte, Leonardo Helicopters, Italy; S. Ricci¹; ¹Politecnico di Milano, Italy DESIGN OF AN INNOVATIVE WING TIP FOR AEROELASTIC CONTROL: FROM SCRATCH TO FLIGHT TEST |
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ICAS2022_0519: S. Hosseini¹, H.R. Ovesy¹, M.A. Vaziri-Zanjani¹; ¹Amirkabir University of Technology, Iran WING LOADING PROCESS IN KNOWLEDGE-BASED AIRCRAFT DESIGN AND OPTIMIZATION FRAMEWORK |
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ICAS2022_0524: R.C.M. Cheung¹, H. Gu¹, F. Healy¹, D. Rezgui¹, J.E. Cooper¹; ¹University of Bristol, United Kingdom LATERAL GUST BEHAVIOUR OF AIRCRAFT INCORPORATING FLARED FOLDING WINGTIPS |
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ICAS2022_0532: A. Tamkan¹, P. Flassig¹, M. Meyer, Rolls-Royce Deutschland, Germany; ¹Technische Hochschule Brandenburg, Germany ENHANCEMENT OF FLEXIBLE STRATEGY FOR AUGMENTING DESIGN POINTS FOR COMPUTER EXPERIMENTS AND APPLICATION TO A MDO OF A FAN-BLISK |
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ICAS2022_0545: T. Miyake¹, H. Terashima¹; ¹Hokkaido University, Japan NUMERICAL INVESTIGATION ON THE DOUBLE TRANSONIC DIP OF SUPERCRITICAL AIRFOIL FLUTTER |
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ICAS2022_0560: Y. Le Lamer¹, J. Morlier, ICA, Université de Toulouse, ISAE-SUPAERO, MINES ALBI, UPS, INSA, France; E. Benard¹, P. He, Iowa State University, United States; ¹ISAE-SUPAERO, Université de Toulouse, France AEROELASTIC ANALYSIS OF HIGH ASPECT RATIO AND STRUT-BRACED WINGS |
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ICAS2022_0616: W. Grendysa, Warsaw University of Technology, Poland A NEW APPROACH TO SHAPING THE PUSHROD TUBE AS THE MAIN COMPONENT OF THE CONTROL SYSTEM, OPTIMIZATION, AND MANUFACTURING TECHNOLOGY. |
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ICAS2022_0644: G. Dessena¹, D.I. Ignatyev¹, J.F. Whidborne¹, A. Pontillo, University of Bristol, United Kingdom; L. Zanotti Fragonara¹; ¹Cranfield University, United Kingdom GROUND VIBRATION TESTING OF A HIGH ASPECT RATIO WING WITH REVOLVING CLAMP |
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ICAS2022_0656: C. Wallace¹, S. Schulz¹, N. Fezans¹, T. Kier¹, G. Weber, Liebherr-Aerospace, Germany; ¹German Aerospace Center (DLR), Germany EVALUATION ENVIRONMENT FOR CASCADED AND PARTLY DECENTRALIZED MULTI-RATE LOAD ALLEVIATION CONTROLLERS |
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ICAS2022_0663: K. Bramsiepe¹, M. Braune¹, W. Krüger¹, L. Tichy¹; ¹DLR - Institute of Aeroelasticity, Germany WIND TUNNEL EXPERIMENT WITH AN EPP-WING TO INVESTIGATE AEROELASTIC EFFECTS OF NONLINEAR ELASTIC STIFFNESSES |
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ICAS2022_0694: T.R. De Paula¹, V.P. Fernandes¹, A.G.P. Sarmento¹, D.F.C. Zuñiga¹, A.G. Souza, Universidade de Lisboa, Portugal; R.G.A. Silva¹, L.C.S. Góes¹; ¹Aeronautics Institute of Technology, Brazil PARAMETER IDENTIFICATION BY UPDATING THE STRUCTURAL MODEL OF A UAV WITH FLEXIBLE WING |
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ICAS2022_0718: P. Vaghela¹, H. Raza¹, E. Stumpf, Institute for Aerospace Systems, RWTH Aachen University, Germany; J. Bayandor¹; ¹CRASH Lab, University at Buffalo - The State Univ. of New York, United States HIGH FIDELITY AIRWORTHINESS BIRD AND DRONE STRIKE ANALYSIS OF ON-DEMAND AIR MOBILITY SERVICE AIRCRAFT |
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ICAS2022_0734: H. Raza¹, C. Harey¹, P. Vaghela¹, J. Bayandor¹; ¹CRASH Lab, University at Buffalo, United States DEVELOPMENT OF A PREDICTIVE DAMAGE METHODOLOGY FOR HYBRID WING BODY AIRCRAFT STRUCTURES |
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ICAS2022_0802: A. Siami¹, F. Nitzsche¹; ¹Carleton University, Canada STRUCTURAL ANALYSIS OF TWISTED/CURVED BEAMS USING A HYBRID METHOD |
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ICAS2022_0826: P.J. González¹, G. Stavorinus¹, H. Shahi¹, Y.M. Meddaikar², S. Cumnuantip², A. Voß², T. Klimmek², W.R. Krüger², F.J. Silvestre¹; ¹TU-Berlin, Germany; ²DLR, Germany A PRELIMINARY STRUCTURAL DESIGN OF A FLEXIBLE FLYING DEMONSTRATOR |
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ICAS2022_0827: H.-G. Rho, Korea Aerospace Univeristy, South Korea; P.A. Nguyen¹, J.-S. Bae¹, S.-H. Park, Konkuk University, South Korea; K.-H. Byun, Korea Agency for Defense Development, South Korea; ¹Korea Aerospace University, Vietnam ANALYSIS OF THE HAMMERHEAD LAUNCH VEHICLE USING CFD-CAE COUPLED METHOD IN THE TRANSONIC REGION |
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ICAS2022_0861: A. De Gaspari¹, V. Cavalieri¹, S. Ricci¹; ¹Politecnico di Milano, Italy DESIGN AND EXPERIMENTAL TESTING OF A DROOP NOSE MORPHING FOR ADVANCED REGIONAL AIRCRAFT |
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ICAS2022_0967: M. Grundström¹, S. Ferrari¹; ¹Tampere University, Finland DESIGNING SUSTAINABLE AVIATION SOLUTIONS WITH DIGITAL TWIN APPROACH |
5 - Propulsion |
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ICAS2022_0006: C. Diette, Safran Aircraft Engines, France; E. Obert, Safran, France; G. Marion, Safran Transmission Systems, France; H. De Franssu, Safran Nacelles, France; A. Frezet, Avio Aero, Italy; B. Walther, GE Deutschland, Germany; A. Sjunnesson, GKN Aeropsace Engie Systems, Sweden TECHNOLOGY MATURATION IN CLEAN SKY 2 FOR NEXT GENERATION SMR ENGINE |
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ICAS2022_0019: S. Bhurat¹, S. Das¹, N.K. Shetty¹; ¹RV College of Engineering, India NUCLEAR POWERED AIR-BREATHING ELECTRIC THRUSTERS USED IN UAVS FOR EXTRA-TERRESTRIAL APPLICATIONS |
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ICAS2022_0023: Y. Shang, COMAC, China DESIGN OF AERO-ENGINE FADEC POWER SUPPLY CONTROL SYSTEM BASED ON FORWARD DESIGN |
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ICAS2022_0058: C. Polacsek¹, M. Buszyk¹, R. Barrier¹, V. Clair², E. Salze²; ¹ONERA, France; ²LMFA, France AEROACOUSTIC PERFORMANCES OF A LOW-NOISE AIRFOIL CASCADE WITH SERRATED LEADING EDGES: PREDICTIONS AND MEASUREMENTS |
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ICAS2022_0060: N.-X. Qiao¹, T.-L. Ma¹, X.-S. Wang¹, J.-C. Fu¹; ¹Beihang University, China DESIGN AND EFFICIENCY ANALYSIS OF EVTOL CONTRA-ROTATING PROPELER |
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ICAS2022_0088: D. Rosell, Saab Aeronautics, Sweden; T. Grönstedt, Chalmers Univerity of Technology, Sweden; P.D. Bravo-Mosquera¹, F. Martini Catalano¹; ¹University of Sao Paulo, Brazil LOW BPR TURBOFAN PERFORMANCE WITH POWER EXTRACTION |
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ICAS2022_0094: J. Juracka¹, M. Cervenka¹, M. Horak¹, M. Splichal¹; ¹Brno University of Technology, Czech Republic TREND MONITORING OF TURBOPROP ENGINES |
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ICAS2022_0120: J. Tegner, FOI, Sweden ANALYSIS OF THE OPERATION OF THE PULSEJET ENGINE |
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ICAS2022_0127: M. Migliorini¹, P.K. Zachos¹, D.G. MacManus¹, V. Monnier¹; ¹Cranfield University, United Kingdom A STUDY ON THE DEVELOPMENT OF THE FLOW DISTORTION DOWNSTREAM OF AN S-DUCT INTAKE |
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ICAS2022_0138: V.T. Silva¹, A. Venkatesh¹, M. Lejon ², A. Lundbladh², C. Xisto¹; ¹Chalmers University of Technology, Sweden; ²GKN Aerospace, Sweden MULTIPOINT AERODYNAMIC DESIGN OF A NACELLE FOR AN ELECTRIC FAN |
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ICAS2022_0152: G. Grimaldi, Politecnico di Torino, Italy DEVELOPMENT OF A CONCEPTUAL DESIGN TOOL TO PREDICT PERFORMANCE OF HYDROGEN FUELLED PRECOOLED AIRBREATHING ROCKET ENGINES |
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ICAS2022_0162: A. Swarthout¹, D. MacManus¹, F. Tejero¹, J. Matesanz-Garcia¹, L. Boscagli¹, C. Sheaf, Rolls Royce Plc., United Kingdom; ¹Cranfield University, United Kingdom A COMPARITIVE ASSESSMENT OF MULTI-OBJECTIVE OPTIMISATION METHODOLOGIES FOR AERO-ENGINE NACELLES |
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ICAS2022_0167: F. Sánchez-Moreno¹, D. MacManus¹, J. Hueso-Rebassa¹, F. Tejero¹, C. Sheaf, Rolls Royce, United Kingdom; ¹Cranfield University, United Kingdom OPTIMIZATION OF INSTALLED COMPACT AND ROBUST NACELLES USING SURROGATE MODELS |
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ICAS2022_0188: T. Nilsson¹, C. Fureby¹; ¹Lund University, Sweden LARGE EDDY SIMULATION OF RAMJET TO SCRAMJET TRANSITION |
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ICAS2022_0203: Z. Chunlei¹, C. Hao¹, L. Yi¹; ¹AECC, China NUMERICAL INVESTIGATION ON TURBINE SHROUD FILM COOLING HEAT TRANSFER PERFORMANCE OF TURBINE BLADE WITH GROOVE TIP |
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ICAS2022_0223: R. Wang¹, Q. Yang¹, S. Zhang¹, K. Du, Guiyang Aero-engine Research Institute, China; ¹Northwestern Polytechnical University, China NUMERICAL SIMULATION ANALYSIS OF INFRARED RADIATION AND ELECTROMAGNETIC SCATTERING CHARACTERISTICS OF DIFFERENT MIXERS |
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ICAS2022_0234: M. Bruno¹, R. Cambertoni¹, A. Pellegrino¹, P. Petrachi¹, C. Spampinato¹; ¹Polytechnic of Turin, Italy ANALYSIS AND SIZING OF GREEN PROPULSION SYSTEM FOR A SUBORBITAL AIRCRAFT |
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ICAS2022_0235: P. Roncioni¹, L. Cutrone¹, M. Marini¹; ¹CIRA, Italy AEROPROPULSIVE CHARACTERIZATION OF THE HYPERSONIC CRUISER VEHICLE IN STRATOFLY PROJECT |
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ICAS2022_0274: A. Åkerblom, Lund University, Sweden THE IMPACT OF REACTION MECHANISM COMPLEXITY IN LES MODELING OF LIQUID KEROSENE SPRAY COMBUSTION |
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ICAS2022_0313: J. Wang¹, D. Meng¹, D. Feng¹, Q. Zhao¹; ¹Shenyang Engine Research Institute of AECC, China STUDY ON THE OBJECTIVE FUNCTION OF THE PROFILED ENDWALL OPTIMIZATION OF AN EMBEDDED COMPRESSOR STATOR |
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ICAS2022_0339: M. Buszyk¹, L. Vienne², T. Le Garrec¹, J.-F. Boussuge², C. Polacsek¹, R. Barrier¹; ¹ONERA, France; ²CERFACS, France LATTICE BOLTZMANN METHOD FOR BROADBAND NOISE PREDICTIONS ON A TURBULENCE-CASCADE TEST RIG INCLUDING SERRATED VANES |
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ICAS2022_0366: S. de Graaf¹, S. Kazula¹; ¹DLR e.V., Germany DEVELOPMENT OF A CONTROLS APPROACH FOR FUEL CELL-POWERED ALL-ELECTRIC AERO ENGINES BASED ON AN FHA |
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ICAS2022_0370: G. Avanzini, University of Salento, Italy; G. Bernardini¹, S. Moretti¹, J. Serafini¹; ¹Roma Tre University, Italy SERIES-HYBRID RETROFIT OF AN XV-15 TILTROTOR AND EMERGENCY PROCEDURE ENERGETIC ANALYSIS |
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ICAS2022_0390: A.H.R. Lamkin¹, A. Yildirim¹, J.R.R.A. Martins¹; ¹University of Michigan, United States COUPLED AEROPROPULSIVE ANALYSIS AND OPTIMIZATION OF A HIGH BYPASS TURBOFAN ENGINE |
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ICAS2022_0409: F. Wang¹, T. Mizukaki¹; ¹Tokai University, Japan NUMERICAL ANALYSIS OF PROPAGATION OF DETONATION WAVE PLUNGING ENTRY THE FUEL JET TRAIN INSIDE ROTATING DETONATION COMBUSTOR |
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ICAS2022_0456: A. Link¹, J. Ludowicy¹, M. Staggat¹; ¹German Aerospace Center (DLR), Germany ASSESSMENT OF A SERIAL COOLING CONCEPT FOR HTPEM FUEL CELL SYSTEMS FOR AVIATION APPLICATIONS |
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ICAS2022_0480: R. Lundberg¹, L. Ellbrant¹, P. Johansson¹, U. Johansson¹, M. Billson¹, B. Gustafsson¹; ¹GKN Aerospace Sweden AB, Sweden STATUS OF GKN AEROSPACE\'S ENGINE MODULE DEMONSTRATORS IN THE CLEAN SKY-2 PROJECT |
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ICAS2022_0489: T. Sinnige¹, W. de Gruijl¹, W. de Haan¹, G. Eitelberg¹; ¹Delft University of Technology, Netherlands RAPID AEROACOUSTIC PLANFORM DESIGN OPTIMIZATION OF INSTALLED PROPELLERS |
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ICAS2022_0495: Z.-B. Zhang¹, Y.-H. Zhang¹, Y.-H. Chen¹; ¹Shenyang Engine Research Institute, China EXPERIMENTAL STUDY ON THE EFFECT OF INTERSTAGE BLEEDING ON THE PERFORMANCE OF FULL-SCALE MULTISTAGE AXIAL COMPRESSOR |
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ICAS2022_0497: J. Häßy¹, J. Schmeink¹; ¹DLR, Germany KNOWLEDGE-BASED CONCEPTUAL DESIGN METHODS FOR GEOMETRY AND MASS ESTIMATION OF RUBBER AERO ENGINES |
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ICAS2022_0499: A. Görtz, German Aerospace Center, Institute of Propulsion Technology, Germany; D. Silberhorn, German Aerospace Center, Institute of System Architectures in Ae, Germany THERMODYNAMIC POTENTIAL OF TURBOFAN ENGINES WITH DIRECT COMBUSTION OF HYDROGEN |
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ICAS2022_0502: Y. Chen¹, Z. Zhang¹, A. Wang¹; ¹AECC Shenyang Engine Institute, China EXPERIMENTAL STUDY OF FLAT BAFFLE INLET TOTAL-PRESSURE DISTORTION IN A THREE-STAGE FAN |
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ICAS2022_0507: A.-P. Chalke¹, N. Glodic¹, M. Gutierrez Salas¹; ¹KTH Royal Institute of Technology, Sweden AEROELASTIC TAILORING OF COMPRESSOR BLADES |
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ICAS2022_0510: B.-W. Yu¹, X. Yu¹, M.-G. Cao¹, X.-Z. Zhang¹, C.-L. Zhang¹, H.-B. Ji, Institute of Metal Research, Chinese Academy of Sciences, China; W.-T. Tong, Avic GuZhou YongHong Aviation Machinery Co, China; ¹Shenyang Aeroengine Research Institute, China RESEARCH ON FLOW HEAT TRANSFER CHARACTERISTICS OF HEAT EXCHANGER BASED ON BIONIC FRACTAL STRUCTURE |
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ICAS2022_0514: V. Vikhorev¹, V. Chernoray¹, A.M. Zuher², J. Larsson²; ¹Chalmers University of Technology, Sweden; ²GKN Aerospace Engine Systems, Sweden THE INFLUENCE OF THE VANE LEAN ON THE FLOW IN A TURBINE REAR STRUCTURE |
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ICAS2022_0566: P. Bohnert, United Kingdom; S.X. Ying, United States; M. Selier, Netherlands DEMONSTRATION FLIGHTS OF HYBRID ELECTRIC AIRCRAFT |
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ICAS2022_0603: F. Gao, Northwestern Polytechnical University, China; Z. Zhang¹, J. Li¹; ¹AECC Shenyang Engine Research Institute, China ANALYSIS OF THE AERODYNAMIC CHARACTERISTICS AND ITS INFLUENCE OF TURBOMACHINERY IN TRANSITION STATE |
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ICAS2022_0657: B.-O. Schröder¹, P.J. González¹, F.J. Silvestre¹; ¹TU Berlin, Germany TESTING AND MODELLING OF A DUCTED FAN MOTOR FOR UAV APPLICATIONS |
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ICAS2022_0666: B. Mangin¹, M. Daroukh¹, G. Gabard, LAUM, France; ¹ONERA, France STUDY OF THE IMPACT OF AZIMUTHAL FLOW DISTORTION ON IN-DUCT ACOUSTIC PROPAGATION USING A MULTIMODAL FORMULATION |
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ICAS2022_0751: A. Sato¹, R. Yasuda¹, M. Harada¹, S. Shibasaki¹, H. Moriai¹; ¹Kanazawa Institute of Technology, Japan STUDY ON THE APPLICATION OF EMULSIFIED FUEL IN SMALL JET ENGINES |
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ICAS2022_0756: M. Harada¹, N. Osawa¹, H. Moriai¹; ¹Kanazawa Institute of Technology, Japan EXPERIMENTAL STUDY ON THE LASER PLASMA JET PROPULSION - PLASMA JET GENERATION AND THRUST MEASUREMENT |
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ICAS2022_0782: M. Assato, IAE, Brazil; A. Altar Inceer¹, L. Moraes¹, J. Takachi Tomita², C. Bringhenti², P. Bravo-Mosquera, USP, Brazil; D. Rosell, SAAB Aeronautcs, Sweden; T. Grönstedt¹; ¹Chalmers University, Sweden; ²ITA, Brazil PERFORMANCE BENEFITS OF A FAN ON BLADE – FLADE – FOR A VARIABLE CYCLE ENGINE |
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ICAS2022_0786: N. Zettervall¹, K. Nordin-Bates¹, C. Ibron¹, C. Fureby, Lund University, Sweden; ¹FOI, Sweden LES OF COMBUSTION DYNAMICS IN AN ETHYLENE-HYDROGEN-AIR RAMJET |
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ICAS2022_0788: I. Jonsson¹, R. Ranman¹, A. Capitao¹, C. Xisto¹; ¹Chalmers Tekniska Hogskola AB, Sweden EFFECT OF HEAT EXCHANGER INTEGRATION IN AERODYNAMIC OPTIMISATION OF AN AGGRESSIVE S-DUCT |
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ICAS2022_0801: J. Kos¹, J. Posada-Duque², B. Peerlings¹, N. Ben Salah², N. Lim¹, W. Lammen¹, I. Stepchuk, TU Delft, Faculty of Technology and Policy Management, Netherlands; E. van der Sman¹, M. Palmeros-Parada²; ¹Royal Netherlands Aerospace Centre, Netherlands; ²TU Delft, Faculty of Applied Sciences, Netherlands NOVEL AIRCRAFT PROPULSION AND AVAILABILITY OF ALTERNATIVE, SUSTAINABLE AVIATION FUELS IN 2050 |
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ICAS2022_0813: C.-A. Pham¹, Q.-H. Nguyen¹, T.-A. Vu¹, N.-V. Nguyen¹; ¹Viettel Aerospace Institute, Viettel Group, Vietnam MULTIDISCIPLINARY OPTIMIZATION OF COMBUSTION CHAMBER FOR SMALL GAS TURBINE ENGINES |
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ICAS2022_0818: T.-G. Nguyen¹, Q.-H. Nghiem¹, Q.-H. Nguyen¹, N.-V. Nguyen¹, D.-L. Chu¹, P.-M. Nguyen¹; ¹Viettel Aerospace Institute, Vietnam DEVELOPMENT OF THE LOW-COST AND LIMITED SPACE SEA-LEVEL RAM AIR TEST (RAT) MACH 0.8 SYSTEM |
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ICAS2022_0830: H. Miki¹, J. Akatsuka¹, I. Kikura, Tokyo University of Agriculture and Technology, Japan; Y. Watanabe¹; ¹JAXA, Japan FEASIBILITY STUDY OF SHORT SUBSONIC DIFFUSER CONCEPT FOR SUPERSONIC INLET |
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ICAS2022_0832: T. Grönstedt¹, C. Xisto¹, X. Zhao¹, I. Jonsson¹, A. Reinap², M. Genrup², N. Glodic³, M. Guiterrez Salas³, M. Lejon*, R. Avellan*, H. Mårtensson*; ¹Chalmers University, Sweden; ²Lund University, Sweden; ³Royal Institute of Technology, Sweden; *GKN Aerospace, Sweden MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEM |
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ICAS2022_0845: G. Saccone¹, M. Marini¹; ¹Italian Aerospace Research Centre - CIRA, Italy HIGH PRESSURE HYDROGEN OXYGEN COMBUSTION KINETIC ASSESSMENT FOR AIR-BREATHING PROPULSION SUPERSONIC GREEN AVIATION |
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ICAS2022_0847: J.-Z. Fan¹, Q.-Z. Yang¹, X.-B. Du¹, H.-Q. Yang¹, Y.-B. He¹, Y.-Q. Shi¹; ¹Northwestern Polytechnical University, China EFFECT OF TAILCONE SHAPE ON HOT STREAK PHENOMENA AND INFRARED SIGNATURE OF SERPENTINE NOZZLE WITH AFT DECK |
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ICAS2022_0855: F. Petrosino¹, M. Barbarino¹; ¹CIRA, Italy COMPARISON OF ANALYTICAL SEMI-EMPIRICAL MODEL FOR JET NOISE PREDICTION |
6.1 - Flight Dynamics and Control (Control & Modelling) |
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ICAS2022_0080: O. Luderer¹, F. Thielecke¹; ¹Hamburg University of Technology, Germany VALIDATION OF A HYBRID LOADS OBSERVER FOR A SUBSCALE TEST AIRCRAFT WITH DISTRIBUTED ELECTRIC PROPULSION |
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ICAS2022_0110: H.S. Luu¹, Y. Ochi¹; ¹National Defense Academy, Japan ESTIMATION OF STEPWISE VARYING WIND BASED ON DERIVATIVE ESTIMATION OF AIRCRAFT USING SLIDING WINDOW RECURSIVE LEAST SQUARES METHOD |
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ICAS2022_0135: T. Takamatsu¹, Y. Ochi¹; ¹National Defense Academy, Japan FLIGHT TESTS AND SIMULATION OF A HANG GLIDER |
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ICAS2022_0174: D. Planas, ONERA & ISAE SUPAERO, France; C. Döll, ONERA, France; P. Pastor, ISAE SUPAERO, France HANDLING QUALITIES OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT |
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ICAS2022_0273: D.B. Rossato, Faculdade de Tecnologia SENAI , Brazil; K.H. Kienitz, Instituto Tecnológico de Aeronáutica, Brazil FLIGHT CONTROLLABILITY ANALYSIS IN TIGHT FORMATION AND CRUISE FLIGHT FOR FUEL SAVING |
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ICAS2022_0275: P. Piprek¹, P.M. Dias¹, D. Schwalb¹; ¹Airbus Defence and Space GmbH, Germany A GENERALISED MULTI-OBJECTIVE ISLAND MODEL FOR FLIGHT CONTROL SYSTEM CLEARANCES |
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ICAS2022_0291: D.S. Alarcon¹, J.H. Bidinotto¹; ¹University of São Paulo, Brazil DEEP REINFORCEMENT LEARNING FOR EVTOL HOVERING CONTROL |
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ICAS2022_0346: L. Kim¹, D. Lee¹, H. Bang¹; ¹Korea Advanced Institute of Science and Technology, South Korea INCREMENTAL NONLINEAR DYNAMIC CONTROL WITH SPARSE NON-PARAMETRIC BAYESIAN REGRESSION OF DAMAGED AIRCRAFT |
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ICAS2022_0348: L. Yao¹, H. Yu¹, Z. Zhao¹, J. Zheng¹; ¹Shenyang Aircraft Design and Research Institute, China RESEARCH ON SERVO CONTROL METHOD AND DAMPING CHARACTERISTICS OF ACTIVE CONTROL DEVICE |
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ICAS2022_0395: A. Kwiek¹, M. Figat¹, T. Goetzendorf-Grabowski ¹; ¹Warsaw University of Technology, Poland PRELIMINARY STUDY ON A DESIGN OF A RETURN FLIGHT TRAJECTORY OF A SUBORBITAL VEHICLE |
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ICAS2022_0423: J.-F. Wang¹, S.-G. Lu¹, S. Feng¹, M.-H. Wang¹; ¹AVIC Aerodynamics Research Institute, China FREE FLIGHT TEST IN HORIZONTAL WIND TUNNEL WITH POWERED AIRCRAFT |
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ICAS2022_0430: M. Naruoka¹, T. Ninomiya¹; ¹Japan Aerospace Exploration Agency, Japan STATISTICAL DATA SELECTION FOR BETTER FLIGHT CHARACTERISTIC MODELING |
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ICAS2022_0438: D.-W. Lee¹, L.-S. Kim¹, H.-C. Bang¹; ¹KAIST, South Korea FAULT-TOLERANT CONTROL FOR AIRCRAFT WITH STRUCTURAL DAMAGE USING GAUSSIAN PROCESS REGRESSION |
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ICAS2022_0439: D. Niedermeier¹, K. Giese¹, D. Leißling¹; ¹DLR, Germany THE NEW RESEARCH AIRCRAFT ISTAR - EXPERIMENTAL FLIGHT CONTROL SYSTEM |
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ICAS2022_0441: R. Larsson¹, U. Ringertz, Royal Institute of Technology, KTH, Sweden; D. Lundström, Linköping University, LIU, Sweden; A. Sobron¹; ¹Saab Aeronautics, Sweden RAPID PROTOTYPING IN AIRCRAFT DESIGN USING CFD, WIND TUNNEL AND FLIGHT TESTING |
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ICAS2022_0458: E. Johansson¹, P. Månsson¹, P. Sjöberg¹; ¹Saab Aeronautics, Sweden FLIGHT DYNAMICS SIMULATION AND FCS AUTO-GENERATION IN THE CONCEPTUAL DESIGN PHASE OF AN UNSTABLE SUPERSONIC AIRCRAFT |
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ICAS2022_0488: H.J. Jeaong¹, C. Roh¹, Y.H. Jang¹, J.Y Suk¹, S.K. Kim¹; ¹Department of Aerospace Engineering, Chungnam National Universit, South Korea EFFECTIVENESS ANALYSIS OF DOBC Q-FILTER PARAMETERS FOR A MULTICOPTER UAV |
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ICAS2022_0490: T.J. Ludena Cervantes, Peru; Y. Kim, South Korea; B.S. Kim, South Korea NEURAL-NETWORK ADAPTIVE DECENTRALIZED FORMATION CONTROL |
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ICAS2022_0536: V.L.M. Veras, EMBRAER, Brazil; L.C.S. Góes, ITA, Brazil SYNTHETIC AIR DATA - A COMPARATIVE PRACTICAL STUDY |
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ICAS2022_0538: H.J. Lee¹, S.H. Hahn¹, S.C. Lee¹; ¹Korea Aerospace University, South Korea GENERATION OF TERRAIN PROFILE FOR TERRAIN FOLLOWING |
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ICAS2022_0568: J. Mabboux¹, S. Delbecq¹, V. Pommier-Budinger¹, J. Bordeneuve-Guibe¹, A. Truc-Hermel², J.-M. Kai²; ¹ISAE Supaero, France; ²SAFRAN, France A BI-LEVEL CO-DESIGN APPROACH FOR MULTICOPTERS |
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ICAS2022_0623: R.L. Pereira, ITA, Brazil; P.J. González¹, F.J. Silvestre¹; ¹TU Berlin, Germany DESIGN OF STABILITY AUGMENTATION SYSTEMS FOR A FLEXIBLE AIRCRAFT USING LQ OUTPUT-FEEDBACK CONTROL VIA LMI |
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ICAS2022_0671: E.M. Thoma¹, T. Grönstedt¹, E. Otero Sola, KTH, Royal Institute of Technology, Sweden; X. Zhao¹; ¹Chalmers University of Technology, Sweden ENVIRONMENTAL ASSESSMENT OF NOISE ABATEMENT APPROACH TRAJECTORIES |
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ICAS2022_0719: J. Vlk¹, P. Chudy¹, M. Prustomersky¹; ¹Brno University of Technology, Czech Republic LQR BASED DIGITAL AUTOPILOT FOR LIGHT SPORT AIRCRAFT |
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ICAS2022_0733: L.M.B.C. Campos, Instituto Superior Técnico, Universidade de Lisboa, Portugal; J.M.G. Marques, Universidade de Évora, Portugal ON LATERAL-LONGITUDINAL CONTROL COUPLING FOR SHORT- AND LONG-FUSELAGE BWB AIRCRAFT CONFIGURATIONS |
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ICAS2022_0785: J.-F. Wang, China; H. Tan, China; H. Chen, China; S. Feng, China; M.-H. Wang, China DESIGN OF A TYPICAL MANEUVERING PROCESS SIMULATION TEST CONTROL SYSTEM WITH CONTROLLABLE RUDDER SURFACE |
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ICAS2022_0810: C.-G. Jung¹, C.-H. Lee¹, M.-J. Tahk¹; ¹KAIST, South Korea CONVEX PROGRAMMING-BASED OPTIMAL THREE-DIMENSIONAL MID-COURSE GUIDANCE WITH LOSSLESS CONVEXIFICATION |
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ICAS2022_0816: R.L. Pereira, ITA, Brazil; P.J. González¹, F.J. Silvestre¹; ¹TU Berlin, Germany LPV/LFR CONTROL FOR ACTIVE FLUTTER SUPPRESSION OF A SMART AIRFOIL MODEL |
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ICAS2022_0835: S. Scherer¹, M. Speckmaier¹, D. Gierszewski¹, C. Mishra¹, A. Steinert¹, R. Steffensen¹, S. Wulf¹, F. Holzapfel¹; ¹Technical University of Munich,, Germany AUTOMATIC TAKE-OFF AND LANDING OF A VERY LIGHT ALL ELECTRIC OPTIONALLY PILOTED AIRCRAFT |
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ICAS2022_0841: S. Scherer¹, C. Mishra¹, F. Holzapfel¹; ¹Technical University of Munich, Germany EXTENSION OF THE CAPABILITIES OF AN AUTOMATIC LANDING SYSTEM WITH PROCEDURES MOTIVATED BY VISUAL-FLIGHT-RULES |
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ICAS2022_0870: V.T. Sant'Ana¹, I. Staack, Linköping University, Sweden; R.M. Finzi Neto¹; ¹Federal University of Uberlândia, Brazil LATERAL-DIRECTIONAL AERODYNAMIC MODELLING FOR NUMERICAL RESULTS USING NEURO-FUZZY WITH DIFFERENTIAL EVOLUTION |
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ICAS2022_0873: C. Fischer, ITA and IFSP, Brazil; L.M. Nepomuceno¹, E.A. Moura¹, R.G.A. da Silva¹, L.C.S. Góes¹; ¹ITA, Brazil IDENTIFICATION OF THE COMPLETE AERODYNAMIC MODEL OF A SUBSCALE FLIGHT TESTING |
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ICAS2022_0879: S.-H. Kim¹, Y. Jung¹, Y. Kim¹; ¹Seoul National University, South Korea META-REINFORCEMENT LEARNING-BASED FAULT TOLERANT CONTROL FOR A QUADROTOR WITH A SEVERE LOSS OF ROTOR |
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ICAS2022_0891: R.C. Machado, Instituto de Fomento e Coordenação Industrial (IFI), Brazil; D.F.C. Zúniga, 2Universidade Estadual Paulista Júlio de Mesquita Filho, Brazil; A. Souza, Instituto Superior Técnico de Lisboa, Portugal; T. Rosado¹, L.C.S. Góes¹; ¹Instituto Tecnológico de Aeronáutica, Brazil OPEN-LOOP SUBSPACE IDENTIFICATION OF A FLEXIBLE UNMANNED AERIAL SYSTEM |
6.2 - Flight Dynamics and Control (UAV related) |
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ICAS2022_0049: B. Zhang¹, W. Li, The Second Representative Office of Air Force Armament Departmen, China; Z. Miao¹, Y. Zhang, Beijing System Design Institute of Mechanical-Electrical Enginee, China; ¹Northwestern Polytechnical University, China THREE DIMENSIONAL PATH FOLLOWING CONTROL FOR A FIXED-WING UAV ON SO(3) WITH INPUT SATURATION |
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ICAS2022_0065: R. Wang¹, Z. Zhou¹, X. Zhu¹, L. Zheng, Delft University of Technology, Netherlands; ¹Northwestern Polytechnical University, China USING DEEP REINFORCEMENT LEARNING TO IMPROVE THE ROBUSTNESS OF UAV LATERAL-DIRECTIONAL CONTROL |
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ICAS2022_0085: L. Scagnellato¹, M. Lecce¹, N. Bloise¹, M. Carreño Ruiz¹, E. Capello¹, G. Guglieri¹; ¹Politecnico di Torino, Italy ADAPTIVE PATH PLANNING FOR SPRAYING UAS IN VINEYARD UNDER VARIABLE WIND CONDITION |
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ICAS2022_0108: S.-G. Lee¹, H.-H. Yang¹, Y.-J. Han¹, J.-H. Han¹; ¹Korea Advanced Institute of Science and Technology, South Korea DESIGN OF AN EFFICIENT CLIMBING FLIGHT TRAJECTORY FOR A FLAPPING-WING MICRO AIR VEHICLE |
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ICAS2022_0109: H.-H. Yang¹, S.-G. Lee¹, Y.-J. Han¹, J.-H. Han¹; ¹Korea Advanced Institute of Science and Technology, South Korea OPTIMAL HOVERING WING KINEMATICS OF FLAPPING-WING MODEL USING REINFORCEMENT LEARNING |
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ICAS2022_0141: T.G. Kim¹, Y.J. Kim¹, S.K. Kim¹; ¹Chungnam National University, South Korea PREFLIGHT DIAGNOSIS OF MULTICOPTER ACTUATOR FAULT USING SUPERVISED LEARNING WITH DISTURBANCE OBSERVER OUTPUTS |
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ICAS2022_0222: S. Ahn¹, H. Choi¹, S. Kim¹, J. Kim¹, H. Ryu¹; ¹Korea Aerospace Research Institute, South Korea A PREPARATORY RESEARCH FOR UAM COLLISION AVOIDACE USING ADSB |
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ICAS2022_0326: Y. Lemmens¹, C. Teirlink¹, A. Hegde¹, D. Pla Guerrero¹, G. Olivares², H. Shah²; ¹Siemens Digital Industries Software, Belgium; ²National Institute for Aviation Research, United States INVESTIGATION OF SIMULATION FRAMEWORKS FOR THE EVALUATION OF AUTOMATED FLIGHT FUNCTIONS FOR EVTOL AIRCRAFT |
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ICAS2022_0364: Y.J. Hasan¹, N. Fezans¹, A. Voß, DLR, Institute of Aeroelasticity, Germany; ¹DLR, Institute of Flight Systems, Germany LANDING SIMULATION OF A HIGH-ALTITUDE PLATFORM WITH SKID-TYPE LANDING GEAR – FLIGHT PROCEDURE, CONTROLLER, AND LOADS |
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ICAS2022_0389: L.D. Jesus¹, A.J.D. Filho¹, M.A. Almeida¹, W. M. Martins¹, T.C. Pimenta¹, A.C.B. Ramos¹, L. A. Baldochi¹, L.O. Carvalho¹, P. Funk, Mälardalen University, Sweden; ¹Federal University of Itajubá, Brazil USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTION |
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ICAS2022_0406: W. Yuan¹, A. Wall¹, X. Zhang², D. Poirel²; ¹National Research Council (NRC) Canada, Canada; ²Royal Military College of Canada (RMC),, Canada NUMERICAL MODELLING OF PITCHING WINGS FOR GUST MITIGATION |
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ICAS2022_0420: Y.J. Kim¹, T.G. Kim¹, S.K. Kim¹; ¹Chungnam National University, South Korea FAULT DIAGNOSIS FOR SENSOR AND ACTUATOR OF HEXACOPTER UAV USING DUAL EXTENDED KALMAN FILTER |
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ICAS2022_0428: K.K. Deveerasetty¹, K. Oka¹, A. Harada¹; ¹Kochi University of Technology, Japan CONTROL AUGMENTATION SYSTEM DESIGN FOR THE QUAD TILT-WING UAV VIA H-INFINITY STRUCTURE WITH GWO |
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ICAS2022_0448: N. Morita¹, S. Nakasuka¹, T. Tsuchiya¹, K. Takashima¹, Y. Taguchi¹, K. Suzuki¹, T. Koyama¹, R. Eto¹, I. Baba¹; ¹the University of Tokyo, Japan DEVELOPMENT OF MULTI-CANARD UAV FOR ACTIVE AEROELASTIC CONTROL TOWARD PSEUDO-SMALL SATELLITES |
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ICAS2022_0476: H. Hiraiwa¹, M. Bando¹, S. Hokamoto¹; ¹Kyushu university, Japan ALTITUDE ESTIMATION BY WIDE-FIELD-INTEGRATION OF OPTIC FLOW |
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ICAS2022_0520: M.R. Kartal¹, D. Ignatyev¹, A. Zolotas¹; ¹Cranfield University, United Kingdom FIXED-WING UAVS CONTROL WITH MODEL UNCERTAINTIES |
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ICAS2022_0539: H.J. Ahn¹, C.S. Lim¹, D.W. Lee¹, H.C. Bang¹; ¹Korea Advanced Institute of Science and Technology(KAIST), South Korea SAFE REINFORCEMENT LEARNING BASED MULTI-ROTOR COLLISION AVOIDANCE WITH UNEXPECTED OBSTACLES |
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ICAS2022_0576: T. Goetzendorf-Grabowski¹, D. Kacik¹, K. Pobikrowska, Lukasiewicz Research Network – Institute of Aviation, Poland; J. Mieloszyk¹; ¹Warsaw University of Technology, Poland OPTIMIZATION OF ENERGY CONSUMPTION IN THE TRANSITION STATE OF A QUAD-PLANE |
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ICAS2022_0717: J. Novák ¹, P. Chudý¹; ¹Brno University of Technology, Czech Republic UNMANNED AERIAL VEHICLE\\\'S TRAJECTORY OPTIMIZATION IN CONSTRAINED ENVIRONMENTS |
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ICAS2022_0740: K. Muraoka¹, M. Sato¹; ¹Japan Aerospace Exploration Agency, Japan FLIGHT VERIFICATION OF AUTOMATIC TRANSITION FOR QUAD TILT WING SMALL UAV |
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ICAS2022_0781: Y. Lu¹, Q. Chen¹, Y. Wang¹; ¹National University of Defense technology, China COOPERATIVE PATH PLANNING AND ADJUSTING STRATEGY FOR UAVS WITH STRICT TIME CONSTRAINS |
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ICAS2022_0796: Y. Huang¹, M. Bando¹, S. Hokamoto¹; ¹Kyushu University, Japan INFLUENCE OF OVERALL LAYOUT DESIGN OF COMPOUND MULTI-ROTOR VEHICLES ON FLIGHT PERFORMANCE |
7 - Systems, Subsystems and Equipment |
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ICAS2022_0003: I. Berlowitz, IBAero Engineering, Israel ELECTRICALLY POWERED LANDING GEAR SYSTEM FOR TRANSPORT AIRCRAFT TAXIING |
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ICAS2022_0017: R.K. Rangel¹, V.A. Rodrigues¹, A.L. Maitelli¹, T.M. de Souza¹; ¹IBRV - Institute of Research & Development, Brazil HYDRO ENVIRONMENTAL AND ELECTRICAL ASSETS MAPPING TOOL USING SWARMS AND MACHINE LEARNING, UAV & USV |
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ICAS2022_0048: P. Khanal, Chalmers University of Technology, Sweden; P. Hallander¹, R. Luo¹; ¹Saab AB, Sweden SMART SKIN FOR AEW AIRCRAFT |
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ICAS2022_0072: X. Pang¹, H. Sui¹, X. Jiang¹, G. Liu¹; ¹AECC, China STUDY ON OIL-GAS TWO-PHASE FLOW CHARACTERISTICS IN AIR-OIL HEAT EXCHANGER |
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ICAS2022_0113: S. Oberschwendtner¹, M. Hornung¹; ¹Technical University of Munich, Germany THE INFLUENCE OF THE MODEL PARAMETERS OF LI-ION BATTERIES ON THE WIRING HARNESS PERFORMANCE OF EVTOL AIRCRAFT |
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ICAS2022_0115: B. Müller¹, A. Lindner¹, V. Norrefeldt¹, Y. Song, TU Delft, Netherlands; N. Mansfield, Nottingham Trent University, United Kingdom; P. Vink, vhp Human Performance, Netherlands; ¹Fraunhofer IBP, Germany MEASUREMENT OF NOISE AND INDOOR CLIMATE ON BOARD A TURBOPROP AIRPLANE FLIGHT |
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ICAS2022_0116: V. Norrefeldt¹, F. Mayer¹, A. Pathak¹, M. Pschirer¹, M. Kienberger¹, A. Lindner¹, S. Johann¹, A. Nagele-Renzl¹, M. Buschhaus¹, G. Grün¹; ¹Fraunhofer IBP, Germany USE OF THE FLIGHT TEST FACILITY MOCK-UPS IN THE EUROPEAN CLEAN SKY 2 PROGRAM |
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ICAS2022_0130: K. Szilder¹, P. Forsyth¹; ¹National Research Council, Canada NUMERICAL SIMULATION OF ICE ACCRETION ON A PITOT TUBE |
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ICAS2022_0151: G. Gastaldo¹, V. Palanque, ISAE-Supaero and ONERA, France; M. Budinger, INSA/ICA, France; V. Pommier-Budinger¹; ¹ISAE-Supaero, France STRESS AND ENERGY RELEASE RATE INFLUENCE ON ICE SHEDDING WITH RESONANT ELECTROMECHANICAL DE-ICING SYSTEMS |
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ICAS2022_0159: A. Pathak¹, M. Pschirer¹, M. Kienberger¹, V. Norrefeldt¹; ¹Fraunhofer IBP, Germany ZONAL MODEL VALIDATION FOR AN ENVIRONMENTALLY FRIENDLY AIRCRAFT CARGO FIRE PROTECTION SYSTEM WITH CONTAINERIZED LOAD |
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ICAS2022_0224: A. Broatch¹, J. García-Tíscar¹, A. Felgueroso¹, M. Gelain², A. Couilleaux²; ¹Universitat Politecnica de Valencia, Spain; ²Safran Aircraft Engines, France NON-INTRUSIVE AEROTHERMAL CHARACTERIZATION OF SURFACE HEAT EXCHANGERS FOR TURBOFAN AEROENGINES |
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ICAS2022_0245: D. Åkerman¹, O. Fästh, ST Airborne Solutions, Sweden; M. Persson, Unibap, Sweden; D. Sabel¹, D. Åsvärn¹; ¹Spacemetric, Sweden INNOONBOARD FOR IMPROVED IMAGE HANDLING IN AIRBORNE COASTAL RECONNAISSANCE – A PROJECT PRESENTATION |
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ICAS2022_0254: J.-N. Walther¹, C. Hesse¹, J. Biedermann¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany EXTENSIBLE AIRCRAFT FUSELAGE MODEL GENERATION FOR A MULTIDISCIPLINARY, MULTI-FIDELITY CONTEXT |
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ICAS2022_0327: C. Cabaleiro¹, M. Fioriti, Politecnico di Torino, Italy; L. Boggero¹; ¹German Aerospace Center (DLR), Germany METHODOLOGY FOR THE AUTOMATED PRELIMINARY CERTIFICATION OF ON-BOARD SYSTEMS ARCHITECTURES THROUGH REQUIREMENTS ANALYSIS |
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ICAS2022_0354: R. Lopez Pereira, Safran Engineering Services GmbH, Germany; L. Rammos, Skyflox Sarl, Luxembourg CERTIFICATION ASPECTS OF AN EARTH OBSERVATION PAYLOAD INSTALLED ON COMMERCIAL TRANSPORT AIRCRAFT |
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ICAS2022_0368: A. Joksimovic¹, X. Carbonneau¹, F. Brazier, Delft University of Technology, Netherlands; R. Vingerhoeds¹; ¹ISAE-SUPAERO, France ENERGY-BASED SYSTEM ARCHITECTURE DESIGN - ENVIRONMENTAL CONTROL SYSTEM |
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ICAS2022_0382: A. Reinap¹, M. Genrup¹, R. Avellán², H. Mårtensson²; ¹Lund University, Sweden; ²GKN Aerospace, Sweden ANALYSIS AND DEVELOPMENT OF INTEGRATED LOW-PRESSURE SHAFT GENERATOR |
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ICAS2022_0485: D. Sabel¹, A. Maki¹, T. Westin², D. Åsvärn²; ¹KTH Royal Institute of Technology, Sweden; ²Spacemetric AB, Sweden VISION-BASED LOCALISATION FOR AUTONOMOUS AERIAL NAVIGATION IN GNSS-DENIED SITUATIONS |
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ICAS2022_0513: R. Simões Lopes Junior¹, D. Oliveira e Silva¹, M.P. Nostrani¹, A. Dell´Amico, Saab AB, Sweden; P. Krus, Linköping University, Sweden; V.J. De Negri¹; ¹Federal University of Santa Catarina, Brazil A COMPARATIVE ANALYSIS OF INNOVATIVE DIGITAL HYDRAULIC ACTUATORS FOR PRIMARY FLIGHT CONTROL |
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ICAS2022_0537: X. Guo¹, Q. Yang¹, H. Zheng¹, W. Dong¹; ¹Shanghai Jiaotong University, China EFFECTS OF ANISOTROPIC THERMAL CONDUCTIVITY OF COMPOSITE SHIELD ON THE ELECTROTHERMAL ANTI-ICING SYSTEMS |
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ICAS2022_0575: F. Larsson¹, C. Reichenwallner², A. Dell'Amico¹, P. Krus²; ¹Saab AB, Sweden; ²Linköping University, Sweden MODEL-BASED PERFORMANCE EVALUATION OF AIRCRAFT ACTUATOR TECHNOLOGIES |
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ICAS2022_0601: C. Reichenwallner, Linköping university, Sweden; F. Larsson¹, A. Dell'Amico¹; ¹Saab AB, Sweden AN EVALUATION METHOD FOR AIRCRAFT ACTUATION SYSTEMS OPERATIONAL COST |
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ICAS2022_0677: L.Z. Lima¹, M.N. Duval¹, T. Zantner¹, D. Metzler¹, T. Lammering¹, F. Thielecke², N. Trochelmann², P.S. Bischof²; ¹Liebherr-Aerospace Lindenberg GmbH, Germany; ²Hamburg University of Technology, Germany DEVELOPMENT OF A HIGH EFFICIENT HYDRAULIC POWER PACK |
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ICAS2022_0730: S. Nambiar¹, D. Ferreto¹; ¹Politecnico di Torino, Italy MATHEMATICAL MODELLING AND ANALYSIS OF THERMAL MANAGEMENT SYSTEM ARCHITECTURE FOR HYPERSONIC AIRCRAFT |
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ICAS2022_0742: K. Borodacz¹, C. Szczepanski¹; ¹Lukasiewicz Research Network - Institute of Aviation, Poland IMPACT OF MOTION-DEPENDENT ERRORS ON THE ACCURACY OF AN UNAIDED STRAPDOWN INERTIAL NAVIGATION SYSTEM |
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ICAS2022_0753: G. Kong, China; P. Cui, China; W. Du, China; R. Chen, China DESIGN OF ELECTRONICALLY PHASE-TUNING REFLECTARRAY ANTENNA FOR AIRBORNE RADAR APPLICATION |
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ICAS2022_0794: C.W. Schwarz, DLR, Germany THE SENS4ICE EU PROJECT – SENSORS AND CERTIFIABLE HYBRID ARCHITECTURES FOR SAFER AVIATION IN ICING ENVIRONMENT – PROJECT OVERVIEW AND INITIAL RESULTS |
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ICAS2022_0795: H. Li, China; Z. Zhao, China; Z. Wan, China; L. Xu, China; S. Zhao, China; P. Sun, China AN INTEGRATED CONTROL SCHEME FOR STARTER/GENERATOR SYSTEM IN MORE ELECTRIC AIRCRAFT |
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ICAS2022_0856: A. Drego¹, S. Steinkellner¹; ¹Saab AB, Sweden A SYSTEM INTEGRATOR’S PERSPECTIVE ON VEHICLE SYSTEM EVALUATION AT THE AIRCRAFT CONCEPT STAGE |
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ICAS2022_0877: A. Hatamoto¹, K. Emori¹, H. Nishida¹; ¹Tokyo University of Agriculture and Technology, Japan EXPERIMENTAL ANALYSIS OF HEAT TRANSFER CHARACTERISTICS OF DIELECTRIC BARRIER DISCHARGE PLASMA ACTUATOR |
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ICAS2022_0911: C.L.S. Raposo¹, J.M.M. Sousa¹; ¹IDMEC, Instituto Superior Técnico, Portugal COMPUTATIONAL STUDY OF AIRFLOW AND DISPERSION OF AIRBORNE PATHOGENS INSIDE AN AIRCRAFT CABIN |
8 - Manufacturing and Supply Chain Management |
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ICAS2022_0026: J. Shipley¹, A. Magnusson¹, C. Beamer, Quintus Technologyes LLC, United States; ¹Quintus Technologies AB, Sweden LATEST DEVELOPMENTS IN HIGH PRESSURE HEAT TREATMENT OF AEROSPACE COMPONENTS |
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ICAS2022_0053: J. Steffen, HAW Hamburg, Germany VIKA - CONCEPT OF A DIGITAL PLATFORM FOR IMPLICIT KNOWLEDGE AND VIRTUAL ASSISTANCE FOR ADDITIVE MANUFACTURED PARTS |
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ICAS2022_0176: C. Diao¹, E. Eimer¹, S. Mancini, Thales Alenia Space, Italy; S. Krishnaswamy¹, F. Schwarz¹, E. Pagone¹, J. Ding¹, S. Williams¹, Z. Pinter², F. Martina²; ¹Cranfield University, United Kingdom; ²WAAM3D, United Kingdom MANUFACTURE OF LARGE-SCALE SPACE EXPLORATION COMPONENTS USING WIRE + ARC ADDITIVE MANUFACTURING |
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ICAS2022_0314: F. Guo¹, C. Song¹, X. Zhang², Q. Xiao²; ¹University of Science and Technology Beijing, China; ²AVIC Manufacturing Technology Institute, China MOTION STROKE DESIGN ON FLEXIBLE ASSEMBLY TOOLING FOR MULTIPLE AIRCRAFT COMPONENTS |
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ICAS2022_0321: L. Chen¹, X. Li¹, Z. Zhang¹, W. Huang¹, R. Wu¹, Y. Li¹; ¹AVIC Chengdu Aircraft Industrial (Group) Co., Ltd., China DOMAIN MODEL CONSTRUCTION METHOD OF AVIATION EQUIPMENT MANUFACTURING OPERATION MANAGEMENT |
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ICAS2022_0336: L. Loiodice¹, S. Grendene¹, T. Binetti¹, I. Boni ¹, F. Lovero ¹, R. Piani¹; ¹Politecnico di Torino, Italy STUDY OF THE COST EFFICIENCY AND LAMINATE QUALITY USING DIFFERENT MOULD-MAKING TECHNOLOGIES |
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ICAS2022_0534: B. Peukert¹, J. Vesterberg¹, J. Birberg, Saab AB , Sweden; ¹KTH, Sweden REAL-TIME IDENTIFICATION OF USER ACTIONS IN COMPUTER-AIDED MANUFACTURING USING MACHINE LEARNING AND COMPUTER VISION |
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ICAS2022_0618: G. Donelli¹, J.M.G.D. Mello², F.I.K. Odaguil², T. Lefebvre³, N. Bartoli³, T. van der Laan, GKN Fokker, Netherlands; L. Boggero¹, B. Nagel¹; ¹DLR, Germany; ²Embraer, Brazil; ³ONERA, France A VALUE-DRIVEN QUANTITATIVE FRAMEWORK COUPLING AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN BY LEVERAGING THE AGILE 4.0 MBSE-MDO FRAMEWORK |
9 - Air Transport System Efficiency |
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ICAS2022_0022: A.H.O. Carvalho, Pontifícia Universidade Católica de Minas Gerais – PUC Minas, Brazil; E.M.M. Torga, Centro Universitário UNA, Brazil; F.R.V. Paiva, Universidade FUMEC - Fundação Mineira de Educação e Cultura, Brazil COMPETITIVITY, STRATEGY AND VALUE ON AIRPORTS A METHOD OF DIAGNOSIS, SUGGESTIONS AND ACTIONS FOR INTERNATIONAL AIRPORTS WITH A CASE STUDY OF CNF |
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ICAS2022_0054: D. Vechtel¹, P. Pauly¹; ¹German Aerospace Center (DLR), Germany ASSESSMENT OF ENERGY-EFFICIENT APPROACHES WITH INCREASED GLIDESLOPE ANGLES |
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ICAS2022_0087: G. Enea, MIT Lincoln Laboratory, United States; J. Bronsvoort, Airservices Australia, Australia TRAJECTORY-BASED OPERATIONS TO IMPROVE LONG-RANGE AIR TRAFFIC FLOW MANAGEMENT |
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ICAS2022_0105: R. Mori, ENRI, Japan AIRCRAFT MASS ESTIMATION USING CRUISE FLIGHT PROFILE |
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ICAS2022_0106: E. Itoh, The University of Tokyo/ENRI, Japan; D. Iwata, The University of Tokyo, Japan; M. Schultz, Bundeswehr University Munich, Germany DEVELOPING A DEPARTURE QUEUE MODEL FOR INTEGRATED ARRIVAL AND DEPARTURE OPERATION OF RUNWAYS |
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ICAS2022_0122: M. Jameel, DLR, Germany DEMAND PATTERN INFLUENCE ON RELATION OF TURNAROUND DURATION AND GATE OCCUPATION DEPENDING ON AVAILABLE RESOURCES |
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ICAS2022_0132: K. Higasa, The University of Tokyo, Japan; E. Itoh, Electronic Navigation Research Institute, Japan ASSESSMENT AND CONTROL OF ARRIVAL FLOW AND WAITING TIME APPLYING GT/GI/ST+GI TIME-VARYING QUEUING MODEL |
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ICAS2022_0168: A. Hillebrecht¹, T. Marks¹, V. Gollnick, Hamburg University of Technology, Germany; ¹German Aerospace Center, Air Transportation Systems, Germany ASSESSMENT OF REAL-TIME DATA TRANSMISSION VIA AD-HOC COMMUNICATION NETWORKS IN THE NORTH ATLANTIC OCEANIC AIRSPACE |
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ICAS2022_0213: L. Nöhren¹, M. Schaper¹, L. Tyburzy¹, K. Muth¹; ¹German Aerospace Center (DLR), Germany REAL-TIME CALCULATION AND ADAPTION OF CONFLICT-FREE AIRCRAFT GROUND TRAJECTORIES |
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ICAS2022_0233: T. Ehlers¹, S. Hagemann², V. Gollnick², K. Lütjens¹; ¹German Aerospace Center, Germany; ²Hamburg University of Technology, Germany ON KEY PARAMETERS FOR THE ATTRACTIVENESS OF ON-DEMAND INTER-CITY AIR MOBILITY |
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ICAS2022_0264: T. Finck¹, M.-C. Névir, Technische Universität Dresden, Germany; C. Kluenker¹; ¹German Aerospace Center, Germany DESIGN & VALIDATION OF A FLIGHT CENTRIC WORKLOAD MODEL INCLUDING ATC TASK CHANGE & CONSIDERING INFLUENCING FACTORS |
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ICAS2022_0267: F. Kato¹, E. Itoh¹; ¹The University of Tokyo, Japan APPLYING MACHINE LEARNING TO TAXI-TIME PREDICTION ATTOKYO INTERNATIONAL AIRPORT |
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ICAS2022_0268: I. Gerdes¹, M. Jameel¹, R. Hunger¹, L. Christoffels¹, H. Gürlük¹; ¹German Aerospace Center DLR, Germany THE AUTOMATION EVOLVES: CONCEPT FOR A HIGHLY AUTOMATED CONTROLLER WORKING POSITION |
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ICAS2022_0271: N. Morikawa, Faculty of Aerospace Engineering, The University of Tokyo, Japan; E. Itoh, Air Traffic Management Department, Electronic Navigation Researc, Japan MACHINE LEARNING METHODS ENSURING BOTH PERFORMANCE AND INTERPRETABILITY OF ESTIMATING AIRCRAFT ARRIVAL TIMES |
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ICAS2022_0285: M. Nylin¹, J. Nilsson¹, J. Lundberg², M. Bång²; ¹LiU/LFV, Sweden; ²LiU, Sweden ATCO STRATEGIES IN TACTICAL TBO: A SIMULATOR STUDY |
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ICAS2022_0293: T. Marks¹, A. Hillebrecht¹; ¹German Aerospace Center, Germany CLUSTER STRUCTURE AND GATEWAY AVAILABILITY OF AD-HOC COMMUNICATION NETWORKS IN THE NORTH ATLANTIC AIRSPACE |
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ICAS2022_0360: A. Nieto¹, G. Alonso¹, J. Cubas¹; ¹Universidad Politécnica de Madrid, Spain IMPLICATIONS OF POTENTIAL NEW REGULATORY MEASURES TO ADDRESS AVIATION EMISSIONS |
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ICAS2022_0401: K. Sekine¹, T. Tatsukawa¹, K. Fujii¹, E. Itoh, The University of Tokyo, Japan; ¹Tokyo University of Science, Japan AIR TRAFFIC SIMULATION ACROSS FIR IN JAPAN USING CELLULAR AUTOMATON |
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ICAS2022_0451: I.C. Metz¹, S. Schier-Morgenthal¹; ¹German Aerospace Center DLR, Germany AN OPERATIONAL CONCEPT FOR THE INTEGRATION OF URBAN AIR MOBILITY VEHICLES INTO THE AIR TRAFFIC CONTROL PROCESSES |
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ICAS2022_0452: S. Bagassi¹, M. Corsi¹, F. Galuppi¹; ¹University of Bologna, Italy V/A-R AIR GESTURES HMI INTERACTION IN AIRPORT CONTROL TOWERS |
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ICAS2022_0486: M. Schultz, Universität der Bundeswehr München, Germany; M. Soolaki, University of Westminster, United Kingdom; O. Michler, Dresden University of Technology, Germany; E. Itoh, University of Tokyo, Japan REDUCED TRANSMISSION RISKS FOR PASSENGER OPERATIONS DURING COVID-19 PANDEMIC |
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ICAS2022_0574: M. Mendiguchia Meuser¹, B. Luehrs², V. Gollnick¹, F. Linke², S. Matthes³, S. Dietmüller³, S. Baumann³, M. Soler*, A. Simorgh*, F. Yinº, F. Castinoº; ¹University of Technology Hamburg, Institute of Air Transportatio, Germany; ²German Aerospace Center, Air Transportation Systems, Germany; ³German Aerospace Center, Institute of Atmospheric Physics, Germany; *Universidad Carlos III de Madrid, 4Department of Aerospace Engin, Spain; ºDelft University of Technology, Aircraft Noise and Climate Effe , Netherlands MITIGATION OF AVIATION’S CLIMATE IMPACT THROUGH ROBUST CLIMATE OPTIMIZED TRAJECTORIES IN INTRA-EUROPEAN AIRSPACE |
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ICAS2022_0627: T. Bauer¹, F. Abdelmoula¹, J. Boyer, Thales, France; M. Gerber, Swiss Sklylab Foundation, Switzerland; J. Meister², J.M. Wunderli²; ¹DLR e.V., Germany; ²Empa, Swiss Fed. Laboratories for Materials Science & Technology, Switzerland IMPROVED CONFIGURATION MANAGEMENT FOR GREENER APPROACHES – EVALUATION OF A NOVEL PILOT SUPPORT CONCEPT |
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ICAS2022_0652: T. Nagashima¹, M. Ding, Institutes of Innovation for Future Society, Nagoya University, Japan; K. Fujii¹, K. Takeda¹; ¹Graduate School of Informatics, Nagoya University, Japan OPTIMIZATION OF AIRCRAFT FLIGHT PATHS CONSIDERING THE CONFLICTING PARAMETERS OF ECONOMY AND SAFETY |
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ICAS2022_0693: C.G. Schuetz, Johannes Kepler University Linz, Austria; S. Ruiz, EUROCONTROL Innovation Hub, France; E. Gringinger¹, C. Fabianek¹, T. Loruenser, AIT Austrian Institute of Technology, Austria; ¹Frequentis AG, Austria AN AUCTION-BASED MECHANISM FOR A PRIVACY-PRESERVING MARKETPLACE FOR ATFM SLOTS |
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ICAS2022_0728: N. Yoshikawa, Mitsubishi Electric, Japan QUANTUM ARRIVAL AND DEPARTURE MANAGEMENT |
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ICAS2022_0783: S. Zaninotto¹, J. Gauci¹, B. Zammit¹; ¹University of Malta, Malta AN ENGINELESS TAXI OPERATIONS SYSTEM USING BATTERY-OPERATED AUTONOMOUS TOW TRUCKS |
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ICAS2022_0798: A. Errico¹, V. Di Vito¹; ¹CIRA - Italian Aerospace Research Center, Italy A METHOD FOR EVALUATING AIRCRAFT DEPENDENCIES USING THE CLOSEST POINT OF APPROACH METHODOLOGY TO SUPPORT ATM OPERATIONS |
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ICAS2022_0821: R. Camilleri¹, A. Batra¹; ¹Institute of Aerospace Technologies (IAT), University of Malta, Malta KINETIC ENERGY RECOVERY FROM A LANDING AIRCRAFT: ENERGY ANALYSIS, ENVIRONMENTAL AND ECONOMIC PROSPECTS |
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ICAS2022_0844: A. Lau¹, T. Ehlers¹, M. Derra¹, B. Lührs¹; ¹German Aerospace Center (DLR), Germany CONSIDERATIONS FOR MULTI-CRITERIA ROUTE DESIGN ON DIFFERENT ATMOSPHERIC SCALES |
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ICAS2022_0853: Z. Zengerling¹, F. Linke¹, C. Weder¹, K. Dahlmann¹; ¹Deutsches Zentrum für Luft- und Raumfahrt, Germany A COMPARISON OF CLIMATE-OPTIMISED AND FUEL-OPTIMISED INTERMEDIATE STOP OPERATIONS FOR SELECTED CASE STUDIES |
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ICAS2022_0907: N. Matayoshi, Japan Aerospace Exploration Agency, Japan NEW ENTRANTS’ AIRSPACE INTEGRATION IN JAPAN: JAXA’S ONGOING CONTRIBUTION |
10 - Safety and Security |
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ICAS2022_0047: J. Eltgen¹, T. Schüppstuhl¹; ¹Hamburg University of Technology, Germany TECHNICAL CONCEPTS FOR INSPECTING UAVS FOR DAMAGE |
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ICAS2022_0077: R.G. Cortes¹, E. Villani¹, M.M. Cardoso Júnior¹; ¹Aeronautics Institute of Technology, Brazil EXPLORATORY STUDY OF MENTAL WORKLOAD IN HELICOPTER AIR-TO-GROUND ROCKET FIRING |
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ICAS2022_0144: L. Sarperi¹, M. Jäger¹, P. Müller¹, M. Felux¹; ¹ZHAW, Switzerland LOCALIZATION OF INTERROGATORS WITH A 1030/1090 MHZ SPECTRUM MONITORING SYSTEM |
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ICAS2022_0180: K. Roush, United States DESIGNING FOR SECURITY: A CYBERSECURITY INTRODUCTION FOR AEROSPACE EDUCATION |
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ICAS2022_0185: C. Reiser, Embraer, Brazil; E. Villani¹, M. Machado Cardoso Junior¹; ¹ITA, Brazil LONG TOUCHDOWN THROUGH A SAFETY-II PERSPECTIVE |
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ICAS2022_0332: H. Stepien, Saab Aeronautics, Sweden; M. Bilger, Saab Surveillance, Sweden; H. Forsberg¹, B. Lindgren, Saab Dynamics, Sweden; J. Hjorth¹; ¹Mälardalen University, Sweden A NOVEL METHOD FOR DETECTING UAVS USING PARALLEL NEURAL NETWORKS WITH RE-INFERENCE |
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ICAS2022_0386: S. Ding, Civil Aviation University of China, China; C. Gan¹, T. Qiu¹, P. Liu¹, Q. Ma¹; ¹Beihang University, China SYSTEM SAFETY-BASED SUSTAINABLE AVIATION FUEL SAFETY ASSESSMENT METHOD AND AIRWORTHINESS CERTIFICATION |
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ICAS2022_0503: J. Deng, China; L. Zhang, China; K. Zhang, China; Z. Wang, China RESEARCH ON CROSSTALK CHARACTERISTICS OF AIRCRAFT ELECTRICAL CABLE |
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ICAS2022_0504: Å. Svensson, LFV, Sweden; N. Rönnberg, Linköping University, Sweden EXPECTED TEAMWORK ATTRIBUTES BETWEEN HUMAN OPERATOR AND AUTOMATION IN AIR TRAFFIC CONTROL |
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ICAS2022_0567: I. Panchal¹, I.C. Metz, German Aerospace Center, Germany; M. Ribeiro, TU Delft, Netherlands; S.F. Armanini¹; ¹TU Munich, Germany URBAN AIR TRAFFIC MANAGEMENT FOR COLLISION AVOIDANCE WITH NON-COOPERATIVE AIRSPACE USERS |
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ICAS2022_0629: A. Devta¹, I.C. Metz, DLR, Germany; S.F. Armanini¹; ¹Technical University of Munich, Germany EVALUATION AND QUANTIFICATION OF THE POTENTIAL CONSEQUENCES OF BIRD STRIKES IN URBAN AIR MOBILITY |
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ICAS2022_0662: B.R. Teixeira¹, L.G.L. de Paula¹, A.C.S. Freitas¹, R.G. Cortes², M.Y.D. Ribeiro², M.M.C. Júnior², E. Vilani²; ¹Brazilian Air Force Flight Test and Research Institute, Brazil; ²Instituto Tecnológico de Aeronáutica , Brazil DECISION LADDER APPLICATION ANALYZING A HELICOPTER EMERGENCY |
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ICAS2022_0704: S. Khan¹, G. Singh Gaba¹, A. Gurtov¹; ¹Linköping University, Sweden A FEDERATED LEARNING BASED SECURITY FOR CONTROLLER-PILOT DATA LINK COMMUNICATION |
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ICAS2022_0721: J. Hanak¹, J. Vlk¹, P. Chudy¹; ¹Brno University of Technology, Czech Republic PILOT’S ATTENTION DISTRIBUTION MODELING USING HIDDEN MARKOV MODELS |
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ICAS2022_0723: A.G.P. Sarmento¹, T. Rosado de Paula¹, A.S. Oliveira¹, E.T. da Silva¹, J. Possamai¹, H.C. Marques¹, M.M. Cardoso Junior¹, E. Villani¹; ¹Aeronautics Institute of Technology (ITA), Brazil A HUMAN-MACHINE INTERFACE ANALYSIS FOR TELEOPERATION OF UAV OVERTIME DELAY |
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ICAS2022_0725: P. Hausmann¹, H. Meeß, Fraunhofer IVI, Germany; G. Elger¹; ¹Technische Hochschule Ingolstadt, Germany IMAGE SEGMENTATION BASED EMERGENCY LANDING FOR AUTONOMOUS AND AUTOMATED UNMANNED AERIAL VEHICLES |
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ICAS2022_0903: L. Meyer¹, C. Bjursten Carlsson¹, Å. Svensson¹, M. Peukert¹, L. Danielson, SDATS, Sweden; B. Josefsson¹; ¹LFV, Sweden STRESSING SAFETY ASSESSMENT METHODS BY HIGHER LEVELS OF AUTOMATION |
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ICAS2022_0918: A. Vozella, Italian Aerospace Research Centre, Italy; P. Bieber, ONERA, France AVIATION SECURITY CONCERNS |
11 - Operations and Sustainment |
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ICAS2022_0265: E. Olsson¹, O. Candell¹, P. Funk², R. Sohlberg², M. Castaño, Luleå University of Technology, Sweden; M. Gustafsson¹, P. Bladh¹; ¹Saab Aeronautics, Sweden; ²Mälardalen University, Sweden GRAPH-BASED KNOWLEDGE REPRESENTATION AND ALGORITHMS FOR AIR AND MAINTENANCE OPERATIONS |
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ICAS2022_0328: F. Sachs¹, F. Abdelmoula¹, D. Vechtel¹; ¹DLR, Germany THE ALBATROSS PROJECT – A EUROPEAN INITIATIVE TO REDUCE AVIATION’S CARBON DIOXIDE EMISSIONS IN LARGE SCALE |
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ICAS2022_0381: S.M. Aydin¹, A.G. Yavuz, Turkish Aerospace Industries, Turkey; M. Kaya¹; ¹Yildirim Beyazit University, Turkey AERODYNAMIC INVESTIGATION OF VERY CLOSELY FLYING FIGHTERS TO DEVELOP NEW FORMATION TYPES |
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ICAS2022_0474: H. Takizawa¹, Z. Lei¹; ¹Suwa University of Science, Japan OPERATIONAL FEASIBILITY STUDY OF AIR TAXI SERVICE USING EVTOL |
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ICAS2022_0550: S.S. Manikar, Airbus/ ISAE-SUPAERO, France; J. Jezegou¹, P. de Saqui-Sannes¹, P. Asseman, Airbus, France; E. Benard¹; ¹ISAE-SUPAERO, France OPERABILITY PROJECTION OF MAJOR AIRCRAFT COMPONENTS DURING EARLY AIRCRAFT DESIGN |
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ICAS2022_0626: Y.-H. Song¹, X.-L. Zhang¹, Q.-H. Liu, Northwestern Polytechnical University, China; Y.-L. Thang¹; ¹Chinese Flight Test Establishment, China EQUIVALENT CALCULATION METHOD OF FLYOVER NOISE LEVEL OF CUTBACK TAKE-OFF FOR CIVIL JET AIRPLANE AIRWORTHINESS CERTIFICATION |
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ICAS2022_0650: R.T. Sorrentino¹, R.C. Parello¹, M. Delage¹, C.Y. Justin¹, D.N. Mavris¹, C. Jouannet², K. Amadori²; ¹Georgia Institute of Technology, United States; ²Saab AB/Saab Aeronautics, Sweden ZERO-EMISSION REGIONAL AVIATION IN SWEDEN |
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ICAS2022_0698: O. Lehmann¹, R. El-Jabi¹, K. Webster¹, A. Rachdi¹; ¹Abu Dhabi University, United Arab Emirates NEW GENERATION SPACE VEHICLE OPERATIONS IN THE UNITED ARAB EMIRATES – AN AIRSPACE AND RISK ASSESSMENT |
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ICAS2022_0747: M.J. Scott¹, S. Koschel¹, W. Verhagen¹, O. Levinski, Defence Science and Technology Group, Australia; P. Marzocca¹; ¹RMIT University, Australia AUGMENTED REALITY FOR AIRCRAFT FATIGUE NON-DESTRUCTIVE EVALUATION |
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ICAS2022_0817: R. Rameshbabu¹, D. Rajaram¹, O.J.P. Fischer¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States ESTIMATION OF ROTOR IMBALANCE AND MODEL DISCREPANCY USING A BAYESIAN APPROACH |
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ICAS2022_0825: H. Hardell¹, A. Lemetti¹, T. Polishchuk¹; ¹Linköping University, Sweden PERFORMANCE EVALUATION OF THE ARRIVAL OPERATIONS IN TERMINAL AREA |
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ICAS2022_0868: H. Meyer¹, A.-K. Koschlik¹, F. Raddatz¹; ¹German Aerospace Center, Germany DIGITAL TWIN CONCEPT FOR AIRCRAFT COMPONENTS |
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ICAS2022_0871: O.C. Okoro¹, M. Zaliskyi¹, D. Serhii , National Aviation University , Ukraine; S. Qudus, Tamara Niger Aviation, Niger; ¹National Aviation University, Ukraine DATA-DRIVEN APPROACH TO OPTIMAL AIRCRAFT MAINTENANCE |
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ICAS2022_0919: M.A. Kelly, Lockheed Martin Aeronautics, United States MODEL-BASED SYSTEMS ENGINEERING FOR FUTURE DIGITAL FLIGHT LINES |
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ICAS2022_0922: M.P.P. Osund-Ireland¹, A.J. Powell¹, C.J. Ireland¹; ¹susteer AB, Sweden A GLOBAL APPROACH TO ASSESSING THE CLIMATE RESILIENCE OF AIRPORTS |
14 - Education and Training |
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ICAS2022_0209: W. Zhao, Civil Aviation University of China, China THE CONVERSATION ANALYSIS OF AVIATION ENGLISH FROM SYSTEMIC FUNCTIONAL LINGUISTICS PERSPECTIV |
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ICAS2022_0284: S. Sun, Civil Aviation University of China, China; R. Gong, University of Waterloo, Canada INTEGRATE ONLINE QUERY&DEFENSE INTO PROJECT BASED LEARNING TO PROMPT ENGINEERING AUTHENTIC EXPERIENCES |
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ICAS2022_0315: E. Cestino, Politecnico di Torino, Italy; V. Sapienza, Aerospace Consultant, Italy; S. Sapienza, Istituto Italiano Psicoanalisi di Gruppo, Italy; F. Carena, Trainer and HR Senior Consultant, Italy A STUDENT TEAM BASED TEACHING APPROACH: THE TEAM S55 EXPERIENCE |
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ICAS2022_0523: A.G. Slongo¹, C. Jochims Lau¹, G.L. de Oliveirra¹, B.M. Ramos¹, T.B. Volkman¹; ¹AEL Sistemas, Brazil A FRAMEWORK FOR INNOVATION WITHIN AEROSPACE SEGMENT |
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ICAS2022_0675: G. Kontos¹, O. Lehmann¹; ¹Abu Dhabi University, United Arab Emirates PILOT TRAINING CHALLENGES FOR ADVANCED AIR MOBILITY |
15 - Guest lectures |
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ICAS2022_0056: D.N. Markatos¹, S.G. Pantelakis¹; ¹University of Patras, Greece ASSESSMENT OF THE SUSTAINABILITY OF THE IMPLEMENTATION OF CIRCULAR ECONOMY PRINCIPLES IN PRODUCING AIRCRAFT STRUCTURES |
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ICAS2022_0125: A. Filippatos¹, K. Abhyankar, Institute of Lightweight Engineering and Polymer Technology, Tec, Germany; G. Tzortzinis¹; ¹Dresden Center for Intelligent Materials (DCIM), Technische Univ, Germany INVESTIGATION ON INTEGRATING RECYCLABILITY AS A FUNCTION AT THE DESIGN PHASE OF COMPLEX-LOADED STRUCTURAL COMPONENTS |
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ICAS2022_0300: A. Kuenz¹, J. Lieb¹, M. Rudolph¹, A. Volkert¹, D. Geister¹, N. Ammann¹, D. Zhukov¹, P. Feurich, FlyNex, Germany; J. Gonschorek¹, M. Gessner¹, T. Kraft¹, H. Hackbarth, KopterKraft OÜ, Estonia; G. Peklar, NXP Semiconductors, Germany; L. Schalk¹, D. Becker¹, D. Gerbeth¹, C. Zhu¹, O. Garcia Crespillo¹, K. Caprdja², H. Walther², Jan Pertz¹, Klaus Lütjens¹; ¹DLR, Germany; ²DFS, Germany CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS |
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ICAS2022_0306: R. Gardner, UK - Aerospace Research Consortium, United Kingdom; I. Gray, Cranfield University, United Kingdom UK-AEROSPACE RESEARCH CONSORTIUM - EXPANDING THE VALUE OF UK ACADEMIC RESEARCH |
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ICAS2022_0322: J. Tai, Georgia Tech, United States SYSTEM LEVEL STUDIES FOR NASA - MODEL DEVELOPMENT TOWARD ZERO EMISSIONS |
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ICAS2022_0392: M. Page, United States; J. Vassberg, United States JETZERO BWB ENABLING TECHNOLOGIES |
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ICAS2022_0397: N.A. Harrison, Boeing Research & Technology, United States; G.M. Gatlin, NASA Langley Research Center, United States; E.D. Dickey¹, A.M. Malone¹; ¹Boeing Commercial Airplanes, United States TRANSONIC TRUSS-BRACED WING VISION VEHICLE TECHNOLOGY MATURATION |
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ICAS2022_0398: B. Loxton, United States A ROADMAP TOWARDS ENVIRONMENTALLY SUSTAINABLE AVIATION |
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ICAS2022_0454: H. Pfeiffer¹, H. Sekler, Deutsche Lufthansa AG, Germany; M. Wevers¹; ¹KU Leuven, Belgium SIGMOIDAL SENSING DEVICES FOR MONITORING TO IMPROVE MAINTENANCE OPERATIONS IN AERONAUTICS |
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ICAS2022_0543: N.J. Allen, Aerospace Technology Institute, United Kingdom; M.R. Schofield, Ellondee Ltd, United Kingdom IMPACT OF NASCENT TECHNOLOGIES ON THE SUSTAINABILITY ATTRIBUTES OF AN EVOLUTIONARY SINGLE-AISLE AIRCRAFT |
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ICAS2022_0648: L. Frigerio¹, I. De Visscher, Wake Prediction Technologies (WaPT), Belgium; G. Stempfel¹, R. Barragan Montes², C. Chalon Morgan²; ¹Euranova, Belgium; ²EUROCONTROL, Belgium DYNAMIC PAIRWISE WAKE VORTEX SEPARATIONS FOR ARRIVALS USING PREDICTIVE MACHINE LEARNING MODELS |
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ICAS2022_0681: E. Villani, Aeronautics Institute of Technology (ITA), Brazil; P. Krus, Linköping University, Sweden; V.J. de Negri, Federal University of Santa Catarina (UFSC), Brazil; L. Pereira, Federal University of ABC (UFABC), Brazil; G. Caurin, University of São Paulo (USP), Brazil THE BENEFIT OF BILATERAL RESEARCH NETWORKS - THE SARC AND BARINET INITIATIVES AND THE BRAZILIAN SWEDISH COLLABORATION IN AERONAUTICS |
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ICAS2022_0688: C. Voigt, Germany; M. Rapp, Germany; U. Herrmann, Germany NOVEL PATHWAYS TO SUSTAINABLE AVIATION |
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ICAS2022_0708: E. Campillo Borrás¹, M. Fischer¹, A. Kaysser-Pyzalla¹, A. Klöckner¹, D. Kügler¹, R. Mönig¹, B. Nagel¹, C.-C. Rossow¹, M. Wiedemann¹; ¹Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany FIT FOR CHANGE - DLR STRATEGY TOWARDS ZERO-EMISSION AVIATION |
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ICAS2022_0716: J. Hartmann, German Aerospace Center (DLR), Germany ELIMINATING CLIMATE IMPACT FROM AVIATION – REVIEW OF PROMISING AIRCRAFT CONCEPTS AND ENABLING TECHNOLOGY BRICKS |
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ICAS2022_0736: C. Tschida, United States TOWARD DIRECT DRIVE ELECTRIFIED PROPULSION CONCEPTS FOR SUSTAINABLE AVIATION |
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ICAS2022_0748: D.W. Zingg¹, T. Chau¹, A.L. Gray¹, T.A. Reist¹; ¹University of Toronto Institute for Aerospace Studies, Canada A MULTIFIDELITY MULTIDISCIPLINARY APPROACH TO UNCONVENTIONAL AIRCRAFT DEVELOPMENT AND ASSESSMENT WITH APPLICATION TO THE STRUT-BRACED-WING AND HYBRID-WING-BODY CONFIGURATIONS |
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ICAS2022_0774: R. Jansen¹, C.C. Kiris², T. Chau², L. Machado², T.P. Dever¹, J.S. Litt¹, J.J. Arthur³, M.N. Lynde³, J.W. Chapman¹, J.L. Kratz¹, M.G. Turner¹, A. Mirhashemi¹, C.L. Denham³, J.M. Wishart*, K. Mahavier*, M.J. Boucherº, N. Heersemaº, E.J. Stalcup¹; ¹NASA Glenn Research Center, United States; ²NASA Ames Research Center, United States; ³NASA Langley Research Center, United States; *Volpe National Transportation Systems Center, United States; ºNASA Armstrong Research Center, United States UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATION |
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ICAS2022_0807: D.S. Lazzara¹, N.A. Harrison¹; ¹Boeing, United States MDAO OF A TRANSONIC TRUSS-BRACED WING VISION VEHICLE |
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ICAS2022_0838: R. Gardner, UK-Aerospace Research Consortium, United Kingdom MAXIMISING VALUE FROM UK ACADEMIC RESEARCH - THE UK-AEROSPACE RESEARCH CONSORTIUM THEME APPROACH |
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ICAS2022_0843: M. Méheut¹, G. Arnoult¹, O. Atinault¹, Q. Bennehard¹, C. Francois¹; ¹ONERA, France OVERVIEW OF AERODYNAMIC DESIGN ACTIVITIES PERFORMED AT ONERA TO REDUCE AVIATION'S CLIMATE IMPACT |
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ICAS2022_0872: C.Y. Justin¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States REGIONAL AIR MOBILITY MARKET STUDY |
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ICAS2022_0892: O. Brodersen, Germany; T. Wunderlich, Germany; M. Abu-Zurayk, Germany; S. Görtz, Germany; C. Ilic, Germany; L. Reimer, Germany APPLICATION OF AERODYNAMIC AND AERO-STRUCTURAL OPTIMIZATION FOR ENERGY EFFICIENT AIRCRAFT |
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ICAS2022_0901: S. Hopkins, BAE Systems, United Kingdom; I. Noakes, BAe Systems, United Kingdom FUTURE COMBAT AIRCRAFT SYSTEM THE COMPLEXITY OF THE SKILLS EQUATION |
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ICAS2022_0904: A. Andreeva-Mori¹, J. Homola², M. Johnson², K. Kobayashi¹, Y. Okuno¹, P. Kopardekar²; ¹JAXA, Japan; ²NASA, United States INTEGRATED UAS TRAJECTORY OPTIMIZATION FOR DISASTER RESPONSE RECONNAISSANCE MISSIONS |
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ICAS2022_0908: S. Pendry, ATI, United Kingdom FLYZERO: THE UK VISION FOR ZERO-CARBON EMISSION AIR TRAVEL |
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ICAS2022_0909: A. Andreeva-Mori¹, J. Homola², M. Johnson², K. Kobayashi¹, Y. Okuno¹, P. Kopardekar²; ¹JAXA, Japan; ²NASA, United States OVERVIEW OF JAXA AND NASA COLLABORATION ON MANNED AND UNMANNED AIRCRAFT OPERATION INTEGRATION IN DISASTER RESPONSE |
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ICAS2022_0910: P. Renzoni, Centro Italiano Ricerche Aerospaziali, Italy GARTEUR: NEARLY HALF A CENTURY OF EUROPEAN COLLABORATION IN AERONAUTICS |
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ICAS2022_0912: B. Korn, DLR, Germany; M. Hagström, FOI, Sweden THE GROUP OF RESPONSABLES "FLIGHT MECHANICS, SYSTEMS AND INTEGRATION (GOR FM)": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES |
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ICAS2022_0915: G. Mingione, CIRA, Italy; P. Coustols, ONERA, France; F. Monge, INTA, Spain; H. van der Ven, NLR, Netherlands; K. Richter, DLR, Germany; M. Tormalm, FOI, Sweden; L.R. Calavera¹, B. Stefes¹, D. Pagan, MBDA, France; P. Eliasson, SAAB, Sweden; M. Mallet, DASSAULT, France; R. Gemma, LEONARDO, Italy; ¹AIRUBS, Spain THE GROUP OF RESPONSABLES "AERODYNAMICS (GOR AD)" AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES |
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ICAS2022_0916: H.G.S.J. Thuis, NLR, Netherlands THE GROUP OF RESPONSABLES "STRUCTURES AND MATERIALS (GOR SM)": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES |
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ICAS2022_0917: A. Visingardi, CIRA, Italy; R. Heger, Airbus Helicopters, Germany; A. Le Pape, ONERA, France; R. Markiewicz, DSTL, United Kingdom; B. Ohlenforst, NLR, Netherlands; K. Pahlke, DLR, Germany; M. White, University of Liverpool, United Kingdom THE GROUP OF RESPONSABLES "ROTORCRAFT (RC-GOR)": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES |
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ICAS2022_0921: J. Ritter¹, H. Kahlo¹, N. Mandry¹, A.G. Can¹, P. Modi¹, B. Knoblauch¹, J. Schneider¹, A. Stromayer¹, T. Dietl², P. Ratei², P. Shiva Prakasha², B. Nagel²; ¹University of Stuttgart, Germany; ²German Aerospace Center (DLR), Germany DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFT |
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ICAS2022_0923: S. Dubois, Clean Aviation JU, Belgium CLEAN SKY 2 PROGRAMME OVERVIEW |
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ICAS2022_0924: Y.C. Roth, Airbus, Germany SUSTAINABLE TECHNOLOGIES FOR COMMERCIAL AIRCRAFT OF TOMORROW - INTEGRATED MULTIFUNCTIONAL FUSELAGE DEMONSTRATOR |
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ICAS2022_0925: C. Diette, Safran Aircraft Engines, France OPEN FAN ENGINE ARCHITECTURE FOR NEXT GENERATION SMR |
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ICAS2022_0926: J. Lery, Dassault Aviation, France; M. Werner, Airbus, Germany; E. Coustols, ONERA, France PROGRESS IN WING DESIGN, STATUS AND PERSPECTIVES |
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ICAS2022_0927: J.-F. Brouckaert, Belgium THE CLEAN SKY 2 TECHNOLOGY EVALUATOR 1ST GLOBAL ASSESSMENT |
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ICAS2022_0928: R. van Manen, Clean Aviation, Belgium CLEAN AVIATION PROGRAMME RATIONALE AND OVERVIEW |
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ICAS2022_0929: M. Calvo Blanco, Belgium ULTRA-EFFICIENT AIRCRAFT AND PROPULSION ARCHITECTURES FOR LOW-EMISSION SHORT/MEDIUM RANGE [SMR] AIRCRAFT |
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ICAS2022_0930: A. Marino, Belgium HYBRID-ELECTRIC AND FULL ELECTRIC ARCHITECTURES FOR LOW-EMISSION HYBRID-ELECTRIC REGIONAL [REG] AIRCRAFT |
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ICAS2022_0931: P. Trinchieri, Belgium DISRUPTIVE TECHNOLOGIES TO ENABLE ZERO-CARBON HYDROGEN–POWERED [HPA] SHORT RANGE AIRCRAFT |
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ICAS2022_0933: J. Morrison¹, M. Nikbay, Istanbul Technical University, Turkey; E. Walker¹; ¹NASA Langley Research Center, United States NATO AVT-297 DEVELOPMENT OF A FRAMEWORK FOR VALIDATION OF COMPUTATIONAL TOOLS FOR ANALYSIS OF AIR VEHICLES |
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ICAS2022_0934: J.M. Luckring, NASA Langley Research Center, United States; S. Shaw, MBDA UK Ltd., United Kingdom; W.L. Oberkampf, WLO Consulting, Inc., United States; R. Graves, Air Force Research Laboratory, United States CONNECTING SYSTEM DESIGN TO MODELING AND SIMULATION CAPABILITIES |
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ICAS2022_0935: D.N. Mavris¹, E.Y. Yarbasi¹, B. Bagdatli¹; ¹Georgia Institute of Technology, United States SYSTEM LEVEL IDENTIFICATION OF CRITICAL UNCERTAINTIES TO ENABLE VALIDATION EXPERIMENTS |
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ICAS2022_0936: op panel, United States OPEN PANEL DISCUSSION |
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ICAS2022_0937: T. Petersson, Sweden THE SWEDISH AIR FORCE INTO THE FUTURE – AIMING FOR A HIGHER GROUND AND A SHARPER EDGE |
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ICAS2022_0940: G. Girard, France FUTURE COMBAT AIR SYSTEMS: REQUIREMENTS AND TECHNOLOGIES |
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ICAS2022_0943: S.E. Tsentis, Greece; V.G. Gkoutzamanis, Greece; A.D. Gaitanis, Greece; A.I. Kalfas, Greece MULTI-PLATFORM APP-EMBEDDED MODEL FOR HYBRID AIR-BREATHING ROCKET-CYCLE ENGINE IN HYPERSONIC ATMOSPHERIC ASCENT |
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ICAS2022_0944: C. Andrews¹, A. Simpson¹; ¹GE, United States HYBRID ELECTRIC PROPULSION DEVELOPMENT FOR COMMERCIAL AVIATION |
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ICAS2022_0945: L.-Y. Jiang¹, X. Wu¹, Q. Yang¹; ¹National Research Council Canada, Canada SAND EROSION MODELING IN GENERIC COMPRESSOR RIG TESTING |
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ICAS2022_0948: A. Andreeva-Mori, JAXA, Japan; S. Sharma¹, S. Verma¹, B. Dziugiel, Lukasiewicz Research Network, Poland; D. Sziroczak, Budapest University of Technology and Economics, Hungary; ¹Ames Research Center, United States AN INTERNATIONAL RESEARCH PERSPECTIVE ON AIRSPACE INTEGRATION IN THE FRAMEWORK OF URBAN AIR MOBILITY |
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ICAS2022_0949: C. Eschmann, DLR, Germany; D.L. Hackenberg, National Aeronautics and Space Administration (NASA), United States; C. Vidal, National Research Council Canada (NRC), Canada INTERNATIONAL SCIENTIFIC ASSESSMENT ON URBAN AIR MOBILITY AS A CONTRIBUTION TO FUTURE AVIATION STANDARDS |
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ICAS2022_0950: J. Huete¹, D. Nalianda¹, P. Pilidis¹; ¹Cranfield University, United Kingdom PROPULSION SYSTEM INTEGRATION FOR A FIRST GENERATION HYDROGEN CIVIL AIRLINER? |
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ICAS2022_0951: M. Page, United States; J. Vassberg, United States JETZERO BWB ENABLING TECHNOLOGIES |
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ICAS2022_0952: W. Orisamolu, United States AN INNOVATIVE HYDROGEN-POWERED PROPULSION SYSTEM FOR SINGLE-AISLE AIRCRAFT |
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ICAS2022_0953: M.R. Khorrami, United States TOWARD A COMMUNITY NOISE ASSESSMENT OF SINGLE-AISLE AIRCRAFT WITH HYBRID-ELECTRIC PROPULSION |
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ICAS2022_0954: U. Kerlin, Airbus, Germany CERTIFICATION BY ANALYSIS - SOME THOUGHTS |
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ICAS2022_0955: O. Pinon Fischer, United States; D. Mavris, United States NEXT STEPS TOWARDS CERTIFICATION BY ANALYSIS - A DIGITAL THREAD PERSPECTIVE |
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ICAS2022_0956: R. Gregg, Boeing, United States TOWARDS CERTIFICATION BY ANALYSIS FOR FLIGHT CHARACTERISTICS |
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ICAS2022_0957: S. Ying, AMPAIRE, United States AMPAIRE AND THE ELECTRIFIED PROPULSION JOURNEY |
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ICAS2022_0958: I. De Visscher, WaPT, Belgium; M. Langer¹, K. Bayram¹, T. Feuerle², P. Hecker², F. Rooseleer³, C. Chalon Morgan³; ¹2CACTUS partners GmbH, Germany; ²TU Braunschweig, Germany; ³EUROCONTROL, Belgium FLIGHT SIMULATION TO SUPPORT SAFETY CASE FOR PAIR-WISE WAKE TURBULENCE SEPARATION ON DEPARTURES |
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ICAS2022_0959: M. Kyriakopoulos, Belgium EUROPEAN AVIATION RESEARCH AND INNOVATION TOWARDS CLIMATE NEUTRALITY |
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ICAS2022_0960: J.G. Nairus, United States POWER/THERMAL 2030 VISION - AIR PLATFORM ELECTRIFICATION |
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ICAS2022_0961: M. Langer, Germany FLIGHT SIMULATION TO SUPPORT SAFETY CASE FOR PAIR-WISE WAKE TURBULENCE SEPARATION ON DEPARTURES |
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ICAS2022_0962: M. Wiedemann¹, D. Wilckens¹, M. Kleineberg¹; ¹DLR, Germany DESIGN,MANUFACTURING & CERTIFICATION STRATEGIES FOR INNOVATIVE HYDROGEN STORAGE SYSTEMS TO ENABLE ZERO EMISSION AVIATION |
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ICAS2022_0963: J.P. Clark, Universal Hydrogen, United States REALISTIC HYDROGEN-BASED SOLUTIONS FOR SUSTAINABLE AVIATION |
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ICAS2022_0964: N. Nagel, Germany; C. Jouannet, Sweden ICAS DIGITAL PIONEERING INITIATIVE AND SYSTEM OF SYSTEM CHALLENGES |
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ICAS2022_0965: P. Schmollgruber, France; I. Staack, Sweden CHALLENGES OF MULTIDISCIPLINARY DESIGN OPTIMIZATION FOR GREEN AVIATION |
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ICAS2022_0966: S. Bagassi, Italy; L. Boggero, Germany POTENTIAL OF EXTENDED REALITY IN ENGINEERING AND CHALLENGES OF UNCONVENTIONAL VEHICLE DESIGN |