Preliminary Programme - Session List
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Attention: Be advised that there might be changes till the congress, so please do not adjust your travel plans based on this preliminary programme.
"(invited)" behind a session means that those presentation were invited by the programme committee. They can, of course, be attended by everyone without "invitation
Tuesday, 06. Sep 2022
0.3 | GL 2 “Towards Certification by Analysis for Flight Characteristics” Robert Gregg III , USA Chair: F. Collier ICAS EC member | |||
06. Sep 22 | 08:00 | 09:00 |
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0.4 | Interactive Presentations (Coffee will be served after 10:00) Chair: O. Pinon Fischer ICAS PC Member | |||
06. Sep 22 | 09:00 | 10:30 |
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06. Sep 22 | 10:30 | 11:00 | 1.4.1 |
CERTIFICATION BY ANALYSIS - SOME THOUGHTS (invited) U. Kerlin, Airbus, Germany | |||
06. Sep 22 | 11:00 | 11:30 | 1.4.2 |
NEXT STEPS TOWARDS CERTIFICATION BY ANALYSIS - A DIGITAL THREAD PERSPECTIVE (invited) O. Pinon Fischer, United States; D. Mavris, United States | |||
06. Sep 22 | 11:30 | 12:00 | 1.4.3 |
TOWARDS CERTIFICATION BY ANALYSIS FOR FLIGHT CHARACTERISTICS (invited) R. Gregg, Boeing, United States | |||
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06. Sep 22 | 10:30 | 11:00 | 2.4.1 |
DEEP LEARNING TECHNIQUES FOR HIGH-DIMENSIONAL SURROGATE-BASED AERODYNAMIC DESIGN M.A. Hariansyah¹, K. Shimoyama¹; ¹Institute of Fluid Science, Tohoku University, Japan | |||
06. Sep 22 | 11:00 | 11:30 | 2.4.2 |
SUCCESSIVE KNOWLEDGE BUILDUP AND TRANSFER DURING THE ANALYSIS OF SCALED UAV WINGS BY MEANS OF MACHINE LEARNING T. Klaproth¹, M. Hornung¹; ¹Technical University of Munich, Germany | |||
06. Sep 22 | 11:30 | 12:00 | 2.4.3 |
AIRCRAFT DESIGN PARAMETER ESTIMATION USING DATA-DRIVEN MACHINE LEARNING MODELS S. Shin¹, S. Lee¹, C. Son, Cheongju University, South Korea; K. Yee, Seoul National University, South Korea; ¹Korea Institute of Industrial Technology, South Korea | |||
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06. Sep 22 | 10:30 | 11:00 | 3.4.1 |
EXPLORATION OF BOX-WING AIRCRAFT CONCEPT USING HIGH-FIDELITY AERODYNAMIC SHAPE OPTIMIZATION P.D. Bravo-Mosquera¹, T. Chau², F.M. Catalano¹, D.W. Zingg²; ¹University of São Paulo, Brazil ;²University of Toronto, Canada | |||
06. Sep 22 | 11:00 | 11:30 | 3.4.2 |
CONCEPTUAL STUDY OF HYBRID-ELECTRIC BOX-WING AIRCRAFT TOWARDS THE REDUCTION OF AVIATION EFFECTS ON LOCAL AIR QUALITY AND CLIMATE CHANGE K. Abu Salem¹, V. Cipolla¹, G. Palaia¹, V. Binante², D. Zanetti²; ¹University of Pisa, Italy ;²SkyBox Engineering, Italy Presenter: Karim Abu Salem, University of Pisa, Dep. of Civil and Industrial Engineering | |||
06. Sep 22 | 11:30 | 12:00 | 3.4.3 |
MULTIDISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION PROCESS DEDICATED TO BLENDED WING BODY CONFIGURATIONS J. Gauvrit-Ledogar¹, A. Tremolet¹, F. Moens¹, M. Méheut¹, S. Defoort¹, R. Liaboeuf¹, F. Morel¹, B. Paluch¹; ¹ONERA, France | |||
Reserve Paper | 3.4.R |
RESEARCH ON THE SELECTION METHOD OF TYPICAL RCS BENCHMARK BASED ON AHP Y.-L. Huang¹, D.-Q. Huang¹, W. Du¹, J. Liu, Beihang University, China; ¹AVIC CHENGDU AIRCRAFT INDUSTRIAL(GROUP) CO.LTD, China | |||||
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06. Sep 22 | 10:30 | 11:00 | 4.4.1 |
WING BUFFET PRESSURE LOAD PREDICTION BASED ON A HYBRID DEEP LEARNING MODEL R. Zahn¹, A. Weiner, Technical University of Braunschweig, Germany; C. Breitsamter¹; ¹Technical University of Munich (TUM), Germany | |||
06. Sep 22 | 11:00 | 11:30 | 4.4.2 |
AN ASSESSMENT OF REDUCED-ORDER AND MACHINE LEARNING MODELS FOR STEADY TRANSONIC FLOW PREDICTION ON WINGS R. Castellanos¹, J. Bowen Varela¹, A. Gorgues¹, E. Andrés¹; ¹INTA, Spain Presenter: Rodrigo Castellanos, INTA | |||
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06. Sep 22 | 10:30 | 11:00 | 5.4.1 |
ASSESSMENT OF THE SUSTAINABILITY OF THE IMPLEMENTATION OF CIRCULAR ECONOMY PRINCIPLES IN PRODUCING AIRCRAFT STRUCTURES D.N. Markatos¹, S.G. Pantelakis¹; ¹University of Patras, Greece Presenter: Dionysios Markatos | |||
06. Sep 22 | 11:00 | 11:30 | 5.4.2 |
INVESTIGATION ON INTEGRATING RECYCLABILITY AS A FUNCTION AT THE DESIGN PHASE OF COMPLEX-LOADED STRUCTURAL COMPONENTS A. Filippatos¹, K. Abhyankar, Institute of Lightweight Engineering and Polymer Technology, Tec, Germany; G. Tzortzinis¹; ¹Dresden Center for Intelligent Materials (DCIM), Technische Univ, Germany | |||
06. Sep 22 | 11:30 | 12:00 | 5.4.3 |
SIGMOIDAL SENSING DEVICES FOR MONITORING TO IMPROVE MAINTENANCE OPERATIONS IN AERONAUTICS H. Pfeiffer¹, H. Sekler, Deutsche Lufthansa AG, Germany; M. Wevers¹; ¹KU Leuven, Belgium | |||
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06. Sep 22 | 10:30 | 11:00 | 6.4.1 |
ANALYSIS OF THE EFFECT OF FLOW TRANSITION OVER THE WINGS OF THE BLADE DEMONSTRATOR R. Larsson, Saab Aeronautics, Sweden | |||
06. Sep 22 | 11:00 | 11:30 | 6.4.2 |
TO CFD OR NOT TO CFD? COMPARING RANS AND VISCOUS PANEL METHODS FOR AIRFOIL SHAPE OPTIMIZATION E.J. Adler¹, A.C. Gray¹, J.R.R.A. Martins¹; ¹University of Michigan, United States | |||
06. Sep 22 | 11:30 | 12:00 | 6.4.3 |
PUSHER PROPELLER INFLUENCE ON A LAMINAR WING TRANSITION LOCATION USING INFRARED THERMOGRAPHY J.P. Eguea¹, G.P.G. Silva¹, F.M. Catalano¹; ¹USP, Brazil | |||
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06. Sep 22 | 10:30 | 11:00 | 7.4.1 |
EFFECT OF NITRIDING ON MICROSTRUCTURE AND MECHANICAL PROPERTIES ON A TI64 ALLOY FOR AEROSPACE APPLICATIONS S. Stekovic¹, R. Romero-Ramirez¹, L. Selegård, Saab Aeronautics, Sweden; ¹Linköping University, Sweden Presenter: Rodger Romero-Ramirez, Linköping University | |||
06. Sep 22 | 11:00 | 11:30 | 7.4.2 |
MECHANICAL CHARACTERIZATION OF A COMPOSITE STRUCTURAL BATTERY LAMINATE G. Di Mauro¹, P. Russo, Institute for Polymers, Composites and Biomaterials, C.N.R., Italy; M. Guida¹; ¹University of Naples Federico II – Department of Industrial Eng., Italy | |||
06. Sep 22 | 11:30 | 12:00 | 7.4.3 |
DOPAMINE-COATED UHMWPE/HYDROGEN-RICH BENZOXAZINE COMPOSITES FOR SPACE RADIATION SHIELDING J.-H. Cha¹, C.-G. Kim¹; ¹KAIST, South Korea | |||
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06. Sep 22 | 10:30 | 11:00 | 8.4.1 |
DEVELOPMENT OF INNOVATIVE AND ECO-FRIENDLY AIRFRAME TECHNOLOGIES TO IMPROVE AIRCRAFT LIFE CYCLE ENVIRONMENTAL FOOTPRINT – LIFE CYCLE ASSESSMENT ACTIVITIES AT ECOTECH / CLEANSKY 2 L.A.S.A Prado¹, T.S.G. Das¹, S. Coskun¹, A. Kötter¹; ¹Capgemini Engineering / Altran Deutschland und SAS KG, Germany Presenter: Luis Antonio Sanchez de Almeida Prado, Capgemini Engineering / Altran Deutschland und SAS KG | |||
06. Sep 22 | 11:00 | 11:30 | 8.4.2 |
NUMERICAL MODELING OF FLUID-STRUCTURE INTERACTION OF A 3D WEDGE DURING WATER IMPACT WITH VARIATION OF VELOCITY AND PITCH ANGLE F. Valpiani¹, P. Cicolini¹, D. Esposto¹, A. Galletti¹, D. Guagliardo¹; ¹Politecnico di Torino, Italy | |||
06. Sep 22 | 11:30 | 12:00 | 8.4.3 |
EFFICIENT SURROGATE-BASED MULTI-OBJECTIVE OPTIMIZATION ALGORITHM WITH A NEW ADAPTIVE WEIGHT VECTOR GENERATION Z. Lu¹, Z.-H. Han¹, Z. Zhou, Science and Technology on Scramjet Laboratory,CARDC, China; W.-P. Song¹, Y. Zhang¹; ¹Northwestern Polytechnical University, China | |||
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06. Sep 22 | 10:30 | 11:00 | 9.4.1 |
DEVELOPMENT OF A CONCEPTUAL DESIGN TOOL TO PREDICT PERFORMANCE OF HYDROGEN FUELLED PRECOOLED AIRBREATHING ROCKET ENGINES G. Grimaldi, Politecnico di Torino, Italy | |||
06. Sep 22 | 11:00 | 11:30 | 9.4.2 |
LARGE EDDY SIMULATION OF RAMJET TO SCRAMJET TRANSITION T. Nilsson¹, C. Fureby¹; ¹Lund University, Sweden | |||
06. Sep 22 | 11:30 | 12:00 | 9.4.3 |
AEROPROPULSIVE CHARACTERIZATION OF THE HYPERSONIC CRUISER VEHICLE IN STRATOFLY PROJECT P. Roncioni¹, L. Cutrone¹, M. Marini¹; ¹CIRA, Italy | |||
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06. Sep 22 | 10:30 | 11:00 | 10.4.1 |
ENVIRONMENTAL ASSESSMENT OF NOISE ABATEMENT APPROACH TRAJECTORIES E.M. Thoma¹, T. Grönstedt¹, E. Otero Sola, KTH, Royal Institute of Technology, Sweden; X. Zhao¹; ¹Chalmers University of Technology, Sweden | |||
06. Sep 22 | 11:00 | 11:30 | 10.4.2 |
DESIGN OF A TYPICAL MANEUVERING PROCESS SIMULATION TEST CONTROL SYSTEM WITH CONTROLLABLE RUDDER SURFACE J.-F. Wang, China; H. Tan, China; H. Chen, China; S. Feng, China; M.-H. Wang, China | |||
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06. Sep 22 | 10:30 | 11:00 | 11.4.1 |
A PREPARATORY RESEARCH FOR UAM COLLISION AVOIDACE USING ADSB S. Ahn¹, H. Choi¹, S. Kim¹, J. Kim¹, H. Ryu¹; ¹Korea Aerospace Research Institute, South Korea | |||
06. Sep 22 | 11:00 | 11:30 | 11.4.2 |
SAFE REINFORCEMENT LEARNING BASED MULTI-ROTOR COLLISION AVOIDANCE WITH UNEXPECTED OBSTACLES H.J. Ahn¹, C.S. Lim¹, D.W. Lee¹, H.C. Bang¹; ¹Korea Advanced Institute of Science and Technology(KAIST), South Korea | |||
06. Sep 22 | 11:30 | 12:00 | 11.4.3 |
INVESTIGATION OF SIMULATION FRAMEWORKS FOR THE EVALUATION OF AUTOMATED FLIGHT FUNCTIONS FOR EVTOL AIRCRAFT Y. Lemmens¹, C. Teirlink¹, A. Hegde¹, D. Pla Guerrero¹, G. Olivares², H. Shah²; ¹Siemens Digital Industries Software, Belgium ;²National Institute for Aviation Research, United States | |||
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06. Sep 22 | 10:30 | 11:00 | 12.4.1 |
SMART SKIN FOR AEW AIRCRAFT P. Khanal, Chalmers University of Technology, Sweden; P. Hallander¹, R. Luo¹; ¹Saab AB, Sweden | |||
06. Sep 22 | 11:00 | 11:30 | 12.4.2 |
CERTIFICATION ASPECTS OF AN EARTH OBSERVATION PAYLOAD INSTALLED ON COMMERCIAL TRANSPORT AIRCRAFT R. Lopez Pereira, Safran Engineering Services GmbH, Germany; L. Rammos, Skyflox Sarl, Luxembourg | |||
06. Sep 22 | 11:30 | 12:00 | 12.4.3 |
DESIGN OF ELECTRONICALLY PHASE-TUNING REFLECTARRAY ANTENNA FOR AIRBORNE RADAR APPLICATION G. Kong, China; P. Cui, China; W. Du, China; R. Chen, China | |||
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06. Sep 22 | 10:30 | 11:00 | 13.4.1 |
EXPECTED TEAMWORK ATTRIBUTES BETWEEN HUMAN OPERATOR AND AUTOMATION IN AIR TRAFFIC CONTROL Å. Svensson, LFV, Sweden; N. Rönnberg, Linköping University, Sweden | |||
06. Sep 22 | 11:00 | 11:30 | 13.4.2 |
PILOT’S ATTENTION DISTRIBUTION MODELING USING HIDDEN MARKOV MODELS J. Hanak¹, J. Vlk¹, P. Chudy¹; ¹Brno University of Technology, Czech Republic Presenter: Jiri Hanak | |||
Reserve Paper | 13.4.R |
EXPLORATORY STUDY OF MENTAL WORKLOAD IN HELICOPTER AIR-TO-GROUND ROCKET FIRING R.G. Cortes¹, E. Villani¹, M.M. Cardoso Júnior¹; ¹Aeronautics Institute of Technology, Brazil Presenter: Emilia Villani, Aeronautics Institute of Technology | |||||
Reserve Paper | 13.4.R |
STRESSING SAFETY ASSESSMENT METHODS BY HIGHER LEVELS OF AUTOMATION L. Meyer¹, C. Bjursten Carlsson¹, Å. Svensson¹, M. Peukert¹, L. Danielson, SDATS, Sweden; B. Josefsson¹; ¹LFV, Sweden | |||||
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06. Sep 22 | 10:30 | 11:00 | 14.4.1 |
AERODYNAMIC DEVELOPMENT OF SAAB FCAS UNMANNED SUPERSONIC COMBAT AIRCRAFT M. Hackström¹, F. Kållberg¹, P. Nordström¹; ¹Saab Aeronautics, Sweden Presenter: Fredrik Kållberg, Saab AB | |||
Reserve Paper (interactive) | 14.4.R |
NUMERICAL SIMULATION OF MISSILE AIR-LAUNCHED DYNAMIC PROCESS UNDER DOWNWASH FLOW OF HELICOPTER ROTOR W.-Y. Zhou¹, G.-Q. Yang¹, X. Gao¹, X.-Y. Zhu¹, B.-X. Zhou¹; ¹AVIC Xi’an Flight Automatic Control Research Institute, China | |||||
Reserve Paper (interactive) | 14.4.R |
RESEARCH ON THE INFLUENCE OF FLIGHT ATTITUDE ON UNILATERAL MISSILE SEPARATION FROM EMBEDDED BAY Z. Wei, China |
12:00 - 13:00 | Lunch Break |
0.5 | ICAS Enoch Thulin Lecture for Innovation in Aeronautics“Reflections on Active Aeroelastic Control and the Multidisciplinary Design Optimization of Aircraft” Eli Livne Chair: C. Atkin ICAS PPSC Chair | |||
06. Sep 22 | 13:00 | 14:00 |
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06. Sep 22 | 14:00 | 14:30 | 1.5.1 |
ICAS DIGITAL PIONEERING INITIATIVE AND SYSTEM OF SYSTEM CHALLENGES N. Nagel, Germany; C. Jouannet, Sweden | |||
06. Sep 22 | 14:30 | 15:00 | 1.5.2 |
CHALLENGES OF MULTIDISCIPLINARY DESIGN OPTIMIZATION FOR GREEN AVIATION P. Schmollgruber, France; I. Staack, Sweden | |||
06. Sep 22 | 15:00 | 15:30 | 1.5.3 |
POTENTIAL OF EXTENDED REALITY IN ENGINEERING AND CHALLENGES OF UNCONVENTIONAL VEHICLE DESIGN S. Bagassi, Italy; L. Boggero, Germany | |||
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06. Sep 22 | 14:00 | 14:30 | 2.5.1 |
MORE ELECTRIC AIRCRAFT (MEA) SCALING ASPECTS AND WEIGHT IMPACT E. Holmgren¹, D. Haldar¹, L. Bertling Tjernberg, School of Electrical Engineering and Computer Science, KTH Royal, Sweden; A. Johansson, SAAB, Sweden; ¹KTH Royal Institute of Technology, Sweden | |||
06. Sep 22 | 14:30 | 15:00 | 2.5.2 |
SIZING AND OPTIMIZATION OF A MORE ELECTRIC AIRCRAFT INTEGRATING SHORT-TERM INCREMENTAL TECHNOLOGIES T. Planès¹, S. Delbecq¹, V. Pommier-Budinger¹, V. Palanque¹, E. Bénard¹; ¹ISAE-SUPAERO, France | |||
06. Sep 22 | 15:00 | 15:30 | 2.5.3 |
IMPLEMENTATION OF WING ICE PROTECTION SYSTEM IN MORE ELECTRIC AIRCRAFT TECHNOLOGIES D. Haldar¹, E. Holmgren¹, A. Johansson¹; ¹KTH Royal Institute of Technology, Sweden | |||
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06. Sep 22 | 14:00 | 14:30 | 3.5.1 |
AEROSHAPE AND TRAJECTORY DESIGN OF NEXT GENERATION RE-ENTRY VEHICLES N. Montella¹, A. Aprovitola¹, L. Iuspa¹, G. Pezzella¹; ¹University of Campania , Italy | |||
06. Sep 22 | 14:30 | 15:00 | 3.5.2 |
A RAPID DESIGN METHOD FOR QUIET SPIKE OF SUPERSONIC TRANSPORT AIRCRAFT L.-W. Zhang¹, Z.-H. Han¹, J.-L. Qiao¹, Y.-L. Ding¹, Q. Chen¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China | |||
06. Sep 22 | 15:00 | 15:30 | 3.5.3 |
“CONCORDE-NEO”: A BIOFUEL PROPELLED SUPERSONIC COMMERCIAL AIRCRAFT WITH CONCORDE CONFIGURATION M. Borghi¹, G. Clinca¹, F.A. D'Amico¹, F. Fornaseri¹, E. Versino¹; ¹Politecnico di Torino, Italy | |||
Reserve Paper | 3.5.R |
CONCEPT DESIGN OF A LOW BOOM SSBJ TO SATISFY SOCIAL ACCEPTANCE S. Horinouchi, SuperSonic Jet Planning Inc., Japan | |||||
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06. Sep 22 | 14:00 | 14:30 | 4.5.1 |
CAD DEFORMATION FOR THE CONSIDERATION OF AEROELASTIC EFFECTS P. Wegener¹, S. Keye¹; ¹DLR, Germany | |||
06. Sep 22 | 14:30 | 15:00 | 4.5.2 |
AUTOMATIC FREE-FORM DEFORMATION AS GEOMETRIC PARAMETERIZATION FOR AERODYNAMIC DESIGN M.A.L. Matunaga, ITA - Instituto Tecnológico de Aeronáutica, Brazil; J.L.F Azevedo, IAE - Instituto de Aeronáutica e Espaço, Brazil | |||
06. Sep 22 | 15:00 | 15:30 | 4.5.3 |
HEAT TRANSFER ENHANCEMENT BY SUSPENDED PARTICLES IN A TURBULENT SHEARLESS FLOW H.R. Zandi Pour¹, M. Iovieno¹; ¹Politecnico di Torino, Italy | |||
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06. Sep 22 | 14:00 | 14:30 | 5.5.1 |
TRANSITIONAL FLOW MODELLING OF A HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER TRANSONIC TRANSPORT AIRCRAFT WING M.M. Jentys¹, C. Breitsamter¹; ¹Technical University of Munich, Germany | |||
06. Sep 22 | 14:30 | 15:00 | 5.5.2 |
REACTIVE CONTROL OF BYPASS TRANSITION IN A WING BOUNDARY LAYER J.M. Faúndez Alarcón¹, K. Sasaki¹, A. Hanifi¹, R. Larsson, Saab Aeronautics, Sweden; D.S. Henningson¹; ¹KTH Royal Institute of Technology, Linné FLOW Centre, Sweden | |||
06. Sep 22 | 15:00 | 15:30 | 5.5.3 |
DIRECT NUMERICAL SIMULATIONS OF A THICK, ROTATING AIRFOIL AT A LOW REYNOLDS NUMBER T. Coelho Leite Fava¹, D. Henningson¹, A. Hanifi¹; ¹KTH, Sweden | |||
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06. Sep 22 | 14:00 | 14:30 | 6.5.1 |
PRELIMINARY AERODYNAMIC WING DESIGN OPTIMISATION FOR WING-IN-GROUND EFFECT AIRCRAFT R. Jesudasan¹, R. Mariani¹, A. Hanifi¹; ¹KTH Royal Institute of Technololgy, Stockholm, Sweden | |||
06. Sep 22 | 14:30 | 15:00 | 6.5.2 |
ON THE APPLICABILITY ASSESSMENT OF VON KARMAN’S MOMENTUM THEORY IN PREDICTING THE WATER-ENTER LOAD OF V-SHAPED BODY Y. Lu, China; A. Del Buono, Italy; T. Xiao, China; A. Iafrati, Italy; J. Xu, China | |||
06. Sep 22 | 15:00 | 15:30 | 6.5.3 |
AERODYNAMIC AND AEROTHERMODYNAMIC ASSESSMENT OF A LIFTING-BODY RE-ENTRY VEHICLE A. Aprovitola¹, N. Montella¹, L. Iuspa¹, G. Pezzella¹, A. Viviani¹; ¹University of Campania , Italy | |||
Reserve Paper (interactive) | 6.5.R |
NUMERICAL STUDY ON WATER DISPLACEMENT DRAG CHARACTERISTICS OF AIRCRAFT ELASTIC TIRE ON CONTAMINATED RUNWAYS C.H. Ge¹, P.Q. Liu¹, Q.L. Qu¹; ¹Beihang University, China | |||||
Reserve Paper (interactive) | 6.5.R |
EFFICIENT MID-FIDELITY AERODYNAMIC MODELING OF A TILT-WING EVTOL FOR CONTROL APPLICATIONS D. Perdolt¹, D. Milz¹, M. May¹, M. Thiele, Technical University of Munich, Germany; ¹German Aerospace Center, Germany Presenter: Daniel Perdolt, German Aerospace Center Institute of System Dynamics and Control | |||||
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06. Sep 22 | 14:00 | 14:30 | 7.5.1 |
TI-6AL-4V ADDITIVE MANUFACTURING MEASURE OF QUALITY ACCORDING TO FATIGUE CRACK INITIATION VS. CRACK PROPAGATION C. Matias¹, A. Diskin¹, O. Golan, Afeka- Tel-Aviv Academic College of Engineering, Israel; A. Garkun², E. Strokin²; ¹Israel Aerospace Industries (IAI), Israel ;²The Israel Institute of Metals,, Israel | |||
06. Sep 22 | 14:30 | 15:00 | 7.5.2 |
RVE-BASED HOMOGENIZATION OF ADDITIVELY MANUFACTURED POROUS METALS A. Alaimo¹, G. Mantegna¹, C. Orlando¹, D. Tumino¹, C.R. Vindigni¹; ¹Faculty of Engineering and Architecture Kore University of Enna, Italy | |||
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06. Sep 22 | 14:00 | 14:30 | 8.5.1 |
AMPAIRE AND THE ELECTRIFIED PROPULSION JOURNEY (invited) S. Ying, AMPAIRE, United States | |||
06. Sep 22 | 14:30 | 15:00 | 8.5.2 |
REALISTIC HYDROGEN-BASED SOLUTIONS FOR SUSTAINABLE AVIATION J.P. Clark, Universal Hydrogen, United States | |||
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06. Sep 22 | 14:00 | 14:30 | 9.5.1 |
PROPULSION SYSTEM INTEGRATION FOR A FIRST GENERATION HYDROGEN CIVIL AIRLINER? J. Huete¹, D. Nalianda¹, P. Pilidis¹; ¹Cranfield University, United Kingdom Presenter: Jon Huete, Cranfield University | |||
06. Sep 22 | 14:30 | 15:00 | 9.5.2 |
SAND EROSION MODELING IN GENERIC COMPRESSOR RIG TESTING L.-Y. Jiang¹, X. Wu¹, Q. Yang¹; ¹National Research Council Canada, Canada | |||
06. Sep 22 | 15:00 | 15:30 | 9.5.3 |
MULTI-PLATFORM APP-EMBEDDED MODEL FOR HYBRID AIR-BREATHING ROCKET-CYCLE ENGINE IN HYPERSONIC ATMOSPHERIC ASCENT S.E. Tsentis, Greece; V.G. Gkoutzamanis, Greece; A.D. Gaitanis, Greece; A.I. Kalfas, Greece Presenter: Spyros Tsentis, Aristotle University of Thessaloniki | |||
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06. Sep 22 | 14:00 | 14:30 | 10.5.1 |
HANDLING QUALITIES OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT D. Planas, ONERA & ISAE SUPAERO, France; C. Döll, ONERA, France; P. Pastor, ISAE SUPAERO, France | |||
06. Sep 22 | 14:30 | 15:00 | 10.5.2 |
PRELIMINARY STUDY ON A DESIGN OF A RETURN FLIGHT TRAJECTORY OF A SUBORBITAL VEHICLE A. Kwiek¹, M. Figat¹, T. Goetzendorf-Grabowski ¹; ¹Warsaw University of Technology, Poland | |||
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06. Sep 22 | 14:00 | 14:30 | 11.5.1 |
UNMANNED AERIAL VEHICLE\\\\\\\'S TRAJECTORY OPTIMIZATION IN CONSTRAINED ENVIRONMENTS J. Novák ¹, P. Chudý¹; ¹Brno University of Technology, Czech Republic | |||
06. Sep 22 | 14:30 | 15:00 | 11.5.2 |
NUMERICAL MODELLING OF PITCHING WINGS FOR GUST MITIGATION W. Yuan¹, A. Wall¹, X. Zhang², D. Poirel²; ¹National Research Council (NRC) Canada, Canada ;²Royal Military College of Canada (RMC),, Canada | |||
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06. Sep 22 | 14:00 | 14:30 | 12.5.1 |
VISION-BASED LOCALISATION FOR AUTONOMOUS AERIAL NAVIGATION IN GNSS-DENIED SITUATIONS D. Sabel¹, A. Maki¹, T. Westin², D. Åsvärn²; ¹KTH Royal Institute of Technology, Sweden ;²Spacemetric AB, Sweden | |||
06. Sep 22 | 14:30 | 15:00 | 12.5.2 |
INNOONBOARD FOR IMPROVED IMAGE HANDLING IN AIRBORNE COASTAL RECONNAISSANCE – A PROJECT PRESENTATION D. Åkerman¹, O. Fästh, ST Airborne Solutions, Sweden; M. Persson, Unibap, Sweden; D. Sabel¹, D. Åsvärn¹; ¹Spacemetric, Sweden Presenter: Daniel Sabel, Spacemetric | |||
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06. Sep 22 | 14:00 | 14:30 | 13.5.1 |
MANUFACTURE OF LARGE-SCALE SPACE EXPLORATION COMPONENTS USING WIRE + ARC ADDITIVE MANUFACTURING C. Diao¹, E. Eimer¹, S. Mancini, Thales Alenia Space, Italy; S. Krishnaswamy¹, F. Schwarz¹, E. Pagone¹, J. Ding¹, S. Williams¹, Z. Pinter², F. Martina²; ¹Cranfield University, United Kingdom ;²WAAM3D, United Kingdom | |||
06. Sep 22 | 14:30 | 15:00 | 13.5.2 |
LATEST DEVELOPMENTS IN HIGH PRESSURE HEAT TREATMENT OF AEROSPACE COMPONENTS J. Shipley¹, A. Magnusson¹, C. Beamer, Quintus Technologyes LLC, United States; ¹Quintus Technologies AB, Sweden | |||
06. Sep 22 | 15:00 | 15:30 | 13.5.3 |
VIKA - CONCEPT OF A DIGITAL PLATFORM FOR IMPLICIT KNOWLEDGE AND VIRTUAL ASSISTANCE FOR ADDITIVE MANUFACTURED PARTS J. Steffen, HAW Hamburg, Germany | |||
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06. Sep 22 | 14:00 | 14:30 | 14.5.1 |
A FRAMEWORK FOR INNOVATION WITHIN AEROSPACE SEGMENT A.G. Slongo¹, C. Jochims Lau¹, G.L. de Oliveirra¹, B.M. Ramos¹, T.B. Volkman¹; ¹AEL Sistemas, Brazil | |||
06. Sep 22 | 14:30 | 15:00 | 14.5.2 |
INTEGRATE ONLINE QUERY&DEFENSE INTO PROJECT BASED LEARNING TO PROMPT ENGINEERING AUTHENTIC EXPERIENCES S. Sun, Civil Aviation University of China, China; R. Gong, University of Waterloo, Canada Presenter: shuguang SUN, Civil Aviation University of China |
15:30 - 16:00 | Break |
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06. Sep 22 | 16:00 | 16:30 | 1.6.1 |
NATO AVT-297 DEVELOPMENT OF A FRAMEWORK FOR VALIDATION OF COMPUTATIONAL TOOLS FOR ANALYSIS OF AIR VEHICLES (invited) J. Morrison¹, M. Nikbay, Istanbul Technical University, Turkey; E. Walker¹; ¹NASA Langley Research Center, United States | |||
06. Sep 22 | 16:30 | 17:00 | 1.6.2 |
CONNECTING SYSTEM DESIGN TO MODELING AND SIMULATION CAPABILITIES (invited) J.M. Luckring, NASA Langley Research Center, United States; S. Shaw, MBDA UK Ltd., United Kingdom; W.L. Oberkampf, WLO Consulting, Inc., United States; R. Graves, Air Force Research Laboratory, United States | |||
06. Sep 22 | 17:00 | 17:30 | 1.6.3 |
SYSTEM LEVEL IDENTIFICATION OF CRITICAL UNCERTAINTIES TO ENABLE VALIDATION EXPERIMENTS D.N. Mavris¹, E.Y. Yarbasi¹, B. Bagdatli¹; ¹Georgia Institute of Technology, United States | |||
06. Sep 22 | 17:30 | 18:00 | 1.6.4 |
OPEN PANEL DISCUSSION (invited) op panel, United States | |||
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06. Sep 22 | 16:00 | 16:30 | 2.6.1 |
BOEING/SAAB CO-DEVELOPMENT PROGRAMME OF T-7A TRAINER - A JOINT DIGITAL JOURNEY (invited) D.C. Yates, Boeing, United States Presenter: Tomas Karlsson, Saab | |||
06. Sep 22 | 16:30 | 17:00 | 2.6.2 |
TOWARDS A SEAMLESS SIMULATION OF THE AIR TRANSPORT SYSTEM E. Moerland¹, A. Mancini¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany | |||
06. Sep 22 | 17:00 | 17:30 | 2.6.3 |
CERTIFICATION DRIVEN DESIGN FROM STAKEHOLDERS’ NEEDS TO MDAO FORMULATION WITHIN AGILE 4.0 PROJECT M. Fioriti, Politecnico di Torino, Italy; C. Cabaleiro, DLR, Germany; T. Lefebvre, ONERA, France; P. Della Vecchia¹, M. Mandorino¹, S. Liscouët-Hanke², A. Jeyarai²; ¹Università di Napoli Federico II, Italy ;²Concordia University, Canada | |||
06. Sep 22 | 17:30 | 18:00 | 2.6.4 |
DIGITAL COLLABORATIVE DESIGN: AN INNOVATIVE FRAMEWORK IN AERONAUTICAL EDUCATION Z. Cui¹, M. Luo¹, H. Liu¹, X. Sun¹, Z. Ji¹, Y. Hua, China Academy of Launch Vehicle Technology, China; ¹Beihang University, China | |||
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06. Sep 22 | 16:00 | 16:30 | 3.6.1 |
INNOVATIVE URBAN AIR MOBILITY FROM THE PERSPECTIVE OF THE HAMBURG METROPOLITAN REGION D. Kloock-Schreiber¹, M. Swaid², V. Gollnick¹, A. Fay, HSU, Institute of Automation Technology, Germany; M. Niklaß²; ¹TUHH, Institute of Air Transportation Systems, Germany ;²DLR, Institute of Air Transportation Systems, Germany | |||
06. Sep 22 | 16:30 | 17:00 | 3.6.2 |
ESTIMATION OF EVTOL FLIGHT PERFORMANCE USING ROTORCRAFT THEORY Y. Fukumine¹, Z. Lei¹; ¹Suwa University of Science, Japan | |||
06. Sep 22 | 17:00 | 17:30 | 3.6.3 |
MIXED INTEGER NONLINEAR PROGRAMMING FOR EVTOL AIRCRAFT DESIGN AND OPTIMIZATION T. Jiang¹, M. Li¹, Y. Liu¹, Y. Zheng¹; ¹School of Aeronautics and Astronautics, Zhejiang University, China Presenter: Tianhong Jiang | |||
06. Sep 22 | 17:30 | 18:00 | 3.6.4 |
RESEARCH ON THE DESIGN OF UNMANNED AERIAL VERICLE FOR MINE INSPECTION Z.-K. Li¹, S.-G. Su, Aerospace Times Feihong Technology Co., Ltd. , China; Z.-Y. Li¹, F.-R. Li¹, G. Chao¹; ¹Northwestern Polytechnical University, China Presenter: Zhi-Yu Li, Northwestern Polytechnical University | |||
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06. Sep 22 | 16:00 | 16:30 | 4.6.1 |
EFFECT OF LES LENGTH SCALE AND NUMERICAL SCHEME IN HYBRID RANS-LES OF FREE SHEAR LAYER FLOWS S. Arvidson¹, M. Carlsson, Chalmers University of Technology, Sweden; S. Nilsson¹; ¹Saab Aeronautics, Sweden | |||
06. Sep 22 | 16:30 | 17:00 | 4.6.2 |
INVESTIGATION OF LEADING-EDGE VORTICES ON A TRIPLE-DELTA-WING CONFIGURATION USING SCALE-ADAPTIVE SIMULATION T. Di Fabbio¹, E. Tangermann¹, M. Klein¹; ¹Universität der Bundeswehr München, Germany | |||
06. Sep 22 | 17:00 | 17:30 | 4.6.3 |
NUMERICAL INVESTIGATION OF HYPERSONIC TURBULENT BOUNDARY LAYERS WITH HIGH-TEMPERATURE EFFECTS D. Passiatore¹, L. Sciacovelli, ENSAM Paris, France; P. Cinnela , Sorbonne Université, France; G. Pascazio¹; ¹Politecnico di Bari, Italy | |||
06. Sep 22 | 17:30 | 18:00 | 4.6.4 |
HYBRID RANS-LES MODELLING: SOME RECENT DEVELOPMENT AND AERODYNAMIC APPLICATIONS S.-H. Peng, Swedish Defence Research Agency, FOI, Sweden Presenter: Shia-Hui Peng, Swedish Defence Research Agency, FOI | |||
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06. Sep 22 | 16:00 | 16:30 | 5.6.1 |
STABILITY OF A LAMINAR BOUNDARY LAYER OVER LOCALISED SURFACE INDENTATION E.R. Gowree, ISAE-SUPAERO, France; C.J. Atkin, University of East Anglia, United Kingdom | |||
06. Sep 22 | 16:30 | 17:00 | 5.6.2 |
ANALYSIS OF THE STABILITY OF MULTIPLE HELICAL VORTICES USING COMPLEX-STEP LINEARIZATION V.G. Kleine, ITA, Brazil; A. Hanifi¹, D.S. Henningson¹; ¹KTH, Sweden | |||
06. Sep 22 | 17:00 | 17:30 | 5.6.3 |
EXPERIMENTAL EVALUATION OF A PASSIVE FLOW-CONTROL DEVICE FOR A TILTROTOR AIRCRAFT A.R. Proenca¹, S.A. Prince¹, L. Banks-Davies¹, K.P. Garry¹; ¹Cranfield University, United Kingdom | |||
06. Sep 22 | 17:30 | 18:00 | 5.6.4 |
RESEARCH ON PRESSURE LOAD OF AN EMBEDDED JET NOZZLE H. Li¹, X. Wang¹, D. Yu¹, F. Liu¹; ¹Shenyang Aircraft Design and Research Institute, China | |||
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06. Sep 22 | 16:00 | 16:30 | 6.6.1 |
PREDICTING STEADY LIFT AND DRAG COEFFICIENT OF TANDEM AIRCRAFT USING PRANDTL’S EXTENDED LIFTING-LINE THEORY IMPLEMENTED UNDER ASWING R. Jan¹, J.-M. Moschetta¹, J.-P. Condomines, ENAC, France; ¹ISAE-SUPAERO, France | |||
06. Sep 22 | 16:30 | 17:00 | 6.6.2 |
ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUP R. Boisard¹, L. Lefevre¹, T. Zhang², G. Barakos², A. Visingardi, CIRA, Italy; F. Lößle³, A. Kostek³, T. Andronikos, NTUA, Greece; M. Keßler*, R. Wickersheim*, A. Colliº, G. Gibertiniº, A. Zanottiº; ¹ONERA, France ;²University Of Glasgow, United Kingdom ;³DLR, Germany ;*University of Stuttgart, Germany ;ºPolitecnico di Milano, Italy | |||
06. Sep 22 | 17:00 | 17:30 | 6.6.3 |
COMPARING POTENTIAL FLOW SOLVERS FOR AERODYNAMIC CHARACTERISTICS ESTIMATION OF THE T-FLEX UAV F. Yu¹, J. Bartasevicius¹, M. Hornung¹; ¹Technical University of Munich, Germany | |||
06. Sep 22 | 17:30 | 18:00 | 6.6.4 |
INVESTIGATION FLAPPING-FLIGHT AERODYNAMICS OF A ROBOTIC BIRD H.W.M. Hoeijmakers¹, L.H. Groot Koerkamp¹, L.D. de Santana¹, C.H. Venner¹, S. Stramigioli¹, J.L. Mulder¹, A. Brentjes¹, F. Gijsman¹, S.A. Hartman¹; ¹University of Twente, Netherlands | |||
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06. Sep 22 | 16:00 | 16:30 | 7.6.1 |
WING STATIC STRUCTURAL ANALYSIS AND EXPERIMENTAL TESTING OF A COMPOSITE 1:8 S55-X REPLICA G. Nicolosi¹, A. Lunghitano ¹, S. Lombardi ¹, T. Talamucci¹, A. Caivano¹, N. Simone¹, E. Cestino¹, V. Sapienza, Aeronautical Engineering Consultant, Italy; ¹Politecnico di Torino, Italy | |||
06. Sep 22 | 16:30 | 17:00 | 7.6.2 |
ASSESSMENT OF FAILURE UNDER LONGITUDINAL COMPRESSION OF UNIDIRECTIONAL COMPOSITES WITH IN-PLANE FIBER MISALIGNMENT A.R. de Faria, ITA, Brazil Presenter: Alfredo Rocha de Faria, ITA | |||
06. Sep 22 | 17:00 | 17:30 | 7.6.3 |
DAMAGE QUANTIFICATION ON COMPOSITE STRUCTURES USING NEURAL NETWORKS AND HYBRID DATA L.P.S. Ferreira¹, M.O. Yano², S. Silva², C.A. Cimini¹; ¹UFMG, Brazil ;²UNESP, Brazil | |||
06. Sep 22 | 17:30 | 18:00 | 7.6.4 |
TRIBOLOGICAL AND STRUCTURAL EVALUATION OF 3D PRINTED EPOXY RESINS G.C. Cristea¹, A. Stefan¹, K. Krawczyk, Joanneum Research, Austria; C.-E. Pelin¹, S. Ilina¹; ¹INCAS, Romania | |||
Reserve Paper (interactive) | 7.6.R |
STUDY ON MECHANICAL PROPERTIES OF CARBON FIBER RESIN MATRIX COMPOSITE BOLTED JOINT STRUCTURE AT HIGH TEMPERATURE D. Wang, School of Aeronautics, Northwestern Polytechnical University, Xi, China; G.W. Li, School of civil aviation, Northwestern Polytechnical University, China; H.Y. Huang, School of Aeronautics, Northwestern Polytechnical University, China Presenter: Dong Wang, Northwestern Polytechnical University | |||||
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06. Sep 22 | 16:00 | 16:30 | 8.6.1 |
AEROELASTIC MODELING, LOADS ANALYSIS AND STRUCTURAL DESIGN OF A FIGHTER AIRCRAFT A. Voß¹, T. Klimmek¹; ¹DLR Institute of Aeroelasticity , Germany | |||
06. Sep 22 | 16:30 | 17:00 | 8.6.2 |
LOADS ANALYSIS AND STRUCTURAL OPTIMIZATION OF A LONG-RANGE TRANSPORT CONFIGURATION WITH HYBRID LAMINAR FLOW CONTROL V. Handojo¹, T. Klimmek¹, T. Streit, DLR - Institute of Aerodynamics and Flow Technology, Germany; ¹DLR - Institute of Aeroelasticity, Germany | |||
06. Sep 22 | 17:00 | 17:30 | 8.6.3 |
LATERAL GUST BEHAVIOUR OF AIRCRAFT INCORPORATING FLARED FOLDING WINGTIPS R.C.M. Cheung¹, H. Gu¹, F. Healy¹, D. Rezgui¹, J.E. Cooper¹; ¹University of Bristol, United Kingdom | |||
06. Sep 22 | 17:30 | 18:00 | 8.6.4 |
SET-BASED DESIGN COORDINATION BETWEEN COUPLED SYSTEMS: A WING AERO-STRUCTURAL DESIGN PERSPECTIVE X. Chen¹, A. Riaz¹, M.D. Guenov¹; ¹Cranfield University, United Kingdom | |||
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06. Sep 22 | 16:00 | 16:30 | 9.6.1 |
LATTICE BOLTZMANN METHOD FOR BROADBAND NOISE PREDICTIONS ON A TURBULENCE-CASCADE TEST RIG INCLUDING SERRATED VANES M. Buszyk¹, L. Vienne², T. Le Garrec¹, J.-F. Boussuge², C. Polacsek¹, R. Barrier¹; ¹ONERA, France ;²CERFACS, France | |||
06. Sep 22 | 16:30 | 17:00 | 9.6.2 |
OPTIMIZATION OF INSTALLED COMPACT AND ROBUST NACELLES USING SURROGATE MODELS F. Sánchez-Moreno¹, D. MacManus¹, J. Hueso-Rebassa¹, F. Tejero¹, C. Sheaf, Rolls Royce, United Kingdom; ¹Cranfield University, United Kingdom | |||
06. Sep 22 | 17:00 | 17:30 | 9.6.3 |
AEROACOUSTIC PERFORMANCES OF A LOW-NOISE AIRFOIL CASCADE WITH SERRATED LEADING EDGES: PREDICTIONS AND MEASUREMENTS C. Polacsek¹, M. Buszyk¹, R. Barrier¹, V. Clair², E. Salze²; ¹ONERA, France ;²LMFA, France | |||
06. Sep 22 | 17:30 | 18:00 | 9.6.4 |
EFFECT OF HEAT EXCHANGER INTEGRATION IN AERODYNAMIC OPTIMISATION OF AN AGGRESSIVE S-DUCT I. Jonsson¹, R. Ranman¹, A. Capitao¹, C. Xisto¹; ¹Chalmers Tekniska Hogskola AB, Sweden | |||
Reserve Paper | 9.6.R |
MULTIPOINT AERODYNAMIC DESIGN OF A NACELLE FOR AN ELECTRIC FAN V.T. Silva¹, A. Venkatesh¹, M. Lejon ², A. Lundbladh², C. Xisto¹; ¹Chalmers University of Technology, Sweden ;²GKN Aerospace, Sweden | |||||
Reserve Paper | 9.6.R |
EFFECT OF TAILCONE SHAPE ON HOT STREAK PHENOMENA AND INFRARED SIGNATURE OF SERPENTINE NOZZLE WITH AFT DECK J.-Z. Fan¹, Q.-Z. Yang¹, X.-B. Du¹, H.-Q. Yang¹, Y.-B. He¹, Y.-Q. Shi¹; ¹Northwestern Polytechnical University, China | |||||
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06. Sep 22 | 16:00 | 16:30 | 10.6.1 |
AUTOMATIC TAKE-OFF AND LANDING OF A VERY LIGHT ALL ELECTRIC OPTIONALLY PILOTED AIRCRAFT S. Scherer¹, M. Speckmaier¹, D. Gierszewski¹, C. Mishra¹, A. Steinert¹, R. Steffensen¹, S. Wulf¹, F. Holzapfel¹; ¹Technical University of Munich,, Germany | |||
06. Sep 22 | 16:30 | 17:00 | 10.6.2 |
LPV/LFR CONTROL FOR ACTIVE FLUTTER SUPPRESSION OF A SMART AIRFOIL MODEL R.L. Pereira, ITA, Brazil; P.J. González¹, F.J. Silvestre¹; ¹TU Berlin, Germany | |||
06. Sep 22 | 17:00 | 17:30 | 10.6.3 |
LQR BASED DIGITAL AUTOPILOT FOR LIGHT SPORT AIRCRAFT J. Vlk¹, P. Chudy¹, M. Prustomersky¹; ¹Brno University of Technology, Czech Republic | |||
06. Sep 22 | 17:30 | 18:00 | 10.6.4 |
EXTENSION OF THE CAPABILITIES OF AN AUTOMATIC LANDING SYSTEM WITH PROCEDURES MOTIVATED BY VISUAL-FLIGHT-RULES S. Scherer¹, C. Mishra¹, F. Holzapfel¹; ¹Technical University of Munich, Germany | |||
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06. Sep 22 | 16:00 | 16:30 | 11.6.1 |
FAULT DIAGNOSIS FOR SENSOR AND ACTUATOR OF HEXACOPTER UAV USING DUAL EXTENDED KALMAN FILTER Y.J. Kim¹, T.G. Kim¹, S.K. Kim¹; ¹Chungnam National University, South Korea | |||
06. Sep 22 | 16:30 | 17:00 | 11.6.2 |
CONTROL AUGMENTATION SYSTEM DESIGN FOR THE QUAD TILT-WING UAV VIA H-INFINITY STRUCTURE WITH GWO K.K. Deveerasetty¹, K. Oka¹, A. Harada¹; ¹Kochi University of Technology, Japan | |||
06. Sep 22 | 17:00 | 17:30 | 11.6.3 |
OPTIMIZATION OF ENERGY CONSUMPTION IN THE TRANSITION STATE OF A QUAD-PLANE T. Goetzendorf-Grabowski¹, D. Kacik¹, K. Pobikrowska, Lukasiewicz Research Network – Institute of Aviation, Poland; J. Mieloszyk¹; ¹Warsaw University of Technology, Poland Presenter: Katarzyna Pobikrowska, ?ukasiewicz Research Network - Institute of Aviation | |||
06. Sep 22 | 17:30 | 18:00 | 11.6.4 |
FLIGHT VERIFICATION OF AUTOMATIC TRANSITION FOR QUAD TILT WING SMALL UAV K. Muraoka¹, M. Sato¹; ¹Japan Aerospace Exploration Agency, Japan | |||
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06. Sep 22 | 16:00 | 16:30 | 12.6.1 |
ELECTRICALLY POWERED LANDING GEAR SYSTEM FOR TRANSPORT AIRCRAFT TAXIING I. Berlowitz, IBAero Engineering, Israel | |||
06. Sep 22 | 16:30 | 17:00 | 12.6.2 |
THE INFLUENCE OF THE MODEL PARAMETERS OF LI-ION BATTERIES ON THE WIRING HARNESS PERFORMANCE OF EVTOL AIRCRAFT S. Oberschwendtner¹, M. Hornung¹; ¹Technical University of Munich, Germany | |||
06. Sep 22 | 17:00 | 17:30 | 12.6.3 |
ANALYSIS AND DEVELOPMENT OF INTEGRATED LOW-PRESSURE SHAFT GENERATOR A. Reinap¹, M. Genrup¹, R. Avellán², H. Mårtensson²; ¹Lund University, Sweden ;²GKN Aerospace, Sweden | |||
06. Sep 22 | 17:30 | 18:00 | 12.6.4 |
AN INTEGRATED CONTROL SCHEME FOR STARTER/GENERATOR SYSTEM IN MORE ELECTRIC AIRCRAFT H. Li, China; Z. Zhao, China; Z. Wan, China; L. Xu, China; S. Zhao, China; P. Sun, China | |||
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06. Sep 22 | 16:00 | 16:30 | 13.6.1 |
STUDY OF THE COST EFFICIENCY AND LAMINATE QUALITY USING DIFFERENT MOULD-MAKING TECHNOLOGIES L. Loiodice¹, S. Grendene¹, T. Binetti¹, I. Boni ¹, F. Lovero ¹, R. Piani¹; ¹Politecnico di Torino, Italy | |||
06. Sep 22 | 16:30 | 17:00 | 13.6.2 |
A VALUE-DRIVEN QUANTITATIVE FRAMEWORK COUPLING AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN BY LEVERAGING THE AGILE 4.0 MBSE-MDO FRAMEWORK G. Donelli¹, J.M.G.D. Mello², F.I.K. Odaguil², T. Lefebvre³, N. Bartoli³, T. van der Laan, GKN Fokker, Netherlands; L. Boggero¹, B. Nagel¹; ¹DLR, Germany ;²Embraer, Brazil ;³ONERA, France | |||
06. Sep 22 | 17:00 | 17:30 | 13.6.3 |
REAL-TIME IDENTIFICATION OF USER ACTIONS IN COMPUTER-AIDED MANUFACTURING USING MACHINE LEARNING AND COMPUTER VISION B. Peukert¹, J. Vesterberg¹, J. Birberg, Saab AB , Sweden; ¹KTH, Sweden Presenter: Bernd Walter Peukert, KTH | |||
06. Sep 22 | 17:30 | 18:00 | 13.6.4 |
DOMAIN MODEL CONSTRUCTION METHOD OF AVIATION EQUIPMENT MANUFACTURING OPERATION MANAGEMENT L. Chen¹, X. Li¹, Z. Zhang¹, W. Huang¹, R. Wu¹, Y. Li¹; ¹AVIC Chengdu Aircraft Industrial (Group) Co., Ltd., China | |||
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06. Sep 22 | 16:00 | 16:30 | 14.6.1 |
OVERVIEW OF JAXA AND NASA COLLABORATION ON MANNED AND UNMANNED AIRCRAFT OPERATION INTEGRATION IN DISASTER RESPONSE A. Andreeva-Mori¹, J. Homola², M. Johnson², K. Kobayashi¹, Y. Okuno¹, P. Kopardekar²; ¹JAXA, Japan ;²NASA, United States Presenter: Marcus Johnson, NASA | |||
06. Sep 22 | 16:30 | 17:00 | 14.6.2 |
INTEGRATED UAS TRAJECTORY OPTIMIZATION FOR DISASTER RESPONSE RECONNAISSANCE MISSIONS A. Andreeva-Mori¹, J. Homola², M. Johnson², K. Kobayashi¹, Y. Okuno¹, P. Kopardekar²; ¹JAXA, Japan ;²NASA, United States | |||
06. Sep 22 | 17:00 | 17:30 | 14.6.3 |
DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFT (invited) J. Ritter¹, H. Kahlo¹, N. Mandry¹, A.G. Can¹, P. Modi¹, B. Knoblauch¹, J. Schneider¹, A. Stromayer¹, T. Dietl², P. Ratei², P. Shiva Prakasha², B. Nagel²; ¹University of Stuttgart, Germany ;²German Aerospace Center (DLR), Germany | |||
06. Sep 22 | 17:30 | 18:00 | 14.6.4 |
DESIGNING FOR SECURITY: A CYBERSECURITY INTRODUCTION FOR AEROSPACE EDUCATION K. Roush, United States |
18:00 - 19:30 | ICAS Speed Mentoring: For all early careers (students and young professionals) Meeting professionals from companies, research institutes, and universities in aeronautics all over the world (auditorium A1) |