ICAS 2026: TOPICS AND TITLES |
1.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools) |
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ICAS2026_0034: T. Batty, Defence Science and Technology Group, Department of Defence, Australia MULTI-OBJECTIVE OPTIMISATION OF AERIAL VEHICLES USING REINFORCEMENT LEARNING |
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ICAS2026_0042: M. Maier¹, K. Sørensen-Libik², Ö. Petersson², C. Breitsamter¹; ¹Technical University of Munich (TUM), Germany; ²Airbus Defence and Space GmbH, Germany HIGH-FIDELITY DATASET-BASED SHAPE AND STRUCTURE OPTIMIZATION FOR AIRCRAFT DESIGN |
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ICAS2026_0088: W. Wei¹, Y. Ma¹, Z. Han¹; ¹ School of Aeronautics, Northwestern Polytechnical University, China MULTIDISCIPLINARY PHYSICS-CONSTRAINED GENERATIVE DESIGN OF DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT |
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ICAS2026_0100: Y.Y. Ma, China; W.Y. Wei, China; Y.Q. Du, China; M. Abouhamzeh, Netherlands; Z.H. Han, China INVERSE AEROELASTIC SIZING FOR STRUT-BRACED WINGS VIA PHYSICS-GUIDED GENERATIVE MODELING |
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ICAS2026_0130: J. Song¹, S. Park², D. Lee², Y.-E. Kang¹, Y. Kim¹, W.I. Choi¹, S. Lee¹; ¹Manufacturing AI Research Center, KITECH, South Korea; ²Department of Unmanned Aircraft Systems, Hanseo University, South Korea DEVELOPING AN AGENTIC AI WORKFLOW FOR AUTOMATED CONCEPTUAL DESIGN OF AIRCRAFT USING RISPECT+ |
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ICAS2026_0155: A. Wang¹, R. Carrese¹, L. Brown¹, J. Collins¹, P. Marzocca, RMIT University, Australia; ¹Boeing Aerostructures Australia, Australia GEOMETRY PARAMETERISATION VIA A STRUCTURAL MODAL BASIS FOR AERODYNAMIC SHAPE OPTIMISATION |
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ICAS2026_0201: E. Espinosa-Juárez¹, A. Dell'Amico¹; ¹Linköping University, Sweden MODELLING COUPLED ON-BOARD SYSTEMS IN AIRCRAFT DESIGN |
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ICAS2026_0209: L. Liu¹, Y. Wu¹, M.A. Hariansyah¹, R.P. Liem, ICL, Department of Aeronautics, United Kingdom; ¹HKUST, Department of Mechanical and Aerospace Engineering, Hong Kong SAR of China A BILEVEL STRATEGY FOR ON-DESIGN EVTOL SIZING AND OFF-DESIGN STRUCTURAL WEIGHT OPTIMIZATION |
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ICAS2026_0214: S. Hellbrück¹, P. Zemke¹, C. Hesse¹, M. Fuchs¹, J. Biedermann¹, B. Nagel¹; ¹DLR e.V., Germany AUTOMATED KNOWLEDGE-BASED CABIN DESIGN AND EVALUATION WITHIN A PRELIMINARY AIRCRAFT DESIGN LOOP |
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ICAS2026_0229: S. Valencia-Ibáñez¹, S. Liscouët-Hanke¹; ¹Concordia University, Canada INTEGRATING SYSTEM ARCHITECTURE OPTIMIZATION INTO MODEL-BASED SYSTEMS ENGINEERING METHODS |
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ICAS2026_0254: J. Wu, China; W. Song, China; H. Nie, China; C. Liu, China AN EFFICIENT TRANSITION PREDICTION METHOD USING NEURAL NETWORK SURROGATE MODELS |
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ICAS2026_0273: D. Eisenhut, Germany; A. Strohmayer, Germany DATA-DRIVEN FAST NOISE PREDICTION OF AN UNCONVENTIONAL AIRCRAFT USING HIGH-FIDELITY SIMULATION DATA |
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ICAS2026_0278: Y.-H. Peng¹, K.-S. Zhang¹, Q. Chen¹, Z.-H. Han¹; ¹Northwestern Polytechnical University, China DEEP LEARNING-BASED INVERSION OF NEAR-FIELD OVERPRESSURE SIGNATURES FOR LOW-BOOM SUPERSONIC TRANSPORT |
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ICAS2026_0285: G. Palaia, Polytechnic of Turin, Italy; K. Abu Salem, University of Trento, Italy; A.A. Quarta, University of Pisa, Italy; P.D. Bravo-Mosquera, University of São Paulo, Brazil ASSESSMENT OF LIQUID HYDROGEN-POWERED AIRCRAFT RANGE: A NOVEL BREGUET FORMULATION |
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ICAS2026_0293: A.P.S. Inderawan¹, M. Hoogreef¹; ¹Delft University of Technology, Netherlands EFFECT OF ENGINE RESPONSE TIME IN AIRCRAFT CONCEPTUAL DESIGN |
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ICAS2026_0305: F.H. Christiansen¹, M.C. Berschik¹, S. Wehrend¹, D. Krause¹; ¹Hamburg Univeristy of Technology, TUHH, Germany LINKING PRODUCT FAMILY ARCHITECTURE ANALYSIS AND COMPONENT-LEVEL OPTIMISATION USING SYSTEM MODELS |
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ICAS2026_0320: B.D. Phillips¹, E. Aretskin-Hariton¹, A. DeBlois², J, Singh², M. Abu-Zurayk, German Aerospace Center (DLR), Germany; J.A. Schaefer³, S. Wakayama³; ¹NASA Glenn Research Center, United States; ²Bombardier Aviation, Canada; ³The Boeing Company, United States A BENCHMARK FOR UNCERTAINTY QUANTIFICATION AND OPTIMIZATION UNDER UNCERTAINTY IN CONCEPTUAL AIRCRAFT DESIGN: THE F25-OUU CHALLENGE PROBLEM |
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ICAS2026_0346: N. Morita¹, N. Okubo¹, T. Ogawa¹, Y. Sasaki¹; ¹Velcity Aeroworks .Inc, Japan DYNAMIC ANALYSES AND FLIGHT TESTING FOR THE DESIGN OF FLOATING CANARD AIRCRAFT |
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ICAS2026_0348: J. Vézina¹, S. Liscouët-Hanke¹; ¹Concordia University, Canada A FRAMEWORK FOR AUTOMATED SYSTEM COMPONENT PLACEMENT IN AIRCRAFT CONCEPTUAL DESIGN |
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ICAS2026_0353: K. Becker¹, J.P. Haug¹, M. Schuff¹; ¹German Aerospace Center (DLR), Germany TOWARDS AN ONTOLOGY-BASED APPROACH FOR DISCIPLINE-SPECIFIC ENGINEERING VIEWS IN ENGINE DESIGN |
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ICAS2026_0393: Z.X Li¹, Z.H Han¹, K. Song¹, K.S Zhang¹; ¹Northwestern Polytechnical University, China ADAPTIVE-PREFERENCE MULTI-OBJECTIVE REINFORCEMENT LEARNING FOR WIDE-SPEED-REGIME AIRFOIL OPTIMIZATION |
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ICAS2026_0400: G. Palaia, Politecnico di Torino, Italy; K. Abu Salem, University of Trento, Italy; A.A. Quarta, University of Pisa, Italy; P.D. Bravo-Mosquera, São Carlos School of Engineering, University of São Paulo, Brazil AN INTEGRATED CONCEPTUAL DESIGN WORKFLOW FOR LIQUID HYDROGEN-POWERED BOX-WING AIRCRAFT |
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ICAS2026_0406: P. Inselmann¹, F.D. Bischop¹, F.H. Christiansen¹, M. Höhner¹, T. Schüppstuhl¹, D. Krause¹; ¹Hamburg University of Technology, Germany ASSESSING THE POTENTIAL OF MULTI-MODEL TOPOLOGY OPTIMIZATION FOR MODULAR LIGHTWEIGHT DESIGN OF AIRCRAFT CABIN STRUCTURES |
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ICAS2026_0445: J.L.C. Chan¹, D. Pasquale¹, W. Widjaja¹, S. Lyu¹, J. Rispin¹, H. Smith¹; ¹Cranfield University, United Kingdom COMPARING DIFFERENT SEMI-EMPIRICAL AERODYNAMIC TOOLS FOR ANALYSING NOVEL AIRCRAFT CONFIGURATIONS |
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ICAS2026_0455: X. Lu¹, S. Chen¹, X. Wang¹, J. Yu¹, D. Li¹; ¹Northwestern Polytechnical University, China CST PARAMETRIC MODELING AND MULTI-OBJECTIVE OPTIMIZATION RECONFIGURATION STUDY OF A BLENDED-WING-BODY AIRCRAFT |
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ICAS2026_0458: X.M. zhang, China; H. Zhao, China; Z. Gong, China RESEARCH ON GENERALIZED REPRESENTATION OF FLYING-WING CONFIGURATIONS BASED ON DEEP LEARNING |
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ICAS2026_0466: X. Liu, China; T. Yu, China; B. Song, China; D. Xue, China STUDY ON INDUCED DRAG CALCULATION FOR BIRD-LIKE WINGTIP SLOTS USING WAKE-PLANE INTEGRATION |
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ICAS2026_0469: S.A. Bakhshi¹, A. Yildirim¹, J.R.R.A. Martins¹; ¹University of Michigan, United States A MIXED-FIDELITY VISCOUS-INVISCID INTERACTION APPROACH FOR WING AERODYNAMIC DESIGN OPTIMIZATION |
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ICAS2026_0476: W. Lin¹, C.C. Nian¹, J.C. Li¹; ¹Northwestern Polytechnical University, China DATA-DRIVEN SHAPE PARAMETERIZATION FOR EFFECTIVE AERODYNAMIC DESIGN OPTIMIZATION OF PROPELLERS |
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ICAS2026_0484: H. Guan, Australia; K.C. Wong, Australia RESONANT ELASTIC SHAFT THRUST VECTORING: IMPLICATIONS FOR UAV DESIGNS |
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ICAS2026_0485: J.Y. He¹, H. Zhao¹; ¹Northwestern Polytechnical University, China MULTI-FIDELITY BAYESIAN NEURAL NETWORKS FOR STEALTH/AERODYNAMIC DATA FUSION METHOD |
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ICAS2026_0515: J.W. He¹, B.G. Mi¹, J.Y. Zhang¹; ¹School of Aeronautics of Northwestern Polytechnical University, China A UNIFIED PARAMETRIC MODELING METHOD FOR CONVENTIONAL, SEMI-BURIED, AND EMBEDDED INLETS |
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ICAS2026_0524: B. Wang, The University of Sydney, Australia; D. Lee¹, G. Lee¹; ¹Hanyang University, South Korea A SINGLE-LOOP BAYESIAN OPTIMIZATION FRAMEWORK FOR MULTIDISCIPLINARY DESIGN OPTIMIZATION UNDER UNCERTAINTY |
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ICAS2026_0528: J.-Z, Zhang¹, Z.-H. Han¹, W.-P. Song¹, K.-S. Zhang¹, Y. Zhang¹; ¹Northwestern Polytechnical University, China POINT-CLOUD-BASED INTELLIGENT DESIGN OF FLYING-WING CONFIGURATIONS WITH CONDITIONAL GENERATION AND PRESSURE PREDICTION |
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ICAS2026_0552: Y. Lin¹, K.S. Zhang¹, Z.H. Han¹, Q. Chen¹; ¹Northwestern Polytechnical University, China LOW BOOM DESIGN AND ANALYSIS OF A BLENDED-WING-BODY CONFIGURATION FOR LARGE-SIZED SUPERSONIC TRANSPORT |
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ICAS2026_0575: A. Kirste¹, L. Faltum¹, E. Stumpf¹; ¹Institute of Aerospace Systems, RWTH Aachen University, Germany AGENTIC AI FOR AIRCRAFT PRELIMINARY DESIGN: PROOF OF CONCEPT |
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ICAS2026_0577: X. Tang¹, B.G. Mi¹; ¹Northwestern Polytechnical University, China RESEARCH ON AERODYNAMIC-STRUCTURAL RAPID EVALUATION AND OPTIMIZATION METHODS FOR JOINED-WING CONFIGURATIONS |
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ICAS2026_0578: Zhengdong LUO¹, Baigang MI¹; ¹School of Aeronautics of Northwestern Polytechnical University, China A RAPID AERODYNAMIC ASSESSMENT METHOD FOR BATTLE-DAMAGED CRUISE MISSILES |
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ICAS2026_0596: W.Z. Liu, China; B.L. Shang, China; P.F. Li, China; R.X. Ling, China; Y.Z. Wang, China; K.A. Xing, China; H.X. Li, China; M.Z. Hou, China RESEARCH ON EFFECTIVENESS-DRIVEN INTELLIGENT OPTIMIZATION METHOD FOR CONCEPTUAL LAYOUT OF AIRCRAFT |
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ICAS2026_0602: E. Stragiotti¹, E. Nguyen Van¹, R. Parello¹, S. Defoort¹, D. Losada Costoso², C. Mollet², M. Méheut², O. Atinault², F. Moëns², L. Vertonghen³, C. Julien³, A. Lannoo*, V. Priasso*; ¹DTIS, ONERA, Université de Toulouse, France; ²DAAA, ONERA, Institut Polytechnique de Paris, France; ³DMAS, ONERA, Université Paris-Saclay, France; *DMAS, ONERA, France SWIFT: AN ULTRA HIGH ASPECT RATIO STRUT-BRACED DRY WING HYDROGEN-POWERED AIRCRAFT |
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ICAS2026_0604: Y. Yamai¹, M. Itoh¹, M.-P. Pacaux-Lemoine, Université Polytechnique Hauts-de-France, France; ¹University of Tsukuba, Japan MULTI-STATE FLIGHT DECK DISPLAY LAYOUT OPTIMIZATION UNDER FAILURE AND REVERSION CONDITIONS |
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ICAS2026_0609: N. Okubo¹, N. Morita, Velocity Aeroworks .Inc, Japan; T. Tuchiya¹; ¹The University of Tokyo, Japan COMPARISON OF FLEXIBLE AIRCRAFT CONFIGURATIONS USING AEROELASTIC ANALYSIS |
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ICAS2026_0610: B. Blaxall¹, F. Di Fiore¹, D. Venetsanos¹, L. Mainini¹; ¹Imperial College London, United Kingdom MULTIDISCIPLINARY DESIGN OF COMPLIANT DEFORMABLE WINGS FOR IMPROVED AIRCRAFT EFFICIENCY: INTRODUCING AN ARCHITECTURE-AWARE OPTIMIZATION STRATEGY |
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ICAS2026_0631: M.A. Hariansyah¹, C. Reyner¹, R.P. Liem, Imperial College London, United Kingdom; P.S. Palar, Institut Teknologi Bandung, Indonesia; ¹The Hong Kong University of Science and Technology, Hong Kong SAR of China OPTIMAL CONCEPTUAL DESIGN AND UPGRADE STRATEGIES FOR EVTOL AIRCRAFT UNDER EVOLVING TECHNOLOGIES |
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ICAS2026_0668: P. Krus, Linköping University, Sweden AI-SUPPORTED AIRCRAFT SYSTEM ARCHITECTURE SYNTHESIS |
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ICAS2026_0687: T.X.Q. Hoang¹, T.A. Pham¹, X.H. Vu¹, H.H. Nguyen¹, C.A. Pham¹, D.L. Chu¹; ¹Viettel Aerospace Institute, Vietnam A HYBRID 0D–2D WHOLE-ENGINE MATCHING FRAMEWORK FOR TURBOJET ENGINE PERFORMANCE SIMULATION |
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ICAS2026_0836: D. Ciliberti¹, A. De Marco¹, F. Nicolosi¹; ¹University of Naples Federico II, Italy MIXED-FIDELITY, NONLINEAR AIRCRAFT MISSION MODELING FOR HYBRID REGIONAL AIRCRAFT DESIGN VERIFICATION |
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ICAS2026_0837: G. Babunaidu¹, A. Hammad¹; ¹Technical University of Munich, Germany IMPACT OF DIFFERENT PROPELLER CONFIGURATIONS ON THE FLIGHT DYNAMICS AND STABILITY OF A SMALL REGIONAL ELECTRIC AIRCRAFT |
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ICAS2026_0873: S. Choi¹, Y. Lee¹, H. Choi¹, B. Cho¹, Y. Kim¹, D. Jung¹; ¹Korea Aerospace University, South Korea THREE-DIMENSIONAL AERODYNAMIC ANALYSIS OF A WING–ROTOR CONFIGURATION FOR A FOLDING WING UAV |
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ICAS2026_0876: P. Moreno-Escolastico¹, M. Raiola¹, R. Castellanos¹, A. Cini¹; ¹Universidad Carlos III de Madrid, Spain AN INCREMENTAL MODULAR MDO FRAMEWORK FOR HYDROGEN-ELECTRIC POWERTRAIN SIZING AND INTEGRATION IN GENERAL AVIATION AIRCRAFT |
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ICAS2026_0894: K. Swannet¹, N.A.K. Doan, Imperial College London, United Kingdom; C. Varriale¹; ¹Delft University of Technology, Netherlands INVERSE AIRFOIL DESIGN USING AERODYNAMICALLY CONDITIONED VARIATIONAL AUTOENCODERS |
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ICAS2026_0899: M.C. Moruzzi¹, T. Fadda¹, E. Caligari¹, S. Bagassi¹; ¹Università di Bologna, Italy AURAL DIGITAL TWIN FOR AIRCRAFT CABIN DESIGN |
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ICAS2026_0915: T.A. Ramprakash¹, D. Di Pasquale¹, S. Kumar¹; ¹Cranfield University, United Kingdom IMPLEMENTATION OF PROPELLER-WING INTERFERENCE MODEL AND HORIZONTAL TAIL ANALYSIS INTO A VISCOUS FULL POTENTIAL FLOW SOLVER FRAMEWORK FOR AIRCRAFT DESIGN |
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ICAS2026_1112: C. Zhou¹, Y. Ma¹, Z. Han¹; ¹Northwestern Polytechnical University, China PROPULSIVE EFFICIENCY AND ENERGY ANALYSIS OF AIRCRAFT CONCEPTS WITH AFT-FUSELAGE BOUNDARY-LAYER-INGESTION |
1.2 - Aircraft Design and Integrated Systems (Use cases and Applications) |
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ICAS2026_0055: M. Sankrithi, RIC Enterprises, United States; D. Mavris¹, R. Sundar¹; ¹Georgia Institute of Technology, United States MODELING & PRELIMINARY ANALYSIS OF AN ECOFRIENDLY AIRBORNE GLOBAL LUXURY EKRANOPLAN |
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ICAS2026_0062: K. Wang¹, Z. Zhou¹, J. Wang¹; ¹Northwestern Polytechnical University, China AERODYNAMIC EFFECTS OF DISTRIBUTED PROPULSION WING CONFIGURATION PARAMETERS |
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ICAS2026_0073: B. Türkyilmaz¹, M.G. Kolb¹, X. Zhao, Chalmers University of Technology, Sweden; M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany DESIGN AND INVESTIGATION OF A SHORT-TO-MEDIUM-RANGE AIRCRAFT WITH LIQUID HYDROGEN AND SAF MULTI-FUEL PROPULSION |
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ICAS2026_0078: L. Li¹, M. Chao¹, L. Wang, AVIC (CHENGDU) UAS CO., LTD., China; J. Zhong, School of Aeronautics, Northwestern Polytechnical University, China; F. Li, Xinjiang Institute of Intelligent Equipment, China; ¹School of Future Transportation, Chang’an University, China COMPARATIVE DESIGN OF SBW AIRCRAFT WITH AERODYNAMIC SHAPE OPTIMIZATION FOR THREE DIFFERENT PROPULSION LAYOUTS |
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ICAS2026_0187: J. Ruberte Bailo¹, T. Streit¹, A. Seitz¹; ¹DLR, Germany A LAMINAR TAILORED WING WITH CATNLF AND HLFC FOR EXTRA LONG RANGE |
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ICAS2026_0213: B. Legrand¹, N. Gavrilovic¹; ¹Département Aérodynamique, Energie et Propulsion, ISAE-SUPAERO, France CHALLENGES AND SOLUTIONS FOR LIQUID HYDROGEN-POWERED UAVS: REGULATIONS AND CASE STUDY INSIGHTS |
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ICAS2026_0274: E.M. Künstler¹, S. Roscher², A. Bardenhagen², A. Strohmayer¹; ¹University of Stuttgart, Germany; ²Technische Universität Berlin, Germany EMISSION REDUCTION POTENTIAL OF UNCONVENTIONAL CONFIGURATIONS FOR LONG-RANGE AIRCRAFT |
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ICAS2026_0296: F. Nikodem¹, C. Weiser¹; ¹DLR e.V., Germany FLIGHT TESTING OF A HIGH-ALTITUDE UNCREWED AND SOLAR POWERED PLATFORM HEAVIER THAN AIR |
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ICAS2026_0316: A. Tramposch¹, F. Thilker¹, S. Pfeifer¹, P. Kirschnek¹; ¹University of Applied Sciences FH Joanneum GesmbH, Austria AN INTEGRATED SYSTEM-LEVEL AND MULTIPHYSICS APPROACH FOR AIRCRAFT LH2 FUEL SYSTEM DESIGN |
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ICAS2026_0319: N. Schneiders¹, D. Keller¹, A. Link¹, T. Burschyk¹, G. Atanasov¹; ¹German Aerospace Center (DLR), Germany INTEGRATION OF A SOLID OXIDE FUEL CELL PROPULSION SYSTEM: A TECHNOLOGY DEVELOPMENT GOAL FOR REGIONAL AIRCRAFT |
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ICAS2026_0331: I. Pruter¹, G. Schmitz¹, H. Duda¹, M. Laubner¹, S. Lorenz¹; ¹DLR e.V., Germany FLIGHT OPERATIONS AND TESTING OF A 450 KG EXPERIMENTAL GYROPLANE UAV |
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ICAS2026_0333: M. Kotzem¹, J. Häßy¹, V. Kriewall Peters, Hamburg University of Technology (TUHH), Germany; P. Schatrow¹, S. Wöhler¹; ¹German Aerospace Center (DLR), Germany ADVANCED MODELING AND ANALYSIS OF A LIQUID HYDROGEN SHORT-MEDIUM RANGE AIRCRAFT CONCEPT FOR 2035 |
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ICAS2026_0360: S. Trepiccione¹, G. Melone¹, F. Nicolosi¹, G. Piscopo, Leonardo, Italy; M. Di Stasio¹; ¹UNINA, Italy MULTIDISCIPLINARY DESIGN EXPLORATION OF HYBRID-ELECTRIC REGIONAL AIRCRAFT |
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ICAS2026_0371: E. Riccio¹, R. Bombardieri¹, A. Ceresa¹, V.R. Baraniello¹, F. Tufano¹, G. Persechino¹, D. Coiro, University Federico II of Naples, Italy; ¹Italian Aerospace Research Centre, Italy MULTIDISCIPLINARY APPROACH FOR THE AERODYNAMIC CHARACTERIZATION OF AN INFLATABLE CLOSED-WING HYBRID HIGH-ALTITUDE PSEUDO-SATELLITE |
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ICAS2026_0401: D.E. Lampl, Technical University of Munich, Germany; S.F. Armanini, Imperial College London, United Kingdom PROPULSION SYSTEM MODELING AND OPTIMIZATION FOR CONCEPTUAL DESIGN OF HYBRID-ELECTRIC VTOL AIRCRAFT |
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ICAS2026_0416: E. Cassidy¹, A. Garcia, Collins Aerospace, France; G. Cinar¹; ¹University of Michigan, United States A MULTI-SCALE COMPUTATIONAL FRAMEWORK FOR EVALUATING TECHNOLOGY IMPACTS ON FUTURE AIRCRAFT FLEETS |
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ICAS2026_0420: A.S.J. van Heerden¹, N.M. Ahamad¹, J.F. Castiblanco Aponte¹, J. Gibbs¹, I.J. Taylor¹; ¹University of Glasgow, United Kingdom CONCEPTUAL DESIGN OF A MIDDLE-OF-THE-MARKET AIRCRAFT FOR EDUCATIONAL PURPOSES |
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ICAS2026_0447: J.L.C Chan¹, H Smith¹; ¹Cranfield University, United Kingdom PERFORMANCE COMPARISON BETWEEN PASSENGER AIRCRAFT WITH NOVEL PROPULSION SYSTEMS AT CONCEPTUAL DESIGN LEVEL |
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ICAS2026_0482: B. Li¹, B. Mi¹; ¹Northwestern Polytechnical University, China RESEARCH ON OVERALL AERODYNAMIC DESIGN OF GRID-DUCT INTEGRATED VERTICAL TAKE-OFF AND LANDING (VTOL) FIXED-WING AIRCRAFT |
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ICAS2026_0576: H. Reindle¹, J. Hoffelner¹, N. Sekyra¹, N. Schlautmann¹, M. Weber¹, V. Sittel¹, C. Mishra¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, TUM, Germany RESEARCH PLATFORM AIRSHIP: DESIGN AND FLIGHT CHARACTERISTICS FOR URBAN OPERATIONS |
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ICAS2026_0594: P.P. Kapoor¹, R.S. Pant, IIT Bombay, India; M. Abdelrahman¹, D. Mohd-Nasir, University of Sheffield, United Kingdom; M.S. Ismail¹; ¹University of Hull, United Kingdom DESIGN AND TESTING OF A BUOYANT UAV FOR AGRICULTURAL SURVEILLANCE |
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ICAS2026_0625: G. Atanasov¹, D. Silberhorn¹, V. Nugnes¹; ¹German Aerospace Center (DLR), Germany A MULTI-RANGE HYBRID-ELECTRIC OPEN-ROTOR AIRCRAFT CONCEPT FOR THE WIDE-BODY PASSENGER CLASS |
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ICAS2026_0636: A. Orgiu, ISAE-SUPAERO, Concordia University, Canada; S. Delbecq, ISAE-SUPAERO, France; J. Liscouët, Concordia University, Canada ENDURANCE EVALUATION OF DIFFERENT UAV CONFIGURATIONS AND POWERTRAIN ARCHITECTURES |
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ICAS2026_0643: A. Frediani¹, E. Rizzo¹, G. Palaia, Politecnico di Torino, Italy; K. Abu Salem, University of Trento, Italy; M. Martini¹; ¹SkyBox Engineering, Italy LIFT-AND-CRUISE EVTOL BOX-WING CONFIGURATION FOR THE LOW ALTITUDE ECONOMY |
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ICAS2026_0673: M. Bouchard¹, M. Bashir², D. Rancourt¹, S. Liscouët-Hanke², F. Sirois, Polytechnique Montréal, Canada; S. Lloyd², A. Tfaily³, M. Mark³, R. Freer, Pratt & Whitney Canada, Canada; J. Moriot, Calogy Solutions, Canada; ¹Université de Sherbrooke, Canada; ²Concordia University, Canada; ³Bombardier, Canada EXPLORATION OF ALTERNATIVE PROPULSION ARCHITECTURES FOR BUSINESS AVIATION |
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ICAS2026_0688: S. Trivedi¹, A.K. Munshi¹, R.S. Pant¹; ¹Indian Institute Technology Bombay, India PRELIMINARY SIZING METHODOLOGY FOR HYBRID-ELECTRIC PROPULSION SYSTEM IN CARGO AIRSHIPS |
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ICAS2026_0696: G. Shen¹, X. Zhang¹, W. Hao¹, Z. Wang¹; ¹Northwestern Polytechnical University, China MISSION-PROFILE-BASED HYBRID POWER SYSTEM DESIGN AND OPTIMIZATION FOR VTOL AIRCRAFT IN REGIONAL AIR MOBILITY |
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ICAS2026_0703: M. Di Stasio¹, F. Nicolosi¹; ¹UNINA, Italy TOP-LEVEL AIRCRAFT REQUIREMENT TRADE STUDIES FOR HYDROGEN FUEL CELL REGIONAL AIRCRAFT |
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ICAS2026_0783: L. Falcone¹, S. Corcione¹, F. Nicolosi¹, S. Trepiccione¹; ¹University of Naples Federico II, Italy COST-DRIVER MULTIDISCIPLINARY FRAMEWORK FOR WINGLET DESIGN: A REGIONAL AIRCRAFT CASE STUDY |
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ICAS2026_0801: J. Rasines Mazo¹, B. Van Magill¹, D. Verstraete¹; ¹The University of Sydney, Australia COMMON RESEARCH MODELS FOR SMALL UNCREWED AERIAL VEHICLES |
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ICAS2026_0817: H.B. Rogers¹, T.T. Takahashi¹, J.A. Camberos¹, R.V. Grandhi¹; ¹AFIT, United States EVALUATION OF PERCEIVED X-15 FLYING QUALITIES BASED ON RAPID AERODYNAMIC PREDICTIONS |
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ICAS2026_0888: P. Schmollgruber¹, S. Defoort¹, E. Nguyen-Van¹, J. Gauvrit-Ledogar¹, J. Chan², C. Lawson², L. Kugler³, T. Zill³, J. Kos, NLR, Netherlands; ¹ONERA, France; ²Cranfield University, United Kingdom; ³DLR, Germany FUTURE LONG RANGE AIRCRAFT CONCEPT EXPLORATION AND FLIGHT TEST NEEDS IDENTIFICATION |
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ICAS2026_0926: N. Viola¹, R. Fusaro¹, D. Feretto¹; ¹Politecnico di Torino, Italy SUPPORTING THE REGULATORY COMMUNITY SHAPING THE FUTURE OF SUSTAINABLE HIGH-SPEED CIVIL AVIATION: THE ESATTO FRAMEWORK |
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ICAS2026_0931: B.-B. Huyssen¹, D. Fenthum¹, J. Huyssen, CSIR, South Africa; ¹University of Pretoria, South Africa INVESTIGATING A STABLE LIFTING FUSELAGE FOR A TWO SEAT SAILPLANE OF THE GULL WING CONFIGURATION |
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ICAS2026_0960: Joachim Huyssen, CSIR, South Africa; Eduard van Heerden, University of Pretoria, South Africa PROPOSING A STABLE LIFTING FUSELAGE FOR AN AIRLINER OF THE IDEAL AIRCRAFT CONFIGURATION |
2 - Systems Engineering and Integration |
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ICAS2026_0016: Y. Chen, University of New South Wales, Australia MODEL PREDICTIVE CONTROL OF HYDROGEN–ELECTRIC AIRPORT ENERGY SYSTEMS FOR SUSTAINABLE GROUND OPERATIONS |
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ICAS2026_0046: L. Knöös Franzén, Linköping University, Sweden; C. Jouannet, Saab Aeronautics, Sweden ONTOLOGY-BASED EXPLORATION OF SYSTEM-OF-SYSTEMS ARCHITECTURES USING A FEDERATED STRUCTURE |
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ICAS2026_0076: S. Malka¹, M. Ben Simon¹, O. Yakimenko¹; ¹Naval Postgraduate Shcool, United States DIGITAL TWIN FOR AIR DEFENSE: LIVE-VIRTUAL-CONSTRUCTIVE INTEGRATION AND DECISION SUPPORT |
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ICAS2026_0252: K. Joyce¹, K. Joiner¹, V. Daria, Royal Australian Air Force, Australia; J. Young¹; ¹University of New South Wales, Australia BEYOND THE HARDWARE: REGULATION AND CERTIFICATION AS THE CRITICAL PATH TO ADF AUTONOMOUS CAPABILITY |
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ICAS2026_0279: V. Voth¹, J. Wade, UCSD, United States; O. Bertram¹, A. Bierig¹; ¹German Aerospace Center (DLR), Germany LLM-ASSISTED GENERATION OF SYSML V2 MODELS FROM STRUCTURED ENGINEERING REPORTS |
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ICAS2026_0336: G. Donelli¹, P. Pantelas¹, H. Niemann², C. Özkan², C. Christen ², L. Boggero¹, B. Nagel¹; ¹DLR, Germany; ²Airbus Operation, Germany VALUE DRIVEN CO-ARCHTIECTING AND TRADESPACE EXPLORATION: AN AERONAUTICAL CASE STUDY INVOLVING INDUSTRIAL SYSTEMS |
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ICAS2026_0337: G. Donelli¹, L. Boggero¹, M. Forlingieri, PTL, Germany; ¹DLR, Germany AIRCRAFT AND INDUSTRIAL SYSTEMS CO-ARCHITECTING BASED ON VALUE-DRIVEN MBPLE APPROACH |
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ICAS2026_0399: S.M. Lübbe¹, M. Schäfer¹, O. Bertram¹, A. Bierig¹; ¹German Aerospace Center (DLR), Germany PROPAGATING SAFETY ASSESSMENT RESULTS FOR SYSTEM ARCHITECTURE CANDIDATES IN MBSE |
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ICAS2026_0479: Y.L. Ren¹, L.F. You¹, X.H. Gao¹, Z.Q. Wang¹, C.Y. Chang¹, Z.Q. Guo¹; ¹Beihang University, China AUTOMATIC GENERATION OF PHYSICAL SYSTEM MODELS FOR AIRCRAFT SYSTEMS BASED ON LLMS |
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ICAS2026_0607: C. Jouannet¹, K. Amadori¹, R. Perez, Royal Military College of Canada, Canada; E. Moerland, DLR, Germany; ¹Saab Aeronautics an Linköpings University, Sweden THE CONFERENCE LOCATIONS: A QUANTITATIVE APPROACH TO REDUCING IMPACT GLOBAL TRAVEL |
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ICAS2026_0671: P.F. Li¹, W.Z. Liu¹, B.L. Shang¹, Y.Z. Wang¹, R.X. Lin¹; ¹Northwestern Polytechnical University, China COARSE–FINE COUPLED MBSE FOR SURVIVABILITY PARAMETER DESIGN OF STEALTH CARRIER-BASED TANKER |
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ICAS2026_0674: M. Schäfer¹, S. Lübbe¹, O. Bertram¹, A. Bierig¹; ¹German Aerospace Center (DLR), Germany MODEL-BASED FUNCTIONAL HAZARD ASSESSMENT BASED ON ARP4761A USING SYSML V1 AND SYSML V2 |
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ICAS2026_0675: H. Budig¹, E. Zegarra Berodt¹, N.G. Wood¹, V. Gollnick¹; ¹Hamburg University of Technology, Germany INTERFACING MISSION SIMULATION WITH INTELLIGENT AGENTIC SYSTEMS FOR OPERATIONAL AND ETHICAL EVALUATION |
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ICAS2026_0722: L. Gómez Falcón¹, V. Montiel Viruel¹, E. Espinosa-Juárez, Linköping University, Sweden; ¹Universidad Autonoma de Baja California, Mexico TOWARDS A SYSTEM-OF-SYSTEMS ENGINEERING ROADMAP FOR INTEGRATING SUSTAINABLE AVIATION FUEL INTO MEXICO’S AIRPORT FUEL INFRASTRUCTURE |
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ICAS2026_0910: W. Cheng¹, S. Chen¹, G. Wang¹, H. Cao¹, Y. Wu¹; ¹Aviation Industry Development Research Center of China (ADR), China MODELING, SIMULATION AND EVALUATION OF LARGE FOREST FIRE EXTINGUISHING AND RESCUE BASED ON AVIATION MATERIEL |
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ICAS2026_0917: L.H.J. Machado¹, J.L.C. Reis¹, A. Zaramella, ACS Aviation / MOYA Aero, Brazil; L.G.M. Soltz¹; ¹Universidade Federal de Minas Gerais, Brazil MODEL-BASED INTEGRATION OF FLIGHT-TEST EVIDENCE AND SEMI-EMPIRICAL PERFORMANCE MODELS: THE ACS-100 SORA LIGHT AIRCRAFT CASE STUDY |
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ICAS2026_0918: A.M. Zarate Villazon¹, M. Balchanos¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States FEATURE MODEL CREATION THROUGH MISSION ANALYSIS IN THE CONTEXT OF VEHICLE FAMILIES |
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ICAS2026_0957: W. Bliemetsrieder¹, P. Panchal¹, N. Sorokina¹, S. Diecke, Ingenieurbüro Stephan Diecke, Germany; T. Weyh¹; ¹University of the Bundeswehr Munich, Germany ANALYSIS OF SOFTWARE DEVELOPMENT METHODS FOR A RECONFIGURABLE BATTERY SYSTEM FOR USE IN AN ELECTRIC AIRCRAFT |
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ICAS2026_0959: H. Rizk¹, H. Yamaguchi¹, S. Morioka², T. Inagawa²; ¹Osaka University, Japan; ²Interstellar Technologies Inc., Japan MANEUVER- AND DELAY-ROBUST DISTRIBUTED SATELLITE SSA VIA SPATIO-TEMPORAL GRAPH FORECASTING |
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ICAS2026_0966: M. Rabiega¹, C. Reynolds¹; ¹The Boeing Company, United States ENABLING HIGH RATE COMPOSITE MANUFACTURING THROUGH A ROBUST MANUFACTURING DIGITAL ECOSYSTEM |
3.1 - Aerodynamics – CFD Methods and Validation |
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ICAS2026_0043: J. Xu, China; L. Zhou, China; J. Shi, China; Z. Wang, China; H. Shi, China INVESTIGATION OF PLUME NON-EQUILIBRIUM INFRARED RADIATION CHARACTERISTICS AT DIFFERENT MACH NUMBERS |
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ICAS2026_0051: G. Dalinajara Abreu Smith Borges¹, V. Silva Figueredo¹, G.L. Olichevis Halila¹, J. Messias Magalhães Júnior, Georgia Institute of Technology, United States; J.L. F. Azevedo, Instituto Tecnológico de Aeronáutica, Brazil; ¹Pontifícia Universidade Católica do Paraná, Brazil PHYSICS-INFORMED NEURAL OPERATORS FOR DISTURBANCE FIELD PREDICTION IN NONPARALLEL BOUNDARY-LAYER STABILITY ANALYSIS |
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ICAS2026_0052: L. Rodrigues Arnaud¹, F. Maia Nunes Celestino¹, G.L. Olichevis Halila¹, J.L. F. Azevedo, Instituto Tecnológico de Aeronáutica, Brazil; ¹Pontifícia Universidade Católica do Paraná, Brazil HIGH-FIDELITY AERODYNAMIC SHAPE OPTIMIZATION OF WIND TURBINES USING A DISCRETE ADJOINT APPROACH |
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ICAS2026_0054: J. Fernández¹, R. Bardera¹, J.C. Matías¹, E. Barroso¹, A.A. Rodríguez-Sevillano, Universidad Politécnica de Madrid, Spain; ¹Instituto Nacional de Técnica Aeroespacial, Spain CFD ANALYSIS OF MMRTG THERMAL PLUME ON THE EXTERNAL AERODYNAMICS OF A MARS ROVER |
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ICAS2026_0061: G. Dessio Junior¹, G.L. Olichevis Halila¹, J. Messias Magalhães Júnior, Georgia Institute of Technology, United States; J.L. F. Azevedo, Instituto Tecnológico de Aeronáutica, Brazil; ¹Pontifícia Universidade Católica do Paraná, Brazil A MACHINE-LEARNING-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION FRAMEWORK USING FREE-FORM DEFORMATION AND DEEP NEURAL NETWORKS |
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ICAS2026_0065: G.M. Poltronieri¹, F.C. Moreira¹, J.L.F. Azevedo¹; ¹Instituto Tecnológico de Aeronáutica, Brazil A STUDY ON THE CELL REYNOLDS NUMBER AS A PARAMETER FOR MESH QUALITY ON HYPERSONIC FLOWS |
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ICAS2026_0089: D. Xue¹, Y. Gao¹, T. Wu¹, B. Song¹, W. Song¹; ¹Northwestern Polytechnical University, China OPTIMIZATION OF MORPHOLOGICAL AND KINEMATIC PARAMETER FOR FLAPPING WING IN FORWARD FLIGHT |
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ICAS2026_0105: C. Brunelli¹, M. Avirovic¹, B. Janssens¹, B.G. Marinus¹; ¹Royal Military Academy, Belgium CONTINUOUS UNSTEADY ADJOINT VARIATIONAL MULTISCALE METHOD FOR AIRFOILS SHAPE OPTIMIZATION |
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ICAS2026_0112: Z.Z. He¹, Y.F. Zhang¹; ¹Tsinghua University, China DATA-DRIVEN TURBULENCE MODELING FOR MULTI-MECHANISM SEPARATED FLOWS OVER ICED AIRFOILS |
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ICAS2026_0119: S. Shahjahan¹, E. Sirak¹, V. Ahuja¹; ¹Siemens Digital Software Industries, United States SIMULATION OF FIFTH-GENERATION HIGH-PERFORMANCE AIRCRAFT USING VISCOUS SURFACE-VORTICITY PANEL METHOD |
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ICAS2026_0120: S. Shahjahan¹, V. Ahuja¹; ¹Siemens Digital Software Industries, United States SIMULATION OF AERODYNAMIC GROUND EFFECT FOR TILTED PROPELLERS USING VISCOUS SURFACE-VORTICITY PANEL METHOD |
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ICAS2026_0168: Z.P. Zhang¹, Z.Y. Ye¹; ¹Northwestern Polytechnical University, China REYNOLDS NUMBER EFFECTS OF A BIRD-FEATHER-INSPIRED POROUS-MEDIUM AIRFOIL |
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ICAS2026_0183: M. Candon¹, T. Gerner¹, A. Das¹, Z. Hoffman¹, P. Marzocca¹, L. Munholand², V. Viti², E. H. Dowell, Duke University, United States; ¹RMIT University, Australia; ²ANSYS, United States TRANSONIC BUFFET AND STATIC AEROELASTIC RESPONSE OF A COMMERCIAL TRANSPORT AIRCRAFT |
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ICAS2026_0193: H. Wang¹, J. Wang¹, Z. Li¹, W. Yang¹, X. Yang¹; ¹Northwestern Polytechnical University, China EFFECTS OF FLAPPING–PITCHING PHASE DIFFERENCE ON THE AERODYNAMIC PERFORMANCE OF HOVERING DRAGONFLY WINGS |
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ICAS2026_0196: M. de Rosa Jacinto¹, D. Skrna¹, M. Berens¹; ¹Technische Universität Wien, Austria PREDICTION OF PROPELLER NOISE IN LOW REYNOLDS NUMBER OPERATION USING MACHINE LEARNING MODELS |
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ICAS2026_0197: D. Skrna¹, M. de Rosa Jacinto¹, M. Berens¹; ¹Technische Universität Wien, Austria INTEGRATION OF ACOUSTIC LINERS AND INTERNAL BYPASS CHANNELS INTO AAM PROPELLERS FOR NOISE REDUCTION |
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ICAS2026_0226: F. Parra¹, D. Domínguez¹, A. Delgado¹, J. Gonzalo¹; ¹Universidad de León, Spain ACCURACY AND EFFICIENCY OF TRANSITION–TURBULENCE MODELS IN PREDICTING HIGH AND LOW REYNOLDS NUMBER PROPELLER PERFORMANCE |
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ICAS2026_0238: E. Shima¹, K. Yonezawa, CRIEPI, Japan; M. Sato, Kogakuin Univ., Japan; A. Oyama¹; ¹JAXA, Japan SUPERIOR CRUISE EFFICIENCY OF A NOVEL EVTOL CONFIGURATION FEATURING INCLINED PROPELLERS AND A PARASOL WING |
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ICAS2026_0241: G. Wang¹, Z.-K. Liu¹, T.-Y. Lin¹, H.-Y. Wang¹; ¹Northwestern Polytechnical University, China AN ADAPTIVE AND PARAMETER-FREE SLOPE LIMITER FOR UNSTRUCTURED COMPRESSIBLE FLOW SOLVER |
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ICAS2026_0263: Y. Gao¹, H. Zhao¹, K. Gan¹; ¹Northwestern Polytechnical University, China EFFECTS OF FLYING WING CONFIGURATION PARAMETERS ON AERODYNAMICS AND STABILITY |
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ICAS2026_0267: P. Catalano¹, F.A. D'Aniello¹; ¹C.I.R.A., Italy LARGE EDDY SIMULATIONS OF LOW-REYNOLDS NUMBER FLOWS IN THE COMPRESSIBLE REGIME |
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ICAS2026_0280: K. You, China; R. Zhu, China; Z. Chen, China A COMPARATIVE STUDY OF THE AERODYNAMIC CHARACTERISTICS OF FOUR CONFIGURATIONS |
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ICAS2026_0281: L. Pirillo¹, R. Bianchini¹, D. Palma¹, F. Stella¹; ¹Sapienza University of Rome, Italy UNCERTAINTY QUANTIFICATION AND CROSS-CORRELATION EFFECTS IN AERODYNAMIC COEFFICIENTS DERIVED QUANTITIES |
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ICAS2026_0282: D. Palma¹, L. Pirillo¹, M. Bernardini¹, F. Stella¹; ¹Sapienza university of Rome, Italy BUFFETING SCALE EFFECTS ON A LAUNCH VEHICLE: HYBRID RANS-LES ANALYSIS |
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ICAS2026_0283: H. Mohsin¹, S.A. Prince¹, D. Di Pasquale¹; ¹Cranfield University, United Kingdom NUMERICAL BOUNDARY LAYER VALIDATION TECHNIQUE USING RAE M2155 SWEPT WING |
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ICAS2026_0352: Z.C. Su, China; P.F. Zhu, China; G.L. Li, China; C.H. Zhong, China; Y.G. Lyu, China; T.S. Xie, China HIGH-ALTITUDE PERFORMANCE AND ONE-DIMENSIONAL MODELING OF A DUAL-ROTOR GEROTOR PUMP FOR AEROENGINE LUBRICATION SYSTEMS |
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ICAS2026_0368: E. Tangermann¹, A. Jagadeesha¹, M. Klein¹; ¹Universität der Bundeswehr München, Germany LAMINAR SEPARATION ON AN AIRFOIL WITH PERTURBATION OF OUTER AND INNER BOUNDARY CONDITIONS |
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ICAS2026_0373: H.C. Yang¹, X.K. Ma¹, R.B. Zhu¹, K. You¹, Z.L. Chen¹; ¹Northwestern Polytechnical University, China EXERGY-BASED AERODYNAMIC CHARACTERISTICS ANALYSIS OF THE NASA COMMON RESEARCH MODEL AND BWB CONFIGURATION CIVIL AIRCRAFT |
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ICAS2026_0462: K. Gan¹, H. Zhao¹, S. Wang¹; ¹Northwestern Polytechnical University, China RESEARCH ON AERODYNAMIC-STEALTH INTEGRATED DESIGN METHODOLOGY BASED ON MPPO ALGORITHM |
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ICAS2026_0463: K.Y. Zhou¹, W.P. Song¹, J.H. Xu¹; ¹Northwestern Polytechnical University, China A ROTOR TRANSITION PREDICTION METHOD BASED ON GALILEAN INVARIANCE AND THE C1 CROSSFLOW TRANSITION CRITERION |
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ICAS2026_0480: H. Wang¹, T. Lin¹, G. Wang¹, L. Xu¹; ¹Northwestern Polytechnical University, China NUMERICAL STUDY ON DYNAMIC STALL OF FIGHTER AIRCRAFT AT HIGH ANGLE OF ATTACK USING DYNAMIC IMPROVED DELAYED DETACHED EDDY SIMULATION |
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ICAS2026_0488: T. Ikeda¹, K. Yasue¹, M. Kanayama, Ryoyu Systems, Japan; ¹JAXA, Japan THE NUMERICAL SIMULATIONS OF THE ACOUSTIC SHIELDING EFFECTS ON THE BLADE-VORTEX INTERACTION NOISE OF THE HART-II MODEL |
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ICAS2026_0490: Y. Fan¹, Y. Sun¹, J. Xue¹, Y. Wang¹, B. Mi¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China EXPLAINABLE KNOWLEDGE DRIVEN LLM AGENTS FOR TRUSTWORTHY AIRFOIL AERODYNAMIC OPTIMIZATION DESIGN |
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ICAS2026_0492: S. Li¹, W.P. Song¹, Z.Q. Shen¹; ¹ Northwestern Polytechnical University, China EFFICIENT ROTOR AERODYNAMIC SHAPE DESIGN USING A MULTI-FIDELITY NEURAL NETWORK-BASED GLOBAL OPTIMIZATION METHOD |
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ICAS2026_0530: M.S. Abulela¹, M.I. Alam¹; ¹King Fahd University of Petroleum and Minerals, Saudi Arabia MACHINE LEARNING-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION OF NACA AIRFOILS UNDER GEOMETRIC DESIGN CONSTRAINTS |
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ICAS2026_0550: S. Gunasekaran, Cranfield Univeristy, United Kingdom; Z.A. Rana, Prince Mohammad Bin Fahd University, Saudi Arabia; S. Prince, Cranfield University, United Kingdom NUMERICAL INVESTIGATION OF SHOCKWAVE TURBULENT BOUNDARY LAYER INTERACTION AT MACH 2.5 OVER A COMPRESSION RAMP |
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ICAS2026_0569: T. Moses¹, M. Hornung¹; ¹Technical University of Munich, Germany NOISE-OPTIMIZED HOVER PROPELLER DESIGN FOR VTOL CARGO DRONES IN TRANSIENT FLIGHT CONDITIONS |
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ICAS2026_0572: N. Montella¹, D. Quagliarella¹, L. Iuspa², A. Aprovitola², G. Pezzella², A. Viviani ²; ¹CIRA (Centro Italiano Ricerche Aerospaziali), Italy; ²University of Campania , Italy NUMERICAL REBUILDING OF AERODYNAMIC WIND TUNNEL ANALYSES OF A CREW RETURN VEHICLE |
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ICAS2026_0634: P. Kovar, Czech Technical University in Prague, Czech Republic; J. Fürst, Czech Technical University,, Czech Republic; G. Frulla¹, G.M. Di Cicca¹, E. Cestino¹; ¹Polytechnic University of Turin, Italy MORPHING TRAILING-EDGE AERODYNAMICS AND THE ROLE OF TURBULENCE MODELING |
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ICAS2026_0653: Z. Zhu¹, Y. Xi¹, S. Fu¹; ¹Tsinghua University, China HYPERSONIC RECEPTIVITY TO FREESTREAM DISTURBANCES OVER A BLUNT WEDGE: A LINEARIZED NAVIER-STOKES APPROACH |
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ICAS2026_0654: C. Paillard¹, G. Bourreau-Tirel, Aura Aero and ISAE-SUPAERO, University of Toulouse, France; S. Duplaa¹, M. Fiore¹; ¹ISAE-SUPAERO, University of Toulouse, France EPSILON V4: AN OPEN-SOURCE TOOL FOR EXTENDED AERODYNAMICS EXERGY ANALYSIS |
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ICAS2026_0693: Hassan Ali Abid, King Fahd University of Petroleum and Minerals, Saudi Arabia HIGH-FIDELITY AEROACOUSTIC AND UNSTEADY FLOW ANALYSIS OF WIND TURBINE BLADES |
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ICAS2026_0720: L. Avoni¹, M. Bronz¹, J.-M. Moschetta¹, J.-P. Condomines¹; ¹Fédération ENAC ISAE-SUPAERO ONERA, Université de Toulouse, France A STALL EXTENSION TO LIFTING-LINE THEORY: IMPLEMENTATION AND VALIDATION IN ASWING |
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ICAS2026_0747: K.R. Yang¹, B.F. Song¹, D. Xue¹; ¹Northwestern Polytechnical University, China RESEARCH ON AN AERODYNAMIC LOAD METHODOLOGY FOR FLAPPING WINGS BASED ON EXPERIMENTALLY ACQUIRED DEFORMATION |
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ICAS2026_0785: T. Chen¹, Z. Zeng¹, Y. Zhao¹, J. He¹, Y. Yang¹; ¹NorthWestern Polytechnical University, China NUMERICAL INVESTIGATION OF GUST LOAD ALLEVIATION FOR WINGS WITH PASSIVELY RELEASED FFWT |
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ICAS2026_0795: J. He¹, Y. Zhao¹, X. Wei¹, T. Chen¹, Y. Yang¹; ¹Northwestern Polytechnical University, China COMPARATIVE ANALYSIS OF DIFFERENT NUMERICAL SIMULATION METHODS FOR PROPELLER SLIPSTREAM |
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ICAS2026_0796: Y. Zhao¹, J. He¹, X. Wei¹, T. Chen¹, Y. Yang¹; ¹Northwestern Polytechnical University, China AILERON EFFICIENCY ANALYSIS OF FLEXIBLE HIGH-ASPECT-RATIO WING |
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ICAS2026_0849: P.-F. Zhu¹, T.-S. Xie¹, R.-S. Feng¹, S. Zhang¹, C. Zhang¹; ¹Northwestern Polytechnical University, China STUDY ON THE INJECTOR JETTING CHARACTERISTICS FOR VENTILATION EFFICIENCY OPTIMIZATION IN AIRCRAFT ENGINE LUBRICATION SYSTEMS |
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ICAS2026_0862: X. Li¹, L. Yang¹, Y. Wei¹; ¹Beijing Jiaotong University, China LEAKAGE PREDICTION AND GEOMETRIC PARAMETER OPTIMIZATION OF STEPPED LABYRINTH SEALS BASED ON DATA-DRIVEN SURROGATE MODELS |
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ICAS2026_0923: W. Klimczyk, Lukasiewicz Research Network - Institute of Aviation, Poland PRACTICAL ASPECTS OF ROTOR AERODYNAMIC AND AEROACOUSTIC DESIGN OPTIMIZATION |
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ICAS2026_0927: M.R. Rajanna¹, J. Lua¹, N. Phan, Naval Air System Command, United States; M.-C. Hsu, Iowa State University, United States; ¹Global Engineering and Materials, Inc., United States HIGH-FIDELITY ANALYSIS OF AIRCRAFT TAIL BUFFETING UNDER DYNAMIC MANEUVERING |
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ICAS2026_0936: J.G. Coder, Penn State University, United States OVERVIEW OF VERIFICATION AND VALIDATION EFFORTS FOR PDE-BASED LAMINAR-TURBULENT TRANSITION MODELS |
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ICAS2026_0939: T.A. Missato¹, R.G. Annes da Silva¹, A.F. de Castro da Silva¹, T. Wainwright, Zenotech, United Kingdom; ¹Instituto Tecnológico de Aeronáutica, Brazil ASSESSING VORTEX BREAKDOWN AND COUPLING IN DELTA WING PLANFORMS THROUGH HIGH-FIDELITY DDES SIMULATIONS |
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ICAS2026_0953: G.C. Ribolla¹, L.J.F. Meirelles¹, L.F.S. Gomes¹, M.B. Stergiou¹, R.M. Granzoto, Embraer, Brazil; P. Bufacchi¹; ¹Insper, Brazil COST-EFFECTIVE CFD REPRODUCTION OF DPW-7 CASE 2A FOR CRM TRANSONIC PITCHING-MOMENT PREDICTION AND ADAPTIVE-REFINEMENT ASSESSMENT |
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ICAS2026_0998: J. Slotnick, United States CFD VISION 2030 PROGRESS AND NEXT STEPS |
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ICAS2026_0999: J. Coder, United States CFD VISION 2030 LOOKING FORWARD: PANEL DISCUSSION WITH J.CODER, J.P.SLOTNICK, N.J.WYMAN, C.WINKLER |
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ICAS2026_1000: N. Wyman, United States GEOMETRY AND MESHING ADVANCEMENTS TOWARD CFD VISION 2030 |
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ICAS2026_1022: N.J. Wyman, Cadence Design Systems, Inc., United States; N. Ashton, NVIDIA, United States THE ROLE OF NEXT-GENERATION HPC AND MACHINE LEARNING IN ACHIEVING THE 2030 VISION GOALS |
3.2 - Experimental Aerodynamics |
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ICAS2026_0033: J. Li¹, Y. Yendrew¹, D. Moreau¹, C. Doolan¹; ¹University of New South Wales, Australia EXPERIMENTAL INVESTIGATION ON THE INNER DUCT SURFACE UNSTEADY PRESSURE OF A DUCTED PROPELLER |
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ICAS2026_0049: J.C. Matias¹, R. Bardera¹, E. Barroso¹, J. Fernández¹; ¹INTA, Spain WIND TUNNEL INVESTIGATION OF HELICOPTER LOADS DURING URBAN OPERATIONS ON A BUILDING WITH COLUMNAR VORTEX GENERATORS |
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ICAS2026_0133: N. Gavrilovic¹, D. Lanot¹, M. Bronz, ENAC, France; ¹ISAE-SUPAERO, France COMPARATIVE ATMOSPHERIC MEASUREMENTS USING UAV-MOUNTED ULTRASONIC ANEMOMETER AND DOPPLER LIDAR |
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ICAS2026_0151: N. Schwagerus¹, M. Stößel¹, D. Kozulovic¹; ¹University of the Bundeswehr Munich, Germany EXPERIMENTAL VALIDATION OF A COANDA-BASED FLUIDIC THRUST VECTORING NOZZLE USING A HIGH-SPEED WIND TUNNEL |
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ICAS2026_0203: D. Farcy¹, S. Prince², M. Alam², G. Tanguy¹, N. Vauchel¹, A. Proenca²; ¹ONERA, France; ²Cranfield University, United Kingdom STATIC AND DYNAMIC WIND-TUNNEL TESTING OF A TRANSPORT AIRCRAFT MODEL IN-STALL AND POST-STALL FLIGHT REGIMES |
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ICAS2026_0218: A. Kumar¹, R. Vos¹; ¹Delft University of Technology, Netherlands LOW-SPEED EXPERIMENTAL INVESTIGATION OF PODDED ENGINE INTEGRATION OF FLYING V AIRCRAFT |
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ICAS2026_0232: D. Domínguez¹, F. Parra¹, D. López¹, A. García-Gutiérrez¹; ¹Universidad de León, Spain EXPERIMENTAL INVESTIGATION OF WISHBONE VORTEX GENERATOR EFFECTS ON THE NACA 4412 AIRFOIL AT LOW REYNOLDS NUMBERS |
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ICAS2026_0256: M. Kohzai¹, M. Murayama¹, A. Sansica¹, D. Lusher¹, T. Takaishi¹, H. Abe¹; ¹Japan Aerospace Exploration Agency, Japan AERODYNAMIC CHARACTERISTICS OF 8% SCALE SEMI-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT THE JAXA 6.5M X 5.5M LOW SPEED WIND TUNNEL |
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ICAS2026_0328: T. Hashioka¹, Y. Murahashi¹, H. Yasuda¹, Y. Sawaki¹, S. Suzuki¹, W. Suzuki¹, T. Kawamura¹; ¹KHI, Japan NEW TEST RESULTS OF THE 3.23% FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL |
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ICAS2026_0347: X. Delon¹, J. Abou Khalil, ONERA - Toulouse, France; N. Maynard², A. Marouf¹, R. El Akoury³, Y. Hoarau¹, C. Doll, Onera - Toulouse, France; J.-F. Rouchon², M. Braza³; ¹ICUBE - Strasbourg, France; ²LAPLACE - Toulouse, France; ³IMFT - Toulouse, France AERODYNAMIC PERFORMANCE INCREASE OF AN A320 MORPHING WING IN SUBSONIC |
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ICAS2026_0362: A. Goerttler¹, S. Koch¹, M. Werner¹, F. Tocci¹, F. Mayer, Airbus Defence and Space GmbH, Germany; A. Wagner¹; ¹German Aerospace Center (DLR), Germany REYNOLDS NUMBER SCALING EFFECTS IN TRANSONIC CAVITY AERODYNAMICS: A HIGH-FIDELITY EXPERIMENTAL AND NUMERICAL FRAMEWORK |
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ICAS2026_0427: E. Barroso, instituto Nacional de Técnica Aeroespacial (INTA),, Spain; R. Bardera¹, J.C. Matías¹, J. Fernández¹, A.A. Rodríguez Sevillano, Universidad Politécnica de Madrid, Spain; ¹Instituto Nacional de Técnica Aeroespacial (INTA),, Spain DESIGN, MANUFACTURING, AND TESTING OF HUMPBACK WHALE-INSPIRED TUBERCLES FOR ENHANCED LOW-REYNOLDS WING PERFORMANCE. |
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ICAS2026_0428: C. Hiemcke¹, R. Buth¹, C. Schneider¹, C.J. Jones¹; ¹General Atomics Aeronautical Systems, Inc., United States METROLOGY METHODS FOR ISOLATING PROFILE FORM, WAVINESS, STEPS, AND TWIST FROM SCANS OF SMALL-SCALE LAMINAR FLOW WIND TUNNEL MODELS |
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ICAS2026_0472: K.J. Groot, University of Wyoming, United States; N.J. Porfido¹, H.L. Reed¹, J.G. Coder, Penn State University, United States; D.M. Somers, Airfoils, Incorporated, United States; ¹Texas A&M University, United States EVALUATING THE LAMINAR FLOW ON A SLOTTED, NATURAL-LAMINAR-FLOW WING IN THE NASA AMES 11-FOOT TRANSONIC WIND TUNNEL |
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ICAS2026_0517: Y. Tanhashi¹, F. Sakai¹, S. Nishizuka¹, T. Ikeda¹, N. Kishimoto, Kwansei Gakuin University, Japan; M. Tamayama, Japan Aerospace Exploration Agency, Japan; Y. Iwami², N. Tomita²; ¹Chubu University, Japan; ²Yamashina Institute for Ornithology, Japan EFFECT OF MOLTING ON THE AERODYNAMIC CHARACTERISTICS OF BLACK-TAILED GULLS |
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ICAS2026_0545: Y.X. Jia¹, H.R. Shen¹, J.M. Wu¹; ¹Xian Jiaotong University, China EFFECTS OF SLOT LOCATION ON FLOW AND HEAT TRANSFER IN A LATTICEWORK COOLING CHANNEL: AN MRV EXPERIMENT AND NUMERICAL STUDY |
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ICAS2026_0592: H. Mohsin¹, S.A. Prince¹, D. Di Pasquale¹; ¹Cranfield University, United Kingdom PROPOSAL FOR DISTINGUISHING USABLE DATA UNDER HIGH WIND TUNNEL BLOCKAGE USING AN RAE2822 TEST CASE |
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ICAS2026_0705: T. Piovesan¹, A. Giannouloudis¹, J. Hueso Rebassa¹, M. Migliorini¹, P. Zachos¹, D. MacManus¹; ¹Cranfield University, United Kingdom MIDAS: A MODULAR SOFTWARE FOR INTAKE FLOW DISTORTION ANALYSIS |
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ICAS2026_0730: A. Sumi¹, S. Otomo¹, H. Nishida¹; ¹Tokyo University of Agriculture and Technology, Japan EXPERIMENTAL STUDY OF LOAD ALLEVIATION WITH PASSIVE ADAPTIVE CAMBER AIRFOILS |
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ICAS2026_0743: S. Montoya-Ospina¹, R. Gojon¹, H. Parisot-Dupuis¹, F. Simon, DMPE-ONERA, France; ¹ISAE-SUPAERO, France STUDY OF THE FEASIBILITY OF ACOUSTIC LINERS INSIDE THE BEAM THAT INTERACTS WITH A UAV DRONE ROTOR |
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ICAS2026_0748: J. McCarthy¹, C. Marshall¹, C. Brown, RMIT University, Australia; M. Jones¹; ¹Defence Science and Technology Group, Australia INTERMITTENT LOW FREQUENCY EXPERIMENTAL CAVITY DYNAMICS |
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ICAS2026_0749: C. Marshall¹, N. Heath², D. Handford², J. Smith², P. Manovski¹, T. Avadiar¹, M. Jones¹, A. Neely²; ¹Defence Science and Technology Group, Australia; ²University of New South Wales, Australia CONCURRENT UNSTEADY SURFACE PRESSURE FIELD AND SCHLIEREN MEASUREMENTS OF THE COMMON FRONT END HYPERSONIC GEOMETRY IN TRANSONIC CONDITIONS |
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ICAS2026_0756: M. Murayama¹, Y. Murata¹, M. Kohzai¹, K. Yamamoto¹, Y. Ito¹, H. Ura¹, T. Takaishi¹; ¹Japan Aerospace Exploration Agency, Japan AEROACOUSTIC WIND TUNNEL TESTING AND CFD STUDY USING JAXA 8% SEMISPAN HIGH-LIFT COMMON RESEARCH MODEL IN JAXA FQUROH-2 PROJECT |
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ICAS2026_0763: L. Malicki¹, M. Marciniuk¹, L. Kiszkowiak², P. Piskur, Polish Naval Academy of the Heroes of Westerplatte, Poland; S. Kachel²; ¹Wroclaw University of Science and Technology, Poland; ²Military University of Technology, Poland WATER TUNNEL EXPERIMENTS AND CFD ANALYSES OF A COMBAT AIRCRAFT WITH LEADING-EDGE VORTEX CONTROLLERS |
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ICAS2026_0775: D.T. Rajeepan¹, N.J. Lawson¹, A. Galffy, Turbulence Solutions, Austria; ¹University of Sydney, Australia ANALYSIS OF A DUAL AIR DATA AND MULTI-HOLE PRESSURE PROBE BOOM |
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ICAS2026_0789: M. Marciniuk¹, M. Szumski², Z. Szczerba², L. Kiszkowiak³, L. Malicki¹, P. Piskur, Polish Naval Academy of the Heroes of Westerplatte, Poland; K. Sibilski, Air Force Institute of Technology, Poland; S. Kachel³; ¹Wroclaw University of Science and Technology, Poland; ²Rzeszow University of Technology, Poland; ³Military University of Technology, Poland EVALUATION OF MORPHOUS WING CHARACTERISTICS IN WATER AND WIND TUNNEL IN THE CONTEXT OF UAV OPERATIONAL FLEXIBILITY |
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ICAS2026_0790: C. Brown, RMIT university, Australia; J. McCarthy¹, C. Marshall¹, M. Jones¹, I. Maatz, Air Force Research Laboratory (AFRL), United States; ¹Defence Science and Technology Group (DSTG), Australia FORCE RECONSTRUCTION TECHNIQUES FOR DYNAMIC LOAD ESTIMATION ON GENERIC GEOMETRIES IN LOW-SPEED WIND TUNNEL TESTING |
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ICAS2026_0793: V.C.B. Sousa¹, E. Sozer², K. Ravikumar¹, S.S. Hosseini², J. Duensing²; ¹Analytical Mechanics Associates, United States; ²NASA, United States A COMPARATIVE WMLES STUDY OF THE CRM-HL IN FREE-AIR AND IN THE NTF FACILITY |
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ICAS2026_0804: N. Pradyumna¹, M. Li¹, D. Verstraete¹; ¹The University of Sydney, Australia TOROIDAL RECIRCULATION, SADDLE-POINT TOPOLOGY, AND WALL-JET OUTWASH IN A TWIN-ROTOR SYSTEM IN GROUND EFFECT |
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ICAS2026_0828: I. Peleshok¹, M. Hornung¹; ¹Technical University of Munich, Germany PHASE-SPECIFIC SEMI-EMPIRICAL AEROACOUSTIC NOISE MODELING OF A CARGO EVTOL UAV WITH CONSIDERATION OF A SIMPLIFIED URBAN FLYOVER CASE |
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ICAS2026_0844: C.S. Winski¹, M. Rivers¹, S.S. Hosseini¹; ¹NASA, United States CROSS-TEST COMPARISONS AND REYNOLDS NUMBER EFFECTS IN THE CRM-HL ECOSYSTEM |
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ICAS2026_0896: S. Min¹, D. Di Pasquale¹, H. Moshin¹, A. Vincent¹, S. Prince¹, D. MacManus¹; ¹Cranfield University, United Kingdom MODELLING SENSITIVITIES IN THREE-DIMENSIONAL FZRA-SPECTRUM ICE-SHAPE PREDICTION FOR THE CRM-HL STOWED CONFIGURATION |
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ICAS2026_0970: M. Li¹, M.A. Legovich, Cranfield University, United Kingdom; N.J. Lawson¹; ¹The University of Sydney, Australia EXPERIMENTAL STUDY OF GROUND EFFECT ON A HEAVING NACA0012 AEROFOIL |
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ICAS2026_0977: S. Prince¹, D. MacManus¹, D. Di Pasquale¹, A. Vincent¹, A. Sharma¹, S. Daniels¹, K.K. Hood, The Boeing Company, United States; M.B. Rivers², C.S. Winski², T.A. Ozoroski, NASA Glenn Research Center, United States; P. White³, J. Brown³, S. Gates*, M. Schulz*, C. Jux*, H. Quix*, G. Dietz*; ¹Cranfield University, United Kingdom; ²NASA Langley Research Center, United States; ³Airbus, United Kingdom; *European Transonic Windtunnel, Germany ICING EFFECT EXPERIMENTS ON THE NASA HIGH-LIFT COMMON RESEARCH MODEL |
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ICAS2026_1082: S. Mazharmanesh¹, J. Weightman¹, P.A.S. Nogueira¹, D. Edgington-Mitchell¹; ¹Monash University, Australia MECHANISMS OF SCREECH MODE STAGING IN UNDEREXPANDED SUPERSONIC JETS |
3.3 - Basic Fluid Dynamics and Flow Control |
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ICAS2026_0070: M. Dong, Institute of Mechanics, Chinese Academy of Sciences, China; L. Zhao, Departiment of Mechanics, Tianjin University, China RECEPTIVITY OF NON-MODAL STREAKS IN HYPERSONIC BLUNT BOUNDARY LAYERS: FROM NUMERICS TO ASYMPTOTICS |
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ICAS2026_0094: G. Jiang¹, M. Dong¹; ¹Institute of Mechanics, Chinese Academy of Sciences, China ORIGIN OF TRANSIENT TURBULENT SPOTS IN HYPERSONIC SWEPT BOUNDARY LAYERS WITH MORPHING SWEEP ANGLES |
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ICAS2026_0185: Y. Mou¹, Y. Wu¹, T. Liu², D. Li², Y. Xiang¹, H. Liu¹; ¹School of Aero. & Astro., Shanghai Jiao Tong Univ., China; ²COMAC Shanghai Aircraft Design and Research Institute, China PHYSICAL DESIGN CONCEPTS OF VORTEX GENERATOR ARRAYS FOR AIRCRAFT AFT-BODIES DRIVEN BY DISTINCT DRAG REDUCTION MECHANISMS |
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ICAS2026_0194: Y. Wu¹, Z. Xiao¹, Y. Xiang¹, Z.Y. Zhu¹; ¹Shanghai Jiao Tong University, China RESPONSE CHARACTERISTICS OF WINGTIP VORTEX INSTABILITY TO EXTERNAL DISTURBANCES |
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ICAS2026_0228: Z. Hoffman¹, S. Vahaji¹, A. Das¹, M. Candon¹, N. Jayarathne, Navantia Australia, Australia; P. Marzocca¹; ¹RMIT, Australia NON-LINEAR PARAMETRIC MODEL FOR THE 3DOF MOTION OF A BOX IN WAVES USING SPARSE REGRESSION |
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ICAS2026_0255: L. He¹, F. Chen¹, Y. Wei¹; ¹Shanghai Jiao Tong University, China ACTIVE FLOW CONTROL AND THERMAL PROTECTION FOR A WING-BODY CONFIGURATION BASED ON LATERAL JET |
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ICAS2026_0311: H. Shi¹, C. Song¹, H. Xiao¹; ¹Northwestern Polytechnical University, China NUMERICAL SIMULATION OF HYPERSONIC PLASMA FLOW BASED ON NONLINEAR COUPLED CONSTITUTIVE RELATIONS |
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ICAS2026_0374: A. Jürisson¹, P.H.L. Blom¹; ¹Royal Netherlands Aerospace Centre, Netherlands REDUCED-ORDER MODELLING OF MINI-TAB SPOILER DYNAMICS FOR GUST LOAD ALLEVIATION |
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ICAS2026_0637: J. Mourad¹, V. Ferrand¹, E. Gowree¹; ¹ISAE-Supaero, France THIN AEROFOILS OSCILLATING IN A CONFINED INVISCID FLOW |
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ICAS2026_0655: B. Anilir¹, D.F. Kurtulus¹, M.F. Platzer, University of California, Davis, United States; ¹Middle East Technical University, Turkey INTERACTION OF COUNTER-PLUNGING BIPLANE AIRFOILS WITH A FLAT PLATE BOUNDARY LAYER AND WAKE |
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ICAS2026_0781: X.W. Chen¹, M.S. He¹, B. Yu¹, W. Wang¹, H. Liu¹; ¹Shanghai Jiao Tong University, China AFTERBODY CURVATURE EFFECTS ON FLOW LOSS CHARACTERISTICS BASED ON ENTROPY PRODUCTION |
3.4 - Applied Aerodynamics |
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ICAS2026_0047: N. van Luijk¹, A. van Meenen¹, R. Vos¹; ¹Delft University of Technology, Netherlands VORTEX FLOW CONTROL USING JUNCTURE FILLETS ON A BLUNT-NOSED, CRANKED SWEPT WING |
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ICAS2026_0066: N. Saadeh¹, D.W. Zingg¹; ¹University of Toronto, Canada SWEEP ANGLE STUDY OF A STRUT-BRACED-WING REGIONAL JET WITH NATURAL LAMINAR FLOW |
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ICAS2026_0087: F. Husain¹, D.W. Zingg¹; ¹University of Toronto Institute for Aerospace Studies, Canada AERODYNAMIC SHAPE OPTIMIZATION OF INFINITE SWEPT WINGS FOR NATURAL LAMINAR FLOW AT TRANSONIC CRUISE CONDITIONS |
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ICAS2026_0108: B.-M. Xu¹, K.-L. Wang¹, Z. Zhou¹, S.-K. Li¹; ¹School of Aeronautics, Northwestern Polytechnical University, China INVESTIGATION OF DISTRIBUTED PROPELLER PROPULSIVE CHARACTERISTICS UNDER NON-AXIAL INFLOW |
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ICAS2026_0122: J. Wang¹, Z. Zhou¹, K. Wang¹, M. Li¹; ¹Northwestern Polytechnical University, China AERODYNAMIC OPTIMIZATION DESIGN OF FULL-WING SOLAR-POWERED UAV FOR FLOW SEPARATION CONTROL |
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ICAS2026_0147: X. Xu¹, W. Yang¹, J. Xuan¹; ¹Northwestern Polytechnical University, China STUDY ON AERODYNAMICS OF THE WING WITH FLAP INSPIRED FROM BIRD COVERTS |
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ICAS2026_0162: M.A. Mwasandube¹, M. Marino¹, J.L. Palmer¹; ¹RMIT University, Australia VORTEX TOPOLOGY AND CORE-UNWINDING MECHANISM IN SPIROID WINGTIP DEVICES USING LAGRANGIAN PARTICLE TRACKING |
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ICAS2026_0171: K. Qiao, China; D. Wei, China; L. Han, China; Z. Chen, China; Z. Yan, China; Y. Qin, China; G. Xu, China; H. Tang, China FLUTTER FEATURES AND AERODYNAMIC DAMPING CALCULATION METHODS FOR PLATE-HEAT EXCHANGERS IN HIGH-SPEED TURBINE ENGINES |
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ICAS2026_0182: S.S. Cao¹, W.Q. Yang¹, Y.G. Zhang¹, X.L. Xu¹; ¹Northwestern Polytechnical University, China INVESTIGATION ON THE HIGH-EFFICIENCY PROPULSION MECHANISMS OF DUCK-WEBBED PADDLING FOR BIOINSPIRED AIRCRAFT APPLICATIONS |
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ICAS2026_0184: J. Liu¹, W. Yang¹, Y. Guo¹, Y. Zhang¹; ¹Northwestern Polytechnical University, China AERODYNAMIC PERFORMANCE ANALYSIS OF A NOVEL LIFT-THRUST INTEGRATED ROTARY FLAPPING AERIAL VEHICLE |
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ICAS2026_0200: M. Li¹, Z. Zhou¹, K. Wang¹; ¹Northwestern Polytechnical University, China EFFECT OF LIP/NOZZLE DEFLECTION ANGLE ON THE AERODYNAMIC AND PROPULSIVE CHARACTERISTICS OF PROPULSIVE WING UNIT |
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ICAS2026_0221: M. Avirovic¹, C. Brunelli¹, B.G. Marinus¹, J. Degroote, University of Ghent, Belgium; J. van Beeck, von Karman Insititute for Fluid Dynamics , Belgium; E. Van Vaerenbergh¹; ¹Royal Military Academy, Belgium INFLUENCE OF ZIGZAG TAPE–INDUCED TRANSITION ON THE DU89-134 AIRFOIL PERFORMANCE AT LOW REYNOLDS NUMBER |
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ICAS2026_0223: D. Losada Costoso¹, O. Atinault¹, M. Meheut¹, G. Starck¹, E. Stragiotti¹, E. Nguyen Van¹; ¹ONERA, France AERODYNAMIC TRANSONIC DESIGN OF A STRUT-BRACED WING |
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ICAS2026_0235: S.K. Wang¹, H. Zhao¹; ¹Northwestern Polytechnical University, China SPARSE POLYNOMIAL CHAOS-BASED ROBUST OPTIMIZATION DESIGN OF AERODYNAMIC AND SONIC BOOM |
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ICAS2026_0242: H. Yan¹, H. Zheng¹, Z. Dong¹, W. Dong¹; ¹Shanghai Jiao Tong University, China NUMERICAL SIMULATION OF SUPERCOOLED LARGE DROPLET IMPINGEMENT ON ROTATING FAN BLADES |
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ICAS2026_0269: Z. Zhang¹, H. Zhao¹, W. Zhang¹, J. He¹, Z. Gao¹; ¹Northwestern Polytechnical University, China FLIGHT-TEST DATA-DRIVEN HIGH-ANGLE-OF-ATTACK DYNAMICS MODELING VIA LSTM-POLYNOMIAL HYBRID APPROACH |
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ICAS2026_0284: A. Petrillo¹, D. Palma¹, L. Pirillo¹, P.P. Ciottoli¹, M. Bernardini¹, F. Stella¹; ¹Sapienza university of Rome, Italy MULTI-OBJECTIVE SHAPE OPTIMIZATION OF A LAUNCH VEHICLE FAIRING ACROSS MULTIPLE FLOW REGIMES |
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ICAS2026_0295: C. Zheng¹, Q. Qu¹, P. Liu¹, T. Hu¹; ¹Beihang University, China STATIC GROUND EFFECT OF HIGH-ASPECT-RATIO WINGS |
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ICAS2026_0297: B. Li, China; X. Zhu, China; Z. Zhou, China; M. Li, China; R. Wang, China DATA-DRIVEN AERODYNAMIC MODEL OF THE DISTRIBUTED PROPULSION WING |
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ICAS2026_0318: P. Kirschnek¹, S. Lesak¹, A. Tramposch¹; ¹FH JOANNEUM, Austria AERODYNAMIC AND STABILITY-DRIVEN PRE-DESIGN OF A FUEL-CELL POWERED FLYING WING AIRCRAFT |
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ICAS2026_0330: K. Kania, Warsaw University of Technology, Poland STUDY ON THE IMPACT OF TRIM CONDITION ON LATERAL AND DIRECTIONAL STABILITY FOR A TAILLESS AIRCRAFT |
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ICAS2026_0339: Z.Y. Dong, China; H.R. Zheng, China; H. Yan, China; P.Y. Wang, China; W. Dong, China JET-INDUCED SWIRLING FLOW AND WALL HEAT TRANSFER FOR AERO-ENGINE NACELLE SWIRL ANTI-ICING SYSTEM |
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ICAS2026_0358: A. Goerttler¹, D. Hines¹, A. Wagner¹; ¹German Aerospace Center (DLR), Germany A GRAPH NEURAL NETWORK SIMULATOR FOR TRANSONIC VORTEX-DOMINATED FLOWS ON THE DLR-F23 CONFIGURATION |
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ICAS2026_0378: G. Bourreau-Tirel¹, S. Duplaa, ISAE-SUPAERO, France; J.P. Ruscio¹; ¹Aura Aero, France EXERGY AND INTEGRAL BOUNDARY LAYER PARAMETERS CHARACTERISTIC CURVES FOR AERODYNAMIC DESIGN AND OPTIMIZATION |
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ICAS2026_0392: J. Guo¹, Y. Sun¹; ¹Cranfield University, United Kingdom UNCONTROLLED TAILLESS GLIDING: PAPER AEROPLANES GEOMETRY, AERODYNAMICS AND FLIGHT DURATION ANALYSIS |
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ICAS2026_0444: S. Montagner¹, J. Serpieri¹, G. Cafiero¹; ¹Politecnico di Torino, Italy PROPELLER AERODYNAMICS UNDER NON-UNIFORM INFLOWS |
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ICAS2026_0456: F. Kuci¹, N. Railean¹, P. Kantzidis², P. Marzocca², V. Muscarello²; ¹Polytechnic University of Turin, Italy; ²Royal Melbourne Institute of Technology, Australia GROUND-EFFECT ANALYSIS OF SMALL DUCTED PROPELLERS: A NUMERICAL–EXPERIMENTAL STUDY |
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ICAS2026_0473: W.-F. Zhang¹, H. Zhao¹, S.-K. Wang¹; ¹Northwestern Polytechnical University, China MULTI-SCALE LINEAR FEATURE MODULATION DEEP NEURAL OPERATOR FOR RAPID PRESSURE COEFFICIENT PREDICTION |
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ICAS2026_0501: Q. Chen¹, Z.-H. Han¹, K.-S. Zhang¹, K. Song¹; ¹Northwestern Polytechnical University, China AIRFRAME-INLET INTEGRATION DESIGN FOR AN OVER-WING-MOUNTED SUPERSONIC TRANSPORT CONFIGURATION |
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ICAS2026_0502: Y. Gan¹, H. Zhao¹, S. Wang¹; ¹Northwestern Polytechnical University, China SUPERVISED DIMENSIONALITY-REDUCED MULTI-FIDELITY SURROGATE MODEL ASSISTED HIGH-DIMENSIONAL NATURAL LAMINAR FLOW OPTIMIZATION |
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ICAS2026_0516: H.-X. He¹, W.-P. Song¹, Y. Wang¹, Y.-H. Wang¹, Y.-J. Shi, China Ship Scientific Research Center, China; ¹Northwestern Polytechnical University, China EFFECTS OF DISTRIBUTED PROPELLER PLACEMENT ON LIFT ENHANCEMENT OF A HIGH-LIFT CONFIGURATION |
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ICAS2026_0542: Y.C. Liu, China; B. Song, China; L. Zhou, China AERODYNAMIC EFFECT OF PITCHING MOTION FOR FLAPPING AIRFOIL ACROSS DIFFERENT SWEEPING TRAJECTORIES |
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ICAS2026_0546: P. Scavella¹, G. Paolillo¹, C.S. Greco¹; ¹University Of Naples Federico II, Italy AIRFOIL DESIGN OPTIMIZATION FOR HIGH-LIFT AND HIGH-EFFICIENCY APPLICATIONS USING DEEP REINFORCEMENT LEARNING |
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ICAS2026_0598: Y.Y. Xun¹, Q.L. Qu¹, P.Q. Liu¹; ¹Beihang University, China SUPERSONIC GROUND EFFECT AERODYNAMICS OF A SLENDER BODY |
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ICAS2026_0632: M.A. Escudero¹, B.G. Marinus, Royal Military Academy, Belgium; K. Depuru-Mohan¹; ¹Cranfield University, United Kingdom FLOW SOLUTIONS AROUND VON KÁRMÁN OGIVES AT SUPERSONIC SPEEDS USING PHYSICS-INFORMED NEURAL NETWORKS AND PSP |
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ICAS2026_0665: M. Krasniqi¹, S.F. Armanini¹; ¹Imperial College London, United Kingdom AERODYNAMIC OPTIMISATION OF BIOINSPIRED CORRUGATED WINGS FOR HIGH-EFFICIENCY MAV GLIDING |
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ICAS2026_0723: J.J. Whittaker, University of New South Wales, Australia PARAMETRIC AERODYNAMIC STUDY OF LEADING-EDGE SERRATIONS ON WING SECTIONS ACROSS REYNOLDS NUMBERS |
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ICAS2026_0759: M.J. Ericksen¹, N.J. Lawson¹; ¹The University of Sydney, Australia NUMERICAL CHARACTERISATION OF SHIP-AIRWAKE EFFECTS ON MEDIUM-WEIGHT UAV APPROACH AND GO-AROUND OPERATIONS TO CANBERRA-CLASS LHDS |
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ICAS2026_0767: D. Sasaki¹, C. Yuma¹, Y. Kawamoto¹, M. Okamoto, Kanazawa Institute of Technology, Japan; H. Nagai, Institute of Fluid Science, Tohoku University, Japan; ¹Osaka Metropolitan University, Japan UNSTEADY AERODYNAMIC OPTIMIZATION OF A THIN ANGULAR AIRFOIL USING CARTESIAN MESH CFD WITH THE LEVEL SET METHOD |
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ICAS2026_0777: H.-H. Yang¹, S.-G. Lee¹, E.-H. Lee¹, H.-S. Ko¹, J.-H. Han¹; ¹Korea Advanced Institude of Science and Technology, South Korea AERO-MECHANICAL ANALYSIS OF A BIRD-INSPIRED ORNITHOPTER USING AN INTEGRATED SIMULATION FRAMEWORK |
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ICAS2026_0841: H. Iijima¹, Y. Iijima¹, N. Tokugawa¹; ¹JAXA, Japan DEVELOPMENT OF HYDROPHILIC COATINGS FOR PRACTICAL APPLICATION OF LAMINAR FLOW WINGS |
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ICAS2026_0866: B.I. Soemarwoto, Royal Netherlands Aerospace Centre NLR, Netherlands AERODYNAMIC FEASIBILITY OF A NOVEL SWIVEL ROTOR ARCHITECTURE |
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ICAS2026_0916: B. Anilir¹, D.F. Kurtulus¹, M.F. Platzer, University of California, Davis, United States; ¹Middle East Technical University, Turkey THREE-DIMENSIONAL FLOW STRUCTURES OVER A LOW-ASPECT-RATIO PLUNGING WING |
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ICAS2026_0934: A. Heletkanycz¹, C.J. Axten¹, J.G. Coder¹; ¹Penn State University, United States MULTIPOINT INVERSE DESIGN FOR TRANSONIC, SLOTTED, NATURAL-LAMINAR-FLOW WINGS |
4.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance |
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ICAS2026_0036: S.A. Brown¹, P. Sangkarat¹, Z. Sha, Western Sydney University, Australia; C.-H. Wang¹; ¹University of New South Wales, Australia DEVELOPMENT OF CONDUCTIVE COMPOSITE MATERIALS FOR HIGH VOLTAGE APPLICATIONS |
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ICAS2026_0053: G.C. Cristea¹, M. Pop¹, A. Stefan¹, M. Botan¹, A. Dragomirescu¹; ¹INCAS, Romania ARCHITECTED LATTICE SANDWICH STRUCTURES FOR LIGHTWEIGHT IMPACT AND ENERGY ABSORPTION APPLICATIONS |
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ICAS2026_0071: C.Y. Yang¹, R. Zhao¹, Y.S. Gu¹, Z.C. Yang¹; ¹Northwestern Polytechnical University School of Aeronautics, China GEOMETRICALLY EXACT MODEL OF CANTILEVER BEAM UNDERGOING LARGE DEFLECTION AND LINEARIZED DYNAMICS CHARACTERIZATION |
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ICAS2026_0082: R.B. Ma¹, C.Y. Wang¹, X.M. Chen, Aircraft Strength Research Institute of China, China; W.Z. Wang¹; ¹Northwestern Polytechnical University, China COMPRESSIVE PERFORMANCE OF VARIABLE-STIFFNESS COMPOSITE HYPERBOLIC STIFFENED PANELS BASED ON GEOMETRIC PATH MAPPING |
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ICAS2026_0083: X. Yao¹, Y. Wang¹, H. Wang¹, Y. Wang¹; ¹Northwestern Polytechnical University, China MULTIPHYSICS COUPLING EFFECT ON INTERFACIAL PROPERTIES OF CNT/GFRP/CFRP COMPOSITES FOR ELECTROTHERMAL ANTI-/DE-ICING APPLICATIONS |
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ICAS2026_0115: Y.C. Roth, Airtbus Operations GmbH, Germany; P. Joern, Airbus Operations GmbH, Germany; A. Sadelfeld, Airbus Aerostructures GmbH, Germany; C. Rowedder, CTC GmbH, Germany; J. Buck, CTC GmbH, Germany; B. Demel, Airbus Helicopters Deutschland GmbH, Germany COMPOSITE FUSELAGE TECHNOLOGIES FOR NEXT GENERATION COMMERCIAL AIRCRAFT |
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ICAS2026_0127: X. Zhang¹, D. Wei¹, S. Yang¹; ¹Beihang University School of Energy and Power Engineering, China EXPERIMENTAL INVESTIGATION OF FRETTING WEAR IN TI-6AL-4V DOVETAIL ASSEMBLIES UNDER RESONANT VIBRATION |
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ICAS2026_0160: J. Reiner, Deakin University, Australia; R. Vaziri, The University of British Columbia, Canada EFFICIENT SIMULATION AND UNCERTAINTY QUANTIFICATION OF PROGRESSIVE CRUSHING IN COMPOSITE LAMINATES |
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ICAS2026_0172: X. Liu¹, D.S. Wei¹, S.Z. Jin, AVIC Manufacturing Technology Institute, China; S. Yang¹, D.X. Yin², B. Niakate², D. Lasne²; ¹Beihang university, China; ²BSS Turbotech Ltd., China FRACTURE AND GRAIN BOUNDARY DAMAGE IN AM NI-BASED SUPERALLOYS UNDER HIGH-TEMPERATURE TENSILE LOADING |
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ICAS2026_0181: R. Degenhardt, DLR, Italy; F. Ferrigno, CIRA, Italy; A. Gliszczynski, Lodz University of Technology, Poland; A.-L. Delot, ONERA, France INTERNATIONAL AND EUROPEAN RESEARCH AND TECHNOLOGY INFRASTRUCTURE DATA BASES IN AVIATION |
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ICAS2026_0225: C. Pagwiwoko¹, K. Warnakula¹, M. Silla¹, C. Barber¹, T. Hallwright¹, O. Kaleagasi¹, D. Schoemaker, Gyro Technic Inc., United States; ¹SYOS Aerospace, New Zealand DESIGN ASSESSMENT OF A HELICOPTER BLADE |
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ICAS2026_0234: I. Field¹, J. Rogers, RMIT, Australia; N. Tugwell¹; ¹DSTG, Australia NEW INSIGHTS INTO AA7085 ENVIRONMENTALLY ASSISTED CRACKING THROUGH HIGH RESOLUTION FRACTOGRAPHY |
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ICAS2026_0250: J. Rodrigues¹, M. Pelosi², W. Foster², S. Barter¹, R. Das¹; ¹RMIT University, Australia; ²DSTG, Australia DETECTION OF SURFACE DISCONTINUITIES IN ADDITIVELY MANUFACTURED ALSI10MG USING THERMOELASTIC STRESS ANALYSIS |
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ICAS2026_0253: N. Tugwell¹, M. Salagaras¹, J. Rogers, RMIT, Australia; ¹DSTG, Australia LABORATORY METHOD FOR REPLICATING FASTENER HOLE CORROSION IN AA7085 |
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ICAS2026_0276: G. Chen¹, L. Yao¹, B. Li¹, X. Tong¹; ¹Northwestern Polytechnical University, China NUMERICAL SIMULATION OF STRESS-OXIDATION DAMAGE IN C/SIC COMPOSITES AT HIGH TEMPERATURES |
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ICAS2026_0313: A. Gliszczynski, Lodz University of Technology, Poland; R. Degenhardt¹, F. Franzoni¹, T.D. Baciu, PFH, Germany; ¹DLR, Germany ADVANCES IN NON-DESTRUCTIVE BUCKLING PREDICTION OF THIN-WALLED STRUCTURES BY VIBRATIONS |
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ICAS2026_0351: S.H. Vattathurvalappil, King Fahd University of Petroleum and Minerals, Saudi Arabia ELECTROMAGNETISM FOR SMART MANUFACTURING OF POLYMER COMPOSITES |
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ICAS2026_0357: A.M. Caporale¹, G. Janszen¹, A.S. Jambhulkar¹, M. Ursic², A. Tasca², R. Passoni², A. Airoldi¹; ¹Politecnico di Milano, Italy; ²Brembo N.V., Italy IMPACT TOLERANCE OF DRILLED THICK C/SIC CERAMIC MATRIX COMPOSITES |
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ICAS2026_0365: H Park¹, D Lee¹, M Seok¹, H Choi¹, Y Kwon¹; ¹Korea Institute of Materials Science, South Korea FEASIBILITY OF ELECTROPULSING-INDUCED FATIGUE CRACK CLOSURE IN AEROSPACE METALLIC MATERIALS |
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ICAS2026_0493: Z. Li¹, D. Wei¹, W. Zeng, Chinese Academy of Sciences, China; K.K. Alynur¹, X. Liu¹, B. Zhao¹, S. Li¹, L. Ma, KUCH ENERGY Technology Co., Ltd., China; S. Yang¹; ¹Beihang University, China MODELING CREEP DEFORMATION AND PREDICTING RUPTURE LIFE OF STRESS-CONCENTRATED DZ411 SUPERALLOY COMPONENTS USING A THREE-STAGE CREEP FRAMEWORK |
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ICAS2026_0499: C. Koutsambasis¹, M. Marino¹, N.J. Brown¹, W. Wu¹; ¹RMIT University, Australia FLYING BY THE THREAD OF MY PANTS: USING HOUSEHOLD TEXTILES COMPOSITES FOR ACCESSIBLE UAV AIRFRAMES |
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ICAS2026_0507: M. Davids, HH Industries, University of Cape Town, South Africa; J. Strauss¹, D. Hagedorn-Hansen¹, T.H. Becker, University of Cape Town, South Africa; ¹HH Industries, South Africa LASER SCANNING STRATEGIES TO INVESTIGATE THE EFFECTS OF OXIDATION IN PURE TANTALUM |
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ICAS2026_0640: S. Stekovic¹, P. Krus¹; ¹Linköping University, Sweden TRACING MATERIAL PROPERTIES TO SYSTEM-LEVEL PERFORMANCE: A NORMALISED SENSITIVITY ANALYSIS FOR A BOEING 737-CLASS AIRCRAFT |
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ICAS2026_0776: J. Heo¹, J. Lee¹, A.-A. Reynolds¹, J. Cho¹, J.-H. Han¹; ¹KAIST, South Korea EXPERIMENTAL INVESTIGATION OF BLOWING RATIO EFFECT ON FLOW REGIMES OF TRANSPIRATION COOLING IN LATTICE POROUS MEDIA |
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ICAS2026_0830: T. Moran¹, I. Grothe¹, C. King, United States Air Force, United States; L. Hunt¹, P. Clark¹; ¹Southwest Research Institute, United States FIVE DEACADES OF T-38 WING TEARDOWNS: DATA, INSIGHT, AND IMPACT |
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ICAS2026_0861: H.R. Spratling¹, M.E. Ibrahim¹; ¹Defence Science and Technology Group, Australia ULTRASONIC NON-DESTRUCTIVE TESTING: SYSTEM SELECTION FOR CHARACTERISATION AND DETECTION OF DEFECTS IN REPAIRED COMPOSITE MATERIALS |
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ICAS2026_0868: M. Bhasin¹, A.P. Mouritz¹; ¹RMIT University, Australia ENHANCEMENT AND DEGRADATION: THE DUAL ROLE OF GRAPHENE NANOPLATELETS ON THE STRUCTURAL PERFORMANCE OF COMPOSITE T-JOINTS AND MECHANISTIC INSIGHTS |
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ICAS2026_0930: D. Cardone¹, R. Cavallaro, Barcelona Supercomputing Center, Spain; A. Cini¹; ¹Universidad Carlos III de Madrid, Spain HIERARCHICAL HIGH-ORDER BEAM MODELS FOR OPTIMISATION-ORIENTED ANALYSIS OF COMPOSITE WING-LIKE STRUCTURES |
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ICAS2026_0940: J. Lua¹, M.R. Rajanna¹, H. Yu, Virginia Tech, United States; A. Timmons², G. Murray², N. Phan²; ¹Global Engineering and Materials, Inc., United States; ²Naval Air Systems Command, United States A PROCESS-STRUCTURE-PROPERTY-PERFORMANCE FRAMEWORK FOR DIGITAL ENGINEERING-ENABLED REPAIR OF ALUMINUM PARTS |
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ICAS2026_0943: C.D. Scott¹, A.M. Comer¹, J.C. Hanan¹, A. Nunley¹; ¹Oklahoma State University, United States OPTIMIZATION OF INTERCONNECTED 3D-PRINTED STRUCTURES FOR UAVS |
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ICAS2026_1100: J. Bayandor, United States PROGRESSIVE FAILURE TIMELINE RECOUNT OF AN ATMOSPHERIC REENTRY TRAGEDY - IN MEMORY OF STS-107 CREW, AND DR. FRANK ABDI |
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ICAS2026_1111: N. Sawalhi¹, W. Wang¹; ¹Platforms Division, Defence Science and Technology Group (DSTG),, Australia CYCLOSTATIONARY ANALYSIS AND UNSUPERVISED CLUSTERING FOR DETECTING CRACKS IN HELICOPTER GEARBOX CASING |
4.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity |
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ICAS2026_0014: J. Cecrdle¹, O. Vich¹, P. Malinek¹, R. Kulhanek¹; ¹VZLU AEROSPACE, Czech Republic WIND TUNNEL TESTING OF WHIRL FLUTTER AEROELASTIC DEMONSTRATOR |
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ICAS2026_0032: K. Niessen¹, D. Franke¹; ¹Defence Science and Technology Group, Australia KEY PARAMETER IDENTIFICATION IN AIRCRAFT STRAIN PREDICTION MODELS |
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ICAS2026_0072: S. Miao¹, Y. Ge¹, Y. Pei¹; ¹Northwestern Polytechnical University, China SEMI-SUPERVISED MULTI-TASK CONSISTENCY LEARNING FOR DEFECT DETECTION AND DEPTH ESTIMATION |
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ICAS2026_0141: Y. Guo¹, W. Yang¹, X. Xu¹, Z. Li¹, J. Liu¹, S. Cao¹; ¹Northwestern Polytechnical University, China AN AEROELASTIC DYNAMICS MODELING METHOD FOR INSECT-INSPIRED FLEXIBLE FLAPPING-WING UAV |
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ICAS2026_0153: A. Das¹, J. Yao¹, G. Coppotelli, University of Rome, La Sapienza, Italy; M. Candon¹, M. Fard¹, P. Marzocca¹; ¹RMIT University, Australia GROUND VIBRATION TEST ANALYSIS OF A PC-9 AIRCRAFT USING DELAY-EMBEDDED DYNAMIC MODE DECOMPOSITION WITH CONTROL |
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ICAS2026_0157: G. Swanton¹, A. Manning¹, B. Evans¹, M. Chipper, RMIT University, Australia; ¹Defence Science and Technology Group, Australia A FULL-SCALE DEMONSTRATOR FOR RAPID TESTING OF HELICOPTER AIRFRAMES USING ADVANCED CONTROL SYSTEM METHODOLOGIES |
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ICAS2026_0179: Z.Y. Xi¹, Y.T. Dai¹, C. Yang¹; ¹Beihang University, China FLUTTER ANALYSIS OF A DYNAMIC VARIABLE-SWEEP WING |
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ICAS2026_0211: V. Priasso¹, A. Lannoo¹; ¹DMAS, ONERA, 59000, Lille, France, France AIRCRAFT MASS EVALUATION MODEL: FROM TUBE-AND-WING TO BLENDED WING BODY USING WHALE. |
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ICAS2026_0230: V.N. Mueller¹, N. Singer¹, N. Moser¹, T. Siemer¹, F. Daoud¹; ¹Technical University of Munich, Germany NOVEL MULTIDISCIPLINARY MISSION-OPTIMISED AIRCRAFT DEVELOPMENT METHODOLOGY IN CONSIDERATION OF PASSIVE/ACTIVE CONTROL |
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ICAS2026_0262: W.L. Lei, China; Y.S. Gu, China; Z.C. Yang, China AEROSERVOELASTIC MODELING AND ANALYSIS OF THRUST VECTORING LAUNCH VEHICLE CONSIDERING RIGID-ELASTIC INTERACTION |
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ICAS2026_0277: F. Yu¹, M. Hornung¹; ¹Technical University of Munich, Germany MANEUVER LOAD ALLEVIATION OF THE DRY WING FOR HYDROGEN AIRCRAFT |
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ICAS2026_0290: A. Lloyd¹, K.C. Wong¹; ¹University of Sydney, Australia ENERGY DISSIPATION OF THIN-WALLED RIBBED SPHERES FOR CARGO AIRDROP |
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ICAS2026_0326: M. Kouchlef¹, N. Tsushima¹, T. Yokozeki¹; ¹The University of Tokyo, Japan PARAMETRIC AEROELASTIC STUDY OF WINGLET GEOMETRY USING VORTEX LATTICE METHOD FOR FUTURE PASSIVE MORPHING APPLICATIONS |
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ICAS2026_0342: C. Mollet¹, L. Vertonghen¹, C. Julien¹; ¹ONERA, France AEROELASTIC DESIGN OF A STRUT-BRACED DRY WING FOR A HYDROGEN AIRCRAFT IN AN MDO FRAMEWORK |
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ICAS2026_0355: L. Vertonghen¹, C. Mollet, DAAA, ONERA, Institut Polytechnique de Paris, France; C. Julien¹, F.-X. Irisarri¹; ¹DMAS, ONERA, Université Paris-Saclay, France COMBINED TOPOLOGY AND COMPOSITE LAMINATE OPTIMIZATION OF A STRUT-BRACED DRY WING FOR A HYDROGEN AIRCRAFT |
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ICAS2026_0364: C. Hesse¹, P. Allebrodt¹, S. Proskurov¹, B. Nagel¹; ¹DLR, Germany NUMERICAL PREDICTION OF CABIN NOISE FOR FUTURE SHORT-HAUL AIRCRAFT IN EARLY AIRCRAFT DESIGN |
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ICAS2026_0379: S.Y. Liang¹, T. Yang¹, Z.C. Yang¹; ¹Northwestern Polytechnical University, China IMPACT LOAD IDENTIFICATION METHOD FOR AIRCRAFT RUDDER PLANES BASED ON NARX NEURAL NETWORK |
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ICAS2026_0381: F. Saachi¹, F. Healy¹, D. Rezgui¹, J. Cooper¹; ¹University of Bristol, United Kingdom ENABLING FORWARD SWEPT WING DESIGNS |
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ICAS2026_0448: N. Tsushima, Kyushu University, Japan; R. Higuchi¹, T. Yokozeki¹; ¹The University of Tokyo, Japan AEROELASTIC TAILORING FOR COMPOSITE ADAPTIVE WINGLETS |
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ICAS2026_0452: N. Demant, FH Aachen University of Applied Sciences, Germany; P. Kantzidis¹, G. Lazzaro, Polytechnic University of Milan, Italy; V. Muscarello¹; ¹Royal Melbourne Institute of Technology, Australia DEVELOPMENT OF CONTROL LAWS FOR ENHANCED PERFORMANCE AND AEROELASTIC STABILITY OF EVTOL AIRCRAFT |
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ICAS2026_0494: C.Y. Zhao, China; B.G. Mi, China; X. Bai, China MODELING AND ANALYSIS OF ACTIVE FLUTTER SUPPRESSION OF THE PREPOSITIVE ELLIPTICAL WING-MAIN WING COMPOSITE CONFIGURATION |
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ICAS2026_0566: X. Ai¹, Z. Chen¹, Z. Liang¹, Z. An¹, X. Xu¹, Y. Lu¹, W. Qian¹; ¹Dalian University of Technology, China MECHANISM OF ALL-MOVABLE RUDDER NONLINEAR AEROELASTIC BEHAVIOR INDUCED BY BENDING FREEPLAY |
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ICAS2026_0614: M. Mauersberger¹, J. Rehfeldt¹, F. Hähnel¹, J. Markmiller¹; ¹Dresden University of Technology (TUD), Germany OPTIMIZATION APPROACHES FOR THE SHEAR-POSTBUCKLING DESIGN OF THERMOPLASTIC THIN-PLY COMPOSITE SHELLS IN HELICOPTERS |
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ICAS2026_0620: C.-Y. Li¹, S. He¹, Z.-C. Yang¹; ¹Northwestern Polytechnical University, China TIME-VARYING AEROELASTIC MODELING AND FLUTTER ANALYSIS OF TELESCOPIC WINGS |
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ICAS2026_0627: W. Qian¹, J. Liu¹, X. Hu¹, C. Han¹, X. He¹, X. Ran¹, X. Ai¹; ¹Dalian University of Technology, China A FLUTTER VERIFICATION METHOD FOR ALL-MOVABLE CONTROL SURFACE CONSIDERING FREE-PLAY NONLINEARITY |
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ICAS2026_0628: Y. Pan¹, M. Alam¹; ¹Cranfield University, United Kingdom CRITICAL LOAD-CASE AND CONSTRAINT IDENTIFICATION FOR PRELIMINARY COMPOSITE WING SIZING USING RAPID DESIGN TOOLS |
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ICAS2026_0706: G. Dessena¹, M. Civera², E.P. Mottola², O.E. Bonilla-Manrique¹; ¹Universidad Carlos III de Madrid, Spain; ²Politecnico di Torino, Italy AIRFRAME HEALTH MONITORING ON THE BAE SYSTEMS HAWK T1A JET TRAINER |
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ICAS2026_0724: G. Dessena¹, A. Dell'Edera, Politecnico di Bari, Italy; F.M.A. Mitrotta, University of Bristol, United Kingdom; O.E. Bonilla-Manrique¹; ¹Universidad Carlos III de Madrid, Spain VALIDATION OF A LOW-COST DATA ACQUISITION SYSTEM FOR AIRCRAFT VIBRATION TESTING |
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ICAS2026_0852: N. Kishimoto¹, R. Sakata¹, Y. Iwami², N. Tomita², M. Tamayama, JAXA, Japan; Y. Tanahashi³, T. Ikeda³; ¹Kwansei Gakuin University, Japan; ²Yamashina Institute for Ornithology, Japan; ³Chubu University, Japan EFFECT OF MORPHOLOGICAL CHANGES ON THE AERODYNAMIC CHARACTERISTICS OF THE WING AND TAIL FEATHERS OF A TAXIDERMY BLACK-TAILED GULL |
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ICAS2026_0853: R. Yang¹, S. Li¹, S. Sun ¹; ¹School of Mechanical Engineering Dalian University of Technology, China CURVATURE-CONTROLLED MORPHING OF FOLDING WINGTIPS USING HONEYCOMB PLATES |
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ICAS2026_0885: Z. Sajid¹, T. Rehman¹, A.H. Baluch¹; ¹King Fahd University of Petroleum & Minerals, Saudi Arabia IMPACT RESISTANCE ENHANCEMENT IN FIBER-REINFORCED COMPOSITES USING CARBON/BASALT HYBRIDIZATION APPROACHES |
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ICAS2026_0901: G.R. Dias¹, D.V.R. Silva¹, A.G. Heck¹, D.A. Rade¹; ¹Aeronautics Institute of Technology, Brazil PREDICTION OF STRUCTURAL VIBRATIONS INDUCED BY MASS-UNBALANCED ELECTRIC PROPULSION SYSTEMS |
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ICAS2026_0948: N. Ziakos, Spain; A. Cini, Spain AN AUTOMATED PARAMETRIC FRAMEWORK FOR EARLY-STAGE STRUCTURAL DESIGN AND OPTIMIZATION OF COMPOSITE AIRFRAMES |
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ICAS2026_1080: J. Kirkness¹, N.J. Lawson¹, G. Vio, 2Defence Science and Technology, Australia; ¹University of Sydney, Australia EXPERIMENTAL INVESTIGATION OF BOUNDARY LAYER CONTROLLED CAVITY FLOW FOR PIEZOELECTRIC ENERGY HARVESTING APPLICATIONS |
5 - Propulsion and Energy |
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ICAS2026_0024: S.M. Jeon, Korea Aerospace Research Institute, South Korea ACTIVE THRUST BALANCING CONTROL OF A TURBOPUMP WITH A SWIRL BREAKER |
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ICAS2026_0084: G. Braggett¹, K.F. Joiner¹, A. Somerville¹, D. Hill, Altavia Aerospace, Australia; ¹University of New South Wales, Australia FEASIBILITY OF ELECTRIC DUCTED FANS TO REPLACE OPEN PROPELLERS ON AN ELECTRIFIED TRAINING AIRCRAFT |
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ICAS2026_0110: J. Hueso-Rebassa¹, D. MacManus¹, R. Christie¹, J. Matesanz-Garcia¹, Y. Frey², C. Sheaf²; ¹Cranfield University, United Kingdom; ²Rolls-Royce plc., United Kingdom NOVEL METHODS FOR THE CHARACTERISATION OF INTAKE FLOW DISTORTION |
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ICAS2026_0111: J. Hueso-Rebassa¹, D. MacManus¹, F. Tejero¹, T. Williams, Cambridge University, United Kingdom; Y. Frey², G. Thorne²; ¹Cranfield University, United Kingdom; ²Rolls-Royce plc., United Kingdom EFFECT OF INTAKE AERODYNAMICS AND FLOW DISTORTION ON FAN STALL INCEPTION |
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ICAS2026_0139: S. Bäumler, Chair of Electrified Aero Engines, BTU Cottbus-Senftenberg, Germany; S. Kazula¹, A. Zwingler, Department of Mechanical Engineering, TU Munich, Germany; L. Enghardt¹; ¹DLR Institute of Electrified Aero Engines, Germany IMPACT ASSESSMENT OF COMPONENT FAILURES IN A PEM-FUEL CELL BASED PROPULSION SYSTEM FOR AIRCRAFT APPLICATIONS FOCUSING ON WATER MANAGEMENT |
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ICAS2026_0148: G.A. Liang¹, L.F. Gou¹, L.J. Lu¹; ¹School of Power and Energy,Northwestern Polytechnical University, China ADAPTIVE PREDICTION HORIZON-BASED MODEL PREDICTIVE CONTROL FOR AERO ENGINE |
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ICAS2026_0149: L.J. Lu¹, Y.Z. Chen¹, G.A. Liang¹, L.F. Gou¹; ¹School of Power and Energy,Northwestern Polytechnical University, China ROBUST FAULT DIAGNOSIS FOR AERO-ENGINE NETWORKED CONTROL SYSTEMS UNDER TRANSMISSION UNCERTAINTIES |
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ICAS2026_0207: L. Carrea¹, K. Kyprianidis¹; ¹Mälardalen University, Sweden COMPARATIVE ASSESSMENT OF PROPULSION SYSTEM ARCHITECTURES TAILORED FOR SUPERSONIC APPLICATIONS |
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ICAS2026_0261: P. Wehrel¹, J. Häßy¹, R. Schnell¹, S. Wöhler¹; ¹German Aerospace Center (DLR)), Germany CONCEPTUAL PERFORMANCE AND MASS ASSESSMENT OF AN OPEN FAN ENGINE FOR THE DLR-F25 AIRCRAFT |
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ICAS2026_0299: F. Thilker¹, R. Krewinkel, Graz University of Technology , Austria; A. Tramposch¹; ¹University of Applied Sciences JOANNEUM GmbH, Austria EXPERIMENTAL AND NUMERICAL INVESTIGATION OF HYDROGEN FLAMES UNDER COLD INJECTION CONDITIONS |
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ICAS2026_0314: C. Song¹, H. Shi¹, Z. Huang¹, H. Xiao¹; ¹Northwestern Polytechnical University, China PD-STGNN: A PHYSICS-INFORMED DYNAMIC SPATIO-TEMPORAL GRAPH NEURAL NETWORK FOR AERO-ENGINE THRUST PREDICTION |
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ICAS2026_0334: L. Oberthür¹, M. Stößel¹, D. Kozulovic¹, M. Krummenauer, Bundeswehr Technical Center for Aircraft and Aeronautical Equipm, Germany; ¹University of the Bundeswehr Munich, Germany INVESTIGATION OF GENERIC SWIRL DISTORTION AND ITS EFFECTS ON COMPRESSOR PERFORMANCE AND FLOW STABILITY |
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ICAS2026_0338: G. Marinaro¹, C. Serpico¹, L. Garbarino¹, M. Inverno¹, G. Malaponte¹, A. Bono¹, A. Pagano¹; ¹Italian Research Centre - CIRA, Italy REAL-TIME EMULATION TESTBENCH FOR FUEL-CELL/BATTERY HYBRIDIZATION IN HYDROGEN-ELECTRIC AVIATION |
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ICAS2026_0341: S. Li¹, J.P. Hu¹, J. Wang¹, Y.P. Li¹, Y.B. Wang, China; ¹Northwestern Polytechnical University School of Power and Energy, China STRUCTURAL DESIGN AND PERFORMANCE STUDY OF A TWO-STAGE DYNAMIC PRESSURE OIL-AIR SEPARATOR |
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ICAS2026_0370: K. Tsukuda¹, H. Kato¹, D. Sasaki¹, C. Fujio², S. Takahashi², T. Isono², M. Koga², M. Takegoshi²; ¹Osaka Metropolitan University, Japan; ²Japan Aerospace Exploration Agency, Japan PROPULSION-AIRFRAME INTEGRATED AERODYNAMIC PREDICTION METHOD USING FASTAR FOR SPACEPLANE CONCEPTUAL DESIGN |
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ICAS2026_0398: H. Schlickenmaier, HS Advanced Concepts LLC, United States; V. Schultz, Revolutionary Concepts LLC, United States; C. Baczynski, BAC Aerospace Inc, Canada; J, Maris, Flight Test Centre of Excellence d.b.a. Cert Center Canada, Canada; M. Cummings, Certification Engineering Services, LLC, United States; M. Traskos, Lectromec, United States ENTRY INTO SERVICE REQUIRES CERTIFICATION FOR NOVEL TECHNOLOGY |
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ICAS2026_0418: H. Miki¹, J. Akatsuka¹, R. Nimura, Tokyo University of Agriculture and Technology, Japan; ¹JAXA, Japan SPILLAGE DRAG REDUCTION IN DIVERTERLESS SUPERSONIC INLET |
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ICAS2026_0426: P. Gonzales-DeGreiff, New Granada Military University (UMNG), Colombia; J. Gonzalez-Mitte¹, G. Palaia², K. Salem², P. Bravo-Mosquera¹; ¹São Carlos School of Engineering, University of São Paulo (EESC , Brazil; ²Department of Mechanical and Aerospace Engineering, Politecnico , Italy IGNIT3: AN INTEGRATED COMPUTATIONAL FRAMEWORK FOR NON-IDEAL THERMODYNAMIC ANALYSIS AND OPTIMIZATION OF TURBOJET AND TURBOFAN ENGINES |
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ICAS2026_0461: Y.P. Li, China; J.P. Hu, China; G.L. Li, China; H.L. Zhao, China; S. Li, China STUDY ON OIL CAVITATION AND PUMPING CHARACTERISTICS OF SURFACE MICROTOPOGRAPHY GRAPHITE SEALS |
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ICAS2026_0487: S. Ogawa¹, T. Hongo¹, Y. Maeda¹, H.P.U. Nguyen¹, K. Mori¹; ¹Osaka Metropolitan University, Japan ASSESSMENT OF ENGINE-OUT ATMOSPHERIC EMISSIONS FROM COCONUT-OIL-DERIVED BIOJET FUEL |
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ICAS2026_0504: T. Isono, Japan Aerospace Exploration Agency, Japan NUMERICAL PREDICTION AND EXPERIMENTAL VALIDATION ON THRUST PERFORMANCE OF SCRAMJET EXTERNAL NOZZLES |
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ICAS2026_0508: A. Roco¹, H. Chisholm, Advanced Composite Structures Australia, Australia; D. Hartley¹; ¹Defence Science and Technology Group, Australia HYBRID ROCKET HOT-GAS DRIVER FOR DIRECT-CONNECT SCRAMJET THERMO-STRUCTURAL SCREENING |
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ICAS2026_0510: L.L. Shi¹, Y. Fan¹, B.G. Mi¹; ¹Northwestern Polytechnical University, China NUMERICAL STUDY OF UNSTEADY DISTORTION IN AN S-DUCT INTAKE SUBJECTED TO BLAST SHOCK WAVES |
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ICAS2026_0551: P. Kirschnek¹, A. Görtz², M. Schmelcher², F. Thilker¹, J. Häßy²; ¹FH JOANNEUM, Austria; ²Deutsches Zentrum für Luft- und Raumfahrt, Germany EVALUATION OF LIQUID HYDROGEN CONDITIONING CONCEPTS FOR AIRCRAFT ENGINES EMPLOYING EXHAUST GAS WASTE HEAT RECOVERY |
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ICAS2026_0574: A. Görtz¹, J. Häßy¹, M. Baier Schmelcher¹, M. El-Soueidan¹, F. Herbst¹; ¹German Aerospace Center, Germany HEAT EXCHANGER MODELING METHODS FOR HYDROGEN POWERED AERO ENGINES DURING THERMODYNAMIC CYCLE DESIGN |
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ICAS2026_0579: T.Q. Dinh¹, H.X. Vu¹, A.C. Pham¹, L.D. Chu¹; ¹Viettel Aerospace Institute, Vietnam PARAMETRIC DESIGN AND MULTI-OBJECTIVE OPTIMIZATION OF EXHAUST NOZZLE FOR GAS TURBINE ENGINES |
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ICAS2026_0584: M. Qiao¹, Y.Z. Huang, Shenzhen Research Institute of NPU , China; L.F. Gou¹; ¹Northwestern Polytechnical University, China INTELLIGENT FULL-ENVELOPE OPTIMIZATION OF TRANSIENT CONTROL LAWS FOR ADAPTIVE CYCLE ENGINES VIA TRANSFER LEARNING-ENHANCED DEEP REINFORCEMENT LEARNING |
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ICAS2026_0597: C. Rieger¹, M. Hornung¹; ¹Chair of Aircraft Design, Technical University of Munich, Germany IN-FLIGHT LOW-COST THRUST MEASUREMENT SYSTEM FOR SMALL UNMANNED AERIAL VEHICLES |
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ICAS2026_0612: J. Häßy¹, J. Schmeink¹, B. Fröhler¹; ¹German Aerospace Center (DLR), Germany RUBBER ENGINE INTEGRATED OPTIMIZATION STRATEGY FOR OVERALL AIRCRAFT DESIGN |
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ICAS2026_0613: A. Suti¹, M. Budinger¹, G. Di Rito, Università di Pisa, Italy; A. Reysset¹, I. Hazyuk¹; ¹INSA Toulouse, France A MODEL PREDICTIVE CONTROL STRATEGY FOR THE ENERGY MANAGEMENT OF HYBRID ELECTRIC PROPULSION SYSTEMS IN FIXED-WING UAVS |
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ICAS2026_0619: A. Suti¹, M. Budinger¹, G. Di Rito, Università di Pisa, Italy; A. Reysset¹, I. Hazyuk¹; ¹INSA Toulouse, France POWER-HIL TESTING OF LI-PO BATTERY PACKS FOR LIGHTWEIGHT EVTOL UAVS |
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ICAS2026_0652: C.K. Sain¹, S. Bhapkar¹, M. Kober¹, S. Kazula¹; ¹German Aerospace Center (DLR), Germany NUMERICAL AND EXPERIMENTAL EVALUATION OF COMPACT TPMS AND OFFSET-STRIP-FIN HEAT EXCHANGERS FOR FUEL CELL SYSTEM COOLING IN AN ELECTRIC AIRCRAFT |
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ICAS2026_0678: Hussain Ali Abid¹, Igor SOLNTSEV, GPU Prime LTD, United Kingdom; Andrea RAPISARDA¹, Hassan Ali Abid, King Fahd University of Petroleum and Minerals, Saudi Arabia; Sergey A. Karabasov¹; ¹Queen Mary University of London, United Kingdom HIGH-FIDELITY NUMERICAL INVESTIGATION OF ROTOR-WING INTERACTIONS IN A MULTI-ROTOR DISTRIBUTED ELECTRIC PROPULSION CONFIGURATION |
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ICAS2026_0690: Y. Liu¹, L. Gou¹, Y. Huang, Shenzhen Research Institute of Northwestern Polytechnical Univer, China; ¹School of Power and Energy, Northwestern Polytechnical Universit, China FLIGHT-DATA-DRIVEN PHYSICS-INFORMED COMPONENT MAP DERIVATION WITH STRUCTURAL COMPLIANCE |
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ICAS2026_0712: A. Stuermer¹, M. Hepperle¹, P. Wegener¹; ¹DLR, Germany SURROGATE-BASED OPTIMIZATION OF AIRCRAFT PROPELLER PERFORMANCE USING A HIGH-FIDELITY AND EFFICIENT RANS FRAMEWORK |
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ICAS2026_0739: N.K. Chaudhary, Australia MAGNETOPLASMAIONIC (MPI) ENGINE |
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ICAS2026_0768: K. Omoto¹, D. Sasaki¹, K. Matsui², M. Yamagami²; ¹Osaka Metropolitan University, Japan; ²IHI Corporation, Japan INITIAL GEOMETRIC UNCERTAINTY ASSESSMENT IN COMPRESSOR AIRFOILS USING PHYSICS-BASED DIRECT MANIPULATED FFD |
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ICAS2026_0788: Y. Wu¹, L. Zhou¹, J. Shi¹, Y. Meng¹, Z. Wang¹; ¹Northwestern Polytechnical University, China NUMERICAL INVESTIGATION OF GEOMETRIC EFFECTS ON INFRARED CHARACTERISTICS OF MULTI-STREAM SERPENTINE NOZZLES |
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ICAS2026_0813: T. Otten¹, T. Matuschek¹, J. Häßy¹, J. Frank¹, R.G. Brakmann¹; ¹German Aerospace Center (DLR), Germany MODULAR JET AND PROPELLER ENGINE – PART I: INITIAL STUDIES |
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ICAS2026_0826: S. Bhapkar¹, C. Sain¹, M. Kober¹, S. Kazula¹; ¹German Aerospace Center, Germany THERMAL–HYDRAULIC OPTIMIZATION OF AXIALLY GRADED OFFSET STRIP-FIN HEAT EXCHANGERS FOR MEGAWATT-CLASS FUEL CELL ELECTRIC AIRCRAFT |
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ICAS2026_0829: T. Matuschek¹, T. Otten¹, J. Häßy¹, R. Brakmann¹, J. Frank¹, P. Wehrel¹; ¹German Aerospace Center (DLR), Germany MODULAR JET AND PROPELLER ENGINE – PART II: INTEGRATED DESIGN PROCESS AND DESIGN SPACE ASSESSMENT |
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ICAS2026_0882: B Van Magill¹, D Verstraete¹; ¹The University of Sydney, Australia TOWARDS A DATABASE OF MICRO-ELECTRIC MOTORS AND ELECTRONIC SPEED CONTROLLERS FOR SMALL UNCREWED AERIAL SYSTEMS |
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ICAS2026_0906: X.K. Ma¹, H.C. Yang¹, K. You¹, R.B. Zhu¹, Z.L. Chen¹; ¹Northwestern Polytechnical University, China INLET OPTIMIZATION DESIGN OF A BOUNDARY LAYER INGESTION PROPULSION SYSTEM |
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ICAS2026_0954: F. Pak¹, U. Perra¹, F. Willems¹, T. Hofman¹, M. Salazar¹; ¹Eindhoven University of Technology, Netherlands AN OPTIMAL POWER MANAGEMENT POLICY FOR HYDROGEN BASED HYBRID AERO ENGINES |
6.1 - Flight Dynamics and Control (Control & Modelling) |
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ICAS2026_0011: V. Martinez Jimenez¹, F. Asensio Nieto¹, I. Romo Martinez¹, A. Sanz De Blas¹, D. Lodares Gomez¹; ¹AIRBUS, Spain ADAPTIVE FLIGHT CONTROL LAWS APPLIED TO AIR REFUELING WITH RECEIVERS EQUIPPED WITH RECEPTACLE OUT OF THE PLANE OF SYMMETRY |
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ICAS2026_0099: Y.-X. Yang¹, Z. Xu¹; ¹Northwestern Polytechnical University, China A HYBRID CNN-LSTM AND PSEUDOSPECTRAL METHOD FOR RAPID SPACECRAFT REENTRY OPTIMIZATION |
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ICAS2026_0106: R. Wang¹, Y. Liu¹, M. Zhang¹; ¹Northwestern Polytechnical University, China AERODYNAMIC REQUIREMENTS ASSESSMENT OF CIVIL AIRCRAFT BASED ON AIRWORTHINESS PERFORMANCE |
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ICAS2026_0109: Z. Wu¹, S. Yang¹, Z. Zhang¹, Y. Qu¹, B. Xiao¹; ¹Northwestern Polytechnical University, China PHYSICS-INFORMED NEURAL NETWORK BASED MODELING OF DYNAMIC BEHAVIOR OF AERIAL REFUELING HOSE |
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ICAS2026_0123: L. Mudrik, Naval Postgraduate School, United States; Y. Oshman, Technion---Israel Institute of Technology, Israel ROBUST ESTIMATION-AWARE GUIDANCE FOR STOCHASTIC INTERCEPTION WITH PARAMETRIC UNCERTAINTY |
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ICAS2026_0125: K. Yoshioka¹, T. Tsuchiya¹; ¹The University of Tokyo, Japan PILOT-IN-THE-LOOP SIMULATION OF OPTIMAL DEEP-STALL RECOVERY FOR T-TAIL AIRLINER |
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ICAS2026_0152: M. May¹, D. Milz¹, S.F. Armanini, Imperial College London, Germany; ¹German Aerospace Center (DLR), Germany KNOW YOUR LIMITS: ESTIMATING THE TILT-WING TRANSITION CORRIDOR UNDER FAILURE CONDITIONS |
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ICAS2026_0164: W.S. Lee¹, S.J. Kim¹, S.K. Kim¹; ¹Chungnam National University, South Korea TRAJECTORY OPTIMIZATION FOR TAKEOFF/LANDING BASED ON FLAP-AND-GLIDE FOR FLAPPING-WING UNMANNED AERIAL VEHICLE |
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ICAS2026_0166: S.W. Kim¹, T.W Yun¹, D.H. Seo¹, J.Y. Suk¹, S.K. Kim¹; ¹Chungnam National University, South Korea DISTURBANCE OBSERVER-BASED ADAPTIVE NONSINGULAR TERMINAL SLIDING MODE CONTROL FOR FAULT-TOLERANT CONTROL OF QUAD-TILTROTOR EVTOL |
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ICAS2026_0174: H.S. Choi¹, S. Shin¹, H.M. Lee¹, I. Yang¹, C.-H. Lee, KAIST, South Korea; ¹KARI, South Korea HYPERSONIC VEHICLE FLIGHT SIMULATION AND FLIGHT CONTROL |
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ICAS2026_0176: E.J. Kim¹, B. Seo¹, S.K. Kim¹, J.Y. Suk¹; ¹Chungnam National University, South Korea SYSTEM IDENTIFICATION OF SMALL-SCALE HELICOPTER VIA EKF WITH DATA-DRIVEN NOISE COVARIANCE DETERMINATION |
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ICAS2026_0191: L.B. Zhou¹, B.F. Song¹, Y.C. Liu¹, M.X. Chen, COMAC Shanghai Aircraft Manufacturing Co., Ltd., China; Q. Fu¹; ¹Northwestern Polytechnical University, China MULTI-BODY DYNAMIC MODELING OF A BIRD-LIKE FLAPPING-WING VEHICLE: ANALYSIS OF FLAPPING-AERODYNAMIC COUPLING EFFECTS |
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ICAS2026_0206: J. Luo, The Boeing Company, United States AIRCRAFT BUFFET QUANTIFICATION |
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ICAS2026_0224: A. Lemetti¹, T. Polishchuk¹, L. Smetanova¹; ¹LiU, Sweden AIRSPACE CAPACITY IMPLICATIONS OF CONTRAIL-AWARE TRAJECTORY OPTIMIZATION |
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ICAS2026_0246: T. Sakurai¹, S. Ueno¹, T. Higuchi¹, H. Akiyama¹; ¹Yokohama National University, Japan FLIGHT DYNAMICS AND GUIDANCE CONTROL FOR AIRCRAFT IN TYPHOON ENVIRONMENTS FOR DELIVERY OF TYPHOON CONTROL SUBSTANCE |
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ICAS2026_0306: M.X. Zhang¹, Y.S. Zhang, Chinese Flight Test Establishment, China; B.G. Mi¹, Y. Liu¹, R.Q. Wang¹; ¹Northwestern Polytechnical University, China STUDY ON DAMAGE SEVERITY ASSESSMENT METHODS FOR ASYMMETRICALLY DAMAGED LOITERING MUNITIONS |
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ICAS2026_0344: I.H. Lee, Korea Institute of Industrial Technology, South Korea AFFINE-INVARIANT ELLIPTICAL STATE ESTIMATION FOR ROBUST EXTENDED OBJECT TRACKING |
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ICAS2026_0361: J. Clarendon¹, T. Fields¹, J. Nguyen¹, A. Chance¹, O. Yakimenko, Naval Postgraduate School, United States; ¹University of Missouri-Kansas City, United States ATTITUDE CONTROL TECHNIQUES FOR A MICRO-SCALE FLAP-BASED AERODYNAMIC DECELERATOR SYSTEM |
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ICAS2026_0372: D. Surmann¹, S. Myschik¹; ¹University of the Bundeswehr Munich, Germany GAIN OPTIMIZATION FOR CASCADED INDI CONTROL WITH INTEGRATED PERFORMANCE AND ROBUSTNESS REQUIREMENTS |
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ICAS2026_0377: G. Fernandes Lourenço¹, C. Varriale¹; ¹Delft University of Technology, Netherlands TRIM PERFORMANCE EXPLORATION FOR AN AIRCRAFT WITH DISTRIBUTED ELECTRIC PROPULSION AND A TAIL THRUST UNIT |
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ICAS2026_0425: J.E.M. Fernandes¹, F.L. Cardoso-Ribeiro¹, M.A.V. Morales¹; ¹Instituto Tecnológico de Aeronáutica, Brazil FIXED-WING AIRCRAFT PORT-HAMILTONIAN DYNAMICS AND CONTROL |
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ICAS2026_0441: C. Weiser, German Aerospace Center (DLR), Germany FLIGHT ENVELOPE PROTECTION FOR HIGH ALTITUDE LONG ENDURANCE AIRCRAFT |
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ICAS2026_0505: J. Shim¹, J.-I. Jang¹, C.-H. Lee¹; ¹Korea Advanced Institute of Science and Technology, South Korea OPTIMAL GUIDANCE ALGORITHM FOR BOOST-BACK OF REUSABLE LAUNCH VEHICLES |
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ICAS2026_0506: S.W. Han¹, T.L. Ma¹, J.C. Fu¹, X.O. Zhang¹, Q.L. Zhang¹, L.Z. Wang¹; ¹Beihang University, China ROBUST ATTITUDE RECOVERY CONTROL FOR AIR-LAUNCHED FOLDING-WING UAVS VIA DISTURBANCE-COMPENSATED SUPER-TWISTING SLIDING MODE |
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ICAS2026_0518: M. Lowenberg¹, D. Pusztai¹; ¹University of Bristol, United Kingdom EVALUATION OF STALL BEHAVIOUR OF T-TAIL AIRCRAFT: MODELLING AND FLIGHT TEST |
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ICAS2026_0532: Y. Jung, Korea Aerospace Research Institute, South Korea; S. Cho, Cheongju University, South Korea CONVEX OPTIMIZATION-BASED EMERGENCY LANDING TRAJECTORY GENERATION FOR UAM VEHICLES |
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ICAS2026_0534: S.-J. Im¹, C.-H. Lee¹, J.-H. Jin, Sunchon National University, South Korea; H.-C. Bang¹; ¹Korea Advanced Institute of Science and Technology, South Korea TRAJECTORY OPTIMIZATION OF HIT-TO-KILL INTERCEPTORS VIA SEQUENTIAL CONVEX PROGRAMMING APPROACH |
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ICAS2026_0539: L. Hein¹, S. Myschik¹; ¹University of the Bundeswehr Munich, Germany FLIGHT PERFORMANCE ANALYSIS OF ELECTRIC AIRCRAFT UNDER MOTOR FAILURE CONDITIONS USING REDUCED-ORDER MODELING |
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ICAS2026_0563: S. Kim¹, K.-W. Jung¹, C.-H. Lee¹; ¹Korea Advanced Institute of Science and Technology, South Korea OPTIMAL ZEM-BASED MIDCOURSE GUIDANCE FOR INTERCEPTORS USING TRAJECTORY PREDICTION |
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ICAS2026_0567: D. Kim¹, J.D. Lee¹, H. Lee¹, Y. Kim¹, H. Bang¹; ¹KAIST, South Korea LEARNING-BASED CONTROL ALLOCATION FOR OVER-ACTUATED VTOL AIRCRAFT WITH NONLINEAR DYNAMICS |
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ICAS2026_0622: R Larsson, Saab Aeronautics, Sweden SYSTEM IDENTIFICATION USING FLIGHT TEST DATA AND MACHINE LEARNING |
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ICAS2026_0624: J.H. Wang¹, L.X. Wang¹, R. Zhao², Z. Wu², Y.F. Xu¹, H.L. Liu¹, S. Tai¹, T. Yue¹; ¹Beihang University, China; ²COMAC Shanghai Aircraft Customer Service Co. Ltd., China PHYSICS-INFORMED LSTM-BASED LONGITUDINAL STALL AEROFYNAMIC MODELING FRAMEWORK OF CIVIL AIRCRAFT USING FLIGHT TEST DATA |
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ICAS2026_0630: M. Alam¹, J. Renault¹, M. Hromcik², T. Hanis²; ¹Cranfield University, United Kingdom; ²Czech Technical University, Czech Republic LATERAL-DIRECTIONAL HANDLING AND FLYING QUALITIES ASSESSMENT OF A BLENDED WING BODY (BWB) ACFA 2020 CONFIGURATION |
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ICAS2026_0633: J. Cox¹, K.C. Wong¹, G. Chamitoff, Texas A&M University College of Engineering, United States; ¹The University of Sydney, Australia GUST ERROR METHOD (GEM): PARAMETER IDENTIFICATION FOR AIRCRAFT SUBJECT TO VON KÁRMÁN PROCESS NOISE |
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ICAS2026_0647: Y.L. Niu¹, L.X. Wang¹, J.X. Li², Y.N. Gao², S.H. Xu, COMAC Beijing Aircraft Technology Research Institute, China; T. Yue¹, S. Tai¹, H.L. Liu¹; ¹Beihang University, China; ²The First Aircraft Institute AVIC, China BACKSTEPPING-BASED PREDICTIVE PERFORMANCE CONTROL FOR AERIAL REFUELING BOOM ATTITUDE CONTROL |
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ICAS2026_0648: C. Koopman¹, D. Zammit Mangion¹; ¹University of Malta, Malta SUPPORTING PILOT SITUATIONAL AWARENESS BY EXTRACTING INSIGHTS FROM AN AI EXPERT |
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ICAS2026_0658: A. Kwiek¹, K. Kania¹; ¹Warsaw University of Technology, Poland A NEW APPROACH TO MODELLING THE FLIGHT DYNAMICS OF A TAILLESS AIRCRAFT |
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ICAS2026_0662: T. Bernhofer¹, A. Seefried¹; ¹German Aerospace Center (DLR), Germany A SIMULATION STUDY ON THE EFFECT OF EXTENDED ROTATIONAL KINEMATICS IN HEXAPOD MOTION SIMULATORS |
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ICAS2026_0664: D. Sanghi, United States; C.E.S. Cesnik, United States RESIDUAL LEARNING FRAMEWORK FOR NONLINEAR AEROELASTIC–FLIGHT-DYNAMICS CONTROL-ORIENTED MODELING OF VERY FLEXIBLE AIRCRAFT |
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ICAS2026_0680: M. Alexander, National Research Council of Canada/Flight Research Laboratory , Canada AN INVESTIGATION OF SAFETY-CRITICAL GROUND INTERFACE (TAKEOFF, LANDING) REGIME RECOGNITION FOR AUTOMATED AND AUTONOMOUS VERTICAL LIFT AIRCRAFT MISSION TASK DESIGN |
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ICAS2026_0686: A. Navarro¹, M. Alam¹, A. Elliott¹, E. Jinks, Siemens Digital Industries Software, United Kingdom; ¹Cranfield University, United Kingdom PHYSICS-INFORMED MACHINE LEARNING FOR FLIGHT DYNAMICS IDENTIFICATION OF THE SAAB 340B USING FLIGHT TEST DATA |
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ICAS2026_0725: C. Doll, ONERA, France CONTROL ALLOCATION AND SIZING FOR OVER-ACTUATED AIRCRAFT |
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ICAS2026_0742: Y.L. He, China; X.P. Xu, China; Z. Zhou, China; S. Song, China WIND FIELD PERCEPTION AND FEATURE PREDICTION FOR LOW-ALTITUDE SMALL FIXED-WING UAVS TOWARDS ENERGY HARVESTING |
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ICAS2026_0791: M.T. Morales¹, M.A. Rempel, Embraer, Brazil; M.A.V. Morales¹, J.E.M. Fernandes¹; ¹ITA, Brazil AUTOPILOT DESIGN OF AN UNSTABLE FIGHTER USING MODEL PREDICTIVE CONTROL |
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ICAS2026_0805: H. Kim¹, S. Lee¹; ¹Kookmin University, South Korea DUAL BEZIER SPACE-TIME OPTIMIZATION UNDER HARD OBSERVATION-WINDOW CONSTRAINTS: A FEASIBILITY-ORIENTED JERK-CAP COMPARISON |
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ICAS2026_0821: S. Fuchsgruber¹, M. Gerdts, University of the Bundeswehr Munich, Germany; F. Holzapfel¹; ¹Technical University of Munich, Germany SENSITIVITY-BASED REFERENCE TRAJECTORY UPDATES FOR AIRCRAFT PATH-FOLLOWING MODEL PREDICTIVE CONTROL |
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ICAS2026_0843: N. Gee-Landman¹, J.L. Palmer¹; ¹RMIT University, Australia AIRBRAKES CONTROL SYSTEM FOR PRECISE APOGEE CONTROL OF A SOUNDING ROCKET |
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ICAS2026_0858: S. Kim¹, J. Shin¹, H.-G. Kim, Konkuk University, South Korea; ¹Chungbuk National University, South Korea OFFLINE REINFORCEMENT LEARNING FOR INFRARED IMAGE-BASED MISSILE GUIDANCE AND CONTROL |
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ICAS2026_0865: J. Han¹, S. Kim¹, M. Jung¹, J. Woo¹, H.-S. Kim, APPIA Engineering Co., Ltd., South Korea; H. Bang¹; ¹Korea Advanced Institute of Science and Technology, South Korea PHYSICS-INFORMED LEARNING-BASED RECOVERY TRAJECTORY PREDICTION FOR AUTOMATIC GROUND COLLISION AVOIDANCE |
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ICAS2026_0869: S. Joshin¹, F. Tanaka, RIKEN R-CCS, Japan; T. Amano¹, A. Hiromori¹, A. Uchiyama¹, H. Yamaguchi¹, S. Morioka², T. Inagawa²; ¹The University of Osaka, Japan; ²Interstellar Technologies Inc., Japan HPC-BASED PARAMETER SPACE EXPLORATION FOR DENSE PICOSAT FORMATION FLYING TOWARD DIRECT-TO-DEVICE COMMUNICATIONS |
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ICAS2026_0872: H.J. Kim¹, J.H. Shin¹; ¹Chungbuk national University, South Korea NEURAL NETWORK BASED SLIDING MODE CONTROL FOR HYPERSONIC LONGITUDINAL CONTROL |
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ICAS2026_0891: M. Szymanski¹, V. Gollnick¹; ¹Hamburg University of Technology, Germany DATA-DRIVEN SYNTHESIS OF AIRCRAFT FEEDBACK CONTROL LAWS FOR NEW COMMERCIAL FLIGHT SCENARIOS |
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ICAS2026_0924: M.R. de Kock¹, B.B. Huyssen¹, R.J. Huyssen, Council for Scientific and Industrial Research, South Africa; ¹University of Pretoria, South Africa EFFECTS OF LIFT DISTRIBUTION AND WING POSTURE ON THE STABILITY AND CONTROL OF TAILLESS AIRCRAFT |
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ICAS2026_1033: L. Busse¹, M. Kumar¹; ¹University of Cincinnati, United States MULTI-SENSOR BASED ADAPTIVE FUSION SCHEME FOR POSITION ESTIMATION OF MULTIROTOR UAV SYSTEMS IN GPS-DENIED ENVIRONMENTS |
6.2 - Flight Dynamics and Control (UAV related) |
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ICAS2026_0037: X.L. Li¹, C.Q. Wang¹, Y. Guo¹, A.J. Li¹; ¹Northwestern Polytechnical University, China ADAPTIVE PRACTICAL PRESCRIBED-TIME FAULT-TOLERANT CONTROL FOR SMALL TANDEM-ROTOR UAV FORMATIONS |
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ICAS2026_0079: M. Ben Simon¹, S. Malka¹, D. Chudnovsky¹, O. Yakimenko¹; ¹Naval Postgraduate School, United States SIMULATION-BASED ANALYSIS OF REDUNDANT UAV NAVIGATION UNDER GNSS OUTAGES |
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ICAS2026_0096: K. Okamoto¹, T. Tsuchiya¹; ¹The University of Tokyo, Japan A SYSTEMATIC, TUNING-FREE ATTITUDE CONTROL METHOD FOR VTOL UAVS |
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ICAS2026_0098: J. Fang¹, Y. Guo¹, A. Li¹, C. Wang¹; ¹Northwestern Polytechnical University, China PREDEFINED-TIME AFFINE FORMATION FAULT-TOLERANT CONTROL FOR FIXED-WING UAVS WITH INPUT SATURATION |
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ICAS2026_0128: S. Song¹, X. Zhu¹, Z. Zhou¹; ¹Northwestern Polytechnical University, China CASCADE ADRC FOR TRAJECTORY TRACKING OF A FLYING-WING SOLAR AIRCRAFT UNDER WIND DISTURBANCES |
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ICAS2026_0138: Y. Xie, School of Aeronautics, Northwestern Polytechnical University Cit, China; Z. Zhou, Northwestern Polytechnical University, China SLIPSTREAM MODELING AND CONTROL ALLOCATION OF A DISTRIBUTED HETEROGENEOUS ELECTRIC PROPULSION TANDEM-WING UAV |
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ICAS2026_0143: R. Perz, WUT, Institute of Aeronautics and Applied Mechanics, Poland; P. Wozniak¹, R. Chalupczynski¹, K. Barys², J. Konowalski², A. Abratanski², J. Swierk¹, I. Dabrowski²; ¹Uavionics Ltd Poland, Poland; ²Rafal Perz Scientific Network, Poland MULTI-CAMERA PANORAMIC SENSING FOR LOCALISATION AND MULTI-OBJECT TRACKING IN UAVS |
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ICAS2026_0156: S. Crase¹, S. Pywell¹, K. Rosser¹; ¹Defence Science and Technology Group, Australia FLIGHT TRIALS OF DRONES CONTROLLED BY AI LARGE LANGUAGE MODELS |
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ICAS2026_0163: M. Yanagisawa¹, R. Okabayashi¹, T. Yamaguchi², M. Takamoto², M. Bando¹, S. Hokamoto¹; ¹Kyushu University, Japan; ²Mitsubishi Electric Corporation, Japan ROBUST MOTION ESTIMATION FOR INDOOR MAVS USING WIDE-FIELD-INTEGRATION OF OPTIC FLOW |
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ICAS2026_0167: Y.C. Yang¹, J.H. Jeong, Hanseo University, South Korea; S.K. Kim¹, J.Y. Suk¹; ¹Chungnam National University, South Korea SOFTWARE-IN-THE-LOOP SIMULATION OF DISTRIBUTED 3D INTEGRATED SWARM GUIDANCE FOR FIXED-WING UAVS |
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ICAS2026_0204: M. Zintl¹, F. Holzapfel¹; ¹Technical University of Munich, Germany FAMILIARIZATION, OPERATION, AND DEBRIEFING: AN ADAPTIVE AUGMENTED REALITY SUPPORT SYSTEM FOR UAV FLIGHT TESTING |
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ICAS2026_0208: Y.J. Hasan, DLR Institute of Flight Systems, Germany ASSESSMENT OF THE LANDING CAPABILITIES OF A FLEXIBLE HIGH-ALTITUDE PLATFORM AT LONGITUDINAL AND LATERAL-DIRECTIONAL WIND DISTURBANCES |
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ICAS2026_0217: Z. Lin¹, D. Geraghty¹, S.F. Armanini¹, L. Mainini¹; ¹Imperial College London, United Kingdom DYNAMIC RECONFIGURABLE PATH PLANNING FOR FIRE-FIGHTING UAVS |
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ICAS2026_0219: C. Galinski¹, T. Goetzendorf-Grabowski¹; ¹Warsaw University of Technology, Poland STABILITY ANALYSIS OF A LIGHT UAV WITH SOLAR PROPULSION |
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ICAS2026_0237: Y.K. Bu¹, L. Qiao¹, L. Li, Chang’an University, China; H.J. Feng¹, J.Q. Bai¹; ¹Northwestern Polytechnical University, China QUASI-STEADY AERODYNAMIC AND MBD COUPLED FLIGHT SIMULATION OF FOLDING MORPHING UAV |
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ICAS2026_0248: H. Iwamoto¹, N. Yokoyama, Japan Aerospace Exploration Agency, Japan; T. Higuchi¹; ¹Yokohama National University, Japan AUTONOMOUS PATH PLANNING ALGORITHM FOR EMERGENCY LANDING OF AAM CONSIDERING WIND DISTURBANCES |
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ICAS2026_0259: Y. Huang, Australia; K.C. Wong, Australia EXPERIMENTAL FLIGHT DYNAMICS AND CONTROL OF AN AGILE FIXED-WING UAV USING HYBRID ONBOARD AND OFFBOARD CONTROL |
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ICAS2026_0288: R. Schmidt¹, J. Rüter¹; ¹German Aerospace Center (DLR), Germany DEEP LEARNING VS. TRADITIONAL COMPUTER VISION FOR UAV LANDING SITE DETECTION IN ADVERSE WEATHER |
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ICAS2026_0289: K. Thomessen¹, S. Schopferer¹, P. Nagarajan¹; ¹German Aerospace Center (DLR), Germany ONBOARD MISSION MANAGEMENT FOR A DECENTRALIZED MULTI-UAV SYSTEM USING BEHAVIOR TREES |
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ICAS2026_0404: D. Milz¹, L. Ott¹, M. May¹; ¹German Aerospace Center (DLR), Germany TETHERED HOVER FLIGHT TESTS OF BASELINE CONTROL LAWS FOR A TANDEM TILT-WING SUB-SCALE DEMONSTRATOR |
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ICAS2026_0435: C.-V. Boruga¹, N. Zalewska¹, D. Lundström¹, P. Krus¹; ¹Linköping University, Sweden SIMULATION-BASED AUTOPILOT TUNING FOR FIXED-WING UAVS |
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ICAS2026_0513: M. Lee¹, M. Park¹; ¹Changwon National Unviersity, South Korea INFORMATIVE PATH PLANNING BASED ON REDUCED-RANK GAUSSIAN PROCESS FOR HAZARDOUS SUBSTANCE MONITORING |
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ICAS2026_0529: M.I. Alam¹, A.H. Baluch¹, S.H. Vattathurvalappil¹; ¹King Fahd University of Petroleum and Minerals, Saudi Arabia ENSEMBLE MACHINE LEARNING FOR UAV PROPELLER PERFORMANCE PREDICTION WITH UNCERTAINTY QUANTIFICATION |
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ICAS2026_0531: H. Zhang¹, J.N Liu¹, Z. Xu¹, Y.X. Yang¹; ¹School of Astronautics, Northwestern Polytechnical University, China RESEARCH ON OFFENSIVE AUTONOMOUS VEHICLE TRAJECTORY PREDICTION METHOD BASED ON IMPROVED INVERSE REINFORCEMENT LEARNING IN AIRCRAFT ACTIVE DEFENSE MODE |
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ICAS2026_0649: S.K. Li¹, N.H. Zhu¹, Z. Zhou¹; ¹Northwestern Polytechnical University, China AUTONOMOUS FLIGHT AND INTELLIGENT TARGET LOCALIZATION FOR JUNGLE RECONNAISSANCE UAVS |
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ICAS2026_0670: P. Nagarajan¹, S. Schopferer¹, K. Thomessen¹; ¹German Aerospace Center (DLR), Germany AN AUTONOMY ARCHITECTURE FOR COLLABORATIVE UAV SWARMS - A BOTTOM-UP PERSPECTIVE |
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ICAS2026_0689: P. Bhandari¹, Z. Atkinson¹, A. Comer¹; ¹Oklahoma State University, United States EXPERIMENTAL CHARACTERIZATION OF PROPELLER-WING INTERACTIONS FOR A SUBSCALE LIFT + CRUISE VTOL UAV |
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ICAS2026_0695: A. Fallast¹, S. Lesak¹; ¹FH JOANNEUM University of Applied Sciences, Austria MODELING OF CRITICAL WEATHER FLIGHT PERFORMANCE OF MULTICOPTER UAVS FOR RESILIENT CONTROLLER DESIGN. |
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ICAS2026_0709: D.Y. Yoon¹, J.Y. Ka¹, D.J. Lee¹, Z. Wang², K.C. Wong²; ¹Hanseo University, South Korea; ²The University of Sydney, Australia COOPERATIVE TRACKING ALGORITHM OF MULTIPLE UAVS USING PSO FOR AERIAL SURVEILLANCE |
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ICAS2026_0713: D. Lundström¹, C.-V. Boruga¹, S. Riethausen¹, R. Larsson¹; ¹Linköping University, Sweden A 3D-PRINTED TESTBED FOR FLIGHT CONTROL SYSTEM RESEARCH. |
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ICAS2026_0735: R.B. Zhu¹, K. You¹, H.C. Yang¹, X.K. Ma¹, Z.L. Chen¹; ¹Northwestern Polytechnical University, China 2D AND 3D TRAJECTORY PLANNING FOR UAVS FORMATION SYSTEM USING DYNAMIC WINDOW APPROACH |
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ICAS2026_0737: Y.R. Kim¹, J.H. Hong¹, Y.J. Jang¹, J.H. Moon¹; ¹Cheongju University, South Korea FLIGHT TEST VALIDATION OF A VISION-GUIDED MULTIROTOR TERMINAL INTERCEPTION SYSTEM |
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ICAS2026_0765: C. Kang¹, J. Jeong¹; ¹Hanseo University, South Korea REINFORCEMENT LEARNING-BASED ADAPTIVE WEIGHTING OF SWARM GUIDANCE LAWS FOR SMALL FIXED-WING UAVS |
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ICAS2026_0771: J. McGuire¹, B. McIvor¹, S. Crase¹; ¹DSTG, Australia IMPLEMENTATION OF DISTRIBUTED SWARM GUIDANCE ALGORITHMS ON LOW-COST UAVS |
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ICAS2026_0815: R. Wang¹, Y. Wu¹, Z. Zhou¹, S. Yao¹, Z. Zhang¹; ¹Northwestern Polytechnical University, China RESEARCH ON FLIGHT DYNAMICS AND CONTROL CHARACTERISTICS OF MULTI-UAV WINGTIP-LINKED FLIGHT |
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ICAS2026_0845: I. Chakraborty¹, B. Kunwar¹, S. Putra¹, R. Bhandari¹, C. McCormick¹; ¹Department of Aerospace Engineering, Auburn University, United States A WORKFLOW FOR RAPID DESIGN, SIMULATION, FABRICATION, AND SUBSCALE FLIGHT-TESTING OF NOVEL AIRCRAFT CONCEPTS |
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ICAS2026_0859: Z. Zhang¹, S. Li¹, X.P. Xu¹, Z. Zhou¹; ¹Northwestern Polytechnical University, China VANE-LESS 3D WIND ESTIMATION FOR FIXED-WING UAVS: A PHYSICS-AUGMENTED TEMPORAL RESIDUAL NETWORK APPROACH |
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ICAS2026_0867: T. Gerner¹, M. Candon¹, A.K. Gostar¹, N. Jayarathne, Navantia Australia, Australia; J. Venning, University of Tasmania, Australia; M. Saska, Czech Technical University in Prague, Czech Republic; P. Marzocca¹; ¹RMIT University, Australia DECOUPLED DEEP REINFORCEMENT LEARNING FOR AUTONOMOUS LANDING OF UAVS ON SHIPS |
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ICAS2026_0874: Y. Zhu¹, R. Wang¹, Y.H. Xie¹, Z. Zhou¹; ¹Northwestern Polytechnical University, School of Aeronautics, China RAPID FLIGHT DYNAMICS EVALUATION OF STRONGLY COUPLED DISTRIBUTED PROPULSION |
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ICAS2026_0929: B. Kunwar¹, S. Putra¹, R. Bhandari¹, C. McCormick¹, I. Chakraborty¹; ¹Auburn University, United States SIMULATION MODEL CALIBRATION USING SYSTEM IDENTIFICATION FOR A VECTORED-THRUST MULTI-TILT-ROTOR CONFIGURATION |
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ICAS2026_0932: A.G.P. Sarmento¹, P. Krus, Linköping University (LiU), Sweden; E. Villani¹; ¹Aeronautics Institute of Technology (ITA), Brazil METHODOLOGY AND V1 PROTOTYPE OF AN ADAPTIVE/ADAPTABLE MULTI-UAV GCS HMI IN A FLOOD SAR CO-SIMULATION TESTBED |
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ICAS2026_0937: A.G.P. Sarmento¹, C.C. Duarte da Silva¹, G.V. Ferreira¹, E. Villani¹, D. Rade¹; ¹Aeronautics Institute of Technology (ITA), Brazil A SIMULATION METHODOLOGY FOR MULTIROTOR-ASSISTED UAV LAUNCH |
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ICAS2026_1012: James Garth, BAE SYSTEMS Australia, Australia DISCRIMINATORY AUTONOMY: OPERATING FASTER, SMARTER, AND WITH PURPOSE |
7 - Systems, Subsystems and Equipment |
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ICAS2026_0025: Y. Ying, Northwestern Polytechnical University , China; X. Yao¹, Y. Feng¹, W. Huang¹; ¹Northwestern Polytechnical University, China A THERMO-MECHANICAL PHASE FIELD MODEL CONSIDERING SOLID-LIQUID TRANSITION: APPLICATION TO ELECTROTHERMAL DE-ICING |
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ICAS2026_0028: R.X. Gong, Airbus (Tianjin) Final Assembly Company Limited, China; S.G. Sun¹, M. Xu¹, Y. Zheng, Northeast Air Traffic Management Bureau of Civil Aviation of Chi, China; ¹civil aviation university of China, China ANOMALY B-VALUE DETECTION AND EXCLUSION OF GBAS BASED ON WAVELET MULTI-RESOLUTION ANALYSIS |
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ICAS2026_0030: W. Mooney¹, M. Gendron, Calogy Solutions, Canada; X. Arcand¹, D. Francoeur¹, D. Rancourt¹; ¹Université de Sherbrooke, Canada DESIGN AND OPERATION OF LOW-COST MULTI-SCALE TEST BEDS FOR BATTERY THERMAL RUNAWAY INITIATION AND PROPAGATION |
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ICAS2026_0093: O. Bertram¹, H. Schumann¹, R. Kowalski¹, A. Bagdahn¹; ¹DLR (German Aerospace Center), Germany A MULTIDIMENSIONAL FRAMEWORK FOR DEMONSTRATION AND V&V CAPABILITIES FOR NEXT-GENERATION FLIGHT CONTROL SYSTEMS |
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ICAS2026_0170: Q.-V. Pham, Viettel Aeropsace, Vietnam; N.-V. Nguyen¹, V.-T. Nguyen¹, T.-.B. Nguyen¹, P.-M. Nguyen¹; ¹Viettel Aerospace, Vietnam A RELIABLE AND COST-EFFICIENT DATA ACQUISITION SYSTEM FOR MIL-HDBK-1763-COMPLIANT STATIC EJECTION TESTING OF AIRCRAFT EXTERNAL STORES |
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ICAS2026_0186: L. Mangiacrapa¹, T. Klaas², N. Rehfeld², F. Amoroso, Eurotech s.r.l., Italy; G. Mingione¹, S. Ameduri¹; ¹Italian Aerospace Research Centre, Italy; ²Fraunhofer IFAM , Germany ICE DETECTION: CORRELATION OF ICE ACCRETIONS AND DYNAMIC RESPONSES ON SMALL-SCALE AIRFOIL PROTOTYPES TESTED IN ICING WIND TUNNEL |
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ICAS2026_0265: P. Thöne¹, F. Abdelmoula¹, M. Gerber², M. Hornby³, N.A. Epps³, A. Winhard², F. Schwerzmann², C. Deiler¹; ¹German Aerospace Center - DLR, Germany; ²Swiss Skylab Foundation, Switzerland; ³NATS, United Kingdom DYN-MARS: A NEW CONCEPT ENABLING THE BEST APPROACH FLIGHT PROFILE |
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ICAS2026_0303: A. Testera¹, G. Ferrara¹, F. Di Fede¹, S. Caggese¹, V. Barba¹, G. Accardo¹, R. Pennino¹; ¹Leonardo SpA, Italy EXPERIMENTAL VALIDATION OF A FUEL CELL SYSTEM DIGITAL TWIN FOR A FULL-ELECTRIC AIRCRAFT POWERTRAIN |
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ICAS2026_0322: L. Zhao¹, W. Cheng¹, G. Wang¹; ¹Aviation Industry Development Research Center of China, China SYSTEM EFFECTIVENESS EVALUATION OF CHINA'S AVIATION EMERGENCY COMMUNICATION SYSTEM |
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ICAS2026_0335: G. Schmitz¹, I. Pruter¹, H. Duda¹, M. Laubner¹, S. Lorenz¹; ¹DLR e.V., Germany IMPACT OF SYSTEM LATENCIES ON PILOT INTERACTION AND HANDLING OF AN ELECTRICALLY POWERED GYROPLANE UAV WITH FPV-BASED REMOTE CONTROL |
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ICAS2026_0438: Z. Milani¹, L. Nichman², E. Matida¹, M. Wolde², A. Brown², A. Benmeddour², M. Mamou², R.S. Martins, ONERA, France; D. Orchard²; ¹Carleton University, Canada; ²National Research Council of Canada, Canada WEATHER, AVIATION, AND CLIMATE: CURRENT TOPICS IN AIRBORNE RESEARCH |
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ICAS2026_0460: J. Chang, McGill University, Canada; M. Kokkolaras, Clemson University, United States MODELING OF AIRCRAFT COMPONENT PLACEMENTS WITH BIN PACKING |
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ICAS2026_0483: F.L. Liu¹, L.Q. Zhao¹, Y.G. Lyu¹, B.S. Chang¹, Z.X. Liu¹; ¹Northwestern Polytechnical University, China HIGH-PRECISION EDDY-CURRENT TIP CLEARANCE SENSOR WITHEXCEPTIONALHEAT RESISTANCE |
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ICAS2026_0557: P. Panchal¹, W. Bliemetsrieder¹, N. Sorokina¹, S. Myschik¹; ¹University of the Bundeswehr Munich, Germany HARDWARE-IN-THE-LOOP VERIFICATION OF A SAFETY-CRITICAL RECONFIGURABLE BATTERY MANAGEMENT SYSTEM FOR AN ELECTRIC AIRCRAFT |
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ICAS2026_0561: L. Jiang¹, Y. Li¹, S. Bai¹, Z. Li¹, K. Jia¹, Y. Shang¹; ¹Beihang University, China POWER FLOW DYNAMICS AND COUPLING MECHANISMS IN POWER-BY-WIRE ACTUATION: A COMPREHENSIVE MODELING AND ANALYSIS APPROACH |
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ICAS2026_0590: J.B. Cheng¹, J. Li, AVIC Chengdu Aircraft Design and Research Institute, China; B.X. Wang¹, C. Chen, Information Center of the National Administration of Defense Sci, China; P. He, AVIC Luoyang Institute of Electro-Optical Equipment, China; K. Zhang¹; ¹Northwestern Polytechnical University, China A DISTRIBUTED MULTI-SOURCE SENSOR FUSION METHOD FOR COLLABORATIVE TARGET TRACKING |
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ICAS2026_0593: S.Y. Chen¹, J. Fu¹, K. Ci¹, H.Z. Song, Beijing Institute of Precision Mechatronics and Controls, China; Z.L. Li¹, D.C. Lyu¹; ¹Beihang University, China PREDICTION OF MINIMUM STARTING PRESSURE FOR HYDROSTATIC HELICAL ROTARY ACTUATOR USING PHYSICS-INFORMED NEURAL NETWORKS |
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ICAS2026_0621: S. Bai¹, Y. Li¹, L. Jiang¹, Z. Li¹, K. He¹, Z. Jiao¹; ¹Beihang University, China INTEGRATED CONTROL STRATEGY BASED ON PHYSICS-INFORMED MODEL-BASED REINFORCEMENT LEARNING FOR AIRBORNE HIGH-ENERGY SYSTEMS |
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ICAS2026_0623: Z. Zhu¹, Y. Lyu¹, L. Jiang¹, Z. Liu¹, S. Li¹, F. Liu¹; ¹Northwestern Polytechnical University, China MULTI-OBJECTIVE OPTIMIZATION OF AERO-ENGINE BEARING CHAMBER SCAVENGE STRUCTURE BASED ON NSGA-II |
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ICAS2026_0660: A. Suti¹, J. Pothin², M. Budinger¹, V. Pommier-Budinger², A. Reysset¹; ¹INSA Toulouse, France; ²Isae Supaero, France A MPC–MHE STRATEGY FOR FREQUENCY TRACKING AND PARAMETERS ESTIMATION OF RESONANT DE-ICING SYSTEMS |
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ICAS2026_0663: S. Pfeifer¹, F. Thilker¹, A. Tramposch¹, A. Buchroithner, University of Technology, Austria; ¹FH JOANNEUM, Austria MODAL-BASED FUEL LEVEL ESTIMATION OF CRYOGENIC PROPELLANT TANKS |
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ICAS2026_0683: I.O. Skusa, ITA/Embraer, Brazil; R.N. Calvo, Embraer, Brazil; A.A. Filho, ITA, Brazil OSCILLATORY FAILURE DETECTION IN AIRCRAFT ACTUATION SYSTEMS USING WAVELET TRANSFORM |
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ICAS2026_0684: N. Sorokina¹, W. Bliemetsrieder¹, P. Panchal¹, L. Hein¹, T. Weyh¹; ¹Universität der Bundeswehr München, Germany RECONFIGURABLE MULTILEVEL BATTERY ARCHITECTURE FOR SMALL UAV PROPULSION SYSTEMS |
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ICAS2026_0715: D.C. Lyu¹, J. Fu¹, S.J. Zhao, Beijing Institute of Precision Mechatronics and Controls, China; Y.Y. Wang¹; ¹Beihang University, China AN EMBEDDED PHYSICS-INFORMED NEURAL NETWORK (PINN) FRAMEWORK FOR HIGH-FIDELITY REAL-TIME SIMULATION OF A FLIGHT CONTROL SURFACE ACTUATION SYSTEM |
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ICAS2026_0784: S. Guan¹, J. Fu¹, T.Q. Yang¹, Z.H. Ge¹, T.Y. Zhang², Z.Y. Zhao²; ¹Beihang University, China; ²AVIC Shenyang Aircraft Design Institute, China PERFORMANCE DEGRADATION ANALYSIS OF RESOLVER FAULTS IN ELECTRO-MECHANICAL ACTUATOR |
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ICAS2026_0807: T. Prakash, Larsen and Toubro, India; R.S. Pant, Indian Institute of Technology Bombay, India SIZING OF LINEAR ACTUATORS FOR SPAN EXTENSION OF HALE UAV |
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ICAS2026_0809: I. de Souza Rehder¹, P. Krus, LIU, Brazil; E. Villani¹; ¹ITA, Brazil AUTOMATING SYSTEM MODELING USING LARGE LANGUAGE MODELS |
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ICAS2026_0831: M.G. Tutty¹, S. McKee¹, A. Cenko¹; ¹JAIME AMERICA LLC, Australia NEUROMORPHIC ASCENT: REVOLUTIONISING AIRCRAFT STORES COMPATIBILITY AND INTELLIGENT & AUTONOMOUS SYSTEMS |
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ICAS2026_0833: A.A.J. Oliveira¹, L.H.J. Machado¹, M.S. Ferreira¹, J.P.B. Souza¹, E.J.T. Santos¹, J.V.N. Oliveira¹, P.H.C. Picanço¹; ¹Universidade Federal de Minas Gerais, Brazil STATE-SPACE SIMULATION OF PASSIVE LANDING GEAR IMPACT RESPONSE FOR LIGHTWEIGHT FIXED-WING UAVS |
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ICAS2026_0961: T.Q. Yang¹, J. Fu¹, S. Guan¹, J. Pan², C.F. Yao², H.L. Qu²; ¹Beihang University, China; ²AVIC Xi'an Flight Automatic Control Research Institute, China MECHANISM-DATA FUSION MODELING METHOD FOR AEROSPACE ELECTROMECHANICAL ACTUATION SYSTEMS |
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ICAS2026_0991: Z.C. Xu¹, E. Tang¹, N. Teyssier¹, M.F. Humphreys¹, J. Jiang¹; ¹Imperial College London, United Kingdom LIGHTWEIGHT BIMETALLIC GEARS FOR AEROSPACE TRANSMISSIONS ENABLED BY OPEN-AIR DIFFUSION BONDING |
8 - Manufacturing and Supply Chain Management |
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ICAS2026_0058: M. Tatar¹, L. Branko¹, R.W. Grube¹, R. Noll¹, G.M. Buckus¹, O. Wagner¹; ¹Boeing, United States GAP OPTIMIZATION ADAPTIVE TOOL FOR LARGE SCALE FLEXIBLE STRUCTURE ASSEMBLY |
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ICAS2026_0080: I. Ali¹, C. Silva², E. Villani², J.M. Mello¹, W. Oliveira²; ¹Embraer, Brazil; ²ITA, Brazil EVALUATION OF TRUST AS A HUMAN FACTOR IN COLLABORATIVE ROBOTICS ASSOCIATED WITH ARTIFICIAL INTELLIGENCE APPLIED TO THE AERONATUCAL INDUSTRY |
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ICAS2026_0124: H. Zhang¹, L. Wang¹, D.D. Gu¹; ¹Nanjing University of Aeronautics and Astronautics, China BALANCING STRENGTH AND THERMAL CONDUCTIVITY IN LPBF-PROCESSED ALUMINUM-BASED MATERIALS |
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ICAS2026_0126: L. Xi, China; Z. Wang, China; D.D. Gu, China PROCESS OPTIMIZATION, MANUFACTURING QUALITY AND MECHANICAL PROPERTIES OF HIGH-VOLUME-FRACTION TIB2 REINFORCED AL-BASED COMPOSITES PREPARED BY SELECTIVE LASER MELTING |
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ICAS2026_0140: R. Yang¹, L.K. Yang¹, L. Wei¹, S.Y. Sun¹; ¹Dalian University of Technology, China 3D ANALYSIS AND PREDICTION FOR ASSEMBLY STEP DEVIATIONS OF FOUR-BAR LINKAGE BAY DOORS |
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ICAS2026_0198: A.T. Ferraz¹, C.C.D. Silva¹, J.M.G. Mello, EMBRAER, Brazil; E. Villani¹; ¹ITA, Brazil VIRTUAL COMMISSIONING APPLIED TO ROS AIRCRAFT ROBOTIC CELL |
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ICAS2026_0260: D.-D. Gu, Nanjing University of Aeronautics and Astronautics, China MATERIAL-STRUCTURE INTEGRATED LASER ADDITIVE MANUFACTURING OF HIGH-PERFORMANCE PARTS FOR AERONAUTICAL APPLICATIONS |
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ICAS2026_0270: Y.S. Chen¹, D.D. Gu¹; ¹Nanjing University of Aeronautics and Astronautics, China A NOVEL DUAL-PHASE BAYESIAN ESTIMATION AND MULTI-TASK LEARNING METHOD FOR PROCESS OPTIMIZATION FOR REDUCING LACK-OF-FUSION DEFECTS DURING LASER POWDER BED FUSION |
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ICAS2026_0286: M. Ravandi¹, G. Miris¹, P. Burka¹; ¹AIR Hub, Swinburne University Of Technology, Australia HIGH-RATE AUTOMATED STAMP FORMING OF CF/LM-PAEK COMPOSITES FOR NEXT-GENERATION UAV AEROSTRUCTURES |
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ICAS2026_0651: R. Van Manen¹, K. Van Rijswijk¹, L. Veldenz¹; ¹Stichting Luchtvaart in Transitie, Netherlands THE MAKING OF LUCHTVAART IN TRANSITIE (LIT) AND THE REMAKING OF A STRONG GLOBALLY CONNECTED NATIONAL AERONAUTICS INDUSTRY |
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ICAS2026_0766: Y.A.D. Martins¹, C.C.D. Silva¹, D.A. Rade¹, J.M.G. Mello², A.V.S. Silva², A.P.C. Cuco²; ¹Aeronautics Institute of Technology, Brazil; ²Embraer S. A., Brazil A QUALITATIVE FRAMEWORK FOR AIRCRAFT WING MANUFACTURING AND DECISION MAKING |
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ICAS2026_0825: J.-H. Hong, Korea Institute of Materials Science, South Korea A MULTI-STAGE FORMING APPROACH FOR MANUFACTURING TITANIUM BIPOLAR PLATES FOR FUEL CELLS |
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ICAS2026_0840: T. Mahr¹, L. Whiteman¹, A. Daley¹, S. Hewa Witharange¹, J. Prpic¹, K. Holtta-Otto¹, M. Das¹; ¹University of Melbourne, Australia RE-THINKING END OF LIFE AIRCRAFT INTERIORS THROUGH CO-DESIGN AND REPURPOSING |
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ICAS2026_0945: F. S. Braga¹, E. B. S. de Andrade¹, W. R. de Oliveira¹; ¹ITA, Brazil A FORMALLY VERIFIED, EVENT-DRIVEN ROS SCADA SUPERVISORY SYSTEM ARCHITECTURE FOR SAFETY-CRITICAL ROBOTIC CELLS IN AEROSPACE MANUFACTURING |
9 - Crewed and Uncrewed Aircraft Operations and Traffic Management |
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ICAS2026_0048: S.B. Goeppel¹, E. Asadi¹, E. Itoh, he University of Tokyo, Japan; M. Schultz, University of the Bundeswehr, Germany; ¹University of the Bundeswehr Munich, Germany REDUCING AIR TRAFFIC COMPLEXITY IN JAPANESE AIRSPACE THROUGH MINOR LATERAL TRAJECTORY ADJUSTMENTS |
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ICAS2026_0103: A. Edsel¹, W.A. Crossley¹, D.A. DeLaurentis¹; ¹Purdue University, United States SCHEDULING AND ROUTING FOR TIMETABLE-BOUND URBAN AIR MOBILITY OPERATIONS |
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ICAS2026_0150: D.S. Nithya¹, F. Monteleone¹, V. Muscarello, RMIT University, Australia; G. Quaranta¹; ¹Politecnico di Milano, Italy VERTIPORT FINAL APPROACH AND TAKEOFF AREA ORIENTATION IDENTIFICATION USING COUPLED MICROSCALE WIND AND FLIGHT DYNAMICS ANALYSIS |
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ICAS2026_0178: T. Finck¹, V. Bottino¹, M. Weber¹, B. Korn¹; ¹German Aerospace Center, Germany FLIGHT CENTRIC ATC – HOW TO SOLVE CONFLICTS WITHOUT COMMUNICATION AND COORDINATION OVERLOADS? |
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ICAS2026_0212: T. Ehlers¹, A. Lau¹, M. Mendiguchia Meuser¹, A. Kuenz¹, S. Dietmüller¹, S. Matthes¹; ¹DLR, Germany JOINT TRAJECTORY OPTIMIZATION AND DECONFLICTION FOR CLIMATE IMPACT MITIGATION |
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ICAS2026_0216: R. Sáez¹, R. Pitarque¹, B. Heesbeen, Royal Netherlands Aerospace Centre (NLR), Netherlands; Y.J. Hasan², J. Kurz², D. Vechtel², M. Gerber, Swiss Skylab Foundation (Skylab), Switzerland; ¹Technical University of Catalonia (UPC), Spain; ²German Aerospace Centre (DLR), Germany NEXT-GEN FLAP SYSTEMS: VALIDATION RESULTS AND IMPLICATIONS FOR AIR TRAFFIC MANAGEMENT |
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ICAS2026_0247: H. Akiyama¹, S. Ueno¹, T. Higuchi¹, T. Sakurai¹; ¹Yokohama National University, Japan DESIGN AND FEASIBILITY ASSESSMENT OF TRANSPORT OPERATIONS FOR DELIVERING TYPHOON CONTROL SUBSTANCES |
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ICAS2026_0272: C.S.X. Ng¹, M. Schultz, University of Bundeswehr Munich, Germany; E. Itoh¹; ¹The University of Tokyo, Japan AN AUGMENTED AIRPORT MODEL FOR GROUND OPERATIONS ANALYSIS: A CASE STUDY OF NARITA INTERNATIONAL AIRPORT |
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ICAS2026_0292: K.A. Buchtal¹, A. Lau¹; ¹German Aerospace Center (DLR), Germany THREE-DIMENSIONAL ADAPTIVE TRAJECTORY OPTIMIZATION FOR RPAS-BASED ATMOSPHERIC MEASUREMENTS |
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ICAS2026_0298: G. Wang¹, W. Cheng¹, Y. Wu¹, L. Zhao¹; ¹Aerial Industry Development Research Center of China, China QUANTIFYING LAND AERIAL RESCUE DEMAND INTENSITY: A DATA-DRIVEN MODELING APPROACH FOR DEFINING THE AIR-GROUND OPERATIONAL BOUNDARY |
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ICAS2026_0302: L. Nöhren¹, A. Simon¹, M. Schaper¹; ¹DLR, Germany EVALUATING HUMAN-MACHINE-TEAMING CONCEPTS FOR A HIGHLY AUTOMATED GROUND CONTROLLER WORKING POSITION |
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ICAS2026_0325: P. Sathya Kumar¹, M. Schultz¹, E. Asadi¹; ¹Universität der Bundeswehr München, Germany SIMULATION-BASED EVALUATION OF SIGNALISED INTERSECTIONS FOR EMERGENCY SAFETY LANDINGS IN URBAN AIR MOBILITY |
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ICAS2026_0329: R. Kajikawa¹, N. Takeichi¹; ¹Tokyo Metropolitan University, Japan FEASIBILITY STUDY ON IMPROVING ARRIVAL-SEPARATION STABILITY THROUGH ARRIVAL TRAJECTORY ANALYSIS AT CONGESTED AIRPORTS |
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ICAS2026_0332: N.K. Wickramasinghe, Electronic Navigation Research Institute, Japan; R. Mori, Kobe University, Japan A PEAKS-OVER-THRESHOLD APPROACH TO RUNWAY COLLISION RISK ESTIMATION FOR EFFICIENT ARRIVAL OPERATIONS |
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ICAS2026_0345: B.I. Schuchardt¹, A.J. Torija, University of Salford, United Kingdom; I. Legriffon, Office National d’Études et de Recherches Aérospatiales (ONERA), France; D. Casalino, Delft University of Technology, Netherlands; L. Bertsch¹, R. Aalmoes, Netherlands Aerospace Centre (NLR), Netherlands; ¹German Aerospace Center (DLR), Germany CHALLENGES IN ADVANCED AIR MOBILITY NOISE PREDICTION - FROM SOURCE TO PERCEPTION |
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ICAS2026_0408: E. Asadi¹, G. Enea, MIT Lincoln Laboratory, United States; M. Schultz¹; ¹University of the Bundeswehr Munich, Germany RUNWAY-AWARE CAPACITY ENVELOPES FOR LONG-RANGE ARRIVAL METERING UNDER OPERATING-DIRECTION CHANGES AT SINGAPORE CHANGI |
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ICAS2026_0412: G. Enea¹, V. Mollwitz², T. Finck², T. Reynolds¹, B. Korn²; ¹MIT Lincoln Laboratory, United States; ²DLR Institute of Flight Guidance, Germany A COMPARISON OF TRAJECTORY-BASED OPERATIONS IN THE UNITED STATES AND EUROPE IN SUPPORT OF GLOBAL HARMONIZATION |
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ICAS2026_0446: S. Tsuru¹, A. Andreeva-Mori¹; ¹Osaka Metropolitan University, Japan AIRCRAFT SEQUENCING UNDER UNCERTAINTY: GAME-THEORETIC OPTIMIZATION AND A COMPARATIVE ASSESSMENT OF GLOBAL AND INTRA-AIRLINE COOPERATIVE DECISION FRAMEWORKS |
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ICAS2026_0521: Y. Cho¹, J. Lee¹, Y. Kim¹, C. Jung², S. Kang², J. Kim¹; ¹Sejong University, South Korea; ²TOFF Mobility, South Korea UNDERSTANDING THE IMPACT OF OPERATIONAL VARIABLES ON ELECTRIC AIRCRAFT BATTERY PERFORMANCE VIA REAL-FLIGHT DATA ANALYSIS |
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ICAS2026_0538: M. Xu¹, L. Wang, School of Reliability and Systems Engineering, Beihang universi, China; T. Ma¹, X. Wang, School of Reliability and Systems Engineering, Beihang universit, China; J. Fu¹; ¹Institute of Unmanned System, Beihang University, China A BIONIC-INSPIRED COLLABORATIVE SYSTEM FOR MANNED AND UNMANNED AERIAL VEHICLES IN EMERGENCY RESCUE MISSIONS |
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ICAS2026_0554: Z. Chen¹, Y. Zhao¹, X. Wang¹, W. Dai¹, K.H. Low¹; ¹Civil Aviation University of China, China UNIFIED SEPARATION ASSURANCE FOR MULTI-UAV OPERATIONS: RISK-CALIBRATED BASELINES AND FAULT-AWARE ADAPTIVE RESOLUTION |
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ICAS2026_0568: J. Meier¹, M.-M. Temme¹, R. Hunger¹, S. Shetty¹, M. Hagl¹, O. Ohneiser¹, M. Finke¹; ¹German Aerospace Center (DLR), Germany VALIDATION OF TRADITIONAL COMPETENCY-BASED ASSESSMENT AND EXPERIENCE-BASED AUTHORISATION FOR AIR TRAFFIC CONTROLLERS |
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ICAS2026_0580: Y. Wang¹, J. Guo¹, Y. He¹, F. Wu¹, Z. Gao¹; ¹The Hong Kong University of Science and Technology, Hong Kong SAR of China LOW-NOISE VERTIPORT PROCEDURE PLANNING USING DEEP REINFORCEMENT LEARNING |
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ICAS2026_0587: Y. He¹, Y. Wang¹, F. Wu¹, J. Guo¹, Z. Gao¹; ¹HKUST, Hong Kong SAR of China RECIPROCITY-GUIDED JOINT BASE STATION PLACEMENT AND FLIGHT CORRIDOR PLANNING FOR URBAN AIR MOBILITY |
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ICAS2026_0591: Y. Matsuno¹, H. Matsuda¹; ¹Japan Aerospace Exploration Agency, Japan IMPACT OF DYNAMIC METERING OPERATIONS UNDER ADVERSE WEATHER AND MITIGATION THROUGH OPTIMAL SEQUENCING |
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ICAS2026_0605: F. Wu, China; Y. He, China; J. Guo, China; Y. Wang, China; Z. Gao, China GEOMETRY-DRIVEN AIR TRAFFIC CONFLICT RESOLUTION VIA CAUCHY-STOKES RANDERS METRIC |
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ICAS2026_0666: M. Clococeanu¹, C.M. Weder¹, H. Bruder¹, Z.L. Zengerling¹; ¹German Aerospace Center, Germany GLOBAL EMISSION MONITOR FOR 2023 |
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ICAS2026_0672: M. Swaid, German Aerospace Center (DLR), Germany IMPACT OF BOOKING LEAD TIME ON FLEET AND INFRASTRUCTURE IN URBAN AIR MOBILITY |
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ICAS2026_0682: S. Abdulhak, University of Michigan, Industrial and Operations Engineering, United States; B. Donaldson¹, A. Kamat¹, K. Hu¹, Z. Huang¹, M.Z. Li, University of Michigan, United States; ¹University of Michigan, Aerospace Engineering, United States EXPLORING DETROIT METROPOLITAN WAYNE COUNTY AIRPORT AS A TESTBED FOR RESOLVING INTEGRATION CHALLENGES FOR AIR TAXI OPERATIONS |
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ICAS2026_0697: H. Suizu¹, H. Hirabayashi¹, N. Takeichi, Tokyo Metropolitan University, Japan; ¹Electronic Navigation Research Institute, Japan A PRELIMINARY STUDY ON DYNAMIC AIRSPACE CONFIGURATION USING FLEXIBLE VERTICAL BOUNDARIES IN DOUBLE-LAYER AIRSPACE |
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ICAS2026_0779: K. Sekine¹, T. Tatsukawa, Tokyo University of Science, Japan; Y. Kawagoe, Tohoku University, Japan; E. Itoh¹; ¹The University of Tokyo, Japan EVALUATING IMPACT OF INTERNATIONAL DEPARTURE TIME CONTROL ON DOMESTIC ARRIVAL DELAYS IN JAPAN USING MULTI-OBJECTIVE SIMULATION-BASED OPTIMIZATION |
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ICAS2026_0802: J.S. Lee¹, K.R. Oh¹; ¹Korea Aerospace Research Institute, South Korea ESTIMATION AND ANALYSIS OF RNP REQUIREMENTS FOR HETEROGENEOUS UAM CONFIGURATIONS: INSIGHTS FROM OPPAV DEMONSTRATION |
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ICAS2026_0811: S. Bagassi¹, T. Fadda¹; ¹University of Bologna, Italy AUGMENTED REALITY SAFETY NETS FOR INCREASED AIRPORT SAFETY |
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ICAS2026_0816: P. Singh¹, R.S. Pant¹; ¹IIT Bombay, India LIMITED HORIZON AIRLINE SCHEDULING USING GREY THEORY AND GRASP FRAMEWORK |
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ICAS2026_0838: H.W. Kim¹, Y.J. Eun¹, D.K. Jeon¹; ¹Korea Aerospace Research Institute, South Korea WEATHER-DRIVEN DEEP LEARNING FOR AIRPORT RUNWAY DIRECTION FORECASTING |
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ICAS2026_0860: Y. Iwatsuki, Mitsubishi Research Institute, Inc./ Kyushu University, Japan; A. Harada¹, S. Higashino¹; ¹Kyushu University, Japan SENSITIVITY STUDY OF DEPARTURE TIME ACCURACY FOR AIRPORT COLLABORATIVE DECISION MAKING USING FAST-TIME SIMULATION |
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ICAS2026_0863: S. Kontani¹, R. Mori¹; ¹Kobe University, Japan APPROPRIATE ATC GO-AROUND INSTRUCTION TIMING TO PREVENT RUNWAY COLLISIONS |
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ICAS2026_0870: K. Sumaja¹, T.-R.T. Koo¹, S. Mooney, School of Biological, Earth and Environmental Sciences, UNSW, Australia; T.H. Rashidi¹; ¹School of Civil and Environmental Engineering, UNSW, Australia CLIMATE HAZARD TIMING AND FLIGHT DEMAND COOCCURRENCE: A DEMAND-WEIGHTED EXPOSURE FRAMEWORK |
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ICAS2026_0871: V. Kramar, VTT Technical Research Centre of Finland (VTT) , Finland; L. Asmer¹, B. Schuchardt¹, A. Badea², J. Teutsch², J. Vreeken², E. Sunil², B. Gungen², J. Kok², M. Murça, Technological Institute of Aeronautics (ITA), Brazil; I. Borshchova³, J. Keillor³, L. Pinjala*, A. Hebbar*, G. Madhuranath*, D.M. Manindrakumar*, N. Yokoyama, Japan Aerospace Exploration Agency (JAXA), Japan; H.U. Park, Korea Aerospace Administration (KASA), South Korea; P.H. Kopardekar, National Aeronautics and Space Administration (NASA), United States; ¹German Aerospace Center (DLR) , Germany; ²Royal Netherlands Aerospace Centre (NLR), Netherlands; ³National Research Council Canada (NRC) , Canada; *Council of Scientific & Industrial Research (CSIR), India ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES |
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ICAS2026_0893: H. Seon¹, K. Lee¹, M. Brown², H. Hirabayashi²; ¹Korea Aerospace University, South Korea; ²Electronic Navigation Research Institute, Japan AIRCRAFT CLIMB PROFILE PREDICTION VIA MACHINE LEARNING-BASED FRAMEWORK |
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ICAS2026_0897: M. Corsi, DLR German Aerospace Center, Institute of Flight Guidance, Germany; K. Schweiger¹, C. Bettremieux¹, C. Nava Gaxiola², A. Mangas Pita², M. Hardt³, A. Tutku Altun³, S. McNamee Freire, URBANV S.p.A., Italy; G. Riccardi, ENAV S.p.A., Italy; E. Fornaciari, D-Flight S.p.A., Italy; ¹EUROCONTROL Innovation Hub, France; ²AENA S.M.E., Spain; ³Boeing Aerospace Spain, Spain ADVANCING TRAFFIC MANAGEMENT SERVICES FOR VERTIPORT OPERATIONS IN EUROPE: INSIGHTS FROM THE EUREKA PROJECT |
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ICAS2026_0900: A. Tiwari¹, R.S. Pant¹; ¹Indian Institute of Technology Bombay, India OPTIMISATION OF OPERATING RADII FOR DRONE WAREHOUSES |
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ICAS2026_0946: F. Naeem¹, V. Gollnick¹; ¹Hamburg University of Technology, Germany STANDARDIZED TAKE-OFF AND LANDING PROCEDURES FOR AIR TAXIS: URBAN AIR MOBILITY |
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ICAS2026_0995: T.L. Teck, Changi Airport Group, Singapore; D.S. Man Fung, Institutions of Engineers, Singapore INNOVATION & TRANSFORMATION AT SINGAPORE CHANGI AIRPORT AND A CASE STUDY ON AI-ENABLED LINE MAINTENANCE OPERATIONS |
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ICAS2026_1003: A. Dickinson, Qantas Airways Limited, Australia FLIGHT PLANNING, THE FORGOTTEN ASSET |
10 - Safety and Security |
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ICAS2026_0038: A. Reisier¹, M.M. Cardoso-Junior¹; ¹Technological Institute of Aeronautics, Brazil ACCELERATING THE LEARNING CURVE: GENERATIVE AI FOR WORKED EXAMPLES IN HUMAN FACTORS ANALYSIS |
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ICAS2026_0041: J. Armstrong¹, O.M. Ozcakir¹, L.L. Waite¹, T. Austin¹, C.A. Pepper¹, A. Tvaryanas², H. Uyhelji², S. Gearhart, US CDC, United States; P. Lebbin, Canadian NRC, Canada; I.S. Koolhof¹; ¹Boeing, Australia; ²FAA, United States A MODEL OF DISEASE TRANSMISSION AND MITIGATION OPTIONS FOR AVIATION FROM GATE BOARDING TO IN-FLIGHT, A BOEING/FAA/US CDC AND CANADIAN NRC COLLABORATION. |
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ICAS2026_0056: B.R.C. Molesworth, UNSW Sydney, School of Aviation, Australia; M. Burgess, UNSW Sydney, School of Built Environment, Australia QUANTIFYING THE EFFECT OF IN-CABIN NOISE ON COGNITION |
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ICAS2026_0059: B. Molesworth¹, D. Estival¹, L. Chow¹; ¹UNSW, Australia FACTORS AFFECTING COMMUNICATION IN AVIATION |
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ICAS2026_0086: Y. Yan¹, S. Boufous¹, B.R.C. Molesworth¹; ¹School of Aviation, University of New South Wales, Australia A HUMAN-CENTRIC APPROACH TO UNDERSTANDING THE CONTRIBUTING FACTORS OF PILOT-RELATED RUNWAY INCURSIONS |
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ICAS2026_0091: W.D. Xiao¹, C.L. Zhao, Shanghai Aircraft Design and Research Institute, China; Y. Gao¹, Y.Y. Lu¹, S. Fu¹; ¹Shanghai Jiao Tong University, China PILOT WORKLOAD PROFILES UNDER CONTINUOUS MULTI-TASKING AND SPARSE EVENTS VIGILANCE |
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ICAS2026_0118: A. Lemetti¹, L. Meyer², M. Peukert², T. Polishchuk¹, C. Schmidt¹, H. Alpfjord Wylde²; ¹Linköping University (LiU), Sweden; ²Air Navigation Services of Sweden (LFV), Research & Innovation, Sweden UNCERTAINTY ANALYSIS AND EYE-TRACKING-BASED CLUSTERING IN AIR TRAFFIC CONTROLLER WORKLOAD PREDICTION |
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ICAS2026_0154: A. Reis¹, C. Lessa¹, P. Kurka¹, R. Santos Alencar, ITA , Brazil; M. Machado Cardoso Júnior ¹; ¹ITA, Brazil WHO SHOULD SIT AT THE EXIT ROW? A HUMAN FACTORS APPROACH TO EMERGENCY EVACUATION PASSENGER SELECTION IN COMMERCIAL AVIATION |
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ICAS2026_0192: J.I. González Cabeza¹, S. Petersen¹, J.-P. Buch¹, D. Niedermeier¹, M. Wies¹, A. Papenfuß¹; ¹DLR e.V., Germany ASSESSING AN ALTERNATE AIRPORT ASSISTANT |
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ICAS2026_0210: J.M. Christensen¹, T. Stefani¹, E. Hoemann¹, F. Köster¹, S. Hallerbach¹; ¹German Aerospace Center, Germany ON THE APPLICABILITY OF SAFETY NETS: A SAFETY-BY-DESIGN SOLUTION FOR CERTIFYING NEURAL NETWORKS |
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ICAS2026_0291: R. Hähnel, German Aerospace Centre (DLR), Germany EVALUATION OF METHODS FOR ANOMALY DETECTION IN THE APPROACH PHASE OF OPERATIONAL FLIGHT DATA |
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ICAS2026_0307: B. Rietdijk¹, B. Sulejmanovic¹, R. Coertze¹; ¹Conscious Aerospace BV, Netherlands CONCEPT OF OPERATIONS FOR A HYDROGEN-ELECTRIC POWERED MODIFIED DASH 8-300 REGIONAL AIRCRAFT: PERFORMANCE, OPERATIONAL, AND REGULATORY IMPACTS |
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ICAS2026_0363: T. Treichl, German Aerospace Center, Germany; T.S. Paul, Thales France, France TOWARDS THE INTEGRATION OF NEUROPHYSIOLOGICAL SIGNALS AND HUMAN BODY DYNAMICS FOR ADAPTIVE CONTROL ALLOCATION |
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ICAS2026_0422: C.R. Vindigni¹, A. Esposito¹, C. Orlando¹, A. Alaimo¹; ¹University of Enna Kore, Italy HRV BASED PILOTS WORKLOAD PREDICTION FOR AN INTELLIGENT COCKPIT WARNING SYSTEM |
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ICAS2026_0439: Y.H. Mei¹, Z.H. Wang¹; ¹The university of Sydney, Australia EARLY WARNING FOR POTENTIAL BIRD STRIKES: STRATEGIC OPTIMIZATION OF PAN-TILT-ZOOM SENSOR NETWORKS FOR BIRD HAZARD DECREASE IN AIRPORT ENVIRONMENT |
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ICAS2026_0457: J. Gao¹, T.Q. Wang, Taiyuan University of Technology, China; H. Gao¹, Y. Ding¹, Z. Wan¹; ¹ University of Sydney, Australia TEMPORAL INJECTION FOR REAL-TIME FLYING-BIRD DETECTION WITH RT-DETR |
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ICAS2026_0536: T. Stefani¹, J.M. Christensen¹, E. Hoemann¹, F. Koester¹, S. Hallerbach¹; ¹DLR, Germany COVERAGE-DRIVEN VERIFICATION FOR SAFETY-BY-DESIGN IN AI-BASED COLLISION AVOIDANCE SYSTEMS |
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ICAS2026_0685: A. Chappell¹, S. Karunathilake¹, A. Comer¹, P. Saravanan¹; ¹Oklahoma State University, United States SUBSCALE FLIGHT TRAINING EFFECTS ON PILOT WORKLOAD AND PERFORMANCE DURING VTOL HQTES |
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ICAS2026_0701: C.A. Dautel¹, M. Werthwein¹, M. Homolya¹, M. Lehmann¹, S. Queiroz¹, B. Annighoefer¹; ¹University of Stuttgart, Institute of Aircraft Systems (ILS), Germany VLSEC: A CONCEPT FOR SECURING VIRTUAL LINKS IN AVIONICS NETWORKS THROUGH CENTRALIZED GROUP KEY MANAGEMENT |
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ICAS2026_0782: J. Gao¹, T. Wang, Taiyuan University of Technology, China; H. Gao¹, Y. Ding¹, Z. Wang¹; ¹ University of Sydney, Australia RINGCO-DETR: INFERENCE-NEUTRAL STABILIZATION OF ORIENTED TRANSFORMER DETECTION FOR AERIAL SENSING |
11 - Operations and Sustainment |
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ICAS2026_0010: N. Ahmed, Sudan REBUILDING AGRICULTURAL STATISTICS IN POST-WAR SUDAN: A STRATEGIC FRAMEWORK FOR RECOVERY AND RESILIENCE |
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ICAS2026_0031: H. Nakamura, The University of Tokyo, Japan ASSESSING AIRLINE PURCHASE MOTIVATION FOR HYDROGEN AIRCRAFT UNDER FUTURE CORSIA |
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ICAS2026_0134: D. Tang¹, W. Yang¹, J. Xuan¹; ¹Northwestern Polytechnical University, China LIGHTWEIGHT AND ROBUST REAL-TIME DETECTION SYSTEM FOR AIRCRAFT SKIN DEFECTS UNDER COMPLEX UAV INSPECTION CONDITIONS |
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ICAS2026_0159: S. Zhu¹, J. Panta¹, R. Yang¹, Y.X. Zhang, Univeristy of Technology Sydney , Australia; ¹Western Sydney University, Australia FEMTOSECOND LASER PAINT STRIPPING ON AIRCRAFT COATINGS: EXPERIMENTAL AND NUMERICAL ASSESSMENT |
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ICAS2026_0222: S.I. Hallstedt¹, P.L.Y. Léonard¹, M. Aldèn¹, G. Dokter¹, O. Isaksson¹; ¹Chalmers University of Technology, Sweden KEY STAKEHOLDERS IN AEROSPACE FOR A SUSTAINABLE AND CIRCULAR PRODUCT DEVELOPMENT - A SYSTEMATIC APPROACH |
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ICAS2026_0244: J. Rogers, RMIT University, Australia; I. Field¹, N. Tugwell¹, M. Salagaras¹, B. Dixon¹; ¹DSTG, Australia ACCELERATED EXPERIMENTAL INVESTIGATION OF ENVIRONMENTALLY ASSISTED CRACKING IN AA7085 |
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ICAS2026_0264: L.Y. Hou¹, J.T. Liu¹, Y.L. Song¹, H. Xiao¹; ¹Nanjing University of Aeronautics and Astronautics, China PARAMETER INVERSION ALGORITHM FOR AERO-ENGINE γ-PHOTON FLOW FIELD IMAGES BASED ON UNET-GAN ARCHITECTURE |
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ICAS2026_0315: Z.L. Zengerling¹, A. Lau¹, M. Clococeanu¹, R. Kanitz¹, J. Schwengler², A. Vogel², K. Abu-Taa²; ¹German Aerospace Center (DLR), Germany; ²Rolls-Royce Deutschland, Germany FLIGHT MISSION MODELING WITH VARYING BASELINE DATA: APPLICAITON IN BUSINESS AVIATION |
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ICAS2026_0396: N. Barry¹, C. Gallagher¹, C. Stuart¹; ¹Trinity College Dublin, Ireland INVESTIGATION OF DECARBONISATION PATHWAYS FOR SHORT HAUL AVIATION USING A DISCRETE OPTIMISATION DECISION-MAKING ALGORITHM |
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ICAS2026_0451: J. Roesing, RWTH Aachen University, Germany LIFE CYCLE ANALYSIS OF EMISSIONS IN AVIATION: IDENTIFIYING AND ADJUSTING FACTORS TO REDUCE CARBON EMISSIONS |
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ICAS2026_0573: L. Jilke¹, M. Schubert¹, N. Hosters², F. Raddatz¹, M. Behr², G. Wende¹; ¹German Aerospace Center (DLR), Germany; ²RWTH Aachen University, Germany PHYSICS-INFORMED NEURAL NETWORKS FOR ULTRASONIC LAMB WAVE RECONSTRUCTION IN NON-DESTRUCTIVE TESTING |
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ICAS2026_0611: M. Schultz¹, S. Göppel¹, S. Reitmann, University of Technology Chemnitz, Germany; ¹University of the Bundeswehr Munich, Germany PROVIDING SENSOR INFORMATION FOR BOARDING TIME PREDICTION |
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ICAS2026_0710: A. Apostolidis, KLM Royal Dutch Airlines, Netherlands; K.P. Stamoulis, Amsterdam University of Applied Sciences, Netherlands FROM DATA TO DECISIONS: A CONCEPTUAL FRAMEWORK FOR DATA-DRIVEN AIRLINE OPERATIONS AND SUSTAINMENT |
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ICAS2026_0716: C. Klein¹, E. Arts¹, B. Atanasoaie¹, H. Meyer¹, F. Raddatz¹, Z. Daw, University of Stuttgart, Institute of Aircraft Systems, Germany; ¹German Aerospace Center (DLR), Germany ONTOLOGY-BASED SENSOR HEALTH MONITORING: A DYNAMIC ONTOLOGY-BASED FAULT DETECTION AND CLASSIFICATION FOR TIMESERIES DATA |
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ICAS2026_0738: V. Kekoc, Defence Science and Technology Group, Australia; M. Scott¹, W.J.C. Verhagen¹, P. Marzocca¹; ¹RMIT University, Australia EXPLAINABLE NATURAL LANGUAGE PROCESSING FOR AIRCRAFT STRUCTURAL INTEGRITY DEFECT CLASSIFICATION |
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ICAS2026_0770: M. Kim¹, S.-H. Jeong¹, I. Lee¹, B. Shim¹; ¹Korea Aerospace Industries, LTD, South Korea AI-BASED MAINTENANCE CODE CORRECTION FOR RELIABLE MTBF ANALYSIS |
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ICAS2026_0803: E. Yoshikawa¹, S. Horishita², Y. Hamada², T. Ushio¹, V. Chandrasekar, Colorado State University, United States; ¹The University of Osaka, Japan; ²Japan Aerospace Exploration Agency, Japan ON THE FEASIBILITY OF MACHINE LEARNING-BASED DETECTION OF AIRCRAFT LIGHTNING STRIKE RISK AREAS |
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ICAS2026_0822: A. Sanchez Mata, SANMATC Aircraft Technical & Financial Consulting, Mexico; E. Espinosa Juarez¹, A.M. Zarate Villazon², B. Ravikanti², H. Szöke-Erös³, P. Shiva Prakasha³, L. Knöös Franzén¹; ¹Linköping University, Sweden; ²Georgia Institute of Technology, United States; ³German Aerospace Center (DLR), Germany LOSS OF RELIABILITY OF NEW GENERATION ENGINES: THE CASE STUDY OF THE PW1100G ENGINE RECALL ON MEXICAN AVIATION AS A SYSTEM OF SYSTEMS |
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ICAS2026_0856: Z. Huang¹, D. Xiao¹, X. Guo¹, L. Zhao¹, C. Song¹; ¹Northwestern Polytechnical University, China PERFORMANCE DEGRADATION ASSESSMENT METHOD FOR AERO-ENGINES ACROSS THE FULL-LIFE-CYCLE BASED ON DIGITAL TWIN |
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ICAS2026_0914: A. Filippatos¹, D. Markatos¹, T. Kalampoukas¹, N. Raptis¹, M. Abouhamzeh², K. Stamoulis², S. Pantelakis¹; ¹Department of Mechanical Engineering & Aeronautics, University o, Greece; ²Faculty of Technology, Amsterdam University of Applied Sciences, Netherlands TOWARDS INTEGRATING MAINTENANCE, REPAIR, AND OVERHAUL (MRO) ASPECTS INTO SUSTAINABILITY-DRIVEN DESIGN OF AIRCRAFT STRUCTURES: INSPECTABILITY ASSESSMENT OF HAT-STIFFENED PANELS |
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ICAS2026_1034: A. Dadashi, DLR, Germany DATA-DRIVEN TECHNOLOGY INTELLIGENCE: AN APPLICATION TO AIRCRAFT ENGINE MAINTENANCE |
12 - Host Nation (by personal invitation only) |
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ICAS2026_0195: D. Skrna¹, M. de Rosa Jacinto¹, L. Frei¹, B. Mittenecker¹, J. Nagl¹, H. Mad¹, M. Berens¹; ¹Technische Universität Wien, Austria AERODYNAMIC AND AEROACOUSTIC ASSESSMENT OF 3D PRINTED AAM PROPELLER BLADES WITH SURFACE TREATMENTS |
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ICAS2026_0912: K. Benameur¹, M. Jacinto, TU Wien, Austria; F. Simon¹, L. Bertsch², B. Schuchardt²; ¹ONERA, France; ²DLR, Germany IFAR 2025 PERSPECTIVES ON NOISE REDUCTION FOR EMERGING AND CONVENTIONAL AIR TRANSPORT |
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ICAS2026_0947: R. Fernandes Viana¹, C. Rutili de Lima¹, V. Abrão S. Marques, Federal University of Triângulo Mineiro, Brazil; M. Condé Rocha Murça¹, M. R. O. A. Maximo¹, Q.F. Carlos Henrique¹; ¹Aeronautics Institute of Technology, Brazil A SEMI-AUTONOMOUS DECISION SUPPORT TOOL FOR ATC IN EN-ROUTE REROUTING OPERATIONS |
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ICAS2026_0964: W. Klimczyk¹, P. Kekus-Kumor¹, M. Rajek¹, A. Sieradzki¹; ¹Lukasiewicz Research Network - Institute of Aviation, Poland RECENT ADVANCES IN AEROACOUSTIC DESIGN OF ADVANCED AIR MOBILITY VEHICLES |
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ICAS2026_1001: C. Mertens, Royal Netherlands Aerospace Centre, Netherlands ON THE GROUND AND IN FLIGHT: AERODYNAMIC AND AEROELASTIC TESTING SUPPORTING INNOVATION IN AERONAUTICS |
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ICAS2026_1002: M. Lugrin, ONERA, France UNDERSTANDING HYPERSONIC BOUNDARY LAYER LAMINAR TO TURBULENT TRANSITION IN WIND TUNNEL ENVIRONMENT |
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ICAS2026_1007: C. Bahm, United States X-59: PART 2 BY C.M.BAHM AND P.G.COEN |
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ICAS2026_1021: D. Verstraete, Australia EVTOL AND PROPULSION R&D IN THE SYDNEY PROPULSION LAB |
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ICAS2026_1084: K. Stevens, Australia OPTIMISING THE HUMAN FACTORS IN ADVANCED AIR MOBILITY |
14 - Education and Training |
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ICAS2026_0380: C. Varriale¹, F. Angioni¹; ¹Delft University of Technology, Netherlands INTERACTIVE NOTEBOOKS TO BRIDGE THE DIDACTIC GAP BETWEEN CALCULUS AND FLIGHT PERFORMANCE OPTIMIZATION |
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ICAS2026_0453: J. Abulawi, HAW Hamburg, Germany; P. Raj, Virginia Tech, United States PREPARING AERONAUTICAL ENGINEERING UNDERGRADUATES FOR WORKING IN GLOBAL TEAMS |
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ICAS2026_0464: M.A. Higinio¹, M.J. Scott¹, W.J.C. Verhagen¹; ¹RMIT University, Australia A MIXED REALITY FRAMEWORK FOR EVALUATING AIRCRAFT PRE-FLIGHT WALK-AROUND TRAINING |
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ICAS2026_0549: K. Ramotsabi¹, L. Strydom¹, L. Zwane¹; ¹CSIR, South Africa REFLECTIONS ON THE AEROSPACE ENGINEERING DEVELOPMENT PROGRAMME AT THE CSIR |
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ICAS2026_0639: A.M. Zarate Villazon¹, E. Espinosa-Juarez, Linköping Universitet, Sweden; F. Perez Fuentes, Consejo Mexicano de Educacion Aeroespacial, Mexico; D.N. Mavris¹; ¹Georgia Institute of Technology, United States TOWARDS AN ECOSYSTEM FOR AERONAUTICAL RESEARCH IN MEXICO |
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ICAS2026_0692: P.B. Kurka¹, E. Villani¹; ¹Aeronautics Institute of Technology, Brazil FROM DATA TO DEBRIEF: A FRAMEWORK FOR PILOT PERFORMANCE ASSESSMENT |
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ICAS2026_0718: N. Moser¹, N. Singer¹, V. N. Mueller¹, T. Siemer¹, F. Daoud¹; ¹TU Munich, Germany AN INDIVIDUALISED, SCALABLE PROJECT-BASED LEARNING FRAMEWORK FOR STRUCTURE DESIGN COURSES ESTABLISHED IN A LARGE AEROSPACE STUDY PROGRAMME |
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ICAS2026_0827: B. Sebastiani¹, M. Stefanetti¹, F.D. Fabozzi¹, A. Bitelli¹, N. Cognolato¹, L. Linguerri¹, T. Fadda¹, S. Bagassi¹; ¹University of Bologna, Italy DESIGN, BUILD AND TEST A FULLY AUTONOMOUS UAV FOR HUMANITARIAN AID DELIVERY |
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ICAS2026_0933: L.H.J. Machado¹, J.L.C. Reis¹, M. Lott², R. Carlana²; ¹Universidade Federal de Minas Gerais, Brazil; ²Boeing, Brazil AN MBSE-ORIENTED FRAMEWORK FOR AEROSPACE SYSTEMS EDUCATION: THE CEA-UFMG LIGHT-AIRCRAFT DESIGN-BUILD-TEST TRADITION |
15 - Guest lectures |
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ICAS2026_0177: J. Würfel¹, B. Djartov¹, M. Friedrich¹, S. Schog¹, A. Papenfuss¹; ¹German Aerospace Center (DLR), Germany EXPLAINABILITY AT ALL LEVELS OF SYSTEM DEVELOPMENT: INSIGHTS FROM THE DESIGN OF INTELLIGENT SYSTEMS IN AVIATION |
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ICAS2026_0359: A. Mayima¹, C. Bejarano Espada¹, A. Gampe², A. Hamann², R. De Masellis¹, A. Fuchs¹, M. Athanasiadou¹, H. Palop¹, D. Watkins¹; ¹Collins Aerospace, Applied Research & Technology, Ireland; ²German Aerospace Center, Institute of Flight Guidance, Germany APPLYING HUMAN-CENTERED DESIGN: A PRACTICAL CASE STUDY DEVELOPING AN AI-BASED DIGITAL ASSISTANT FOR PILOTS |
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ICAS2026_0450: J.P.A. Dantas¹, J.A. Cunha¹, G. Dietzsch¹; ¹Instituto de Estudos Avançados, Brazil OFFLINE MULTIMODAL LARGE LANGUAGE MODELS FOR DECISION SUPPORT IN AIR OPERATIONS |
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ICAS2026_0547: R. De Masellis¹, A. Fuchs¹, A. Mayima¹, C. Bejarano Espada¹, M. Athanasiadou¹, H. Palop¹, D. Watkins¹; ¹Collins Aerospace, Applied Research & Technology, Italy AI IN THE COCKPIT: THE JARVIS STORY |
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ICAS2026_0758: C. Bahm, United States X-59: THE FIRST CHAPTER IN THE QUESST FOR QUIET COMMERICAL SUPERSONIC FLIGHT |
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ICAS2026_0769: R.E. Bailey¹, S.P. Williams¹, J.J. (Trey) Arthur¹, K.S. Kibler¹; ¹NASA, United States X-59 EXTERNAL VISION SYSTEM FLIGHT TESTING |
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ICAS2026_0839: M. Boucher, United States X-59 FLIGHT DYNAMICS AND CONTROL |
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ICAS2026_0975: A. Filippatos¹, T. Kyriazis¹, S. Pantelakis¹, D. Markatos¹; ¹Department of Mechanical Engineering and Aeronautics, University, Greece AI-ASSISTED DESIGN OF HOLISTICALLY SUSTAINABLE AEROSTRUCTURES |
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ICAS2026_0976: G. Alonso-Rodrigo, Universidad Politecnica de Madrid, Spain CHALLENGES AND BREAKTHROUGHS IN AIR TRANSPORT SYSTEM: VISION FROM EUROPE |
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ICAS2026_0981: O. Isaksson¹, T. Grönstedt¹, S.I. Hallstedt¹, A. Brahma¹, R. Avellan, GKN Aerospace, Sweden; T. Kipouros, Cambridge University, United Kingdom; ¹Chalmers University of Technology, Sweden CURRENT AND ALTERNATIVE PROPULSION SYSTEMS IN EUROPE; TECHNOLOGIES AND THEIR INTEGRATION |
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ICAS2026_0982: R. Wahls, United States GLOBAL SUSTAINABLE AVIATION PANEL DISCUSSION WITH VERONIQUE ROCA, ALAN NEWBY, JIM HILEMAN, CHRISTINE ANDREWS, RICH WAHLS AND CLAIRE WAGHORN (DURATION 100 MINUTES) |
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ICAS2026_0983: N. Madavan, NASA, United States; M. Fischer, DLR, Germany NASA RESEARCH FOR AIRLINERS OF 2050 AND BEYOND / DLR\'S PERSPECTIVES & PROGRESS ON AIRLINERS FOR 2050+ ENERGY LANDSCAPES |
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ICAS2026_0984: F. Nicolosi¹, M. Di Stasio¹; ¹UNINA, Italy OVERVIEW OF CRITICAL ISSUES AND OPPORTUNITIES FOR NEW A/C WITH HYBRID AND FULL-ELECTRIC POWERTRAIN |
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ICAS2026_0985: E. Mason, Australia JET ZERO: ATJ SAF PROJECT DEVELOPER |
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ICAS2026_0986: M. Suzuki, Japan JAL’ CHALLENGE TO THE NET-ZERO GH GAS EMISSION |
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ICAS2026_0987: M. Drake, United States BOEING PRODUCT DEVELOPMENT - CHALLENGES AND OPPORTUNITIES IN SUSTAINABILITY |
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ICAS2026_0988: P. Burka¹, P. Smith¹; ¹Swinburne University of Technology, Australia A HOLISTIC APPROACH TO ENABLE ADVANCED AIR MOBILITY FOR REGIONAL, RURAL AND REMOTE AUSTRALIA |
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ICAS2026_0989: M. Tormalm, Sweden THE GARTEUR GROUP OF RESPONSABLES IN AERODYNAMICS (GOR AD) AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES |
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ICAS2026_0990: T. Citron, United States APPLICATION OF AI IN AEROSPACE AND IMPLICATIONS FOR AEROSPACE ENGINEERS |
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ICAS2026_0992: J. Hileman, United States ECONOMIC, ENVIRONMENTALLY SUSTAINABLE AVIATION ENERGY |
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ICAS2026_0993: G. Bezos OConnor, United States AEROSPACE ELECTRIFICATION - DEVELOPMENT AND TEST FOR MORE ELECTRIFIED AIRCRAFT |
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ICAS2026_0994: J.-H. Kim, Seoul National University, South Korea COMBINED IMPACT OF JET STREAM AND TURBULENCE ON LONG-TERM TRANS-OCEANIC FLIGHT ROUTES |
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ICAS2026_0996: P. Catalano, C.I.R.A., Italy GARTEUR AG59 IMOLA: IMPROVING THE MODELLING OF LAMINAR SEPARATION BUBBLES |
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ICAS2026_0997: J. Hileman, The Boeing Company, United States PROGRESS IN AIRCRAFT-BASED METEOROLOGICAL OBSERVATIONS |
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ICAS2026_1004: F. Laurin¹, Y. Delgado González, NLR, Netherlands; S. Reh, DLR, Germany; A. Russo, 4Università degli Studi della Campania , Italy; C. Footer, QINETIQ, United Kingdom; F. Roudolff¹; ¹ONERA, France CHARACTERIZATION AND MODELLING OF CERAMIC MATRIX COMPOSITES SUBMITTED TO SEVERE THERMO-MECHANICAL LOADING |
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ICAS2026_1005: M.L. Montero-Sistiaga¹, M. de Smit¹, A. Pastor Muro², N. Redondo Torrico², M. Thomas³, A. Morel³, S. Drawin³, F. Palm, Airbus, Central Research & Technology (CRT), Germany; ¹Royal NLR-Netherlands Aerospace Centre, Netherlands; ²National Institute of Aerospace Technology (INTA), Spain; ³DMAS, ONERA, France ADDITIVE MANUFACTURING OF NOVEL HIGH STRENGTH ALUMINIUM ALLOYS |
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ICAS2026_1006: F.J. San Millán¹, J. Garcia-Martinez¹, P. Pflueger Tejero¹, I. Martinez Teres¹, U. Dincer², M. Misol, Germany; P. Wierach², A. Riccio³, A. Garofano³, M. Battaglia³, J. Berthe*, R. Ortiz*, J. Germain*, F. Roudolff*, W.W. Witsº, B. Noordmanº, O. Erartsinº, J. de Kruijk, Netherlands; ¹INTA, Spain; ²DLR, Germany; ³University of Campania, Italy; *ONERA, France; ºNLR, Netherlands MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS |
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ICAS2026_1008: A. Murphy, United States PRATT & WHITNEY: MEETING THE FUTURE PROPULSION NEEDS OF COMMERCIAL AVIATION |
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ICAS2026_1009: R. Elia, Univesity of Campania Luigi Vanvitelli, Italy; P. Bieber¹, D. Pascarella, CIRA, Italy; M. Rak, University of Naples Federico II, Italy; C. Döll¹; ¹ONERA, France AI IN AVIATION CYBERSECURITY RISK ASSESSMENT: OPPORTUNITIES AND CHALLENGES |
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ICAS2026_1010: C.-A. Andrews, GE Aerospace, United States CFM INTERNATIONAL'S RISE PROGRAM: A STEP-CHANGE FOR DURABILITY AND EFFICIENCY |
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ICAS2026_1011: E. Andrés Pérez¹, D. Quagliarella, CIRA, Italy; D. Hines Chaves², P. Bekemeyer², T. Taddei, Sapienza University of Rome, Italy; J. Peter, Onera, France; O. Amoignon, FOI, Sweden; A. Alaia³, A. Scardigli³, R. Castellanos, UC3M, Spain; J. Nieto-Centenero¹; ¹INTA, Spain; ²DLR, Germany; ³OPTIMAD/ESTECO, Italy GARTEUR RESEARCH GROUP AG60 EXPERIENCE AND ACTIVITIES ON MACHINE LEARNING AND DATA-DRIVEN APPROACHES FOR AERODYNAMICS AND UNCERTAINTY QUANTIFICATION |
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ICAS2026_1013: William Dean Donovan, DiamondStream Partners, United States PRACTICAL INNOVATION IN AEROSPACE |
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ICAS2026_1015: X.S. Zheng, United States; J. Mukhopadhaya, United States; J. Benoit, United States; S.N. Kumar, United States; D. Rutherford, United States; D. Rhode, Germany; D. Sitompul, United States AVIATION VISION 2050: THE POTENTIAL FOR CLIMATE NEUTRAL GROWTH |
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ICAS2026_1016: A. Murphy, United States A MULTI-FUEL PROPULSION SYSTEM STRATEGY FOR AVIATION TRANSPORT RESILIENCE |
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ICAS2026_1017: J. Porter, Australia THE ROLE OF COMMUNITY ENGAGEMENT IN INTRODUCING UNMANNED AERIAL VEHICLE TECHNOLOGY: A RAPID SCOPING REVIEW |
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ICAS2026_1018: D. Gueyffier, ONERA, France HYBRID AI-SIMULATION FOR AERODYNAMICS APPLICATIONS |
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ICAS2026_1019: M. Hudson, Austria THE WHOLE JOURNEY: PEOPLE, PLANET AND PROGRESS AT QANTAS |
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ICAS2026_1020: A Krein, Clean Aviation, Germany SETTING THE STAGE FOR THE GLOBAL SUSTAINABLE AVIATION TRACK WITH GLOBAL AIRLINES |
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ICAS2026_1023: V Roca, Airbus SAS, France AIRBUS PRODUCT DEVELOPMENT - CHALLENGES AND OPPORTUNITIES IN SUSTAINABILITY |
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ICAS2026_1024: F. Haselbach, Germany AIRBUS\' PERSPECTIVES & PROGRESS ON AIRLINERS FOR 2050+ ENERGY LANDSCAPES |
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ICAS2026_1026: V di Nucci, Embraer, Brazil EMBRAER'S PERSPECTIVES & PROGRESS TOWARDS NEXTGEN AIRLINERS |
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ICAS2026_1027: C. Waghorn, New Zealand FUTURE SUSTAINABLE AVIATION INFRASTRUCTURE: PROSPECTS & CHALLENGES FROM CHRISTCHURCH AIRPORT\'S PERSPECTIVE |
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ICAS2026_1028: P Panel, PANEL DISCUSSION Q&A WITH THE AIRLINES |
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ICAS2026_1029: P Panel, PANEL DISCUSSION Q&A WITH THE AIRCRAFT OEMS |
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ICAS2026_1031: P Panel, PANEL DISCUSSION Q&A WITH THE SPEAKERS |
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ICAS2026_1032: P Panel, PANEL DISCUSSION Q&A WITH THE SPEAKERS |
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ICAS2026_1035: R. Burbidge, Belgium ADAPTING AVIATION TO A CHANGING CLIMATE: A GLOBAL AND REGIONAL PERSPECTIVE |
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ICAS2026_1037: T Newby, Rolls-Royce plc, United Kingdom RR PERSPECTIVES & PROGRESS ON NEXTGEN PROPULSION FOR FUTURE AIRLINERS |
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ICAS2026_1038: 1 Panel, PANEL DISCUSSION |
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ICAS2026_1042: S. Pate, United States DESIGN AND DEVELOPMENT OF A BLENDED WING BODY CONCEPT USING AUGMENTED INTELLIGENCE FOR SYSTEMS ENGINEERING |
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ICAS2026_1043: O. Pinon-Fischer, United States BEYOND AI HYPE: TRUST, EVALUATION, AND HUMAN JUDGEMENT IN AEROSPACE ENGINEERING |
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ICAS2026_1044: D. Moreau, UNSW, Australia LOW MACH NUMBER AEROACOUSTICS R&D AT UNSW SYDNEY |
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ICAS2026_1045: K.C. Wong, Australia DRONE TECHNOLOGIES IN AUSTRALIA: FROM AIR-VEHICLE DEVELOPMENT TO AUTONOMOUS FLIGHT SYSTEMS |
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ICAS2026_1046: M. Rivers, United States ECOSYSTEM UPDATES AND PLANS |
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ICAS2026_1047: 1 Q, PANEL DISCUSSION AND Q&A |
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ICAS2026_1048: &A Q, PANEL DISCUSSION AND Q&A |
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ICAS2026_1049: P. Krus, Sweden; V. Kaster Marini, Sweden A CASE STUDY OF CONTEXT OPERATIONS WITH LARGE LANGUAGE MODELS FOR THE SYSTEMS ARCHITECTURE DESIGN OF A HEAVY SAR UAV |
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ICAS2026_1050: A. Neely, Australia EXPERIMENTAL DEVELOPMENT OF HIGH-SPEED AEROSPACE SYSTEMS: CHALLENGES & OPPORTUNITIES |
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ICAS2026_1051: S. Geisbauer, DLR, Germany; S. Shaw, MBDA, United Kingdom TOWARDS CERTIFICATION BY ANALYSIS: A MILITARY AIRWORTHINESS PERSPECTIVE |
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ICAS2026_1052: M. Amano, Japan EXPLORING AIRWORTHINESS CBA: A STALL SPEED CASE STUDY BASED ON AERO-STRUCTURAL COUPLED ANALYSIS |
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ICAS2026_1053: J.A. Schaefer, United States PROGRESS TOWARDS AIRCRAFT CERTIFICATION BY ANALYSIS WITHIN THE AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTIC |
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ICAS2026_1054: T. Ishida, Japan AN EFFORT TOWARD PROCESS DEVELOPMENT OF CBA FOR FLIGHT CHARACTERISTICS |
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ICAS2026_1055: J. Slotnick, United States PANEL DISCUSSION WITH J. SLOTNICK, B.APONSO, D.PETERSON, T.ISHIDA, H.SCKLICKENMAIER (DURATION 100 MINUTES) |
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ICAS2026_1059: J. Stevens, NASA, United States OVERVIEW OF PROPULSION-AIRFRAME INTEGRATION RESEARCH AT NASA (PART I) |
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ICAS2026_1060: J. Stephens, United States OVERVIEW OF PROPULSION-AIRFRAME INTEGRATION RESEARCH AT NASA (PART II) |
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ICAS2026_1061: J. Melkert¹, G. Rao¹; ¹TU Delft, Netherlands BLI/PROPULSION STUDIES AT TU DELFT (PART I) |
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ICAS2026_1062: J. Melkert¹, G. Rao¹; ¹TU Delft, Netherlands BLI/PROPULSION STUDIES AT TU DELFT (PART II) |
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ICAS2026_1063: P. Discussion, PANEL DISCUSSION WITH H. SCHLICKENMAIER (MODERATOR), D. PETERSON, M. CUMMINGS, C. BACZYNSKI, J. MARIS AND M. TRASKOS (DURATION TIL END OF THE BLOCK) |
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ICAS2026_1064: A. Neely, UNSW, Australia RECENT DEVELOPMENTS IN HYPERSONIC INNOVATION, SCIENCE & TECHNOLOGY IN AUSTRALIA |
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ICAS2026_1065: N. Viola, Politecnico di Torino, Italy EUROPEAN HYPERSONICS OVERVIEW |
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ICAS2026_1066: B.J. Lee, Seoul National University, South Korea HYPERSONIC RESEARCH AND DEVELOPMENT IN THE REPUBLIC OF KOREA: FROM FUNDAMENTAL AEROTHERMODYNAMICS TO FLIGHT DEMONSTRATION |
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ICAS2026_1067: J. Akatsuka¹, S. Takahashi¹, Y. Makino¹, S. Tomioka¹, M. Takegoshi¹, M. Koga¹, T. Isono¹; ¹JAXA, Japan AN OVERVIEW OF JAXA’S HIGH-SPEED FLIGHT R&D: FROM SUPERSONIC FLIGHT TO HYPERSONIC TRANSPORTATION |
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ICAS2026_1068: S. Rao, Indian Institute of Science, India TOWARDS MULTI-DISCIPLINARY OPTIMIZATION OF A GENERIC HYPERSONIC VEHICLE – AN OVERVIEW OF RESEARCH AT LHSR, IISC |
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ICAS2026_1069: M. Santer, Imperial College London, United Kingdom AERO-THERMO-STRUCTURAL OPTIMIZATION OF INTEGRATED THERMAL PROTECTION SYSTEMS |
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ICAS2026_1070: S. Takahashi¹, T. Nagata, Nagoya University, Japan; M. Koga¹, T. Isono¹, M. Takegoshi¹; ¹JAXA, Japan SDF-BASED GEOMETRY BLENDING OF HYPERSONIC VEHICLE CONCEPTS |
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ICAS2026_1071: J. Merrifield, Fluid Gravity Engr Ltd., United Kingdom THE TREATMENT OF NON-IDEAL SURFACE TOPOLOGIES RELATED TO HIGH-SPEED VEHICLE DESIGN |
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ICAS2026_1072: A. Wart, Hypersonix, Australia; M. Smart, Australia THE DART HYPERSONIC VEHICLE: FROM CONCEPT TO LAUNCH |
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ICAS2026_1073: A. Duggleby, Venus Aerospace, United States FROM FIRST ROTATING DETONATION ROCKET ENGINE (RDRE) FLIGHT TO HYPERSONIC RDRE FLIGHT |
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ICAS2026_1074: H. Taguchi, Tokio University of Science, Japan; T. Sato¹, C. Fujio¹, M. Tsue², T. Tsuchiya², S. Nakaya², K. Takizawa², A. Matsuo, Keio University, Japan; T. Hirotani³, H. Takahashi³, M. Hongoh³, A. Tezuka¹; ¹Waseda University, Japan; ²University of Tokyo, Japan; ³JAXA, Japan MACH 5 WIND TUNNEL TEST OF HIGH-MACH INTEGRATED CONTROL EXPERIMENT AIRCRAFT (HIMICO) |
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ICAS2026_1075: C. Fureby, Lund University, Sweden PHYSICAL AND NUMERICAL MODELING OF SUPERSONIC COMBUSTION FOR HYPERSONIC FLIGHT |
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ICAS2026_1076: M. Heitzmann, University of Queeensland, Australia FROM HIGH-TEMPERATURE MATERIALS TO HIGH-RATE PRODUCTION: OVERVIEW OF EXISTING RESEARCH EFFORTS AND OUTLOOK |
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ICAS2026_1077: P. Panel PANEL DISCUSSION (TIL END OF THE BLOCK) |
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ICAS2026_1081: L. Mainini, please select... COMPUTATIONAL AVENUES TO ADVANCE DIGITAL CAPABILITIES AND EMPOWER SYNERGIES FOR THE BLUE SKIES |
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ICAS2026_1083: J.L. Palmer¹, C. Zhang¹, Y. Xie¹, M. Alidadi¹, A. Bubb¹, M.J. Hasan¹, N. Kumar¹, D. Notman¹; ¹RMIT University, Australia IMPLICATIONS OF AAM OPERATIONS FOR FUTURE SHARED AIRSPACE IN VICTORIA, AUSTRALIA |
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ICAS2026_1085: C. Meglio¹, Z. Chen¹, B. Sun¹, C.S. Greco, University of Naples, Italy; C. Atkinson¹, J. Soria¹; ¹Monash University, Australia PASSIVE FLOW CONTROL OF A TURBULENT BOUNDARY LAYER AT THE VERGE OF SEPARATION USING SURFACE ROUGHNESS |
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ICAS2026_1087: A. Habibi Husain, please select... MBSE AS A KEY ENABLER IN AEROSPACE DIGITAL ENGINEERING |
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ICAS2026_1088: O. Pinon-Fischer, United States DIGITAL ENGINEERING FOR TRANSFORMATIVE AEROSPACE |
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ICAS2026_1089: R. Sharp, Airservices Australia, Australia; J. Connolly, THALES, Australia MODERNISING AT SCALE: DELIVERING AUSTRALIA’S NEXT-GENERATION AIR TRAFFIC SYSTEM |
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ICAS2026_1091: P. Gupta, Australia SOME OBSERVATIONS ON DEEP STALL LANDING, WITH APPLICATION TO SMALL UNMANNED AIRCRAFT |
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ICAS2026_1092: B. Stoufflet, France THE COLLABORATIVE NATURE OF AVIATION INDUSTRY |
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ICAS2026_1093: A. Neely, UNSW, Australia PREDICTING THE RESPONSE OF HIGH-TEMPERATURE STRUCTURE FOR HIGH-SPEED VEHICLES THROUGH SIMULATION AND MEASUREMENT |
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ICAS2026_1094: J. Rodrigues, Australia DETECTION OF SURFACE DISCONTINUITIES IN ADDITIVELY MANUFACTURED ALSI10MG USING THERMOELASTIC STRESS ANALYSIS (PITCH SESSION) |
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ICAS2026_1095: P. Faezeh, Netherlands AN OPTIMAL POWER MANAGEMENT POLICY FOR HYDROGEN BASED HYBRID AERO ENGINES (PITCH SESSION) |
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ICAS2026_1096: K. Thomessen, Germany ONBOARD MISSION MANAGEMENT FOR A DECENTRALIZED MULTI-UAV SYSTEM USING BEHAVIOR TREES (PITCH SESSION) |
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ICAS2026_1097: S. Chen, China NONLINEAR FRICTION MODELING OF HELIX SWING HYDRAULIC CYLINDERS FOR MORPHING AIRCRAFT USING PHYSICS-INFORMED NEURAL NETWORKS (PITCH SESSION) |
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ICAS2026_1098: Y. Iwatsuki, Mitsubishi Research Institute, Inc., Japan SENSITIVITY STUDY OF DEPARTURE TIME ACCURACY FOR AIRPORT COLLABORATIVE DECISION MAKING USING FAST-TIME SIMULATION (PITCH SESSION) |
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ICAS2026_1099: E. Dalbies, SAFRAN, France PERSPECTIVES & PROGRESS ON NEXTGEN PROPULSION FOR FUTURE AIRLINERS FROM SAFRAN’S STANDPOINT |
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ICAS2026_1101: B. Hammer, Germany GARTEUR: FRAMEWORK, ORGANIZATION AND COLLABORATIVE RESEARCH |
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ICAS2026_1102: B. Loxton, United States BUILDING A TECHNOLOGY PLATFORM FOR THE ELECTRIC AGE |
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ICAS2026_1103: C. Andrews, GE Aerospace, United States BEYOND 30,000 FEET: GE AEROSPACE AND THE FUTURE OF ELECTRIC FLIGHT |
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ICAS2026_1104: P.D. Panel, PANEL DISCUSSION |
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ICAS2026_1105: B. Edmonds¹, A. Romesh¹, L. Clark¹; ¹LEAP, Australia LOWERING THE BARRIER TO AEROACOUSTIC PREDICTION: GPU-COMPUTED SBES FOR FAR-FIELD LANDING GEAR NOISE PREDICTION |
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ICAS2026_1106: D. Peterson, Australia EXPERIENCES CERTIFYING INNOVATIVE VEHICLES IN AUSTRALIA |
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ICAS2026_1107: B. Nagel, DLR, Germany; P. Schmollgruber, ONERA, France PIONEERING THE EXCHANGE OF KNOWLEDGE IN AIRCRAFT DESIGN |
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ICAS2026_1108: J. Abulawi¹, C. Jouannet, SAAB, Sweden; P. Prakasha¹; ¹DLR, Germany DIGITAL ENGINEERING IN THE AGE OF AI AS BASIS FOR SYSTEM OF SYSTEMS ENGINEERING |
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ICAS2026_1109: T. Fadda, Uni Bologna, Italy; A.K. Koschlik, DLR, Germany; M. Scott, RMIT, Australia VR FOR CABIN DESIGN AND CERTIFYING DIGITAL MRO MEASURES |
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ICAS2026_1110: N. Viola, HYPERSONIC TRANSPORT AND WAY FORWARDS WITH THE ICAS DIGITAL PIONEERING INITIATIVE |
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ICAS2026_1113: B. van Magill, Australia TOWARDS A DATABASE OF MICRO-ELECTRIC MOTORS AND ELECTRONIC SPEED CONTROLLERS FOR SMALL UNCREWED AERIAL SYSTEMS |
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ICAS2026_1114: N. van Luijk, Netherlands VORTEX FLOW CONTROL USING JUNCTURE FILLETS ON A BLUNT-NOSED, CRANKED SWEPT WING |
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ICAS2026_1115: M. Higinio, Australia A MIXED REALITY FRAMEWORK FOR EVALUATING AIRCRAFT PRE-FLIGHT WALK-AROUND TRAINING |
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ICAS2026_1116: I. Frascareli Ali, Brazil EVALUATION OF TRUST AS A HUMAN FACTOR IN COLLABORATIVE ROBOTICS ASSOCIATED WITH ARTIFICIAL INTELLIGENCE APPLIED TO THE AERONATUCAL INDUSTRY |