
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.
Monday, 05. Sep 2022
07:00 - 08:00 | Registration |
08:00 - 09:00 | Opening Ceremony |
0.1 | ICAS Daniel & Florence Guggenheim Memorial Lecture, “Aeronautical Innovation – Swedish and European Perspectives”, Anders Blom, Sweden Chair: J.L. Azevedo ICAS President | |||
05. Sep 22 | 09:00 | 10:00 |
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10:00 - 10:30 | Coffee Break |
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05. Sep 22 | 10:30 | 11:00 | 1.1.1 |
THE SWEDISH AIR FORCE INTO THE FUTURE – AIMING FOR A HIGHER GROUND AND A SHARPER EDGE T. Petersson, Sweden | |||
05. Sep 22 | 11:00 | 11:30 | 1.1.2 |
BAE SYSTEMS ICAS BRIEF FUTURE COMBAT AIRCRAFT SYSTEM (FCAS) - THE COMPLEXITY OF THE SKILLS EQUATION Steve Hopkins, BAE Systems, United Kingdom; Ian Noakes, BAe Systems, United Kingdom | |||
05. Sep 22 | 11:30 | 12:00 | 1.1.3 |
FUTURE COMBAT AIR SYSTEMS: REQUIREMENTS AND TECHNOLOGIES G. M. Girard, Dassault Aviation, France | |||
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05. Sep 22 | 10:30 | 11:00 | 2.1.1 |
LARGE-SCALE MULTIFIDELITY AEROSTRUCTURAL OPTIMIZATION OF A TRANSPORT AIRCRAFT N. Y. Wu¹, C. A. Mader¹, J. R. R. A. Martins¹; ¹University of Michigan, United States Presenter: Neil Wu, University of Michigan | |||
05. Sep 22 | 11:00 | 11:30 | 2.1.2 |
REGIONAL JET RETROFITTING DESIGN: FROM STAKEHOLDERS’ NEEDS AND SYSTEM’S REQUIREMENTS TO MDAO WORKFLOW FORMULATION M. Mandorino¹, P. Della Vecchia¹, F. Nicolosi¹, S. Corcione¹, V. Trifari¹, G. Cerino, Leonardo Aircraft Division, Italy; M. Fioriti², C. Cabailero², T. Lefebvre, ONERA/DTIS, Université de Toulouse, France; ¹University of Naples Federico II, Italy ;²Politecnico di Torino, Italy | |||
05. Sep 22 | 11:30 | 12:00 | 2.1.3 |
COAST - A SIMULATION AND CONTROL FRAMEWORK TO SUPPORT MULTIDISCIPLINARY OPTIMIZATION AND AIRCRAFT DESIGN WITH CPACS D. Kiehn¹, J. Autenrieb¹, N. Fezans¹; ¹German Aerospace Center (DLR), Germany | |||
Reserve Paper | 2.1.R |
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 | |||||
Reserve Paper | 2.1.R |
OBJECT ORIENTED MULTI FIDELITY AIRCRAFT DESIGN TOOL FOR FIXED WING EVTOL UAVS T Seren, Chair of Aircraft Design - Technical University of Munich, Germany | |||||
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05. Sep 22 | 10:30 | 11:00 | 3.1.1 |
HIGH-SPEED COMPOUND HELICOPTER RESEARCH AT JAXA M. Sugiura¹, Y. Tanabe¹, N. Kobiki¹, H. Sugawara¹, K. Kimura¹; ¹JAXA, Japan | |||
05. Sep 22 | 11:00 | 11:30 | 3.1.2 |
DESIGN OF A FLYING V SUBSONIC TRANSPORT J. Benad¹, R. Vos¹; ¹Delft University of Technology, Netherlands | |||
05. Sep 22 | 11:30 | 12:00 | 3.1.3 |
DESIGN AND WIND TUNNEL TESTING OF A GENERAL AVIATION BLENDED WING BODY AIRCRAFT F Staub¹, T Tsuchiya¹; ¹The University of Tokyo, Japan | |||
Reserve Paper | 3.1.R |
DEVELOPMENT OF AN AERODYNAMIC ANALYSIS TOOL FOR BOUNDARY LAYER INGESTION CONCEPT DESIGN Xin Zhao¹, Carlos Xisto¹, Shia-Hui Peng, Chalmers University of Technology/FOI, Sweden; ¹Chalmers University of Technology, Sweden | |||||
Reserve Paper | 3.1.R |
EXPERIMENTAL ASSESSMENT OF A NEXT-GENERATION AIRLINER WITH BOUNDARY LAYER INGESTION P. D. Bravo-Mosquera¹, J. P. Eguea¹, H. D. Cerón-Muñoz¹, F. Catalano¹; ¹University of São Paulo, Brazil | |||||
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05. Sep 22 | 10:30 | 11:00 | 4.1.1 |
UNSTEADY TURBULENT FLOW SIMULATION OF ROTOR BLADES ON MOVING CARTESIAN GRIDS USING RECURSIVE FITTING APPROACH Keisuke Sugaya¹, Taro Imamura¹; ¹The University of Tokyo, Japan Presenter: Keisuke Sugaya, The University of Tokyo | |||
05. Sep 22 | 11:00 | 11:30 | 4.1.2 |
COMPUTATIONAL ANALYSIS OF SUPERSONIC FLOW AROUND A WEDGE AND A CYLINDER USING BUILDING-CUBE METHOD Kumpei Abe¹, Sayaka Miyazaki¹, Daisuke Sasaki¹, Shun Takahashi², Gohji Yamada²; ¹Kanazawa Institute of Technology, Japan ;²Tokai University, Japan | |||
05. Sep 22 | 11:30 | 12:00 | 4.1.3 |
ON THE INFLUENCE OF GRADIENT RECONSTRUCTION PROCEDURES OVER THE ACCURACY OF FINITE VOLUME BASED SCHEMES F. B. Oliveira, Instituto Tecnológico de Aeronáutica, Brazil; J. L. F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil | |||
Reserve Paper | 4.1.R |
INVESTIGATION OF TWO-DIMENSIONAL VORTEX DYNAMICS IN V103 CASCADE CHANNEL Yihan Zhao¹, Yang Liu¹, Shuaichen Zhu¹, Hongyi Xu¹, Duo Wang¹; ¹Department of Aeronautics and Astronautics, Fudan University, China | |||||
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05. Sep 22 | 10:30 | 11:00 | 5.1.1 |
GARTEUR: NEARLY HALF A CENTURY OF EUROPEAN COLLABORATION IN AERONAUTICS RESEARCH P. Renzoni, Centro Italiano Ricerche Aerospaziali, Italy | |||
05. Sep 22 | 11:00 | 11:30 | 5.1.2 |
THE GROUP OF RESPONSABLES AERODYNAMICS GOR AD AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES P. Coustols, ONERA, France; F. Monge, INTA, Spain; 4 van der Ven, NLR, Netherlands; K. Richter, DLR, Germany; M. Tormalm, FOI, Sweden; L.R. Calavera, AIRBUS, Spain; B. Stefes, AIRUBS, Germany; D. Pagan, MBDA, France; P. Eliasson, SAAB, Sweden; M. Mallet, DASSAULT, France; R. Gemma, LEONARDO, Italy | |||
05. Sep 22 | 11:30 | 12:00 | 5.1.3 |
THE GARTEUR GROUP OF RESPONSABLES “STRUCTURES AND MATERIALS: AN OVERVIEW OF ACTIVITIES AND SUCCES STORIES B. Thuis, NLR, Netherlands | |||
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05. Sep 22 | 10:30 | 11:00 | 6.1.1 |
EXPERIMENTAL INVESTIGATION OF THE EFFECT OF THE YAW ANGLE ON THE DRAG REDUCTION RATE FOR TRAPEZOIDAL RIBLETS A INASAWA¹, R TANIGUCHI¹, M ASAI¹, M SASAMORI², M KURITA²; ¹Tokyo Metropolitan University, Japan ;²JAXA, Japan | |||
05. Sep 22 | 11:00 | 11:30 | 6.1.2 |
ON THE GROWTH OF DISTURBANCES IN A LAMINAR SEPARATION BUBBLE SUBJECTED TO FREESTREAM TURBULENCE Thomas Jaroslawski¹, Olivier Vermeersch¹, Jean-Marc Moschetta², Maxime Forte¹, Erwin Gowree²; ¹ONERA, France ;²ISAE-SUPAERO, France | |||
05. Sep 22 | 11:30 | 12:00 | 6.1.3 |
UNIFORM MOMENTUM ZONES IN A TURBULENT BOUNDARY LAYER OVER PERFORATED WALLS F. Scarano, ISAE - SUPAERO, France | |||
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05. Sep 22 | 10:30 | 11:00 | 7.1.1 |
A SEMANTIC KNOWLEDGE BASED ENGINEERING FRAMEWORK FOR THE RAPID GENERATION OF NOVEL AIR VEHICLE CONFIGURATIONS Jacopo Zamboni¹, Arthur Zamfir¹, Erwin Moerland¹, Björn Nagel¹; ¹German Aerospace Center (DLR), Germany | |||
05. Sep 22 | 11:00 | 11:30 | 7.1.2 |
RULE-BASED VERIFICATION OF A GEOMETRIC DESIGN USING THE CODEX FRAMEWORK B. Boden¹, Y. Cabac¹, T. Burschyk¹, B. Nagel¹; ¹DLR, Germany | |||
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05. Sep 22 | 10:30 | 11:00 | 8.1.1 |
AEROELASTIC ANALYSIS OF HIGH ASPECT RATIO AND STRUT-BRACED WINGS Yoann Le Lamer¹, Emmanuel Benard¹, Joseph Morlier, ICA, Université de Toulouse, ISAE-SUPAERO, MINES ALBI, UPS, INSA, France; Ping He, Iowa State University, United States; ¹ISAE-SUPAERO, Université de Toulouse, France | |||
05. Sep 22 | 11:00 | 11:30 | 8.1.2 |
COMPARING REDUCED ORDER MODEL FORMS FOR NONLINEAR DYNAMICAL SYSTEMS D Massegur¹, D Clifford¹, A Da Ronch¹, S Symon¹; ¹University of Southampton, United Kingdom | |||
05. Sep 22 | 11:30 | 12:00 | 8.1.3 |
NUMERICAL INVESTIGATION ON THE DOUBLE TRANSONIC DIP OF SUPERCRITICAL AIRFOIL FLUTTER T Miyake¹, H Terashima¹; ¹Hokkaido University, Japan | |||
Reserve Paper (interactive) | 8.1.R |
A STUDY ON THE AEROELASTICITY OF AIR-TO-AIR MISSLE IN OVER-THE-SHOULDER LAUNCH K. Lu¹, W.-P. Song¹, K. Ye¹, C.-H. Gao¹, S.-Q Han, Sichuan University, China; ¹Northwestern Polytechnical University, China | |||||
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05. Sep 22 | 10:30 | 11:00 | 9.1.1 |
SERIES-HYBRID RETROFIT OF AN XV-15 TILTROTOR AND EMERGENCY PROCEDURE ENERGETIC ANALYSIS Giulio Avanzini, University of Salento, Italy; Giovanni Bernardini¹, Simone Moretti¹; ¹Roma Tre University, Italy | |||
05. Sep 22 | 11:00 | 11:30 | 9.1.2 |
DEVELOPMENT OF A CONTROLS STRATEGY FOR FUEL CELL-POWERED ALL-ELECTRIC AERO ENGINES BASED ON A FHA S. de Graaf¹, S. Kazula¹, L. Enghardt¹; ¹DLR e.V., Germany | |||
05. Sep 22 | 11:30 | 12:00 | 9.1.3 |
TECHNOLOGY DEMONSTRATOR HYBRID POWER SYSTEM FOR NEW GENERATION OF VTOL UNMANNED AERIAL VEHICLES WITH MTOW UP TO 300 KG M. Wojtas¹, P. Wyszkowski¹, P. Kmita¹, R. Praski¹; ¹Lukasiewicz -Institute of Aviation, Poland | |||
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05. Sep 22 | 10:30 | 11:00 | 10.1.1 |
FINITE ELEMENT MODELLING FOR THE DESIGN OF A PROTECTIVE SHIELD FOR A LEADING EDGE TO WITHSTAND BIRD STRIKE EVENTS A. De Luca, University of Campania L. Vanvitelli, Italy | |||
05. Sep 22 | 11:00 | 11:30 | 10.1.2 |
A REDUCED ORDER MODEL FOR FULL-SCALE DRONE COLLISIONS Florian Franke¹, Uli Burger¹, Christian Hühne, German Aerospace Center, Germany; ¹Technische Hochschule Ingolstadt, Germany | |||
05. Sep 22 | 11:30 | 12:00 | 10.1.3 |
HIGH FIDELITY AIRWORTHINESS BIRD AND DRONE IMPACT ANALYSIS OF ON-DEMAND AIR MOBILITY SERVICE AIRCRAFT P. Vaghela¹, H. Raza¹, E. Stumpf, Institute for Aerospace Systems, RWTH Aachen University, Germany; J. Bayandor¹; ¹CRASH Lab, University at Buffalo - The State Univ. of New York, United States | |||
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05. Sep 22 | 10:30 | 11:00 | 11.1.1 |
LANDING SIMULATION OF A HIGH-ALTITUDE PLATFORM WITH SKID-TYPE LANDING GEAR – FLIGHT PROCEDURE, CONTROLLER, AND LOADS Y. J. Hasan¹, N. Fezans¹, A. Voß, DLR, Institute of Aeroelasticity, Germany; ¹DLR, Institute of Flight Systems, Germany | |||
05. Sep 22 | 11:00 | 11:30 | 11.1.2 |
ALTITUDE ESTIMATION BY WIDE-FIELD-INTEGRATION OF OPTIC FLOW Hiromitsu HIRAIWA¹, Mai BANDO¹, Shinji HOKAMOTO¹; ¹Kyushu university, Japan | |||
05. Sep 22 | 11:30 | 12:00 | 11.1.3 |
FIXED-WING UAVS CONTROL WITH MODEL UNCERTAINTIES Dmitry Ignatyev¹, Argyrios Zolotas¹; ¹Cranfield University, United Kingdom | |||
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05. Sep 22 | 10:30 | 11:00 | 12.1.1 |
REAL-TIME CALCULATION AND ADAPTION OF CONFLICT-FREE AIRCRAFT GROUND TRAJECTORIES L. Nöhren¹, M. Schaper¹, L. Tyburzy¹, K. Muth¹; ¹German Aerospace Center (DLR), Germany | |||
05. Sep 22 | 11:00 | 11:30 | 12.1.2 |
DEVELOPING A DEPARTURE QUEUE MODEL TOWARDS INTEGRATED ARRIVAL AND DEPARTURE RUNWAY OPERATION E. Itoh, The University of Tokyo/ENRI, Japan; D. Iwata, The University of Tokyo, Japan; M. Schultz, Bundeswehr University Munich, Germany Presenter: Daiki Iwata, The University of Tokyo | |||
05. Sep 22 | 11:30 | 12:00 | 12.1.3 |
ASSESSMENT AND CONTROL OF ARRIVAL FLOW AND WAITING TIME APPLYING GT/GI/ST+GI TIME-VARYING QUEUEING MODEL Koki Higasa, The University of Tokyo, Japan; Eri Itoh, Electronic Navigation Research Institute, Japan | |||
Reserve Paper | 12.1.R |
QUANTUM ARRIVAL AND DEPARTURE MANAGEMENT Yoshikawa Nobuyuki, Mitsubishi Electric, Japan | |||||
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05. Sep 22 | 10:30 | 11:00 | 13.1.1 |
LONG TOUCHDOWN THROUGH A SAFETY-II PERSPECTIVE C. Reiser, Embraer, Brazil; E. Villani¹, M. Machado Cardoso Junior¹; ¹ITA, Brazil Presenter: Moacyr Machado Cardoso Junior, ITA | |||
05. Sep 22 | 11:00 | 11:30 | 13.1.2 |
DECISION LADDER APPLICATION ANALYZING A HELICOPTER EMERGENCY Bruno R. Teixeira¹, Luís G L. de Paula¹, Alexandre C. S. Freitas¹, Raphael G. Cortes², Marcelle Y. D. Ribeiro², Moacyr M. C. Júnior², Emília Vilani²; ¹Brazilian Air Force Flight Test and Research Institute, Brazil ;²Instituto Tecnológico de Aeronáutica , Brazil Presenter: Moacyr Machado Cardoso-Júnior, Aeronautical Institute of Technology | |||
05. Sep 22 | 11:30 | 12:00 | 13.1.3 |
SYSTEM SAFETY-BASED SUSTAINABLE AVIATION FUEL SAFETY ASSESSMENT METHOD AND AIRWORTHINESS CERTIFICATION S Ding, Civil Aviation University of China, China; C Gan¹, T Qiu¹, P Liu¹; ¹Beihang University, China | |||
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05. Sep 22 | 10:30 | 11:00 | 14.1.1 |
OPERATIONAL FEASIBILITY STUDY OF AIR TAXI SERVICE USING EVTOL H. Takizawa¹, Z. LEI¹; ¹Suwa University of Science, Japan | |||
05. Sep 22 | 11:00 | 11:30 | 14.1.2 |
NEW GENERATION SPACE VEHICLE OPERATIONS IN THE UNITED ARAB EMIRATES – AN AIRSPACE AND RISK ASSESSMENT O. Lehmann¹, R. El-Jabi¹, K. Webster¹, A. Rachdi¹; ¹Abu Dhabi University, United Arab Emirates | |||
05. Sep 22 | 11:30 | 12:00 | 14.1.3 |
EQUIVALENT CALCULATION METHOD OF FLYOVER NOISE LEVEL OF CUTBACK TAKE-OFF FOR CIVIL JET AIRPLANE AIRWORTHINESS CERTIFICAT SONG Yahui¹, ZHANG Xiaoliang¹, LIU Qiuhong, Northwestern Polytechnical University, China; ZHANG Yuelin¹; ¹Chinese Flight Test Establishment, China | |||
Reserve Paper | 14.1.R |
A GLOBAL APPROACH TO ASSESSING THE CLIMATE RESILIENCE OF AIRPORTS M P Osund-Ireland¹, A J Powell¹, C J Ireland¹; ¹susteer AB, Sweden | |||||
Reserve Paper (interactive) | 14.1.R |
THE DIONYSUS PROGRAM: 99942 APOPHIS, TRANS-MARS INJECTION AND SPACE LIFT CONSTRUCTION (99942 AT-MIASLC) A Sanks, United States Air Force Academy, United States |
12:00 - 13:00 | Lunch Break |
0.2 | GL1 “Future Airspace – Meeting Demand Through Integration” Lynne Thompson Hopper, USA Chair: S. Bagassi ICAS EC member | |||
05. Sep 22 | 13:00 | 14:00 |
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05. Sep 22 | 14:10 | 14:40 | 1.2.1 |
A ROADMAP TOWARDS AN ENVIRONMENTALLY SUSTAINABLE AVIATION MARKETPLACE B Loxton, MAGNIX, United States | |||
05. Sep 22 | 14:40 | 15:10 | 1.2.2 |
HYBRID ELECTRIC PROPULSION DEVELOPMENT FOR COMMERCIAL AVIATION C. Andrews, GE, United States Presenter: Christine Andrews, GE | |||
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05. Sep 22 | 14:10 | 14:40 | 2.2.1 |
MULTIDISCIPLINARY DESIGN OF AN ADVANCED EMPENNAGE AND REAR FUSELAGE CONCEPT FOR A COMMERCIAL AIRCRAFT R.C. Llamas-Sandin¹, C.D. Handal-Rivera¹; ¹Airbus OSL, Spain | |||
05. Sep 22 | 14:40 | 15:10 | 2.2.2 |
SYSTEMS ARCHITECTING A PRACTICAL EXAMPLE OF DESIGN SPACE MODELING AND SAFETY-BASED FILTERING WITHIN THE AGILE 4.0PROJECT A.K. Jeyaraj¹, J.H. Bussemaker², S. Liscouët-Hanke¹, L. Boggero²; ¹Concordia University, Canada ;²DLR, Germany | |||
05. Sep 22 | 15:10 | 15:40 | 2.2.3 |
AN EFFICIENT SOLUTION FOR AERODYNAMIC SHAPE OPTIMIZATION WITHIN THE MID-RANGE APPROXIMATION FRAMEWORK Y. ZHANG¹, F. QU¹, J. Q. BAI¹, D. S. JIA², E. K. Bontoft², V. V. Toropov²; ¹Northwestern Polytechnical University, China ;²Queen Mary University of London, United Kingdom | |||
Reserve Paper | 2.2.R |
EFFICIENT SURROGATE-BASED MULTI-OBJECTIVE OPTIMIZATION ALGORITHM WITH A NEW ADAPTIVE WEIGHT VECTORS 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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05. Sep 22 | 14:10 | 14:40 | 3.2.1 |
UNMANNED AERIAL VEHICLE – HUMAN PERFORMANCE EVALUTION UNDER CRITICAL OPERATIONAL SCENARIO Andrew Gomes P. Sarmento ¹, Thiago Rosado de Paula ¹, Emilia Villani ², Abner Souza Oliveira ², Moacyr Machado Cardoso ², Henrique Costa Marques ²; ¹Aeronautics Institute of Technology, Brazil ;²Aeronautics Institute of Technology , Brazil Presenter: Emilia Villani , Aeronautics Institute of Technology | |||
05. Sep 22 | 14:40 | 15:10 | 3.2.2 |
RESEARCH ON THE OVERALL DESIGN OF A HIGH-SPEED MORPHING UAV C. Ding, School of Aeronautic Science and Engineering,Beihang University, China; T.-L. Ma, Institute of Unmanned System, Beihang University, China; J.-C. Fu, School of Transportation ScienceandEngineering,BeihangUniversity, China; X.-S. Wang, School of Aeronautic Science and Engineering, Beihang University, China | |||
05. Sep 22 | 15:10 | 15:40 | 3.2.3 |
MULTIDISCIPLINARY DESIGN OPTIMIZATION OF A LOW OBSERVABLE UAV Muhammad Shafique, Insitute of Space Technology, Pakistan; Dr. Syed Hussein Raza Hamadani¹, Sohaib Khan¹, Taimoor Jan Durrani¹; ¹Institute of Space Technology, Pakistan | |||
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05. Sep 22 | 14:10 | 14:40 | 4.2.1 |
VALIDATION STUDY OF BLUNTED AND SHARP CONES AT HYPERSONIC SPEED E. K. T. Carias¹, S. A. Prince¹; ¹Cranfield University, United Kingdom | |||
05. Sep 22 | 14:40 | 15:10 | 4.2.2 |
AERODATABASE DEVELOPMENT AND INTEGRATION OF HYPERSONIC CRUISER VEHICLES IN MORE&LESS PROGRAM P. Roncioni¹, M. Marini¹, R. Fusaro², N. Viola²; ¹CIRA, Italy ;²POLITO, Italy | |||
05. Sep 22 | 15:10 | 15:40 | 4.2.3 |
TURBULENCE MODELLING STUDIES OF SHOCK-WAVE/BOUNDARY-LAYER INTERACTIONS ON HIFIRE-1 AXISYMMETRIC CONE CYLINDER FLARE FA Maulana, Bandung Institute of Technology, Indonesia | |||
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05. Sep 22 | 14:10 | 14:40 | 5.2.1 |
THE GROUP OF RESPONSABLES “FLIGHT MECHANICS, SYSTEMS AND INTEGRATION”: AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES Bernd Korn, DLR, Germany; Martin Hagström, FOI, Sweden | |||
05. Sep 22 | 14:40 | 15:10 | 5.2.2 |
• THE GROUP OF RESPONSABLES “ROTORCRAFT (GOR RC)”: AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES Antonio Visingardi, CIRA, Italy; Rainer Heger, Airbus Helicopters, Germany; Arnaud Le Pape, ONERA, France; Richard Markiewicz, DSTL, United Kingdom; Barbara Ohlenforst, NLR, Netherlands; Klausdieter Pahlke, DLR, Germany; Mark White, University of Liverpool, United Kingdom | |||
05. Sep 22 | 15:10 | 15:40 | 5.2.3 |
AVIATION SECURITY CONCERNS Angela Vozella, Italian Aerospace Research Centre, Italy; Pierre Bieber, ONERA, France | |||
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05. Sep 22 | 14:10 | 14:40 | 6.2.1 |
STRAKE SECTION IMPACT ON HYBRID-DELTA-WING AERODYNAMICS D. Sedlacek, Technical University of Munich, Germany | |||
05. Sep 22 | 14:40 | 15:10 | 6.2.2 |
VOLUMETRIC VELOCITY MEASUREMENTS OF A HELICAL VORTEX PAIR Dominic Schröder¹, Thomas Leweke, CNRS, Aix-Marseille Université, Centrale Marseille, France; Ralf Hörnschemeyer¹, Eike Stumpf¹; ¹Institute of Aerospace Systems, RWTH Aachen University, Germany | |||
05. Sep 22 | 15:10 | 15:40 | 6.2.3 |
CFD AND EXPERIMENTS ON THE DLR-F23 COMBAT AIRCRAFT WIND TUNNEL MODEL J. Zastrow¹, F. Oberdieck¹, U. Henne¹, C. Klein¹; ¹DLR - German Aerospace Center, Germany | |||
Reserve Paper (interactive) | 6.2.R |
INFLUENCE OF TIP DIHEDRAL ON ROTOR AERODYNAMIC PERFORMANCE AND TIP VOTEX M.-H. Kang¹, X. Zhao¹, R. Yao¹, H.-Y. Li¹; ¹Norhwestern Polytechnical University, China Presenter: Hongyan Li, Norhwestern Polytechnical University | |||||
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05. Sep 22 | 14:10 | 14:40 | 7.2.1 |
ASSESSMENT OF THE SUSTAINABILITY OF THE IMPLEMENTATION OF CIRCULAR ECONOMY PRINCIPLES IN PRODUCING AIRCRAFT STRUCTURES Dionysios Markatos¹, Spiros Pantelakis¹; ¹University of Patras, Greece Presenter: Dionysios Markatos | |||
05. Sep 22 | 14:40 | 15:10 | 7.2.2 |
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 | |||
05. Sep 22 | 15:10 | 15:40 | 7.2.3 |
SIGMOIDAL SENSING DEVICES FOR MONITORING TO IMPROVE MAINTENANCE OPERATIONS IN AERONAUTICS Helge Pfeiffer¹, Hans Sekler, Deutsche Lufthansa AG, Germany; Martine Wevers¹; ¹KU Leuven, Belgium | |||
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05. Sep 22 | 14:10 | 14:40 | 8.2.1 |
XRF1 HIGH LIFT LOAD ANALYSIS OF WING AND HIGH LIFT SYSTEM S. Pülm¹, V. Handojo¹, R. B. Seidler¹; ¹German Aerospace Center (DLR), Germany Presenter: Sven Pülm, German Aerospace Center (DLR) | |||
05. Sep 22 | 14:40 | 15:10 | 8.2.2 |
AEROELASTIC STABILITY ANALYSIS OF THE HAMMERHEAD LAUNCH VEHICLE USING CFD-CAE COUPLED METHOD IN THE TRANSONIC REGION H.G. Rho, Korea Aerospace Univeristy, South Korea; J.S. Bae¹, S.H. Park, Konkuk University, South Korea; P.-A. Nguyen¹; ¹Korea Aerospace University, South Korea | |||
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05. Sep 22 | 14:10 | 14:40 | 9.2.1 |
ASSESSMENT OF A SERIAL COOLING CONCEPT FOR HTPEM FUEL CELL SYSTEMS FOR AVIATION APPLICATIONS A. Link¹, J. Ludowicy¹, M. Staggat¹; ¹German Aerospace Center (DLR), Germany | |||
05. Sep 22 | 14:40 | 15:10 | 9.2.2 |
LITHIUM-ION BATTERY HAZARD IDENTIFICATION AND SAFETY RISK MANAGEMENT IN AIRCRAFT WITH ELECTRIC PROPULSION T. Raoofi¹, M. Yildiz, Erciyes university, Turkey; S. Tolun¹; ¹University of Kyrenia, Turkey | |||
05. Sep 22 | 15:10 | 15:40 | 9.2.3 |
DEMONSTRATION FLIGHTS OF HYBRID ELECTRIC AIRCRAFT P. Bohnert, United Kingdom; S. X. Ying, United States; M. Selier, Netherlands | |||
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05. Sep 22 | 14:10 | 14:40 | 10.2.1 |
MACHINE LEARNING METHODS ENSURING BOTH PERFORMANCE AND INTERPRETABILITY OF ESTIMATING AIRCRAFT ARRIVAL TIMES N. Morikawa, Faculty of Aerospace Engineering, The University of Tokyo, Japan; E. Itoh, Air Traffic Management Department, Electronic Navigation Researc, Japan | |||
05. Sep 22 | 14:40 | 15:10 | 10.2.2 |
APPLYING MACHINE LEARNING FOR TAXI-TIME PREDICTION AT TOKYO INTERNATIONAL AIRPORT E. Itoh, The University of Tokyo, Japan | |||
05. Sep 22 | 15:10 | 15:40 | 10.2.3 |
AN AUCTION-BASED MECHANISM FOR A PRIVACY-PRESERVING MARKETPLACE FOR ATFM SLOTS C. G. Schuetz, Johannes Kepler University Linz, Austria; S. Ruiz, EUROCONTROL Innovation Hub, France; E. Gringinger¹, C. Fabianek¹, Thomas Loruenser, AIT Austrian Institute of Technology, Austria; ¹Frequentis AG, Austria | |||
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05. Sep 22 | 14:10 | 14:40 | 11.2.1 |
EXPECTED TEAMWORK ATTRIBUTES BETWEEN HUMAN OPERATOR AND AUTOMATION IN AIR TRAFFIC CONTROL Å Svensson, LFV, Sweden; N Rönnberg, Linköping University, Sweden | |||
05. Sep 22 | 14:40 | 15:10 | 11.2.2 |
HANDLING QUALITIES RATING SCALE THE IMPACT OF THE PILOT SUBJECTIVITY IN WORKLOAD EVALUATION Mariane D. Turaça, Universidade de São Paulo, Brazil | |||
05. Sep 22 | 15:10 | 15:40 | 11.2.3 |
PILOT’S ATTENTION DISTRIBUTION MODELING USING HIDDEN MARKOV MODELS Jiri Hanak¹, Jan Vlk¹, Peter Chudy¹; ¹Brno University of Technology, Czech Republic | |||
Reserve Paper | 11.2.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 | 11.2.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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05. Sep 22 | 14:10 | 14:40 | 12.2.1 |
DIGITAL TWIN CAPABILITIES AND CHALLENGES IN THE CONTEXT OF IVHM IN AVIATION M. Castaño Arranz, Luleå University of Technology, Sweden | |||
05. Sep 22 | 14:40 | 15:10 | 12.2.2 |
OPERABILITY PROJECTION OF MAJOR AIRCRAFT COMPONENTS DURING EARLY AIRCRAFT DESIGN S. S. MANIKAR, Airbus/ ISAE-SUPAERO, France; J. JEZEGOU¹, P. de SAQUI-SANNES¹, P. ASSEMAN, Airbus, France; E. BENARD¹; ¹ISAE-SUPAERO, France | |||
05. Sep 22 | 15:10 | 15:40 | 12.2.3 |
DIGITAL TWIN CONCEPT FOR AIRCRAFT COMPONENTS H. Meyer¹, A.-K. Koschlik¹, F. Raddatz¹; ¹German Aerospace Center, Germany | |||
Reserve Paper | 12.2.R |
DESIGNING SUSTAINABLE AVIATION SOLUTIONS WITH DIGITAL TWIN APPROACH M. J. Grundström , Tampere university, Finland | |||||
Reserve Paper (interactive) | 12.2.R |
ESTIMATION OF ROTOR IMBALANCE AND MODEL DISCREPANCY USING A BAYESIAN APPROACH Rahul Rameshbabu¹, Dushhyanth Rajaram¹, Olivia J. Pinon Fischer¹, Dimitri N. Mavris¹; ¹Georgia Institute of Technology, United States |
15:40 - 16:00 | Break |
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05. Sep 22 | 16:00 | 16:30 | 1.3.1 |
A MULTIFIDELITY MULTIDISCIPLINARY APPROACH TO UNCONVENTIONAL AIRCRAFT DEVELOPMENT AND ASSESSMENT WITH APPLICATIONS D. W. Zingg, University of Toronto Institute for Aerospace Studies, Canada | |||
05. Sep 22 | 16:30 | 17:00 | 1.3.2 |
OVERVIEW OF AERODYNAMIC DESIGN ACTIVITIES PERFORMED AT ONERA TO REDUCE AVIATION\'S CLIMATE IMPACT M. Méheut¹, G. Arnoult¹, O. Atinault¹, Q. Bennehard¹, C. Francois¹; ¹ONERA, France | |||
05. Sep 22 | 17:00 | 17:30 | 1.3.3 |
MDAO OF A TRANSONIC TRUSS-BRACED WING VISION VEHICLE N. A. Harrison, the Boeing Co., United States | |||
05. Sep 22 | 17:30 | 18:00 | 1.3.4 |
APPLICATION OF AERODYNAMICS AND AERO-STRUCTURAL OPTIMIZATION FOR ENERGY EFFICIENT AIRCRAFT O Brodersen, Germany | |||
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05. Sep 22 | 16:00 | 16:30 | 2.3.1 |
VALIDATION OF SCALED FLIGHT TESTING P. Schmollgruber, ONERA, France | |||
05. Sep 22 | 16:30 | 17:00 | 2.3.2 |
TECHNOLOGY INTEGRATION FOR FUTURE AIRCRAFT CONFIGURATIONS D Reckzeh, Airbus, Germany | |||
05. Sep 22 | 17:00 | 17:30 | 2.3.3 |
MARKET ANALYSIS, TLARS SELECTION AND PRELIMINARY DESIGN INVESTIGATIONS FOR A REGIONAL HYBRID-ELECTRIC AIRCRAFT V. Marciello¹, M. Ruocco, SmartUp Engineering s.r.l., Italy; F. Nicolosi¹, M. Di Stasio¹; ¹University of Naples Federico II, Italy | |||
05. Sep 22 | 17:30 | 18:00 | 2.3.4 |
UNMANNED AEW/ISR PLATFORM CONCEPTUAL DESIGN AND TECHNOLOGY ASSESSMENT K. Amadori, Saab Aeronautics, Sweden; M. Emeneth, PACE America Inc., United States; A. Papageorgiou, Linköpings University, Sweden | |||
Reserve Paper (interactive) | 2.3.R |
INVENTIVE PROBLEM-SOLVING PRINCIPLES APPLIED TO DECISION-MAKING PROCESS OF PRODUCTS PLATFORM P.B. Barros Soares, Embraer S.A., Brazil | |||||
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05. Sep 22 | 16:00 | 16:30 | 3.3.1 |
A COMMON FRAMEWORK FOR THE DESIGN OPTIMIZATION OF FIXED-WING, MULTICOPTER AND VTOL UAV CONFIGURATIONS F. Pollet¹, S. Delbecq¹, M. Budinger, ICA, Université de Toulouse, ISAE-SUPAERO, MINES ALBI, UPS, INSA, France; J.-M. Moschetta¹, J. Liscouët, Concordia University, Canada; ¹ISAE-SUPAERO, France | |||
05. Sep 22 | 16:30 | 17:00 | 3.3.2 |
DESIGN OF A HALE UAV FOR ATMOSPHERIC IMAGING V. Nan Fernandez-Ayala¹, L. Vimláti¹, A. Matoses Gimenez¹, H. Delmotte¹, M. Ivchenko¹, R. Mariani¹; ¹KTH Royal Institute of Technology, Sweden | |||
05. Sep 22 | 17:00 | 17:30 | 3.3.3 |
ENHANCING UAS DESIGN PROCESS FOR SPECIFIC CATEGORY OPERATIONS USING SORA. R. Kalra¹, P. Flores-Peña, Drone Hopper S.L., Spain; A. Sanchez-Carmona¹, C. Cuerno-Rejado¹; ¹Universidad Politécnica de Madrid, Spain | |||
05. Sep 22 | 17:30 | 18:00 | 3.3.4 |
OPENVSP BASED AERODYNAMIC DESIGN OPTIMIZATION TOOL BUILDING METHOD AND ITS APPLICATION TO TAILLESS UAV J. Kim¹, T. Tsuchiya¹; ¹The University of Tokyo, Japan | |||
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05. Sep 22 | 16:00 | 16:30 | 4.3.1 |
MODEL-BASED PERFORMANCE EVALUATION OF AIRCRAFT ACTUATOR TECHNOLOGIES F Larsson¹, C Reichenwallner², A Dell'Amico¹, P Krus²; ¹Saab AB, Sweden ;²Linköping University, Sweden | |||
05. Sep 22 | 16:30 | 17:00 | 4.3.2 |
A COMPARATIVE ANALYSIS OF INNOVATIVE DIGITAL HYDRAULIC ACTUATORS FOR PRIMARY FLIGHT CONTROL R. Simões Lopes Junior¹, D. Oliveira e Silva¹, M. P. Nostrani¹, A. Dell´Amico, Saab AB, Sweden; P. Krus, Linköping University, Sweden; V. J. De Negri¹; ¹Federal University of Santa Catarina, Brazil | |||
05. Sep 22 | 17:00 | 17:30 | 4.3.3 |
AN EVALUATION METHOD FOR AIRCRAFT ACTUATION SYSTEMS OPERATIONAL COST C Reichenwallner, Linköping university, Sweden; F Larsson¹, A Dell'Amico¹; ¹Saab AB, Sweden | |||
05. Sep 22 | 17:30 | 18:00 | 4.3.4 |
DEVELOPMENT OF A HIGH EFFICIENT HYDRAULIC POWER PACK L.Z. Lima¹, M.N. Duval¹, T. Zantner¹, D. Metzler¹, T. Lammering¹, F. Thielecke², N. Trochelmann², P.S. Bischof²; ¹Liebherr-Aerospace Lindenberg GmbH, Germany ;²Hamburg University of Technology, Germany Presenter: Leonardo Zanetti de Lima | |||
Reserve Paper | 4.3.R |
USING EXISTING HARDWARE IN THE EARLY CONCEPT PHASE OF FLIGHT CONTROL ACTUATION SYSTEM DESIGN A. Dell'Amico, Sweden | |||||
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05. Sep 22 | 16:00 | 16:30 | 5.3.1 |
FLYZERO: THE UK VISION FOR ZERO-CARBON EMISSION AIR TRAVEL D J Debney, Aerospace Technology Institute, United Kingdom | |||
05. Sep 22 | 16:30 | 17:00 | 5.3.2 |
IMPACT OF NASCENT TECHNOLOGIES ON THE SUSTAINABILITY ATTRIBUTES OF AN EVOLUTIONARY SINGLE-AISLE AIRCRAFT N.J. Allen, Aerospace Technology Institute, United Kingdom; M.R. Schofield, Ellondee Ltd, United Kingdom | |||
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05. Sep 22 | 15:30 | 16:00 | 6.3.1 |
NUMERICAL AND EXPERIMENTAL STRUCTURAL CHARACTERIZATION OF COMPOSITE ADVANCED JOINT FOR ULTRA LIGHT AEROSPACE PLATFORMS A. Polla, Politecnico di Torino; Royal Melbourne Institute of Technology, Italy; G. Frulla¹, E. Cestino¹, R. Das², P. Marzocca²; ¹Politecnico di Torino, Italy ;²Royal Melbourne Institute of Technology, Australia Presenter: Enrico Cestino, Politecnico di Torino | |||
05. Sep 22 | 16:00 | 16:30 | 6.3.2 |
COMPARISON OF SCARF REPAIR AND SCARF JOINT PERFORMANCE UNDER TENSILE LOAD CONSIDERING THE EFFECT OF STACKING SEQUENCE S Tashi, Sharif University of Technology, Iran | |||
05. Sep 22 | 16:30 | 17:00 | 6.3.3 |
DAMAGE RECOGNITION OF COMPOSITE STRUCTURES BASED ON DOMAIN ADAPTIVE MODEL Shuaishuai Lyu, China | |||
05. Sep 22 | 17:30 | 18:00 | 6.3.4 |
APPLICATION OF THE VIRTUAL CRACK CLOSURE TECHNIQUE FOR CRACKS IN BUILT-UP PANELS W. R. P. Mendonca¹, M. R. B. Rodrigues¹; ¹Embraer S.A., Brazil Presenter: Willy Mendonca, Embraer S.A. | |||
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05. Sep 22 | 16:00 | 16:30 | 7.3.1 |
WIND TUNNEL EXPERIMENT WITH AN EPP-WING TO INVESTIGATE AEROELASTIC EFFECTS OF NONLINEAR ELASTIC STIFFNESSES K. Bramsiepe¹, M. Braune¹, W. Krüger¹, L. Tichy¹; ¹DLR - Institute of Aeroelasticity, Germany | |||
05. Sep 22 | 16:30 | 17:00 | 7.3.2 |
DESIGN OF AN INNOVATIVE WING TIP FOR AEROELASTIC CONTROL: FROM SCRATCH TO FLIGHT TEST Francesco Toffol¹, Federico Fonte, Leonardo Helicopters, Italy; Sergio Ricci¹; ¹Politecnico di Milano, Italy | |||
05. Sep 22 | 17:00 | 17:30 | 7.3.3 |
LONGITUDINAL DYNAMICS IDENTIFICATION OF A FLEXIBLE UAV P. Fernandes, Brazil | |||
05. Sep 22 | 17:30 | 18:00 | 7.3.4 |
EVALUATION ENVIRONMENT FOR CASCADED AND PARTLY DECENTRALIZED MULTI-RATE LOAD ALLEVIATION CONTROLLERS C. Wallace¹, S. Schulz¹, N. Fezans¹, T. Kier¹, G. Weber, Liebherr-Aerospace, Germany; ¹German Aerospace Center (DLR), Germany | |||
Reserve Paper | 7.3.R |
SOME EXPERIMENTAL RESULTS ON DYNAMIC AEROELASTICITY OF PLATES AND SHELLS IN SUBSONIC AND SUPERSONIC FLOW. J. Lübker, Germany | |||||
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05. Sep 22 | 16:00 | 16:30 | 8.3.1 |
A COMPARITIVE ASSESSMENT OF MULTI-OBJECTIVE OPTIMISATION METHODOLOGIES FOR AERO-ENGINE NACELLES A. Swarthout¹, D. MacManus¹, F. Tejero¹, J. Matesanz-Garcia¹, L. Boscagli¹, C. Sheaf, Rolls Royce Plc., United Kingdom; ¹Cranfield University, United Kingdom | |||
05. Sep 22 | 16:30 | 17:00 | 8.3.2 |
KNOWLEDGE-BASED CONCEPTUAL DESIGN METHODS FOR GEOMETRY AND MASS ESTIMATION OF RUBBER AERO ENGINES J. Häßy¹, J. Schmeink¹; ¹DLR, Germany | |||
05. Sep 22 | 17:00 | 17:30 | 8.3.3 |
COUPLED AEROPROPULSIVE ANALYSIS AND OPTIMIZATION OF A HIGH BYPASS TURBOFAN ENGINE A. H. R. Lamkin¹, A. Yildirim¹, J. R. R. A. Martins¹; ¹University of Michigan, United States | |||
Reserve Paper (interactive) | 8.3.R |
MULTIDISCIPLINARY OPTIMIZATION OF COMBUSTION CHAMBER FOR SMALL GAS TURBINE ENGINES Cong-Anh Pham¹, Quang-Hai Nguyen¹, Tuan-Anh Vu¹, Nhu-Van Nguyen¹, Phi-Minh Nguyen¹; ¹Viettel Aerospace Institute, Viettel Group, Vietnam Presenter: Nhu-Van Nguyen, Viettel Aerospace Institute, Viettel Group | |||||
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05. Sep 22 | 16:00 | 16:30 | 9.3.1 |
FLIGHT DYNAMICS SIMULATION AND FCS AUTO-GENERATION IN THE CONCEPTUAL DESIGN PHASE OF AN UNSTABLE SUPERSONIC AIRCRAFT E Johansson¹, P Månsson¹, P Sjöberg¹; ¹Saab Aeronautics, Sweden | |||
05. Sep 22 | 16:30 | 17:00 | 9.3.2 |
VALIDATION OF A HYBRID LOADS OBSERVER FOR A SUBSCALE TEST AIRCRAFT WITH DISTRIBUTED ELECTRIC PROPULSION O. Luderer¹, F. Thielecke¹; ¹Hamburg University of Technology, Germany | |||
05. Sep 22 | 17:00 | 17:30 | 9.3.3 |
A BI-LEVEL CO-DESIGN APPROACH FOR MULTICOPTERS J. MABBOUX¹, S. DELBECQ¹, V. POMMIER-BUDINGER¹, J. BORDENEUVE-GUIBE¹, A. TRUC-HERMEL², J.-M. KAI²; ¹ISAE Supaero, France ;²SAFRAN, France | |||
05. Sep 22 | 17:30 | 18:00 | 9.3.4 |
DEEP REINFORCEMENT LEARNING FOR EVTOL HOVERING CONTROL D.S. Alarcon¹, J. H. Bidinotto¹; ¹University of São Paulo, Brazil | |||
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05. Sep 22 | 16:00 | 16:30 | 10.3.1 |
ATTENTION-BASED RECURRENT NEURAL NETWORK ASSISTED EXTENDED KALMAN FILTER FOR MANEUVERING TARGET TRACKING Dongshik Won¹, Dongwoo Lee¹, Hyochoong Bang¹; ¹KAIST, South Korea | |||
05. Sep 22 | 16:30 | 17:00 | 10.3.2 |
OPTIMAL HOVERING WING KINEMATICS OF FLAPPING-WING MODEL USING REINFORCEMENT LEARNING H.-H. Yang¹, S.-G. Lee¹, Y.-J. Han¹, J.-H. Han¹; ¹Korea Advanced Institute of Science and Technology, South Korea Presenter: Hyeon-Ho Yang, Korea Advanced Institute of Science and Technology | |||
05. Sep 22 | 17:00 | 17:30 | 10.3.3 |
PREFLIGHT DIAGNOSIS OF MULTICOPTER ACTUATOR FAULT USING SUPERVISED LEARNING WITH DISTURBANCE OBSERVER OUTPUTS T.G Kim¹, Y.J Kim¹, S.K Kim¹; ¹Chungnam National University, South Korea | |||
05. Sep 22 | 17:30 | 18:00 | 10.3.4 |
USING DEEP REINFORCEMENT LEARNING TO IMPROVE THE ROBUSTNESS OF UAV LATERAL-DIRECTIONAL CONTROL Rui Wang¹, Zhou Zhou¹, Zhu Xiaoping¹, Zheng Liming, Delft University of Technology, Netherlands; ¹Northwestern Polytechnical University, China | |||
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05. Sep 22 | 16:00 | 16:30 | 11.3.1 |
IMPROVED CONFIGURATION MANAGEMENT FOR GREENER APPROACHES – EVALUATION OF A NOVEL PILOT SUPPORT CONCEPT T. Bauer¹, F. Abdelmoula¹, J. Boyer, Thales, France; M. Gerber, Swiss Sklylab Foundation, Switzerland; J. Meister², J. M. Wunderli²; ¹DLR e.V., Germany ;²Empa, Swiss Fed. Laboratories for Materials Science & Technology, Switzerland | |||
05. Sep 22 | 16:30 | 17:00 | 11.3.2 |
A COMPARISON OF CLIMATE-OPTIMISED AND FUEL-OPTIMISED INTERMEDIATE STOP OPERATIONS FOR SELECTED CASE STUDIES Z. L. Zengerling¹, F. Linke¹, C. Weder¹, Katrin Dahlmann¹; ¹Deutsches Zentrum für Luft- und Raumfahrt, Germany | |||
05. Sep 22 | 17:00 | 17:30 | 11.3.3 |
IMPLICATIONS OF POTENTIAL NEW REGULATORY MEASURES TO ADDRESS AVIATION EMISSIONS A. NIETO¹, G. ALONSO¹, J. CUBAS¹; ¹Universidad Politécnica de Madrid, Spain | |||
05. Sep 22 | 17:30 | 18:00 | 11.3.4 |
AN ENGINELESS TAXI OPERATIONS SYSTEM USING BATTERY-OPERATED AUTONOMOUS TOW TRUCKS S. Zaninotto¹, J. Gauci¹, B. Zammit¹; ¹University of Malta, Malta | |||
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05. Sep 22 | 16:00 | 16:30 | 12.3.1 |
A NOVEL METHOD FOR DETECTING UAVS USING PARALLEL NEURAL NETWORKS WITH RE-INFERENCE H. Stepien, Saab Aeronautics, Sweden; M. Bilger, Saab Surveillance, Sweden; H. Forsberg¹, B. Lindgren, Saab Dynamics, Sweden; J. Hjorth¹; ¹Mälardalen University, Sweden | |||
05. Sep 22 | 16:30 | 17:00 | 12.3.2 |
URBAN AIR TRAFFIC MANAGEMENT FOR COLLISION AVOIDANCE WITH UNCOOPERATIVE AIRSPACE USERS I. Panchal¹, I.C. Metz, German Aerospace Center, Germany; M. Ribeiro, TU Delft, Netherlands; S.F. Armanini¹; ¹TU Munich, Germany | |||
05. Sep 22 | 17:00 | 17:30 | 12.3.3 |
A HUMAN-MACHINE INTERFACE ANALYSIS FOR TELEOPERATION OF UAV OVERTIME DELAY A. G. P. Sarmento¹, T. Rosado de Paula¹, A. S. Oliveira¹, E. T. da Silva¹, J. Possamai¹, H. C. Marques¹, M. M. Cardoso Junior¹, E. Villani¹; ¹Aeronautics Institute of Technology (ITA), Brazil Presenter: Moacyr Machado Cardoso Júnior , Aeronautics Institute of Technology | |||
05. Sep 22 | 17:30 | 18:00 | 12.3.4 |
IMAGE SEGMENTATION BASED EMERGENCY LANDING FOR AUTONOMOUS AND AUTOMATED UNMANNED AERIAL VEHICLES P. Hausmann¹, H. Meeß, Fraunhofer IVI, Germany; G. Elger¹; ¹Technische Hochschule Ingolstadt, Germany | |||
Reserve Paper | 12.3.R |
EVALUATION AND QUANTIFICATION OF THE POTENTIAL CONSEQUENCES OF BIRD STRIKES IN URBAN AIR MOBILITY A. Devta¹, I. C. Metz, DLR, Germany; S. F. Armanini¹; ¹Technical University of Munich, Germany | |||||
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05. Sep 22 | 16:00 | 16:30 | 13.3.1 |
THE ALBATROSS PROJECT – A EUROPEAN INITIATIVE TO REDUCE AVIATION’S CARBON DIOXIDE EMISSIONS IN LARGE SCALE Falk Sachs¹, Fethi Abdelmoula¹, Dennis Vechtel¹; ¹DLR, Germany Presenter: Dennis Vechtel, DLR | |||
05. Sep 22 | 16:30 | 17:00 | 13.3.2 |
ZERO-EMISSION REGIONAL AVIATION IN SCANDINAVIA R. T. Sorrentino¹, R. C. Parello¹, M. Delage¹, C. Y. Justin¹, D. N. Mavris¹, C. Jouannet², K. Amadori²; ¹Georgia Institute of Technology, United States ;²Saab AB/Saab Aeronautics, Sweden Presenter: Robbie Sorrentino, Georgia Institute of Technology | |||
05. Sep 22 | 17:00 | 17:30 | 13.3.3 |
PERFORMANCE EVALUATION OF THE ARRIVAL OPERATIONS IN TERMINAL AREA H Hardell¹, A Lemetti¹, T Polishchuk¹; ¹Linköping University, Sweden | |||
05. Sep 22 | 17:30 | 18:00 | 13.3.4 |
AERODYNAMIC INVESTIGATION OF VERY CLOSELY FLYING FIGHTERS TO DEVELOP NEW FORMATION TYPES Süleyman Mert Aydin¹, Abdurrahman Gazi Yavuz, Turkish Aerospace Industries, Turkey; Mustafa Kaya¹; ¹Yildirim Beyazit University, Turkey | |||
Reserve Paper | 13.3.R |
DATA-DRIVEN APPROACH TO OPTIMAL AIRCRAFT MAINTENANCE O.C Okoro¹, M Zaliskyi¹, D Serhii , National Aviation University , Ukraine; S Qudus, Tamara Niger Aviation, Niger; ¹National Aviation University, Ukraine |
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 | 2.4.1 |
AERODYNAMIC SHAPE OPTIMIZATION OF CRM WING VIA DEEP LEARNING-ASSISTED GENETIC ALGORITHM 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 CONCEPT USING AERODYNAMIC SHAPE OPTIMIZATION P. D. Bravo-Mosquera¹, T Chau², F Catalano¹, D 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 TOWARD THE REDUCTION OF AVIATION EFFECTS ON LOCAL AIR QUALITY [..] 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 Yu-Lu Huang¹, Wei Du¹, Dao-Qin Huang¹, Jia 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 |
MACHINE LEARNING FOR AERODYNAMICS PREDICTION Rodrigo Castellanos¹, Alejandro Gorgues¹, Jaime Bowen¹, Esther Andrés¹; ¹INTA, Spain Presenter: Rodrigo Castellanos, INTA | |||
06. Sep 22 | 11:30 | 12:00 | 4.4.3 |
EFFICIENT UNCERTAINTY QUANTIFICATION VIA MULTI-FIDELITY POLYNOMIAL CHAOS-KRIGING METAMODELLING TECHNOLOGY Zhao Huan, Sun Yat-Sen University, China; Gao Zhenghong¹, Xia Lu¹; ¹Northwestern Polytechnical University, China Presenter: Huan ZHAO, SUN YAT-SEN UNIVERSITY | |||
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06. Sep 22 | 10:30 | 11:00 | 5.4.1 |
TRANSITIONAL FLOW MODELLING OF A HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER TRANSONIC TRANSPORT AIRCRAFT WING M. Jentys¹, C. Breitsamter¹; ¹Technical University of Munich, Germany | |||
06. Sep 22 | 11:00 | 11:30 | 5.4.2 |
REACTIVE CONTROL OF BYPASS TRANSITION IN A WING BOUNDARY LAYER José M. Faúndez Alarcón¹, Kenzo Sasaki¹, Ardeshir Hanifi¹, Roger Larsson, Saab Aeronautics, Sweden; Dan S. Henningson¹; ¹KTH Royal Institute of Technology, Linné FLOW Centre, Sweden | |||
06. Sep 22 | 11:30 | 12:00 | 5.4.3 |
DIRECT NUMERICAL SIMULATIONS OF THE EFFECTS OF ROTATION ON A THICK AIRFOIL T. Coelho Leite Fava¹, D. Henningson¹, A. Hanifi¹; ¹KTH, Sweden | |||
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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, P. Östlund, NewSoTech AB, Germany; 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. M. DI MAURO¹, R. M. RUSSO, Institute for Polymers, Composites and Biomaterials, C.N.R., Italy; G. M. GUIDA¹; ¹University of Naples Federico II – Department of Industrial Eng., Italy | |||
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06. Sep 22 | 10:00 | 10:30 | 8.4.1 |
TOPOLOGY OPTIMIZATION OF COMPLIANT TRAILING EDGE AIRFOIL WITH A PATH-FOLLOWING EQUILIBRIUM SOLUTION C. E. de Souza, Federal University of Santa Maria, Brazil | |||
06. Sep 22 | 10:30 | 11:00 | 8.4.2 |
MORPHING FORWARD WING SECTION SKIN DESIGN FOR A SAILPLANE CONSIDERING WING BENDING Fabian Sturm¹, Mirko Hornung¹; ¹Technical University of Munich, Germany | |||
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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 Thommie Nilsson¹, Christer 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, KTH, Royal Institute of Technology, Sweden; X. Zhao¹; ¹Chalmers University of Technology, Sweden | |||
06. Sep 22 | 11:00 | 11:30 | 10.4.2 |
A MULTIPLE MODEL ADAPTIVE ESTIMATOR FOR AIRCRAFT AERODYNAMIC PARAMETER AND THRUST DEVIATION IDENTIFICATION D. Ding, China Aerodynamics Research and Development Center, China | |||
06. Sep 22 | 11:30 | 12:00 | 10.4.3 |
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 |
PREPARATORY RESEARCH FOR UAM COLLISION AVOIDANCE USING ADSB Seokmin Ahn¹, Hyunjin Choi¹, Sungyuk Kim¹, Jaeeun Kim¹, Hyeok Ryu¹; ¹Korea Aerospace Research Institute, South Korea | |||
06. Sep 22 | 11:00 | 11:30 | 11.4.2 |
SAFE REINFORCEMENT LEARNING BASED MULTIROTOR 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 Yves Lemmens¹, Casper Teirlink¹, Anoosh Hegde¹, David Pla Guerrero¹, Gerardo Olivares², Harsh 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 Prabhat Khanal, Chalmers University of Technology, Sweden; Per Hallander¹, Ruoshan 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 Gexing Kong, China; Peng Cui, China; Wei Du, China; Rui Chen, China | |||
Reserve Paper | 12.4.R |
CALVERT AND PAPI LIGHT SYSTEM USED FOR AN AUTOMATIC APPROACH AND LANDING T. R. Rogalski, Rzeszow University of Technology,, Poland | |||||
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06. Sep 22 | 10:30 | 11:00 | 13.4.1 |
TECHNICAL CONCEPTS FOR INSPECTING UAVS FOR DAMAGE J. Eltgen¹, T. Schüppstuhl¹; ¹Hamburg University of Technology, Germany | |||
06. Sep 22 | 11:00 | 11:30 | 13.4.2 |
LOCALIZATION OF INTERROGATORS WITH A 1030/1090 MHZ SPECTRUM MONITORING SYSTEM Luciano Sarperi¹, Michael Jäger¹, Pascal Müller¹, Michael Felux¹; ¹ZHAW, Switzerland Presenter: Michael Jäger, ZHAW School of Engineering | |||
06. Sep 22 | 11:30 | 12:00 | 13.4.3 |
A FEDERATED LEARNING BASED SECURITY FOR CONTROLLER-PILOT DATA LINK COMMUNICATION Suleman Khan¹, Gurjot Singh Gaba¹, Andrei Gurtov¹; ¹Linköping University, Sweden Presenter: Suleman Khan, Linköping University |
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 |
DYNAMIC PAIRWISE WAKE VORTEX SEPARATIONS FOR ARRIVALS USING PREDICTIVE MACHINE LEARNING MODELS L Frigerio¹, I De Visscher, Wake Prediction Technologies (WaPT), Belgium; G Stempfel¹, R Barragan Montes², C Chalon Morgan²; ¹Euranova, Belgium ;²EUROCONTROL, Belgium Presenter: Lorenzo Frigerio, Euranova | |||
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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 Montella Nicolina¹, Andrea Aprovitola¹, Luigi Iuspa¹, Giuseppe Pezzella¹; ¹University of Campania , Italy | |||
06. Sep 22 | 14:30 | 15:00 | 3.5.2 |
CONCEPT DESIGN OF A LOW BOOM SSBJ TO SATISFY SOCIAL ACCEPTABILITY Shigeru Horinouchi, SuperSonic Jet Planning Inc., Japan | |||
06. Sep 22 | 15:00 | 15:30 | 3.5.3 |
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 | |||
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06. Sep 22 | 14:00 | 14:30 | 4.5.1 |
ADJOINT SENSITIVITY ANALYSIS OF TIME DEPENDENT FLOWS WITH RESPECT TO NON-GEOMETRICAL PARAMETERS T. S. Privato¹, J. S. B. Lima, IMT, Brazil; D. I. Dolci¹, M. T. Hayashy, UFABC, Brazil; B. S. Carmo¹, E. V. Volpe¹; ¹USP, Brazil Presenter: Ernani Volpe, USP | |||
06. Sep 22 | 14:30 | 15:00 | 4.5.2 |
POWER, COMPRESSION AND EFFICIENY: A BLADE PROFILE PARAMETRIC STUDY ON MULTI-STAGE AXIAL COMPRESSOR A Koksal, Turkey | |||
06. Sep 22 | 15:00 | 15:30 | 4.5.3 |
AUTOMATIC FREE-FORM DEFORMATION AS GEOMETRIC PARAMETERIZATION FOR AERDYNAMIC DESIGN Matunaga, M.A.L. Marco Aurélio Leonel Matunaga, ITA - Instituto Tecnológico de Aeronáutica, Brazil; Azevedo, J. L. F Joao Luiz Filgueiras de Azevedo, IAE - Instituto de Aeronáutica e Espaço, Brazil | |||
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06. Sep 22 | 14:00 | 14:30 | 5.5.1 |
STABILITY OF A LAMINAR BOUNDARY LAYER OVER A LOCALISED SURFACE INDENTATION E. R. Gowree, ISAE-SUPAERO, France; C. J. Atkin, University of East Anglia, United Kingdom | |||
06. Sep 22 | 14:30 | 15:00 | 5.5.2 |
DIRECT NUMERICAL SIMULATIONS OF A TURBULENT AIR INTAKE Y.-C. Xi, Tsinghua University, China | |||
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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 Rejish Jesudasan¹, Raffaello Mariani¹, Ardeshir Hanifi¹; ¹KTH Royal Institute of Technololgy, Stockholm, Sweden | |||
06. Sep 22 | 14:30 | 15:00 | 6.5.2 |
AERODYNAMIC ANALYSIS OF LOW SPEED TANDEM CHANNEL WING FOR EVTOL AIRCRAFT CONSIDERING PROPELLER-WING INTERACTION .M Chang¹, Z.Y. Zheng¹, X.X Meng¹, J.Q Bai¹, B. Wang, Chinese Academy of Sciences, China; ¹Northwestern Polytechnical University, China Presenter: Zhongyuan Zheng, Northwestern Polytechnical University | |||
06. Sep 22 | 15:00 | 15:30 | 6.5.3 |
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 | |||
Reserve Paper | 6.5.R |
AERODYNAMIC AND AEROTHERMODYNAMIC ASSESSMENT OF A LIFTING-BODY RE-ENTRY VEHICLE Andrea Aprovitola¹, Nicolina Montella¹, Luigi Iuspa¹, Giuseppe Pezzella¹, Antonio 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 |
DEFECT BASED MODELLING OF LIFE IN ELECTRON BEAM MELTED TI-6AL-4V H. Sandell, Luleå University of Technology, Sweden | |||
06. Sep 22 | 15:00 | 15:30 | 7.5.3 |
RVE-BASED HOMOGENIZATION OF ADDITIVELY MANUFACTURED POROUS METALS A. Alaimo¹, G. Mantegna¹, C. Orlando¹, D. Tumino¹, C. Vindigni¹; ¹Faculty of Engineering and Architecture Kore University of Enna, Italy | |||
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06. Sep 22 | 13:30 | 14:00 | 8.5.1 |
DESIGN AND EXPERIMENTAL TESTING OF A DROOP NOSE MORPHING FOR ADVANCED REGIONAL AIRCRAFT A. De Gaspari¹, V. Cavalieri¹, S. Ricci¹; ¹Politecnico di Milano, Italy | |||
06. Sep 22 | 14:00 | 14:30 | 8.5.2 |
STRUCTURAL ANALYSIS OF TWISTED/CURVED BEAMS USING A HYBRID METHOD A. Siami¹, F. Nitzsche¹; ¹Carleton University, Canada Presenter: Fred Nitzsche, Carleton University | |||
06. Sep 22 | 15:00 | 15:30 | 8.5.3 |
EXPERIMENTAL AND NUMERICAL ANALYSES OF A PRE-STRESSED TENSEGRITY MEMBRANE V. A. S. Paiva¹, L. H. S. Teixeira¹, J. H. Izuka¹, P. G. Ramos¹, P. R. G. Kurka¹; ¹UNICAMP, Brazil | |||
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06. Sep 22 | 14:00 | 14:30 | 9.5.1 |
MULTI-PLATFORM APP-EMBEDDED MODEL FOR HYBRID AIR-BREATHING ROCKET-CYCLE ENGINE IN HYPERSONIC ATMOSPHERIC ASCENT S. Tsentis, Greece Presenter: Spyros Tsentis, Aristotle University of Thessaloniki | |||
06. Sep 22 | 14:30 | 15:00 | 9.5.2 |
SAND EROSION MODELING IN GENERIC COMPRESSOR RIG TESTING Xija wu¹, Qi Yang¹; ¹National Research Council Canada, Canada | |||
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06. Sep 22 | 14:00 | 14:30 | 10.5.1 |
HANDLING QUALITIES OF A DISTRIBUTED PROPULSION ELECTRIC AIRCRAFT D PLANAS ANDRES, ONERA & ISAE SUPAERO, France; C DOLL, 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 | 13:30 | 14:00 | 11.5.1 |
NUMERICAL MODELLING OF PITCHING WINGS FOR GUST MITIGATION Weixing Yuan¹, Alanna Wall¹, Xiaoyang Zhang², Dominique Poirel²; ¹National Research Council (NRC) Canada, Canada ;²Royal Military College of Canada (RMC),, Canada | |||
06. Sep 22 | 14:00 | 14:30 | 11.5.2 |
UNMANNED AERIAL VEHICLE\\\\\\\'S TRAJECTORY OPTIMIZATION IN CONSTRAINED ENVIRONMENTS J. Novák ¹, P. Chudý¹; ¹Brno University of Technology, Czech Republic | |||
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06. Sep 22 | 14:00 | 14:30 | 12.5.1 |
MACHINE LEARNING IN SHIP MOTION PREDICTION AND UAV RECOVERY J Lakkis¹, B Cees¹; ¹RMIT University, Australia | |||
06. Sep 22 | 14:30 | 15:00 | 12.5.2 |
AIRCRAFT FUEL LEVEL GAUGE MECHANISMS: A HIGH PRECISION FUEL SYSTEM IN ACROBAT-CRAFTS M. A. D. Di Marzo, University of São Paulo, Brazil | |||
06. Sep 22 | 15:00 | 15:30 | 12.5.3 |
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 | |||
Reserve Paper | 12.5.R |
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 Chad Beamer, Quintus Technologyes LLC, United States; Anders Magnusson, Quintus 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 C Jochims Lau¹, A. G. Slongo¹, T. V. Bins¹, G. L. de Oliveirra¹; 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 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 |
A MODEL VALIDATION HIERARCHY FOR CONNECTING SYSTEM DESIGN TO MODELING AND SIMULATION CAPABILITIES 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. 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 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) Donn 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 |
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 Daniel Kloock-Schreiber¹, Majed Swaid², Volker Gollnick¹, Alexander Fay, HSU, Institute of Automation Technology, Germany; Malte 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 |
COMPUTATIONAL INVESTIGATION ON AERODYNAMIC CHARACTERISTICS OF COAXIAL ROTORS FOR EVTOL AIRCRAFT Z. Xu, Northwestern Polytechnical University, China; M. Chang¹, J. Bai¹, M. Dai, China North Industries Corporation (NORINCO), Germany; ¹Unmanned System Research Institute, Northwestern Polytechnical, China | |||
06. Sep 22 | 17:30 | 18:00 | 3.6.4 |
MIXED INTEGER NONLINEAR PROGRAMMING FOR EVTOL AIRCRAFT DESIGN AND OPTIMIZATION Tianhong Jiang¹, Mingkang Li¹, Yaolong Liu¹, Yao Zheng¹; ¹School of Aeronautics and Astronautics, Zhejiang University, China Presenter: Tianhong Jiang | |||
Reserve Paper | 3.6.R |
RESEARCH ON THE DESIGN OF UNMANNED AERIAL VERICLE FOR MINE INSPECTION Zhan-Ke Li¹, Shi-Gao Su, Aerospace Times Feihong Technology Co., Ltd. , China; Zhi-Yu Li¹, Fu-Rong Li¹, Gao 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 Tony Di Fabbio¹, Eike Tangermann¹, Markus 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 | |||
Reserve Paper | 4.6.R |
HEAT TRANSFER MODULATION BY SUSPENDED PARTICLES IN A SHEARLESS MIXING LAYER Hamid Reza Zandi Pour¹, Michele Iovieno¹; ¹Politecnico di Torino, Italy | |||||
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06. Sep 22 | 16:00 | 16:30 | 5.6.1 |
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 | 16:30 | 17:00 | 5.6.2 |
EXPERIMENTAL EVALUATION OF A PASSIVE FLOW-CONTROL DEVICE FOR A TILT-ROTOR AIRCRAFT A R Proenca¹, S P Prince¹, Lynton Banks-Davies¹, K P Garry¹; ¹Cranfield University, United Kingdom | |||
06. Sep 22 | 17:00 | 17:30 | 5.6.3 |
STUDY ON FLOW AND HEAT TRANSFER CHARACTERISTICS OF SUPERCRITICAL RP-3 KEROSENE IN AN INCLINED RECTANGULAR CHANNEL J.-J. Yu, Chonqqing University, China | |||
06. Sep 22 | 17:30 | 18:00 | 5.6.4 |
RESEARCH ON PRESSURE LOAD OF AN EMBEDDED JET NOZZLE Hongyang Li¹, Xiao Wang¹, Dongsheng Yu¹, Fangliang Liu¹; ¹Shenyang Aircraft Design and Research Institute, China | |||
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06. Sep 22 | 16:00 | 16:30 | 6.6.1 |
WIND TUNNEL TESTS RESULTS AND PERFORMANCE OF THE MOTHIF BLOWN FLAP P. D'Alesio¹, G. Travostino¹, P. Planquart², G. Glabeke²; ¹Piaggio Aerospace, Italy ;²von Karman Institute, Belgium | |||
06. Sep 22 | 16:30 | 17:00 | 6.6.2 |
A STUDY OF HIGH-LIFT DEVICES FOR LOW REYNOLDS NUMBER APPLICATIONS Y. Leng¹, K. Fayez, DELAIR, France; J.-M. Moschetta¹, M. Bronz, ENAC, France; ¹ISAE-SUPAÉRO, France | |||
06. Sep 22 | 17:00 | 17:30 | 6.6.3 |
COMPLETION OF AN EXISTING FAST TURN-AROUND SLAT NOISE PREDICTION MODEL BASED ON STATISTICAL ANALYSIS Jose Manuel Rendón-Arredondo¹, Laura Botero-Bolívar², Alejandro Marulanda-Tobon¹, Henry Laniado¹, Leandro de Santana²; ¹Universidad EAFIT, Colombia ;²University of Twente, Netherlands | |||
06. Sep 22 | 17:30 | 18:00 | 6.6.4 |
MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF 2D HIGH-LIFT DEVICE BASED ON DISTRIBUTED DEEP REINFORCEMENT LEARNING J.-H. Dai¹, P.-Q. Liu¹, L. Li¹; ¹Beihang University, China | |||
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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 UTILIZING 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 EPOXY RESINS G.C Cristea¹, A. Stefan¹, K.K Krawczyk, Joanneum Research, Austria; C.-E Pelin¹, S. Ilina¹; ¹INCAS, Romania | |||
Reserve Paper | 7.6.R |
DOPAMINE COATED UHMWPE HYDROGEN-RICH / BENZOXAZINE COMPOSITES FOR SPACE RADIATION SHIELDING J.H Cha¹, C.G Kim¹; ¹KAIST, South Korea | |||||
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 |
TRANSIENT RELEASE AND LATERAL GUST BEHAVIOUR OF AIRCRAFT INCORPORATING THE SEMI AEROELASTIC HINGE 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 COUPLE SYSTEMS: A WING AERO-STRUCTURAL DESIGN PERSPECTIVE X. Chen¹, A. Riaz¹, M. D. Guenov¹; ¹Cranfield University, United Kingdom | |||
Reserve Paper (interactive) | 8.6.R |
DEVELOPMENT OF NOVEL ANALYTICAL METHOD FOR TIME DOMAIN AEROELASTIC ANALYSIS OF HIGH ASPECT RATIO WING USING UNSTEADY IND Zia Ur Rehman Rehman, Pakistan | |||||
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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 Isak Jonsson¹, Robert Ranman¹, Xisto Carlos ¹, Tomas Grönstedt¹; ¹Chalmers Tekniska Hogskola AB, Sweden | |||
Reserve Paper | 9.6.R |
MULTIPOINT AERODYNAMIC DESIGN OF A SHORT NACELLE FOR AN ELECTRIC FAN V. T Silva¹, M. Lejon ², A. Lundbladh², C. Xisto¹, A. Venkatesh ¹; 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.P. 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 Renan Pereira, ITA, Brazil; Pedro González¹, Flávio Silvestre¹; ¹TU Berlin, Germany | |||
06. Sep 22 | 17:00 | 17:30 | 10.6.3 |
LQR BASED DIGITAL AUTOPILOT FOR LIGHT SPORT AIRCRAFT Jan Vlk¹, Peter Chudy¹, Milan 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.P. 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 Kranthi Kumar Deveerasetty¹, Koichi OKA¹, Akinori 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 | |||
06. Sep 22 | 17:30 | 18:00 | 11.6.4 |
FLIGHT VERIFICATION OF AUTOMATIC TRANSITION FOR QUAD TILT WING SMALL UAV Koji Muraoka¹, Masayuki 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 Ilan Berlowitz, IBAero Engineering, Israel | |||
06. Sep 22 | 16:30 | 17:00 | 12.6.2 |
AN INTEGRATED CONTROL SCHEME FOR STARTER/GENERATOR SYSTEM IN MORE ELECTRIC AIRCRAFT Hong Li, China; Zhengda Zhao, China; Zaihong Wan, China; Long Xu, China; Shuangxin Zhao, China; Pengyu Sun, China | |||
06. Sep 22 | 17:00 | 17:30 | 12.6.3 |
THE INFLUENCE OF THE MODEL PARAMETERS OF LIION BATTERIES ON THE WIRING HARNESS PERFORMANCE OF EVTOL AIRCRAFT S. Oberschwendtner¹, M. Hornung¹; ¹Technical University of Munich, Germany | |||
06. Sep 22 | 17:30 | 18:00 | 12.6.4 |
ANALYSIS AND DEVELOPMENT OF INTEGRATED LOW-PRESSURE SHAFT GENERATOR Magnus Genrup, Lund University, Sweden; Richard Avellán¹, Hans Mårtensson¹; ¹GKN Aerospace, Sweden | |||
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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 CONCURRENTLY COUPLING AIRCRAFT DESING, MANUFACTURING AND SUPPLY CHAIN Giuseppa Donelli¹, João Mello², Felipe Odaguil², Thierry Lefebvre³, Nathalie Bartoli³, Ton van der Laan, GKN Fokker, Netherlands; Luca Boggero¹, Björn Nagel¹; ¹DLR, Germany ;²Embraer, Brazil ;³ONERA, France | |||
06. Sep 22 | 17:00 | 17:30 | 13.6.3 |
CONTRASTING YOLOV5 AND A CNN MODEL IN IDENTIFYING USER ACTION IN COMPUTER-AIDED MANUFACTURING IN REAL-TIME B. W. 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 Chen Lin¹, Li Xiaohua¹, Zhang Zhengxin¹, Huang Wei¹, Wu RenZhong¹, Li Yan¹; ¹AVIC Chengdu Aircraft Industrial (Group) Co., Ltd., China | |||
Reserve Paper | 13.6.R |
RESEARCH ON COMMUNICATION AND DATA ACQUISITION TECHNOLOGY OF AVIATION SPECIAL EQUIPMENT LH.-Z. Zhong, Chengdu Aircraft Company, China | |||||
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06. Sep 22 | 16:00 | 16:30 | 14.6.1 |
INTEGRATED INTEGRATED SUAS 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 | 16:30 | 17:00 | 14.6.2 |
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 | 17:00 | 17:30 | 14.6.3 |
DLR DESIGN CHALLENGE 2022 ON ADVANCED AERIAL FIREFIGHTING SYSTEMS OF SYSTEMS T. Dietl¹, P. Ratei¹, P. Shiva Prakasha¹, T. Zill¹, B. Nagel¹; ¹German 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 |
Wednesday, 07. Sep 2022
10:00 - 10:30 | Coffee Break |
0.6 | GL 3 Panel session “Towards Sustainable Air Transport” Chair: J.L. Azevedo, ICAS President Brazil, R.Parker, former ISABE President UK | |||
07. Sep 22 | 08:00 | 10:00 |
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07. Sep 22 | 10:30 | 11:00 | 1.7.1 |
TECHNOLOGIES ENABLING EMISSIONS-REDUCING AIRCRAFT AND FUTURE EMISSIONS-FREE AIRCRAFT DESIGNS C.-A. Hoover, Wright Electric, Inc., United States | |||
07. Sep 22 | 11:00 | 11:30 | 1.7.2 |
REGIONAL AIR MOBILITY MARKET STUDY C Y JUSTIN¹, D Mavris¹; ¹Georgia Institute of Technology, United States | |||
07. Sep 22 | 11:30 | 12:00 | 1.7.3 |
ICAS SUBSONIC SINGLE AFT ENGINE (SUSAN) TRANSPORT AIRCRAFT CONCEPT AND TRADE SPACE EXPLORATION OVERVIEW R. H. Jansen, NASA Glenn Research Center, United States | |||
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07. Sep 22 | 10:30 | 11:00 | 2.7.1 |
ZONAL MODEL BASED AIRCRAFT PASSENGER THERMAL COMFORT COMPARATIVE STUDY S. Tarroc Gil¹, J. Schminder¹, A. Guerrero i Almirall, UptimAI, Czech Republic; J. I. Tarraga Prieto, MAHLE Electronics S.L.U, Slovenia; R. Vaz Linn, Federal University of Rio Grande do Sul, Brazil; ¹Linköping University, Sweden | |||
07. Sep 22 | 11:00 | 11:30 | 2.7.2 |
AURALIZATION OF NOISE IN A VIRTUAL REALITY AIRCRAFT CABIN FOR PASSENGER WELL-BEING USING HUMAN-CENTRED APPROACH. S. Santhosh¹, M.C. Moruzzi¹, F. De Crescenzio¹, S. Bagassi¹; ¹University of Bologna, Italy | |||
07. Sep 22 | 11:30 | 12:00 | 2.7.3 |
AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM AIR QUALITY ENHANCEMENT I. Berlowitz, IBAero Engineering, Israel | |||
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07. Sep 22 | 10:30 | 11:00 | 3.7.1 |
COMPARING SERIES AND PARALLEL HYBRID-ELECTRIC PROPULSION SYSTEMS ON AIRCRAFT PERFORMANCE A Batra¹, R.C. Camilleri¹, Reiko Raute, Dept. Ind. Elec. Power Conv., University of Malta, Malta; ¹Institute of Aerospace Technologies (IAT), University of Malta , Malta | |||
07. Sep 22 | 11:00 | 11:30 | 3.7.2 |
DEVELOPMENT OF A HYDROGEN-POWERED FUSELAGE-MOUNTED BLI PROPULSOR ADD-ON FOR PASSENGER AIRCRAFT Alexander Heidbrecht¹, Maurice Hoogreef¹, Klaas Burger¹, Roelof Vos¹, Arvind Gangoli Rao¹; ¹TU Delft, Netherlands | |||
07. Sep 22 | 11:30 | 12:00 | 3.7.3 |
TECHNOLOGY ROADMAP AND CONCEPTUAL DESIGN OF HYBRID AND ELECTRIC CONFIGURATIONS IN THE COMMUTER CLASS F. Nicolosi¹, V. Marciello¹, V. Cusati¹, F. Orefice¹; ¹University of Naples Federico II, Italy Presenter: Fabrizio Nicolosi, University of Naples Federico II | |||
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07. Sep 22 | 10:30 | 11:00 | 5.7.1 |
USING ACTIVE FLOW CONTROL TO IMPROVE THE AERODYNAMIC EFFICIENCY OF THE NEXT GENERATION CIVIL TILT ROTOR AIRCRAFT J.B. Vos¹, A. Gehri¹, H Truong², A. Marouf², Y. Hoarau²; ¹CFS Engineering, Switzerland ;²University of Strasbourg, ICUBE Research Institute, France | |||
07. Sep 22 | 11:00 | 11:30 | 5.7.2 |
ON THE AERODYNAMIC ANALYSIS OF A MODERN ALL-ELECTRIC POWERED CE-LINER AIRCRAFT Tung Wan¹, H.L. Zhan¹; ¹Tamkang University, Taiwan, China | |||
07. Sep 22 | 11:30 | 12:00 | 5.7.3 |
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) | 5.7.R |
NUMERICAL SIMULATION OF MISSILE AIR-LAUNCHED DYNAMIC PROCESS UNDER DOWNWASH FLOW OF HELICOPTER ROTOR Wang-Yi Zhou¹, Guo-Qiang Yang¹, Xiang Gao¹, Xue-Yao Zhu¹, Bo-Xiao Zhou¹; ¹AVIC Xi’an Flight Automatic Control Research Institute, China | |||||
Reserve Paper (interactive) | 5.7.R |
RESEARCH ON THE INFLUENCE OF FLIGHT ATTITUDE ON UNILATERAL MISSILE SEPARATION FROM EMBEDDED BAY Zhou Wei, China | |||||
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07. Sep 22 | 10:30 | 11:00 | 6.7.1 |
A NUMERICAL MODEL OF THE DYNAMIC RESPONSE OF THE PRESSURE-SENSITIVE PAINTS S.-J. Song, China | |||
Reserve Paper (interactive) | 6.7.R |
EXPERIMENTAL INVESTIGATION ON JET IMPINGEMENT HEAT TRANSFER WITH CROSS FLOW FOR AERO-ENGINE INLET CONE Xinwei Jiang¹, Guochao Liu¹, Jianjun Zhou¹, Qi Jia¹; ¹AECC Shenyang Engine Research Institute, China | |||||
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07. Sep 22 | 10:30 | 11:00 | 7.7.1 |
A GLOBAL/LOCAL ELEMENT-WISE APPROACH FOR THE BUCKLING AND POST-BUCKLING ANALYSIS OF THIN MULTILAYERED STRUCTURES R. Augello¹, E. Carrera¹, A. Pagani¹, M. Petrolo¹; ¹Politecnico di Torino, Italy | |||
07. Sep 22 | 11:00 | 11:30 | 7.7.2 |
OPTIMAL DESIGN OF STIFFENED PANELS: CAD BASED PARAMETERIZATION WITH SIMULTANEOUS LAYOUT AND SIZING OPTIMIZATION Hammad Rahman¹, Roeland De Breuker¹, Saullo Castro¹; ¹Delft University of Technology, Netherlands | |||
07. Sep 22 | 11:30 | 12:00 | 7.7.3 |
INVESTIGATION OF BUCKLING RESPONSE OF CYLINDRICAL SHELLS USING 3D-PRINTING TECHNOLOGY C. Bisagni¹, E. Labans¹; ¹Delft University of Technology, Netherlands | |||
Reserve Paper | 7.7.R |
ADHESIVELY- BONDED SINGLE LAP JOINTS SUBJECTED TO PROJECTILES WITH HIGH VELOCITIES F Kadioglu, Ankara Y?ld?r?m Beyaz?t Üniversitesi, Turkey | |||||
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07. Sep 22 | 10:30 | 11:00 | 8.7.1 |
LINEAR AND GEOMETRICALLY NONLINEAR STRUCTURAL SHAPE SENSING FROM STRAIN DATA USING BASIS FUNCTION METHOD C.-G. Pak, NASA Armstrong Flight Research Center, United States | |||
07. Sep 22 | 11:00 | 11:30 | 8.7.2 |
PARAMETER IDENTIFICATION BY UPDATING THE STRUCTURAL MODEL OF A UAV WITH FLEXIBLE WING T. R. De Paula¹, V. P. Fernandes¹, A. G. P. Sarmento¹, D. F. C. Zuñiga¹, A. G. Souza, Universidade de Lisboa, Portugal; R. G. A. Silva¹, L. C. S. Góes¹; ¹Aeronautics Institute of Technology, Brazil Presenter: Luiz Góes, Aeronautics Institute of Technology | |||
07. Sep 22 | 11:30 | 12:00 | 8.7.3 |
NUMERICAL VALIDATION OF CURVED DISPLACEMENT TRANSFER FUNCTIONS FOR LARGE DEFORMATION STRUCTURE SHAPE PREDICTIONS S.-F. Lung, Peerless Technologies, United States; W.-L. Ko¹, V.-T. Fleischer¹; ¹NASA AFRC, United States | |||
Reserve Paper | 8.7.R |
RESEARCH ON THE EFFECT OF SHOT PEENING AND STRENGTHENING PROCESS ON FATIGUE STRENGTH OF HIGH STRENGTH ALUMINUM ALLOY G-W Li¹, T-H Luo¹, H-Y Hang¹; ¹Northwestern Polytechnical University, China | |||||
Reserve Paper (interactive) | 8.7.R |
BENDING-TORSION FLUTTER OF TAPERED COMPOSITE FINS: ANALYSIS AND EXPERIMENT B. Rasuo, University of Belgrade, Faculty of Mechanical Engineering, Serbia | |||||
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07. Sep 22 | 10:30 | 11:00 | 9.7.1 |
FEASIBILITY STUDY OF SHORT SUBSONIC DIFFUSR CONCEPT FOR SUPERSONIC INLET J. Akatsuka¹, I. Kikura, Tokyo Unicersity of Agriculture and Technology, Japan; Y. Watanabe¹; ¹JAXA, Japan | |||
07. Sep 22 | 11:00 | 11:30 | 9.7.2 |
A STUDY ON THE DEVELOPMENT OF THE FLOW DISTORTION DOWNSTREAM OF AN S-DUCT INTAKE M. Migliorini¹, P. K. Zachos¹, D. G. MacManus¹, V. Monnier¹; ¹Cranfield University, United Kingdom | |||
07. Sep 22 | 11:30 | 12:00 | 9.7.3 |
IMPACT OF AZIMUTHAL FLOW DISTORTION ON THE ACOUSTICPROPAGATION IN A 3D WAVEGUIDE B. Mangin¹, M. Daroukh¹, G. Gabard, LAUM, France; ¹ONERA, France | |||
Reserve Paper (interactive) | 9.7.R |
NUMERICAL SIMULATION ANALYSIS OF INFRARED RADIATION AND ELECTROMAGNETIC SCATTERING CHARACTERISTICS OF DIFFERENT MIXERS Wang Rui¹, Yang Qingzhen ¹, Zhang Saile¹, Du Kai, Guiyang Aero-engine Research Institute, China; ¹Northwestern Polytechnical University, China | |||||
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07. Sep 22 | 10:30 | 11:00 | 10.7.1 |
META-REINFORCEMENT LEARNING-BASED FAULT TOLERANT CONTROL FOR A QUADROTOR WITH A SEVERE LOSS OF ROTOR Yeontaek Jung¹, Youdan Kim¹; ¹Seoul National University, South Korea | |||
07. Sep 22 | 11:00 | 11:30 | 10.7.2 |
CONDITIONS OF FLIGHT OF WINGMAN AIRCRAFT IN TIGHT FORMATION FLIGHT FOR FUEL SAVING Daniel Barbuto Rossato, Faculdade de Tecnologia SENAI , Brazil; Karl Heinz Kienitz, Instituto Tecnológico de Aeronáutica, Brazil | |||
07. Sep 22 | 11:30 | 12:00 | 10.7.3 |
DESIGN OF STABILITY AUGMENTATION SYSTEMS FOR A FLEXIBLE AIRCRAFT USING LQ OUTPUT-FEEDBACK CONTROL VIA LMI Renan Pereira, ITA, Brazil; Pedro González¹, Flávio Silvestre¹; ¹TU Berlin, Germany | |||
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07. Sep 22 | 10:30 | 11:00 | 11.7.1 |
THE SIMULATION FOR PASSENGERS’ DIGITAL DOOR- TO-DOOR AIR TRAVEL IN THE LONG-DISTANCE TRIP J. La¹, C. Bil¹, I. Heiets¹, K.-A. Lau, Qatar Airways, Qatar; ¹RMIT University, Australia Presenter: Cees Bil, RMIT University | |||
07. Sep 22 | 11:00 | 11:30 | 11.7.2 |
ENVIRONMENTAL AGENT-BASED MODELLING FOR A FIREFIGHTING SYSTEM OF SYSTEMS Jorge Lovaco¹, Ingo Staack¹, Petter Krus¹; ¹Linköpings Universitet, Sweden | |||
07. Sep 22 | 11:30 | 12:00 | 11.7.3 |
REQUIREMENTS-BASED GENERATION OF OPTIMAL VERTICAL TAKEOFF AND LANDING TRAJECTORIES FOR ELECTRIC AIRCRAFT C. Krammer, Germany; F. Schweighofer, Germany; D. Gierszewski, Germany; S. Scherer, Germany; T. Akman, Germany; H. Hong, Germany; F. Holzapfel, Germany | |||
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07. Sep 22 | 10:30 | 11:00 | 12.7.1 |
UK-AEROSPACE RESEARCH CONSORTIUM - EXPANDING THE VALUE OF UK ACADEMIC RESEARCH R M Gardner, UK-Aerospace Research Consortium, United Kingdom | |||
07. Sep 22 | 11:00 | 11:30 | 12.7.2 |
MAXIMISING VALUE FROM UK ACADEMIC RESEARCH - THE UK-AEROSPACE RESEARCH CONSORTIUM THEME APPROACH R M Gardner, UK-Aerospace Research Consortium, United Kingdom | |||
07. Sep 22 | 11:30 | 12:00 | 12.7.3 |
THE BENEFIT OF BILATERAL RESEARCH NETWORKS - SARC AND BARINET AND THE BRAZILIAN SWEDISH COLLABORATION IN AERONAUTICS E. Villani, Aeronautics Institute of Technology (ITA), Brazil; P. Krus, Linköping University, Sweden; V. J. de Negri, Federal University of Santa Catarina (UFSC), Brazil; L. Pereira, Federal University of ABC (UFABC), Brazil; G. Caurin, University of São Paulo (USP), Brazil | |||
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07. Sep 22 | 10:30 | 11:00 | 13.7.1 |
OPTIMIZATION OF THE INDUCTION WELDING PROCESS THROUGH THE INTEGRATION OF A THERMAL CAMERA G. B. Buccoliero, CETMA, Italy | |||
07. Sep 22 | 11:00 | 11:30 | 13.7.2 |
TEMPERATURE ANALYSIS AND PREDICTION OF ASSEMBLY TOOLING OF LARGE AIRCRAFT BASED OPTIMIZED BP NEURAL NETWORK R.-L. Liu, China | |||
07. Sep 22 | 11:30 | 12:00 | 13.7.3 |
MOTION STROKE DESIGN ON FLEXIBLE ASSEMBLY TOOLING FOR MULTIPLE AIRCRAFT COMPONENTS Feiyan Guo¹, Changjie Song¹, Xuerui Zhang², Qingdong Xiao²; ¹University of Science and Technology Beijing, China ;²AVIC Manufacturing Technology Institute, China | |||
Reserve Paper | 13.7.R |
RIVETING-INDUCED DEFORMATIONS ON AIRCRAFT STRUCTURES UNDER MATERIAL ANISOTROPY EFFECT J. A. N. Figueira, ITA -Aeronautics Institute of Technology, Brazil | |||||
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07. Sep 22 | 10:30 | 11:00 | 14.7.1 |
NON-INTRUSIVE AEROTHERMAL CHARACTERIZATION OF SURFACE HEAT EXCHANGERS FOR TURBOFAN AEROENGINES A. Broatch¹, J. García-Tíscar¹, A. Felgueroso¹, M. Gelain², A. Couilleaux²; ¹Universitat Politecnica de Valencia, Spain ;²Safran Aircraft Engines, France | |||
07. Sep 22 | 11:00 | 11:30 | 14.7.2 |
ZONAL MODEL VALIDATION FOR AN ENVIRONMENTALLY FRIENDLY AIRCRAFT CARGO FIRE PROTECTION SYSTEM WITH CONTAINERIZED LOAD A. Pathak¹, M. Pschirer¹, M. Kienberger¹, V. Norrefeldt¹; ¹Fraunhofer IBP, Germany | |||
Reserve Paper | 14.7.R |
ELECTROMAGNETIC COMPATIBILITY PREDICATION METHOD BASED ON THE HARDWARE IN THE LOOP SIMULATION FOR AIRCRAFT RF UNITS Y.-L. Long, University of Electronic Science and Technology of China, China | |||||
Reserve Paper (interactive) | 14.7.R |
STUDY ON OIL-GAS TWO-PHASE FLOW CHARACTERISTICS IN AIR-OIL HEAT EXCHANGER Pang Xiaodong¹, SUI Hongren¹, Jiang Xinwei¹, Liu Guochao¹; ¹AECC, China |
12:00 - 13:00 | Lunch Break |
0.7 | “Developing and Flying the Gripen E” Marcus Wandt, Sweden Chair: G. Holmberg ICAS Treasurer | |||
07. Sep 22 | 13:00 | 13:45 |
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07. Sep 22 | 13:55 | 14:25 | 1.8.1 |
ICAS DIGITAL PIONEERING INITIATIVE B Nagel, DLR, Germany | |||
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07. Sep 22 | 13:55 | 14:25 | 2.8.1 |
INSTALLATION PENALTY OF AERO-ENGINES ON NARROW BODY AIRCRAFT T.E. Boogaart¹, M.F.M. Hoogreef¹, A. Gangoli Rao¹; ¹Delft University of Technology, Netherlands | |||
07. Sep 22 | 14:25 | 14:55 | 2.8.2 |
A MAINTAINABILITY PREDICTION AND OPTIMIZATION FRAMEWORK FOR MULTI COMPONENT SYSTEMS IN PRELIMINARY AIRCRAFT DESIGN STAGE P. Hansmann, Institute of Aerospace Systems, RWTH Aachen University, Germany | |||
07. Sep 22 | 14:55 | 15:25 | 2.8.3 |
A CREDIBILITY-BASED CRITERION FOR THE ASSESSMENT OF FUTURISTIC AIRCRAFT CONCEPTS NFM Wahler¹, L Radomsky¹, LV Hanisch¹, R Mallwitz¹, M Henke¹, A Elham, University of Southampton, United Kingdom; ¹TU Braunschweig, Germany | |||
07. Sep 22 | 15:25 | 15:55 | 2.8.4 |
FAST-OAD-GA: AN OPEN-SOURCE EXTENSION FOR OVERALL AIRCRAFT DESIGN OF GENERAL AVIATION AIRCRAFT F Lutz¹, J Jézégou¹, A Reysset, INSA Toulouse, France; A Busteros-Ramos¹, V Pommier-Budinger¹; ¹ISAE-SUPAERO, France | |||
Reserve Paper | 2.8.R |
CONCEPTUAL DESIGN OF FUTURE MILITARY AIR SYSTEMS - AN EDUCATIONAL APPROACH V. Gollnick¹, B. Muth, TU Braunschweig, Germany; Th. Weber¹, K. Scheibe, HAW Hamburg, Germany; M. Grünewald, FH Aachen, Germany; E. Aydin¹; ¹TU Hamburg, Germany | |||||
Reserve Paper | 2.8.R |
NUMERICAL MODELING OF FLUID-STRUCTURE INTERACTION OF A 3D WEDGE DURING WATER IMPACT WITH VARIATION OF VELOCITY AND PITC F. Valpiani¹, P. Cicolini¹, D. Esposto¹, A. Galletti¹, Davide Guagliardo¹; ¹Politecnico di Torino, Italy | |||||
Reserve Paper | 2.8.R |
THE USE OF COMPUTATIONAL FLUID DYNAMICS METHODS IN THE PRELIMINARY DESIGN OF A NEW GENERATION LIGHT COMBAT AIRPLANE L. Kiszkowiak¹, A. Olejnik¹, A. Dziubinski, Lukasiewicz Research Network – Institute of Aviation, Poland; ¹Military University of Technology, Poland | |||||
Reserve Paper | 2.8.R |
METHODOLOGY AND EXAMPLE OF CONCEPTUAL DESIGN FOR A FOOT-LAUNCHABLE SPORT SAILPLANE L. M. F. Barbosa, Heart Aerospace, Sweden | |||||
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07. Sep 22 | 13:25 | 13:55 | 3.8.1 |
A SCALABLE HYDROGEN PROPULSION SYSTEM FOR CIVIL TRANSPORT AIRCRAFT A.S.J. van Heerden¹, S. Sasi¹, R. Ghelani¹, D. Sanders¹, I. Roumeliotis¹; ¹Cranfield University, United Kingdom | |||
07. Sep 22 | 13:55 | 14:25 | 3.8.2 |
MODULARIZED HYBRID ELECTRIC PROPULSION SYSTEM ARCHITECTURE MODELING AND EVALUATION Mahmoud Fouda¹, Eytan J. Adler², Jasper H. Bussemaker¹, Joaquim R.R.A. Martins², D.F. Kurtulus, Middle East Technical University, Turkey; Luca Boggero¹, Björn Nagel¹; ¹DLR, Germany ;²University of Michigan, United States | |||
07. Sep 22 | 14:25 | 14:55 | 3.8.3 |
DESIGN AND PERFORMANCE OF LIQUID HYDROGEN FUELLED AIRCRAFT FOR YEAR 2050 EIS Carlos Xisto, Chalmers University of Technology, Sweden; Anders Lundbladh, GKN Aerospace AB, Sweden Presenter: Anders Lundbladh , GKN Aerospace | |||
07. Sep 22 | 15:25 | 15:55 | 3.8.4 |
NUMERICAL INVESTIGATION ON THE AERO-PROPULSION EFFECT OF DISTRIBUTED PROPULSION FOR S/VTOL APPLICATION Sichen Song¹, Shuanghou Deng¹, Qingxi Li, AVIC General Aircraft Research Institute, China; Hongyu Qiao¹, Yujin Lu¹; ¹Nanjing University of Aeronautics and Astronautics, China | |||
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07. Sep 22 | 13:55 | 14:25 | 4.8.1 |
DATA-DRIVEN ADAPTATION AND OPTIMIZATION OF HIGH-ORDER TURBULENT FLOW SIMULATIONS K.J. Fidkowski, University of Michigan, United States | |||
07. Sep 22 | 14:25 | 14:55 | 4.8.2 |
ASSESSMENT OF HIGH-ORDER SHOCK-CAPTURING SCHEMES FOR IMPLICIT LARGE EDDY SIMULATION H.J. Kook, South Korea | |||
07. Sep 22 | 14:55 | 15:25 | 4.8.3 |
HIGH-ORDER ACCURATE EMBEDDED-BOUNDARY DISCONTINUOUS GALERKIN METHODS FOR INVISCID GAS DYNAMICS V Gulizzi, University of Palermo, Italy Presenter: Vincenzo Gulizzi, University of Palermo | |||
07. Sep 22 | 15:25 | 15:55 | 4.8.4 |
HIGHLY ACCURATE NUMERICAL SIMULATION FOR VORTEX FLOW OVER SLENDER MISSILE AT HIGH ANGLE OF ATTACK W.P. Song¹, S.Q. Han¹, K. Lu¹, Y. Wang¹, Z.H. Han¹, B. Wu, Shanghai Electro-mechanical Engineering Institute, China; ¹Northwestern Polytechnical University, China | |||
Reserve Paper | 4.8.R |
A COMPUTATIONAL STUDY ON BLADE-VORTEX INTERACTION FOR COAXIAL ROTORS IN HOVER USING A NOVEL HIGH-ORDER SCHEME Shao-Qiang Han, Sichuan University, China; Wen-Ping Song¹, Zhong-Hua Han¹; ¹Northwestern Polytechnical University, China Presenter: Shao-Qiang Han, Sichuan University | |||||
Reserve Paper (interactive) | 4.8.R |
VISCOUS CORRECTION FOR HIGH ORDER IMMERSED INTERFACE INTERFACE METHOD FOR COMPRESSIBLE TRANSONIC FLOW L.-V. Velandia, Brazil | |||||
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07. Sep 22 | 13:55 | 14:25 | 5.8.1 |
PREDICTING STEADY LIFT AND DRAG COEFFICIENT OF TANDEM AIRCRAFT USING PRANDTL’S EXTENDED LIFTING-LINE THEORY R JAN¹, J-M MOSCHETTA¹, J-P CONDOMINES, ENAC, France; ¹ISAE-SUPAERO, France | |||
07. Sep 22 | 14:25 | 14:55 | 5.8.2 |
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 | |||
07. Sep 22 | 14:55 | 15:25 | 5.8.3 |
COMPARING POTENTIAL FLOW SOLVERS FOR AERODYNAMIC CHARACTERISTICS ESTIMATION OF THE T-FLEX UAV Fanglin Yu¹, Julius Bartasevicius¹, Mirko Hornung¹; ¹Technical University of Munich, Germany | |||
07. Sep 22 | 15:25 | 15:55 | 5.8.4 |
INVESTIGATION AERODYNAMICS FLAPPING FLIGHT ROBOTIC BIRD Harry Hoeijmakers¹, Luuk Groot Koerkamp¹, Leandro de Santana¹, Cees Venner¹, Stefano Stramigioli¹, Joost Mulder¹, Antoni Brentjes¹, Frank Gijsman¹, Steven Hartman¹; ¹University of Twente, Netherlands | |||
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07. Sep 22 | 13:55 | 14:25 | 6.8.1 |
AERODYNAMIC AND AEROACOUSTIC CHARACTERISTICS OF A NACA 0008 AIRFOIL F.L. dos Santos¹, L. Botero-Bolivar¹, C.H. Venner¹, L.D. de Santana¹; ¹University of Twente, Netherlands | |||
07. Sep 22 | 14:25 | 14:55 | 6.8.2 |
EXPERIMENTAL STUDIES ON THE INTERACTION BETWEEN PROPELLERS AND WING G. P. G. Silva¹, M. V. R. J. Silva¹, J. P. Eguea¹, F. M. Catalano¹; ¹Department of Aeronautical Engineering, University of Sao Paulo, Brazil | |||
07. Sep 22 | 14:55 | 15:25 | 6.8.3 |
IDENTIFICATION OF CRITICAL ACOUSTIC MODES FOR AN OPEN BOX CAVITY WITH ADJUSTABLE DEPTH Steffen Hammer¹, Jens Fridh¹, Mattias Billson, GKN Aerospace Sweden, Sweden; ¹KTH Royal Institute of Technology, Sweden | |||
07. Sep 22 | 15:25 | 15:55 | 6.8.4 |
AN OVERVIEW OF AERO-ACOUSTIC EXPERIMENTAL TECHNOLOGY IN AVIC FL-10 WIND TUNNEL Z. Guocheng¹, B. Anyu ¹, C. Bao¹, L. Xiangnan¹; ¹AVIC ARI, China Presenter: BAO Anyu, AVIC ARI | |||
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07. Sep 22 | 13:55 | 14:25 | 7.8.1 |
ADAPTIVE PATH PLANNING FOR SPRAYING UAS IN VINEYARD UNDER VARIABLE WIND CONDITION L. Scagnellato¹, M. Lecce¹, Nicoletta Bloise¹, M. Carreño Ruiz¹, E. Capello¹, G. Guglieri¹; ¹Politecnico di Torino, Italy Presenter: Nicoletta Bloise, Politecnico di Torino | |||
07. Sep 22 | 14:25 | 14:55 | 7.8.2 |
DESIGN OF AN EFFICIENT CLIMBING FLIGHT TRAJECTORY FOR A FLAPPING-WING MICRO AIR VEHICLE S.-G. Lee¹, H.-H. Yang¹, Y.-J. Han¹, J.-H. Han¹; ¹Korea Advanced Institute of Science and Technology, South Korea | |||
07. Sep 22 | 14:55 | 15:25 | 7.8.3 |
THREE DIMENSIONAL PATH FOLLOWING CONTROL FOR A FIXED-WING UAV ON SO(3) WITH INPUT SATURATION B. Zhang¹, W. Li, The Second Representative Office of Air Force Armament Departmen, China; Z. Miao¹, Y. Zhang, Beijing System Design Institute of Mechanical-Electrical Enginee, China; ¹Northwestern Polytechnical University, China | |||
07. Sep 22 | 15:25 | 15:55 | 7.8.4 |
COOPERATIVE PATH PLANNING AND ADJUSTING STRATEGY FOR UAVS WITH STRICT TIME CONSTRAINS Y. Lu¹, Q. Chen¹, Y. Wang¹; ¹National University of Defense technology, China Presenter: Yafei LU, National University of Defense Technology | |||
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07. Sep 22 | 13:55 | 14:25 | 8.8.1 |
A STRUCTURE PRELIMINARY DESIGN OF A FLEXIBLE FLYING DEMONSTRATOR P. J. González¹, G. Stavorinus¹, H. Shahi¹, Y. M. Meddaikar², S. Cumnuantip², A. Voß², T. Klimmek², W. R. Krüger², F. J. Silvestre¹; ¹TU-Berlin, Germany ;²DLR, Germany | |||
07. Sep 22 | 14:25 | 14:55 | 8.8.2 |
DEVELOPMENT AND APPLICATIONS OF A VIRTUAL HYBRID PLATFORM FOR MULTISCALE ANALYSIS OF ADVANCED STRUCTURES OF AIRCRAFT E. Carrera, Politecnico di Torino, Italy; S. De Rosa, University of Naples Federico II, Italy; P. Gardonio, University of Udine, Italy; A. Milazzo, University of Palermo, Italy; M. Zaccariotto, University of Padua, Italy | |||
07. Sep 22 | 14:55 | 15:25 | 8.8.3 |
SIMPLIFIED METHOD FOR STRUCTURAL MASS ESTIMATIONS OF SMALL AND MEDIUM-SIZED FIXED WING UAVS FOR PRELIMINARY DESIGN T Seren, Chair of Aircraft Design - Technical University of Munich, Germany | |||
07. Sep 22 | 15:25 | 15:55 | 8.8.4 |
VIBRO-ACOUSTIC ANALYSIS OF MULTI-LAYER CYLINDRICAL SHELL-CAVITY SYSTEMS VIA CUF FINITE ELEMENTS M.C. Moruzzi¹, M. Cinefra, Poliecnico di Bari, Italy; S. Bagassi¹, E. Zappino, Politecnico di Torino, Italy; ¹Università di Bologna, Italy | |||
Reserve Paper | 8.8.R |
WING LOADING PROCESS IN KNOWLEDGE-BASED AIRCRAFT DESIGN AND OPTIMIZATION FRAMEWORK S. Hosseini¹, M. A. Vaziri-Zanjani¹, H. R. Ovesy¹; ¹Amirkabir University of Technology, Iran | |||||
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07. Sep 22 | 13:25 | 13:55 | 9.8.1 |
THERMODYNAMIC POTENTIAL OF TURBOFAN ENGINES WITH DIRECT COMBUSTION OF HYDROGEN A Görtz, German Aerospace Center, Institute of Propulsion Technology, Germany; D Silberhorn, German Aerospace Center, Institute of System Architectures in Ae, Germany | |||
07. Sep 22 | 13:55 | 14:25 | 9.8.2 |
DEVELOPMENT OF THE LOW-COST AND LIMITED SPACE SEA-LEVEL RAM AIR TEST (RAT) MACH 0.8 SYSTEM Truong-Giang Nguyen¹, Quoc-Huy Nghiem¹, Quang-Hai Nguyen¹, Nhu-Van Nguyen¹, Duy-Lanh Chu¹, Phi-Minh Nguyen¹; ¹Viettel Aerospace Institute, Vietnam Presenter: Giang Nguyen, Viettel Aerospace Institute | |||
07. Sep 22 | 14:25 | 14:55 | 9.8.3 |
DESIGN AND MODELING OF A CRYOGENIC LIQUID HYDROGEN FUEL SYSTEM FOR A SHORT-MEDIUM RANGE AIRCRAFT M Xisto, Chalmers University of Technology, Sweden | |||
07. Sep 22 | 15:25 | 15:55 | 9.8.4 |
THE INFLUENCE OF THE VANE LEAN ON THE FLOW IN A TURBINE REAR STRUCTURE V. Vikhorev¹, V. Chernoray¹, Z. Abdel Mallak², J. Larsson²; ¹Chalmers University of Technology, Sweden ;²GKN Aerospace Engine Systems, Sweden | |||
Reserve Paper (interactive) | 9.8.R |
NUCLEAR POWERED AIR-BREATHING ELECTRIC THRUSTERS USED IN UAV FOR EXTRA-TERRESTRIAL APPLICATIONS Shubham Das¹, Naman Kumar Shetty¹; ¹RV College of Engineering, India | |||||
Reserve Paper (interactive) | 9.8.R |
TREND MONITORING OF TURBOPROP ENGINES J. Juracka¹, M. Cervenka¹, M. Horak¹, M. Splichal¹; ¹Brno University of Technology, Czech Republic | |||||
Reserve Paper (interactive) | 9.8.R |
ANALYSIS OF THE AERODYNAMIC CHARACTERISTICS AND ITS INFLUENCE OF TURBOMACHINERY IN TRANSITION STATE Gao Feilong, Northwestern Polytechnical University, China; Zhang Zhibo¹, Li Jingyang¹; ¹AECC Shenyang Engine Research Institute, China | |||||
Reserve Paper (interactive) | 9.8.R |
EXPERIMENTAL STUDY ON THE LASER PLASMA JET PROPULSION - PLASMA JET GENERATION AND THRUST MEASUREMENT - M Harada¹, H Moriai¹; ¹Kanazawa Institute of Technology, Japan | |||||
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07. Sep 22 | 13:55 | 14:25 | 10.8.1 |
ESTIMATION OF STEPWISE VARYING WIND BASED ON DERIVATIVE ESTIMATION OF AIRCRAFT H.S. Luu¹, Y. Ochi¹; ¹National Defense Academy, Japan | |||
07. Sep 22 | 14:25 | 14:55 | 10.8.2 |
A GENERALISED MULTI-OBJECTIVE ISLAND MODEL FOR FLIGHT CONTROL SYSTEM CLEARANCES P. Piprek¹, P. M. Dias¹, D. Schwalb¹; ¹Airbus Defence and Space GmbH, Germany | |||
07. Sep 22 | 14:55 | 15:25 | 10.8.3 |
EFFECTS OF DESIGN PARAMETERS ON SWASHPLATELESS ROTOR CONTROL L.K. Tang, China | |||
07. Sep 22 | 15:25 | 15:55 | 10.8.4 |
RESEARCH ON SERVO CONTROL METHOD AND DAMPING CHARACTERISTICS OF ACTIVE CONTROL DEVICE Liyang Yao¹, hui Yu¹, Zhongrui Zhao¹, Jinlei Zheng¹; ¹Shenyang Aircraft Design and Research Institute, China | |||
Reserve Paper | 10.8.R |
STATISTICAL DATA SELECTION FOR BETTER FLIGHT CHARACTERISTIC MODELING M Naruoka¹, T Ninomiya¹; ¹Japan Aerospace Exploration Agency, Japan Presenter: Tetsujiro Ninomiya, Japan Aerospace Exploration Agency | |||||
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07. Sep 22 | 13:55 | 14:25 | 11.8.1 |
VIRTUAL RECONFIGURATION AND ASSESSMENT OF AIRCRAFT CABINS USING MODEL-BASED SYSTEMS ENGINEERING M. Fuchs¹, F. Beckert¹, F. Rauscher¹, C. Goetz¹, J. Biedermann¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany | |||
07. Sep 22 | 14:25 | 14:55 | 11.8.2 |
MORE ELECTRIC AIRPLANE: CASE STUDY STOCKHOLM-COPENHAGEN Andreas Johansson, Saab Aeronautics, Sweden; Mustafa Yildiz¹, Lina Bertling-Tjernberg¹; ¹Royal Institute of Technology (KTH), Sweden | |||
07. Sep 22 | 14:55 | 15:25 | 11.8.3 |
HMI-HUFLAB – A BRAZILIAN - SWEDISH INITIATIVE IN HUMAN FACTORS FOR AERONAUTICS E. Villani¹, J. Alfredsson², M. Bång³, B. Johansson³, U. Anderini², D. Arjoni¹; ¹Aeronautics Institute of Technology (ITA), Brazil ;²SAAB AB, Sweden ;³Linköping University, Sweden | |||
07. Sep 22 | 15:25 | 15:55 | 11.8.4 |
CRITICALITY AND COMFORT ZONE SUPPORTING DESIGN CHOICES TO ACHIEVE SUSTAINABLE REQUIREMENTS THE CASE OF ELECTRIC AIRCRAFT L Pereira, Federal University of ABC, Brazil; P Krus, Linköping University, Sweden | |||
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07. Sep 22 | 13:55 | 14:25 | 13.8.1 |
CLUSTER STRUCTURE AND GATEWAY AVAILABILITY OF AD-HOC COMMUNICATION NETWORKS IN THE NORTH ATLANTIC AIRSPACE T. Marks¹, A. Hillebrecht¹; ¹German Aerospace Center, Germany | |||
07. Sep 22 | 14:25 | 14:55 | 13.8.2 |
DEMAND PATTERN INFLUENCE ON RELATION OF TURNRAROUND DURATION AND GATE OCCUPATION DEPENDING ON AVAILABLE RESOURCES Lothar Christoffels, German Aerospace Center (DLR), Germany; Olga Gluchshenko, Deutsches Zentrum für Luft- und Raumfahrt (DLR), Germany | |||
07. Sep 22 | 14:55 | 15:25 | 13.8.3 |
ASSESSMENT OF REAL-TIME DATA TRANSMISSION VIA AD-HOC COMMUNICATION NETWORKS IN THE NORTH ATLANTIC OCEANIC AIRSPACE A. Hillebrecht¹, T. Marks¹, V. Gollnick, Hamburg University of Technology, Germany; ¹German Aerospace Center, Air Transportation Systems, Germany | |||
07. Sep 22 | 15:25 | 15:55 | 13.8.4 |
AIR TRAFFIC SIMULATION ACROSS FIR IN JAPAN USING CELLULAR AUTOMATON K Sekine¹, T Tatsukawa¹, K Fujii¹, E Itoh, The University of Tokyo, Japan; ¹Tokyo University of Science, Japan | |||
Reserve Paper | 13.8.R |
OPTIMIZATION OF AIRCRAFT FLIGHT PATHS CONSIDERING THE CONFLICTING PARAMETERS OF ECONOMY AND SAFETY Tetsuya Nagashima¹, Ding Ming, Institutes of Innovation for Future Society, Nagoya University, Japan; Fujii Keisuke¹, Takeda Kazuya¹; ¹Graduate School of Informatics, Nagoya University, Japan | |||||
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07. Sep 22 | 13:55 | 14:25 | 14.8.1 |
MEASUREMENT OF NOISE AND INDOOR CLIMATE ON BOARD A TURBOPROP AIRPLANE FLIGHT Victor Norrefeldt¹, Benjamin Müller¹, Andreas Lindner¹, Yu Song, TU Delft, Netherlands; Neil Mansfield, Nottingham Trent University, United Kingdom; Peter Vink, vhp Human Performance, Netherlands; ¹Fraunhofer IBP, Germany | |||
07. Sep 22 | 14:25 | 14:55 | 14.8.2 |
USE OF THE FLIGHT TEST FACILITY MOCK-UPS IN THE EUROPEAN CLEAN SKY 2 PROGRAM Victor Norrefeldt¹, Florian Mayer¹, Arnav Pathak¹, Marie Pschirer¹, Max Kienberger¹, Andreas Lindner¹, Sabine Johann¹, Anna Nagele-Renzl¹, Michael Buschhaus¹, Gunnar Grün¹; ¹Fraunhofer IBP, Germany | |||
07. Sep 22 | 14:55 | 15:25 | 14.8.3 |
COMPUTATIONAL STUDY OF AIRFLOW AND DISPERSION OF AIRBORNE PATHOGENS INSIDE AN AIRCRAFT CABIN C. L. S. Raposo¹, J. M. M. Sousa¹; ¹IDMEC, Instituto Superior Técnico, Portugal Presenter: Carlos Raposo, IDMEC, Instituto Superior Técnico | |||
07. Sep 22 | 15:25 | 15:55 | 14.8.4 |
IMPACT OF MOTION-DEPENDENT ERRORS ON THE ACCURACY OF AN UNAIDED STRAPDOWN INERTIAL NAVIGATION SYSTEM K. Borodacz¹, C. Szczepanski¹; ¹Lukasiewicz Research Network - Institute of Aviation, Poland |
15:55 - 16:15 | Break |
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07. Sep 22 | 16:15 | 16:45 | 1.9.1 |
PROGRESS TOWARD SUSTAINABLE AVIATION F. S. Collier, NASA, United States | |||
07. Sep 22 | 16:45 | 17:15 | 1.9.2 |
TRANSONIC TRUSS-BRACED WING VISION VEHICLE TECHNOLOGY MATURATION N. A. Harrison, Boeing Research and Technology, United States | |||
07. Sep 22 | 17:15 | 17:45 | 1.9.3 |
TRANSONIC TRUSS-BRACED WING DEMONSTRATOR OVERVIEW C. K. Droney, Boeing, United States | |||
07. Sep 22 | 17:45 | 18:15 | 1.9.4 |
THE JETZERO BLENDED WING BODY - BUILDING THE PATH TO ZERO CARBON AVIATION A Page, JetZero, United States | |||
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07. Sep 22 | 16:15 | 16:45 | 2.9.1 |
DESIGN AND ECO-EFFICIENCY ASSESSMENT OF A PEOPLE-MOVER AIRCRAFT IN COMPARISON TO STATE-OF-THE-ART NARROW BODY AIRCRAFT S. Wöhler¹, J.-N. Walther¹, W. Grimme¹; ¹German Aerospace Center (DLR), Germany Presenter: Sebastian Wöhler, German Aerospace Center (DLR) | |||
07. Sep 22 | 16:45 | 17:15 | 2.9.2 |
MINIMIZING THE CLIMATE IMPACT OF THE NEXT GENERATION AIRCRAFT USING NOVEL CLIMATE FUNCTIONS FOR AIRCRAFT DESIGN K. Radhakrishnan, 1Institute of Air Transportation Systems, TUHH, Germany; K. Deck¹, P. Proesmans¹, F. Linke², F. Yin¹, V. Grewe¹, R. Vos¹, B. Lührs², M. Niklaß², I. Dedoussi¹; ¹Delft University of Technology, Netherlands ;²Air Transportation Systems, DLR, Germany | |||
07. Sep 22 | 17:15 | 17:45 | 2.9.3 |
PROPELLER AIRCRAFT DESIGN OPTIMIZATION FOR CLIMATE IMPACT REDUCTION R. Thijssen¹, P. Proesmans¹, R. Vos¹; ¹Delft University of Technology, Netherlands | |||
07. Sep 22 | 17:45 | 18:15 | 2.9.4 |
AIRCRAFT FLEET MODELS USING A BOTTOM-UP APPROACH FOR SIMULATING AVIATION TECHNOLOGICAL PROSPECTIVE SCENARIOS S. Delbecq¹, T. Planès¹, M. Delavenne¹, V. Pommier-Budinger¹, A. Joksimovic¹; ¹ISAE-SUPAERO, France | |||
07. Sep 22 | 18:15 | 18:45 | 2.9.5 |
SUSTAINABLE AVIATION FOR SWEDEN - TECHNOLOGY & CAPABILITY ASSESSMENT TARGETING 2045 C Jouannet, Saab Aeronautics, Sweden; I Staack¹, T Grönstedt², X Zhao², P Krus¹, A Lundbladh, GKN Aerospace, Sweden; B Nagel, DLR, Germany; ¹Linköpings University, Sweden ;²Chalmers, Sweden | |||
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07. Sep 22 | 16:15 | 16:45 | 3.9.1 |
SORA-BASED RISK ASSESSMENT FOR CARGO UNMANNED AERIAL VEHICLES IN THE UAM FRAMEWORK L. Babetto¹, B. Kniebel¹, E. Stumpf¹; ¹ILR, RWTH Aachen University, Germany | |||
07. Sep 22 | 16:45 | 17:15 | 3.9.2 |
MEDIUM SIZE UAV AS TEST PLATFORM FOR NEW TECHNOLOGIES J. Mieloszyk¹, A. Tarnowski¹, A. Kwiek¹, R. Topolewski¹, T. Goetzendorf-Grabowski¹; ¹Warsaw University of Technology, Poland | |||
07. Sep 22 | 17:15 | 17:45 | 3.9.3 |
CONCEPTUAL DESIGN AND SIZING FOR A FIXED WING UAV FOR EXPLORATION OVER MARS P Gupta, Manipal Institute of Technology, Manipal, India, India; R.S Pant, Indian Institute of Technology Bombay, Mumbai, India, India Presenter: Pranav Gupta | |||
07. Sep 22 | 17:45 | 18:15 | 3.9.4 |
AN INVESTIGATION ON THE IMPROVEMENT FOR TANDEM WING PITCHING-MOMENT CHARACTERISTICS Xiangsheng Wang¹, Tielin Ma, Institude of Unmanned System, Beihang University, China; Nanxuan Qiao¹, Jingcheng Fu, SchoolofTransportationScienceandEngineering, Beihang University, China; ¹School of Aeronautic Science and Engineering, Beihang University, China | |||
07. Sep 22 | 18:15 | 18:45 | 3.9.5 |
TASK ALLOCATION METHOD FOR COMPLEX RECONNAISSANCE AREA BY MULTIPLE UAVS YUAN YUE¹, YANG PEI¹, PENG HOU¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | |||
Reserve Paper | 3.9.R |
COOPERATIVE THREAT ENGAGEMENT WITH HETEROGENEOUS DRONES SWARMS L. Giacomossi¹, J. Ricardo Jr¹, J. F. B. Brancalion, EMBRAER, Brazil; M. R. O. A. Maximo¹, D. A. Santos¹; ¹ITA, Brazil | |||||
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07. Sep 22 | 16:15 | 16:45 | 4.9.1 |
ENHANCING CFD PREDICTIONS FOR THE GRIPEN AIRCRAFT (invited) P. Eliasson¹, P. Weinerfelt¹, F. Bramkamp, NSC, Sweden; ¹Saab, Sweden | |||
07. Sep 22 | 16:45 | 17:15 | 4.9.2 |
STUDY OF THE EFFECTS OF NUMERICAL MODEL ENHANCEMENTS FOR AEROSTRUCTURAL ANALYSIS IN TRANSONIC FLOWS J. A. A. Lyrio¹, J. L. F. Azevedo², D. A. Rade¹, R. G. da Silva², C. Breviglieri, Embraer, S. A., Brazil; ¹Instituto Tecnologico de Aeronautica, DCTA/ITA, Brazil ;²Instituto de Aeronautica e Espaço, DCTA/IAE/ALA, Brazil Presenter: Joao Luiz Azevedo, Instituto de Aeronautica e Espaço, IAE/DCTA | |||
07. Sep 22 | 17:15 | 17:45 | 4.9.3 |
A STATIC STABILITY COMPARISON OF WIND TUNNEL AND COMPUTATIONAL FLUID DYNAMIC METHODS L.K. Fitzgerald¹, A.J. Niven¹, P.C. Griffin¹; ¹University of Limerick, Ireland | |||
07. Sep 22 | 17:45 | 18:15 | 4.9.4 |
EXTERNAL-INTERNAL AERODYNAMIC COUPLING ON A TURBOPROP ENGINE USING THE BODY-FORCE METHOD R. Moretti, ONERA, France | |||
07. Sep 22 | 18:15 | 18:45 | 4.9.5 |
DEVELOPMENT OF A CFD MODEL AND METHODOLOGY FOR THE INTERNAL FLOW SIMULATION IN A HYDROGEN-POWERED UAV Alessandro Porcarelli, Netherlands | |||
Reserve Paper | 4.9.R |
INVESTIGATION ON CRUISE PERFORMANCE OF A SOLAR-POWERED UAV FOR ENVIRONMENTAL MONITORING IN TIBET K.-L. Wang¹, Z. Zhou¹; ¹Northwestern Polytechnical University, China | |||||
Reserve Paper | 4.9.R |
CAD DEFORMATION FOR THE CONSIDERATION OF AEROELASTIC EFFECTS Patrick Wegener¹, Stefan Keye¹; ¹DLR, Germany | |||||
Reserve Paper (interactive) | 4.9.R |
CRITICAL REVIEW OF SOUNDING ROCKET FLIGHT DATA AND COMPUTATIONAL FLUID DYNAMICS EFFORTS B. G. Kierulf, Northeastern University, United States | |||||
Reserve Paper (interactive) | 4.9.R |
A FAST PREDICTION METHOD FOR DROPPING WATER OF FIRE FIGHTING AIRCRAFT BASED ON EXTERNAL BALLISTICS OF PARTICLES H.-Y. Li¹, X. Zhao¹, Z.-X. Xia¹; ¹School of Aeronautics, Northwestern Polytechnical University, China Presenter: H.-Y. Li, School of Aeronautics, Northwestern Polytechnical University | |||||
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07. Sep 22 | 16:15 | 16:45 | 5.9.1 |
PARAMETRIC INVESTIGATION OF A DISTRIBUTED PROPULSION SYSTEM ON A REGIONAL AIRCRAF D. de Rosa, CIRA - Italian Aerospace Research Centre, Italy | |||
07. Sep 22 | 16:45 | 17:15 | 5.9.2 |
TRANSONIC NACELLE DESIGN FOR FUTURE MEDIUM RANGE AERO-ENGINES B. D. J. Schreiner¹, D. G. MacManus¹, F. Tejero¹, F. Sanchez-Moreno¹, C. Sheaf, Rolls Royce, United Kingdom; ¹Cranfield University, United Kingdom Presenter: Fernando Tejero, Cranfield University | |||
07. Sep 22 | 17:15 | 17:45 | 5.9.3 |
STUDY OF EFFECTS ON THE WING\\\'S AERODYNAMIC CHARACTERISTICS DUE TO DISTRIBUTED PROPULSION OVER WINGSPAN G. J. Resende¹, V. Malatesta¹, M. C. Savio², B. Castro²; ¹ITA - Aeronautics Institute of Technology, Brazil ;²EMBRAER, Brazil | |||
07. Sep 22 | 17:45 | 18:15 | 5.9.4 |
A NOVEL EMBEDDED INLET BASED ON THE INTEGRATED DESIGN CONCEPT OF FUSELAGE AND INLET Panpan Yan, Shenyang Aircraft Design and Research Institute, China; Fangliang Liu, Shenyang Aircraft Design and Research Institute, Chinese Aeronau, China | |||
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07. Sep 22 | 16:15 | 16:45 | 6.9.1 |
WIND TUNNEL TEST OF A BLENDED WING BODY UNMANNED AERIAL VEHICLE R. Mariani¹, S. Suewatanakul¹, S. Ghika¹, L. A. Penela¹, P. Wennhage¹, B. Zang, University of Bristol, United Kingdom; ¹KTH Royal Institute of Technology, Sweden | |||
07. Sep 22 | 16:45 | 17:15 | 6.9.2 |
WIND TUNNEL EXPERIMENT OF TAXIDERMY BLACK-TAILED GULL(LARUS CRASSIROSTRIS) AND BLACK KITE (MILVUS MIGRANS) N. Kishimoto, Setsunan University, Japan; D. Wada¹, M. Tamayama¹, Y. Iwami², N. Tomita², T. Ikeda³, Y. Tanahashi³, K. Katagiri, Osaka Research Institute of Science and Technology, Japan; ¹JAXA, Japan ;²Yamashina Institute for Ornithology, Japan ;³Chubu University, Japan | |||
07. Sep 22 | 17:15 | 17:45 | 6.9.3 |
ANALYSIS OF LOW-SPEED AERODYNAMIC CHARACTERISTICS OF BUSEMANN BIPLANE AIRFOIL INSTALLED HIGH LIFT DEVICES T. DUONG NGUYEN¹, Masato Taguchi¹, Masashi Kashitani¹, Kazuhiro Kusunose, Formerly Japan Aerospace Exploration Agency, Japan; ¹National Defense Academy of Japan, Japan | |||
07. Sep 22 | 17:45 | 18:15 | 6.9.4 |
EXPERIMENTAL INVESTIGATION ON TRANSPORT AIRPLANE LONGITUDINAL STABILITY ENHANCEMENT IN CRITICAL ICING CONDITION LITAO FAN¹, TIANHAO GUO¹, LEI ZHANG¹, HUI ZHANG¹; ¹CARDC, China Presenter: Litao Fan, China Aerodynamics Research and Development Center | |||
07. Sep 22 | 18:15 | 18:45 | 6.9.5 |
INFLUENCE OF MANEUVERING PROCESS ON PERFORMANCE CHARACTERISTICS OF BELLY INLET OF AIRCRAFT Bin-Bin XU¹, Chaojun Wu¹, Fuzhen Sun¹, Jianping, Tang¹, Wentao Xiong¹; ¹China Aerodynamics Research and Development Center, China | |||
Reserve Paper (interactive) | 6.9.R |
EXPERIMENTAL STUDY ON NON-COMMAND MOTION CHARACTERISTICS OF SMALL ASPECT RATIO FLYING WING Y. Shen¹, S. Feng¹, Y. Wang¹, C. Bu¹, H. Tan¹, W. Mu¹, H. Chen¹; ¹AVIC Aerodynamics Research Institute, China | |||||
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07. Sep 22 | 16:15 | 16:45 | 7.9.1 |
TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES STRUCTURES I. Rivero Arevalo¹, A. Palomar Claudio¹, N. Martin Gonzalez¹, M. Lozano Hidalgo¹, J. Romero Arana¹, B. De Nicolas Urrutia¹, M. Rebollo Rosa¹, J. Gomez-Escalonilla Martin¹; ¹Airbus, Spain | |||
07. Sep 22 | 16:45 | 17:15 | 7.9.2 |
VARIATIONS IN STRUCTURAL PROPERTIES OF LATTICE STRUCTURES DEPENDING ON UNIT CELL SHAPE FOR MORPHING WINGS Yuta Nishijima¹, Hiroaki Tanaka¹, Adrian Biron, Special Military School of Saint-Cyr, France; Takashi Miura¹; ¹National Defense Academy, Japan | |||
07. Sep 22 | 17:15 | 17:45 | 7.9.3 |
PROPOSITION OF A NEW QUALIFICATION IMPACT TEST FOR AEROSPACE SMART STRUCTURES G. Gastaldo, France; Y. Rafik, France; M. Budinger, France; V. Pommier-Budinger, France; P. Olivier, France; P. Navarro, France | |||
07. Sep 22 | 17:45 | 18:15 | 7.9.4 |
DEVELOPMENT OF STRUCTURAL BONDED REPAIRS FOR A350XWB CFRP AIRFRAME R. Starikov, Airbus Operations, Germany; C. Fualdes, Airbus Operations, France | |||
07. Sep 22 | 18:15 | 18:45 | 7.9.5 |
PERIDYNAMIC SIMULATION PLATTFORM TO DETERMINE VIRTUAL ALLOWABLES OF MANUFACTURING DEVIATIONS Christian Willberg¹, Jan-Timo Hesse¹, Daniel Krause¹; ¹German Aerospace Center, Germany | |||
Reserve Paper | 7.9.R |
X-BAND PASS FREQUENCY SELECTIVE SURFACE RASORBER APPLICATION IN RADOMES X Huang, China | |||||
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07. Sep 22 | 16:15 | 16:45 | 8.9.1 |
PRELIMINARY STUDY ON A FLUIDIC DEVICE SUPPORTING AIRCRAFT-FLIGHT CONTROL WIENCZYSLAW STALEWSKI, Lukasiewicz Research Network- Institute of Aviation, Poland | |||
07. Sep 22 | 16:45 | 17:15 | 8.9.2 |
EXPERIMENTS TO INVESTIGATE LIFT PRODUCTION MECHANISMS ON AN OSCILLATING TRAILING-EDGE FLAP M. Bremm¹, R. Hörnschemeyer¹, E. Stumpf¹; ¹RWTH Aachen University, Germany | |||
07. Sep 22 | 17:15 | 17:45 | 8.9.3 |
IMPROVING STALL CHARACTERISTICS OF UCAV WING WITH VORTEX GENERATORS (invited) P. Eliasson, Saab, Sweden; A. Rizzi¹, J. Oppelstrup¹, M. Zhang, Airinnova AB, Sweden; ¹KTH, Sweden Presenter: Arthur Rizzi, KTH | |||
07. Sep 22 | 17:45 | 18:15 | 8.9.4 |
OPTIMIZATION STUDY ON THE FLOW SEPARATION CONTROL USING A SAWTOOTH PLASMA ACTUATOR L. Wang, Beihang University, China; C.W. Wong¹, Y. Zhou¹; ¹Harbin Institute of Technology, China | |||
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07. Sep 22 | 16:15 | 16:45 | 9.9.1 |
THE IMPACT OF REACTION MECHANISM COMPLEXITY IN LES MODELING OF LIQUID KEROSENE SPRAY COMBUSTION A. Åkerblom, Lund University, Sweden | |||
07. Sep 22 | 16:45 | 17:15 | 9.9.2 |
NUMERICAL ANALYSIS OF PROPAGATION OF DETONATION WAVE PLUNGING ENTRY THE FUEL JET TRAIN INSIDE RDC F Wang¹, T Mizukaki¹; ¹Tokai University, Japan | |||
07. Sep 22 | 17:15 | 17:45 | 9.9.3 |
LES OF COMBUSTION DYNAMICS IN AN ETHYLENE/HYDROGEN-AIR RAMJET N. Zettervall¹, K. Nordin-Bates¹, C. Ibron¹, C. Fureby, Lund University, Sweden; ¹FOI, Sweden | |||
07. Sep 22 | 17:45 | 18:15 | 9.9.4 |
HIGH PRESSURE HYDROGEN OXYGEN COMBUSTION KINETIC ASSESSMENT FOR AIR-BREATHING PROPULSION SUPERSONIC GREEN AVIATION G. Saccone¹, M. Marini¹; ¹Italian Aerospace Research Centre - CIRA, Italy | |||
07. Sep 22 | 18:15 | 18:45 | 9.9.5 |
RESEARCH ON FLOW HEAT TRANSFER CHARACTERISTICS OF HEAT EXCHANGER BASED ON BIONIC FRACTAL STRUCTURE B-W Yu¹, X Yu¹, M-G Cao¹, X-Z Zhang¹, C-L Zhang¹, H-B Ji, Institute of Metal Research, Chinese Academy of Sciences, China; W-T Tong, Avic GuZhou YongHong Aviation Machinery Co, China; ¹Shenyang Aeroengine Research Institute, China | |||
Reserve Paper | 9.9.R |
DESIGN OF AERO-ENGINE FADEC POWER SUPPLY CONTROL SYSTEM BASED ON FORWARD DESIGN YANG SHANG, COMAC, China | |||||
Reserve Paper | 9.9.R |
STUDY ON THE APPLICATION OF EMULSION FUEL IN SMALL JET ENGINES Sato Azuma¹, Yasuda Ryota¹, Harada Masanori¹, Shibasaki Sora¹, Moriai Hideki¹; ¹Kanazawa Institute of Technology, Japan Presenter: Ryota Yasuda, Kanazawa Institute of Technology | |||||
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07. Sep 22 | 16:15 | 16:45 | 10.9.1 |
THE NEW DLR FLIGHT CONTROL TESTBED ISTAR - DEVELOPMENT OF THE EFCS Dominik Niedermeier¹, Kai Giese¹, Dirk Leißling¹; ¹DLR, Germany | |||
07. Sep 22 | 16:45 | 17:15 | 10.9.2 |
RAPID PROTOTYPING IN AIRCRAFT DESIGN USING CFD, WIND TUNNEL AND FLIGHT TESTING R Larsson¹, U Ringertz, Royal Institute of Technology, KTH, Sweden; D Lundström, Linköping University, LIU, Sweden; A Sobron¹; ¹Saab Aeronautics, Sweden | |||
07. Sep 22 | 17:15 | 17:45 | 10.9.3 |
SYNTHETIC AIR DATA A COMPARATIVE PRACTICAL STUDY V. L. M. Veras, EMBRAER, Brazil; L. C. S. Góes, ITA, Brazil | |||
07. Sep 22 | 17:45 | 18:15 | 10.9.4 |
AUTOMATIC AIR TO AIR REFUELING FLIGHT CONTROL LAWS M.J Martinez, Spain | |||
07. Sep 22 | 18:15 | 18:45 | 10.9.5 |
FREE FLIGHT TEST IN HORIZONTAL WIND TUNNEL WITH POWERED AIRCRAFT J.-F. Wang¹, S.-G. Lu¹, S. Feng¹, M.-H. Wang¹; ¹AVIC Aerodynamics Research Institute, China | |||
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07. Sep 22 | 16:15 | 16:45 | 11.9.1 |
THE AGILE 4.0 MBSE-MDAO DEVELOPMENT FRAMEWORK: OVERVIEW AND ASSESSMENT Luca Boggero¹, Thierry Lefèbvre, ONERA/DTIS, France; Jos Vankan, Royal Netherlands Aerospace Centre (NLR), Netherlands; Bastiaan Beijer, KE-works, Netherlands; Vincent Saluzzi, Bombardier Aviation, Canada; Björn Nagel¹; ¹German Aerospace Center (DLR), Germany | |||
07. Sep 22 | 16:45 | 17:15 | 11.9.2 |
EXPERIMENTAL INVESTIGATION OF FUEL SLOSH IN A GENERIC FIGHTER WING TANK CONFIGURATION Lisa Debschütz¹, Andreas Seefried², Thomas Westermeier¹, Richard Kuchar², David Schwalb¹; ¹Airbus Defence and Space, Germany ;²German Aerospace Center, Germany Presenter: David Schwalb | |||
07. Sep 22 | 17:15 | 17:45 | 11.9.3 |
COUPLING OF MODEL-BASED SYSTEMS ENGINEERING AND SAFETY ANALYSIS IN CONCEPTUAL AIRCRAFT SYSTEM DESIGN S. Lübbe¹, M. Schäfer¹, Oliver Bertram¹; ¹German Aerospace Center (DLR), Germany | |||
07. Sep 22 | 17:45 | 18:15 | 11.9.4 |
ONTOLOGY-ASSISTED AIRCRAFT CONCEPT GENERATION L. Knöös Franzén¹, R. Chaitanya Munjulury¹, P. Krus¹; ¹Linköping University, Sweden | |||
07. Sep 22 | 18:15 | 18:45 | 11.9.5 |
HYBRID ELECTRIC PROPULSION SYSTEM OPTIMIZATION FOR A COMMUTER AIRCRAFT P Krus¹, I Staack¹, A Oliveira, Federal University of Santa Catharina, Brazil; ¹Linköping University, Sweden | |||
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07. Sep 22 | 16:15 | 16:45 | 12.9.1 |
FIT FOR CHANGE Elena Campillo Borrás¹, Markus Fischer¹, Anke Kaysser-Pyzalla¹, Andreas Klöckner¹, Dirk Kügler¹, Reinhard Mönig¹, Björn Nagel¹, Cord-Christian Rossow¹, Martin Wiedemann¹; ¹Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany | |||
07. Sep 22 | 16:45 | 17:15 | 12.9.2 |
NOVEL PATHWAYS TO SUSTAINABLE AVIATION C. Voigt, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany | |||
07. Sep 22 | 17:15 | 17:45 | 12.9.3 |
CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AIRSPACE Alexander Kuenz¹, Joonas Lieb¹, Andreas Volkert¹, Dagi Geister¹, Nikolaus Ammann¹, Dmytro Zhukov¹, Patrick Feurich, FlyNex, Germany; Julia Gonschorek¹, Matthias Gessner¹, Thomas Kraft¹, Helge Hackbarth, KopterKraft OÜ, Estonia; Gerald Peklar, NXP Semiconductors, Germany; Lukas Schalk¹, Dennis Becker¹, Daniel Gerbeth¹, Chen Zhu¹, Omar Garcia Crespillo¹, Kristijan Caprdja², Heiko Walther², Jan Pertz¹; ¹DLR, Germany ;²DFS, Germany | |||
07. Sep 22 | 17:45 | 18:15 | 12.9.4 |
DESIGN,MANUFACTURING & CERTIFICATION STRATEGIES FOR INNOVATIVE HYDROGEN STORAGE SYSTEMS TO ENABLE ZERO EMISSION AVIATION - Wiedemann, DLR, Germany | |||
07. Sep 22 | 18:15 | 18:45 | 12.9.5 |
ELIMINATING CLIMATE IMPACT FROM AVIATION – REVIEW OF PROMISING AIRCRAFT CONCEPTS AND ENABLING TECHNOLOGY BRICKS J. Hartmann, German Aerospace Center (DLR), Germany | |||
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07. Sep 22 | 16:15 | 16:45 | 13.9.1 |
ATCO STRATEGIES IN TACTICAL TBO: A SIMULATOR STUDY M. Nylin¹, J. Nilsson¹, J. Lundberg², M. Bång²; ¹LiU/LFV, Sweden ;²LiU, Sweden | |||
07. Sep 22 | 16:45 | 17:15 | 13.9.2 |
TRAJECTORY-BASED OPERATIONS TO IMPROVE LONG-RANGE AIR TRAFFIC FLOW MANAGEMENT G Enea, MIT Lincoln Laboratory, United States; J Bronsvoort, Airservices Australia, Australia Presenter: Gabriele Enea, MIT Lincoln Laboratory | |||
07. Sep 22 | 17:15 | 17:45 | 13.9.3 |
ASSESSMENT OF ENERGY-OPTIMAL APPROACHES WITH INCREASED GLIDESLOPE ANGLES D. Vechtel¹, P. Pauly¹; ¹German Aerospace Center (DLR), Germany | |||
07. Sep 22 | 17:45 | 18:15 | 13.9.4 |
COMPETITIVITY, STRATEGY AND VALUE ON AIRPORTS A METHOD OF DIAGNOSIS, SUGGESTIONS AND ACTIONS FOR INTERNATIONAL AIRPORTS A. H. O. Carvalho, Pontifícia Universidade Católica de Minas Gerais – PUC Minas, Brazil; R. V. C. Paiva, Universidade FUMEC - Fundação Mineira de Educação e Cultura, Brazil; E. M. M. F. Torga, Centro Universitário UNA, Brazil | |||
07. Sep 22 | 18:15 | 18:45 | 13.9.5 |
AIRCRAFT MASS ESTIMATION USING CRUISE FLIGHT PROFILE R. Mori, ENRI, Japan | |||
Reserve Paper | 13.9.R |
KINETIC ENERGY RECOVERY FROM A LANDING AIRCRAFT: ENERGY ANALYSIS, ENVIRONMENTAL AND ECONOMIC PROSPECTS R.C. Camilleri¹, A Batra¹; ¹Institute of Aerospace Technologies (IAT), University of Malta, Malta | |||||
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07. Sep 22 | 16:15 | 16:45 | 14.9.1 |
ENERGY-BASED SYSTEM ARCHITECTURE DESIGN - ENVIRONMENTAL CONTROL SYSTEM A. Joksimovic¹, X. Carbonneau¹, F. Brazier, Delft University of Technology, Netherlands; R. Vingerhoeds¹; ¹ISAE-SUPAERO, France | |||
07. Sep 22 | 16:45 | 17:15 | 14.9.2 |
METHODOLOGY FOR THE AUTOMATED PRELIMINARY CERTIFICATION OF ON-BOARD SYSTEMS ARCHITECTURES THROUGH REQUIREMENTS ANALYSIS C. Cabaleiro¹, M. Fioriti, Politecnico di Torino, Italy; L. Boggero¹; ¹German Aerospace Center (DLR), Germany | |||
07. Sep 22 | 17:15 | 17:45 | 14.9.3 |
A SYSTEM INTEGRATOR’S PERSPECTIVE ON VEHICLE SYSTEM EVALUATION AT THE AIRCRAFT CONCEPT STAGE Adelia Drego¹, Sören Steinkellner¹; ¹Saab Aeronautics, Sweden | |||
07. Sep 22 | 17:45 | 18:15 | 14.9.4 |
EXTENSIBLE AIRCRAFT FUSELAGE MODEL GENERATION FOR A MULTIDISCIPLINARY, MULTI-FIDELITY CONTEXT J.-N. Walther¹, C. Hesse¹, J. Y.-C. Biedermann¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany | |||
07. Sep 22 | 18:15 | 18:45 | 14.9.5 |
MATHEMATICAL MODELLING AND ANALYSIS OF THERMAL MANAGEMENT SYSTEM ARCHITECTURE FOR HYPERSONIC AIRCRAFT Shrrirup Nambiar, Politecnico di Torino, Italy | |||
Reserve Paper | 14.9.R |
HYDRO ENVIRONMENTAL MAPPING TOOL USING SWARMS AND MACHINE LEARNING, UAV & USV R.K. Kuntz - Rodrigo, IBRV - Institute of Research & Development, Brazil | |||||
Reserve Paper | 14.9.R |
SURVEYING INDOOR NAVIGATION SYSTEMS FOR AUTONOMOUS MOBILITY OF PEOPLE WITH VISUAL IMPAIRMENT AND DEAFBLINDNESS LP Pereira, Federal University of ABC, Brazil | |||||
Reserve Paper (interactive) | 14.9.R |
HIGH-PRECISION MULTI-DISCIPLINARY OPTIMIZATION: CONFIGURATIONS, METHODS AND STRATEGIES Melody Liu, Science and Technology on Electro-optic Control Laboratory, China | |||||
Reserve Paper (interactive) | 14.9.R |
DYNAMIC MODEL AND EXPERIMENT INVESTIGATION OF PIEZOELECTRIC-POWERED DRAGONFLY-SCALE WING FLAPPING W.-L Wang, China |
Thursday, 08. Sep 2022
0.8 | General lecture V: ICAS/IFAR „Transforming Aviation towards Zero Emission - to mitigate the climate impact“ I. Yimer, NRC Canada, B. Sainjon, ONERA France, M. Fischer, DLR Germany, Y. Watanabe, JAXA Japan, P. Krus, SARC Sweden Chair: D. Mavris ICAS PC Chair | |||
08. Sep 22 | 08:00 | 09:30 |
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09:30 - 10:00 | Coffee Break |
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08. Sep 22 | 10:00 | 10:30 | 1.10.1 |
CS2 PROGRAMME OVERVIEW S. Dubious, France | |||
08. Sep 22 | 10:30 | 11:00 | 1.10.2 |
SUSTAINABLE TECHNOLOGIES FOR COMMERCIAL AIRCRAFT OF TOMORROW - INTEGRATED MULTIFUNCTIONAL FUSELAGE DEMONSTRATOR Y.C. Roth, Germany | |||
08. Sep 22 | 11:00 | 11:30 | 1.10.3 |
OPEN FAN ENGINE ARCHITECTURE FOR NEXT GENERATION SMR C. DIETTE, Safran Aircraft Engines, France | |||
08. Sep 22 | 11:30 | 12:00 | 1.10.4 |
PROGRESS IN WING DESIGN, STATUS AND PERSPECTIVES J. LERY, Dassault Aviation, France; M. WERNER, Airbus, Germany; E. COUSTOLS, ONERA, France | |||
08. Sep 22 | 12:00 | 12:30 | 1.10.5 |
THE CLEAN SKY 2 TECHNOLOGY EVALUATOR 1ST GLOBAL ASSESSMENT RESULTS J.F. Brouckaert, Belgium | |||
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08. Sep 22 | 10:00 | 10:30 | 2.10.1 |
COMBINED APPLICATION OF HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER IN PRELIMINARY AIRCRAFT DESIGN T. Effing¹, V. Schmitz¹, F. Schültke¹, F. Peter, Bauhaus Luftfahrt e.V, Germany; E. Stumpf¹; ¹RWTH Aachen University, Germany | |||
08. Sep 22 | 10:30 | 11:00 | 2.10.2 |
CLEAN-SKY 2 LARGE PASSENGER AIRCRAFT PLATFORM 1 ADVANCED ENGINE AND AIRCRAFT CONFIGURATIONS D. KIERBEL, AIRBUS, France | |||
08. Sep 22 | 11:00 | 11:30 | 2.10.3 |
AERODYNAMIC DESIGN AND ANALYSIS OF HLFC WINGS WITHIN THE EUROPEAN PROJECT HLFC-WIN Thomas Streit¹, Martin Kruse¹, Thomas Kilian¹, Ilias Petropoulos, ONERA, France; Judith v Geyr¹; ¹DLR, Germany | |||
08. Sep 22 | 11:30 | 12:00 | 2.10.4 |
ECONOMICS OF SUSTAINABLE REGIONAL AIR MOBILITY P De Felipe¹, D Yang¹; ¹Imperial College London, United Kingdom | |||
08. Sep 22 | 12:00 | 12:30 | 2.10.5 |
TOWARD A GREENER AIRCRAFT ARCHITECTURE F Vidal de Saint Jean, Dassault Aviation, France | |||
Reserve Paper | 2.10.R |
DEVELOPMENT OF INNOVATIVE AND ECO-FRIENDLY AIRFRAME TECHNOLOGIES TO IMPROVE AIRCRAFT LIFE CYCLE ENVIRONMENTAL FOOTPRINT L.A.S.A Prado¹, S. Coskun¹, T.S.G. Das¹, A. Kötter¹; ¹Capgemini Engineering / Altran Deutschland und SAS KG, Germany Presenter: Luis Antonio Sanchez de Almeida Prado, Capgemini Engineering / Altran Deutschland und SAS KG | |||||
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08. Sep 22 | 10:00 | 10:30 | 3.10.1 |
SCALABILITY ANALYSIS OF RADICAL TECHNOLOGIES TO VARIOUS AIRCRAFT CLASS - PART I: INITIAL DESIGNS M.F.M. Hoogreef¹, V.O. Bonnin¹; ¹Delft University of Technology, Netherlands | |||
08. Sep 22 | 10:30 | 11:00 | 3.10.2 |
SCALABILITY ANALYSIS OF RADICAL TECHNOLOGIES TO VARIOUS AIRCRAFT CLASS - PART II: SENSITIVITY ANALYSIS V.O. Bonnin¹, M.F.M. Hoogreef¹; ¹Delft University of Technology, Netherlands | |||
08. Sep 22 | 11:00 | 11:30 | 3.10.3 |
REGIONAL TRANSPORT AIRCRAFT DESIGN USING TURBO-ELECTRIC DISTRIBUTED PROPULSION SYSTEM V. Polepeddi¹, P. Raj¹, Mathias Emeneth, PACE America, United States; ¹Virginia Tech, United States | |||
08. Sep 22 | 11:30 | 12:00 | 3.10.4 |
RETROFITTING EXISTING AIRCRAFT WITH HYDROGEN PROPULSION E. Fourquet-Beramendi¹, A.S.J. van Heerden¹, I. Roumeliotis¹, S. Brown¹, V. Pachidis¹; ¹Cranfield University, United Kingdom Presenter: Elorie Fourquet-Beramendi, Airbus | |||
08. Sep 22 | 12:00 | 12:30 | 3.10.5 |
ARRIVING AT CERTIFIABLE NOVEL AIRLINER USING LIQUID HYDROGEN & EFFICIENCY METRICS Raj (Dr) Nangia, Nangia, United Kingdom; Leslie (Mr) Hyde, Consulting, United Kingdom | |||
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08. Sep 22 | 10:00 | 10:30 | 4.10.1 |
STEADY-STATE AERODYNAMICS TIP GAP INFLUENCE IN A TRANSONIC LINEAR CASCADE AT NEAR STALL Carlos Tavera Guerrero¹, Nenad Glodic¹, Hans Mårtensson, GKN Aerospace Sweden AB, Germany; ¹KTH, Sweden | |||
08. Sep 22 | 10:30 | 11:00 | 4.10.2 |
LARGE EDDY SIMULATION OF A LYNX HELICOPTER LANDING IN THE BARROSO CORVETTE SHIP D. M. Pio¹, C.F. Rafael¹, P. S. C. Villela¹, G. A. L. da Silva¹, M. J. M. Guedes, Marinha do Brasil, Brazil; M. Ferro, Laboratorio Nacional de Computacao Cientifica - LNCC, Brazil; ¹Aerothermal Solutions - ATS, Brazil | |||
08. Sep 22 | 11:00 | 11:30 | 4.10.3 |
NUMERICAL INVESTIGATIONS OF ROTORCRAFT PRESSURE ERROR CORRECTION BY UTILIZATION OF AIR DAMS A.-O. Sezer, Turkish Aerospace, Turkey; M. Elfarra, Ankara Y?ld?r?m Beyaz?t University, Turkey | |||
08. Sep 22 | 11:30 | 12:00 | 4.10.4 |
TRANSONIC FLOW OVER DELTA WING USING ENTROPIC LATTICE BOLTZMANN METHOD M Dhake¹, C Thantanapally¹, S Arcidiacono¹, S Ansumali¹; ¹SankhyaSutra Labs Ltd, India Presenter: Chakradhar Thantanapally, SankhyaSutra Labs Limited | |||
08. Sep 22 | 12:00 | 12:30 | 4.10.5 |
CFD TAKE-OFF ANALYSIS OF A SEAPLANE HULL THROUGH A DYNAMIC MULTIPHASE MODEL M. Sinisi¹, G. Occhipinti¹, G. Cantanna¹, A. Caramazza¹, G. Dilonardo¹, E. Cestino¹; ¹Politecnico di Torino, Italy | |||
Reserve Paper | 4.10.R |
EFFECTS OF TWO WINGLET TIP GEOMETRIES ON THE FLOW AND AERODYNAMIC PERFORMANCE OF A HYDRAULIC AXIAL TURBINE D. S. Tonon¹, J. T. Tomita¹, C. Bringhenti¹, D. F. C. Barbosa¹, L. H. L. Whitacker¹, L. E. N. Almeida, AVIBRAS, Brazil; ¹Aeronautics Institute of Technology , Brazil | |||||
Reserve Paper (interactive) | 4.10.R |
VALIDATING AIRSPACE CFD MODELS FOR DRONE OPERATION WITH FLIGHT TEST DATA D. Standingford¹, C. Sequeira², M. Allan¹, G. Furse², J. Sharpe¹; ¹Zenotech, United Kingdom ;²Flare Bright, United Kingdom | |||||
Reserve Paper (interactive) | 4.10.R |
COMPARATIVE ANALYSIS OF AERODYNAMIC CHARACTERISTICS OBTAINED BY ANALYTICAL, PANEL AND CFD METHODS. G. Muchla¹, A. Kwiecien¹; ¹Faculty of Power and Aeronautical Engineering, WUT, Poland Presenter: Adrianna Kwiecien, Faculty of Power and Aeronautical Engineering, WUT | |||||
Reserve Paper (interactive) | 4.10.R |
REDESIGNING AND SIMULATION EVALUATION ON LARGE-FLOW HIGH-TEMPERATURE HIGH-PRESSURE BYPASS SURGE-OUT SYSTEM Zhi-peng:Z.-P Li, AECC Shenyang Engine Research Institute, China | |||||
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08. Sep 22 | 10:00 | 10:30 | 5.10.1 |
AERONAUTICAL CFD AND TURBULENCE - PROGRESS AND CHALLENGES PART 1 (invited) A Rizzi¹, DS Henningson¹; ¹KTH, Sweden | |||
08. Sep 22 | 10:30 | 11:00 | 5.10.2 |
AERONAUTICAL CFD AND TURBULENCE - PROGRESS AND CHALLENGES PART 2 (invited) A Rizzi¹, D. Henningson¹; ¹KTH, Sweden | |||
08. Sep 22 | 11:00 | 11:30 | 5.10.3 |
OPEN CAVITY SIMULATIONS UNDER SIDESLIP CONDITIONS Karthick Rajkumar¹, Joseph Radtke¹, Eike Tangermann¹, Markus Klein¹; ¹University of the Bundeswehr Munich, Germany | |||
08. Sep 22 | 11:30 | 12:00 | 5.10.4 |
APPLICATION OF GP AND ANN APPROACHES FOR RECONSTRUCTION OF TURBULENT JET FLOW FIELDS V. Gryazev, United Kingdom; U. Armani, United Kingdom; A.R. Murali, France; A.P. Markesteijn, United Kingdom; S.A. Karabasov, United Kingdom; V. Toropov, United Kingdom; S.E. Naghibi, United Kingdom; V. Riabov, Japan | |||
08. Sep 22 | 12:00 | 12:30 | 5.10.5 |
UNSTEADY SIMULATIONS OF MASSIVELY SEPARATED FLOW AROUND NACA0021 AIRFOIL USING A TRANSITIONAL IDDES MODEL Y. Wang, China; S.-Q. Zhang, China; W.-P. Song, China; Z.-H. Han, China | |||
Reserve Paper | 5.10.R |
INVESTIGATION ON THE INFLUENCES OF TURBULENCE MODEL AND OPERATING CONDITIONS ON THE CENTRIFUGAL NOZZLE PERFROMANCE Da Mo¹, Hongjun Lin¹, Caiyun Liang¹, Shoutang Shang¹, Jiaohui Xia, Aero Engine Academy of China, China; Yixiong Liu¹; ¹AECC Shenyang Engine Research Institute, China | |||||
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08. Sep 22 | 10:00 | 10:30 | 6.10.1 |
EXPERIMENTAL INVESTIGATIONS OF AN AEROELASTIC WIND TUNNEL MODEL FOR TAIL BUFFETING ANALYSIS J. Stegmüller¹, S. Hayböck¹, P. Hartl¹, C. Breitsamter¹; ¹Technical University of Munich, Germany | |||
08. Sep 22 | 10:30 | 11:00 | 6.10.2 |
OPTIMIZATION OF AN ACTIVE DAMPING SYSTEM FOR USE WITH A SINGLE STRUT MOUNT J. L. Pereira, National Research Council Canada, Canada | |||
08. Sep 22 | 11:00 | 11:30 | 6.10.3 |
WIND-TUNNEL TEST ON LEADING-EDGE VORTEX OF LOW-ASPECT-RATIO FLAPPING PLATES J.-S. Han¹, C. Breitsamter¹; ¹Technical University of Munich, Germany | |||
08. Sep 22 | 11:30 | 12:00 | 6.10.4 |
POWERED WIND TUNNEL TESTING WITH HYDRAULIC MOTORS D. Steiling¹, P. Aschwanden¹, J. Müller¹, T. Jax¹; ¹RUAG AG, Switzerland Presenter: Peter Aschwanden, RUAG AG | |||
08. Sep 22 | 12:00 | 12:30 | 6.10.5 |
EXPERIMENTING ROTORCRAFT FLIGHT IN COMPLEX ENVIRONMENTAL CONDITIONS USING WIND TUNNEL: HELICOPTER SHIP LANDING CASE A. Zanotti¹, G. Gibertini¹, G. Quaranta¹; ¹Politecnico di Milano, Italy | |||
Reserve Paper | 6.10.R |
RESEARCH ON VIRTUAL FLIGHT TEST OF LARGE-SCALE LOW-SPEED WIND TUNNEL W.-Y. Yanling, Aerodynamics Research Institute,Harbin, China | |||||
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08. Sep 22 | 10:00 | 10:30 | 7.10.1 |
INCREMENTAL FATIGUE DAMAGE MODEL: APPLICATION TO PLANE PROBLEMS WITH NON-PROPORTIONAL LOADING Z Kapidzic¹, S. B. Lindström, Linköping University, Sweden; J Lundgren¹; ¹Saab AB, Sweden | |||
08. Sep 22 | 10:30 | 11:00 | 7.10.2 |
FATIGUE OF STANDARD SPECIMENS – THE INFLUENCE OF THE STRESS GRADIENT ON THE S-N CURVE IN DIFFERENT AL2024 KT=2.0 DESIGNS S Sieberer¹, J Homan, Fatec Engineering, Netherlands; M Schagerl¹; ¹Johannes Kepler University Linz, Austria | |||
08. Sep 22 | 11:00 | 11:30 | 7.10.3 |
FATIGUE LIFE ENHANCEMENT OF TYPICAL AERONAUTICAL JOINTS BY MEANS OF ENGINEERED RESIDUAL STRESSES L. Boni ¹, F Bovecchi¹, D. O. Busse, AIRBUS Operations GmbH, Germany; D. Furfari, IRBUS Operations GmbH, Germany; ¹University of Pisa, Italy | |||
08. Sep 22 | 11:30 | 12:00 | 7.10.4 |
FATIGUE CHARACTERIZATION OF ADHESIVE JOINTS IN AEROPLANES-THE DEVELOPMENT OF A NEGATIVE LOAD RATIO (R<0) TESTING METHOD O Orell¹, J Jokinen¹, M Kanerva¹; ¹Tampere University, Finland | |||
08. Sep 22 | 12:00 | 12:30 | 7.10.5 |
FATIGUE DAMAGE MODEL OF HIGH TEMPERATURE POLYMER COMPOSITES IN AERO-ENGINES Vivek Richards Pakkam Gabriel¹, Patrik Fernberg¹; ¹Luleå University of Technology, Sweden | |||
Reserve Paper | 7.10.R |
FATIGUE CRACK PROPAGATION IN ADDITIVELY MANUFACTURED POLYMER PARTS H.H El Fazani¹, J. Laliberté¹, J. Coil¹; ¹Carleton University , Canada | |||||
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08. Sep 22 | 10:00 | 10:30 | 8.10.1 |
DEVELOPMENT OF A PREDICTIVE DAMAGE METHODOLOGY FOR HYBRID WING BODY AIRCRAFT STRUCTURES H. Raza¹, C. Harey¹, P. Vaghela¹, J. Bayandor¹; ¹CRASH Lab, University at Buffalo, United States Presenter: Christopher Harley, CRASH Lab, Dept. of MAE, University at Buffalo | |||
08. Sep 22 | 10:30 | 11:00 | 8.10.2 |
NUMERICAL ANALYSIS AND COMPARISON WITH RESULTS OF FRACTURE TESTS OF LUG MANUFACTURED IN COMPOSITE MATERIAL G. C. Fonseca, Embraer Minas Gerais, Brazil; S. F. M. Almeida, Instituto Tecnológico de Aeronáutica, Brazil | |||
08. Sep 22 | 11:00 | 11:30 | 8.10.3 |
ENHANCEMENT OF FLEXIBLE STRATEGY FOR AUGMENTING DESIGN POINTS FOR COMPUTER EXPERIMENTS AND APPLICATION TO A MDO OF A FAN-BLISK A. Tamkan¹, P. Flassig¹, M Meyer, Rolls-Royce Deutschland, Germany; ¹Technische Hochschule Brandenburg, Germany | |||
08. Sep 22 | 11:30 | 12:00 | 8.10.4 |
TRANSIENT AND FREE-VIBRATION ANALYSIS OF LAMINATED SHELLS THROUGH THE DISCONTINUOUS GALERKIN METHOD G. Guarino¹, V. Gulizzi¹, A. Milazzo¹; ¹1University of Palermo, Department of Engineering, Italy | |||
08. Sep 22 | 12:00 | 12:30 | 8.10.5 |
DESIGN AND STUDY ON NOISE REDUCTION PROPERTIES OF A MULTISTAGE BIONIC MEMBRANE-TYPE ACOUSTIC METAMATERIAL X. J. Zhang¹, D. Guo¹, H. Y. Huang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | |||
Reserve Paper | 8.10.R |
MODELING AND ANALYSES OF A MULTI-FUNCTIONAL PIEZO-SMA-COMPOSITE WING G.C. Silva, Technische Universität Berlin, Germany | |||||
Reserve Paper | 8.10.R |
A NEW APPROACH TO SHAPING THE PUSHROD TUBE AS THE MAIN COMPONENT OF THE CONTROL SYSTEM, OPTIMIZATION, AND MANUFACTURING. W. Grendysa, Warsaw University of Technology, Poland | |||||
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08. Sep 22 | 10:00 | 10:30 | 9.10.1 |
AEROELASTIC TAILORING OF COMPRESSOR BLADES A.-P. Chalke¹, N Glodic¹, M Gutierrez Salas¹; ¹KTH Royal Institute of Technology, Sweden | |||
08. Sep 22 | 10:30 | 11:00 | 9.10.2 |
RAPID AEROACOUSTIC PLANFORM DESIGN OPTIMIZATION OF INSTALLED PROPELLERS T. Sinnige¹, W. de Gruijl¹, W. de Haan¹, G. Eitelberg¹; ¹Delft University of Technology, Netherlands | |||
08. Sep 22 | 11:00 | 11:30 | 9.10.3 |
PERFORMANCE BENEFITS OF A FAN ON BLADE – FLADE – FOR A VARIABLE CYCLE ENGINE Marcelo Assato, IAE, Brazil; Ali Altar Inceer¹, Lucilene Moraes¹, Jesuino Takachi Tomita², Cleverson Bringhenti², Pedro Bravo-Mosquera, USP, Brazil; Daniel Rosell, SAAB Aeronautcs, Sweden; Tomas Grönstedt¹; ¹Chalmers University, Sweden ;²ITA, Brazil | |||
08. Sep 22 | 11:30 | 12:00 | 9.10.4 |
STATUS OF GKN AEROSPACE\\\'S ENGINE MODULE DEMONSTRATORS IN THE CLEAN SKY-2 PROJECT Robert Lundberg¹, Lars Ellbrant¹, Patrik Johansson¹, Ulf Johansson¹, Mattias Billson¹, Bernhard Gustafsson¹; ¹GKN Aerospace Sweden AB, Sweden Presenter: Lars Ellbrant, GKN Aerospace Sweden AB | |||
08. Sep 22 | 12:00 | 12:30 | 9.10.5 |
STUDY ON THE OBJECTIVE FUNCTION OF THE PROFILED ENDWALL OPTIMIZATION OF AN EMBEDDED COMPRESSOR STATOR Jiayu Wang¹, Dejun Meng¹, Dongmin Feng¹, Qingwei Zhao¹; ¹Shenyang Engine Research Institute of AECC, China | |||
Reserve Paper | 9.10.R |
DESIGN AND EFFICIENCY ANALYSIS OF EVTOL CONTRA-ROTATING PROPELLER N.-X Qiao¹, T.-L Ma¹, X.-S Wang¹, J.-C Fu¹; ¹Beihang University, China | |||||
Reserve Paper | 9.10.R |
EXPERIMENTAL STUDY ON THE EFFECT OF INTERSTAGE BLEEDING ON THE PERFORMANCE OF FULL-SCALE MULTISTAGE AXIAL COMPRESSOR Z.-B. Zhang¹, Y.-H. Zhang¹, Y.-H. Chen¹; ¹Shenyang Engine Research Institute, China | |||||
Reserve Paper | 9.10.R |
EXPERIMENTAL STUDY OF FLAT BAFFLE INLET TOTAL-PRESSURE DISTORTION IN A THREE-STAGE FAN CHEN Yehui¹, ZHANG Zhibo¹, WANG Anni¹; ¹AECC Shenyang Engine Institute, China Presenter: Yehui CHEN, AECC Shenyang Engine Institute | |||||
Reserve Paper (interactive) | 9.10.R |
SURGE CHARACTERISTICS IN FRONT OF EACH STAGE FOR A HIGH PRESSURE FIVE STAGE COMPRESSOR Jia Bobo¹, Zhang Zhibo¹, Li Hongxin, AECC, China; ¹AECC Shenyang Engine Institute, China | |||||
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08. Sep 22 | 10:00 | 10:30 | 10.10.1 |
INCREMENTAL NONLINEAR DYNAMIC CONTROL WITH SPARSE NON-PARAMETRIC BAYESIAN REGRESSION OF DAMAGED AIRCRAFT L Kim¹, D Lee¹, H Bang¹; ¹Korea Advanced Institute of Science and Technology, South Korea | |||
08. Sep 22 | 10:30 | 11:00 | 10.10.2 |
FAULT-TOLERANT CONTROL FOR AIRCRAFT WITH STRUCTURAL DAMAGE USING GAUSSIAN PROCESS REGRESSION D.-W. LEE¹, L.-S KIM¹, H.-J. AHN¹, H.-C. BANG¹; ¹KAIST, South Korea | |||
08. Sep 22 | 11:00 | 11:30 | 10.10.3 |
EFFECTIVENESS ANALYSIS OF DOBC Q-FILTER PARAMETERS FOR A MULTICOPTER UAV H.J. Jeaong¹, C.S. Roh¹, Y.H. Jang¹, J.Y Suk¹, S.K. Kim¹; ¹Department of Aerospace Engineering, Chungnam National Universit, South Korea | |||
08. Sep 22 | 11:30 | 12:00 | 10.10.4 |
CONVEX PROGRAMMING-BASED OPTIMAL THREE-DIMENSIONAL MID-COURSE GUIDANCE WITH LOSSLESS CONVEXIFICATION C.-G. Jung¹, C.-H. Lee¹, M.-J. Tahk¹; ¹KAIST, South Korea | |||
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08. Sep 22 | 10:00 | 10:30 | 11.10.1 |
HETEROGENEOUS SYSTEMS MODELLING IN SUPPORT OF INCREMENTAL DEVELOPMENT R. Hällqvist¹, J. Naeser¹, J. Wallén Axehill¹, E. Herzog¹; ¹Saab AB, Sweden | |||
08. Sep 22 | 10:30 | 11:00 | 11.10.2 |
A MODEL BASED SYSTEMS ENGINEERING APPROACH TO STREAMLINED NOISE CERTIFICATION OF TRANSPORT-TYPE AIRCRAFT D Kim¹, F Karagoz¹, S Datta¹, M Balchanos¹, D Anvid¹, E Harrison¹, D Mavris¹; ¹Georgia Institute of Technology, United States | |||
08. Sep 22 | 11:00 | 11:30 | 11.10.3 |
A HOLISTIC AIRCRAFT CABIN METAMODEL AS AN APPROACH TOWARDS AN INTERCONNECTED DIGITISED CABIN LIFECYCLE M. C. Berschik¹, M. Blecken¹, H. Kumawat¹, J.-E. Rath¹, D. Krause¹, R. God¹, T. Schüppstuhl¹; ¹Hamburg University of Technology, Germany | |||
08. Sep 22 | 11:30 | 12:00 | 11.10.4 |
A COLLABORATIVE DESIGN METHOD FOR CIVIL AIRCRAFT BASED ON AN ENDURING AND EVOLUTIONARY AUTHORITATIVE SOURCE OF TRUTH X Sun¹, M Luo¹, Z Cui¹, Z Ji¹, H Liu¹; ¹Beihang University, China | |||
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08. Sep 22 | 10:00 | 10:30 | 13.10.1 |
DESIGN & VALIDATION OF A FLIGHT CENTRIC WORKLOAD MODEL INCLUDING ATC TASK CHANGE & CONSIDERING INFLUENCING FACTORS T. Finck¹, M.-C. Névir, Technische Universität Dresden, Germany; C. Kluenker¹; ¹German Aerospace Center, Germany | |||
08. Sep 22 | 10:30 | 11:00 | 13.10.2 |
REDUCED TRANSMISSION RISKS FOR PASSENGER OPERATIONS DURING COVID-19 PANDEMIC Michael Schultz, Universität der Bundeswehr München, Germany; Majid Soolaki, University of Westminster, United Kingdom; Oliver Michler, Dresden University of Technology, Germany; Eri Itoh, University of Tokyo, Japan | |||
08. Sep 22 | 11:00 | 11:30 | 13.10.3 |
VOICE PROJECT: REDUCED SEPARATIONS AND IMPROVED EFFICIENCY BASED ON VHF COMMUNICATIONS OVER LEO SATELLITES E. Delgado Pinedo¹, R-F. Flores Acedo¹, S. Lora García¹, D. Polo Álvarez¹; ¹Indra Sistemas, S.A., Spain | |||
08. Sep 22 | 11:30 | 12:00 | 13.10.4 |
V/A-R AIR GESTURES HMI INTERACTION IN AIRPORT CONTROL TOWERS S. Bagassi¹, M. Corsi¹, F. Galuppi¹; ¹University of Bologna, Italy | |||
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08. Sep 22 | 10:00 | 10:30 | 14.10.1 |
MODEL-BASED SYSTEMS ENGINEERING FOR FUTURE DIGITAL FLIGHT LINES M.A. Kelly, Lockheed Martin Aeronautics, United States | |||
08. Sep 22 | 10:30 | 11:00 | 14.10.2 |
MACHINE LEARNING ENABLED MIXED REALITY SYSTEMS – FOR EVALUATION AND VALIDATION OF AUGMENTED EXPERIENCE IN AIRCRAFT MAINT T. Gulrez¹, V. Kakoc¹, G. Emmanuel², M. Schumacher², T. Mills¹; ¹Defence Science and Technology Group, Australia ;²Airbus Australia Pacific, Australia | |||
08. Sep 22 | 11:00 | 11:30 | 14.10.3 |
GRAPH-BASED KNOWLEDGE REPRESENTATION AND ALGORITHMS FOR AIR AND MAINTENANCE OPERATIONS E. Olsson¹, O. Candell¹, P. Funk², R. Sohlberg², M. Castaño, Luleå University of Technology, Sweden; M. Gustafsson¹, P. Bladh¹; ¹Saab Aeronautics, Sweden ;²Mälardalen University, Sweden | |||
08. Sep 22 | 11:30 | 12:00 | 14.10.4 |
AUGMENTED REALITY FOR AIRCRAFT FATIGUE NON-DESTRUCTIVE EVALUATION Michael Scott¹, Stephan Koschel¹, Wim Verhagen¹, Oleg Levinski, Defence Science and Technology Group, Australia; Pier Marzocca¹; ¹RMIT University, Australia | |||
08. Sep 22 | 12:00 | 12:30 | 14.10.5 |
ATTENTION GUIDANCE AI-SYSTEM FOR REMOTE TOWER OPERATIONS G.L Söderholm, Linköpings University, Sweden | |||
Reserve Paper | 14.10.R |
REAL-TIME TRAJECTORY PLANNING SYSTEM USING HYBRID DATASET FOR ROBOTIC OPERATIONS SY Yildirim, Cranfield University, United Kingdom | |||||
Reserve Paper (interactive) | 14.10.R |
ECONOMIC PERFORMANCE EVALUATION OF AIRCRAFT MAINTENANCE USING DATA-DRIVEN APPROACH X. Zhao, Nanjing University of Aeronautics and Astronautics, China |
12:30 - 13:30 | Lunch Break |
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08. Sep 22 | 13:30 | 14:00 | 1.11.1 |
CA PROGRAMME RATIONALE AND OVERVIEW R. van Manen, Netherlands | |||
08. Sep 22 | 14:00 | 14:30 | 1.11.2 |
ULTRA-EFFICIENT AIRCRAFT AND PROPULSION ARCHITECTURES FOR LOW-EMISSION SHORT/MEDIUM RANGE [SMR] AIRCRAFT M. Calvo Blanco, Spain | |||
08. Sep 22 | 14:30 | 15:00 | 1.11.3 |
HYBRID-ELECTRIC AND FULL ELECTRIC ARCHITECTURES FOR LOW-EMISSION HYBRID-ELECTRIC REGIONAL [REG] AIRCRAFT A. Marino, Italy | |||
08. Sep 22 | 15:00 | 15:30 | 1.11.4 |
DISRUPTIVE TECHNOLOGIES TO ENABLE ZERO-CARBON HYDROGEN–POWERED [HPA] SHORT RANGE AIRCRAFT P. Trinchieri, Italy | |||
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08. Sep 22 | 13:30 | 14:00 | 2.11.1 |
AERODYNAMIC CHARACTERISTICS OF BOX WINGS FOR AN INNOVATIVE EVTOL CONFIGURATION Eiji SHIMA, Japan Aerospace Exploration Agency, Japan; Koichi YONEZAWA, Central Research Institute of Electric Power Industry, Japan; Ryoma NISHIDA¹, Shusuke HONDA ¹, Makoto SATO ¹; ¹Kogakuin University, Japan | |||
08. Sep 22 | 14:00 | 14:30 | 2.11.2 |
IMPACT OF NO. OF WING STATIONS ON TWIST OF BWB CONCEPTUAL DESIGN IN A MDAO ENVIRONMENT TO MATCH TARGET LIFT DISTRIBUTION B. Fröhler¹, M. Iwanizki¹, P. Balack¹, J. Häßy¹, D. Silberhorn1¹; ¹German Aerospace Center (DLR), Germany | |||
08. Sep 22 | 14:30 | 15:00 | 2.11.3 |
CS2 – MANTA – MULTI-FUNCTIONAL FLAP MECHANISM OFFERING A SECOND DEGREE OF FREEDOM M Desmet¹, J. Vervliet¹, D. De Wit¹, R. Seidler, Deutsches Zentrum Fuer Luft und Raumfahrt E.V., Germany; J. Docter, Netherlands Aerospace Centre, Netherlands; B. Everaert¹; ¹Asco Industries nv/sa, Belgium | |||
08. Sep 22 | 15:00 | 15:30 | 2.11.4 |
INFLUENCES OF CHANGING THE INSTALLING POSITIONS OF MULTIPLE WINGLETS ON AERODYNAMIC CHARACTERISTICS E Kobayashi¹, K Chiba¹; ¹The University of Electro-Communications, Japan | |||
Reserve Paper | 2.11.R |
DESIGN AND FLUTTER ANALYSIS OF SWEPT BAFFLED INFLATABLE WING N. Ma¹, F.-M. Meng¹, J.-H. Meng¹, L. Liu¹; ¹Beijing Institute of Technology, China | |||||
Reserve Paper | 2.11.R |
AIRFOIL DESIGN BY MULTI-ADDITIONAL SAMPLING MULTI-FIDELITY EFFICIENT GLOBAL OPTIMIZATION Krittin Khankwa¹, Tharathep Phiboon¹, Atthaphon Ariyarit¹, Rattaporn Kasemsri¹, Masahiro Kanazaki, Tokyo Metropolitan University, Japan; ¹Suranaree University of Technology, Thailand | |||||
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08. Sep 22 | 13:30 | 14:00 | 3.11.1 |
COOLING SYSTEM OF STRATOFLY HYPERSONIC VEHICLE: CONCEPTUAL DESIGN, NUMERICAL ANALYSIS AND VERIFICATION R. Scigliano¹, V. De Simone¹, R. Fusaro², D. Ferretto², M. Marini¹, N. Viola²; ¹Italian Aerospace Research Center - CIRA scpa, Italy ;²Politecnico di Torino (PoliTo), Italy | |||
08. Sep 22 | 14:00 | 14:30 | 3.11.2 |
HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONS N. Viola¹, R. Fusaro¹, D. Ferretto¹, O. Gori¹, M. Marini², P. Roncioni², B. O. Cakir³, A. C. Ispir³, B. H. Saracoglu³; ¹Politecnico di Torino, Italy ;²CIRA, Italy ;³VKI, Belgium Presenter: Oscar Gori, Politecnico di Torino | |||
08. Sep 22 | 14:30 | 15:00 | 3.11.3 |
LTO NOISE AND SONIC BOOM PREDICTIONS IN EARLY CONCEPTUAL DESIGN PHASES G. Piccirillo¹, S. Graziani¹, R. Fusaro¹, N. Viola¹; ¹Politecnico di Torino, Italy | |||
08. Sep 22 | 15:00 | 15:30 | 3.11.4 |
SIMPLIFIED MODELS FOR THE PRELIMINARY AERODYNAMIC CHARACTERIZATION OF HIGH-SPEED VEHICLES TO SUPPORT MISSION ANALYSIS O. Gori, Politecnico di Torino, Italy | |||
Reserve Paper | 3.11.R |
“CONCORDE-NEO”: A BIOFUEL PROPELLED SUPERSONIC COMMERCIAL AIRCRAFT WITH CONCORDE CONFIGURATION F. Fornaseri¹, M. Borghi¹, G. Clinca¹, F. A. D'Amico¹, E. Versino¹; ¹Politecnico di Torino, Italy | |||||
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08. Sep 22 | 13:30 | 14:00 | 4.11.1 |
ACCURATE TWO-DIMENSIONAL STEADY-STATES FOR THE SUPERSONIC FLOW OVER A COMPRESSION CORNER R D Santos¹, L. S. de B. Alves¹, N Cerulus², H. R. Quintanilha Jr², V. Theofilis²; ¹UFF, Brazil ;²UoL, United Kingdom | |||
08. Sep 22 | 14:00 | 14:30 | 4.11.2 |
NUMERICAL MODELING OF LAMINAR-TURBULENT TRANSITION IN AN INTERCONNECTING COMPRESSOR DUCT A Capitao Patrao¹, B González Lozano¹, I Jonsson¹, C Xisto¹; ¹Chalmers University of Technology, Sweden | |||
08. Sep 22 | 14:30 | 15:00 | 4.11.3 |
ANALYSIS OF A LAMINAR SEPARATION BUBBLE ON A NACA0009 AIRFOIL AT DIFFERENT BACKGROUND NOISE LEVELS J.S. Kern¹, A. Hanifi¹, D.S. Henningson¹; ¹FLOW, Department of Engineering Mechanics, KTH Royal Institute o, Sweden | |||
08. Sep 22 | 15:00 | 15:30 | 4.11.4 |
A STUDY ON THE NUMERICAL SIMULATION OF FLOW TRANSITION INCLUDING CROSSFLOW EFFECTS A. R. S. Righi, ITA, Brazil; G. L. O. Halila¹, J. L. F. Azevedo¹; ¹IAE, Brazil | |||
Reserve Paper | 4.11.R |
WAVE-PACKETS WITH STEADY TRIPLE-DECK SOLUTIONS Diego Exposito¹, Sudhir L. Gai¹, Andrew J. Neely¹; ¹UNSW Canberra, Australia | |||||
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08. Sep 22 | 13:30 | 14:00 | 5.11.1 |
COMPUTATIONALLY ECONOMICAL METHODS FOR LANDING GEAR NOISE SIMULATIONS R. A. Spencer, CFMS Ltd, United Kingdom; M. R. Allan, Zenotech Ltd, United Kingdom | |||
08. Sep 22 | 14:00 | 14:30 | 5.11.2 |
PROPELLER AEROACOUSTIC MODELS IN VARIABLE-FIDELITY DESIGN OPTIMIZATION W. A. Klimczyk¹, A. Sieradzki¹; ¹Lukasiewicz Research Network - Institute of Aviation, Poland | |||
08. Sep 22 | 14:30 | 15:00 | 5.11.3 |
NUMERICAL PREDICTION OF FOCUS BOOM GENERATED BY MANEUVERS S Han¹, Y Xu¹; ¹Chinese Aeronautical Establishment, China | |||
08. Sep 22 | 15:00 | 15:30 | 5.11.4 |
INVERSE DESIGN METHOD OF LOW-BOOM SUPERSONIC AIRCRAFT FROM NEARFIELD SONIC BOOM J.-L. Qiao, Northwestern Polytechnical University , China | |||
Reserve Paper | 5.11.R |
IN-FLIGHT MEASUREMENTS AND ESTIMATION OF SONIC BOOM SIGNATURE OF SUPERSONIC AIRCRAFT Lixia Qu, China; Shuo Han, China; Yahui Song, China; Yue Xu, China; Yuelin Zhang, China; Yuhang Wang, China | |||||
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08. Sep 22 | 13:30 | 14:00 | 6.11.1 |
WALL INTERFERENCE CORRECTIONS USING NONLINEARLEAST-SQUARES OPTIMISATION Simon Noel¹, David Birch², John Doherty², Tanmay Tipnis¹; ¹QinetiQ, United Kingdom ;²University of Surrey, United Kingdom | |||
08. Sep 22 | 14:00 | 14:30 | 6.11.2 |
A BLOWDOWN-INDUCTION FACILITY FOR HYPERSONIC FLOW SIMULATION DRIVEN BY A HIGH VELOCITY OXYGEN FUEL GUN A. ESPOSITO , DEPT.OF INDUSTRIAL ENGINEERING UNIVERSITY OF NAPLES FEDERICO II, Italy; C. ALLOUIS , STEMS-CNR, Italy; M. LAPPA, Dept of Mech. and Aer.Engineering, University of Strathclyde, United Kingdom | |||
08. Sep 22 | 14:30 | 15:00 | 6.11.3 |
RECENT ACTIVITIES ON FLOW QUALITY ASSESSMENT AT THE EUROPEAN TRANSONIC WINDTUNNEL J. H. You¹, M. C.N. Wright¹, H. Quix¹; ¹European Transonic Windtunnel GmbH, Germany | |||
08. Sep 22 | 15:00 | 15:30 | 6.11.4 |
INVESTIGATION ON CORRECTION OF TUNNEL WALL INTERFERENCE FOR DYNAMIC AIRFOIL TEST IN LOW-SPEED WIND TUNNEL Yuqin Jiao, China Presenter: Yuqin Jiao | |||
Reserve Paper | 6.11.R |
DEVELOPMENT AND VERIFICATION OF OSCILLATING BLADE GUST GENERATOR IN LOW-SPEED WIND TUNNEL Chen BU¹, Zhanyuan MA¹, Ying ZHANG¹, Li LI¹; ¹AVIC Aerodynamics Research Institute, China | |||||
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08. Sep 22 | 13:30 | 14:00 | 7.11.1 |
FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSURE Sture Olsson¹, Björn Carlsson¹; ¹Quintus Technologies AB, Sweden | |||
08. Sep 22 | 14:00 | 14:30 | 7.11.2 |
INFLUENCE OF KEYHOLE TIG WELDING PARAMETERS ON THE WELD GEOMETRY OF NEWLY-DEVELOPED SUPERALLOY VDM 780 Achmad Ariaseta, Sweden; Nima Sadeghinia, Sweden; Joel Andersson, Sweden | |||
08. Sep 22 | 14:30 | 15:00 | 7.11.3 |
USE OF FRICTION STIR WELDING ON PRIMARY STRUCTURES OF AIRCRAFTS INSTEAD OF RIVETED JUNCTION D. Desgaches, Stelia Aerospace, France | |||
08. Sep 22 | 15:00 | 15:30 | 7.11.4 |
EXPERIMENTAL INVESTIGATIONS ON TENSILE PROPERTIES OF ALUMINUM HONEYCOMB SANDWICH STRUCTURE WITH SINGLE-SIDED REPAIRING Yan Bing¹, Zhang Guijia¹, Tong Mingbo ¹, Li Lei¹, Yu Dingchang¹, Zhu Shuhua¹, Wu Zhangyu², Wang Hao², Jin Tao, China Special Vehicle Research Institute, China; ¹Nanjing University of Aeronautics & Astronautics, China ;²Nanjing University of Aeronautics and Astronautics, China Presenter: Bing Yan | |||
Reserve Paper | 7.11.R |
ELECTROMAGNETIC INTERFERENCE SHIELDING EFFECTIVENESS OF THE THIN CNF/SICF COMPOSITE Xiaojing JIA¹, Huan DU¹, Liguo ZHANG¹, Zhenquan ZHONG¹, Xinquan ZHANG¹; ¹AVIC The first Aircraft Institute, China | |||||
Reserve Paper | 7.11.R |
RESEARCH ON THE DUCTILE FRACTURE OF AL7085 AND TC11 UNDER COMPLEX STRESS STATE Y.J. LIU, AVIC the First Aircraft Institute, China | |||||
Reserve Paper (interactive) | 7.11.R |
HIGH IMPACT AND DAMAGE TOLERANT MULTICOMPONENT ALLOY FOR HIGH STRAIN RATE APPLICATIONS Muhammad Atif¹, Muhammad Aamir Raza¹, Xianzhe Shi¹, Muhammad Zakir Sheikh¹, Jianghua Shen, Joint International Research Center of Impact Dynamics and Its E, China; Yulong Li, School of Civil Aviation, Northwestern Polytechnical University, China; ¹Northwestern Polytechnical University, China | |||||
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08. Sep 22 | 13:30 | 14:00 | 8.11.1 |
NUMERICAL NONLINEAR VIBRATION-BUCKLING INVESTIGATION OF STRUCTURES SUBJECTED TO MECHANICAL AND THERMAL LOADINGS R. Azzara¹, M. Filippi¹, A. Pagani¹, E. Carrera¹; ¹Politecnico di Torino, Italy | |||
08. Sep 22 | 14:00 | 14:30 | 8.11.2 |
GROUND VIBRATION TESTING OF A HIGH ASPECT RATIO WING WITH REVOLVING CLAMP G. Dessena¹, D.I. Ignatyev¹, J.F. Whidborne¹, A. Pontillo, University of Bristol, United Kingdom; L. Zanotti Fragonara¹; ¹Cranfield University, United Kingdom | |||
08. Sep 22 | 14:30 | 15:00 | 8.11.3 |
UPDATING OF JET TRAINER AIRCRAFT DYNAMIC MODEL TO RESULTS OF GROUND VIBRATION TEST J. Cecrdle, Czech Aerospace Research Centre (VZLU), Czech Republic | |||
08. Sep 22 | 15:00 | 15:30 | 8.11.4 |
DYNAMIC STRSS SIMULATION AND ASYMMETRY STATOR DESIGN FOR A FAN BLISK Yixiong Liu¹, Kening Xu, Aero Engine Academy of China, China; Yuzhi Chen¹, Yunwu Wu¹, Qing Du¹, Da Mo¹; ¹AECC Shenyang Engine Research Institute, China | |||
Reserve Paper | 8.11.R |
DECORATION OF CARBON NANOTUBE - GRAPHENE 3D NANOSTRUCTURES AND THEIR ENHANCEMENTS IN POLYMER MATRIX C Chenxi, Civil Aviation University of China, China | |||||
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08. Sep 22 | 13:30 | 14:00 | 9.11.1 |
TECHNOLOGY MATURATION FOR NEXT GENERATION SMR ENGINE C. DIETTE, Safran Aircraft Engines, France; E. OBERT, Safran, France; G. MARION, Safran Transmission Systems, France; H. DE FRANSSU, Safran Nacelles, France; A. FREZET, Avio Aero, Italy; B. WALTHER, GE Deutschland, Germany; A. SJUNNESSON, GKN Aeropsace Engie Systems, Sweden Presenter: Christophe DIETTE, Safran Aircraft Engines | |||
08. Sep 22 | 14:00 | 14:30 | 9.11.2 |
NOVEL AIRCRAFT PROPULSION AND AVAILABILITY OF ALTERNATIVE, SUSTAINABLE AVIATION FUELS IN 2050 J. Kos¹, J.A. Posada-Duque², B. Peerlings¹, N. Ben Salah², M.N.A. Lim¹, W.F. Lammen¹, I. Stepchuk, TU Delft, Faculty of Technology and Policy Management, Netherlands; E.S. Sman¹, M.P.M. Palmeros-Parada²; ¹Royal Netherlands Aerospace Centre, Netherlands ;²TU Delft, Faculty of Applied Sciences, Netherlands | |||
08. Sep 22 | 14:30 | 15:00 | 9.11.3 |
MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEM Tomas Grönstedt¹, Carlos Xisto¹, Xn Zhao¹, Isak Jonsson¹, Magnus Genrup², Avo Reinap², Nenad Glodic³, Mauricio Guiterrez Salas³, Marcus Lejon*, Richard Avellan*, Mårtensson Hans*; ¹Chalmers University, Sweden ;²Lund University, Sweden ;³Royal Institute of Technology, Sweden ;*GKN Aerospace, Sweden | |||
08. Sep 22 | 15:00 | 15:30 | 9.11.4 |
LOW BPR TURBOFAN PERFORMANCE WITH POWER EXTRACTION D. H. Rosell, Saab Aeronautics, Sweden; U. T. Grönstedt, Chalmers Univerity of Technology, Sweden; P. D. Bravo-Mosquera¹, F. Martini Catalano¹; ¹University of Sao Paulo, Brazil | |||
Reserve Paper | 9.11.R |
ANALYSIS OF THE OPERATION OF THE PULSEJET ENGINE Jon Tegner, FOI, Sweden | |||||
Reserve Paper (interactive) | 9.11.R |
ANALYSIS AND SIZING OF A GREEN PROPULSION SYSTEM FOR A SUBORBITAL AIRCRAFT M. Bruno¹, R. Cambertoni¹, A. Pellegrino¹, P. Petrachi¹, C. Spampinato¹; ¹Polytechnic of Turin, Italy Presenter: Cristina Spampinato, Polytechnic of Turin | |||||
Reserve Paper (interactive) | 9.11.R |
TESTING AND MODELLING OF A DUCTED FAN MOTOR FOR UAV APPLICATIONS B.-O. Schröder¹, P. González¹, F. Silvestre¹; ¹TU Berlin, Germany Presenter: Pedro González, TU Berlin | |||||
Reserve Paper (interactive) | 9.11.R |
COMPARISON OF ANALYTICAL SEMI-EMPIRICAL MODEL FOR JET NOISE PREDICTION F. Petrosino¹, M. Barbarino¹; ¹CIRA, Italy | |||||
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08. Sep 22 | 13:30 | 14:00 | 10.11.1 |
ON LATERAL-LONGITUDINAL CONTROL COUPLING FOR SHORT- AND LONG-FUSELAGE BWB AIRCRAFT CONFIGURATIONS L.M.B.C. Campos, Instituto Superior Técnico, Universidade de Lisboa, Portugal | |||
08. Sep 22 | 14:00 | 14:30 | 10.11.2 |
OPEN-LOOP SUBSPACE IDENTIFICATION OF A FLEXIBLE UNMANNED AERIAL SYSTEM R C M Carvalho Machado, ITA, Brazil | |||
08. Sep 22 | 14:30 | 15:00 | 10.11.3 |
LATERAL-DIRECTIONAL FORCE AND MOMENTS MODELING OF NUMERICAL RESULTS USING NEURO-FUZZY HYBRIDZED WITH DIFFERENTIAL EVOLUT V.T. Santana¹, I. Staack, Linköping University, Sweden; R. M. Finzi¹; ¹Federal University of Uberlândia, Brazil | |||
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08. Sep 22 | 13:30 | 14:00 | 11.11.1 |
TOWARDS CORRECT-BY-CONSTRUCTION DESIGN OF SAFETY-CRITICAL EMBEDDED AVIONICS SYSTEMS I. Sander¹, I. Söderquist², M. Ekman², R. Jordao¹, F. Bahrami¹, R. Chen¹, A. Åhlander²; ¹KTH Royal Institute of Technology, Sweden ;²Saab AB, Sweden | |||
08. Sep 22 | 14:00 | 14:30 | 11.11.2 |
CONCEPT LEVEL EXPLORATION OF IMA-BASED NETWORKED PLATFORMS WITH MIXED TIME-SENSITIVE COMMUNICATION REQUIREMENTS R. Saar de Moraes¹, S. Nadjm-Tehrani¹; ¹Linköping University, Sweden | |||
08. Sep 22 | 14:30 | 15:00 | 11.11.3 |
SYSTEMS ARCHITECTING ASSISTANT (SARA) - ENABLING A SEAMLESS PROCESS CHAIN FROM REQUIREMENTS TO OVERALL SYSTEMS DESIGN N. Kuelper¹, J. Broehan¹, T. Bielsky¹, F. Thieleke¹; ¹Hamburg University of Technology, Germany | |||
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08. Sep 22 | 13:30 | 14:00 | 12.11.1 |
EXPERIMENTAL ANALYSIS OF HEAT TRANSFER CHARACTERISTICS OF DIELECTRIC BARRIER DISCHARGE PLASMA ACTUATOR A. Hatamoto, Japan; K. Emori, Japan; H. Nishida, Japan | |||
08. Sep 22 | 14:00 | 14:30 | 12.11.2 |
THE SENS4ICE EU PROJECT – SAFER AVIATION IN ICING ENVIRONMENT – PROJECT OVERVIEW AND INITIAL RESULTS C. W. Schwarz, DLR, Germany | |||
08. Sep 22 | 14:30 | 15:00 | 12.11.3 |
STRESS AND ENERGY RELEASE RATE INFLUENCE ON ICE SHEDDING WITH RESONANT ELECTROMECHANICAL DE-ICING SYSTEMS G Gastaldo¹, V Palanque, ISAE-Supaero and ONERA, France; M Budinger, INSA/ICA, France; V Budinger¹; ¹ISAE-Supaero, France | |||
08. Sep 22 | 15:00 | 15:30 | 12.11.4 |
NUMERICAL SIMULATION OF ICE ACCRETION ON PITOT TUBE Krzysztof Szilder¹, Peter Forsyth¹; ¹National Research Council, Canada | |||
Reserve Paper | 12.11.R |
EFFECTS OF ANISOTROPIC THERMAL CONDUCTIVITY OF CFRP COMPOSITE ON ELECTROTHERMAL ANTI-ICING SYSTEM Xiaofeng Guo¹, Qian Yang¹, Haoran Zheng¹, Wei Dong¹; ¹Shanghai Jiaotong University, China | |||||
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08. Sep 22 | 13:30 | 14:00 | 13.11.1 |
NEW ENTRANTS’ AIRSPACE INTEGRATION IN JAPAN: JAXA’S ONGOING CONTRIBUTION Naoki Matayoshi, Japan Aerospace Exploration Agency, Japan | |||
08. Sep 22 | 14:00 | 14:30 | 13.11.2 |
ON KEY PARAMETERS FOR THE ATTRACTIVENESS OF ON-DEMAND INTER-CITY AIR MOBILITY T. Ehlers¹, S. Hagemann², V. Gollnick², K. Lütjens¹; ¹German Aerospace Center, Germany ;²Hamburg University of Technology, Germany | |||
08. Sep 22 | 14:30 | 15:00 | 13.11.3 |
THE AUTOMATION EVOLVES: CONCEPT FOR A HIGHLY AUTOMATED CONTROLLER WORKING POSITION I Gerdes¹, M Jameel¹, R Hunger¹, L Christoffels¹, H Gürlük¹; ¹German Aerospace Center DLR, Germany | |||
08. Sep 22 | 15:00 | 15:30 | 13.11.4 |
AN OPERATIONAL CONCEPT FOR THE INTEGRATION OF URBAN AIR MOBILITY VEHICLES INTO THE AIR TRAFFIC CONTROL PROCESSES Isabel C. Metz¹, Sebastian Schier-Morgenthal¹; ¹German Aerospace Center DLR, Germany | |||
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08. Sep 22 | 13:30 | 14:00 | 14.11.1 |
DEVELOPMENT OF MULTI-CANARD UAV FOR ACTIVE AEROELASTIC CONTROL TOWARD PSEUDO-SMALL SATELLITES N Morita¹, N Nakasuka¹, T Tsuchiya¹, K Takashima¹, Y Taguchi¹, K Suzuki¹, T Koyama¹, R Eto¹, I Baba¹; ¹the University of Tokyo, Japan | |||
08. Sep 22 | 14:00 | 14:30 | 14.11.2 |
OVERALL LAYOUT DESIGN OF NEW TYPE TILTROTOR VEHICLES H Kitaba¹, M Bando¹, S Hokamoto¹; ¹Kyushu Univ., Japan Presenter: Shinji Hokamoto, Kyushu University | |||
08. Sep 22 | 14:30 | 15:00 | 14.11.3 |
INFLUENCE OF OVERALL LAYOUT DESIGN OF COMPOUND MULTI-ROTOR VEHICLES ON FLIGHT PERFORMANCE Y HUANG¹, M BANDO¹, S HOKAMOTO¹; ¹Kyushu University, Japan | |||
08. Sep 22 | 15:00 | 15:30 | 14.11.4 |
USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTION L D Jesus¹, A J D Filho¹, M. A. Almeida¹, W. M. Martins¹, T. C. Pimenta¹, A. C. B. Ramos¹, P. Funk, Mälardalen University, Sweden; ¹Federal University of Itajubá, Brazil |
15:30 - 16:00 | Break |
0.9 | 16:00-17:00 ICAS von Karman Lecture: “Clean Sky Programme Achievements and Clean Aviation Outlook” S.Klauke CTO Airbus , E. Dalbies CTO SAFRAN, M. Protti Head of Advanced Research Leonardo Aircraft Chair: A. Krein Head of Clean Sky GER, J.L. Azevedo, ICAS President Brazil | |||
08. Sep 22 | 16:00 | 17:00 |
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17:00 - 17:30 | Closing Ceremony |