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| 11:00 | 11:25 | 1.1.1 |
SUSTAINABLE AVIATION TECHNOLOGY PROGRAMMES IN EUROPE A. Krein, Clean Aviation, Germany | ||||
| 11:25 | 11:50 | 1.1.2 |
UNITED STATES' AIRCRAFT SUSTAINABILITY RESEARCH & DEVELOPMENT EFFORTS A. Orton, Federal Aviation Administration, United States; R. Guerrero, United States Air Force, United States; R. Wahls, National Aeronautics and Space Administration, United States | ||||
| 11:50 | 12:15 | 1.1.3 |
A VIEW LOOKING IN - AVIATION WEEK'S ASSESSMENT OF SUSTAINABLE AVIATION R&D IN CHINA AND THE ASIA-PACIFIC REGION G. Warwick¹, G. Norris¹; ¹Aviation Week, United States | ||||
| 12:15 | 12:40 | 1.1.4 |
Q&A - MINI PANEL Q&A. A, | ||||
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| 11:00 | 11:25 | 2.1.1 |
GLOBAL SENSITIVITY ANALYSIS OF LIQUID HYDROGEN STORAGE DESIGN PARAMETERS FOR OVERALL AIRCRAFT DESIGN T. Burschyk¹, B. Fröhler¹, M. Alder¹, T. Zill¹; ¹DLR, Institute for System Architectures in Aeronautics, Germany | ||||
| 11:25 | 11:50 | 2.1.2 |
GEOMETRIC OPTIMIZATION OF HYDROGEN AIRCRAFT FUSELAGES IN PRELIMINARY DESIGN M. Engelmann¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany | ||||
| 11:50 | 12:15 | 2.1.3 |
RESULTS FROM THE APPU PROJECT: THE POTENTIAL OF LOW-THRESHOLD HYDROGEN-POWERED BLI PROPULSION A. Heidebrecht¹, M. Hoogreef¹, A.T. Isikveren, SAFRAN S.A., Germany; A. Gangoli Rao¹; ¹TU Delft, Netherlands | ||||
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| 11:00 | 11:25 | 3.1.1 |
SET-BASED DESIGN TECHNIQUES FOR EVOLVABILITY EXPLORATION DURING CONCEPTUAL AIRCRAFT DESIGN A.S.J. van Heerden, University of Glasgow, United Kingdom; S. Jimeno Altelarrea¹, A. Riaz¹, X. Chen¹, M.D. Guenov¹, A. Molina-Cristóbal, University of Glasgow Singapore, Singapore; ¹Cranfield University, United Kingdom | ||||
| 11:25 | 11:50 | 3.1.2 |
FAST PARAMETRIC STRUCTURE MODELING FOR VARIETY OF AIRCRAFT CONFIGURATIONS Y.-L. Yin¹, K.-S. Zhang¹, H.-L. Qiao¹, A.-L. Che¹, Z.-H. Han¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | ||||
| 11:50 | 12:15 | 3.1.3 |
TRANSIENT SIMULATION CALCULATION FOR ELECTRIC THERMAL ANTI-ICING PERFORMANCE OF COMPOSITE WING IN ICING ENVIRONMENT Z. Dong¹, X. Guo¹, W. Dong¹, P. Wang¹; ¹Shanghai Jiaotong University, China | ||||
| 12:15 | 12:40 | 3.1.4 |
TILT-DUCT AIRCRAFT WING AERODYNAMIC DESIGN AND OPTIMIZATION BASED ON ADJOINT METHOD Y.-T. Zhang¹, S.-R. Xu¹, Z.-J. Zheng¹, Y. Zheng¹, Y.-L. Liu¹; ¹Zhejiang University, China | ||||
| additional information (interactive) | 3.1.R |
APPLICATION OF LAMBDA FRAMEWORK FOR AIRCRAFT MULTIDISCIPLINARY DESIGN, ANALYSIS AND OPTIMIZATION S. Hosseini¹, M.A. Vaziry Zanjany¹, H.R. Ovesy¹, E. Lekzian, Semnan University, Iran; ¹Amirkabir University of Technology, Iran | |||||
| additional information (interactive) | 3.1.R |
AICRAFT-0 SAT D1 FOR GREENER, SAFER AND AFFORDABLE MORE ELECTRIC (MEA) AND FLY-BY-WIRE (FBW) SMALL AIR TRANSPORT (SAT) M. Alberti¹, G. Apuleo¹, A. Calia¹, D. Cirio¹, A. Cozzolino¹, F. Gravano¹, M. Mancini¹, F. Nunciato¹, A. Terrile¹; ¹Piaggio Aerospace, Italy | |||||
| additional information (interactive) | 3.1.R |
THE INFLUENCE OF DIFFERENT WING MOTIONS ON THE LIFT IN BIO-INSPIRED AERIAL VEHICLES B.T.V. Carnielo¹, D.D. Bueno¹; ¹São Paulo State University, Brazil | |||||
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| 11:00 | 11:25 | 4.1.1 |
AIRCRAFT SYSTEM DESIGN: A MODEL-BASED AND COLLABORATIVE APPROACH V. Voth¹, O. Bertram¹; ¹German Aerospace Center (DLR), Germany | ||||
| 11:25 | 11:50 | 4.1.2 |
TECHMAPS – TECHNOLOGY MANAGEMENT FOR THE ARCHITECTING PROCESS OF AIRCRAFT ON-BOARD SYSTEMS N. Kuelper¹, V. Kriewall¹, K. Beschorner¹, F. Thielecke¹; ¹Hamburg University of Technology, Germany | ||||
| 11:50 | 12:15 | 4.1.3 |
MODEL-BASED APPROACH FOR HYDROGEN PRELIMINARY AIRCRAFT DESIGN CONSIDERING SAFETY AND OPERABILITY A. Sarr¹, J. Jézégou¹, P. de Saqui-Sannes¹; ¹ISAE-SUPAERO, France | ||||
| 12:15 | 12:40 | 4.1.4 |
SAFETY ANALYSIS (CCA) OF THE AIR SUPPLY SYSTEM OF A FUEL CELL-POWERED AERO ENGINE FOR ELECTRIC REGIONAL AIRCRAFT S. Kazula, DLR - Electrified Aero Engines, Germany | ||||
| additional information (interactive) | 4.1.R |
RESEARCH ON TECHNOLOGICAL INNOVATION CAPABILITY EVALUATION INDEX FOR AVIATION INDUSTRIES W. Cheng¹, R. Fan, Aviation Industry Corporation of China, Ltd (AVIC), China; J. Xu¹, H. Zhang¹, Z. Wang¹; ¹Aviation Industry Development Research Center of China (ADR), China | |||||
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| 11:00 | 11:25 | 5.1.1 |
EFFECTIVENESS OF CFD FOR AIRCRAFT DESIGN: STATUS AND PROSPECTS P. Raj, Virginia Tech, United States | ||||
| 11:25 | 11:50 | 5.1.2 |
EFFECTIVENESS OF CFD FOR AIRCRAFT DESIGN: STATUS AND PROSPECTS PART 2 P. Raj, United States | ||||
| 11:50 | 12:15 | 5.1.3 |
COMPUTATIONAL ANALYSIS ON THE EFFECTS OF LEADING EDGE TUBERCLES ON THE PERFORMANCE OF ROTATING PROPELLER D. Di Pasquale¹, T. Tarun, Indian Institute of Technology(BHU) , India; S. Shubham¹, S.A. Prince¹, A. Proenca¹; ¹Cranfield University, United Kingdom | ||||
| 12:15 | 12:40 | 5.1.4 |
INITIAL DEVELOPMENT OF A CFD ICING TOOL J.R. Teixeira Da Silva¹, M.E.M.C. Lopes¹, A.P.R. Preguica¹, C.F. Rafael¹, P.C. Souza Villela¹, G.A. Lima da Silva, Aerothermal Solutions and Software Distributor LLC, United States; H. Jasak, Cambridge University, United Kingdom; ¹ATS Aerothermal Solutions, Brazil | ||||
| additional information (interactive) | 5.1.R |
CONJUGATED HEAT TRANSFER SIMULATION OF BUOYANCY-INDUCED FLOW AND HEAT TRANSFER MECHANISMS IN A COMPRESSOR CAVITY M. Jian¹, Y. Xiao¹, X. Cheng¹, W. Dong¹; ¹Shanghai Jiao Tong University, China | |||||
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| 11:00 | 11:25 | 6.1.1 |
A CFD STUDY OF THE ACTIVE FLOW CONTROL SYSTEM BEHAVIOUR ON A VERTICAL TAIL SECTION OF AN AIRPLANE, WITH THE AID OF AI C. Cordoni¹, A. Saporiti¹, M. Boffadossi¹; ¹DAER, Politecnico di Milano, Via La Masa 34, 20156 Milano, Italy, Italy | ||||
| 11:25 | 11:50 | 6.1.2 |
GENETIC ALGORITHM OPTIMIZATION OF AN OPPOSITION CONTROL STRATEGY IN A FULLY TURBULENT CHANNEL FLOW E. Saccaggi¹, G.M. Di Cicca¹; ¹Politecnico di Torino, Italy | ||||
| 11:50 | 12:15 | 6.1.3 |
FAULT DIAGNOSIS AND TOLERANCE SYSTEM OF FLIGHT STATE PERCEPTION MODEL BASED ON MACHINE LEARNING FOR CO-FLOW JET AIRFOIL Y.-R. Zhao, China; B.-G. Mi, China; H. Zhan, China; H.-Y. Xu, China | ||||
| 12:15 | 12:40 | 6.1.4 |
NUMERICAL INVESTIGATION OF THE FLOW FEATURES ON THE TURRET WITH DIFFERENT CYLINDER HEIGHT IN THE TRANSONIC FLOW X.-T. Tan¹, H.-Y. Xu¹, Z. Pei¹; ¹Northwest Polytechnic University, China | ||||
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| 11:00 | 11:25 | 7.1.1 |
ADVANCING URBAN AIR MOBILITY: COLLABORATIVE EXCELLENCE AND INFRASTRUCTURE INITIATIVES BY DLR O. Bertram¹, B. Schuchardt¹, A. König¹, K. Wendt¹, P. Shiva Prakasha¹; ¹DLR, Germany | ||||
| 11:25 | 11:50 | 7.1.2 |
NASA’S ADVANCED AIR MOBILITY RESEARCH P.H. Kopardekar, United States | ||||
| 11:50 | 12:15 | 7.1.3 |
IFAR-X: COLLABORATIVE ENGINEERING FRAMEWORK FOR NEXT GENERATION OF AEROSPACE ENGINEERS WORKING ON AIRCRAFT DESIGN S. Garg¹, A.M.P. Silva², P.F. Albuquerque², E. Nguyen Van, The French Aerospace Lab (Onera), France; K. Kimura³, Y. Sugioka³, M. Jacinto¹, P. Shiva Prakasha¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany ;²Centre of Engineering and Product Development (CEiiA), Portugal ;³Japan Aerospace Exploration Agency (JAXA), Japan | ||||
| 12:15 | 12:40 | 7.1.4 |
AIRCRAFT WING STRUCTURAL SIZING COMPUTATIONAL TOOL TAILORED FOR A COLLABORATIVE MULTIDISCIPLINARY DESIGN FRAMEWORK P.F. Albuquerque¹, A.M.P. Silva¹, A. Pereira¹; ¹CEiiA, Portugal | ||||
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| 11:00 | 11:25 | 8.1.1 |
EXPERIMENTAL AND NUMERICAL INVESTIGATION OF A STRUCTURAL-DYNAMICALLY SCALED DELTA WING WITH TRAINING EDGE FLAPS K. Bantscheff¹, F. Santelli¹, C. Breitsamter¹; ¹Technische Universität München / Lehrstuhl für Aerodynamik, Germany | ||||
| 11:25 | 11:50 | 8.1.2 |
EVALUATION OF WIND TUNNEL TEST RESULTS OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) N. Kishimoto, Kwansei Gakuin University, Japan; D. Wada¹, M. Tamayama¹, Y. Iwami², N. Tomita², T. Ikeda³, Y. Tanahashi³, K. Katagiri, Hiroshima University, Japan; ¹JAXA, Japan ;²Yamashina Institute of Ornithology, Japan ;³Chubu University, Japan | ||||
| additional information (interactive) | 8.1.R |
EXPLORING WINGTIP COLUMNAR VORTEX GENERATORS FOR UAV PERFORMANCE ENHANCEMENT R. Bardera¹, A.A. Rodríguez-Sevillano², J.C. Matías¹, E. Barroso¹, M. Ojeda², J. Fernández²; ¹Instituto Nacional de Técnica Aeroespacial (INTA)., Spain ;²Escuela Técnica Superior de ingeniería Aeronáutica y del Espacio, Spain | |||||
| additional information (interactive) | 8.1.R |
INFLUENCE OF REINFORCED TRAILING EDGE ON FLAPPING WING AERODYNAMIC FORCE AND DEFORMATION Y.-F. Wang¹, B.-F. Song¹, Y. Luo¹, X.-Y. Lang¹, W. Wang¹; ¹Northwestern Polytechnical University, China | |||||
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| 11:00 | 11:25 | 9.1.1 |
EFFICIENT THERMOMECHANICAL SIMULATION FOR METALLIC LATTICE STRUCTURES FABRICATED BY ADDITIVE MANUFACTURING N. Tsushima, Japan Aerospace Exploration Agency, Japan; M. Kita¹, I. Matsubara¹, M. Ohishi, Ryoyu Systems Co., Ltd., Japan; R. Higuchi, 2The University of Tokyo, Japan; K. Yamamoto¹; ¹3Cybernet Systems Co., Ltd., Japan | ||||
| 11:25 | 11:50 | 9.1.2 |
USE OF GRAPHENE MATERIAL IN AIRCRAFT STRUCTURE FOR LIGHTNING STRIKE PROTECTION P. Jha¹, V.M. Sharma¹, V. Samanyusree¹, A. Sharma¹, S. Maheshwari¹; ¹R. V. College of Engineering, India | ||||
| 11:50 | 12:15 | 9.1.3 |
EFFECT OF LASER PRINTING MODE ON SURFACE TOPOGRAPHY, MICROSTRUCTURE AND CORROSION PROPERTY OF ADDITIVE-MANUFACTURED NITI X. Liu¹, D. Gu¹; ¹Nanjing University of Aeronautics and Astronautics, China | ||||
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| 11:00 | 11:25 | 10.1.1 |
TOWARDS EFFICIENT ANALYSIS OF POSTBUCKLING IN AIRCRAFT STIFFENED STRUCTURES M.H. Elalfy¹, R. de Breuker¹, S.G.P. Castro¹; ¹TU Delft, Netherlands | ||||
| 11:25 | 11:50 | 10.1.2 |
CONCEPTUAL DESIGN AND TOPOLOGY OPTIMIZATION OF A COMPLIANT MORPHING FLAP FOR NEXT GENERATION HYBRID-ELECTRIC REGIONAL AIRCRAFT M.C. Noviello¹, I. Dimino¹, S. Ameduri¹, A. Concilio¹; ¹The Italian Aerospace Research Centre (CIRA), Italy | ||||
| 11:50 | 12:15 | 10.1.3 |
HIGH-VELOCITY DROPLET IMPACT STUDIES ON C/SIC AND C/C COMPOSITES Y. Yue¹, R. Zhao¹, B. Wang¹, Y. Li, Shaanxi Key Laboratory of Impact Dynamics and Engineering Applic, China; ¹School of Aeronautics, Northwestern Polytechnical University, China | ||||
| 12:15 | 12:40 | 10.1.4 |
Lecture canceled | ||||
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| 11:00 | 11:25 | 11.1.1 |
POTENTIAL LIMITS OF LOAD ALLEVIATION IN REDUCING THE STRUCTURAL MASS OF A LONG-RANGE TRANSPORT CONFIGURATION V. Handojo¹, S. Puelm¹; ¹DLR German Aerospace Center, Germany | ||||
| 11:25 | 11:50 | 11.1.2 |
CLOSED-LOOP GUST LOADS ANALYSIS OF A SUPERSONIC FIGHTER AIRCRAFT A. Voß¹, J. Baier¹; ¹DLR Institute of Aeroelasticity, Germany | ||||
| 11:50 | 12:15 | 11.1.3 |
DYNAMIC DROP SIMULATION OF THE MAIN LANDING GEAR OF A GENERAL AVIATION AIRCRAFT N. Li¹, H. Wang¹, Z.Q. Li¹, Z.H. Wang¹; ¹Taiyuan University of Technology, China | ||||
| 12:15 | 12:40 | 11.1.4 |
TRADE OFF STUDIES ON WING MANEUVER LOAD ALLEVIATION STRATEGIES BASED ON AILERONS AND WINGLETS MOVABLE SURFACES R. Pecora, University of Naples Federico II, Italy | ||||
| additional information (interactive) | 11.1.R |
FLIGHT LOADS RESEARCH OF TWIN VERTICAL TAIL FOR BLENDED WING-BODY AIRCRAFT BASED ON STRAIN GAUGE CAILBRATION Z. Guo¹, A. Tang¹, Q. Jing¹; ¹Chinese Flight Test Estsblishment, China | |||||
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| 11:00 | 11:25 | 12.1.1 |
EFFECTS OF SHOCK IMPINGEMENT LOCATION ON PANEL AEROELASTIC STABILITY IN MACH REFLECTION Y. He¹, A. Shi¹; ¹Northwestern Polytechnical University, China | ||||
| 11:25 | 11:50 | 12.1.2 |
PARAMETERISATION OF NONLINEAR AEROELASTIC REDUCED ORDER MODELS WITH AERODYNAMIC AND STRUCTURAL NONLINEARITY M. Candon¹, E. Hale¹, M. Balajewicz, Independent Researcher, United States; A. Delgado-Gutierrez¹, V. Muscarello¹, P. Marzocca¹; ¹RMIT University, Australia | ||||
| 11:50 | 12:15 | 12.1.3 |
EFFICIENT MULTI-FIDELITY REDUCED-ORDER MODELING FOR FLUTTER PREDICTIONS ACROSS MULTIPLE MACH NUMBERS X. Wang¹, X. Peng¹, H. Liu¹, J. Kou¹, W. Zhang¹; ¹Northwestern Polytechnical University, China | ||||
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| 11:00 | 11:25 | 13.1.1 |
FAST PREDICTION METHOD FOR RADIAL GROWTH OF LABYRINTH SEAL CLEARANCE BASED ON TRANSIENT THERMAL-FLUID COUPLING NETWORK Z. Li¹, C. Liu¹, P. Liu¹, Y. Wang¹, X. Jin¹, S. Ding¹; ¹Research Institute of Aero-Engine, Beihang University, China | ||||
| 11:25 | 11:50 | 13.1.2 |
BASE FLOW CHARACTERISTICS FOR A SUB-SCALE HIGH-SPEED EXHAUST AT OVER-EXPANDED MODE S. Tsentis¹, I. Goulos¹, S. Prince¹, V. Pachidis¹, V. Zmijanovic, Reaction Engines Ltd, United Kingdom; ¹Cranfield University, United Kingdom | ||||
| 11:50 | 12:15 | 13.1.3 |
EXPERIMENTAL AND NUMERICAL INVESTIGATIONS OF A SWIRL-STABILIZED JET ENGINE COMBUSTOR B.O. Cakir¹, D. Sanned¹, P. Vauquelin¹, M. Prakash¹, J.-P. Hannappel¹, A. Subash¹, M. Richter¹, X.-S. Bai¹, C. Fureby¹; ¹Lund University, Sweden | ||||
| 12:15 | 12:40 | 13.1.4 |
PERFORMANCE ASSESSMENT OF AN ENGINE-INTEGRATED CLOSED-AIR COOLING THERMAL MANAGEMENT SYSTEM IN A NEXT GENERATION FIGHTER CONFIGURATION T. Matuschek¹, J. Häßy¹, M. Schmelcher¹, A. Görtz¹; ¹German Aerospace Center (DLR), Germany | ||||
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| 11:00 | 11:25 | 14.1.1 |
RESEARCH RESULTS AND PERSPECTIVES ON NON-COOPERATIVE SENSING FOR SAFE UAM OPERATIONS F. Vitiello¹, F. Causa¹, R. Opromolla¹, G. Fasano¹; ¹University of Naples Federico II, Italy | ||||
| 11:25 | 11:50 | 14.1.2 |
SENSOR UNCERTAINTY MITIGATION FOR DETECT AND AVOID SYSTEMS E. Theunissen, Netherlands Defence Academy, Netherlands | ||||
| 11:50 | 12:15 | 14.1.3 |
PRELIMINARY APPLICATION OF FORMAL VERIFICATION TO AN AUTONOMY ARCHITECTURE FOR UNMANNED AIRCRAFT L.R. Humphrey¹, C.A. Muñoz¹; ¹NASA, United States | ||||
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| 11:00 | 11:25 | 15.1.1 |
A TIERED CONTINUOUS CULTIVATING SYSTEM FOR AVIATION TECHNOLOGY TALENTS THAT INTEGRATES STEM AND POPULAR SCIENCE EDUCATION J. Li¹, Y. He, Sichuan Technical Exchange Center, China; X.H. Tang, School of Public Administration, Sichuan University, China; Y.M. Zhou¹, W.F. Huo², J. Zhang², K. Lin², Y. Luo, Mao County Innovation Institute of Intelligent Aircraft Engineer, China; M. Ling, Chenghang Innovation Institute of Intelligent Aerocraft, Chengdu, China; ¹School of Aeronautic Science and Engineering, Beihang University, China ;²Chengdu Xueshang Technology Co., Ltd, China | ||||
| 11:25 | 11:50 | 15.1.2 |
DESIGN BUILD AND FLY: A STUDENT APPROACH TO THE CREATION OF AN RC DRONE FOR UNIVERSITY COMPETITION E. Gaspari¹, E. Bianchini¹, L. Pezzullo¹, A. Giorgi¹, M. Giannetti¹, D.M. Macchini¹, L. Ferrarini¹, F. Bondanese¹, S. Celli¹, T. Strafforello¹, U. Mignemi¹, A. Arnaldi¹, M. Ferrazzani¹, M. Sanna¹, D. Geraci¹, M.R. Chiarelli¹, A.A. Quarta¹, G. Palaia¹, L. Boni¹; ¹University of Pisa, Department of Civil and Industrial Engineeri, Italy | ||||
| 11:50 | 12:15 | 15.1.3 |
MICKEY MOUSE AND A GIANT: COMPARISON OF AERONAUTICS EDUCATION IN FINLAND AND CHINA M. Kanerva¹, Y. Zhang, Tsinghua University, China; R. Yondo Mine¹, L. Qiu, Beihang University, China; M. Wang, BIT, China; ¹Tampere University, Finland | ||||
| 12:15 | 12:40 | 15.1.4 |
DESIGN AND VISUALIZATION OF A KNOWLEDGE-BASED AIRCRAFT CABIN IN VIRTUAL REALITY F. Prokic¹, C. Eriksson¹, R.C. Munjuluru¹; ¹Linköping University, Sweden | ||||
| additional information (interactive) | 15.1.R |
DESIGNING A FRAMEWORK FOR FLIGHT SIMULATOR TRAINING SCENARIOS. AN EVIDENCE BASED TRAINING APPROACH. G. Kontos¹, O. Lehmann¹; ¹Abu Dhabi University, United Arab Emirates | |||||
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| 11:00 | 11:25 | 16.1.1 |
COMPARATIVE ANALYSIS OF MACHINE LEARNING ALGORITHMS FOR HEAT EXCHANGERS DIAGNOSIS IN ELECTRIFIED AIRCRAFT D.F. Migliore¹, G. D'Alessio², S. Caggese², A. De Martin², F. Acerra¹, M. Sorli², M. Fioriti²; ¹Leonardo S.p.A., Italy ;²Politecnico di Torino, Italy | ||||
| 11:25 | 11:50 | 16.1.2 |
APPLICATION OF NATURAL LANGUAGE PROCESSING FOR AIRCRAFT DEFECT TRACKING IN MAINTENANCE OPERATIONS M.J. Scott¹, O. Kirkpatrick¹, W. Verhagen¹, V. Kekoc, Defence Science and Technology Group, Australia; B. Teunisse, Capability Acquisition and Sustainment Group, Australia; J. Zhang¹, H. Fayek¹, P. Marzocca¹; ¹RMIT University, Australia | ||||
| 11:50 | 12:15 | 16.1.3 |
TOWARDS TRUSTWORTHY DATA-DRIVEN GAS TURBINE PROGNOSTICS A. Apostolidis¹, S. Le Dantec, SIGMA Clermont, France; K.P. Stamoulis¹; ¹Amsterdam University of Applied Sciences, Netherlands | ||||
| 12:15 | 12:40 | 16.1.4 |
FASTVIBE SW TOOL FOR RIDE-ALONG VIBRATION SURVEY ANALYSIS S. Bianchi¹, F. Negroni¹, M. Riganti¹; ¹Leonardo Aircraft Division, Italy | ||||
| additional information (interactive) | 16.1.R |
LIFE CYCLE ASSESSMENT OF ALTERNATIVE LAUNCH METHODS S. Wildermuth¹, W. Veraburenon¹, T. Bellier¹, C. Bil¹; ¹RMIT University, Australia | |||||
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| 11:00 | 11:25 | 17.1.1 |
MODEL-BASED DESIGN OF ACTIVE/ACTIVE ELECTRO-HYDROSTATIC ACTUATION FOR HELICOPTER FLIGHT CONTROLS M.-W. Sun¹, J. Fu¹, D.-C. Lyu¹, J.-C. Mare, ICA, INSA-Toulouse, France; ¹Beihang University, China | ||||
| 11:25 | 11:50 | 17.1.2 |
DEVELOPMENT OF AN ELECTRO-HYDROSTATIC NOSE LANDING GEAR ACTUATION AND STEERING SYSTEM M.N. Duval¹, T. Lammering¹; ¹Liebherr-Aerospace Lindenberg GmbH, Germany | ||||
| additional information (interactive) | 17.1.R |
RESEARCH ON MODELING THE TEMPERATURE FIELD OF A NEW AEROSPACE SERVO ELECTRO-HYDROSTATIC MODULE BASED ON THERMO-MAGNETIC BIDIRECTIONAL COUPLING ANALYSIS X. Hu¹, Y. Fu¹, D. Lyu¹, M. Sun¹, S. Zhao, Beijing Institute of Precision Mechatronics and Controls, Labora, China; J. Fu¹, J. Zhao¹; ¹School of Mechanical Engineering and Automation, Beihang Univers, China | |||||
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| 14:30 | 14:55 | 1.2.1 |
JETZERO: RESHAPING AVIATION WITH THE BLENDED WING S.S. Savian, JetZero, United States | ||||
| 14:55 | 15:20 | 1.2.2 |
X-66: ACCELERATED LEARNING THROUGH FULL SCALE PROTOTYPING B. Cobleigh, NASA (AFRC), United States; E. Kaduce, Boeing, United States | ||||
| 15:20 | 15:45 | 1.2.3 |
BOMBARDIER ECOJET RESEARCH PROJECT; THE QUEST FOR SUSTAINABLE AVIATION S. McCullough, Bombardier, Canada | ||||
| 15:45 | 16:10 | 1.2.4 |
Q&A - MINI PANEL Q&A. A, | ||||
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| 14:30 | 14:55 | 2.2.1 |
IMPACT OF HYDROGEN FUEL ON OVERALL DESIGN OF TRANSPORT AIRCRAFT E. Nguyen Van¹, J. Gauvrit-Ledogar¹, C. Julien², B. Paluch², J.L. Ruan, ONERA/DMPE, France; F. Moens, ONERA/DAAA, France; ¹ONERA/DTIS, France ;²ONERA/DMAS, France | ||||
| 14:55 | 15:20 | 2.2.2 |
A PERFORMANCE COMPARISON OF HYDROGEN AIRCRAFT CONCEPTS N. Wood¹, S. Taylor¹, M. Hales¹, M. Joynt¹, S. Chandran¹, D. Sanjeevekumar¹; ¹GKN AEROSPACE, United Kingdom | ||||
| 15:20 | 15:45 | 2.2.3 |
PRELIMINARY SIZING OF HYDROGEN-BURNING JETLINER FOR DIRECT OPERATING COST OPTIMIZATION H. Mohammadi¹, G. Sirtori¹, L. Trainelli¹; ¹DAER, Politecnico di Milano, Italy | ||||
| 15:45 | 16:10 | 2.2.4 |
INVESTIGATING THE FLEXIBLE HYDROGEN AIRCRAFT SYSTEM INTERFACE DESIGN USING THE XR CO-DESIGN APPROACH F. Reimer¹, M. Fuchs¹, J. Herzig¹, S. Cornelje¹, J. Biedermann¹, B. Nagel¹; ¹DLR, Germany | ||||
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| 14:30 | 14:55 | 3.2.1 |
A MORPHOLOGICAL ANALYSIS OF METHODS FOR CONCEPTUAL AIRCRAFT DESIGN UNDER UNCERTAINTIES V.T. Todorov¹, D. Rakov, Blagonravov Institute of Engineering Science, Russia; A. Bardenhagen¹; ¹Technical University of Berlin, Germany | ||||
| 14:55 | 15:20 | 3.2.2 |
NUMERICAL AND THEORETICAL INVESTIGATION OF HELICOPTER DITCHING WITH VARIOUS INITIAL VELOCITY AND PITCHING ANGLE L. Zheng¹, M. Wang², Y. Lu², H. Qiao¹, T. Xiao¹, S. Deng¹; ¹Nanjing University of Aeronautics and Astronautics, China ;²Chinese Aeronautical Establishment, China | ||||
| 15:20 | 15:45 | 3.2.3 |
MAXIMUM SPEED OF BATTERY-POWERED TILT-ROTOR AIRCRAFT N. Roh¹, M. Park¹; ¹Hanwha systems, South Korea | ||||
| 15:45 | 16:10 | 3.2.4 |
EFFICIENT MULTI-OBJECTIVE DESIGN OPTIMIZATION OF ROTOR AIRFOILS FOR IMPROVING DYNAMIC STALL CHARACTERISTICS Z. Lu¹, Z.-H. Han¹, W.-P. Song¹, K.-S. Zhang¹, K.-Y. Zhou¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | ||||
| Reserve Paper | 3.2.R |
AN UNCERTAINTY MULTIDISCIPLINARY PROPAGATION ANALYSIS METHOD FOR CORRELATED HIGH-DIMENSIONAL DATA IN AIRCRAFT DESIGN S. Du, China; C. Li, China; Y. Liu, China | |||||
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| 14:30 | 14:55 | 4.2.1 |
COLOSSUS EU PROJECT – COLLABORATIVE SOS EXPLORATION OF AVIATION PRODUCTS, SERVICES AND BUSINESS MODELS: OVERVIEW AND APPROACH P. Shiva Prakasha¹, N. Naeem¹, K. Amadori, SAAB Aeronautics, Sweden; G. Donelli¹, J. Akbari¹, F. Nicolosi, UNINA, Italy; L. Knöös Franzen, Linkoping University, Sweden; M. Ruocco, Smartup Engineering, Italy; T. Lefebvre, The French Aerospace Lab, France; B. Nagel¹; ¹German Aerospace Center - DLR, Germany | ||||
| 14:55 | 15:20 | 4.2.2 |
A SYSTEM OF SYSTEMS AIRCRAFT DESIGN FRAMEWORK: DEMONSTRATION USING A SEAPLANE TRANSPORT NETWORK IN THE GREEK ISLANDS V. Nugnes¹, C. Varriale, TU Delft, Italy; P. Ratei¹, P. Shiva Prakasha¹, B. Nagel¹; ¹DLR, Italy | ||||
| 15:20 | 15:45 | 4.2.3 |
CONCEPT OF OPERATIONS IN AN AGENT-BASED SIMULATION: A SYSTEM-OF-SYSTEMS APPROACH F. Villas¹, L. Knöös Franzén¹, C. Jouannet², K. Amadori², I. Staack, TU Braunschweig, Germany; ¹Linköping University, Sweden ;²Saab Aeronautics, Sweden | ||||
| 15:45 | 16:10 | 4.2.4 |
SYSTEM OF SYSTEMS ANALYSIS OF AUTONOMOUS AIRCRAFT OPERATIONS IN AIR CARGO FEEDER NETWORKS P.W. Jansen¹, R.E. Perez¹, J.C.-H. Wang, Ribbit Inc, Canada; ¹Royal Military College of Canada, Canada | ||||
| Reserve Paper | 4.2.R |
TECHNICAL RISK MANAGEMENT OF SYSTEM OF SYSTEMS BASED ON TECHNOLOGY READINESS ASSESSMENT H. Cao¹, W. Cheng¹, C. Xing, Chinese Aeronautics Establishment (CAE), China; G. Song¹; ¹ Aviation Industry Development Research Center of China (ADR) , China | |||||
| additional information (interactive) | 4.2.R |
RESEARCH ON ROUTE PLANNING METHOD FOR UAV SWARM AREA COVERAGE MISSIONS BASED ON COMPLEX NETWORKS X. Li¹, L. Deng¹, Y. Ge¹, Y. Pei¹, Y. Gu², L. Cao², A. Shi¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China ;²Shanghai Electro-Mechanical Engineering Institute, China | |||||
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| 14:30 | 14:55 | 5.2.1 |
GRID EFFECT ON M823 BOMB AT TRANSONIC REGIME J. Jiménez-Varona¹, G. Liaño¹; ¹INTA, Spain | ||||
| 14:55 | 15:20 | 5.2.2 |
LOW SPEED AERODYNAMICS OF SIX OPTIMISED UNCONVENTIONAL RE-ENTRY VEHICLE AEROSHAPES S.M. Giannino¹, G. Pezzella¹, A. Viviani¹; ¹Università della Campania Luigi Vanvitelli, Italy | ||||
| 15:20 | 15:45 | 5.2.3 |
SCALE EFFECT ON WATER LANDING PERFORMANCE OF AMPHIBIOUS AIRCRAFT H. Zhang¹, J. Chen², F. Wang¹, G. Zhang¹, Z. Shen, Aircraft Strength Research Institute of China, China; Q. Zhu, China Special Vehicle Research Institute, China; G. Wu, Commercial Aircraft Corporation of China Ltd, China; M. Tong²; ¹Jinling Institute of Technology, China ;²Nanjing University of Aeronautics and Astronautics, China | ||||
| 15:45 | 16:10 | 5.2.4 |
ANALYSIS OF SUCTION FORCE EFFECT ON DIFFERENT FUSELAGE SHAPE DURING THE WATER DITCHING J.-Y. Li¹, X.-Y. Wang, Shanghai Electro-Mechanical Engineering Institute, China; J.-C. Chen¹, J. Jiao, China Special Vehicle Research Institute, China; M.-B. Tong¹, C.-L. Yan, Beijing University Of Aeronautics And Astronautics, China; ¹Nanjing University Of Aeronautics And Astronautics, China | ||||
| additional information (interactive) | 5.2.R |
APPLICATION OF ARTIFICIAL NEURAL NETWORK (ANN) FOR PREDICTION OF DRAG COEFFICIENT OF AXISYMMETRIC BOATTAIL MODELS Q. Nguyen Dinh¹, H. Tran The¹, G. Sharma², J. Tanimoto²; ¹Le Quy Don Technical University, Vietnam ;²Kyushu University, Japan | |||||
| additional information (interactive) | 5.2.R |
SEPARATION SAFETY ANALYSIS IN VARIABLE LAUNCH CONDITION OF SMALL AIR-LAUNCHED UAVS BASED ON NUMERICAL SIMULATION AND FLIGHT TEST B. Guo¹, Y.F. Lu¹, B. Wang, Chinese Academy of Military Science, China; Z. Guo¹, G.W. Jia¹, D.N. Liu¹; ¹National University of Defense Technology, China | |||||
| additional information (interactive) | 5.2.R |
RESEARCH ON AERODYNAMIC PERFORMANCE OF OVERSIZE MODULAR PARAFOIL IN RANDOM WIND FIELD F. Duan¹, J.-Y. Li¹, Z.-D. Li, Aerospace Life-support Industries Ltd, China; M.-B. Tong¹; ¹Nanjing University of Aeronautics and Astronautics, China | |||||
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| 14:30 | 14:55 | 6.2.1 |
PASSIVE FLOW CONTROL DEVICES ON LOW-REYNOLDS DU89-134 AIRFOIL C. Brunelli¹, M. Avirovic¹, B. Janssens¹, B.G. Marinus¹, M. Runacres, Vrije Universiteit Brussel, Belgium; G. May, Von Karman Institute for Fluid Dynamics, Belgium; A. Ecorce², A. Dalbera²; ¹Royal Military Academy, Belgium ;²National Polytechnic Institute of Toulouse , France | ||||
| 14:55 | 15:20 | 6.2.2 |
RESEARCH ON UNSTEADY AERODYNAMIC MODELING METHOD OF PREPOSITIVE WING - MAIN WING COMPOSITE SYSTEM AT HIGH ATTACK ANGLE X. Bai, China; B. Mi, China; J. Zhang, China | ||||
| 15:20 | 15:45 | 6.2.3 |
MITIGATING DYNAMIC STALL WITH A MOVABLE LEADING-EDGE: THE NACA0012-IK30 WING E.A.R. Camacho¹, A.R.R. Silva¹, F.D. Marques, Universidade de São Paulo, Brazil; ¹Universidade da Beira Interior, Portugal | ||||
| 15:45 | 16:10 | 6.2.4 |
NUMERICAL STUDY ON ACTIVE FLOW CONTROL SOLUTIONS FOR HIGH LIFT P. Scavella¹, G. Paolillo¹, T. Astarita¹, G. Cardone¹, C.S. Greco¹; ¹University of Study of Naples Federico II, Italy | ||||
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| 14:30 | 14:55 | 7.2.1 |
AERODYNAMIC NUMERICAL/EXPERIMENTAL COMPARISON OF A HYPERSONIC TEST VEHICLE IN MORE&LESS PROGRAM P. Roncioni¹, M. Marini¹, R. Fusaro², N. Viola², D. Pepelea, INCAS, Romania; B. Cakir, VKI, Belgium; M. Clay, REL, United Kingdom; ¹CIRA, Italy ;²POLITO, Italy | ||||
| 14:55 | 15:20 | 7.2.2 |
ANALYSIS ON COMPLEX HYPERSONIC FLOW DURING THE REENTRY OF EXPIRED SPACECRAFT Z. Han¹, Z.-H. Li, National Laboratory for Computational Fluid Dynamics, China; S.-Y. Chu¹, W.-Y. Cheng¹, C.-S. Wang¹; ¹Aviation Industry Development Research Center of China, China | ||||
| 15:20 | 15:45 | 7.2.3 |
ASSESSMENT OF A MACROSCOPIC MODEL FOR THE AEROTHERMODYNAMICS CHARACTERIZATION OF ICE GIANTS ATMOSPHERIC ENTRY D. Ninni¹, F. Bonelli¹, A. Laricchiuta², G. Colonna², G. Pascazio¹; ¹Politecnico di Bari, Italy ;²CNR ISTP Bari, Italy | ||||
| 15:45 | 16:10 | 7.2.4 |
KINETIC MONTE CARLO BASED CATALYTIC VISCOUS WALL BOUNDARY MODELING IN CFD SIMULATION OF HIGH-ENTHALPY NON-EQUILIBRIUM FLOW Q. Li¹, X. Yang², W. Dong¹, Y. Du²; ¹Shanghai Jiao Tong University, China ;²China Aerodynamics Research and Development Center, China | ||||
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| 14:30 | 14:55 | 8.2.1 |
EVALUATING INSTALLATION EFFECTS IN SEMI-SPAN WIND TUNNEL EXPERIMENTS USING CARTESIAN-GRID-BASED FLOW SOLVER UTCART Y. Tamaki¹, Y. Yokoyama¹, T. Imamura¹; ¹The University of Tokyo, Japan | ||||
| 14:55 | 15:20 | 8.2.2 |
CHARACTERIZATION OF EXTERNAL LIQUID HYDROGEN TANK INTERFERENCE DRAG C. Graham¹, R.E. Perez¹; ¹Royal Military College of Canada, Canada | ||||
| 15:20 | 15:45 | 8.2.3 |
WIND TUNNEL ANALYSIS OF A SPACE RE-ENTRY VEHICLE AT LOW-SPEED CONDITIONS N. Montella, University of Campania/ CIRA, Italy; G.A. Vio, The University of Sydney, Australia; L. Iuspa¹, A. Aprovitola¹, G. Pezzella, University of Campania , Italy; A. Viviani¹; ¹University of Campania, Italy | ||||
| 15:45 | 16:10 | 8.2.4 |
DESIGN OF A HIGHLY EFFICIENT TRANSPORT NLF AIRCRAFT WITH A BACKWARD SWEPT WING AND A LONG SINGLE-AISLE FUSELAGE T. Streit¹, J. Ruberte Bailo¹, A. Büscher, Airbus Operations GmbH, Germany; A. Seitz¹; ¹DLR (GERMAN AEROSPACE CENTER), Germany | ||||
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| 14:30 | 14:55 | 9.2.1 |
WHAT-IF SCENARIO ANALYSIS OF REGIONAL AIR MOBILITY OPERATIONS IN SOUTH KOREA J.C. Lee¹, S.K. Kim, Georgia Institute of Technology, South Korea; S.M. Ahn¹, J.H. Kim, Sejong University, South Korea; ¹Handong Global University, South Korea | ||||
| 14:55 | 15:20 | 9.2.2 |
DEVELOPMENT OF LOW ALTITUDE 4-DIMENSIONAL OPERATIONS MANAGEMENT SYSTEM FOR ADVANCED AIR-MOBILITY T. Iijima¹, N. Matayoshi¹, N. Yokoyama¹, H. Yoshida¹, A. Oosedo¹, S. Kikkawa¹, M. Yawata², S. Nakada², T. Yahata²; ¹JAXA, Japan ;²NEC, Japan | ||||
| 15:20 | 15:45 | 9.2.3 |
EXPLORING RIDESHARING IN PASSENGER URBAN AIR MOBILITY: A COMPARATIVE ANALYSIS A. Edsel¹, S.D. Biswas¹, M. Kilbourne¹, R. Gadre¹, S. Vashi¹, K. Mall¹, W.A. Crossley¹, D.A. DeLaurentis¹, M.D. Patterson², B.E. Sells²; ¹Purdue University, United States ;²NASA Langley Research Center, United States | ||||
| 15:45 | 16:10 | 9.2.4 |
CLASSIFICATION OF EXTENDED REALITY BASED HUMAN MACHINE INTERFACES SCENARIOS FOR URBAN AIR MOBILITY M. Gomes Araujo¹, C. Conte², F. De Crescenzio¹, D. Accardo²; ¹University of Bologna, Italy ;²University of Naples Federico II, Italy | ||||
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| 14:30 | 14:55 | 10.2.1 |
DEMOCRATIZATION OF FATIGUE EVALUATION FOR REALISTIC RIVETING CONFIGURATIONS USING STATE-OF-THE-ART SIMULATIONS I. Rivero¹, A. Palomar¹, M. Rebollo¹, J. Domingo¹, M. Lozano¹, Z. Mujika¹, D. Garijo¹, G. Lara¹, A. Capitan¹, J. Gomez-Escalonilla¹; ¹Airbus, Spain | ||||
| 14:55 | 15:20 | 10.2.2 |
THE FATIGUE LIFE PREDICTION OF THIN-WALLED WELDED JOINTS M. Sladky¹, M. Machac², J. Papuga², I. Jebacek¹; ¹Faculty of Mechanical Engineering, Brno University of Technology, Czech Republic ;²Faculty of Mechanical Engineering, Czech Technical University, Czech Republic | ||||
| 15:20 | 15:45 | 10.2.3 |
SURFACE QUALITY CHALLENGE FOR TI-6AL-4V ADDITIVE MANUFACTURED TOPOLOGIC OPTIMIZED LIGHTWEIGHT STRUCTURE C. Matias¹, A. Diskin¹, O. Golan, Afeka- Tel-Aviv Academic College of Engineering, Israel; A. Garkun², E. Strokin²; ¹Israel Aerospace Industries, Israel ;²Technion Research & Development Foundation, Israel | ||||
| 15:45 | 16:10 | 10.2.4 |
INTEGRATIVE ANALYSIS OF LOW-CYCLE FATIGUE AND CRACK PROPAGATION IN TURBINE BLADES N.M. Hoang¹, M.D. Ha¹, T.Q. Nguyen¹, P.M. Nguyen¹; ¹Viettel Aerospace Institute, Vietnam | ||||
| additional information (interactive) | 10.2.R |
STUDY ON FATIGUE PROPERTIES OF TITANIUM ALLOY BASE MATERIAL AND WELDED STRUCTURE IN THERMAL COMBINED ENVIRONMENT H. Peng¹, B. Wang¹, Y. Zhang¹, L. Ji¹, S. Li¹; ¹AVIC the First Aircraft Institute, China | |||||
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| 14:30 | 14:55 | 11.2.1 |
NUMERICAL METHOD TO DETERMINE STRUCTURAL ELEMENT REDUCED STIFFNESS FOR DESIRED COMPOSITE WING STRUCTURES CONFIGURATIONS S. Stammel¹, C. Bisagni¹; ¹Politecnico di Milano, Italy | ||||
| 14:55 | 15:20 | 11.2.2 |
SEMI-ANALYTICAL SENSITIVITY METHODS FOR AEROELASTIC SHAPE OPTIMIZATION G.M. Gagliardi¹, M.D. Kulkarni, Embry-Riddle Aeronautical University, United States; F. Marulo¹; ¹University of Naples Federico II, Italy | ||||
| 15:20 | 15:45 | 11.2.3 |
ABSOLUTE NODAL COORDINATE FORMULATION FOR NONLINEAR MULTIBODY MODELING OF FLARED HINGED WINGS K. Otsuka, Tohoku University, Japan; C.W. Cheng¹, R. Palacios¹; ¹Imperial College London, United Kingdom | ||||
| 15:45 | 16:10 | 11.2.4 |
OPTIMIZATION DESIGN OF MULTI-SCALE ACTIVE COOLING STRUCTURE FOR AIRCRAFT P. Xu¹, Q.-X. Mu¹, W.-N. Zhang¹; ¹AVIC Shenyang Aircraft Design and Research Institute, China | ||||
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| 14:30 | 14:55 | 12.2.1 |
COMPUTATIONAL/EXPERIMENTAL AEROELASTIC STUDY FOR AN ALL-MOVABLE HORIZONTAL TAIL WITH TORSION FREE-PLAY X.-Y. Ai, China; X.-Y. Chen, China; W.-J. Wang, China; J. Liu, China; X.-J. Ran, China; W. Qian, China | ||||
| 14:55 | 15:20 | 12.2.2 |
NUMERICAL AND EXPERIMENTAL RESEARCH ON AEROELASTICITY OF HIGH-ASPECT-RATIO WINGS J. Liu¹, W. Qian¹, X. Hu¹, X. Ai¹, X. Ran¹; ¹Dalian University of Technology, China | ||||
| 15:20 | 15:45 | 12.2.3 |
W-WING AEROELASTIC DEMONSTRATOR DESIGN MODIFICATION AND UPGRADE J. Cecrdle¹, O. Vich¹, J. Starek¹, J. Vlach¹, M. Kolar¹, M. Smid¹; ¹Czech Aerospace Research Centre (VZLU), Czech Republic | ||||
| 15:45 | 16:10 | 12.2.4 |
MEASUREMENT OF WING BENDING IN-FLIGHT FROM A T67 SLINGSBY FIREFLY LIGHT AIRCRAFT N.J. Lawson, The University of Sydney, Australia; G. Zhao¹, S.C. Place¹, R.A. Harrison¹; ¹Cranfield University, United Kingdom | ||||
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| 14:30 | 14:55 | 13.2.1 |
SUSTAINABLE FUELS SAFETY BOUNDARIES DEMARCATION METHOD T. Qiu¹, S. Bao¹, S. Ding, Civil Aviation University of China, China; Q. Ma¹, X. Wang¹, C. Gan¹; ¹Beihang University, China | ||||
| 14:55 | 15:20 | 13.2.2 |
EFFECTS OF SHAPE AND STREAMWISE SPACING OF PIN-FINS ARRAYS ON FLOW AND HEAT TRANSFER L.W. Li¹, T.L. Dong¹, W.T. Ji¹, J.M. Wu¹; ¹Xi'an Jiaotong University, China | ||||
| 15:20 | 15:45 | 13.2.3 |
MULTI-DIMENTIONAL DESIGN AND THERMAL PROTECTION CAPABILITY OF A REGENERATIVE COOLED RBCC VARIABLE-GEOMETRY COMBUSTOR L. Zhang, China; T.-T. Jing, China; X. Sun, China; T. Gao, China; Z. Xu, China; F. Qin, China | ||||
| 15:45 | 16:10 | 13.2.4 |
NUMERICAL SIMULATION OF HEAT TRANSFER IN MINIATURE RADIALLY ROTATING SODIUM/POTASSIUM HEAT PIPES G. Li, Tianmushan Laboratory, China; Y. Zhang¹, G. Zhang, Beihang University Research Institute of Aero-Engine, China; S. Huang¹, S. Ding, Civil Aviation University of China, China; ¹Beihang UniversitySchool of Energy and Power Engineering, China | ||||
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| 14:30 | 14:55 | 14.2.1 |
VALIDATING ASSUMPTIONS ABOUT PILOT RECOGNITION: A PCM-BASED APPROACH FOR AIRCRAFT CERTIFICATION SAFETY ASSESSMENT PROCESS D.M.C. de Lima¹, D.C. Fernandes¹, M.M. Cardoso Junior¹; ¹Aeronautical Institute of Technology, Brazil | ||||
| 14:55 | 15:20 | 14.2.2 |
THE IMPACT OF PIEZOELECTRIC STACK HEATING ON AIRCRAFT DEICING L. Yuan¹, B. Miao¹, K. Yan¹, C.L. Zhu¹; ¹Nanjing University of Aeronautics and Astronautics, China | ||||
| 15:20 | 15:45 | 14.2.3 |
HANDLING QUALITIES RATING SCALE: THE IMPACT OF THE PILOT SUBJECTIVITY IN WORKLOAD EVALUATION M.D. Turazza¹, J.P.C.A Macedo ¹, J.H. Bidinotto¹; ¹EESC/USP, Brazil | ||||
| 15:45 | 16:10 | 14.2.4 |
CLASSIFICATION OF COGNITIVE LOAD BASED ON THE PILOT’ VISUAL SCAN PATTERNS J. Yao, China; Y. Lu, China; Z. Zhong, China; S. Fu, China | ||||
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| 14:30 | 14:55 | 15.2.1 |
LINEAR QUADRATIC PURSUIT AND EVASION DIFFERENTIAL GAME GUIDANCE STRATEGY WITH OBSTACLE AVOIDANCE X. Wang¹, M. Yang¹, P. Ma¹, T. Chao¹; ¹Harbin Institute of Technology, China | ||||
| 14:55 | 15:20 | 15.2.2 |
LEARNING-BASED FULL-ENVELOPE AUTOPILOT DESIGN BASED ON THE KOOPMAN OPERATOR THEORY Y. Lee¹, J. Kim¹, Y. Kim¹; ¹Seoul National University, South Korea | ||||
| 15:20 | 15:45 | 15.2.3 |
INTEGRATING POST-OPTIMAL SENSITIVITIES INTO SUPERVISED TRAINING OF NEURAL NETWORKS J. Diepolder¹, J.Z. Ben-Asher¹; ¹Technion, Israel | ||||
| 15:45 | 16:10 | 15.2.4 |
PREDICTIVE CONTROL DRIVEN TACTICAL MANEUVERING J. Novák ¹, J. Hanák¹, P. Chudý¹; ¹BUT, Czech Republic | ||||
| additional information (interactive) | 15.2.R |
PURSUIT-BASED LONG-RANGE AIR-TO-AIR MISSILE MIDCOURSE GUIDANCE ROBUST TO CHANGES IN THE PREDICTED IMPACT POINT M. Shin¹, M.-J. Tahk¹, B. Kim¹, C.-H. Lee¹; ¹Korea Advanced Institute of Science and Technology, South Korea | |||||
| additional information (interactive) | 15.2.R |
CONTROL ALLOCATION FOR A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT USING DIFFERENTIAL THRUST C. Döll¹, S. Waitman¹; ¹ONERA, France | |||||
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| 14:30 | 14:55 | 16.2.1 |
HYBRID MODELING APPROACH FOR OPTIMIZATION BASED CONTROL OF MULTIROTOR UNMANNED AERIAL VEHICLES J. Novák ¹, J. Hanák¹, P. Chudý¹; ¹BUT, Czech Republic | ||||
| 14:55 | 15:20 | 16.2.2 |
MEDIAL AXIS TRANSFORMATION-BASED CONVEX MODEL PREDICTIVE CONTROL FOR MULTIROTOR INDOOR AUTONOMOUS FLIGHT WITH FIXED ALTITUDE H.J. Ahn¹, H.C. Bang¹; ¹KAIST, South Korea | ||||
| 15:20 | 15:45 | 16.2.3 |
AERODYNAMIC MODEL IDENTIFICATION OF A VTOL TAILSITTER UAV USING SPARSE IDENTIFICATION OF NONLINEAR DYNAMICS H.-S. Lee¹, D.-W. Lee¹, H.-C. Bang¹; ¹KAIST, South Korea | ||||
| 15:45 | 16:10 | 16.2.4 |
ROBUST SLIDING MODE CONTROL FOR UAV FORMATION WITH EXTERNAL DISTURBANCES UNDER EVENT-TRIGGERED STRATEGY L.H. Wang¹, A.J. Li¹, C.Q. Wang¹, Z. Yury, Samara National Research University, Russia; ¹Northwestern Polytechnical University, China | ||||
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| 14:30 | 14:55 | 17.2.1 |
SMART ELECTRIC POWER MANAGEMENT ONBOARD FUTURE AIRCRAFT F. Cuomo¹, C. Musto¹, S. Bozhko, University of Nottingham, United Kingdom; B. Guida, Aeromechs srl, Italy; ¹Leonardo Aircraft, Italy | ||||
| 14:55 | 15:20 | 17.2.2 |
DESIGNING A HARDWARE-IN-THE-LOOP SIMULATION TEST BED FOR AIRCRAFT ENERGY MANAGEMENT APPLICATIONS A. Dell’Amico, Linköping University, Sweden | ||||
| 15:20 | 15:45 | 17.2.3 |
DUAL STAGE BATTERY SIZING AND PERFORMANCE ASSESSMENT ON-BOARD HYBRID ELECTRIC AIRCRAFT A. Wise¹, S. Bozhko¹, S. Yeoh¹, S. Sumsurooah¹, C. Manrique, Leonardo S.p.A, Italy; ¹University of Nottingham, United Kingdom | ||||
| 15:45 | 16:10 | 17.2.4 |
PRELIMINARY ASSESSMENT FOR STRUCTURAL BATTERY COMPONENTS G. di Mauro¹, M. Guida¹, G. Olivares², L.M. Gomez², R. Turco¹, R. Tesser¹, S. Mallardo¹, G. Santagata¹, P. Russo¹; ¹Università degli Studi di Napoli Federico II, Italy ;²Jerry Moran Center for Advanced Virtual Engineering & Testing (A, United States | ||||
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| 16:30 | 17:00 | 1.3.1 |
CLEAN AVIATION SHORT MEDIUM RANGE AIRCRAFT CONCEPT K. Mokaddem, AIRBUS, France | ||||
| 17:00 | 17:30 | 1.3.2 |
TOWARDS ZERO CLIMATE IMPACT AVIATION G. Llewellyn, Airbus, United Kingdom | ||||
| 17:30 | 18:00 | 1.3.3 |
ACCELERATING THE CLEAN FUTURE OF FLIGHT G. Teofili, ZeroAvia, United Kingdom | ||||
| 18:00 | 18:30 | 1.3.4 |
PANEL DISCUSSION PD. D, | ||||
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| 16:30 | 17:00 | 2.3.1 |
CONCEPTUAL AIRCRAFT DESIGN OF A RESEARCH BASELINE WITH DIRECT LIQUID HYDROGEN COMBUSTION M. Kotzem¹, S. Wöhler¹, T. Burschyk¹, C. Hesse¹, S. Hellbrück¹, T. Zill¹; ¹German Aerospace Center (DLR), Germany | ||||
| 17:00 | 17:30 | 2.3.2 |
DESIGN OPTIMISATION OF A BOUNDARY LAYER INGESTION PROPULSOR FOR A MULTI-FUEL HYDROGEN AIRCRAFT A. Battiston¹, A. Magrini¹, R. Ponza¹, E. Benini¹, B. Türkyilmaz², A. Seitz², A. Heidebrecht, TU Delft, Netherlands; ¹hit09, Italy ;²Bauhaus Luftfahrt, Germany | ||||
| 17:30 | 18:00 | 2.3.3 |
MODELLING HYDROGEN FUEL CELL AIRCRAFT IN SUAVE C. Svensson¹, P. Miltén¹, T. Grönstedt¹; ¹Chalmers University of Technology, Sweden | ||||
| 18:00 | 18:30 | 2.3.4 |
PRELIMINARY DESIGN OF A FULL ELECTRIC GENERAL AVIATION AIRCRAFT POWERED WITH FUEL CELL: A CASE STUDY. G. Cafiero¹, P.J. Comunian¹, A. Lerro¹, F. Ponti², A.N. Damiani Ferretti²; ¹Politecnico di Torino, Italy ;²Università di Bologna, Italy | ||||
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| 16:30 | 17:00 | 3.3.1 |
LARGE LANGUAGE MODEL-DRIVEN SIMULATIONS FOR SYSTEM OF SYSTEMS ANALYSIS IN FIREFIGHTING AIRCRAFT CONCEPTUAL DESIGN J.L. Lovaco¹, R.C. Munjulury¹, I. Staack, Technische Universität Braunschweig, Germany; P. Krus, Linköping University, Sweden; ¹Saab Aeronautics & Linköping University, Sweden | ||||
| 17:00 | 17:30 | 3.3.2 |
DATA-DRIVEN MULTI-RANGE MISSION-BASED OVERALL AIRCRAFT CONCEPTUAL DESIGN OPTIMIZATION L.J. Liu¹, D. Kim, Ecole Nationale de l’Aviation Civile, France; C. Reyner¹, R.P. Liem¹; ¹The Hong Kong University of Science and Technology, Hong Kong SAR of China | ||||
| 17:30 | 18:00 | 3.3.3 |
Lecture canceled | ||||
| 18:00 | 18:30 | 3.3.4 |
A DISTRIBUTED UMDO ARCHITECTURE BASED ON SURROGATE MODELS FOR LAUNCH VEHICLE DESIGN Y. Liu¹, C.N. Li¹, C.L. Gong¹; ¹Northwestern Polytechnical University, China | ||||
| additional information (interactive) | 3.3.R |
AIRFOIL PRESSURE PREDICTION BASED ON PHYSICS-INFORMED DEEP LEARNING APPROACH J.Z. Li¹, Y.J. Yang¹, Y.F. Zhang¹; ¹School of Aerospace Engineering, Tsinghua University, China | |||||
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| 16:30 | 17:00 | 4.3.1 |
NAVIGATING COMPLEXITY: ADAPTING AEROSPACE DEVELOPMENT IN A DYNAMIC WORLD C. Jouannet, Saab Aeronautics, Sweden | ||||
| 17:00 | 17:30 | 4.3.2 |
MODELING CARGO DEMAND FOR REGIONAL AIR TRANSPORT NETWORKS IN CANADA AND THE UNITED STATES M.M. Alexiev¹, R.E. Perez¹, P.W. Jansen¹, J.C.-H. Wang, Ribbit Inc., Canada; ¹Royal Military College of Canada, Canada | ||||
| 17:30 | 18:00 | 4.3.3 |
RESEARCH ON UNMANNED CLUSTER RECONNECTION DECISION-MAKING METHOD CONSIDERING RESOURCE SUPPLEMENTATION M. Yao¹, X. Wang¹, L. Kong, Chinese Aeronautical Establishment, China; G. Fu¹, X. Wang¹, J. Yao¹; ¹School of Reliability and Systems Engineering, Beihang Universit, China | ||||
| 18:00 | 18:30 | 4.3.4 |
FROM ONTOLOGY TO SYSTEM ARCHITECTURE: AN MBSE APPROACH TOWARD THE REALIZATION OF URBAN AIR MOBILITY S. Sinha Roy¹, Y. Huang¹, D. Bekdache¹, T.-Y. Fung¹, B. Beck¹, C. Guariniello¹, D. DeLaurentis¹; ¹Purdue University, United States | ||||
| additional information (interactive) | 4.3.R |
EFFECTIVENESS EVALUATION METHOD FOR AVIATION EMERGENCY RESCUE SYSTEM OF SYSTEMS BASED ON EFFECT CHAIN Y.-Z. Wang¹, B.-L. Shang¹, P.-F. Li¹, W.-Z. Liu¹, R.-X. Lin¹, K.-A. Xing¹, Y.-T. Deng¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | |||||
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| 16:30 | 17:00 | 5.3.1 |
IDENTIFICATION METHOD OF LONGITUDINAL COEFFICIENTS BASED ON THE NUMERICAL STUDY OF THE FLOW TOPOLOGY AROUND THE SACCON GEOMETRY B. Isnard¹, G. Tanguy¹, D. Farcy¹, E. Garnier¹, J.-M. Foucault, LMFL, France; ¹ONERA, France | ||||
| 17:00 | 17:30 | 5.3.2 |
AERODYNAMIC CHARACTERISTICS RESEARCH OF A DISTRIBUTED PROPULSION AIRCRAFT S. Chen¹, Z. Guo¹, G. Jia¹, D. Liu¹; ¹National University of Defense Technology, China | ||||
| 17:30 | 18:00 | 5.3.3 |
HYDRODYNAMIC ANALYSIS OF STATIC WATER IMPACT ON WEDGE-SHAPED HULL WATERTIGHT TEST SPECIMEN THROUGH NUMERICAL ANALYSIS M. Niu, Northwestern Polytechnical University, China; F. Sun, Xi'an Modern Control Technology Research Institute, China; C. Du, AVIC XAC COMMERCIAL AIRCRAFT CO., LTD., China; H. Huang, Northwestern Polytechnical University/Aircraft Strength Reserch , China | ||||
| 18:00 | 18:30 | 5.3.4 |
ON THE AERODYNAMIC CHARACTERISTICS OF CRESCENT WING D.F. Kurtulus¹, B. Anilir¹, D. Raymer, Conceptual Research Corporation, United States; ¹METU, Turkey | ||||
| additional information (interactive) | 5.3.R |
A NUMERICAL VIRTUAL FLIGHT PLATFORM DEVELOPMENT AND ITS APPLICATION ON HIGH MANEUVERABILITY FLIGHT VEHICLES H. Qiao¹, F. Qin¹, S. Deng¹; ¹Nanjing University of Aeronautics and Astronautics, China | |||||
| additional information (interactive) | 5.3.R |
APPLICATION OF CONVOLUTIONAL NEURAL NETWORKS IN DETERMINING THE VELOCITY AND PRESSURE FIELDS AROUND AIRFOIL MODELS G. Sharma¹, T.H. Tran, Le Quy Don Technical University, Vietnam; J. Tanimoto¹; ¹Kyushu University, Japan | |||||
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| 16:30 | 17:00 | 6.3.1 |
VALIDATION OF MULTIPHASE FLOW SIMULATIONS BY EXPERIMENTAL MEASUREMENTS IN A CHANNEL FLOW M. Khaled¹, B. Faraji-Tajrishi¹, A. Herrgen, MTU Aero Engines AG, Germany; B. Weigand¹; ¹Institute of Aerospace Thermodynamics, University of Stuttgart, Germany | ||||
| 17:00 | 17:30 | 6.3.2 |
STUDY OF THE SCAVENGE PUMP PERFORMANCE FOR TWO-PHASE FLOW IN AN AIRCRAFT ENGINE LUBRICATION SYSTEM N. Wu¹, J.-P. Hu¹, Y.-G. Lyu¹, J. Wang¹, Y. Tan¹, Z.-X. Liu¹; ¹Northwestern Polytechnical University, China | ||||
| 17:30 | 18:00 | 6.3.3 |
STUDY OF DROPLET MOTION AND WATER FILM FLOW CHARACTERISTICS ON SUPERHYDROPHOBIC SURFACES UNDER AIRFLOW SHEARING H. Zhao¹, D. Zhu¹, S. Wang², S. Chang², L. Yu¹, Y. Wu¹; ¹AVIC Aerodynamics Research Institute, China ;²Beihang University, China | ||||
| 18:00 | 18:30 | 6.3.4 |
EXPERIMENTAL SETUP FOR THE INVESTIGATION OF WATER SEPARATION IN ANNULAR FLOW WITHIN A CIRCULAR CHANNEL R. Haidl¹, B. Weigand¹; ¹Institute of Aerospace Thermodynamics, University of Stuttgart, Germany | ||||
| additional information (interactive) | 6.3.R |
EXPERIMENTAL STUDY ON MULTI-ATTITUDE OIL SUPPLY STRUCTURE Y. Xu¹, Y.-G. lLyu¹, J.-P. Hu¹, Z. Liu¹; ¹Northwestern Polytechnical University, China | |||||
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| 16:30 | 17:00 | 7.3.1 |
ENHANCING PUBLIC GOOD MISSIONS AND DISASTER RESPONSE WITH ADVANCED AERIAL TECHNOLOGY: OPPORTUNITIES AND CHALLENGES A. Andreeva-Mori, Japan Aerospace Exploration Agency (JAXA), Japan; D. Sziroczák, Budapest University of Technology and Economics (BME), Hungary; G. Schwoch, German Aerospace Center (DLR), Germany; M.C.R. Murça, Aeronautics Institute of Technology (ITA), Brazil; B. Dziugiel, Lukasiewicz Research Network – Institute of Aviation (ILOT), Poland; J. Homola, National Aeronautics and Space Administration (NASA), United States; V. Kramar, VTT Technical Research Centre of Finland, Finland | ||||
| 17:00 | 17:30 | 7.3.2 |
NASA RESEARCH TO EXPAND UAS OPERATIONS FOR DISASTER RESPONSE K. Ellis¹, M. Johnson¹, N. Neogi¹, J. Homola¹; ¹NASA, United States | ||||
| 17:30 | 18:00 | 7.3.3 |
ON-GOING WILDLAND FIRE WORK AT THE NATIONAL RESEARCH COUNCIL OF CANADA WITH A FOCUS ON THE USE OF COTS RPAS FOR REDUCTION OF NON-FIRE PILOT WORKLOAD G. Leblanc¹, G. Ifimov¹, M. Kalacska², O. Lucanus², J.P. Arroyo-Mora¹, J. Gorman¹, M. Wheatley, Ontario Ministry of Natural Resources and Forestry, Canada; C. McFayden, Natural Resources Canada, Canada; ¹National Research Council of Canada (NRC), Canada ;²Applied Remote Sensing Laboratory, McGill University, Canada | ||||
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| 16:30 | 17:00 | 8.3.1 |
MORPHING LEADING-EDGE TUBERCLES ON CESSNA 172 WING G. Abate¹, H.P. Monner¹; ¹German Aerospace Center (DLR), Germany | ||||
| 17:00 | 17:30 | 8.3.2 |
ON THE CHALLENGES OF SURROGATE-BASED AERODYNAMIC SHAPE OPTIMISATION J. Rasines¹, D. Verstraete¹; ¹The University of Sydney, Australia | ||||
| 17:30 | 18:00 | 8.3.3 |
AERODYNAMIC ANALYSIS OF CAMBER MORPHING AIRFOILS USING PARTICLE IMAGE VELOCIMETRY AND COMPUTATIONAL FLUID DYNAMICS METHODS M. Marciniuk¹, L. Kiszkowiak², P. Piskur, Polish Naval Academy of the Heroes of Westerplatte, Poland; L. Malicki¹, K. Strzelecka¹, K. Sibilski², S. Kachel²; ¹Wroclaw University of Science and Technology, Poland ;²Military University of Techology, Poland | ||||
| 18:00 | 18:30 | 8.3.4 |
ENGINEERING-BASED TOOL FOR THREE-DIMENSIONAL ESTIMATIONS OF RE-ENTRY VEHICLES AEROTHERMODYNAMICS P.E. Di Nuzzo, Italy; M. Maione¹, G. Pezzella¹, A. Viviani¹; ¹University of Campania, Italy | ||||
| additional information (interactive) | 8.3.R |
MODELLING ASTEROID TRAJECTORY IN EARTH’S ATMOSPHERE R.H. Morais¹, L.F. Ferreira Marques, ISEC, Portugal; A. Resende Rodrigues da Silva¹, R. Melicio, LAETA-IDMEC, Instituto Superior Técnico, Universidade de Lisboa, Portugal; ¹LAETA-AEROG, Universidade da Beira Interior, Portugal | |||||
| additional information (interactive) | 8.3.R |
AERO-KINEMATIC OPTIMIZATION OF HIGH-LIFT DEVICES WITH DOWNWARD DEFLECTION OF SPOILER C. Wei¹, C. Rao¹, L. Yang¹, T. Zhang¹; ¹Aerodynamics Research Institute, China | |||||
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| 16:30 | 17:00 | 9.3.1 |
ADVANCED HUMAN MACHINE INTERFACES FOR DRONE MONITORING: ASSESSMENT OF THE TECHNOLOGICAL FRAMEWORK FOR THE DESIGN OF AN AUGMENTED REALITY INTERFACE S. Bagassi¹, T. Fadda¹, M. Corsi¹; ¹University of Bologna, Italy | ||||
| 17:00 | 17:30 | 9.3.2 |
CORUS-XUAM: TACKLING URBAN AIR MOBILITY AIRSPACE INTEGRATION CHALLENGES G. Riccardi¹, L. Brucculeri¹, E. Fornaciari, d-flight, Italy; M. D'Onofrio, Techno Sky, Italy; A. Zilli², D. Leanza², G. Ferrara, Eurocontrol, France; M. Molinario³, G. Esposito³, A. Favier, Pipistrel, Italy; ¹ENAV S.P.A, Italy ;²DTA, Italy ;³NAIS, Italy | ||||
| 17:30 | 18:00 | 9.3.3 |
AI-ASSISTED DESIGN OF UAV DOCKING STATION NETWORK FOR DUAL USE PURPOSES A. Avi¹, G. Quaranta¹, A. Valentini, Fondazione Bruno Kessler, Italy; ¹Politecnico di Milano, Italy | ||||
| 18:00 | 18:30 | 9.3.4 |
LOW-ALTITUDE INTEGRATED AIRSPACE OPERATIONS OF AIRCRAFT FLYING UNDER VISUAL FLIGHT RULES: THE VERTICAL DIMENSION A. Andreeva-Mori¹, K. Ohga¹, K. Kobayashi¹; ¹Japan Aerospace Exploration Agency (JAXA), Japan | ||||
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| 16:30 | 17:00 | 10.3.1 |
NUMERICAL SIMULATION STUDY ON THE INFLUENCE OF WING SPACING OF DRAGONFLY-INSPIRED FLAPPING WINGS Y. Luo, China; L. Wang, China; J. Wang, China; X. Lang, China; X. Yang, China | ||||
| 17:00 | 17:30 | 10.3.2 |
COMPUTATIONAL FLUID DYNAMICS ANALYSIS OF A DIRECT AIR CAPTURE FILTER SYSTEM M. Panagopoulos¹, N.J. Lawson¹, D.M. D’Alessandro¹, E. Kearns¹; ¹University of Syndey, Australia | ||||
| 17:30 | 18:00 | 10.3.3 |
DESIGN OF DUAL-FUSELAGE FLIGHT PLATFORM FOR JET CONTROL FUNCTION VERIFICATION C.P. Li, China; G. Zhang, China; N. Liu, China; Y. Zhang, China; L. Xu, China; M. Wang, China | ||||
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| 16:30 | 17:00 | 11.3.1 |
AEROELASTIC ISSUES IN THE DESIGN OF HIGH ASPECT RATIO STRUT-BRACED WING AIRCRAFT E. Roncolini¹, F. Toffol ¹, S. Ricci¹; ¹Politecnico di Milano, Italy | ||||
| 17:00 | 17:30 | 11.3.2 |
DYNAMIC BUCKLING ANALYSIS OF THIN-SHELL COMPOSITE STRUCTURES BASED ON ISOGEOMETRIC ANALYSIS H. Qiu¹, Y. Guo¹, Z. Guan¹, H. Zhu¹, Y. Pan¹; ¹Nanjing University of Aeronautics and Astronautics, China | ||||
| 17:30 | 18:00 | 11.3.3 |
EFFICIENT AEROSTRUCTURAL DESIGN OPTIMIZATION COMBINING GRADIENT-ENHANCED KRIGING WITH COUPLED ADJOINT METHOD H.-J. Guo, China; Z.-H. Han, China; C.-Z. Xu, China; K.-S. Zhang, China; W.-P. Song, China; J.-Q. Luo, China | ||||
| 18:00 | 18:30 | 11.3.4 |
BIRD AND DRONE IMPACT DAMAGE PROGNOSIS OF ON-DEMAND AIR MOBILITY SERVICE AIRCRAFT ENGINE H. Raza¹, P. Vaghela¹, E. Stumpf, RWTH Aachen, Germany; J. Bayandor¹; ¹University at Buffalo, United States | ||||
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| 16:30 | 17:00 | 12.3.1 |
DESIGN OF MEASUREMENT SETUP FOR HIGH-ALTITUDE IN-FLIGHT EXPERIMENTS ON DU89-134/14 AIRFOIL AT LOW REYNOLDS NUMBER M. Avirovic¹, C. Brunelli¹, K. Wykes², C. Mengdehl², B.G. Marinus¹, J. Degroote, University of Ghent, Belgium; J. Van Beeck, Von Karman Institute for Fluid Dynamics, Belgium; ¹Royal Military Academy, Belgium ;²Stemme Belgium, Belgium | ||||
| 17:00 | 17:30 | 12.3.2 |
UPGRADE OF THE VTI T-38 BLOWDOWN TRISONIC TEST FACILITY: WIND TUNNEL CONTROL SYSTEM B. Ilic¹, G. Ocokoljic¹, M. Samardžic¹, J. Isakovic, Academy of Applied Technical Studies, Serbia; ¹Military Technical Institute, Serbia | ||||
| 17:30 | 18:00 | 12.3.3 |
SURFACE VISUALISATION OF TIME AVERAGED FLOW BEHAVIOUR AROUND RIGID AND FLEXIBLE HEMISPHERES UTILISING UV SENSITIVE OIL N. Menakath¹, N.J. Lawson¹, G.A. Vio, Defence Science and Technology Group, Australia; ¹The University of Sydney, Australia | ||||
| 18:00 | 18:30 | 12.3.4 |
HOT-WIRE ANEMOMETRY OF THE BOUNDARY LAYER PRIOR TO A CAVITY IN RESPONSE TO VARIED UPSTREAM GEOMETRY C.O.L. Hamilton Smith¹, N.J. Lawson¹; ¹The University of Sydney, Australia | ||||
| additional information (interactive) | 12.3.R |
REVITALIZATION OF A FLOW-CELL DEVICE FOR AIR INTAKE TESTING AND ITS INTEGRATION WITH WIND TUNNEL SYSTEMS D. Damljanovic¹, D. Vukovic¹, L. Petrovic¹; ¹Military Technical Institute, Serbia | |||||
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| 16:30 | 17:00 | 13.3.1 |
EXPERIMENTAL AND NUMERICAL INVESTIGATION OF NOISE GENERATION IN HYDROGEN AND METHANE-HYDROGEN LAMINAR FLAMES F.G. Schiavone¹, M. Durand², M. Torresi¹, S.M. Camporeale¹, T. Schuller², D. Laera¹; ¹Polytechnic University of Bari, Italy ;²Institut de Mécanique des Fluides de Toulouse, France | ||||
| 17:00 | 17:30 | 13.3.2 |
AN EXPERIMENTAL SIMULATION ON THE INFLUENCE OF DIFFERENT FILM COOLING HOLE SHAPES ON PARTICLE DEPOSITION ON TURBINE VANE Z. Liu¹, R. Ruan¹, L. Cheng¹, Y. Zhang¹, Z. Liu¹, D. Wu¹; ¹Northwestern Polytechnical University, China | ||||
| 17:30 | 18:00 | 13.3.3 |
FUEL CONSUMPTION MONITORING OF TURBOPROP ENGINE J. Juracka¹, Z. Hubnerova¹; ¹Brno University of Technology, Czech Republic | ||||
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| 16:30 | 17:00 | 14.3.1 |
ASSESSING THE TECHNICAL VIABILITY OF ALL-ELECTRIC HYDROGEN-POWERED AIRCRAFTS P. Marocco¹, M.C. Massaro¹, A.H.A. Monteverde¹, M. Santarelli¹; ¹Politecnico di Torino, Italy | ||||
| 17:00 | 17:30 | 14.3.2 |
MODELLING A HYDROGEN FUELLED COMPOSITE CYCLE AEROENGINE A. Johansson¹, P. Miltén¹, A. Lundbladh, GKN Aerospace, Sweden; C. Xisto¹; ¹Chalmers University of Technology, Sweden | ||||
| 17:30 | 18:00 | 14.3.3 |
CFD-BASED SCOUTING FOR THE DESIGN OF A MULTI-FUEL KEROSENE/HYDROGEN ATMOSPHERIC BURNER L. Palanti¹, L. Mazzei¹, C. Bianchini¹, S. Link², K. Dave², F. De Domenico², A.G. Rao²; ¹Ergon Research, Italy ;²TU Delft, Netherlands | ||||
| 18:00 | 18:30 | 14.3.4 |
MODELLING AND INITIAL ASSESSMENT OF A FUEL CELL AUXILIARY PROPULSION AND POWER UNIT M.G. Kolb¹, A. Seitz¹, B. Türkyilmaz¹, Y. Ma¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany | ||||
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| 16:30 | 17:00 | 15.3.1 |
DOWNRANGE CONTROL GUIDANCE FOR REENTRY BURN OF REUSABLE LAUNCH VEHICLE K.-W. Jung¹, C.-H. Lee¹; ¹KAIST, South Korea | ||||
| 17:00 | 17:30 | 15.3.2 |
EXPLICIT MODEL FOLLOWING TRAJECTORY CONTROL SYSTEM FOR MULTIPLE VERTICAL TAKEOFF AND LANDING CONFIGURATIONS A. Comer¹, I. Chakraborty¹; ¹Auburn University, United States | ||||
| 17:30 | 18:00 | 15.3.3 |
CONVEX PROGRAMMING APPROACH OF ROBUST POWERED DESCENT GUIDANCE THROUGH DYNAMIC TUBE MPC J.-I. Jang¹, C.-H. Lee¹, S. He, BIT, China; ¹KAIST, South Korea | ||||
| 18:00 | 18:30 | 15.3.4 |
SYSTEM ARCHITECTURE AND EVALUATION METHOD OF HUMAN-MACHINE COLLABORATION IN FLIGHT CONTROL SYSTEM J. Che¹, X. Chen¹, S. Che, Northwestern Polytechnical University, China; J. Li¹, Z. Sun¹; ¹Flight Automatic Control Research Institute, AVIC, China | ||||
| additional information (interactive) | 15.3.R |
PILOT INDUCED OSCILLATIONS AND FLIGHT PHASES IDENTIFICATION OF THE SPACE SHUTTLE AND TRANSPORT AIRPLANES S. Kolb, CREA, France | |||||
| additional information (interactive) | 15.3.R |
A NOLINEAR MODEL PREDICTIVE CONTROL METHOD FOR AIRBREATHING HYPERSONIC VEHICLE BASED ON KOOPMAN OPERATOR C.R. Li¹, W.Q. Li¹, Y. Li¹, S. Tang¹; ¹Northwestern Polytechnical University, China | |||||
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| 16:30 | 17:00 | 16.3.1 |
HARDWARE-IN-THE-LOOP SIMULATION FRAMEWORK FOR THE EVALUATION OF AUTONOMOUS FLIGHT FUNCTIONS D. Pla Guerrero¹, A. Hegde¹, J. Wan, Flanders Make, Belgium; E. Allegaert¹, Y. Lemmens¹; ¹Siemens Digital Industries Software, Belgium | ||||
| 17:00 | 17:30 | 16.3.2 |
FLIGHT CONTROL SYSTEM KNOWLEDGE GRAPH CONSTRUCTION BASED ON AERONAUTICAL DOMAIN KNOWLEDGE AUGMENTED LARGE LANGUAGE MODEL Y. Fan, China; Y. Sun, China; B. Mi, China | ||||
| 17:30 | 18:00 | 16.3.3 |
AN UAV MANEUVERING DECISION-MAKING ALGORITHM BASED ON DEEP TRANSFER REINFORCEMENT LEARNING K. Li¹, K. Zhang¹, H. Liu², Y. Li², Q. Wang¹; ¹Northwestern Polytechnical University, China ;²Shenyang Aircraft Design and Research Institute, China | ||||
| additional information (interactive) | 16.3.R |
AUTONOMOUS LANDING OF A QUADROTOR ON A MOVING TARGET WITH OCCLUSION AVOIDANCE MANEUVER D. Kim¹, H.J. Kim¹; ¹Seoul National University, South Korea | |||||
| additional information (interactive) | 16.3.R |
ULTRA-LOW-ALTITUDE PENETRATION PATH PLANNING FOR FIXED-WING AIRCRAFT BASED ON NMP ALGORITHM H.-X. Huang¹, D.-B. Li¹, P.-Y. Qi¹, Y.-X. Shang¹; ¹beihang university, China | |||||
| additional information (interactive) | 16.3.R |
AN OPTICAL FLOW BASED GUIDANCE ALGORITHM FOR A QUADROTOR UAV MOVING INSIDE CIRCULAR CORRIDORS A. Bagherzadeh¹, F. Saghafi¹; ¹Sharif University of Technology, Iran | |||||
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| 16:30 | 17:00 | 17.3.1 |
HYBRID AIR DATA SYSTEM ARCHITECTURE: FROM DESIGN TO FLIGHT TEST VERIFICATION M. Rovelli¹, A. Brandl¹, S. Di Bitonto¹, F. Di Donfrancesco¹, E. Maruccia¹, I. Viglietti¹, D. Marchetti¹; ¹Leonardo, Italy | ||||
| 17:00 | 17:30 | 17.3.2 |
DEVELOPMENT AND TESTING OF AN ACTUATION SYSTEM FOR A MORPHING CONTROL SURFACE M. Schäfer¹, R. Keimer¹, O. Bertram¹; ¹German Aerospace Center (DLR), Germany | ||||
| 17:30 | 18:00 | 17.3.3 |
PRELIMINARY ANALYSIS OF TEMPERATURE EFFECTS AND MANEUVER-INDUCED DEFORMATIONS ON FBG OPTIC FIBER INTEGRATED SYSTEMS A. Aimasso¹, M. Bertone¹, C. Ferro¹, M.D.L. Dalla Vedova¹, P. Maggiore¹; ¹Politecnico di Torino, Italy | ||||
| 18:00 | 18:30 | 17.3.4 |
NUMERICAL METHOD FOR DESIGNING AND MODELING AN EXHAUST CLUSTER FOR A SMALL TURBOJET ENGINE TEST CELL T.-G. Nguyen¹, Q.-H. Nghiem¹, P.-M. Nguyen¹; ¹Viettel Aerospace Institute, Vietnam | ||||
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| 10:00 | 10:30 | 1.4.1 |
FUEL CELL BASED POWERTRAINS J. Ludvik, Honeywell, United States | ||||
| 10:30 | 11:00 | 1.4.2 |
CLEAN AVIATION HIGH VOLTAGE NETWORK AND DEMONSTRATION R. Foley, RTX/Collins, United States | ||||
| 11:00 | 11:30 | 1.4.3 |
P&W APPROACH TO SUSTAINABILITY J.M. Thomassin, Pratt & Whitney Canada, Canada | ||||
| 11:30 | 12:00 | 1.4.4 |
PANEL DISCUSSION: ADDITONAL: SUSAN YING, ERIKA HOLTZ, GABRIELE TEOFILI, DAVID SERCOMBE D. P., | ||||
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| 10:00 | 10:30 | 2.4.1 |
OBJECTIVES OF THE UNITED STATES FULL SCALE BLENDED WING BODY FLIGHT DEMONSTRATION F. Collier, NASA (LaRC), United States | ||||
| 10:30 | 11:00 | 2.4.2 |
TECHNICAL APPROACH FOR A BWB AIRLINER TO MEET MARKET DEMANDS M. Page, JetZero, United States | ||||
| 11:00 | 11:30 | 2.4.3 |
TECHNICAL FINDINGS TO DATE TO SUPPORT MARKET DEMANDS OF A BWB AIRLINER M. Page, JetZero, United States | ||||
| 11:30 | 12:00 | 2.4.4 |
GROUND AND SCALED FLIGHT TEST PLANS TO SUPPORT DEVELOPMENT OF A BWB AIRLINER M. Page, JetZero, United States | ||||
| 12:00 | 12:30 | 2.4.5 |
PERFORMANCE COMPARISON OF THE BLENDED WING BODY AND TUBE AND WING CONFIGURATIONS J. Ahuja¹, C. Perron¹, R.D.B. Rivera¹, J.C. Tai¹, D.N. Mavris¹; ¹Georgia Tech, United States | ||||
| Reserve Paper | 2.4.R |
PERFORMANCE COMPARISON OF THE BLENDED WING BODY AND TUBE AND WING CONFIGURATIONS EXTRA J. Tai, Georgia Tech, United States | |||||
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| 10:00 | 10:30 | 3.4.1 |
ROBUST SCHUR-COMPLEMENT SOLVERS AND LARGE-SCALE MULTIDISCIPLINARY DESIGN OPTIMIZATION M.A.S. Abdul-Kaiyoom¹, A. Yildirim¹, J.R.R.A. Martins¹; ¹University of Michigan, United States | ||||
| 10:30 | 11:00 | 3.4.2 |
PROCESSES, METHODS AND TOOLS SUPPORTING THE DEVELOPMENT OF AERONAUTICAL SYSTEMS L. Boggero¹, J. Bussemaker¹, G. Donelli¹, F. Torrigiani¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany | ||||
| 11:00 | 11:30 | 3.4.3 |
MDAX : ENHANCEMENTS IN A COLLABORATIVE MDAO WORKFLOW FORMULATION TOOL S. Garg¹, J.H. Bussemaker¹, L. Boggero¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany | ||||
| 11:30 | 12:00 | 3.4.4 |
SURROGATE-ASSISTED HIERARCHICAL OPTIMIZATION METHOD FOR VARIABLE SWEEP FLIGHT VEHICLE TRAJECTORY N.-H. Ye¹, T. Long¹, B. Fu, Xi’an Modern Control Technology Research Institute, China; R.-H. Shi, Beijing Institute of Technology Chongqing Innovation Center, China; ¹Beijing Institute of Technology, China | ||||
| 12:00 | 12:30 | 3.4.5 |
RAPID DESIGN OF UNCONVENTIONAL AIRCRAFT USING SOFTWARE TOOLS COUPLED IN OPTIMIZATION LOOP – LESSONS LEARNED T. Goetzendorf-Grabowski¹, A. Kwiek¹, J. Mieloszyk, ?ukasiewicz Research Network – Institute of Aviation, Poland; A. Tarnowski¹; ¹Warsaw University of Technology, Poland | ||||
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| 10:00 | 10:30 | 4.4.1 |
REQUIREMENTS UNCERTAINTY PROPAGATION IN CONCEPTUAL DESIGN USING BAYESIAN NETWORKS A. Spinelli¹, A. Sharma, Centre for Aeronautics, Cranfield University, United Kingdom; T. Kipouros¹; ¹Centre for Propulsion and Thermal Power, Cranfield University, United Kingdom | ||||
| 10:30 | 11:00 | 4.4.2 |
APPLICATION OF SYSML IN THE DEVELOPMENT OF AIRCRAFT CABIN HEALTH MANAGEMENT A. Hechelmann¹, T. Mannchen¹; ¹Baden-Wuerttemberg Cooperative State University (DHBW) Ravensbur, Germany | ||||
| 11:00 | 11:30 | 4.4.3 |
AUTOMATION OF ENGINEERING INTEROPERABILITY FOR AIRCRAFT SYSTEM DESIGN F. During¹, R.C. Munjulury¹, R. Hällqvist, System Simulation and Concept Development, Saab Aeronautics, Sweden; ¹FLUMES, Linköping University, Sweden | ||||
| 11:30 | 12:00 | 4.4.4 |
AUTOMATIC SYSTEM REQUIREMENTS VERIFICATION FOR THE MBSE-ORIENTED AIRCRAFT DESIGN PROCESS A. Dagna¹, S. Centomo², E. Brusa¹, C. Delprete¹, R. Gentile²; ¹Politecnico di Torino, Italy ;²Leonardo LABS, Leonardo S.p.A., Italy | ||||
| 12:00 | 12:30 | 4.4.5 |
AN MBSE ENABLED MDAO APPROACH FOR THE CONCEPTUAL DEVELOPMENT OF COMPLEX SYSTEMS M. Fouda¹, L. Willrodt¹, H. Almeida¹, J. Cortez¹, O. Hussein¹, F. Castaneda¹, H. Dhouib¹, C. Dahik¹, V. Drouet¹, R. Brook¹; ¹Capgemini Engineering, Germany | ||||
| additional information (interactive) | 4.4.R |
A MODEL BASED SYSTEM ENGINEERING APPROACH TOWARDS AIRCRAFT DIGITAL CERTIFICATION C. Mirabella¹, M. Tuccillo¹, P. Della Vecchia¹; ¹Università degli Studi Federico II, Italy | |||||
| additional information (interactive) | 4.4.R |
A SEMANTIC MODEL-BASED SYSTEMS ENGINEERING APPROACH FOR SUPERSONIC BUSINESS JET CONCEPTUAL DESIGN Z. Cui¹, M. Luo¹, J. Lu¹, J. Wang¹; ¹Beihang University, China | |||||
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| 10:00 | 10:30 | 5.4.1 |
BREAKING THE SOUND BARRIER: ACHIEVING QUIET SUPERSONIC FLIGHT OVER LAND P. Coen, United States | ||||
| 10:30 | 11:00 | 5.4.2 |
DUAL-STREAM JET NOISE TEST WITH INTERNAL MIXER DESIGN VARIATIONS FOR LTO NOISE OF SUPERSONIC AIRCRAFT R. Habing¹, M.-J. Van der Meulen¹, M. Huet, ONERA / DAAA, France; R. Jaron, DLR, Germany; F. Petrosino², M. Barbarino², O. Zaporozhets, Institute of Aviation, Poland; ¹NLR, Netherlands ;²CIRA, Italy | ||||
| 11:00 | 11:30 | 5.4.3 |
THE FUTURE OF CIVIL SUPERSONIC TRANSPORT IN EUROPE: THE SENECA AND MORE&LESS PROJECTS R. Jaron, DLR, Germany; N. Viola, Politecnico di Torino, Italy | ||||
| 11:30 | 12:00 | 5.4.4 |
POTENTIAL OF THE RANGE EXTENSION OF SUPERSONIC TRANSPORT Z. Lei, SUWA UNIVERSITY OF SCIENCE, Japan | ||||
| 12:00 | 12:30 | 5.4.5 |
ESATTO: THE HOLISTIC FRAMEWORK TO SUPPORT THE DESIGN OF SUSTAINABLE SUPERSONIC AVIATION R. Fusaro¹, G. Piccirillo¹, D. Ferretto¹, G. Saccone, Italian Aerospace Research Center, Italy; D. Bodmer², J. Jäschke², M. Cremaschi, ENVISA, Italy; N. Viola¹; ¹Politecnico di Torino, Italy ;²Hamburg University of Technology, Germany | ||||
| Reserve Paper | 5.4.R |
AERODYNAMIC DESIGN OF A SUPERSONIC TRANSPORT CONFIGURATION CONSIDERING AVERAGE LOUDNESS IN THE WHOLE BOOM CARPET Q. Chen¹, Z.-H. Han¹, J.-L. Qiao¹, Y.-L. Ding¹, K.-S. Zhang¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China | |||||
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| 10:00 | 10:30 | 6.4.1 |
TRANSITION MODELING IN SUPPORT OF CFD VISION 2030 - HIGHLIGHTS OF RECENT EFFORTS AT THE NASA LANGLEY RESEARCH CENTER M. Choudhari¹, E. Beyak¹, N. Hildebrand¹, F. Li¹, E. Vogel¹, P. Paredes, National Institute of Aerospace, United States; V. Srivastava², B. Venkatachari²; ¹NASA Langley Research Center, United States ;²Analytical Mechanics Associates, United States | ||||
| 10:30 | 11:00 | 6.4.2 |
EVALUATION OF CFD TRANSITION MODELING FOR TRANSONIC, NATURAL-LAMINAR-FLOW DESIGN J.G. Coder, Pennsylvania State University, United States | ||||
| 11:00 | 11:30 | 6.4.3 |
ON THE CHOICE OF TURBULENCE MODEL FOR THE SIMULATION OF AIRFOILS AT REYNOLDS NUMBER BELOW 200,000 S. Shahjahan¹, B. Emmerson¹, D. Verstraete¹; ¹The University of Sydney, Australia | ||||
| 11:30 | 12:00 | 6.4.4 |
FLUIDODYNAMIC ANALYSIS OF LOW REYNOLDS NUMBER FLOWS N. Verde, Italy; F. Capoluongo, Italy; P. Catalano, CIRA, Italy; G. Pezzella, University of Campania , Italy; A. Viviani, University of Campania, Italy | ||||
| 12:00 | 12:30 | 6.4.5 |
BOUNDARY-LAYER SUCTION AND AERODYNAMIC SHAPE OPTIMIZATION FOR HYBRID LAMINAR FLOW CONTROL ON A FIN H. Wu¹, W. Song¹, H. Nie¹, Z. Han¹; ¹National Key Laboratory of Aircraft Configuration Design, China | ||||
| additional information (interactive) | 6.4.R |
BOUNDARY LAYER TRANSITION AND RE-LAMINARIZATION IN MACH 6 NOZZLE OF A SHOCK TUNNEL–A NUMERICAL STUDY S. Malekipour¹, M. Mohammadi-Amin¹, I. Bahman-Jahromi¹; ¹Aerospace Research Institute, Iran | |||||
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| 10:00 | 10:30 | 8.4.1 |
FINITE-STATE AEROELASTIC MODELLING OF MORPHING WING THROUGH UNSTEADY LIFTING-LINE THEORY R. Giansante¹, G. Bernardini¹, M. Gennaretti¹; ¹Roma Tre University, Italy | ||||
| 10:30 | 11:00 | 8.4.2 |
DECOUPLING STORE AND PARENT AERODYNAMICS FOR FAST PREDICTION OF SUBSONIC STORE TRAJECTORIES N. Mthembu¹, H. Ndlovu¹, B. Ndebele¹, K. Jamison¹, L. Zwane¹; ¹CSIR, South Africa | ||||
| 11:00 | 11:30 | 8.4.3 |
WIND-TUNNEL TESTS OF INNOVATIVE TAILPLANE CONFIGURATIONS F. Nicolosi¹, P. Della Vecchia¹; ¹University of Naples Federico II, Italy | ||||
| 11:30 | 12:00 | 8.4.4 |
FAST PREDICTION OF PRESSURE DISTRIBUTION FOR 3D CONFIGURATION BASED ON LARGE LANGRAGE MODEL B.W. Shu, Northwestern Polytechnical University, China; Z.H. Gao, China; J.T. Huang, China; X. Chen, China; W. Zhang, China; H. Zhao, China | ||||
| 12:00 | 12:30 | 8.4.5 |
RESEARCH ON AERODYNAMIC DESIGN OF ENGINE NACELLE UNDER THE INFLUENCE OF PROPELLER SLIPSTREAM FOR THE TURBOPROP AIRCRAFT R.-F. Xu¹, W.-P. Song¹, X.-H. Li², R.-Z. Qian², Y.-J. Zhang², J.-H. Xu¹, X.-L. Li¹; ¹Northwestern Polytechnical University, China ;²AVIC The First Aircraft Institute, China | ||||
| additional information (interactive) | 8.4.R |
LONG-WAVE INSTABILITY OF AIRCRAFT WAKE VORTEX UNDER SHEAR CROSSWIND Z. Xu¹, D. Li¹, J. Cai¹, J. Han, N, China; ¹Northwestern Polytechnical University School of Aeronautics, China | |||||
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| 10:00 | 10:30 | 9.4.1 |
EUROPEAN RESEARCH COUNCIL (ERC) - FUNDING OPPORTUNITIES AND REPRESENTATIVE PROJECT HIGHLIGHTS G. Symeonidis, European Research Council Executive Agency (ERCEA), Belgium | ||||
| 10:30 | 11:00 | 9.4.2 |
TOWARDS A FIRST-PRINCIPLE BASED QUANTITATIVE DESCRIPTION OF TURBULENCE WITHOUT THE NEED FOR ADHOC MODELS T.M. Schneider, EPFL, Switzerland | ||||
| 11:00 | 11:30 | 9.4.3 |
METAMATERIALS FOR CONTROL OF FLUID FLOWS M. Kotsonis, Delft University of Technology, Netherlands | ||||
| 11:30 | 12:00 | 9.4.4 |
THERMOACOUSTIC INSTABILITY IN AERO-ENGINE COMBUSTORS A. Morgans, United Kingdom | ||||
| 12:00 | 12:30 | 9.4.5 |
NABUCCO TAKE-OFF: MULTI-STABLE PANELS FOR AN ADAPTIVE WING C. Bisagni, Politecnico di Milano, Italy | ||||
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| 10:00 | 10:30 | 10.4.1 |
HIGH TEMPERATURE BALLISTIC IMPACT TEST TECHNOLOGY BASED ON ELECTROMAGNETIC LAUNCH C. Zhang¹, J. Liu¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China | ||||
| 10:30 | 11:00 | 10.4.2 |
IMPACT TOLERANCE OF CERAMIC MATRIX COMPOSITES FOR AEROSPACE APPLICATIONS G. Janszen¹, A.M. Caporale¹, L. Cavalli, Petroceramics S.p.A., Italy; M. De Stefano Fumo, CIRA, Italy; A. Airoldi¹; ¹Politecnico di Milano, Italy | ||||
| 11:00 | 11:30 | 10.4.3 |
INFLATABLE SPACE SHIELD STRUCTURE FOR SPACE HABITATION MODULE J.-H. Cha, Chosun Uni., South Korea | ||||
| 11:30 | 12:00 | 10.4.4 |
Lecture canceled | ||||
| 12:00 | 12:30 | 10.4.5 |
DAMAGE AND MECHANICAL REPAIR OF COMPOSITE LAMINATES: EFFECTS OF EMBEDDED DEFECTS AND LOW VELOCITY IMPACTS G. Zhang, China; M. Tong, China; B. Yan, China; F. Wang, China; H. Zhang, China | ||||
| Reserve Paper | 10.4.R |
IMPACT RESPONSES AND FAILURE MECHANISMS OF ALMGB14 UNDER DYNAMIC LOADS Y. Lu¹, W. Wang¹, Y. Zhang, Hangzhou Zhiyuan Research Institute, China; Z. Zhang, Northwest Institute of Mechanical and Electrical Engineering, China; ¹Northwestern Polytechnical University, China | |||||
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| 10:00 | 10:30 | 11.4.1 |
DETECTION OF DELAMINATIONS IN DAMAGED COMPOSITE PLATES VIA LOCAL DAMAGE RESONANCE APPROACH F. Nicassio¹, A.P. Fontanella², M. Cinefra², G. Scarselli¹; ¹University of Salento, Italy ;²Politecnico of Bari, Italy | ||||
| 10:30 | 11:00 | 11.4.2 |
FREE VIBRATIONS OF CYLINDRICAL SHELLS WITH CUTOUTS BY A SINGLE-DOMAIN RITZ FORMULATION A. Milazzo, University of Palerrmo, Italy; M. Lo Cascio, University of Palermo, Italy | ||||
| 11:00 | 11:30 | 11.4.3 |
LARGE-SCALE STRUCTURAL DYNAMIC TOPOLOGY OPTIMIZATION DESIGN FOR AIRCRAFT VIBRATION REDUCTION UNDER RANDOM EXCITING RESPONSE S. Xiao¹, L.-Y. Liu¹, H.-M. Xue¹, M.-Q. Wang¹, D.-Y. Chen¹; ¹AVIC Shenyang Aircraft Design and Research Institute, China | ||||
| 11:30 | 12:00 | 11.4.4 |
ACTIVE CONTROL DAMPING WITH THE USE OF VOICE COIL ACTUATORS G. Cardellino¹, T. Melz¹, R. Feldmann¹, C. Adams, Technical University of Graz, Austria; F. Franco², G. Petrone², S. De Rosa²; ¹Technical University of Darmstadt, Germany ;²Universitä degli Studi di Napoli Federico II, Italy | ||||
| 12:00 | 12:30 | 11.4.5 |
ANALYTICAL STUDY ON HYDROSTATIC RESPONSE CHARACTERISTICS DURING WATER LANDINGS OF AMPHIBIOUS AIRCRAFT F. Sun, Xi'an Modern Control Technology Research Institute, China; Y.-H. Zheng¹, S.-S. Zhu¹; ¹Northwestern Polytechnical University, China | ||||
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| 10:00 | 10:30 | 12.4.1 |
TOWARDS SUSTAINABLE AVIATION WITH EFFICIENT AIRSPACE OPERATIONS W.J. Coupe¹, S. Saxena¹; ¹NASA Ames Research Center, United States | ||||
| 10:30 | 11:00 | 12.4.2 |
COMPARING CONVECTIVE WEATHER IMPACTS ON AIR TRAFFIC MANAGEMENT OPERATIONS IN UNITED STATES, CANADA & EUROPE G. Enea¹, T. Reynolds¹, J. Venuti¹, T. Polishchuk², V. Polishchuk², A. Lemetti², A. Lau³, J. Solzer³, T. Bölle³; ¹MIT Lincoln Laboratory, United States ;²Linköping University, Sweden ;³German Aerospace Center (DLR), Germany | ||||
| 11:00 | 11:30 | 12.4.3 |
RELATIONSHIPS BETWEEN AIRCRAFT ROUTES AND TURBULENCE-RELATED WEATHER DATA Y. Nakamura¹, A. Senoguchi¹; ¹Electronic Navigation Research Institute, Japan | ||||
| 11:30 | 12:00 | 12.4.4 |
ROUTE PLANNING FOR VOLCANIC ASH AND RADIOACTIVITY IN-SITU DRONE MEASUREMENTS USING A GENETIC ALGORITHM AND KRIGING K.A. Buchtal¹, A. Lau¹, D. Ebert², J. Richters², K. Schneiders²; ¹German Aerospace Center (DLR), Institute of Air Transport, Germany ;²German Weather Service (DWD), Radioactivity Monitoring, Germany | ||||
| 12:00 | 12:30 | 12.4.5 |
INTEGRATING ECO-EFFICIENT FLIGHT PLANNING IN AIRCRAFT CONCEPTUAL DESIGN: MINIMAL NOX ROUTES FOR HIGH-SPEED AIRCRAFT USING HYDROGEN F. Borgna¹, V. Borio¹, R. Fusaro¹, N. Viola¹, G. Saccone, Italian Aerospace Research Centre (CIRA), Italy; ¹Politecnico di Torino, Italy | ||||
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| 10:00 | 10:30 | 13.4.1 |
ON THE WATER ENHANCED TURBOFAN CONCEPT: PART B – FLOW PATH AND MASS ASSESSMENT J. Häßy¹, A. Görtz¹, M. Schmelcher¹, J. Schmeink¹, M. El-Soueidan¹; ¹DLR, Germany | ||||
| 10:30 | 11:00 | 13.4.2 |
DESIGN AND ANALYSIS OF A SCALED COMPOSITE UHBR FAN BLADE FOR WIND TUNNEL TESTS B.A.T. Noordman¹, W.J. Vankan¹; ¹Royal Netherlands Aerospace Centre, Netherlands | ||||
| 11:00 | 11:30 | 13.4.3 |
ON THE WATER ENHANCED TURBOFAN CONCEPT: PART A - THERMODYNAMICS AND OVERALL ENGINE DESIGN A. Görtz¹, J. Häßy¹, M. Nickl², A. Lessis², M. Schmelcher¹, M. El-Soueidan¹; ¹German Aerospace Center, Germany ;²Bauhaus Luftfahrt e.V., Germany | ||||
| 11:30 | 12:00 | 13.4.4 |
UNSTEADY AERODYNAMICS OF A COUPLED COMPACT INTAKE-FAN IN CROSSWIND L. Lobuono¹, D. MacManus¹, R. Christie¹, L. Boscagli¹; ¹Cranfield University, United Kingdom | ||||
| 12:00 | 12:30 | 13.4.5 |
KNOWLEDGE-BASED TURBINE DISK MODELING – A CONCEPTUAL DESIGN PROCESS CALIBRATED TO THE NASA ENERGY EFFICIENT ENGINE P. Wehrel¹, J. Schmeink¹, J. Häßy¹; ¹German Aerospace Center (DLR), Germany | ||||
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| 10:00 | 10:30 | 14.4.1 |
STUDY OF HYBRIDISATION SCENARIOS FOR TURBOPROP AIRCRAFT IN THE GENERAL AVIATION SEGMENT F. Lutz¹, J. Jézégou¹, M. Budinger², A. Reysset²; ¹ISAE-SUPAERO, France ;²INSA Toulouse, France | ||||
| 10:30 | 11:00 | 14.4.2 |
INSTRUMENTATION OF A SUBESCALE GROUND EFFECT VEHICLE, VOLITAN, TO MEASURE FLIGHT PROPULSION EFFICIENCY C. Fischer, 1Instituto Federal de São Paulo and Aeronautics Institute of Tec, Germany; M.A.R. Diaz¹, L. Souza¹, R.G.A. da Silva¹, L.C.S. Goes¹; ¹Aeronautics Institute of Technology, Brazil | ||||
| 11:00 | 11:30 | 14.4.3 |
A SENSITIVITY ANALYSIS ON THE ENDURANCE EQUATION FOR HYBRID-ELECTRIC AIRCRAFT A. Batra¹, R. Raute, Dept. Ind. Elec. Eng. University of Malta, Malta; R. Camilleri¹; ¹INSTITUTE OF AEROSPACE TECHNOLOGIES (IAT), UNIVERSITY OF MALTA, Malta | ||||
| 11:30 | 12:00 | 14.4.4 |
DESIGN APPROACH FOR HYBRID ELECTRIC PROPULSION CONCEPTS OF MID-RANGE AIRCRAFT INCLUDING SUSTAINABLE AVIATION FUELS K. Ziaja¹, D. Lieder², J. Göing², J. Friedrichs², F. di Mare¹; ¹Ruhr University Bochum, Germany ;²Technische Universität Braunschweig, Germany | ||||
| 12:00 | 12:30 | 14.4.5 |
HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION D. Kierbel¹, T. Neuland¹, P.-E. Roux¹, P. Nehter¹, J. Hollmann², C.N. Dagli², P. Köhler², S. Kabelac², A.G. Rao³, F. de Domenico³, M. Hoogreef³, L. Van Biert³, F. Yin³, C. Rossignol*, L. Dessemond*, M.C. Steil*, P. Maasº, F. Winterº, C. Warschº, S.S. Venturaᵟ, M. Mettenᵟ, M.P. Heddrichᵟ, S.A. Ansarᵟ ; ¹AIRBUS SAS, Germany ;²Leibniz University Hannover, Germany ;³Technische Universiteit Delft, Netherlands ;*Univ. Grenoble Alpes, Univ. Savoie Mont Blanc, France ;ºBauhaus Luftfahrt e.V., Germany ;ᵟGerman Aerospace Center, German | ||||
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| 10:00 | 10:30 | 15.4.1 |
REDESIGN OF AN AERONAUTICAL COMPOSITE STIFFENED PANEL WITH THE DOUBLE-DOUBLE DESIGN APPROACH A. Riccio¹, A. Garofano¹, G. Rigliaco¹, M. Boccaccio², F. Acerra²; ¹University of Campania “Luigi Vanvitelli”, Italy ;²Leonardo S.p.A., Italy | ||||
| 10:30 | 11:00 | 15.4.2 |
MACRO, MESO AND MICRO SCALE ENERGY EVALUATION IN LAMINATED AND COMPOSITE STRUCTURES USING THE COMPONENT-WISE APPROACH S. Saputo¹, R. Augello¹, E. Carrera, Germany; ¹Department of Aeronautics and Aerospace Engineering, Politecnico, Italy | ||||
| 11:00 | 11:30 | 15.4.3 |
ELECTROMAGNETIC INDUCTION HEATING OF TP-CFRP LAMINATES: FEM MODELLING AND VALIDATION W.J. Vankan¹, N. van Hoorn¹, A.J. de Wit¹, T.P.A. Koenis¹; ¹NLR, Netherlands | ||||
| 11:30 | 12:00 | 15.4.4 |
ON AN EFFICIENT GLOBAL/LOCAL STOCHASTIC METHODOLOGY FOR FAILURE PREDICTION OF AIRCRAFT COMPOSITE STRUCTURES P. Minigher, INEGI / University of Porto / University of Girona, Italy; A. Arteiro¹, A. Turon, University of Girona, Spain; J. Fatemi, Airbus NL, Netherlands; S. Guinard, Airbus SAS, France; L. Barrière, Saint Exupéry, France; P.P. Camanho¹; ¹INEGI / University of Porto, Portugal | ||||
| 12:00 | 12:30 | 15.4.5 |
FATIGUE CRACK LIFE PREDICTION BASED ON BAYESIAN DYNAMIC UPDATE Y. Zhang, China; Y. Ning, China; B. Wang, China; H. Peng, China | ||||
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| 10:00 | 10:30 | 16.4.1 |
THE JOURNEY TOWARDS CONDITION-BASED MAINTENANCE: A FRAMEWORK FOR THE HORIZONTAL TAIL ACTUATOR OF AN ADVANCED JET TRAINER AIRCRAFT L. Baldo¹, A. De Martin¹, M. Terner, Leonardo S.p.A. Aircraft Division, Italy; M. Sorli¹; ¹DIMEAS, Politecnico di Torino, Italy | ||||
| 10:30 | 11:00 | 16.4.2 |
HOLISTIC AND SCALABLE SMART OPTIMIZATION FRAMEWORK FOR PRESCRIPTIVE MAINTENANCE A. Giacotto¹, A.C. Pereira Mesquita¹, H. Costa Marques¹, A. Martinetti, University of Twente, Netherlands; ¹ITA, Brazil | ||||
| 11:00 | 11:30 | 16.4.3 |
HYDROGEN TANKERING: TOOLS FOR ECONOMIC AND ENVIRONMENTAL IMPACT SCENARIO STUDIES G. Sirtori¹, L. Trainelli¹, Z. Lahmam¹; ¹DAER, Politecnico di Milano, Italy | ||||
| 11:30 | 12:00 | 16.4.4 |
AN EMPIRICAL AND CUSTOMISABLE FLEET RENEWAL MODEL FOR PROSPECTIVE SCENARIOS USING OPEN-ACCESS DATA P. Viry¹, T. Planès¹, S. Delbecq¹, L. Joly, ISAE-SUPAERO, Université de Toulouse, France; A. Salgas¹; ¹Fédération ENAC ISAE-SUPAERO ONERA, Université de Toulouse, France | ||||
| 12:00 | 12:30 | 16.4.5 |
A NOVEL DEEP MULTIMODAO INFORMATION FUSION MODEL FOR AERO-ENGINE STATE PREDICTION Y. Huang¹, G. Sun¹, J. Tao¹, J. Feng¹; ¹Fudan University, China | ||||
| additional information (interactive) | 16.4.R |
DIGITALISATION AND SUSTAINABILITY IN CABIN DESIGN: SYNERGIES AND DEPENDENCIES M.C. Berschik¹, S. Wehrend¹, F.N. Laukotka¹, D. Krause¹; ¹Hamburg University of Technology, Germany | |||||
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| 10:00 | 10:30 | 17.4.1 |
Lecture canceled | ||||
| 10:30 | 11:00 | 17.4.2 |
HYDROGEN SAFETY: A COMPARATIVE ANALYSIS OF LEAK DETECTION SENSORS O. Petrella¹, A. Martucci¹, P. Caruso¹, L. Travascio¹, A. Vozella¹; ¹CIRA, Italy | ||||
| 11:00 | 11:30 | 17.4.3 |
VIBRATION ANAYLYSIS AND INFLUENCING FACTOR STUTY OF HELICOPTER HYDRAULIC PIPELINNE S. Yang¹, S. Huang¹, Y. Wang¹, Y.-P. Huang¹; ¹CHRDI, China | ||||
| 11:30 | 12:00 | 17.4.4 |
SENS4ICE EU PROJECT HYBRID ICE DETECTION ARCHITECTURES DEMONSTRATION RESULTS C.W. Schwarz¹, C. Deiler¹, J. Lucke¹, T. Jurkat-Witschas¹, A. Orazzo², B. Thillays²; ¹DLR, Germany ;²Safran Aerosystems, France | ||||
| 12:00 | 12:30 | 17.4.5 |
FLIGHT TEST RESULTS FOR PERFORMANCE-BASED ICE DETECTION C. Deiler, DLR, Germany | ||||
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| 14:30 | 14:55 | 1.5.1 |
APPLICATION OF LAMINAR FLOW CONTROL FOR ENHANCED PERFORMANCE AND REDUCED EMISSIONS J. Crouch, Boeing, United States | ||||
| 14:55 | 15:20 | 1.5.2 |
HIGH ASPECT RATION WING CONCEPTS P. Schmollgruber, ONERA, France | ||||
| 15:20 | 15:45 | 1.5.3 |
RIBLETS IN AVIATION- FIRST EVER INDUSTRIALIZATION WITH AEROSHARK J.U. Müller, Lufthansa, Germany | ||||
| 15:45 | 16:10 | 1.5.4 |
Q&A - MINI PANEL QA. A, | ||||
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| 14:30 | 14:55 | 2.5.1 |
THE NASA X-57 “MAXWELL” DISTRIBUTED ELECTRIC PROPULSION FLIGHT DEMONSTRATOR PROJECT H. Maliska, NASA, United States | ||||
| 14:55 | 15:20 | 2.5.2 |
X-57 TRACTION POWER AND COMMAND SYSTEMS DEVELOPMENT S. Clarke¹, J. Terry¹, K. Harris¹, D. Avanesian¹; ¹NASA, United States | ||||
| 15:20 | 15:45 | 2.5.3 |
FLIGHT PERFORMANCE ESTIMATES FOR THE NASA X-57 DISTRIBUTED ELECTRIC PROPULSION FLIGHT DEMONSTRATOR N. Borer, NASA, United States | ||||
| 15:45 | 16:10 | 2.5.4 |
DISTRIBUTED THRUST TAKEOFF FOR THE NASA X-57 MOD IV FLIGHT DEMONSTRATOR N.K. Borer¹, R.D. Wallace², J.R. Reynolds², D.E. Cox¹, C. Sales², T.L. Williams², W.M. Ringelberg²; ¹NASA Langley Research Center, United States ;²NASA Armstrong Flight Research Center, United States | ||||
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| 14:30 | 14:55 | 3.5.1 |
DATA-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION AND MULTI-FIDELITY DESIGN EXPLORATION USING CONDITIONAL DIFFUSION-BASED GEOMETRY SAMPLING METHOD A. Yang¹, J. Zhang, Shanghai Artificial Intelligence Laboratory, China; J. Li, Institute of High Performance Computing, A*STAR, Singapore; R. Liem¹; ¹Hong Kong University of Science and Technology, Hong Kong SAR of China | ||||
| 14:55 | 15:20 | 3.5.2 |
LATENT SPACE CORRELATION FOR INTERPRETABLE AIRFOIL PARAMETERIZATION USING VARIATIONAL AUTOENCODERS K. Swannet¹, C. Varriale¹, N.A.K. Doan¹; ¹Delft University of Technology, Netherlands | ||||
| 15:20 | 15:45 | 3.5.3 |
RESEARCH ON MULTI-ATTRIBUTE DECISION MAKING AND VERIFICATION METHODS FOR SYSTEMS CONFRONTATION Y. Tong¹, M. Luo¹, Z. Cui¹, Z. Liu¹, Z. Ji¹; ¹Beihang University, China | ||||
| 15:45 | 16:10 | 3.5.4 |
EXPLORATION OF EFFICIENT HYPERPARAMETERS ADAPTION OF SUPPORT VECTOR REGRESSION FOR AERODYNAMIC DESIGN K.-S. Zhang¹, H.-L. Qiao¹, P.-H. Wang¹, Y.-Q. Du¹, Z.-H. Han¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | ||||
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| 14:30 | 14:55 | 4.5.1 |
DUCTED HEAT EXCHANGER THERMAL AND AERODYNAMIC SHAPE OPTIMIZATION E.J. Adler¹, A.H.R. Lamkin¹, J.R.R.A. Martins¹; ¹University of Michigan, United States | ||||
| 14:55 | 15:20 | 4.5.2 |
ANALYZING THE IMPACTS OF SUSTAINABLE POWERTRAINS FOR SHORT-HAUL COMMUTER AIRLINES F. Salucci¹, N. Prabhakar¹, D. Karbowski¹; ¹Argonne National Laboratory, United States | ||||
| 15:20 | 15:45 | 4.5.3 |
LOCAL AIR QUALITY AND NOISE OPTIMIZATION OF A LARGE ASPECT RATIO WINGS WITH DISTRIBUTED HYBRID ELECTRIC PROPULSION R. Cavallaro¹, P. Norczyk Simon¹, A. Cini¹; ¹Universidad Carlos III de Madrid, Spain | ||||
| 15:45 | 16:10 | 4.5.4 |
POWER MANAGEMENT SUPPLY OPTIMIZATION FOR HYBRID-ELECTRIC REGIONAL AIRCRAFT G. Palaia¹, K. Abu Salem¹; ¹Polytechnic of Turin, Italy | ||||
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| 14:30 | 14:55 | 5.5.1 |
ESTABLISHING THE DLR-F25 AS A RESEARCH BASELINE AIRCRAFT FOR THE SHORT-MEDIUM RANGE MARKET IN 2035 S. Wöhler¹, J. Häßy¹, V. Kriewall, TUHH, Germany; ¹DLR, Germany | ||||
| 14:55 | 15:20 | 5.5.2 |
BATTERY PERFORMANCE METRICS FOR LARGE ELECTRIC PASSENGER AIRCRAFT R. de Vries¹, R.E. Wolleswinkel¹, D. Rosen Jacobson¹, M. Bonnema², S. Thiede²; ¹Elysian Aircraft, Netherlands ;²University of Twente, Netherlands | ||||
| 15:20 | 15:45 | 5.5.3 |
CONCEPTUAL DESIGN OF A ZERO-EMISSION REGIONAL AIRCRAFT FOR ENHANCED SHORT-HAUL MOBILITY L. Trainelli¹, C.E.D. Riboldi¹, Y.M. Khan¹, F. Salucci, Argonne National Laboratory, United States; G. Sirtori¹; ¹DAER, Politecnico di Milano, Italy | ||||
| additional information (interactive) | 5.5.R |
DESIGN OF REMOTE-CONTROLLED GROUND BASED AIRCRAFT TUG I. Kopec¹, D. Matyja¹; ¹Polish Air Force University, Poland | |||||
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| 14:30 | 14:55 | 6.5.1 |
DATA-DRIVEN UNSTEADY AERODYNAMIC MODELS FOR AEROELASTIC STABILITY ANALYSES A.C.N. Carloni, Instituto Tecnológico de Aeronáutica, Brazil; J.L.F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil | ||||
| 14:55 | 15:20 | 6.5.2 |
NUMERICAL STUDY OF FLOWS OVER LAUNCH VEHICLES WITH VARIOUS FAIRING BY SECOND-MOMENT CLOSURE DETACHED-EDDY SIMULATION Q. Li¹, G. Wang¹, M. Qin¹, L. Xu¹; ¹Northwestern Polytechnical University, China | ||||
| 15:20 | 15:45 | 6.5.3 |
NUMERICAL ANALYSIS OF GENERALIZED AERODYNAMIC FORCES CONSIDERING LAMINAR-TURBULENT TRANSITION ON A NLF WING C. Sebastia Saez¹, J. Martin Ferres¹, M. Hornung¹; ¹Technical University of Munich, Germany | ||||
| 15:45 | 16:10 | 6.5.4 |
LINEAR SYSTEM TECHNIQUES APPLIED TO NONLINEAR AEROSERVOELASTIC ANALYSES M.V.G. Muniz¹, J.A.A. Lyrio, Aeronautics Institute of Technology, Brazil; J.L.F. Azevedo¹; ¹Institute of Aeronautics and Space, Brazil | ||||
| additional information (interactive) | 6.5.R |
SURROGATE MODELING OF VORTEX SHEDDING TURBINE IN LOW REYNOLDS NUMBER J.L. Kurniawan¹, M. Hu¹; ¹Institut Teknologi Bandung, Indonesia | |||||
| additional information (interactive) | 6.5.R |
PREDICTION OF TRANSIENT DEFORMATION BY COUPLING CFD AND FEM ANALYSIS USING MACHINE LEARNING BASED CORRELATION FUNCTION J. Parez¹, P. Kovar¹, T. Vampola¹; ¹Czech Technical University in Prague, Czech Republic | |||||
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| 14:30 | 14:55 | 7.5.1 |
TRAIN ON SYNTHETIC - TEST ON REAL: DOMAIN ADAPTATION FOR STRAIN-BASED DAMAGE DETECTION ON AN AIRCRAFT WING P. Conen¹, F. Raddatz¹, G. Wende¹; ¹DLR, Germany | ||||
| 14:55 | 15:20 | 7.5.2 |
MACHINE LEARNING AND NUMERICAL OPTIMIZATION OF BIO-INSPIRED 3D-PRINTABLE SANDWICH CORE CELL B. Omede'¹, A.M. Grande¹; ¹Politecnico di Milano, Italy | ||||
| 15:20 | 15:45 | 7.5.3 |
FLUID-STRUCTURE INTERACTION OF TWO-PHASE SCATTERER METAMATERIALS FOR VIBRATION SELF-SUPPRESSION W.H. Yuan¹, Y.J. Chai¹, X.W. Yang¹, F. Ripamonti, Politecnico di Milano, Italy; X. Wang¹, Y.M. Li¹; ¹Xi’an Jiaotong University, China | ||||
| 15:45 | 16:10 | 7.5.4 |
A PHASE FIELD BASED DEEP LEARNING APPROACH FOR MECHANICAL PROPERTY PREDICTION OF SINTERED SILVER IN POWER ELECTRONICS B.R. Yang¹, B. Wan¹, G.C. Fu¹, X.H. Wang¹, X.H. Wang¹, J. Yao¹; ¹Beihang University, China | ||||
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| 14:30 | 14:55 | 8.5.1 |
DATA MINING ANALYSIS ON AERODYNAMIC STEALTH DESIGN PRINCIPLES OF AIRFOIL PROFILES S.-Y. Jin¹, Z.-H. Gao¹, S.-S. Chen¹, Y.-Q. Wang, China Aerodynamics Research and Development Center, China; ¹ Northwestern Polytechnical University, China | ||||
| 14:55 | 15:20 | 8.5.2 |
INTELLIGENT RECONSTRUCTION METHOD OF AIRFOIL FLOW FIELD BASED ON DEEP ATTENTION NETWORK K. Zuo¹, X. Yuan, China Aerodynamics Research and Development Center, China; W. Zhang¹, Z. Ye¹; ¹Northwestern Polytechnical University, China | ||||
| 15:20 | 15:45 | 8.5.3 |
CORRELATION MODELLING OF SURFACE INVISCID FLOW CHARACTERISTICS AND FRICTION DISTRIBUTION BASED ON MACHINE LEARNING S. Zhao¹, W. Zhang¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China | ||||
| 15:45 | 16:10 | 8.5.4 |
DYNAMIC STALL PREDICTION THROUGH COMBINING PHYSICAL MODELS AND MACHINE LEARNING W. Zhang¹, X. Wang¹, J. Kou¹, Z. Liu, The China Aerodynamics Research and Development Center, China; ¹ Northwestern Polytechnical University, China | ||||
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| 14:30 | 14:55 | 9.5.1 |
MULTI SENSOR AND MULTI TASK ALLOCATION BASED ON IMPROVED WHALE OPTIMIZATION ALGORITHM B. Yuan¹, S. Zhang¹, B. Wang, School of Electronic and Information, Northwestern Polytechnica, China; K. Zhang, School of Electronic and Information, Northwestern Polytechnical, China; ¹College of Aerospace Science and Engineering, National Universit, China | ||||
| 14:55 | 15:20 | 9.5.2 |
PRELIMINARY DESIGN OF POWER CONTROL STRATEGIES FOR THE HYBRID-ELECTRIC PROPULSION SYSTEM OF A LIGHTWEIGHT FIXED-WING UAV G. Di Rito¹, A. Suti¹; ¹University of Pisa - Dept. of Civil and Industrial Engineering, Italy | ||||
| 15:20 | 15:45 | 9.5.3 |
DEVELOPMENT OF UAVS/DRONES EQUIPPED WITH THERMAL SENSORS FOR THE SEARCH OF INDIVIDUALS LOST UNDER RUBBLE DUE TO EARTHQUAKE COLLAPSES OR ANY EVENTUALITY REQUIRING SUCH CAPABILITIES J.A. Herrera Velasco, National Autonomous University of Mexico (UNAM), Mexico; H.S. Delgado Guevara, UNAM, Mexico | ||||
| 15:45 | 16:10 | 9.5.4 |
MEASURING THE ANGLE OF ATTACK – PRACTICAL CONSIDERATIONS FOR THE DEVELOPMENT OF FAULT DETECTION RESIDUALS C. Raab¹, N. Fezans¹; ¹DLR (German Aerospace Center) - Institute for Flight Systems, Germany | ||||
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| 14:30 | 14:55 | 10.5.1 |
VIBRATION OF COMPOSITE SHELLS OF REVOLUTION USING EQUIVALENT SINGLE LAYER APPROACH E. Carrera , Politecnico, Italy; V.V. Zozulya, iMex, Ukraine | ||||
| 14:55 | 15:20 | 10.5.2 |
DAMAGE TOLERANCE OF A CURVED COMPOSITE STIFFENED PANEL FABRICATED BY AN OUT OF AUTOCLAVE – LIQUID RESIN INFUSION PROCESS D. Fanteria¹, L. Boni¹, F. Romano, 2CIRA S.C.p.A., Italian Aerospace Research Centre, Italy; ¹University of Pisa, Italy | ||||
| 15:20 | 15:45 | 10.5.3 |
NUMERICAL TOOLS FOR SLOW-GROWTH APPROACHES TO DAMAGE TOLERANT COMPOSITE AERONAUTICAL STRUCTURES M. Khella¹, S. Ghiasvand¹, P. Ballarin¹, F. Panzeri¹, S. Piacquadio¹, A. Airoldi¹; ¹Politecnico di Milano, Italy | ||||
| 15:45 | 16:10 | 10.5.4 |
INVESTIGATING THE EFFECT OF DELAMINATION-INDUCED FRICTIONAL CONTACT ON THE DYNAMIC BEHAVIOR OF LAMINATE STRUCTURES S. Kiasat¹, A.S. Nobari, Aeronautics Engineering Department, Imperial College, United Kingdom; M. Filippi¹, E. Carrera¹; ¹POLITECNICO DI TORINO, Italy | ||||
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| 14:30 | 14:55 | 11.5.1 |
STUDY OF AEROELASTIC PROBLEM OF RUDDER SYSTEM WITH ELECTRIC ACTUATOR AND STRUCTURAL NONLINEARITIES W. Qian¹, W.-Z. Feng, Dalian University of Technology, China; C.-X. Han¹, X.-Y. Ai¹; ¹Daian University of Technology, China | ||||
| 14:55 | 15:20 | 11.5.2 |
NOVEL TEST RIG TO DEMONSTRATE A MULTI FUNCTIONAL FLAP MECHANISM OFFERING A 2ND DEGREE OF FREEDOM J. Docter¹, H. Pijlman¹, D. de Wit², J. Vervliet², J. Katarzynski¹, R. Postma¹, K.-J. Bisschop¹, J. Vroon¹; ¹NLR, Netherlands ;²Asco Industries, Belgium | ||||
| 15:20 | 15:45 | 11.5.3 |
GUST LOAD ALLEVIATION IN A SCALED UAV DEMONSTRATOR A. Herwig¹, M. Haupt¹, T. Brack¹, J. Bustamante¹, S. Heimbs¹; ¹Cluster of Excellence SE²A – Techniche Universität Braunschweig, Germany | ||||
| 15:45 | 16:10 | 11.5.4 |
REDUCED ORDER MODELLING OF UNSTEADY AERODYNAMICS FOR GROUND FLUTTER TEST SYSTEM W.-Z. Feng¹, J.-H. Zhang¹, Z.-H. Liang¹, W. Qian¹; ¹Dalian University of Technology, China | ||||
| additional information (interactive) | 11.5.R |
EXPERIMENTAL INVESTIGATION AND NUMERICAL ANALYSIS OF THE EFFECT OF TEMPERATURE ON THE MECHANICAL PROPERTIES OF AEROSPACE COMPOSITE-METAL HYBRID JOINTS R. Hou¹, B.T. Wang, Department of Strength Design, The First Aircraft Institute of A, China; Z.X. Zhu¹, W.C. Gao¹; ¹Department of Astronautical Science and Mechanics, HIT, China | |||||
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| 14:30 | 14:55 | 12.5.1 |
ROTOR DYNAMIC LOADS CHARACTERISTIC ANALYSIS WITH BLADE TIP TWIST DISTRIBUTION Z. Yu¹, J. Huang¹, Q. Jiang¹, F. Fan, CHRDI , Germany; S. Huang¹; ¹CHRDI, China | ||||
| 14:55 | 15:20 | 12.5.2 |
INVESTIGATING AN OPTIMAL AEROELASTIC DESIGN FOR AIRCRAFT WINGS WITH DISTRIBUTED PROPELLERS MADE OF COMPOSITES M. Abouhamzeh, University of Wolverhampton, United Kingdom; Y. Ma, Bauhaus Aviation Research Institute, Germany | ||||
| 15:20 | 15:45 | 12.5.3 |
EXPERIMENTAL VALIDATION OF THE DYNAMIC FINITE ELEMENT MODEL OF A 1:8 SCALE SEAPLANE USING A LASER DOPPLER VIBROMETER (LDV) F. Lovero¹, G. Biggi¹, S. Lombardi¹, M.A.C. Costa¹, V. Amore¹, E. Cestino¹; ¹Politecnico di Torino, Italy | ||||
| 15:45 | 16:10 | 12.5.4 |
DRIVETRAIN INFLUENCE ON THE LEAD-LAG MOTION OF HELICOPTER ROTORS F. Weiss, DLR, Germany | ||||
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| 14:30 | 14:55 | 13.5.1 |
A MOMENTUM-INTEGRAL METHOD TO CALCULATE WINDAGE LOSSES ON A ROTATING DRUM WITH SUPERPOSED FLOW H. Tuo¹, P. Liu¹, S. Ding¹, T. Qiu¹, C. Liu¹, R. Cheng, AECC Shenyang Engine Research Institute, China; ¹Research Institute of Aero-Engine, Beihang University, China | ||||
| 14:55 | 15:20 | 13.5.2 |
AERODYNAMIC OPTIMIZATION OF HIGH-ALTITUDE PROPELLER COMBINED WITH MACHINE LEARNING METHOD D. Li¹, Z. Ge¹, R. Cui¹, L. Yang¹, C. Wei¹, W. Song, Northwestern Polytechnical University, China; ¹AVIC Aerodynamics Research Institute, China | ||||
| 15:20 | 15:45 | 13.5.3 |
AERODYNAMIC PERFORMANCE OF BLADELESS DUCTED FAN BASED ON EJECTION EFFECT WITH DIFFERENT DESIGN VARIABLES K. Han, China; S. Yu, China; J. Huang, China; J. Bai, China; Y. Qiu, China | ||||
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| 14:30 | 14:55 | 14.5.1 |
TRANSFORMATIVE PEDAGOGY: CO-TEACHING COURSE CLUSTERS THROUGH COMPETITIVE TEAM DESIGNS FOR INNOVATIVE TALENT DEVELOPMENT IN AEROSPACE EDUCATION M. Luo¹, H. Liu¹, X. Zhang¹, Z. Cui¹; ¹Beihang University, China | ||||
| 14:55 | 15:20 | 14.5.2 |
LESSONS LEARNED FROM PROJECT BASED TEACHING IN AEROSPACE AT CHALMERS I. Jonsson¹, C. Xisto¹, V. Chernoray¹, A. Capitao Patrao¹; ¹Chalmers University Of Technology, Sweden | ||||
| 15:20 | 15:45 | 14.5.3 |
INTEGRATING UNMANNED AERIAL SYSTEMS INTO THE INTELLIGENT SYSTEMS ENGINEERING CURRICULUM O.D. Dantsker, Indiana University, United States | ||||
| 15:45 | 16:10 | 14.5.4 |
DLR DESIGN CHALLENGE 2024: DESIGN OF A COST AND ENERGY EFFICIENT REGIONAL AIRCRAFT C. Ehrich¹, L. Kriebel¹, T. Schulz¹, M. Tekkel¹, L. Wauer¹, L. Wenz¹, L. Kugler², S. Müller², C. Niro²; ¹Technical University of Berlin, Germany ;²German Aerospace Center (DLR), Germany | ||||
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| 14:30 | 14:55 | 15.5.1 |
A COMPARSION OF TRAJECTORY GENERATION ALGORITHMS FOR A TERRAIN FOLLOWING FLIGHT H. Lee¹, S. Lee¹; ¹Korea Aerospace University, South Korea | ||||
| 14:55 | 15:20 | 15.5.2 |
A GENETIC ALGORITHM FOR TRAJECTORY GENERATION IN ENGINE-OUT EMERGENCY LANDING SCENARIOS OF COMMERCIAL AIRCRAFT J. Gauci, University of Malta, Malta; B. Zammit, Malta; M. Galea, Malta | ||||
| 15:20 | 15:45 | 15.5.3 |
ATTITUDE CONTROL DESIGN FOR A FLYING-CRAWLING INTEGRATED FLAPPING-WING MICRO AIR VEHICLE Z.Y. Yuan¹, W.Y. Yang¹, J.X. Xuan¹; ¹nwpu, China | ||||
| 15:45 | 16:10 | 15.5.4 |
TRAJECTORY OPTIMIZATION FOR LONG-RANGE AIR-LAUNCHED GLIDING VEHICLES USING CONVEX PROGRAMMING C.-G. Jung¹, C.-H. Lee¹, M.-J. Tahk¹; ¹Korea Advanced Institute of Science and Technology(KAIST), South Korea | ||||
| additional information (interactive) | 15.5.R |
OPTIMAL APPROACH AND DEPARTURE TRAJECTORIES WITH ACOUSTIC FOOTPRINT ASSESSMENT FOR AN AIR MOBILITY QUAD-ROTOR C. Varriale¹, F. Yunus¹, M. Snellen¹; ¹Delft University of Technology, Netherlands | |||||
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| 14:30 | 14:55 | 16.5.1 |
INCREMENTAL NONLINEAR DYNAMIC INVERSION CONTROLLER FOR A FLYING WING OPERATED IN AN AIRBORNE WIND ENERGY SYSTEM D.F. Duda¹, H. Fuest¹, J. Müller¹, T. Islam¹, D. Moormann¹; ¹RWTH Aachen Unitversity, Germany | ||||
| 14:55 | 15:20 | 16.5.2 |
ADVANCED SOLUTIONS AND CHALLENGES IN MULTI-DRONE SYSTEMS FOR SEARCH AND RESCUE MISSIONS: TECHNICAL APPROACHES AND UNRESOLVED MATTER E. D'Amato, Università degli Studi di Napoli Parthenope, Italy | ||||
| 15:20 | 15:45 | 16.5.3 |
HAWK-INSPIRED COOPERATIVE ENCIRCLEMENT GUIDANCE OF FIXED-WING UAV SWARM WITH LIMITED COMMUNICATION IN THREAT SCENARIO B.-Y. Qin¹, D. Zhang¹, S. Tang¹; ¹Northwestern Polytechnical University, China | ||||
| 15:45 | 16:10 | 16.5.4 |
A SIMULINK APPROACH TO MODELING HETEROGENEOUS DRONE FORMATIONS FOR AGENT-BASED SIMULATION G. Raspaolo, Italy; G. D'Alterio, Italy; I. Notaro, Italy; E. D'Amato, Italy | ||||
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| 14:30 | 14:55 | 17.5.1 |
ENHANCED AIRCRAFT TAKEOFF/LANDING SAFETY USING DEEP LEARNING MODEL IN RUNWAY ASSISTANCE SYSTEM N.L. Ywet¹, A.A. Maw¹, J.W. Han¹, J. Chung, Toronto Metropolitan University, Canada; J.W. Chang, Korea Aerospace University, South Korea; J.-W. Lee¹; ¹Konkuk University, South Korea | ||||
| 14:55 | 15:20 | 17.5.2 |
NONLINEAR BEHAVIOR IN AIRCRAFT FUEL GAUGE READINGS: AN EXPLORING ANALYSIS M.A.D. Di Marzo¹, O.A. Gonzatto Junior¹, H.N. Najafabadi, Linköping University – LiU, Sweden; J.H. Bidinotto¹; ¹University of São Paulo - USP, Brazil | ||||
| 15:20 | 15:45 | 17.5.3 |
INTEGRITY MONITORING OF TIGHTLY INTEGRATED BDS/SINS USING MULTI-HYPOTHESIS SOLUTION SEPARATION (MHSS) ALGORITHM S. Sun¹, H. Wang¹, R. Liu¹, S. Kuang¹, W. Chen¹; ¹Civil Aviation University of China, China | ||||
| 15:45 | 16:10 | 17.5.4 |
DEVELOPMENT OF THRUST CONTROL SYSTEM FOR SPACECRAFT’S DOCKING MANEUVER H. Lee¹, H. Lee¹, S. Lee¹; ¹Korea Aerospace University, South Korea | ||||
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| 16:30 | 17:00 | 1.6.1 |
NASA HI-RATE COMPOSITE AIRCRAFT MANUFACTURING (HICAM) PROJECT OVERVIEW R. Young, NASA (LaRC), United States | ||||
| 17:00 | 17:30 | 1.6.2 |
SUSTAINABLE HIGH RATE COMPOSITE MANUFACTURE P.C. Crothers, Boeing Aerostructures Australia, Australia | ||||
| 17:30 | 18:00 | 1.6.3 |
FUSELAGE, CABIN & CARGO AND EMPENNAGE OF TOMORROW @ AIRBUS COMMERCIAL - NEW FUSELAGE DESIGN & MATERIALS Y.C. Roth, Airbus, Germany | ||||
| 18:00 | 18:30 | 1.6.4 |
WING OF TOMORROW - LONGER, LEANER, LIGHTER M. Cantrell, Airbus, United Kingdom | ||||
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| 16:30 | 17:00 | 2.6.1 |
AFC FLIGHT-DEMONSTRATOR X-65 PROGRAM OVERVIEW M.L. Post, DARPA/TTO, United States | ||||
| 17:00 | 17:30 | 2.6.2 |
INTEGRATING ACTIVE FLOW CONTROL ON AIRCRAFT J.F. Langford, Aurora Flight Sciences, A Boeing Company, United States | ||||
| 17:30 | 18:00 | 2.6.3 |
THE PATH TO TRANSITION ACTIVE FLOW CONTROL TECHNOLOGY R. Woszidlo, The Boeing Company, United States | ||||
| 18:00 | 18:30 | 2.6.4 |
PERSPECTIVES ON FLOW CONTROL APPLICATIONS FOR LARGE TRANSPORT AIRCRAFT D. Reckzeh, Airbus, Germany | ||||
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| 16:30 | 17:00 | 3.6.1 |
EU IMPACT MONITOR PROJECT - OVERVIEW AND APPROACH P. Shiva Prakasha¹, P. Ratei¹, M. Van Eenige¹, T. Lefebvre, The French Aerospace Lab, France; M. Alder¹, U. Gupta, Cranfield University , United Kingdom; M. Antonio Solazzo, CIRA, Italy; B. Nagel¹; ¹German Aerospace Center - DLR, Germany | ||||
| 17:00 | 17:30 | 3.6.2 |
EVALUATION OF ASWING FOR OVERALL AIRCRAFT DESIGN OF UNCONVENTIONAL CONFIGURATIONS. APPLICATION TO JOINED WINGS WITH FOLDING WINGTIPS R. Jan¹, S. Delbecq¹, E. Benard¹; ¹ISAE-Supaero, France | ||||
| 17:30 | 18:00 | 3.6.3 |
IDENTIFICATION OF THE IMPACT OF BLOWING ON THE AERODYNAMIC MODEL OF AN AIRPLANE WITH DISTRIBUTED ELECTRIC PROPULSION S. Cacciola¹, L. Bottà¹, C.E.D. Riboldi¹, L. Trainelli¹; ¹Politecnico di Milano, Italy | ||||
| 18:00 | 18:30 | 3.6.4 |
MULTIDISCIPLINARY PRELIMINARY DESIGN PROCESS OF HYBRID-ELECTRIC SEAPLANE M. Tuccillo¹, P. Della Vecchia¹; ¹University of Naples Federico II, Italy | ||||
| additional information (interactive) | 3.6.R |
TRANSLATING THE CONCEPT OF SUSTAINABILITY FOR THE DETERMINATION OF REQUIREMENTS FOR THE DESIGN OF FUTURE AIRCRAFT L. Paletti¹, L. Boggero¹, G. Wende¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany | |||||
| additional information (interactive) | 3.6.R |
PERFORMANCE ENHANCEMENTS BETWEEN DIFFERENT APPLICATIONS OF ALTERNATIVE FUELS AND NOVEL AIRCRAFT CONFIGURATIONS J.L.C. Chan¹, Y. Sun¹, H. Smith, Cranfield University , United Kingdom; ¹Cranfield University, United Kingdom | |||||
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| 16:30 | 17:00 | 4.6.1 |
EXPLORATION AND EVALUATION OF KNOWLEDGE-BASED ENGINEERING APPROACH FOR LIQUID HYDROGEN TANK INTEGRATION IN EXISTING FUSELAGE N. Bhargav¹, V. Elangovan¹, R.C. Munjulury, Linköping University, Sweden; C. Hesse², P. Satwan²; ¹Linköping University/DLR, Germany ;²Institute for System Architectures in Aeronautics, DLR, Germany | ||||
| 17:00 | 17:30 | 4.6.2 |
INCREMENTAL TRADE-OFF STUDY OF A HYDROGEN FUEL CELL-BASED PROPULSION SYSTEM USING MDAO TECHNIQUES R. di Giuseppe, ISAE-Supaero, SafranTech, France; S. Delbecq¹, V. Pauvert, SafranTech, France; V. Pommier-Budinger¹; ¹ISAE-SUPAERO, France | ||||
| 17:30 | 18:00 | 4.6.3 |
METHODOLOGIES FOR THE PRELIMINARY SIZING OF HYDROGEN-POWERED AIRCRAFT AND SUPPORTING AIRPORT INFRASTRUCTURES L. Trainelli¹, C.E.D. Riboldi¹, G. Sirtori¹; ¹DAER, Politecnico di Milano, Italy | ||||
| 18:00 | 18:30 | 4.6.4 |
CFD STUDY OF AIR SUPPLY SYSTEM FOR COOLING OF A HYDROGEN POWERED UNMANNED SEAPLANE AND REDUCTION OF THE RESULTING DRAG A. Marsano¹, F. Bustos Ortega¹, G. Santarella¹, S.G. Soundararajan¹, F. Giargia¹; ¹Politecnico di Torino, Italy | ||||
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| 16:30 | 17:00 | 5.6.1 |
INTEGRATED SIZING OF AN ELECTRIFIED TILT-WING AIRCRAFT FOR VERTICAL AND CONVENTIONAL TAKEOFF AND LANDING A.A. Mishra¹, B. Kunwar¹, I. Chakraborty¹; ¹Auburn University, United States | ||||
| 17:00 | 17:30 | 5.6.2 |
IMPACT OF WELL-TO-TANK EFFICIENCY AND EMISSIONS ON HYBRID AIRCRAFT DESIGN OPTIMIZATION M. Blandino¹, M.M. Molinari¹, J. Liberatori¹, P.P. Ciottoli¹, R. Malpica Galassi¹; ¹Sapienza Università di Roma, Italy | ||||
| 17:30 | 18:00 | 5.6.3 |
MASS AND POWER ESTIMATIONS IN PRELIMINARY FLIGHT CONTROL SYSTEM DESIGN S.M. Lübbe¹, M. Schäfer¹, O. Bertram¹; ¹German Aerospace Center (DLR), Germany | ||||
| 18:00 | 18:30 | 5.6.4 |
Lecture canceled | ||||
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| 16:30 | 17:00 | 6.6.1 |
ENHANCING EFFICIENCY FOR UNSTEADY CFD COMPUTATIONS IN AERONAUTICS M. Carlsson¹, P. Eliasson¹, P. Weinerfelt¹; ¹Saab, Sweden | ||||
| 17:00 | 17:30 | 6.6.2 |
ANALYSIS OF THE R FAMILY OF LIMITERS APPLIED TO HIGH-ORDER FR/CPR SCHEMES FOR THE SIMULATION OF SUPERSONIC FLOWS F.B. Oliveira, Instituto Tecnologico de Aeronautica, Brazil; J.L.F. Azevedo, Instituto de Aeronautica e Espaco, Brazil; Z.J. Wang, University of Kansas, United States | ||||
| 17:30 | 18:00 | 6.6.3 |
A HIGH-PRECESION PSEUDO ARC-LENGTH METHOD WITH POSITIVE VALUE PRESERVATION PROPERTIES BASED ON TV SPLITTING C. Wang¹, P. Li¹, L. He¹, G. Li¹, H. Dai¹; ¹Chinese Aeronautical Establishment, China | ||||
| 18:00 | 18:30 | 6.6.4 |
A BOUNDARY INTEGRAL EQUATION FORMULATION FOR POTENTIAL COMPRESSIBLE FLOWS AROUND DEFORMABLE BODIES E. Levati¹, C. Pasquali¹, G. Bernardini¹, M. Gennaretti¹; ¹Roma Tre University, Italy | ||||
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| 16:30 | 17:00 | 7.6.1 |
EXPERIMENTAL INVESTIGATION OF THE DLR-F23 CONFIGURATION AT TRANSONIC SPEEDS USING FAST-RESPONSE PRESSURE-SENSITIVE PAINT P. Hartl¹, M. Ritschel¹, M. Braune¹, H. Mai¹; ¹German Aerospace Center (DLR), Germany | ||||
| 17:00 | 17:30 | 7.6.2 |
ASSESSING THE SONIC BOOM OF A FULL-SIZE AIRCRAFT FROM FREE FLIGHT TESTS ON A SUB-SCALE MODEL G. Fasulo¹, L. Federico¹; ¹Italian Aerospace Research Centre (CIRA), Italy | ||||
| 17:30 | 18:00 | 7.6.3 |
EFFECT OF FREESTREAM DISTURBANCES ON BOUNDARY LAYER TRANSITION IN HYPERSONIC WIND TUNNEL J. Yuan¹, S. Yu¹, Z. Qian¹; ¹AVIC Aerodynamics Research Institute, China | ||||
| 18:00 | 18:30 | 7.6.4 |
ELECTRIC FIELD MEASUREMENT IN GLOW DISCHARGE PLASMA INTERACTING WITH SHOCK WAVE IN HYPERSONIC FLOW N. Cao Van¹, H. Itoh¹, M. Mizoguchi¹, A. Uenaka¹; ¹National Defense Academy of Japan, Japan | ||||
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| 16:30 | 17:00 | 8.6.1 |
SIMULATION OF AN INSTALLED PROPELLER BY MEANS OF STEADY AND UNSTEADY BODY-FORCE MODELING H. Pantel¹, F. Falissard¹, G. Dufour, ISAE-SUPAERO, France; ¹ONERA, France | ||||
| 17:00 | 17:30 | 8.6.2 |
EXPERIMENTAL MEASUREMENTS OF SLIPSTREAM DEFORMATION FOR AN INSTALLED DISTRIBUTED PROPELLER CONFIGURATION. R.R. Duivenvoorden¹, F. do Nascimento Monteiro¹, T. Sinnige¹; ¹Delft University of Technology, Netherlands | ||||
| 17:30 | 18:00 | 8.6.3 |
AERODYNAMIC PERFORMANCE AND INTERACTION EFFECTS OF AN OVER-THE-WING DISTRIBUTED-PROPELLER SYSTEM IN CRUISE CONDITIONS R. de Vries¹, T. Sinnige¹, L.L.M. Veldhuis¹; ¹Delft University of Technology, Netherlands | ||||
| 18:00 | 18:30 | 8.6.4 |
Lecture canceled | ||||
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| 16:30 | 17:00 | 9.6.1 |
COMPARING THE CAPACITY OF DIFFERENT VERTIPORT TOPOLOGIES USING DISCRETE EVENT SIMULATION E. Wille, RWTH Aachen University, Germany | ||||
| 17:00 | 17:30 | 9.6.2 |
DEMAND CAPACITY BALANCING FOR URBAN AIR MOBILITY USING MULTIAGENT SIMULATION G. Sato, Electronic Navigation Research Institute, Japan | ||||
| 17:30 | 18:00 | 9.6.3 |
DESIGN OF A UAM GROUND INFRASTRUCTURE NETWORK WITH RESPECT TO MAINTENANCE CAPACITY REQUIREMENTS M. Swaid, German Aerospace Center (DLR), Germany; S. Papakonstantinou¹, D. Kloock-Schreiber¹, V. Gollnick¹; ¹Hamburg University of Technology (TUHH), Germany | ||||
| 18:00 | 18:30 | 9.6.4 |
AIRPORT INFRASTRUCTURE SIZING FOR A REGIONAL ELECTRIC AVIATION NETWORK F. Vehlhaber¹, M. Salazar¹; ¹Eindhoven University of Technology, Netherlands | ||||
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| 16:30 | 17:00 | 10.6.1 |
STIMULATED THERMOGRAPHY AS NON-DESTRUCTIVE TESTING TO ASSESS THE STRUCTURAL INTEGRITY OF AERONAUTICAL COMPONENT IN CFRP G. Masciopinto¹, E. D'Accardi¹, D. Palumbo¹, U. Galietti¹; ¹Polytechnic University of Bari, Italy | ||||
| 17:00 | 17:30 | 10.6.2 |
NUMERICAL ANALYSIS OF PROCESS-INDUCED DEFORMATIONS AND STRESSES IN AERONAUTICAL COMPOSITE COMPONENTS R. Masia¹, M. Petrolo¹, E. Zappino¹, N. Zobeiry, University of Washingthon, United States; E. Carrera¹; ¹Politecnico di Torino, Italy | ||||
| 17:30 | 18:00 | 10.6.3 |
Lecture canceled | ||||
| 18:00 | 18:30 | 10.6.4 |
ELASTIC/PLASTIC SEMI-ANALYTICAL METHOD FOR ARBITRARY CURVED SURFACES OF SCARF REPAIRED COMPOSITES Y. Liu¹, B. Liu¹; ¹Northwestern Polytechnical University, China | ||||
| additional information (interactive) | 10.6.R |
A METHOD FOR OPTIMISING THE ARRANGEMENT OF INTERNAL CHANNELS IN AIRCRAFT HYDRAULIC MANIFOLDS MANUFACTURED BY ADDITIVE MANUFACTURING D.-B. Li, China; H.-X. Huang, China; X.-C. Liu, China; P.-Y. Hou, China; H.-H. Liao, China | |||||
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| 16:30 | 17:00 | 11.6.1 |
MULTI-OBJECTIVE DESIGN OPTIMIZATION OF A MORPHING AILERON FOR A HYBRID ELECTRIC REGIONAL AIRCRAFT A. De Gaspari¹, V. Cavalieri¹, M. Corti¹, S. Ricci¹; ¹Politecnico di Milano, Italy | ||||
| 17:00 | 17:30 | 11.6.2 |
ADAPTIVE WING FLUTTER SUPPRESSION BY MEANS OF MULTIPLE TRAILING EDGE CONTROL SURFACES - A COMPARATIVE STUDY C.R. Vindigni¹, G. Mantegna¹, A. Esposito¹, C. Orlando¹, A. Alaimo¹; ¹Kore University of Enna, Italy | ||||
| 17:30 | 18:00 | 11.6.3 |
DESIGN OF A BODY FREEDOM FLUTTER FLIGHT MODEL WITH CONVENTIONAL CONFIGURATION X. Tian¹, Y. Gu¹, Z. Yang¹; ¹Northwestern Polytechnical University, China | ||||
| 18:00 | 18:30 | 11.6.4 |
Lecture canceled | ||||
| additional information (interactive) | 11.6.R |
MODELING AND VALIDATION OF MORPHING WING TRAILING EDGE BASED ON ZERO POISSON'S RATIO HONEYCOMB S.-Y. Sun¹, H.-Z. Wang¹, R. Yang¹, W. Qian¹; ¹Dalian University of Technology, China | |||||
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| 16:30 | 17:00 | 12.6.1 |
ADVANCED MULTIDISCIPLINARY DESIGN OF NEXT-GENERATION GREEN AIRCRAFT L. Pustina¹, R.M. Galassi¹, M. Blandino¹, F. Mastroddi¹; ¹Sapienza University of Rome, Italy | ||||
| 17:00 | 17:30 | 12.6.2 |
OPTIMIZATION OF COMPOSITE WING STRUCTURE FOR TILT-DUCT AIRCRAFT CONSIDERING DISCRETE AND CONTINUOUS DESIGN VARIABLES S.-R. Xu, China; Y.-T. Zhang, China; J.-F. Zhang, China; Y. Zheng, China; Y.-L. Liu, China | ||||
| 17:30 | 18:00 | 12.6.3 |
A PRELIMINARY METHODOLOGY TO ASSESS GUST SPECTRA VIA SATELLITE DATA E. Carrera¹, A. Pagani¹, M. Valente¹, G. Palaia¹; ¹Politecnico di Torino, Italy | ||||
| 18:00 | 18:30 | 12.6.4 |
AEROELASTIC DIVERGENCE AND FLUTTER ANALYSIS OF A WING WITH ALL MOVING WING TIP W. Wang¹, W. Qian¹, X. Ai¹; ¹Dalian University of Technology, China | ||||
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| 16:30 | 17:00 | 13.6.1 |
GRADIENT-BASED OPTIMIZATION OF AN AXIAL COMPRESSOR UNDER INLET DISTORTION USING BODY-FORCE MODELING C. Dosne¹, R. Barrier¹, S. Bourasseau¹, M. Carini¹, A. Dumont¹, J. Peter¹; ¹ONERA, France | ||||
| 17:00 | 17:30 | 13.6.2 |
EFFECT OF POPULAR ADDITIVE MANUFACTURING TECHNOLOGIES ON THE PERFORMANCE AND ACOUSTICS OF UAV PROPELLERS J. García-Tíscar¹, P. Quintero¹, F.N. Ramírez¹, A. Cremades, KTH Royal Institute of Technology, Sweden; ¹Universitat Politècnica de València, Spain | ||||
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| 16:30 | 17:00 | 14.6.1 |
SAFETY-DRIVEN BASELINING OF HYBRID ELECTRIC AIRCRAFT ELECTRICAL POWER SYSTEM ARCHITECTURES K. Fong¹, P. Norman¹, C.E. Jones¹; ¹University of Strathclyde, United Kingdom | ||||
| 17:00 | 17:30 | 14.6.2 |
EVALUATION AND SIMULATION OF PARALLEL HYBRID ELECTRIC PROPULSION WITH REAL FLIGHT DATA H. Murphy¹, C. Gallagher¹, C. Stuart¹, S. Spence¹, S. Fitzgerald, Ryanair DAC, Ireland; ¹Dept. of Mechanical Engineering, Trinity College Dublin, Ireland | ||||
| 17:30 | 18:00 | 14.6.3 |
PROJECTION OF KEY POWERTRAIN COMPONENT FIGURES OF MERIT FOR OVERALL ASSESSMENT OF ELECTRIC FLIGHT SCENARIOS A. Link¹, S. de Graaf¹; ¹German Aerospace Center (DLR), Germany | ||||
| 18:00 | 18:30 | 14.6.4 |
AIRPORT CHARGING SYSTEM DESIGNS AND POWER MANAGEMENT FOR MEGAWATT-LEVEL CHARGING OF BATTERY-ELECTRIC AIRCRAFT J. Hellgren¹, M. Persson¹, H. Alfredsson¹; ¹RISE Research Institutes of Sweden, Sweden | ||||
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| 16:30 | 17:00 | 15.6.1 |
STUDY ON CONFIGURATIONS OF AIRBORNE LAUNCH SYSTEM FOR DELIVERY OF SMALL PAYLOAD TO LOW EARTH ORBIT T. Goetzendorf-Grabowski¹, L. Kiszkowiak², A. Kwiek¹, P. Zalewski², K. Chudy², M. Figat¹; ¹Warsaw University of Technology, Poland ;²Military University of Technology, Poland | ||||
| 17:00 | 17:30 | 15.6.2 |
ASSISTED AND AUTOMATED AERIAL REFUELLING – OVERVIEW OF THE CONDUCTED RESEARCH AT THE GERMAN AEROSPACE CENTER (DLR) T. Jann¹, N. Fezans¹, A. Koloschin¹, S.-O. Schmidt¹, P. Link¹, J. Ament¹, S. Krause¹; ¹German Aerospace Center (DLR), Institute of Flight Systems, Germany | ||||
| 17:30 | 18:00 | 15.6.3 |
Lecture canceled | ||||
| 18:00 | 18:30 | 15.6.4 |
INFLUENCE OF CONTROL POWER RATE ON HIGH-ALPHA ROLL MANOEUVRABILITY P. Månsson, Saab AB, Sweden | ||||
| additional information (interactive) | 15.6.R |
STRUCTURED H-INFINITY DESIGN OF PREDICTORS FOR THE MONITORING OF AN AIRCRAFT IN ITS FLIGHT ENVELOPE K.H. Kienitz, Instituto Tecnologico de Aeronautica, Brazil; A. Gonzalez Sorribes¹, R. Sanz Diaz¹, C. Braga de Mendonça, Boeing Brasil, Brazil; P.J. Garcia¹; ¹Universitat Politecnica de Valencia, Spain | |||||
| additional information (interactive) | 15.6.R |
DYNAMICS ANALYSIS AND CONTROL OF A LARGE WINGSPAN FLAPPING-WING VEHICLE C. Zhai¹, B. Song¹, Q. Fu¹, J. Xuan¹, J. Li¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China | |||||
| additional information (interactive) | 15.6.R |
DATA-DRIVEN MODEL DISCOVERY AND CONTROL OF HIGH-PERFORMANCE TRAINER AIRCRAFT VIA SPARSE IDENTIFICATION OF NONLINEAR DYNAMICS M.-W. Kang¹, D.-W. Lee², S.-H. Yun¹, H.-C. Bang²; ¹ADD, South Korea ;²KAIST, South Korea | |||||
| additional information (interactive) | 15.6.R |
GROUND EFFECT ON A SLENDER 65º DELTA WING WITH SIDESLIP, IMAGE METHOD, USING EULER R.K. Nangia¹, T. Nangia¹; ¹Nangia, United Kingdom | |||||
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| 16:30 | 17:00 | 16.6.1 |
REDESIGN AND MACHINING OF LEADING EDGE OF TRANSONIC COMPRESSOR BLADE IN ROBOTIC GRINDING OPERATION H. Li¹, L. Zou¹, W. Wang¹, L. Gui¹; ¹Chongqing University, China | ||||
| 17:00 | 17:30 | 16.6.2 |
DESIGN OF A SUSTAINABLE FLEXFORMING PROCEDURE FOR AERO ENGINE COMPONENTS IS ALLOY 718 P. Ottosson¹, E.-L. Westman¹, I. Nygren, Quintus Technologies, Sweden; T. Pettersson, Permanova LaserTool in Blekinge, Sweden; F. Niklasson², L.-E. Brattström²; ¹RISE Research Institutes of Sweden, Sweden ;²GKN Aerospace Engine Systems Sweden, Sweden | ||||
| 17:30 | 18:00 | 16.6.3 |
PRESERVING HUMAN EXPERTISE: EXPLORING MIXED REALITY TRAJECTORY PLANNING FOR ROBOTIC BELT GRINDING W.-X. Wang¹, H.-L. He¹, T.-Y. Zhou, Cardiff University, United Kingdom; L. Wan¹; ¹Chongqing University, China | ||||
| 18:00 | 18:30 | 16.6.4 |
A DIGITAL METHOD FOR THE COMPENSATED MOLD DESIGN OF COMPOSITE PARTS E. Delsol¹, I. Taouil¹, W. Azoti², B. Castanie², P. Olivier², L. Ratsifandrihana, Segula, France; ¹Segula - ICA, France ;²ICA, France | ||||
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| 16:30 | 17:00 | 17.6.1 |
ANGLE AND DISTANCE EFFECT ON PHOSPHOR THERMOMETRY Q. Yin¹, Y. Quan¹, L. Ma¹, J. Liu¹, J. Chai¹, J. Liu¹, L. Zhang¹; ¹Beihang University, China | ||||
| 17:00 | 17:30 | 17.6.2 |
VOID FRACTION CALCULATION MODEL BASED ON TWO-PHASE FLOW PATTERNS IN THE SCAVENGE PIPE J.-W. Xie¹, P.-F. Zhu¹, J.-P. Hu¹, Y.-G. Lyv¹, Z.-X. Liu¹; ¹Northwestern Polytechnical University, China | ||||
| 17:30 | 18:00 | 17.6.3 |
A STUDY ON THE AIRLOCK MECHANISM OF THE OIL SUPPLY PUMP IN AERO-ENGINE LUBRICATING OIL SYSTEM S. Zhang, China; P.-F. Zhu, China; H. Fan, China; Z.-X. Liu, China | ||||
| 18:00 | 18:30 | 17.6.4 |
POTENTIAL APPLICATION OF PHASE CHANGE MATERIALS FOR THERMAL MANAGEMENT SYSTEM OF NEXT GENERATION AIRCRAFT E. Revello¹, M. Boccaccio, Leonardo Labs, Italy; F. Acerra, Leonardo SpA, Italy; A. Monteverde¹; ¹Politecnico di Torino, DISAT, Italy | ||||
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| 11:00 | 11:25 | 1.7.1 |
BARRIERS TO MW CLASS ELECTRIFIED POWERTRAIN AIRCRAFT PROPULSION SYSTEMS G. Bezos O Connor, NASA (LaRC), United States | ||||
| 11:25 | 11:50 | 1.7.2 |
NASA HYBRID THERMALLY EFFICIENT CORE (HYTEC) PROJECT OVERVIEW A.L. Nerone¹, J.M. Haglage¹, L.M. Nakley¹, R. Tornabene¹; ¹NASA (GRC), United States | ||||
| 11:50 | 12:15 | 1.7.3 |
JAXA EN-CORE PROJECT OVERVIEW AND ACHIEVEMENTS T. Yamane, Japan Aerospace Exploration Agency, Japan | ||||
| 12:15 | 12:40 | 1.7.4 |
Q&A - MINI PANEL QA. A, | ||||
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| 11:00 | 11:25 | 2.7.1 |
A CFD VALIDATION ECOSYSTEM TO ADVANCE THE PREDICTION OF LOW-SPEED AERODYNAMICS J.P. Slotnick, Boeing, United States | ||||
| 11:25 | 11:50 | 2.7.2 |
CHALLENGES IN GEOMETRY DEVELOPMENT FOR THE CRM-HL ECOSYSTEM A.M. Clark¹, D.S. Lacy¹; ¹Boeing Commercial Airplanes, United States | ||||
| 11:50 | 12:15 | 2.7.3 |
NASA CONTRIBUTIONS TO THE HIGH LIFT COMMON RESEARCH MODEL ECOSYSTEM M. Rivers, United States | ||||
| 12:15 | 12:40 | 2.7.4 |
THE CRM-HL ECOSYSTEM - DLR CONTRIBUTIONS R. Rudnik¹, S. Pülm¹, F. Schmidt¹, J. Wild¹, A. Schröder¹, C. Spehr¹, P. Mühlmann¹; ¹DLR, Germany | ||||
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| 11:00 | 11:25 | 3.7.1 |
CLIMATE IMPACT AND ECONOMIC ASSESSMENT OF LIQUID HYDROGEN AND SYNTHETIC KEROSENE LONG-RANGE AIRCRAFT CONCEPTS S. Wöhler¹, K. Buchtal¹, M. Iwanizki¹, J. Häßy¹, K. Dahlmann¹, C. Lois¹, M. Hepperle¹; ¹DLR, Germany | ||||
| 11:25 | 11:50 | 3.7.2 |
SUSTAINABLE AVIATION IN NORDIC COUNTRIES C. Jouanet¹, K. Amadori¹, E. Espinoza Juarez¹; ¹Linköpings University, Sweden | ||||
| 11:50 | 12:15 | 3.7.3 |
A PROPOSAL TOWARDS A STEP CHANGE FROM ECO-DRIVEN TO SUSTAINABILITY-DRIVEN DESIGN OF AIRCRAFT COMPONENTS A. Filippatos¹, D.N. Markatos¹, A. Theochari¹, S. Malefaki¹, T. Kalampoukas¹, S.G. Pantelakis¹; ¹University of Patras, Greece | ||||
| 12:15 | 12:40 | 3.7.4 |
ON THE EXISTENCE OF A FAMILY OF IDEAL AIRCRAFT CONFIGURATIONS R.J. Huyssen, CSIR, South Africa; G.R. Spedding, University of Southern California, United States | ||||
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| 11:00 | 11:25 | 4.7.1 |
CRYOGENIC TANK SIZING MODEL FOR THE CONCEPTUAL DESIGN OF HYDROGEN-POWERED AIRCRAFT G. Licheva¹, S. Liscouët-Hanke¹; ¹Concordia University, Canada | ||||
| 11:25 | 11:50 | 4.7.2 |
HYDROGEN STORAGE SYSTEM DESIGN: CASE STUDIES FOR AIRBORNE APPLICATION F. Mazzoni¹, G. Accardo², R. Biga², E. Brusa¹, C. Delprete¹, C.A. Manrique-Escobar², V. Vercella²; ¹Politecnico di Torino, Italy ;²Leonardo S.p.A., Italy | ||||
| 11:50 | 12:15 | 4.7.3 |
INTEGRATING CRYOGENIC TANKS MODEL IN HYDROGEN AIRCRAFT DESIGN FOR PARAMETRIC PERFORMANCE ANALYSIS R. Parello, ONERA/ISAE-SUPAERO, France; S. Defoort, ONERA, France; E. Benard¹, Y. Gourinat¹; ¹ISAE-SUPAERO, France | ||||
| 12:15 | 12:40 | 4.7.4 |
HYDROGEN AIRLINER TANK OPTIMISATION P. De Felipe¹, C. Cumpsty¹, I. Iturriaga¹, H. Dance¹; ¹ZeroAvia, United Kingdom | ||||
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| 11:00 | 11:25 | 5.7.1 |
ARCHITECTURE DESIGN FOR A COMMERCIALLY VIABLE HYDROGEN-ELECTRIC POWERED RETROFITTED REGIONAL AIRCRAFT B. Rietdijk¹, M. Selier¹; ¹Conscious Aerospace, Netherlands | ||||
| 11:25 | 11:50 | 5.7.2 |
ENVIRONMENTAL IMPLICATIONS OF HYBRID-ELECTRIC REGIONAL AIRCRAFT: EMISSIONS AND CLIMATE CHANGE K. Abu Salem¹, G. Palaia¹; ¹Politecnico di Torino, Italy | ||||
| 11:50 | 12:15 | 5.7.3 |
CLEANSKY2/ CLEAN AVIATION LARGE PASSENGER AIRCRAFT FOR MORE SUSTAINABLE COMMERCIAL FUSELAGE TECHNOLOGIES – MAJOR ACHIEVEMENTS Y.C. Roth¹, R. Herrmann¹, C. Sanchez Santos, Aernnova, Spain; M. Uellendahl, Airbus Aerostructures, Germany; J. Koopman, GKN Fokker Aerospace, Netherlands; A. Henneberg, Diehl Aviation, Germany; J. Kos, Royal Netherlands Aerospace Centre, Netherlands; I.F. Villegas, Delft University of Technology, Netherlands; A. Choudhary, SAMXL, Netherlands; L. Larsen, DLZ Zentrum für Leichtbauproduktionstechnologie, Germany; S. Ferstl, Premium Aerotec, Germany; B. Diehl, Fraunhofer, Germany; F. Emanuelsson, Saab Aerospace Systems, Sweden; J.-B. Sinechal¹, M. Pleth¹, K. Atherton¹; ¹Airbus, Germany | ||||
| 12:15 | 12:40 | 5.7.4 |
ANALYSIS OF BATTERY WEIGHT REQUIREMENTS IN THE DESIGN OF HYBRID ELECTRIC POWERED AIRCRAFT D. Liu¹, Z. Chen¹, Z. Guo¹, B. Zhu¹, G. Jia¹, X. Yang¹; ¹National University of Defense Technology, China | ||||
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| 11:00 | 11:25 | 6.7.1 |
A BRIEF REVIEW OF PANEL AEROELASTICITY WITH SHOCK INTERACTION A. Shi, China; Y. He, China; E.H. Dowell, United States | ||||
| 11:25 | 11:50 | 6.7.2 |
ACTIVE-PASSIVE HYBRID CONTROL OF SHOCK BUFFET C.Q. Gao, China; K. Ren, China; W.W. Zhang, China | ||||
| 11:50 | 12:15 | 6.7.3 |
WALL TEMPERATURE EFFECTS ON AERODYNAMIC HEATING MECHANISMS IN SHOCK WAVE TURBULENT BOUNDARY LAYER INTERACTION Z.Y. Tang, China; H.N. Xu, China; X.Y. Li, China; J. Ren, China | ||||
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| 11:00 | 11:25 | 7.7.1 |
PSYCHOACOUSTICAL ANALYSIS OF SYNTHESIZED MOTOR-PROPELLER ROTOR SYSTEM NOISE J.H. Jeong, Korea Aerospace Research Institute, South Korea; J.W. Ko, Korea Aerospace University, South Korea | ||||
| 11:25 | 11:50 | 7.7.2 |
INFLUENCE OF MOTOR CHARACTERISTICS ON OPTIMAL PROPROTOR DESIGN S. Shahjahan¹, D. Verstraete¹; ¹The University of Sydney, Australia | ||||
| 11:50 | 12:15 | 7.7.3 |
NOVEL SOFTWARE-DRIVEN VARIABLE-PITCH AND LEVEL FLIGHT CONTROL SYSTEM: PRINCIPLES AND APPLICATIONS FOR SMALL AIRCRAFT WITH A QUADROTOR CASE STUDY X. Xiong¹, S. Wu¹; ¹International WYNNBEAR Advanced AeroTech Innovation, United States | ||||
| 12:15 | 12:40 | 7.7.4 |
CHALLENGES OF INTEGRATING PHOTOVOLTAIC CELLS ONTO THE WINGS OF AN UNMANNED SOLAR-POWERED AIRCRAFT R. Lopusiewicz¹, N. Ksiazek¹; ¹AGH University of Krakow, Poland | ||||
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| 11:00 | 11:25 | 8.7.1 |
SONIC BOOM ANALYSIS OF DIFFERENT SUPERSONIC AIRCRAFT A. Glorioso¹, F. Petrosino², M. Barbarino², G. Pezzella¹, A. Viviani¹; ¹University of Campania, Italy ;²CIRA, Italy | ||||
| 11:25 | 11:50 | 8.7.2 |
SPARSE POLYNOMIAL CHAOS-BASED SONIC BOOM UNCERTAINTY QUANTIFICATION AND AERODYNAMIC/SONIC BOOM ROBUST DESIGN OPTIMIZATION UNDER MULTI-PARAMETER UNCERTAINTIES S. Wang¹, H. Zhao¹, K. Gan¹, Z. Gong¹, Y. Gan¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China | ||||
| 11:50 | 12:15 | 8.7.3 |
NUMERICAL EVALUATION FOR FAN-NOISE SHIELDING EFFECTS ON AFT-FUSELAGE MOUNTED AND EMBEDDED ENGINES T. Ikeda¹, R. Furuya, Ryoyu Systems, Japan; M. Murayama¹; ¹JAXA, Japan | ||||
| 12:15 | 12:40 | 8.7.4 |
REFINED PREDICTIONS COMPARED WITH THE PROPULSION AIRFRAME AEROACOUSTICS AND AIRCRAFT SYSTEM NOISE FLIGHT RESEARCH TEST DATA R.H. Thomas¹, Y. Guo, NASA Langley Reseach Center, United States; E.H. Nesbitt¹, I.A. Clark¹, J.C. June¹; ¹NASA Langley Research Center, United States | ||||
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| 11:00 | 11:25 | 9.7.1 |
SPEED GATED INTERCEPT PROCEDURE STUDY FOR INTEGRATION OF INCREASING DIVERSE OPERATIONS (IDO) AT EUROPEAN AIRPORTS T. Welsch¹, M.-M. Temme¹; ¹DLR, Germany | ||||
| 11:25 | 11:50 | 9.7.2 |
VALIDATING FLOW-BASED EN ROUTE AMAN COUPLING ESCAPE LIGHT WITH AIRTOP SOFTWARE K. Sekine¹, P. Bouchaudon, EUROCONTROL Innovation Hub, France; T. Tatsukawa¹, K. Fujii¹, E. Itoh, The University of Tokyo, Japan; ¹Tokyo University of Science, Japan | ||||
| 11:50 | 12:15 | 9.7.3 |
Lecture canceled | ||||
| 12:15 | 12:40 | 9.7.4 |
FEASIBILITY STUDY ON OPERATIONAL FLIGHT PLANS ADAPTED FOR TRAJECTORY BASED OPERATION A. Harada, Kyushu University, Japan; N. Takeichi, Tokyo Metropolitan University, Japan; T. Masuki¹, H. Nakahata¹, S. Inohata¹, N. Nagata¹, A. Yasuda¹; ¹Japan Airlines Co., Ltd., Japan | ||||
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| 11:00 | 11:25 | 10.7.1 |
LASER SHEAROGRAPGY-PREDICTION AND OPTIMIZING ITS FLAW DETECTION CAPABILITIES USING AN ADVANCED HYBRID APPROACH Y. Elbaz, Technion, I.I.T., Israel; H. Abramovich, Technion, I.I.T., Israel | ||||
| 11:25 | 11:50 | 10.7.2 |
FATIGUE PROPERTIES OF ADDITIVELY MANUFACTURED TOOL STEEL C.M. Johnston¹, L.C. Tshabalala¹, M. Davids, University of the Witwatersrand, South Africa; ¹CSIR, South Africa | ||||
| 11:50 | 12:15 | 10.7.3 |
DEVELOPMENT AND ANALYSIS OF THE THEORY OF COMPOSITE EXPANSION RING UNDER ELECTROMAGNETIC LOADING Z.-X. Liu¹, J. Liu¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China | ||||
| additional information (interactive) | 10.7.R |
DEVELOPMENT OF A MACHINE LEARNING-BASED STRESS SPECTRUM ESTIMATION TECHNIQUE FOR FATIGUE MONITORING E.G. Park, South Korea; S.H. Jeong, South Korea; J.Y. Cho, South Korea; J.H. Kim, South Korea | |||||
| additional information (interactive) | 10.7.R |
FULLY-EMBEDDED PRESSURE SENSOR FOR AERODYNAMICS SURFACES BASED ON FBG TECHNOLOGY P.E. Boffa¹, E. Casciaro¹, P. Bettini¹; ¹Politecnico di Milano, Italy | |||||
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| 11:00 | 11:25 | 11.7.1 |
STOCHASTIC BUCKLING ANALYSES OF LAMINATED COMPOSITE PLATES UNDER HYGROTHERMAL, GEOMETRIC AND MATERIAL UNCERTAINTIES MODELED AS NON-GAUSSIAN RANDOM FIELDS H.E.A.A. Santos, Embraer S.A., Brazil; D.A. Rade, Aeronautics Institute of Technology, Brazil | ||||
| 11:25 | 11:50 | 11.7.2 |
SANDWICH COMPOSITES SKIN PANEL OPTIMIZATION FOR THE COMMON RESEARCH MODEL WING Y.M. Meddaikar¹, J.K.S. Dillinger¹, W.R. Krüger¹, R. De Breuker, Delft University of Technology, Netherlands; G.H. Silva¹, P.H. Cabral², A.P. do Prado²; ¹DLR - Institute of Aeroelasticity, Germany ;²Embraer S.A., Brazil | ||||
| 11:50 | 12:15 | 11.7.3 |
AEROELASTIC TAILORING BASED ON VIRTUALLY-GENERATED ALLOWABLES AND HIGH ORDER FINITE ELEMENTS FOR IMPROVED COMPOSITE WING AEROELASTIC TAILORING BASED ON VIRTUALLY-GENERATED ALLOWABLES AND HIGH ORDER FINITE ELEMENTS FOR IMPROVED COMPOSITE WING DESIGN P.H. Cabral¹, A.P. do Prado¹, E. Carrera², A. Pagani², A. Racionero Sánchez-Majano², M. Enea²; ¹Embraer S.A., Brazil ;²Politecnico di Torino, Italy | ||||
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| 11:00 | 11:25 | 12.7.1 |
STRUCTURAL AND AEROELASTIC OPTIMISATION OF A LARGE AIRCRAFT WING WITH A PASSIVE TWIST WINGTIP Y.J. Pan¹, M. Alam¹, A. Spinelli¹, E. Bragado Aldana¹; ¹Cranfield University, United Kingdom | ||||
| 11:25 | 11:50 | 12.7.2 |
DEVELOPMENT OF A MASS EVALUATION TOOL FOR CLASSICAL AND DISRUPTIVE AIRCRAFT STRUCTURES V. Priasso¹, A. Lannoo¹; ¹DMAS, ONERA, France | ||||
| 11:50 | 12:15 | 12.7.3 |
STRUCTURAL DESIGN OF NEXT-GENERATION REGIONAL GREEN AIRCRAFT L. Pustina¹, F. Mastroddi¹, P. Della Vecchia, University of Naples “Federico II”, Italy; G. Cerino, LEONARDO, Aircraft Division, Italy; ¹Sapienza University of Rome, Italy | ||||
| 12:15 | 12:40 | 12.7.4 |
MULTIPHYSICS MODELING FOR SAFE BATTERIES USING LS-DYNA G. Di Mauro¹, M. Guida¹, G. Olivares², L.M. Gomez²; ¹University of Naples Federico II, Italy ;²Jerry Moran Center, AVET, NIAR, WSU, United States | ||||
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| 11:00 | 11:25 | 13.7.1 |
AERO-THERMAL ANALYSIS OF A REUSABLE LAUNCH VEHICLE DURING RE-ENTRY MANOEUVRER A. Assonitis¹, R. Paciorri ¹, V. Orlandini¹, A. Neri, ESA ESRIN, Italy; ¹University of Rome La Sapienza , Italy | ||||
| 11:25 | 11:50 | 13.7.2 |
RESEARCH ON AIRSPEED CORRECTION TECHNOLOGY OF EJECTION SEAT BASED ON CFD L. Jin¹, G. Feng¹, L. Wu¹; ¹Overall Technology R&D Department, AVIC Aerospace Life-support I, China | ||||
| 11:50 | 12:15 | 13.7.3 |
AEROACOUSTIC CAVITY FLOW ENERGY HARVESTING J.M. Kirkness-Duncombe¹, N.J. Lawson¹, G.A. Vio², S.D. Moss², D.J. Munk²; ¹The University of Sydney, Department of Aeronautical Engineering, Australia ;²Defence Science and Technology Group, Aerospace Division, Australia | ||||
| 12:15 | 12:40 | 13.7.4 |
NUMERICAL INVESTIGATION OF THE INTERACTION OF OPPOSING JETS AND SUPERSONIC FREE FLOWS Z.K. Liu¹, Y.L. Liu¹, Q.Z. Li¹, G. Wang¹; ¹Northwestern Polytechnical University, China | ||||
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| 11:00 | 11:25 | 14.7.1 |
FROM THA TO REAL-TIME MONITORING: INTEGRATING NEW VIEW OF SAFETY INTO FLIGHT TEST PROGRAMS T.F. Macedo¹, M.M. Cardoso Junior¹; ¹Technological Institute of Aeronautics, Brazil | ||||
| 11:25 | 11:50 | 14.7.2 |
REMOTE OBSERVATION EXPERIMENT OF VOLCANIC ASH USING POLARIZATION LIDAR H. Inokuchi¹, H. Oikawa¹, G. Morimoto, Metro Weather Co., Ltd, Japan; S. Inaka¹; ¹JAXA, Japan | ||||
| 11:50 | 12:15 | 14.7.3 |
COMPARATIVE ANALYSIS OF EVTOL, DRONE AND GROUND TRANSPORTATION SYSTEMS FOR EMERGENCY DELIVERY OF BLOOD-DERIVED MEDICATION D. Angelini¹, E. Cestino¹, D. Cestino², F. Cattel²; ¹Politecnico di Torino, Italy ;²A.O.U. Città della Salute e della Scienza di Torino, Italy | ||||
| 12:15 | 12:40 | 14.7.4 |
ENABLING AIRWORTHINESS SECURITY BY A HOLISTIC SECURITY ENGINEERING PROCESS AT VARIOUS AIRCRAFT DESIGN LEVELS M. Blecken¹, H. Hintze¹, R. God¹; ¹Hamburg University of Technology, Germany | ||||
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| 11:00 | 11:25 | 15.7.1 |
DYNAMICS OF THE MECHANISM FOR VENTILATION ACROSS FEATHERS IN FLAPPING WING UAV R.C. Silva¹, D.D. Bueno¹; ¹UNESP, Brazil | ||||
| 11:25 | 11:50 | 15.7.2 |
TRAJECTORY OPTIMIZATION OF EVTOL VEHICLES FOR URBAN AIR MOBILITY USING INDIRECT METHODS K. Mall¹, R. Gadre¹, J. Gerardus¹, D.A. DeLaurentis¹; ¹Purdue University, United States | ||||
| 11:50 | 12:15 | 15.7.3 |
IN-FLIGHT VIBRATION SIGNAL BASED DETECTION AND LOCALIZATION FOR UAV PROPELLER ANOMALIES UNDER UNCERTAINTY VIA MACHINE LEARNING TYPE METHODS I.A. Iliopoulos¹, J.S. Korolis¹, S.D. Fassois¹, J.S. Sakellariou¹; ¹University of Patras, Greece | ||||
| 12:15 | 12:40 | 15.7.4 |
STUDY ON CONTROL PERFORMANCE OF A NEW TYPE OF TILT-ROTOR AIRCRAFT K. Miyabe¹, M. Bando¹, S. Hokamoto¹; ¹Kyushu Univercity, Japan | ||||
| additional information (interactive) | 15.7.R |
DESIGN OF ATTITUDE CONTROL SYSTEM FOR DRAGONFLY-INSPIRED FLAPPING WING AERIAL VEHICLE L. Wang¹, X. Yang¹, Y. Luo¹, H. Chen¹, J. Li¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China | |||||
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| 11:00 | 11:25 | 16.7.1 |
AN ONTOLOGY-BASED APPROACH FOR THE CO-DEVELOPMENT AND OPTIMIZATION OF AIRCRAFT CABIN DESIGN AND ASSEMBLY ARCHITECTURES Y. Ghanjaoui¹, J.H. Bussemaker¹, J. Biedermann¹, B. Nagel¹; ¹DLR, Germany | ||||
| 11:25 | 11:50 | 16.7.2 |
FRICTION RIVETING OF THERMOPLASTIC COMPOSITE WITH A CNC MACHINE: EXPERIMENTAL WORK I. Tan¹, G. Cohen¹, A.-C. Araujo¹, A. Daidié¹; ¹Institut Clément Ader, France | ||||
| 11:50 | 12:15 | 16.7.3 |
PRELIMINARY RESULTS FOR AN INSTRUCTION DESIGN PROCEDURE IN AERONAUTICAL MANUFACTURING M. Bartolomei¹, F. Barravecchia¹, L. Mastrogiacomo¹, F. Franceschini¹, F. Acerra², D.M. Gatta², D. Cannizzaro²; ¹Politecnico di Torino, Italy ;²Leonardo S.p.A, Italy | ||||
| 12:15 | 12:40 | 16.7.4 |
SURFACE MORPHOLOGY AND MICROSTRUCTURAL FEATURES OF ELECTRON BEAM SURFI-SCULPTED TI-6AL-4V ALLOY K. Li¹, P. Fu¹, Z. Tang¹, B. Zhang¹, Y. Ma, Chongqing University of Technology, China; ¹AVIC Manufacturing Technology Institute, China | ||||
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| 11:00 | 11:25 | 17.7.1 |
MIXED REALITY FOR AIRCRAFT STRUCTURAL DENT AND BUCKLE NON-DESTRUCTIVE EVALUATION A.-K. Koschlik¹, M.J. Scott², T. Keser¹, F. Rauscher¹, H. Meyer¹, W. Verhagen², P. Marzocca², F. Raddatz¹, G. Wende¹; ¹DLR, Germany ;²RMIT, Australia | ||||
| 11:25 | 11:50 | 17.7.2 |
CINNABAR PROJECT - AUGMENTED REALITY WORKFLOW FOR AIRCRAFT DENT & BUCKLE INSPECTION T. Keser¹, R. Schmied-Kowarzik¹, A.-K. Koschlik¹, L. Kaschub², M.J. Scott, RMIT University, Australia; R. Rodeck², G. Wende²; ¹German Aerospace Center (DRL), Germany ;²German Aerospace Center (DLR), Germany | ||||
| 11:50 | 12:15 | 17.7.3 |
CINNABAR PROJECT: EXAMINING REQUIREMENTS FOR USER ACCEPTANCE OF AIRCRAFT STRUCTURE INSPECTION IN AUGMENTED REALITY R. Schmied-Kowarzik¹, T. Keser¹, L. Kaschub¹, A.-K. Koschlik¹, R. Rodeck¹, G. Wende¹; ¹German Aerospace Center (DLR), Germany | ||||
| 12:15 | 12:40 | 17.7.4 |
CINNABAR PROJECT – COST-BENEFIT ANALYSIS OF DIGITAL PROCESSES FOR NON-DESTRUCTIVE INSPECTIONS OF AIRCRAFT STRUCTURES J. Aigner¹, A.-K. Koschlik¹, H. Meyer¹, F. Raddatz¹, G. Wende¹; ¹German Aerospace Center (DLR), Germany | ||||
| additional information (interactive) | 17.7.R |
DIGITAL TWIN OF AN AIRCRAFT LANDING GEAR TO ENHANCE FAILURE ANALYSIS AND MANAGE PREDICTIVE MAINTENANCE D.Y. Sabag¹, O. Yakimenko, Naval Postgraduate School, United States; H. Alian¹; ¹Israeli Air Force, Israel | |||||
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| 14:30 | 14:55 | 1.8.1 |
SAFRAN PROPULSION STRATEGY AND ROADMAP FOR FUTURE SUSTAINABLE AVIATION D. Dijoud, France | ||||
| 14:55 | 15:20 | 1.8.2 |
MTU’S ROADMAP TOWARDS SUSTAINABLE PROPULSION F. Donus, MTU, Germany | ||||
| 15:20 | 15:45 | 1.8.3 |
DELIVERING THE ROLLS-ROYCE NET ZERO ROADMAP T. Newby, Rolls-Royce plc, United Kingdom | ||||
| 15:45 | 16:10 | 1.8.4 |
Q&A - MINI PANEL QA. A, | ||||
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| 14:30 | 14:55 | 2.8.1 |
BOEING CONTRIBUTIONS TO THE CRM-HL ECOSYSTEM K. Hood, United States | ||||
| 14:55 | 15:20 | 2.8.2 |
TEST SUMMARY OF THE FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL T. Hashioka¹, Y. Murahashi¹, H. Yasuda¹, Y. Sawaki¹, S. Onda¹, Y. Tsuchimoto¹, Y. Nishizaki¹, W. Suzuki¹, T. Kawamura¹; ¹Kawasaki Heavy Industries, Ltd., Japan | ||||
| 15:20 | 15:45 | 2.8.3 |
ACTIVITY PLANS USING CRM-HL AT JAXA M. Kohzai, Japan | ||||
| 15:45 | 16:10 | 2.8.4 |
PANEL DISCUSSION P. D, United States | ||||
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| 14:30 | 14:55 | 3.8.1 |
LARGE LANGUAGE MODEL IN AIRCRAFT SYSTEM DESIGN P. Krus, Linköping University, Sweden | ||||
| 14:55 | 15:20 | 3.8.2 |
APPLYING MODEL-BASED SYSTEM ENGINEERING AND DEVOPS ON THE IMPLEMENTATION OF AN AI-BASED COLLISION AVOIDANCE SYSTEM T. Stefani¹, J.M. Christensen¹, E. Hoemann¹, A. Anilkumar Girija¹, F. Köster, DRL, Germany; T. Krüger¹, S. Hallerbach¹; ¹DLR, Germany | ||||
| 15:20 | 15:45 | 3.8.3 |
A HUMAN-CENTERED SYSTEMS ENGINEERING APPROACH FOR INTEGRATING ARTIFICIAL INTELLIGENCE IN AVIATION: A REVIEW OF AI SYSTEMS L.D.O. Morais¹, P. Krus, Linköping University, Sweden; L. Pereira¹; ¹UFABC, Brazil | ||||
| 15:45 | 16:10 | 3.8.4 |
AN AUTONOMOUS SYSTEM FOR DOCKING AND BATTERY SWAPPING IN UAVS I. Kute¹, J. Dagli¹, E. Khot¹, R. Verma¹, P. Gupta¹, D. Shukla¹, R. Pant¹; ¹Indian Institute of Technology Bombay, India, India | ||||
| additional information (interactive) | 3.8.R |
AUTOMATING THE VERIFICATION OF GEOMETRIC REQUIREMENTS FOR AIRCRAFT FUEL SYSTEMS USING KNOWLEDGE-BASED ENGINEERING B. Boden¹, M. Padilha¹, T. Burschyk¹, C. Cabaleiro de la Hoz¹, E. Moerland¹, M. Fioriti, Politecnico di Torino, Germany; ¹DLR, Germany | |||||
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| 14:30 | 14:55 | 4.8.1 |
A DESIGN APPROACH FOR A MODEL-SCALE VTOL POWERED BY TWO PIVOTING KEROSENE TURBINES T. Müller¹, V. Gollnick¹; ¹Institute of Air Transportation Systems, Germany | ||||
| 14:55 | 15:20 | 4.8.2 |
ENERGY AND EMISSION ANALYSIS OF AN AIR-TAXI SERVICE USING DYNAMIC EVTOL SYSTEM MODELS N. Prabhakar¹, F. Salucci¹, D. Karbowski¹; ¹Argonne National Laboratory, United States | ||||
| 15:20 | 15:45 | 4.8.3 |
SCALED FLIGHT TESTING FOR EVALUATING DISTRIBUTED ELECTRIC PROPULSION H. Jentink, Royal Netherlands Aerospace Centre NLR, Netherlands; C. Döll, ONERA, France; P. Iannelli, CIRA, Italy; M. Hoogreef, TU Delft, Netherlands; D. Kierbel, Airbus, France | ||||
| 15:45 | 16:10 | 4.8.4 |
DETERMINISTIC HYBRID POWER RATIOS CONSIDERING VARIOUS FAILURE CASES FOR QUAD TILTROTOR AIRCRAFT M. Park¹, N. Roh¹; ¹Hanwha systems, South Korea | ||||
| Reserve Paper | 4.8.R |
RETROFITTING A JET DRIVEN UAV TO FORM A MULTI-PURPOSE TEST PLATFORM D. Teubl¹, T.B. Sissing¹, M. Hornung¹; ¹Chair of Aircraft Design, Technical University of Munich, Germany | |||||
| Reserve Paper | 4.8.R |
A STUDY ON BATTERY SEPARATION DRONES TO EXTEND ENDURANCE H. Kim¹, T. Kim, Seoul Digital University, South Korea; C. Son¹; ¹Cheongju University, South Korea | |||||
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| 14:30 | 14:55 | 5.8.1 |
LAUNCH SYSTEM ASSESSMENT OF AN EXPERIMENTAL HYPERSONIC SCRAMJET VEHICLE F. Cascone¹, P. Roncioni¹, O. Russo¹, M. Marini¹, S. Di Benedetto¹, M. Albano², R. Bertacin², G. Ranuzzi²; ¹CIRA, Italy ;²ASI, Italy | ||||
| 14:55 | 15:20 | 5.8.2 |
STABILITY CHARACTERISTICS OF CROSSFLOW MODES IN HYPERSONIC BOUNDARY LAYER WITH EXPANSION CORNER P. Lu¹, Y. Xi¹, J. Sun¹, S. Fu¹; ¹Tsinghua University, China | ||||
| 15:20 | 15:45 | 5.8.3 |
NUMERICAL INVESTIGATION OF HYPERSONIC FLOWS C.-S. Dikmen¹, M.-N. Yüksel¹, M. Yumusak¹; ¹Roketsan, Turkey | ||||
| 15:45 | 16:10 | 5.8.4 |
DETACHED EDDY SIMULATION OF HYPERSONIC SHOCK-WAVE/BOUNDARY-LAYER INTERACTIONS ON HIFIRE-1 AXISYMMETRIC CONE-CYLINDER-FLARE R.O. Bura, Republic Indonesia Defense University, Indonesia; A. Riyadl, National Research and Innovation Agency, Indonesia | ||||
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| 14:30 | 14:55 | 6.8.1 |
NUMERICAL SIMULATION OF FLOWS AROUND AN AIRFOIL DURING ACCELERATED AND DECELERATED FLIGHT R. Yamashita, The University of Tokyo, Japan | ||||
| 14:55 | 15:20 | 6.8.2 |
NUMERICAL INVESTIGATION ON AERODYNAMIC PERFORMANCE OF HOVERING ROTOR IN GROUND EFFECT X.-L. Li¹, J.-H. Xu¹, W.-P. Song¹, S.-Q. Han, Sichuan University, China; Z.-H. Han¹; ¹ Northwestern Polytechnical University, China | ||||
| 15:20 | 15:45 | 6.8.3 |
NONLINEAR DROPLET DYNAMICS IN IDEALIZED TRAILING VORTICES O. Avni¹, Y. Dagan¹; ¹Technion - Israel Institute of Technology, Israel | ||||
| 15:45 | 16:10 | 6.8.4 |
FLYING WING CIRCULATION DISTRIBUTIONS, AERODYNAMIC PERFORMANCE AND WAKE ROLL-UP H.W.M. Hoeijmakers¹, M.P.J Sanders¹, L.H. Groot Koerkamp¹, A. van Garrel¹, C.H. Venner¹; ¹University of Twente, Netherlands | ||||
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| 14:30 | 14:55 | 7.8.1 |
ANALYSIS OF AN ELECTRICAL-POWERED-DUCTED-THRUST VECTORING-FLAP V. Gollnick¹, J. Luehrmann¹, F. Danquah¹, A. Semke¹, T. Mueller¹, J. Thoeben¹; ¹Hamburg University of Technology, Germany | ||||
| 14:55 | 15:20 | 7.8.2 |
AERODYNAMIC INTERACTION EFFECTS OF TILTROTOR EVTOL AIRCRAFT C. Moreira¹, C. Breitsamter¹; ¹Technical University of Munich, Germany | ||||
| 15:20 | 15:45 | 7.8.3 |
PIV AND AERODYNAMIC FORCES ANALYSIS OF A HELICOPTER OPERATING AROUND A BUILDING BY WIND-TUNNEL EXPERIMENTS R. Bardera¹, J.C. Matias¹, E. Barroso¹; ¹Instituto Nacional de Técnica Aeroespacial, Spain | ||||
| 15:45 | 16:10 | 7.8.4 |
EXPERIMENTAL AND NUMERICAL INVESTIGATION ON AERODYNAMIC PERFORMANCE OF A MARS ROTOR SYSTEM Y. Liu¹, J. Xiao¹, N.A. Benai-dara¹, Z. Chen¹, N. Qin, University of Sheffield, United Kingdom; ¹NUAA, China | ||||
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| 14:30 | 14:55 | 8.8.1 |
A HYBRID APPROACH FOR RECONSTRUCTION OF TRANSONIC BUFFET AERODYNAMIC NOISE: INTEGRATING RANDOM FOREST AND COMPRESSIVE SENSING ALGORITHM Q. Zhang, Northwestern Polytechnical University, China; W. Zhang, Northwestern Polytec, China | ||||
| 14:55 | 15:20 | 8.8.2 |
AEROACOUSTICS INVESTIGATION OF PROPELLER LEADING EDGE TUBERCLES APPLIED TO ADVANCED AIR MOBILITY D. Skrna, Austria; M. de Rosa Jacinto, Brazil; M. Berens, Germany | ||||
| 15:20 | 15:45 | 8.8.3 |
OPERATIONAL LIMITS ASSESSMENT FOR HIGH-ALTITUDE LONG-ENDURANCE UAVS CONSIDERING PROPELLER ICING EFFECT Y.H. Kim, South Korea; J.-H. Shin, South Korea; C.J. Woo, South Korea; C.K. Son, South Korea; K.J. Yee, South Korea | ||||
| 15:45 | 16:10 | 8.8.4 |
NUMERICAL SIMULATION OF THE RESPONSE CHARACTERISTICS OF THE WING STRUCTURE OF A SEAPLANE PLANING IN WAVE Z.-W. Lu¹, Y.-H. Li¹, J.-C. Chen¹, M.-B. Tong¹, B. Wu¹; ¹Nanjing University of Aeronautics and Astronautics, China | ||||
| additional information (interactive) | 8.8.R |
NUMERICAL-THEORETICAL EVALUATION OF THE DITCHING OF A HULL WITH DIHEDRAL ANGLES BETWEEN -5 AND 20 DEGREES D. Guagliardo¹, E. Cestino¹, A. Virdis¹, A. Alfero¹, V. Sapienza¹; ¹Politecnico of Turin, Italy | |||||
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| 14:30 | 14:55 | 9.8.1 |
OVERVIEW OF FACTORS RELATED TO AIRCRAFT OPERATION ASSOCIATED WITH A NEGATIVE IMPACT ON THE ENVIRONMENT D. Kacik, Warsaw University of Technology, Poland | ||||
| 14:55 | 15:20 | 9.8.2 |
A COMPREHENSIVE METHODOLOGY FOR PERFORMING PROSPECTIVE LIFE CYCLE ASSESSMENTS OF FUTURE AIR TRANSPORT SCENARIOS F. Pollet¹, T. Planès¹, S. Delbecq¹; ¹Fédération ENAC ISAE-SUPAERO ONERA, Université de Toulouse, France | ||||
| 15:20 | 15:45 | 9.8.3 |
MITIGATING THE CLIMATE IMPACT OF AVIATION BY OPERATIONAL MEANS - A COMPARATIVE STUDY FOR DIFFERENT WEATHER SITUATIONS Z.L. Zengerling¹, M. Mendiguchia Meuser¹, A. Lau¹, V. Gollnick, Hamburg University of Technology (TUHH), Germany; ¹German Aerospace Center (DLR), Germany | ||||
| 15:45 | 16:10 | 9.8.4 |
CHARACTERISING THE ROLE OF FLEET RENEWAL ON THE PATHWAY TO 2050: A EUROPEAN AIRLINE CASE STUDY N. Barry¹, C. Gallagher¹, S. Fitzgerald, Ryanair, Ireland; C. Stuart¹; ¹Trinity College Dublin, Ireland | ||||
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| 14:30 | 14:55 | 10.8.1 |
CONVOLUTIONAL NEURAL NETWORKS ALGORITHMS FOR STRUCTURAL HEALTH MONITORING OF AIRCRAFTS COMPOSITES PANELS E. Monaco¹, F. Ricci¹; ¹Università di Napoli , Italy | ||||
| 14:55 | 15:20 | 10.8.2 |
IMPROVING SHAPE SENSING OF AERONAUTICAL STRUCTURES WITH STRAIN PRE-EXTRAPOLATION AND SENSOR PLACEMENT OPTIMIZATION E. Del Priore¹, L. Lampani¹; ¹Sapienza University of Rome, Italy | ||||
| 15:20 | 15:45 | 10.8.3 |
STRUCTURAL HEALTH MONITORING OF CFRP DURING FATIGUE LOAD VIA THE ASSESSMENT OF CRACK DENSITY BY MEANS OF THERMOGRAPHY R. De Finis, Università del Salento, Italy; D. Palumbo¹, U. Galietti¹; ¹Politecnico di Bari, Italy | ||||
| 15:45 | 16:10 | 10.8.4 |
EMBEDDED SENSORS FOR AIRCRAFT PREDICTIVE MAINTENANCE: SHM SYSTEM INTEGRATION & TRADE-OFF ANALYSIS V.M. Sharma¹, P. Jha¹, V. Samanyusree¹, A. Sharma¹, S. Maheshwari¹, G.S. Mamatha¹; ¹RV College of Engineering, India | ||||
| additional information (interactive) | 10.8.R |
THERMAL HISTORY PAINT UNDER HIGH SUBSONIC FLOW W. Stryczniewicz¹, T. Kwiatkowski¹, I. Kaminska², M. Chojnacki², K. Fronc²; ¹?ukasiewicz Research Network - Institute of Aviation, Poland ;²Institute of Physics Polish Academy of Sciences, Poland | |||||
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| 14:30 | 14:55 | 11.8.1 |
FAST TRANSONIC CORRECTIONS FOR PANEL METHODS USING VISCOUS-INVISCID INTERACTION A. Crovato¹, P. Dechamps¹, A.P. Prado², P.H. Cabral², V.E. Terrapon¹, G. Dimitriadis¹; ¹University of Liège, Belgium ;²Embraer S.A., Brazil | ||||
| 14:55 | 15:20 | 11.8.2 |
EXPLORING MULTI-FIDELITY AEROELASTIC TAILORING: PROSPECT AND MODEL ASSESSMENT H.F. Maathuis¹, S.G.P. Castro¹, R. De Breuker¹; ¹Delft University of Technology, Netherlands | ||||
| 15:20 | 15:45 | 11.8.3 |
A-BASIS AND B-BASIS BUCKLING ALLOWABLES FOR AN AIRCRAFT COMPOSITE WING R.A.S. Cardoso¹, M.S. Reis¹, L.P.S. Ferreira, FEMTO-ST, France; M.P. Alves¹, S.K. Ha, Hanyang University, South Korea; C.A. Cimini Jr.¹; ¹Federal University of Minas Gerais, Brazil | ||||
| 15:45 | 16:10 | 11.8.4 |
ENHANCING THE PERFORMANCE OF SLENDER STRUCTURES WITH GEOMETRIC CONSTRAINTS: A CASE STUDY WITH THE ROORDA FRAME L. Zhu¹, J. Shen, University of Exeter, United Kingdom; R.M.J. Groh¹, M. Schenk¹, A. Pirrera¹; ¹University of Bristol, United Kingdom | ||||
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| 14:30 | 14:55 | 12.8.1 |
Lecture canceled | ||||
| 14:55 | 15:20 | 12.8.2 |
A MESO-SCALED SIMULATION ON THE THICKNESS EFFECT OF TWO-DIMENSIONAL TRIAXIALLY BRAIDED COMPOSITES UNDER TENSILE LOADS Y. Bai¹, P. Liu¹, Z.-Q. Zhao¹, C. Zhang¹; ¹Northwesterm Polytechnical University, China | ||||
| 15:20 | 15:45 | 12.8.3 |
MULTIAXIAL TESTING OF AERONAUTIC COMPOSITE STRUCTURES AT INTERMEDIATE SCALE B. Castanié¹, J.-C. Passieux¹, J.-N. Périé¹, C. Bouvet¹, J.-E. Dufour¹, J. Serra¹; ¹Institut Clément Ader, France | ||||
| 15:45 | 16:10 | 12.8.4 |
DYNAMIC AND STABILITY ANALYSES OF ROTATING THIN-WALLED FILAMENT WOUND GLASS FIBRE COMPOSITE CYLINDERS WITH METAL LINER R. Hu, China; Z. Yuan, China; C. Zhang, China | ||||
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| 14:30 | 14:55 | 13.8.1 |
DESIGN SPACE EXPLORATION OF NEXT-GENERATION SUPERSONIC BUSINESS JET ENGINE WITH A FOCUS ON LANDING AND TAKE-OFF (LTO) NOISE D. Del Gatto¹, S. Adamidis¹, C. Mourouzidis¹, S. Brown¹, V. Pachidis¹; ¹Cranfield University, United Kingdom | ||||
| 14:55 | 15:20 | 13.8.2 |
RAMJET/SCRAMJET TEST BENCH WITH CAVITY INJECTION OF HYDROGEN F. Strauss¹, T. Nilsson, Lund University, Sweden; K. Manassis¹; ¹German Aerospace Center DLR, Germany | ||||
| 15:20 | 15:45 | 13.8.3 |
PROPULSIVE CFD ANALYSIS OF THE SCRAMJET HYPERSONIC EXPERIMENTAL VEHICLE O. Russo¹, P. Roncioni¹, M. Marini¹, S. Di Benedetto¹, G. Ranuzzi², S. Pizzurro², M. Albano²; ¹Italian Aerospace Research Centre (CIRA), Italy ;²Italian Space Agency (ASI), Italy | ||||
| 15:45 | 16:10 | 13.8.4 |
EXPERIMENTAL AND NUMERICAL INVESTIGATION ON SEPARATION CHARACTERISTICS OF SERPENTINE CONVERGENT-DIVERGENT NOZZLE M.-X. Wang¹, L. Zhou¹, J.-W. Shi¹, W.-J. Deng¹, H. Xiao¹; ¹Northwestern Polytechnical University, China | ||||
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| 14:30 | 14:55 | 14.8.1 |
IDENTIFICATION OF FACTORS CONTRIBUTING TO UNFAVORABLE LANDINGS R. Mori, Kobe University, Japan | ||||
| 14:55 | 15:20 | 14.8.2 |
HELICOPTER ACCIDENTS IN BRAZIL: AN ANALYSIS OF MAINTENANCE FROM THE PERSPECTIVE OF HUMAN FACTORS F. de Assis da Silva Junior¹, J.M. Vieira da Fonseca¹, I.N.M. da Silva¹, A.V. Gaspar¹, M.M. Cardoso Junior¹; ¹Technological Institute of Aeronautics, Brazil | ||||
| 15:20 | 15:45 | 14.8.3 |
SENSITIVITY ANALYSIS OF SAFETY FACTORS BASED ON MODEL OF AVIATION RECIPROCATING ENGINE TURBOCHARGING SYSTEM Z. Wang, China; G. Li, China; Y. Teng, China; T. Xu, China; Y. Zhang, China | ||||
| 15:45 | 16:10 | 14.8.4 |
Lecture canceled | ||||
| Reserve Paper | 14.8.R |
STUDY ON THE BALLISTIC-RESISTANT AIRWORTHINESS STANDARDS FOR COMMERCIAL AIRCRAFT COCKPIT DOOR T. Hu¹, J. Song¹, N. Yue¹, Z. Zhang², Y. Zhang², T. Chen²; ¹Airworthiness Technology Research & Management Center, China ;²Shanghai Aviation Airworthiness Certification Center, China | |||||
| additional information (interactive) | 14.8.R |
A METHOD FOR AUTOMATIC GENERATING SAFETY ANALYSIS BASED ON AVIATION PISTON ENGINE MODEL G. Li¹, Y.-D. Teng¹, Z.-L. Wang¹, T.-G. Xu¹, S.-T. Ding, Civil Aviation University of China,, China; ¹Beihang University, China | |||||
| additional information (interactive) | 14.8.R |
IMPROVING DISTRIBUTION OF CRASH ENERGY ABSORPTION FOR CIVIL AIRCRAFT BASED ON PROGRESSIVE BENDING FAILURE MECHANISM T.-J. Jiang¹, Z.-P. Luo¹, Z. Kan¹, J.-W. Xiang¹, X.-C. Liu², C.-Y. Bai², X.-L. Xi²; ¹Beihang University, China ;²Aircraft Strength Research Institute, China | |||||
| |||||||
| 14:30 | 14:55 | 15.8.1 |
IN-FLIGHT MEASUREMENT OF WING SURFACE PRESSURE DISTRIBUTION ON A FIXED-WING UAV AND ITS APPLICATION TO FLIGHT CONTROL Y. Hayashi¹, J.-H. Kim¹, T. Tsuchiya¹; ¹The University of Tokyo, Japan | ||||
| 14:55 | 15:20 | 15.8.2 |
MODEL PREDICTIVE CONTROL DRIVEN AERIAL GRASPING WITH SOFT OPERATIONAL CONSTRAINTS J. Novák ¹, J. Hanák¹, P. Chudý¹; ¹BUT, Czech Republic | ||||
| 15:20 | 15:45 | 15.8.3 |
FUZZING ON TARGET DETECTION SYSTEM OF UNMANNED AERIAL VEHICLE H. Dai¹, Z. Wang¹, J. Ding¹, G. Li¹, C. Wang¹, L. He¹, H. Liu, Swinburne University of Technology, Australia; ¹Chinese Aeronautical Establishment, China | ||||
| 15:45 | 16:10 | 15.8.4 |
FLIGHT PATH RECONSTRUCTION OF A FLEXIBLE WING UAV WITH WING MOUNTED VANES V.P. Fernandes¹, T.R. Paula¹, R.C. Nascimento¹, R.G.A. Silva¹, L.C.S. Góes¹; ¹ITA - Instituto Tecnológico de Aeronáutica, Brazil | ||||
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| 14:30 | 14:55 | 16.8.1 |
LIGHT WEIGHT DESIGN AND LASER ADDITIVE MANUFACTURING OF METAL BIPOLAR PLATES FOR THE APPLICATION OF AIRCRAFT FUEL CELL K.J. Lin, China; Y. Xu, China; D.D. Gu, China; J.H. Shan, China; K.Y. Shi, China; W.L. Zhang, China | ||||
| 14:55 | 15:20 | 16.8.2 |
EFFECTS OF PROCESSING STRATEGIES ON SURFACE QUALITY AND MECHANICAL PROPERTIES IN HYBRID ADDITIVE MANUFACTURING OF IN718 ALLOY T. Wang¹, C. Wang¹, J.-J. Li¹, W.-X. Wang¹; ¹Chongqing University, China | ||||
| 15:20 | 15:45 | 16.8.3 |
BUILDING METHODS FOR A COMPOSITE CONSTRUCTED VTOL USING 3D PRINTING TECHNIQUES T. Müller¹, V. Gollnick¹; ¹Institute of Air Transportation Systems, Germany | ||||
| 15:45 | 16:10 | 16.8.4 |
THE PRODUCTION OF HIGH-PERFORMANCE HEAT EXCHANGERS FOR AEROSPACE APPLICATIONS J. Shipley¹, A. Magnusson¹, J. Gårdstam¹, C. Beamer¹, A. Cassese¹; ¹Quintus Technologies, Sweden | ||||
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| 14:30 | 14:55 | 17.8.1 |
CLIMATE RESILIENCE – THE IMPACT OF EXTREME WEATHER EVENTS - A CASE STUDY: HEATHROW AIRPORT M. Osund-Ireland¹, B. Elzen¹, W.A. Ireland¹; ¹Susteer AB, Sweden | ||||
| 14:55 | 15:20 | 17.8.2 |
SUSTAINABLE ENGINE MAINTENANCE: EVALUATING THE ECOLOGICAL IMPACT OF LIFE LIMITED PART REPLACEMENT A. Oestreicher¹, A. Rahn¹, J. Ramm¹, J. Städing², C. Keller², K. Wicke¹, G. Wende¹; ¹DLR, Germany ;²MTU Maintenance, Germany | ||||
| 15:20 | 15:45 | 17.8.3 |
FACTORS INFLUENCING THE CLIMATE-RELEVANT ENVIRONMENTAL IMPACT OF AIR TRANSPORT COMPARED TO RAIL AND ROAD TRANSPORT J. Roesing, RWTH Aachen University, Germany | ||||
| 15:45 | 16:10 | 17.8.4 |
E-KEROSENE POTENTIAL FOR COMMERCIAL AVIATION DECARBONIZATION G. Quaresma¹, L.B. Magalhães, ISEC, ISEC Lisboa, Portugal; A.F. Ferreira, IDMEC-LAETA, Mechanical Engineering Department, IST/UL, Portugal; A. Silva¹; ¹AEROG-LAETA, Aerospace Sciences Department, UBI, Portugal | ||||
| additional information (interactive) | 17.8.R |
ENSURING THE NEXT GENERATION GREEN AIRCRAFT’ SUSTAINABILITY FROM THE DESIGN PHASE VIA A LIFE-CYCLE COST ANALYSIS E. Stefana¹, E. De Paola¹, L. Pustina¹, R. Patriarca¹, F. Mastroddi¹; ¹Sapienza University of Rome, Italy | |||||
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| 16:30 | 17:00 | 1.9.1 |
PRATT & WHITNEY SUSTAINABILITY STRATEGY & DEMONSTRATORS A.J. Murphy, Pratt & Whitney, United States | ||||
| 17:00 | 17:30 | 1.9.2 |
GE AEROSPACE: RISING TO THE CHALLENGE FOR MORE SUSTAINABLE FLIGHT R. Seele, GE Aerospace, United States | ||||
| 17:30 | 18:00 | 1.9.3 |
FUTURE LANDSCAPE OF AVIATION ENERGY – US PERSPECTIVE M.R. Berube, Department of Energy EERE, United States | ||||
| 18:00 | 18:30 | 1.9.4 |
PANEL DISCUSSION PD. D, | ||||
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| 16:30 | 17:00 | 2.9.1 |
OVERVIEW OF JAPANESE R&D ACTIVITIES ON GREEN TRANSFORMATION AND DIGITAL TRANSFORMATION IN AVIATION S. Watanabe, Japn Aerospace Exploration Agency, Japan | ||||
| 17:00 | 17:30 | 2.9.2 |
DEVELOPMENT OF CORE TECHNOLOGIES FOR HYDROGEN AIRCRAFT M. Kazari, Kawasaki Heavy Industries,Ltd., Japan | ||||
| 17:30 | 18:00 | 2.9.3 |
AIRCRAFT DX IN COMMERCIAL AVIATION SYSTEMS Y. Yamaguchi, Mitsubishi Heavy Industries, Ltd./Commercial Aviation Systems, Japan | ||||
| 18:00 | 18:30 | 2.9.4 |
DEVELOPMENT OF AIRCRAFT SYSTEM ELECTRIFICATION AND HYBRID ELECTRIC PROPULSION N. Seki¹, T. Inoue¹; ¹IHI Corporation, Japan | ||||
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| 16:30 | 17:00 | 3.9.1 |
STRUT-BRACED WING INDUCED DRAG MODELING FOR REGIONAL TURBOPROP AIRCRAFT DESIGN G. Grazioso, University of Naples Federico II, Italy; A. De Marco, University of Naples, Italy | ||||
| 17:00 | 17:30 | 3.9.2 |
STEADY ANALYSIS OF THREE-SURFACE AIRPLANES: IMPROVING THE AERODYNAMIC PERFORMANCE THROUGH REDUNDANT LONGITUDINAL CONTROL S. Cacciola¹, C.E.D. Riboldi¹, C. Spitale¹; ¹Politecnico di Milano, Italy | ||||
| 17:30 | 18:00 | 3.9.3 |
LONGITUDINAL STABILITY PARAMETERS FOR FLYING BOOM AERIAL REFUELING L.H. Peristy¹, R.E. Perez¹; ¹Royal Military College of Canada, Canada | ||||
| 18:00 | 18:30 | 3.9.4 |
ON THE FUTURE OF TRANSONIC FLIGHTS: CURVED PLANFORM WINGS FOR BUFFET-ONSET CONTROL M.R. Chiarelli¹, S. Bonomo¹, G. Cascinelli¹; ¹Department of Civil and Industrial Engineering, Pisa, Italy | ||||
| Reserve Paper | 3.9.R |
INVESTIGATION ON AERODYNAMIC DESIGN OF VTOL AIRCRAFT PROPELLER L.D. Deng¹, W.P. Song¹, J.H. Xu¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | |||||
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| 16:30 | 17:00 | 4.9.1 |
DEVELOPMENT OF A SERVO-DRIVEN FLAPPING-WING AIR VEHICLE WITH FOLDING-WING MECHANISM E.-H. Lee¹, H.-H. Yang¹, S.-G. Lee¹, J.-H. Han¹; ¹KAIST, South Korea | ||||
| 17:00 | 17:30 | 4.9.2 |
PRELIMINARY DESIGN EXPLORATION OF PROSPECTIVE MULTIROTOR AEROBOTS FOR MARS V. Youhanna¹, L. Felicetti¹, D. Ignatyev¹; ¹Cranfield University, United Kingdom | ||||
| 17:30 | 18:00 | 4.9.3 |
MISSION-BASED OPTIMAL PROPELLER SELECTION FOR VTOL SUAV CONFIGURATION C. Reyner¹, C. Lee¹, D. Kim, Ecole Nationale de l’Aviation Civile, France; R.P. Liem¹; ¹The Hong Kong University of Science and Technology, Hong Kong SAR of China | ||||
| 18:00 | 18:30 | 4.9.4 |
MICRO-SIZE MARS AIRPLANE FOR THE STEPWISE MARS LANDING EXPLORATION PROGRAM Y. Shiratsuchi¹, K. Kaneko, The University of Tokyo, Japan; S. Okada, Tokyo University of Agriculture and Technology, Japan; A. Oyama², K. Yamada², H. Tanaka², M. Sato¹; ¹Kogakuin University, Japan ;²Japan Aerospace Exploration Agency, Japan | ||||
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| 16:30 | 17:00 | 5.9.1 |
APPLICATION OF DIFFERENT NUMERICAL TOOLS AND NUMERICAL METHODS FOR PREDICTION OF HEAT EXCHANGER RAMAIR-CONCEPTS FOR HYBRID ELECTRIC PROPULSION AIRCRAFT CONFIGURATIONS A.-R. Hübner¹, J. Kirz¹, K. Weinman¹; ¹German Aerospace Center (DLR), Germany | ||||
| 17:00 | 17:30 | 5.9.2 |
TOWARDS REFINED CONTRAIL SIMULATIONS OF FORMATION FLIGHT SCENARIOS J. Pauen¹, S. Unterstrasser¹, A. Stephan¹; ¹DLR, Germany | ||||
| 17:30 | 18:00 | 5.9.3 |
PERFORMANCE AND ACOUSTIC ANALYSIS OF A DISTRIBUTED ELECTRIC PROPULSION UNMANNED AIRCRAFT R. Navarro¹, L.M. García-Cuevas¹, J. García-Tíscar¹, F.N. Ramírez¹; ¹Universitat Politècnica de València, Spain | ||||
| 18:00 | 18:30 | 5.9.4 |
HIGH FIDELITY MODELING OF ACOUSTIC LINERS FOR AERONAUTICAL APPLICATIONS L. Pinelli¹, M. Marconcini¹, A. Arnone ¹, D. Bacci, Oxford Thermofluids Institute, University of Oxford, United Kingdom; ¹Department of Industrial Engineering, University of Florence, Italy | ||||
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| 16:30 | 17:00 | 6.9.1 |
PRELIMINARY DESIGN OF A FIXED-WING DRONE FOR MARS EXPLORATION ACTIVITIES G. Barbato¹, G. Pezzella¹, A. Viviani¹; ¹Università della Campania Luigi Vanvitelli, Italy | ||||
| 17:00 | 17:30 | 6.9.2 |
PARELLEL UNSTEADY REYNOLDS-AVERAGED NAVIER-STOKES (URANS) STUDEIS OF THE PERFORMANCE OF ONR WATERJET AXWJ-2 S.E. Monroe, Clarkson University, United States | ||||
| 17:30 | 18:00 | 6.9.3 |
NUMERICAL INVESTIGATION ON THE LIQUID SLOSHING DAMPING INSIDE A TANK WITH A FLEXIBLE ANTI-SLOSHING DEVICE F. Rossetti¹, L. Pirillo¹, M. Cimini, ENEA, Italy; M. Bernardini¹, F. Stella¹; ¹Sapienza University, Italy | ||||
| 18:00 | 18:30 | 6.9.4 |
THE EFFECTS OF INITIAL STRESS ON AERODYNAMIC PERFORMANCE OF FLEXIBLE MEMBRANE-SKELETON WINGS WITH FSI SIMULATION Y.-Y. Guo¹, W.-Q. Yang¹, J.-L. Xuan¹, W. Wang¹, D. Xue¹; ¹Northwestern Polytechnical University, China | ||||
| additional information (interactive) | 6.9.R |
VALIDATION OF CFD-BASED DATA SERVICE FOR DRONE INSPECTION OF WIND FARMS WITH FLIGHT TEST DATA M. Turner¹, J. Sharpe¹, M. Kopacz¹, D. Standingford¹, C. Sequeira², B. Sanby², C. Rider²; ¹Zenotech, United Kingdom ;²Flare Bright, United Kingdom | |||||
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| 16:30 | 17:00 | 7.9.1 |
MECHANISM STUDY ON THE IMPACT OF PULSED JET AT THE BLADE TIP LEADING EDGE ON THE FLOW FIELD IN COMPRESSOR Y. Yang, Civil Aviation Flight University of China, China; H. Zhang¹, W. Lu, Nanjing Tech University, China; C. Zhang¹, C. Xu¹, G. Huang¹; ¹Nanjing University of Aeronautics and Astronautics, China | ||||
| 17:00 | 17:30 | 7.9.2 |
IMPLEMENTATION OF ACTIVE FLOW CONTROL ON A SHORT-INLET UHBR ENGINE NACELLE S. Hayböck¹, C. Breitsamter¹; ¹Technical University of Munich, Germany | ||||
| 17:30 | 18:00 | 7.9.3 |
NUMERICAL STUDY OF THE FLOWFIELD IN A DIFFERENTIALLY-THROTTLED LINEAR AEROSPIKE J. Hassan ¹, R. Marsilio¹, G.M. Di Cicca¹, M. Ferlauto¹; ¹Dept. of Mech. and Aerospace Engineering, Politecnico di Torino, Italy | ||||
| 18:00 | 18:30 | 7.9.4 |
ON THE OPTIMIZATION OF (GENERALIZED) IMPEDANCE FOR ACOUSTIC LINERS E. De Bono, France; A.D. Fernandes, Italy; G. Petrone, Italy; M. Ouisse, France; R. Teloli, Italy; S. De Rosa, Italy | ||||
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| 16:30 | 17:00 | 8.9.1 |
AERODYNAMIC SHAPE OPTIMIZATION OF FILLETED INTERSECTIONS WITH SURFACE MESH DEFORMATION H.M. Hajdik¹, A. Yildirim¹, J.R.R.A. Martins¹; ¹University of Michigan, United States | ||||
| 17:00 | 17:30 | 8.9.2 |
NOVEL GRADIENT-ENHANCED MULTI-FIDELITY SURROGATE MODEL ASSISTED ROBUST MULTIDISCIPLINARY DESIGN OPTIMIZATION OF TAILLESS FLYING WING H. Zhao¹, K.-K. Wang¹, Z.-Y. Gong¹, K.Y. Gan¹; ¹Northwestern Polytechnical University, China | ||||
| 17:30 | 18:00 | 8.9.3 |
DESIGN AND AERODYNAMIC OPTIMIZATION OF A THIN-HAUL AIRCRAFT WITH DISTRIBUTED ELECTRIC PROPULSION: ZETHA G. Beghetto¹, M. Boffadossi¹; ¹Politecnico di Milano, Italy | ||||
| 18:00 | 18:30 | 8.9.4 |
ABOUT MODELLING OF EMPIRICAL CORRELATIONS WITHIN AERODYNAMIC PROFILES USING HIGHER ORDER ARTIFICIAL NEURAL NETWORKS P. Kovar, Center of Advanced Aerospace Technology, Czech Republic; J. Fürst, Department of Technical Mathematics, Faculty of Mechanical Engin, Czech Republic | ||||
| additional information (interactive) | 8.9.R |
LOCALIZED AERODYNAMIC SHAPE OPTIMIZATION FOR AUTOMOTIVE APPLICATIONS M. Nayman¹, R.E. Perez¹; ¹Royal Military College of Canada, Canada | |||||
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| 16:30 | 17:00 | 9.9.1 |
WEATHER-AWARE INTEGRATED AIRPORT/AIRSPACE CAPACITY PREDICTION TECHNOLOGIES T. Reynolds¹, K.C. Woodrow¹, H. Iskenderian¹, D. Johnson¹, M. Matthews¹, J. Venuti¹, M. Worris¹, G. Enea¹, B. Crawley, NAV CANADA, Canada; ¹MIT Lincoln Laboratory, United States | ||||
| 17:00 | 17:30 | 9.9.2 |
PROBING AND MODELING LARGE-SCALE AIRLINE NETWORK DISRUPTIONS: 2022 SOUTHWEST AIRLINES SCHEDULING CRISIS M. Peng¹, A. Kamat¹, V. Tran, Harvard University, United States; C. Dawson², C. Fan², M.Z. Li¹; ¹University of Michigan, United States ;²Massachusetts Institute of Technology, United States | ||||
| 17:30 | 18:00 | 9.9.3 |
TIME-BASED CONTROL TO REDUCE TRAJECTORY COMPLEXITY IN THE FLOW-CENTRIC AIR TRAFFIC CONTROL PARADIGM K. Tominaga¹, N. Inoue¹, M. Schultz, University of the Bundeswehr Munich, Germany; Y. Zeng, Nanyang Technological University Singapore, Singapore; E. Itoh¹; ¹The University of Tokyo, Japan | ||||
| 18:00 | 18:30 | 9.9.4 |
APPLICATIONS AND CHALLENGES FOR AIRBORNE AD-HOC COMMUNICATION NETWORKS IN ORP AIRSPACES USING THE L-BAND T. Marks¹, A. Hillebrecht¹, M.A. Bellido-Manganell¹; ¹German Aerospace Center, Germany | ||||
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| 16:30 | 17:00 | 10.9.1 |
DESIGN OF HYDROGEN STORAGE SYSTEMS IN NEW-GENERATION REGIONAL AIRCRAFT V. Memmolo¹, L.M. Cardone¹, G. Petrone¹, S. De Rosa¹; ¹Università degli Studi di Napoli Federico II, Italy | ||||
| 17:00 | 17:30 | 10.9.2 |
THERMAL AND MECHANICAL CYCLING OF THIN-PLY COMPOSITES FOR CRYOGENIC APPLICATIONS M.S. Loukil¹, J. Xu¹, E. Marklund², M. Merzkirch², F. Moreau³, F. Ohlsson³; ¹Linköping University, Sweden ;²Research Institutes of Sweden RISE, Sweden ;³Oxeon AB, Sweden | ||||
| 17:30 | 18:00 | 10.9.3 |
NUMERICAL SOLUTION OF LOX FLOW IN A LIQUID ROCKET ENGINE ADDITIVELY MANUFACTURED COOLING CHANNEL N. Monokrousos¹, L. Könözsy¹, V. Pachidis¹, E. Sozio², F. Rossi²; ¹Cranfield University, United Kingdom ;²Pangea Aerospace, Spain | ||||
| 18:00 | 18:30 | 10.9.4 |
OPTIMIZATION OF POST-PROCESSING HEAT TREATMENT FOR LPBF MODIFIED 2024 ALUMINIUM ALLOY M. Bona¹, A.M. Grande¹; ¹Politecnico di Milano, Italy | ||||
| additional information (interactive) | 10.9.R |
ANALYSIS OF THE POSSIBILITY OF INCREASING THE THERMAL RESISTANCE OF EPOXY RESIN WITH CWNT AND MMT R. Szczepaniak¹, P. Przybylek¹, D. Szczechula¹, A. Krzyzak¹, A. Komorek¹, G. Woroniak, Bialystok University of Technology, Poland; ¹Polish Air Force University, Poland | |||||
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| 16:30 | 17:00 | 11.9.1 |
THE EFFECTS OF ENGINE MASS AND LOCATION ON THE FLUTTER CHARACTERISTICS OF AIRCRAFT WINGS J.R. Banerjee¹, A. Ananthapuvirajah¹, P.H. Cabral, Embraer S.A., Brazil; ¹City, University of London, United Kingdom | ||||
| 17:00 | 17:30 | 11.9.2 |
INFLUENCE OF SKIN CURVATURE ON WINGBOX OPTIMIZATION WITH NONLINEAR STRUCTURAL STABILITY CONSTRAINTS F.M.A. Mitrotta¹, A. Pirrera¹, T. Macquart¹, J.E. Cooper¹, A. Pereira do Prado², P.H. Cabral²; ¹University of Bristol, United Kingdom ;²Embraer, Brazil | ||||
| 17:30 | 18:00 | 11.9.3 |
RANDOM MATRIX MODELLING FOR UNCERTAINTY QUANTIFICATION IN PRESTRESSED STRUCTURES A. Mannoosseril¹, S. Adhikari¹, A.P. Prado², P.H. Cabral²; ¹James Watt School of Engineering, University of Glasgow, United Kingdom ;²Embraer S.A., São José dos Campos, Brazil, Brazil | ||||
| 18:00 | 18:30 | 11.9.4 |
FLUID-SOLID INTERACTIVE MODELLING OF FABRIC-BASED ATMOSPHERIC ENTRY SIZED AERODYNAMIC DECELARATORS E. Malof¹, J. Bayandor¹; ¹University at Buffalo CRASH Lab, United States | ||||
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| 16:30 | 17:00 | 12.9.1 |
PROCESS MODELLING OF COMPOSITES USING A MULTISCALE FRAMEWORK G.M. Odegard, Michigan Technological University, United States; M. Maiaru, Columbia University, United States | ||||
| 17:00 | 17:30 | 12.9.2 |
MICROMECHANICAL MODELING OF THE VISCOELASTIC-VISCOPLASTIC RESPONSE OF FIBER-REINFORCED COMPOSITES T. Nan¹, G.J. Yun, Seoul National University, North Korea; C. Zhang¹; ¹Northwestern Polytechnical University, China | ||||
| 17:30 | 18:00 | 12.9.3 |
A DYNAMIC TEST METHODOLOGY FOR DETERMINING THE LONGITUDINAL COMPRESSIVE RESPONSE OF CARBON FIBER COMPOSITE TOWS J. Gu¹, Y. Bai¹, Z. Zhao¹, C. Zhang¹; ¹Northwestern Polytechnical University, China | ||||
| 18:00 | 18:30 | 12.9.4 |
INVESTIGATION ON VARIABLE-HEIGHT PROTRUSION ARRANGEMENT OF METAL–COMPOSITE HYBRID JOINTS UNDER A TENSILE LOAD Y. Zhao, China; W. Wang, China; X. Wan, China | ||||
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| 16:30 | 17:00 | 13.9.1 |
MODEL-BASED CONCEPTUAL DESIGN AND EVALUATION OF A SOLID-FUEL SCRAMJET VEHICLE M. Bhardwaj¹, S. Rajashankar¹, N. Ananthkrishnan¹, A. Sharma¹, W.-D. Ki², H.-J. Namkoung²; ¹Yanxiki Tech, India ;²Hyundai Rotem, South Korea | ||||
| 17:00 | 17:30 | 13.9.2 |
AERODYNAMIC DEFORMATION EXPERIMENT OF SERPENTINE NOZZLE FOR TURBOFAN AND ANALYSIS OF FLUID-STRUCTURE INTERACTION METHOD Q.-L. Li¹, L. Zhou¹, Z.-X. Wang¹, X.-B. Zhang¹, S. Huang¹; ¹Northwestern Polytechnical University, China | ||||
| 17:30 | 18:00 | 13.9.3 |
DESIGN OF A WIND TUNNEL MODEL FOR A REUSABLE LAUNCH VEHICLE DURING ITS LANDING BURN A.T. Hoang¹, N.J. Lawson¹, T. Bykerk, German Aerospace Center (DLR), Germany; ¹The University of Sydney, Australia | ||||
| 18:00 | 18:30 | 13.9.4 |
COMPARISON OF LIFE CYCLE COST FOR MACH 8 AND MACH 5 HYPERSONIC PASSENGERS AIRCRAFT L. Pugliese¹, D. Ferretto¹, R. Fusaro¹, N. Viola¹; ¹Politecnico di Torino, Italy | ||||
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| 16:30 | 17:00 | 14.9.1 |
DECODING AN IN-FLIGHT REFUELING INCIDENT: AVIATION COMPLEXITY THROUGH STAMP/CAST AND ACCIMAP METHODS J.G. Fowler¹, D.C. Fernandes¹, D.M.C. de Lima¹, G.V. da Rocha¹, M.M. Cardoso Júnior¹; ¹Aeronautic Institute of Technology, Brazil | ||||
| 17:00 | 17:30 | 14.9.2 |
DYNAMIC RESPONSE MONITORING OF FLIGHT CONTROL WITH INCREMENTAL NONLINEAR DYNAMIC INVERSION H. Hofsäß¹, F. Holzapfel¹; ¹Technical University of Munich, Germany | ||||
| 17:30 | 18:00 | 14.9.3 |
INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF WINGS UNDER ICING CONDITIONS AT VARIOUS SWEEP ANGLES X. Xu¹, Y. Zhang¹, G. Chen¹, X. Ma, Xi'an Jiaotong UniversityXi'an Jiaotong University, China; ¹Xi'an Jiaotong University, China | ||||
| 18:00 | 18:30 | 14.9.4 |
SLEEPINESS IN BRAZILIAN AVIATION: A PROBLEM-SOLVING APPROACH V. Gomes¹, T. Paiva¹, A. Herculano¹, T. Dias¹, M.M. Cardoso-Junior¹, M.C. Belderrain¹; ¹ITA, Brazil | ||||
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| 16:30 | 17:00 | 15.9.1 |
FLIGHT MECHANICAL ANALYSIS OF A VERY FLEXIBLE HIGH-ALTITUDE PLATFORM UNDER UNCERTAINTY CONSIDERATIONS Y.J. Hasan¹, N. Fezans¹, A. Voß, DLR Institute of Aeroelasticity, Germany; ¹DLR Institute of Flight Systems, Germany | ||||
| 17:00 | 17:30 | 15.9.2 |
FLIGHT PERFORMANCE AND DYNAMICS OF AN UNCONVENTIONAL SOLAR POWERED UAS G. Charruaz¹, A. Borgia¹, A. Braghin¹, T. Bussi¹, A. Esposito¹, A. Pescosolido¹; ¹Politecnico di Torino, Italy | ||||
| 17:30 | 18:00 | 15.9.3 |
ON THE DEVELOPMENT OF THE STRUCTURAL DIGITAL TWIN OF AN UNMANNED AERIAL VEHICLE X. Zhou¹, M. Dziendzikowski², K. Dragan², M. Giglio³, L. Dong¹, C. Sbarufatti³; ¹Beihang University, China ;²Instytut Techniczny Wojsk Lotniczych, Poland ;³Politecnico di Milano, Italy | ||||
| 18:00 | 18:30 | 15.9.4 |
DYNAMIC FREE FLIGHT TESTS WITH A SUB-SCALE AIRPLANE DESIGNED ACCORDING TO THE FROUDE NUMBER C. Fischer, Instituto Federal de São Paulo and Aeronautics Institute of Tec, Brazil; A.S. Davi, Lilium GmbH, Germany; R.G.A. da Silva¹, L.C.S. Goes¹; ¹Aeronautics Institute of Technology, Brazil | ||||
| additional information (interactive) | 15.9.R |
MANNED AND UNMANNED AERIAL VEHICLES COOPERATIVE COMBAT FRAMEWORK BASED ON LARGE LANGUAGE MODELS H. Shi¹, S. Li, AVIC Chengdu Aircraft Industrial (Group) Co., Ltd., China; Z. Huang¹, S. Li¹, A. Li¹, Y. Zhou¹; ¹BEIHANG UNIVERSITY, China | |||||
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| 16:30 | 17:00 | 16.9.1 |
THERMAL AND GRINDING PERFORMANCE OF 3D PRINTED COMPLIANCE GRINDING TOOLS WITH ROTARY-ENHANCED HEAT TRANSFER STRUCTURE M.C. Li, China; S. Yan, China; K.F. Zhang, China; W. Wang, China; L. Zou, China; Y. Huang, China | ||||
| 17:00 | 17:30 | 16.9.2 |
CYBER-PHYSICAL SYSTEM IMPLEMENTATION FOR THE AR-ASSISTED AIT OF AEROSPACE COMPONENTS J. Pesce¹, A. Carini¹, M. Marinacci¹, M. Boscia¹, P. Marzioli¹, M. Pasquali¹, M. Eugeni¹, M. Mecella¹, P. Piergentili¹, P. Gaudenzi¹; ¹Sapienza University of Rome, Italy | ||||
| 17:30 | 18:00 | 16.9.3 |
DESIGN AND DEVELOPMENT OF THE VISUAL AND AUDITORY LAYER FOR DIFFERENT CABIN/COCKPIT LAYOUT A. Alaimo, Kore Università di Enna, Italy; S. Bagassi¹, E. Carrera, Politecnico di Torino, Italy; T. Fadda¹, M.C. Moruzzi¹; ¹Università di Bologna, Italy | ||||
| |||||||
| 16:30 | 17:00 | 17.9.1 |
MRO FOR VTOLS IN A FUNCTIONAL SEQUENCES SOLUTION SPACE S. Papakonstantinou¹, D. Kloock-Schreiber¹, M. Ziegler², A.N. Mishra, Hamburg University of Technology, Germany; P.K. Jaisawal¹, U. Wieczorek², V. Gollnick¹; ¹Hamburg University of Technology, ILT, Germany ;²Airbus Protect, Germany | ||||
| 17:00 | 17:30 | 17.9.2 |
ASSESSMENT OF A HIGHLY PARAMETERIZED STEADY-STATE MICROSCALE WIND SIMULATOR FOR URBAN AIR MOBILITY APPLICATIONS D.S. Nithya¹, G. Quaranta¹, V. Muscarello², M. Liang²; ¹Politecnico di Milano, Italy ;²RMIT University, Australia | ||||
| 17:30 | 18:00 | 17.9.3 |
A DESIGN OF VFR APPROACH AND DEPARTURE PROCEDURES OF UAM AT VERTIPORTS ADJACENT TO THE AIRPORT S. Kim¹, O. Park¹, H.-S. Shin¹; ¹Cranfield University, United Kingdom | ||||
| 18:00 | 18:30 | 17.9.4 |
ENVIRONMENTAL AND ECONOMIC ASSESSMENT OF AN EVTOL AIRCRAFT FLEET FOR URBAN AIR MOBILITY M. Fioriti¹, M. Borghi¹, G. Pavan¹; ¹Politecnico di Torino, Italy | ||||
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| 10:00 | 10:30 | 1.10.1 |
AIRBUS COMMERCIAL AVIATION SUSTAINABILITY STRATEGY I. Bloy, AIRBUS, France | ||||
| 10:30 | 11:00 | 1.10.2 |
THE CHALLENGE OF SUSTAINABILITY IN COMMERCIAL AVIATION T. Beezhold, Boeing, United States | ||||
| 11:00 | 11:30 | 1.10.3 |
EMBRAER SUSTAINABILITY STRATEGY C.S. Silva, Embraer, Brazil | ||||
| 11:30 | 12:00 | 1.10.4 |
ATR COMMERCIAL AVIATION SUSTAINABILITY STRATEGY D. Cuchet, ATR, France | ||||
| 12:00 | 12:30 | 1.10.5 |
PANEL DISCUSSION PD. D, | ||||
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| 10:00 | 10:30 | 2.10.1 |
HIGH-LIFT PREDICTION WORKSHOPS: RETROSPECTIVE, LESSONS LEARNED, AND FUTURE PROSPECTS C.L. Rumsey, NASA Langley Research Center, United States | ||||
| 10:30 | 11:00 | 2.10.2 |
CFD VALIDATION EXPERIMENTS AT DLR: OVERVIEW AND LESSONS-LEARNED C. Grabe, DLR, Germany | ||||
| 11:00 | 11:30 | 2.10.3 |
THE BEVERLI HILL EXPERIMENTS FOR SMOOTH-BODY TURBULENT FLOW SEPARATION - RETROSPECTIVE, LESSONS LEARNED, AND FUTURE PROSPECTS C.J. Roy¹, K.T. Lowe¹, W.J. Devenport¹, A. Borgoltz¹, A. Gargiulo, University of Virginia, United States; ¹Virginia Tech, United States | ||||
| 11:30 | 12:00 | 2.10.4 |
SYSTEMATIC CFD VERIFICATION - RESULTS FROM THE 2024 HIGH FIDELITY CFD VERIFICATION WORKSHOP M. Galbraith, United States | ||||
| 12:00 | 12:30 | 2.10.5 |
PANEL DISCUSSION P. D, | ||||
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| 10:00 | 10:30 | 3.10.1 |
PERFORMANCE AND ECONOMIC ASSESSMENT OF A WING-INTEGRATED HYBRID LAMINAR FLOW CONTROL SYSTEM B.M.H.J. Fröhler¹, A.A. Pohya¹, J. Häßy¹, T. Kilian¹, A.H. Bismark¹, M. Radestock, Germany; D. Cruz Palacios, Aernnova Aerospace, Spain; ¹German Aerospace Center (DLR), Germany | ||||
| 10:30 | 11:00 | 3.10.2 |
A COST-EFFICIENT PREDICTIVE METHOD FOR AERODYNAMIC PERFORMANCE DEGRADATION OF HORIZONTAL TAIL UNDER ICING CONDITIONS S. Corcione¹, A. De Marco¹, V. Cusati¹; ¹University of Naples Federico II, Italy | ||||
| 11:00 | 11:30 | 3.10.3 |
FUEL-BASED THERMAL MANAGEMENT SYSTEM ARCHITECTURES AND TANK TEMPERATURE EVOLUTION MODELS FOR AVIATION S. Favre¹, F. Di Fede, Leonardo Labs, Leonardo S.p.A., Italy; E. Brusa¹, C. Delprete¹; ¹Politecnico di Torino, Italy | ||||
| 11:30 | 12:00 | 3.10.4 |
SCOPING OF AN AIR SUPPLY CONFIGURATION FOR ACTIVE FLOW CONTROL ON A COMMERCIAL TRANSPORT AIRPLANE HIGH-LIFT SYSTEM C.P. van Dam, University of California - Davis, United States; S.S. Hosseini¹, S.A. Pandya¹; ¹NASA Ames Research Center, United States | ||||
| 12:00 | 12:30 | 3.10.5 |
OPTIMIZATION PROCEDURE FOR THE WING OF A MARS EXPLORATION DRONE A. Viviani¹, A. Aprovitola¹, L. Iuspa², G. Pezzella²; ¹Università della Campania Luigi Vanvitelli , Italy ;²Università della Campania Luigi Vanvitelli , Italy | ||||
| Reserve Paper | 3.10.R |
DESIGN OPTIMIZATION OF A WIG CRAFT’S HIGH LIFT DEVICE CONSIDERING GROUND EFFECT Y.H. Wang¹, W.P. Song¹, H. Nie¹, K.F. Zheng¹, Z.H. Han¹; ¹Northwestern Polytechnical University, China | |||||
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| 10:00 | 10:30 | 4.10.1 |
SONIC BOOM COMPARATIVE STUDY BETWEEN MACH 4.7 OUTDOOR EXPERIMENTAL TESTS AND NUMERICAL SIMULATIONS G. Fasulo¹, L. Federico¹, F. Petrosino¹, S. Graziani², N. Viola², S. Hengy³, B. Martinez³, M. Albisser³; ¹Italian Aerospace Research Centre (CIRA), Italy ;²Politecnico di Torino, Italy ;³French-German research institute of Saint-Louis (ISL), France | ||||
| 10:30 | 11:00 | 4.10.2 |
LANDING AND TAKEOFF NOISE PREDICTION OF CONCEPTUAL SUPERSONIC AIRCRAFT M. Graebert¹, R. Jaron¹, M. Plohr¹, S. Zenkner¹, C. Richter², C. Stöhr², C. Villena Munoz, Cranfield University, United Kingdom; M.-J. van der Meulen³, R. Habing³, M. Huet, ONERA, France; F. Petrosino*, M. Barbarino*, F. Fischer, MTU, Germany; O. Zaporozhets, Institute of Aviation, Poland; ¹DLR, Germany ;²Rolls-Royce Deutschland, Germany ;³NLR, Netherlands ;*CIRA, Italy | ||||
| 11:00 | 11:30 | 4.10.3 |
SENECA’S AIRCRAFT EMISSIONS EVALUATION AND THEIRS ENVIRONMENTAL E. Terrenoire¹, M. Muller¹, E. Ramirez Correra², P. Leyland², K. Synylo³, A. Krupko³, O. Zaporozhets, ILOT, Poland; D. Lee*, B. Owen*, L. Lim*, A. Skowron*, R. Rodriguez DE Leon*, D. Marsh*, S. Matthes, DLR, Germany; P. Madden, RR UK, United Kingdom; S. Bake, RR DE, Germany; C. Mourouzidis, CU, United Kingdom; ¹ONERA, France ;²AEDS, Switzerland ;³NAU, Ukraine ;*MMU, United Kingdom | ||||
| 11:30 | 12:00 | 4.10.4 |
DESIGN OF THE SENECA MACH 1.8 SUPERSONIC AIRLINER WITH MULTI-FIDELITY AERODYNAMIC ANALYSIS FOR NOISE-OPTIMISED TAKE-OFF TRAJECTORIES C. Villena Muñoz¹, C. Lawson¹, A. Riaz¹, A. Sharma¹; ¹Cranfield University, United Kingdom | ||||
| 12:00 | 12:30 | 4.10.5 |
CONCEPTUAL DESIGN METHODOLOGY FOR LOW-SUPERSONIC LH2-POWERED PASSENGERS AIRCRAFT E. Sunzeri¹, D. Ferretto¹, N. Viola¹; ¹Politecnico di Torino, Italy | ||||
| Reserve Paper | 4.10.R |
THERMODYNAMIC DESIGN AND EMISSIONS MODEL OF A MACH 1.8 SUPERSONIC AIRLINER ENGINE M. Plohr¹, S. Zenkner¹, S. Bake², D. Zeitz²; ¹DLR Institute of Propulsion Technology, Germany ;²Rolls-Royce Deutschland Ltd & Co KG, Germany | |||||
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| 10:00 | 10:30 | 5.10.1 |
SHAPING SUSTAINABLE AVIATION WITH CFD-BASED DESIGN OPTIMIZATION J.R.R.A. Martins¹, M.A.S. Abdul-Kaiyoom¹, E.J. Adler¹, A.C. Gray¹, H. Hajdik¹, E. Jonsson¹, A.H.R. Lamkin¹, B. Pacini¹, A. Yildirim¹; ¹University of Michigan, United States | ||||
| 10:30 | 11:00 | 5.10.2 |
ADJOINT-BASED TRANSONIC WING AERODYNAMIC SHAPE OPTIMIZATION INVESTIGATIONS L.V. Rezende Sanches, Universidade Federal do Paraná, Brazil; G.L. Olichevis Halila¹, F. Issamu Kitadani Odaguil¹, J.L.F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil; ¹Embraer, Brazil | ||||
| 11:00 | 11:30 | 5.10.3 |
INVESTIGATING THE INFLUENCE OF AN INBOARD PROPELLER’S VERTICAL OFFSET ON A TRAILING WING’S LIFT AND DRAG DISTRIBUTIONS S.S. Chauhan¹, G. Padovany da Silva, Universidade Federal do Parana, Brazil; G.L. Olichevis Halila, Embraer, Brazil; J.R.R.A. Martins¹, J.L.F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil; ¹University of Michigan, United States | ||||
| 11:30 | 12:00 | 5.10.4 |
A SEQUENTIAL LOCAL ENUMERATION-BASED IMPROVED LATIN HYPERCUBE SAMPLING METHOD FOR BALLISTIC CONSTRAINT DESIGN SPACE H. Zeng¹, Z.-H. Han¹, C.-Z. Xu¹, Y. Zhang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | ||||
| 12:00 | 12:30 | 5.10.5 |
EFFICIENT SHAPE OPTIMIZATION IN AERONAUTICS: INTEGRATING PARAMETRIC CAD AND MESH MORPHING FOR ENHANCED AERODYNAMIC PERFORMANCE A. Lopez¹, G. Magrì², U. Cella¹, G. Urso, RBF Morph srl, Italy; F. Della Barba², M.-E. Biancolini¹; ¹Università di Roma Tor Vergata, Italy ;²Università degli studi di Padova, Italy | ||||
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| 10:00 | 10:30 | 6.10.1 |
RESEARCH ON EFFICIENT ACTIVE T-S WAVE GENERATION METHOD IN BOUNDARY LAYER P. Li¹, Z. Cao¹, D. Li¹; ¹Northwestern Polytechnical University, China | ||||
| 10:30 | 11:00 | 6.10.2 |
NUMERICAL STUDY ON ACOUSTIC RECEPTIVITY OF COMPRESSIBLE LAMINAR FLOW OVER A FLAT PLATE WITH MODIFIED SUPER-ELLIPSE LEADING EDGE B.Z. Xu¹, Z.L. Chen¹; ¹Northwestern Polytechnical University, China | ||||
| 11:00 | 11:30 | 6.10.3 |
CROSSFLOW AND GÖRTLER INSTABILITIES IN HYPERSONIC BOUNDARY LAYERS Y. Xi¹, S. Fu¹; ¹School of Aerospace Engineering, Tsinghua University, China | ||||
| 11:30 | 12:00 | 6.10.4 |
ON THE INFLUENCE OF BASE FLOW CHARACTERISTICS ON CROSSFLOW INSTABILITY IN SWEPT BOUNDARY LAYERS Z.-M. Xu¹, Z.-H. Han¹, H. Nie¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China | ||||
| 12:00 | 12:30 | 6.10.5 |
ON THE INFLUENCE OF SURFACE ROUGHNESS ON BOUNDARY-LAYER TRANSITION FOR SWEPT WINGS V. Prieto, ONERA and ISAE-SUPAERO, France; M. Forte, ONERA, France; E.R. Gowree, ISAE-SUPAERO, France | ||||
| additional information (interactive) | 6.10.R |
NUMERICAL INVESTIGATION ON THE EFFECT OF REYNOLDS NUMBER ON TANDEM DROPLET S.-T. Peng¹, F.-Z. Chen¹, H. Yan¹, X.-Q. Sun¹; ¹Northwestern Polytechnical University, China | |||||
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| 10:00 | 10:30 | 7.10.1 |
A CALL TO ACTION TO ENGAGE THE COMMUNITY TO MEET THE CHALLENGES THAT MUST BE TACKLED TO MAKE ELECTRIFIED AIRCRAFT PROPULSION REAL V.P. Schultz, NASA Langley Research Center, United States; H. Schlickenmaier, HS Advanced Concepts LLC, United States; L. Daelemans, European Union Aviation Safety Authority, Germany; C. Genster, Diamond Aircraft, Austria; M. Walz, Federal Aviation Administration,, United States; E. Holtz, Harbour Air, Canada; S. Ying, Ampaire, United States | ||||
| 10:30 | 11:00 | 7.10.2 |
PANEL DISCUSSION: VINCENT SCHOLTZ, HERBERT SCHLICKENMAIER, LILIAN DAELEMANS, MICHAEL WALTZ, CHRISTOPH GENSTER, EDWARD LOVELACE, ERIKA HOLTZ P. D., | ||||
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| 10:00 | 10:30 | 8.10.1 |
SUMMARY OF DLR RESULTS FROM THE SEVENTH AIAA DRAG PREDICTION WORKSHOP S. Keye¹, O. Brodersen¹, S. Melber-Wilkending¹; ¹German Aerospace Center (DLR), Germany | ||||
| 10:30 | 11:00 | 8.10.2 |
MULTI-FIDELITY SURROGATE MODELING BASED ON DATA EXTENSION USING POD AND ANN W. Wang¹, X. Jia¹, C. Gong¹, C. Li¹; ¹Northwestern Polytechnical University, China | ||||
| 11:00 | 11:30 | 8.10.3 |
FLIGHT TEST AND CFD STUDY OF THE EFFECT OF WING BOUNDARY LAYER TRANSITION ON AILERON BALANCE L. Manfriani¹, X. Liu¹; ¹ZHAW, Switzerland | ||||
| 11:30 | 12:00 | 8.10.4 |
TRANSFER LEARNING FOR REDUCED-ORDER MODELING OF TRANSONIC FLOWS USING MULTIFIDELITY DATA J. Kou¹, C. Ning¹, W. Zhang¹; ¹Northwestern Polytechnical University, China | ||||
| additional information (interactive) | 8.10.R |
RESEARCH ON MULTI-OBJECTIVE AERODYNAMIC/STRUCTURAL DESIGN OPTIMIZATION METHOD FOR LARGE THICKNESS FLATBACK AIRFOILS K.-Y. Zhou¹, S.-Q. Zhang, Jilin Chongtong Chengfei New Material Co., LTD, China; W.-P. Song¹, J.-H. Xu¹, Z.-H. Han¹; ¹Northwestern Polytechnical University, China | |||||
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| 10:00 | 10:30 | 10.10.1 |
FINITE ELEMENT MODEL UPDATE OF VERY FLEXIBLE AIRCRAFT BASED ON GROUND VIBRATION TESTS C.E.S. Cesnik¹, S. Sharqi¹; ¹University of Michigan, United States | ||||
| 10:30 | 11:00 | 10.10.2 |
PRELIMINARY STRUCTURAL DESIGN OF A HIGH ASPECT RATIO RANSPORT AIRCRAFT WITH LAMINAR WING M.R. Ritter¹, M. Schmalz¹, M. Fehrs¹; ¹German Aerospace Center (DLR), Germany | ||||
| 11:00 | 11:30 | 10.10.3 |
NUMERICAL INVESTIGATION OF PASSIVE AND ACTIVE ALLEVIATION OF DYNAMIC LOADS ON HIGH-ASPECT-RATIO-WING VEHICLES C.W. Cheng¹, S. Duessler¹, R. Palacios¹, G. Wilson¹; ¹Imperial College London, United Kingdom | ||||
| 11:30 | 12:00 | 10.10.4 |
CONCEPTUAL DESIGN OF HYDROGEN-POWERED AIRCRAFT: HIGH ASPECT RATIO WINGS AND FLOATING WINGTIPS F. Healy¹, H. Gu¹, D. Rezgui¹, J. Cooper¹; ¹University of Bristol, United Kingdom | ||||
| 12:00 | 12:30 | 10.10.5 |
GUST LOAD PASSIVE ALLEVIATION BY MEANS ON NONLINEAR, BUCKLING DRIVEN, STRUCTURAL RESPONSE F. Toffol¹, C. Bisagni¹; ¹Politecnico di Milano, Italy | ||||
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| 10:00 | 10:30 | 11.10.1 |
HIGHER-ORDER 1D STICK MODELS FOR THE FLUTTER ANALYSIS OF AIRCRAFT STRUCTURES E. Zappino¹, M. Santori¹, M. Petrolo¹, E. Carrera¹; ¹Politecnico di Torino, Italy | ||||
| 10:30 | 11:00 | 11.10.2 |
A FORMULATION FOR WING AEROELASTIC ANALYSIS BASED ON THE UNSTEADY VLM AND STRUCTURAL DISCONTINUOUS GALERKIN TECHNIQUE F. Montano¹, I. Benedetti¹, V. Gulizzi¹; ¹Università degli Studi di Palermo, Italy | ||||
| 11:00 | 11:30 | 11.10.3 |
COUPLED THERMOELASTIC ANALYSIS OF BEAM STRUCTURES USING A REFINED 1D FINITE ELEMENT MODEL M. Filippi¹, R. Azzara¹, M. Santori¹, M. Petrolo¹, E. Carrera¹; ¹Politecnico di Torino, Italy | ||||
| 11:30 | 12:00 | 11.10.4 |
ANALYSIS AND STUDY ON FLUTTER CHARACTERISTICS OF WINGS UNDER TYPICAL FRAGMENT DAMAGE M. Zhang¹, H. Zhan¹, B. Mi¹, Y. Zhang¹, Y. Liu¹; ¹Northwestern Polytechnical University, China | ||||
| 12:00 | 12:30 | 11.10.5 |
REVIEW ON NONLINEAR AEROELASTIC ANALYSIS WITH FREEPLAY Y. Sun¹, Z. Han¹, H. Cao¹, W. Cheng¹, Z. Wu², C. Yang²; ¹Aviation Industry Development Research Center of China, China ;²School of Aeronautic Science and Engineering, Beihang University, China | ||||
| additional information (interactive) | 11.10.R |
INVESTIGATION ON INFLUENCE PARAMETER OF AIRCRAFT-MISSILE SEPARATION BY CONSIDERING AEROELASTICITY Y. Zhang¹, H. Zhan¹, B. Mi¹, M. Zhang¹; ¹Northwestern Polytechnical University, China | |||||
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| 10:00 | 10:30 | 12.10.1 |
INSIGHTS INTO HUMAN FATIGUE: STATISTICAL ANALYSIS IN AIRCRAFT MAINTENANCE J.C. Silva, Brazil; A. Barqueira, Portugal; L.B. Magalhães, Portugal; L.F.F.M. Santos, Portugal | ||||
| 10:30 | 11:00 | 12.10.2 |
PILOT FATIGUE DETECTION USING BP NEUTRAL NETWORKS C.-R. Huang¹, H.-L. Shi¹; ¹AVIC Aerospace Life-Support Industries, Ltd., China | ||||
| 11:00 | 11:30 | 12.10.3 |
ASSESSING MENTAL WORKLOAD AND INTERFACE USABILITY IN MILITARY PILOTS: AN ADVANCED EYE-TRACKING METHODOLOGY A.C. Russo, Universidade de São Paulo, Brazil; A. Sarmento¹, I.S. Rehder¹, M.M. Cardoso-Junior¹, E. Villani¹; ¹Instituto Tecnológico de Aeronáutica, Brazil | ||||
| 11:30 | 12:00 | 12.10.4 |
METAMODELLING OF THE WORKLOAD ASSESSMENT IN SIMULATED FLIGHTS USING THE KRIGING METHOD A. Esposito¹, G. Iacolino¹, C. Orlando¹, A. Alaimo¹; ¹Kore University of Enna, Italy | ||||
| 12:00 | 12:30 | 12.10.5 |
A SYSTEMATIC REVIEW OF HUMAN FACTORS AND AI INFLUENCING OPERATOR PERFORMANCE IN MUM-T ENVIRONMENTS I. de Souza Rehder¹, M.M. Cardoso Júnior¹, E. Villani¹; ¹Aeronautical Institute of Technology, Brazil | ||||
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| 10:00 | 10:30 | 13.10.1 |
OPTIMIZING FLEET ASSIGNMENT DECISIONS FOR REGIONAL AIRLINES WITH HYBRID ELECTRIC AIRCRAFT UPTAKE B. Chan, University of Pennsylvania, United States; Y. Deng¹, N. Tran¹, H. Wu¹, M. Ikeda, RTX Research Center, United States; G. Cinar¹, M.Z. Li¹; ¹University of Michigan, United States | ||||
| 10:30 | 11:00 | 13.10.2 |
SIZING AND PERFORMANCE ANALYSIS OF A MW-CLASS ELECTRIFIED AIRCRAFT PROPULSION (EAP) SYSTEM FOR A PARALLEL HYBRID TURBOPROP CONCEPT D.D.V. Pham¹, C. Recine¹, R.H. Jansen, NASA Glenn Research Center, United States; ¹NASA Ames Research Center, United States | ||||
| 11:00 | 11:30 | 13.10.3 |
REASSESSMENT OF PARAMETRIC OPTIMIZATION AND PERFORMANCE ANALYSIS METHODOLOGY FOR MILD HYBRID AIRCRAFT PROPULSION SYSTEMS J. Gladin¹, E. Aydin¹, J. Kenny¹, A. Burell¹, J. Decroix¹, T. Zaidi¹, R. Gautier¹, D. Mavris¹; ¹ASDL, United States | ||||
| 11:30 | 12:00 | 13.10.4 |
VEHICLE ASSESSMENT AND SYSTEM-WIDE BENEFIT ANALYSES OF HYBRID-ELECTRIC COMMERCIAL AIRCRAFT – ELECTRIFIED POWERTRAIN FLIGHT DEMONSTRATION PROJECT (EPFD) K.D. James¹, A. Meade¹; ¹NASA Ames Research Center, United States | ||||
| 12:00 | 12:30 | 13.10.5 |
PANEL DISCUSSION P. D, United States | ||||
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| 10:00 | 10:30 | 14.10.1 |
MOREALIS – A HOLISTIC APPROACH TO ENHANCE SAFETY FOR MICRO-AIRCRAFT OPERATIONS R.O. Kuchar¹, W. Scholz², B. Dörfler, Rödel Aerospace Systems, Germany; P. Herrmann², P. Jamakatel, University of the Bundeswehr Munich , Germany; J. Karger², J.J. Kiam³, J. Klennert*, M. Klennert*, M. Lindlar, German Aerospace Center (DLR-ME), Germany; M.S. May¹, D. Milz¹, N. Mummº, D. Nospes³, L. Peterº, G. Looye¹, A. Schulte³, P. Stütz³; ¹German Aerospace Center (DLR-SR), Germany ;²SFL GmbH., Germany ;³University of the Bundeswehr Munich, Germany ;*STAR Healthcare Management GmbH., Germany ;ºAmazilia Aerospace GmbH., Germany | ||||
| 10:30 | 11:00 | 14.10.2 |
GENERATION AND COMMUNICATION OF STRATEGIC PLANS AT DIFFERENT LEVELS OF ABSTRACTION FOR INTELLIGENT ASSISTANCE SYSTEMS IN GENERAL AVIATION P. Jamakatel¹, J.J. Kiam ¹; ¹University of the Bundeswehr Munich, Germany | ||||
| 11:00 | 11:30 | 14.10.3 |
PILOT SAFETY – SUPPORT BY BIOMEDICAL MONITORING IN PILOTS WITH HEALTH RISKS M. Lindlar¹, J. Klennert, STAR Healthcare Management GmbH, Germany; S. Plath¹; ¹German Aerospace Center, Germany | ||||
| 11:30 | 12:00 | 14.10.4 |
MIXED FLIGHT CONTROL LAYOUT FOR ULTRALIGHT GENERAL AVIATION AIRCRAFT M. May¹, D. Milz¹, W. Scholz², P. Herrmann², J. Karger², L. Peters³, N. Mumm³, R. Kuchar¹; ¹DLR, Germany ;²SFL GmbH, Germany ;³Amazilia Aerospace GmbH, Germany | ||||
| 12:00 | 12:30 | 14.10.5 |
SENSOR AND COVERAGE PATH PLANNING FOR THE MONITORING OF AIRCRAFT EMERGENCY LANDING SITES D. Nospes¹, P. Stütz¹; ¹University of the Bundeswehr Munich, Germany | ||||
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| 10:00 | 10:30 | 15.10.1 |
APPLICATION OF UAS TECHNOLOGIES TO CREATE RESILIENT RURAL COMMUNITIES M.J. Logan, NASA, United States | ||||
| 10:30 | 11:00 | 15.10.2 |
ENHANCING QUADCOPTER CONTROL: A MODEL REFERENCE ADAPTIVE CONTROL APPROACH WITH NEURAL NETWORKS S.R. Bassolillo¹, G. Raspaolo², L. Blasi², E. D'Amato¹; ¹Università degli Studi di Napoli Parthenope, Italy ;²Università degli Studi della Campania L. Vanvitelli, Italy | ||||
| 11:00 | 11:30 | 15.10.3 |
ONBOARD TRAJECTORY OPTIMIZATION FOR RADIUS TO FIX TURNS D.M. Gierszewski¹, P. Piprek¹, F. Holzapfel, Technische Universität München, Germany; ¹ Technische Universität München, Germany | ||||
| 11:30 | 12:00 | 15.10.4 |
ADAPTIVE CONTROL AND MISSION PLANNER DESIGN FOR UAV OPERATIONS WITH BATTERY MANAGEMENT A. Boldrini¹, G. Gozzini¹, D. Invernizzi¹; ¹Politecnico di Milano, Italy | ||||
| 12:00 | 12:30 | 15.10.5 |
PASSIVE FAULT TOLERANT CONTROL OF A DUAL-SYSTEM UAV IN TRANSITION FLIGHT J. Cai¹, M. Lovera¹; ¹Politecnico di Milano, Italy | ||||
| additional information (interactive) | 15.10.R |
A NOVEL APPROACH TO AUTOMATED TRACKING CONTROL OF HYBRID TILTING ROTOR UAVS USING LQG CONTROLLER AND STATE MACHINE J.L. Kurniawan¹, P.B.A. Baylon¹, R.A. Sasongko¹; ¹Institut Teknologi Bandung, Indonesia | |||||
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| 10:00 | 10:30 | 17.10.1 |
APPLICATION OF CLUSTERING TECHNIQUES IN OPTIMISATION-BASED FLIGHT CONTROL SYSTEM CLEARANCE P. Piprek¹, P.M. Dias¹, J. Tonti¹, D. Schwalb¹; ¹Airbus Defence and Space GmbH, Germany | ||||
| 10:30 | 11:00 | 17.10.2 |
SELF-DRIVING AND MODEL-BASED EXTREMUM SEEKING CONTROL IN TIGHT FORMATION FLIGHT FOR FUEL SAVING D.B. Rossato, Faculdade de Tecnologia SENAI, Brazil; K.H. Kienitz, Instituto Tecnológico de Aeronáutica, Brazil | ||||
| 11:00 | 11:30 | 17.10.3 |
APPLICATION OF A MORE INTEGRATED TOTAL ENERGY CONTROL SYSTEM FOR IMPROVING AIRCRAFT AND ENGINE CONTROL EFFICIENCY T. Giusti Degaspare, Embraer S.A., Brazil; K.H. Kienitz, Instituto Tecnológico de Aeronáutica, Brazil | ||||
| 11:30 | 12:00 | 17.10.4 |
FLYING V DIRECTIONAL FLIGHT CONTROL: AN EXPERIMENTAL INVESTIGATION R. Vos¹, N. Johnson¹, S. Nolet¹; ¹TU Delft, Netherlands | ||||
| 12:00 | 12:30 | 17.10.5 |
REENTRY TRAJECTORY DESIGN FOR DEFORMABLE HYPERSONIC VEHICLES BASED ON NEURAL NETWORKS C.-K. Zhou¹, Z.-F. Luo¹, T. Zhang¹; ¹SUN YAT-SEN UNIVERSITY, China | ||||
| Reserve Paper | 17.10.R |
AILERON-FLAP-INTEGRATED ROLL CONTROL LAW BY OPTIMIZED CONTROL ALLOCATION FOR FLEXIBLE TRANSPORT AIRCRAFT H. Wilke¹, G.C. Silva¹, F.J. Silvestre¹; ¹Technische Universität Berlin, Germany | |||||
| additional information (interactive) | 17.10.R |
A MODEL PREDICTIVE CONTROL ALGORITHM FOR THE FORMATION CONTROL OF NANOSATELLITES IN LEO ORBIT C. Santoro¹, S.R. Bassolillo, University of Naples Parthenope, Italy; A. Ferraro, University of Reggio Calabria Mediterranea, Italy; L. Blasi¹, I. Notaro¹; ¹University of Campania L. Vanvitelli, Italy | |||||
| additional information (interactive) | 17.10.R |
MODELING AND FLIGHT CONTROL LAW DESIGN FOR A SEAPLANE DURING WATER SURFACE TAKEOFF Y. Liu¹, Y.-H. Nong², X. Liu, Shanghai Aircraft Airworthiness Certification Center, China; Z.-H. Cheng², M.-X. Zhang¹; ¹Northwestern Polytechnical University, China ;²AVIC General Huanan Aircraft Industry, China | |||||
| additional information (interactive) | 17.10.R |
TRAJECTORY DESIGN FOR ASTEROID SAMPLE RETURN COMBINING BALLISTIC CAPTURE AND AEROBRAKING Z.-F. Luo¹, Y.-J. Lian, National University of Defense Technology, China; C. Zhang, Chinese Academy of Sciences, China; T. Zhang¹; ¹Sun Yat-sen University, China | |||||
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| 13:30 | 14:00 | 1.11.1 |
NASA SUSTAINABLE FLIGHT NATIONAL PARTNERSHIP OPERATIONS RESEARCH A. Sultan, NASA (ARMD), United States | ||||
| 14:00 | 14:30 | 1.11.2 |
HOW CAN EUROPE BECOME THE MOST EFFICIENT AND ENVIRONMENTALLY-FRIENDLY SKY TO FLY IN THE WORLD? A. Boschen, SESAR Joint Undertaking, Germany | ||||
| 14:30 | 15:00 | 1.11.3 |
RECENT FLIGHT EXPERIMENTS SHOW THE CLIMATE BENEFITS OF SUSTAINABLE AVIATION FUELS (SAF) AND ADVANCED ENGINE TECHNOLOGIES R. Moore, NASA (LaRC), United States; C. Voigt, DLR, Germany | ||||
| 15:00 | 15:30 | 1.11.4 |
AI DRIVEN DECISION SUPPORT IN OPERATIONS STEERING C. Most, Lufthansa, Germany | ||||
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| 13:30 | 14:00 | 2.11.1 |
STRUT-BRACED DRY WING CONCEPT FOR HYDROGEN-POWERED AIRCRAFT M. Méheut¹, D. Losada Costoso¹, F. Moens¹, O. Atinault¹, C. Julien¹, L. Vertonghen¹, L. Coelho¹, V. Priasso¹, A. Lannoo¹, S. Defoort¹, E. NGuyen Van¹, C. David¹, D. Glenis¹, J. Sodja², S. de Boer², J. Schwingel³, D. Eisenhut³; ¹ONERA, France ;² Delft University of Technology, Netherlands ;³University of Stuttgart, Germany | ||||
| 14:00 | 14:30 | 2.11.2 |
OPTIMAL WING ASPECT RATIO OF HIGHLY EFFICIENT LONG-RANGE AIRCRAFT T.F. Wunderlich, German Aerospace Center (DLR), Germany | ||||
| 14:30 | 15:00 | 2.11.3 |
NASA TRANSONIC TRUSS-BRACED WING STUDIES D.P. Wells¹, G.M. Gatlin¹, J.C. June¹, T.V. Marien¹; ¹NASA Langley Research Center, United States | ||||
| 15:00 | 15:30 | 2.11.4 |
EXPLORING ROLL MANEUVERABILITY OF FUTURE AIRCRAFT WITH HIGH AR WINGS D. Sanghi¹, C.E.S. Cesnik¹, C. Riso¹; ¹University of Michigan, United States | ||||
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| 13:30 | 14:00 | 3.11.1 |
CONCEPTUAL DESIGN AND SIZING OF A SOLAR POWERED QUAD-ROTOR FIXED WING HYBRID UAV FOR EXPLORATION OVER MARS A. Kalgutkar¹, P. Gupta¹, P. Priyadarshi, Vikram Sarabhai Space Centre, India, India; R.S. Pant¹; ¹Indian Institute of Technology Bombay, India, India | ||||
| 14:00 | 14:30 | 3.11.2 |
INNOVATIVE UAVS WITH CONFIGURATION OF LIKING BOTH PLANE AND KITE FOR WIND POWER Z.X. Yao, Shenyang Aircraft Design and Research Institute, China | ||||
| 14:30 | 15:00 | 3.11.3 |
FRAMEWORK DEVELOPMENT FOR CONCEPTUAL DESIGN AND CONFIGURATION ANALYSIS OF EVTOL AIRCRAFT R.Y. Yanev¹, I. Staack¹; ¹Technische Universität Braunschweig, Germany | ||||
| 15:00 | 15:30 | 3.11.4 |
ANALYSIS OF STEALTH ENHANCEMENT DESIGN PROCESS AND METHODS FOR UNMANNED AERIAL VEHICLE G. Jia, China; D. Hu, China; Z. Guo, China; Y. Lu, China; D. Liu, China | ||||
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| 13:30 | 14:00 | 4.11.1 |
FROM THEORY TO FLIGHT: THE BOX-WING CONFIGURATION IMPLICATIONS FOR THE NEXT-GENERATION AIRCRAFT K. Abu Salem¹, G. Palaia¹, A. Frediani, SkyBox Engineering, Italy; ¹Politecnico di Torino, Italy | ||||
| 14:00 | 14:30 | 4.11.2 |
PRELIMINARY SIZING OF A LOW-ALTITUDE AIRSHIP INCLUDING ION PLASMA THRUSTERS C.E.D. Riboldi¹, M. Belan¹, S. Cacciola¹, R. Terenzi¹, S. Trovato¹, D. Usuelli¹, G. Familiari¹; ¹Dept. of Aerospace Science and Technology, Politecnico di Milano, Italy | ||||
| 14:30 | 15:00 | 4.11.3 |
GENERAL DESIGN CONSIDERATIONS FOR SOLAR-ELECTRIC HIGH-ALTITUDE LONG-ENDURANCE AIRCRAFT A. Bierig¹, F. Nikodem¹, D. Rothe¹; ¹DLR, Germany | ||||
| 15:00 | 15:30 | 4.11.4 |
CONTINUING DEVELOPMENT OF A NOVEL CERTIFIABLE AIRLINER “GONDOLA” USING LIQUID HYDROGEN R.K. Nangia, Nangia Aero, United Kingdom; L. Hyde, Consulting, United Kingdom; J.E. Cooper, Bristol University, United Kingdom | ||||
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| 13:30 | 14:00 | 5.11.1 |
JET NOISE ABATEMENT VIA SURROGATE MODEL-BASED AEROACOUSTIC OPTIMISATION USING LARGE EDDY SIMULATION G. Yang, University of Bristol, United Kingdom | ||||
| 14:00 | 14:30 | 5.11.2 |
NUMERICAL STUDIES ON NOISE-SHIELDING EFFECTS OF A BLENDED-WING-BODY AIRCRAFT USING BOUNDARY ELEMENT METHOD H.Y. Wang¹, C.T. Mutasa¹, Z.L. Chen¹; ¹Northwestern Polytechnical University, China | ||||
| 14:30 | 15:00 | 5.11.3 |
AERODYNAMICS AND AEROACOUSTIC ANALYSIS OF A SUPERSONIC SLENDER-BODY GEOMETRY M. De Rosa¹, A. Glorioso¹, G. Pezzella¹, A. Viviani¹; ¹University of Campania, Italy | ||||
| 15:00 | 15:30 | 5.11.4 |
MEASUREMENTS OF T-S WAVES DUE TO ACOUSTIC DISTURBANCES IN EXPERIMENTS Z. Cao¹, P.F. Li¹, D. Li¹; ¹Northwestern Polytechnical University, China | ||||
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| 13:30 | 14:00 | 6.11.1 |
UNCERTAINTY ANALYSIS OF THE AERODYNAMIC PERFORMANCE OF EVTOL PROPELLERS VIA REYNOLDS STRESS TENSOR PERTURBATION G. Gori¹, A. Zanotti¹; ¹Department of Aerospace Science and Technology, PoliMI, Italy | ||||
| 14:00 | 14:30 | 6.11.2 |
ASSESSMENT OF AN ADAPTIVE ONE-EQUATION TURBULENCE MODEL FOR LEADING-EDGE VORTEX FLOWS ON MULTIPLE SWEPT DELTA WINGS M. Zieher¹, D. Sedlacek¹, C. Breitsamter¹; ¹Technical University of Munich, Germany | ||||
| 14:30 | 15:00 | 6.11.3 |
EFFECTS OF GEOMETRY PARAMETERS ON AERODYNAMIC CHARACTERISTICS OF ROTOR AIRFOIL IN REVERSE FLOW C.-P. Liu¹, W.-P. Song¹, S.-Q. Han, Sichuan University, China; Z.-H. Han¹; ¹Northwestern Polytechnical University, China | ||||
| 15:00 | 15:30 | 6.11.4 |
ASSESSMENT OF EXPLICIT ALGEBRAIC REYNOLDS STRESS MODELS APPLIED TO AERONAUTICAL FLOWS T. Chagas Silva, Instituto Tecnológico de Aeronáutica, Brazil; J.L.F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil | ||||
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| 13:30 | 14:00 | 7.11.1 |
PIONEERING THE EXCHANGE OF KNOWLEDGE B. Nagel, Germany | ||||
| 14:00 | 14:30 | 7.11.2 |
DIGITAL COLLABORATION FOR SUSTAINABLE AVIATION A.S.J. van Herden, United Kingdom | ||||
| 14:30 | 15:00 | 7.11.3 |
HARNESSING THE POWER OF METAVERSE TO REVOLUTIONIZE AIRCRAFT AND MRO RESEARCH K.K. Koschlik, Germany | ||||
| 15:00 | 15:30 | 7.11.4 |
MANAGING DIGITAL COMPLEXITY C. Jouannet, Sweden | ||||
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| 13:30 | 14:00 | 8.11.1 |
LOW-SUBSONIC AERODYNAMIC ANALYSES OF A NONPLANAR BWB MODEL: AN EXPERIMENTAL AND CFD STUDY M. Nikbay¹, K. Kontis², H. Aleisa², B. Pirlepeli¹; ¹Istanbul Technical University, United Kingdom ;²University of Glasgow, United Kingdom | ||||
| 14:00 | 14:30 | 8.11.2 |
ASPECT RATIO AND ADVANCE RATIO EFFECTS ON AERODYNAMIC CHARACTERISTICS OF FLEXIBLE FLAPPING WINGS R. Addo-Akoto¹, S.-G. Lee¹, J.-S. Han, Chungnam National University, South Korea; J.-H. Han¹; ¹KAIST, South Korea | ||||
| 14:30 | 15:00 | 8.11.3 |
NUMERICAL STUDY ON THE FIRST-STAGE RE-ENTRY TRAJECTORY USING AN INFLATABLE BALLUTE V. Orlandini¹, R. Paciorri¹, A. Assonitis¹, A. Bonfiglioli, Università degli Studi della Basilicata, Italy; ¹University of Rome La Sapienza, Italy | ||||
| 15:00 | 15:30 | 8.11.4 |
AERODYNAMIC ANALYSIS OF A FLAP-BASED DEPLOYABLE RE-ENTRY SYSTEM UNDER RAREFIED CONDITIONS D. Vera Sepúlveda¹, R. Cassineli Palharini¹, E. Gaglio, Scuola Superiore Meridionale, Italy; R. Savino, University of Naples “Federico II”, Italy; ¹Universidad Técnica Federico Santa Marpia, Chile | ||||
| additional information (interactive) | 8.11.R |
SIMULATION STUDY ON AERODYNAMIC CHARACTERISTICS OF COMBINED LOW ASPECT RATIO UAV Y. Li¹, X. Xu¹, Z. Zhou¹, Y. Bai¹, H. Wang¹, B. Xu¹; ¹Northwestern Polytechnical University, China | |||||
| additional information (interactive) | 8.11.R |
RESEARCH ON OPTIMAL TORSIONAL DEFORMATION OF FLAPPING WING J. Liu¹, D. Xue¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | |||||
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| 13:30 | 14:00 | 9.11.1 |
ESTIMATING THE IMPACT OF NUMERICAL WEATHER PREDICTION DATA MODELS ON SHORT-HAUL MINIMUM COST TRACKS N.K. Wickramasinghe¹, Y. Nakamura¹, A. Senoguchi¹; ¹Electronic Navigation Research Institute, Japan | ||||
| 14:00 | 14:30 | 9.11.2 |
PAIRWISE SWAPPING SEQUENCE OPTIMIZATION BY METROPOLIS-HASTING ALGORITHM WITH QUANTUM ANNEALING FOR AIR TRAFFIC CONTROL N. Yoshikawa, Mitsubishi Electric Corporation, Japan | ||||
| 14:30 | 15:00 | 9.11.3 |
AUTOMATED OPERATION OF HIGH-PERFORMANCE FIXED-WING DRONES: A POTENTIAL GAME-CHANGER FOR GREEN AERIAL SERVICES M. Spieck, Thelsys, Germany; J.H. Binnebesel¹, J. Mehnen¹; ¹mb+Partner, Germany | ||||
| 15:00 | 15:30 | 9.11.4 |
STRUCTURED ANALYSIS ESTIMATION FOR ELECTRICAL ENERGY DEMAND ON AIRPORT OPERATIONS FOR HYBRID REGIONAL AND ELECTRIC TOWING PARAMETERIZED BY MOVEMENT METRICS CONSIDERING UPCOMING ELECTRIC INTENSIVE TECHNOLOGIES AND EMISSION REDUCTIONS IN THE UPCOMING DECADE T. Oliveira¹, A. Carvalho¹; ¹The Boeing Company, Brazil | ||||
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| 13:30 | 14:00 | 10.11.1 |
PATCHBOND II - CERTIFICATION OF ADHESIVE BONDED REPAIRS FOR PRIMARY AEROSPACE COMPOSITE STRUCTURES J. Jokinen, Tampere University, Finland; T. Thorvaldsen, Norwegian Defence Research Establishment, Norway; P. Nijhuis, Royal Netherlands Aerospace Centre, Netherlands; M. Kadlec¹, R. Ruzek¹, L. Munch, University of Stuttgart, Institute of Aircraft Design, Germany; M. Hoffmann, Airbus Defence and Space GmbH, Germany; T. Viitanen, Technical Research Center of Finland Ltd, Finland; M. Wallin, Patria Aviation, Finland; G. Sagvolden, Light Structures AS, Norway; C. Sbarufatti², L. Martulli², A. Bernasconi²; ¹Czech Aerospace Research Centre, Czech Republic ;²Politecnico di Milano, Department of Mechanical Engineering, Italy | ||||
| 14:00 | 14:30 | 10.11.2 |
HOT-WET CONDITIONING AND THE SENSITIVITY OF MECHANICAL TESTING WITHIN SURFACE TREATMENT QUALIFICATION FOR AIRCRAFT D. Blanco Garde¹, F. Mews¹, J. Jokinen¹, N. Pournoori¹, M. Kanerva¹; ¹Tampere University, Finland | ||||
| 14:30 | 15:00 | 10.11.3 |
STABLE LOCALIZED CORROSION IN A 7075-T6 ALUMINUM ALLOY FSW JOINT: MECHANISM AND MITIGATION K. Li¹, Y. Ma, Chongqing University of Technology, China; Y. Han¹; ¹AVIC Manufacturing Technology Institute, China | ||||
| 15:00 | 15:30 | 10.11.4 |
INVESTIGATION ON THE MECHANISM OF THERMAL CYCLING FAILURE IN C/SIC COATING COMPOSITE MATERIALS Y. Ma, China; X. Zha, China; P. Cheng, China; J. Xie, China; L. Li, China; X. Liu, China | ||||
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| 13:30 | 14:00 | 11.11.1 |
DESIGN OF A HIGH ENTHALPY HYPERSONIC NOZZLE FOR “GHIBLI” PLASMA WIND TUNNEL D. Guida¹, A. Smoraldi¹, A. Schettino, C.I.R.A., Germany; ¹CIRA Italian Aerospace Research Centre, Italy | ||||
| 14:00 | 14:30 | 11.11.2 |
SPARSE RECONSTRUCTION OF SURFACE LOADS ON AIRCRAFT USING POD AND RBFNN X. Jia¹, C. Gong¹, C. Li¹; ¹Northwestern Polytechnical University, China | ||||
| 14:30 | 15:00 | 11.11.3 |
DEVELOPMENT OF UNSTEADY PRESSURE-SENSITIVE PAINT FOR LOW REYNOLDS NUMBER WIND TUNNEL TESTS IN LOW-PRESSURE ENVIRONMENTS S. Takaya¹, K. Shibata¹, D. Numata¹; ¹Tokai University, Japan | ||||
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| 13:30 | 14:00 | 12.11.1 |
STUDY ON LOW-VELOCITY IMPACT BEHAVIOR AND RESIDUAL PERFORMANCE PREDICTION OF CFRP T-JOINTS J. Zhou, China; C. Zhang, China | ||||
| 14:00 | 14:30 | 12.11.2 |
THE RESISTANCE TO THE HIGH-VELOCITY IMPACT OF THE INTRA-LAYER HYBRID PLAIN WEAVE COMPOSITES H. Wu¹, Y. Bai¹, S.-L. Fang¹, Z.-Q. Zhao¹, C. Zhang¹; ¹Northwestern Polytechnical University, China | ||||
| 14:30 | 15:00 | 12.11.3 |
MODELING THE TEMPERATURE-RISE BEHAVIOR OF 2D TRIAXIAL BRAIDED COMPOSITES UNDER IMPACT LOADS C. Zhang¹, P. Liu¹, Y.-L. Li¹; ¹Northwestern Polytechnical University, China | ||||
| 15:00 | 15:30 | 12.11.4 |
THE EFFECT OF TARGET THICKNESS ON THE BALLISTIC BEHAVIOR OF HYBRID CFRP/KFRP COMPOSITES S. Zhao¹, J. Huang¹, C. Zhang¹; ¹Northwestern Polytechnical University, China | ||||
| additional information (interactive) | 12.11.R |
EFFECT OF INFILL STYLE AND DENSITY ON SELECTED MECHANICAL PROPERTIES OF THE CARBON FIBRE REINFORCED ABS MFD FILAMENT M. Mucha¹, D. Sikorski, 41st Training Air Base, Poland; R. Szczepaniak¹, R. Babel¹, A. Krzyzak¹, T. Zahorski¹; ¹Polish Air Force University, Poland | |||||
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| 13:30 | 14:00 | 13.11.1 |
FLOW CHARACTERISTICS OF THE INLET IN TURBOPROP ENGINE WITH THE INFLUENCE OF SANDS B. Mi¹, H. Zhan¹, J. Yu, No. 5715 Factory of PLA, China; ¹Northwestern Polytechnical University, China | ||||
| 14:00 | 14:30 | 13.11.2 |
DEEP LEARNING BASED FAST PREDICTION OF AERODYNAMIC PARAMETERS FOR DUCTED PROPELLERS L. Liu¹, L. Zeng¹, T. Wang¹, Z. Gao¹, X. Shao¹; ¹Zhejiang University, China | ||||
| 14:30 | 15:00 | 13.11.3 |
LOW-SPEED PROPELLER FOR UAV APPLICATIONS, FROM DESIGN TO EXPERIMENTAL EVALUATION M. Crona¹, S. Dinger¹, P. Samuelsson¹, H. Strömfeldt¹, I. Jonsson¹; ¹Chalmers University of Technology, Sweden | ||||
| 15:00 | 15:30 | 13.11.4 |
Lecture canceled | ||||
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| 13:30 | 14:00 | 14.11.1 |
Lecture canceled | ||||
| 14:00 | 14:30 | 14.11.2 |
A FAST INFORMATION THEORETICALLY SECURE RADIO COMMUNICATION PROTOCOL BASED ON GNSS POSITIONING S. Morioka, Interstellar Technologies Inc., Japan; S. Obana, Hosei University, Japan; M. Yoshida, NICT, Japan | ||||
| 14:30 | 15:00 | 14.11.3 |
MUTUAL POSITION PLAUSIBILITY CHECKING IN FLYING AD-HOC NETWORKS USING DISTANCE MEASUREMENTS T. Marks, German Aerospace Center, Germany; K. Fuger, Hamburg University of Technology, Germany | ||||
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| 13:30 | 14:00 | 15.11.1 |
FAILURE HANDLING ON A SPLIT-FLAP ULTRALIGHT GENERAL AVIATION AIRCRAFT WITH HYBRID NONLINEAR DYNAMIC INVERSION D. Milz¹, M. May¹, J. Martins¹, R. Kuchar¹, G. Looye¹; ¹German Aerospace Center (DLR), Germany | ||||
| 14:00 | 14:30 | 15.11.2 |
EXPLORING A CATEGORY OF LIMIT CYCLE OSCILLATIONS IN AIRCRAFT HYDRAULIC SYSTEMS S. Yang¹, Y. Long, School of Energy and Power Engineering, Beihang University, China; Z. Hu¹; ¹Institute for Aero Engine, Tsinghua University, China | ||||
| 14:30 | 15:00 | 15.11.3 |
SIMPLIFIED MODELS OF PILOT BIOMECHANICS FOR ROTORCRAFT VERTICAL BOUNCE ANALYSIS T. Aresi¹, A. Zanoni¹, G. Cassoni¹, P. Masarati¹; ¹Politecnico di Milano, Italy | ||||
| 15:00 | 15:30 | 15.11.4 |
ENHANCED SAFETY THROUGH AI: AN ASSESSMENT OF ADVERSARIAL REINFORCEMENT LEARNING FOR CONTROL OF COMPLEX AIRCRAFT C. Koopman¹, D. Zammit-Mangion¹; ¹University of Malta, Malta | ||||
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| 13:30 | 14:00 | 16.11.1 |
VALUE-DRIVEN TRADESPACE EXPLORATION FOR AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN G. Donelli¹, J.M.G.D. Mello², F.I.K. Odaguil², T. Van der Laan, GKN/Fokker, Netherlands; L. Boggero¹, B. Nagel¹; ¹German Aerospace Center DLR, Germany ;²Embraer, Brazil | ||||
| 14:00 | 14:30 | 16.11.2 |
UNCERTAINTY PROPAGATION IN VALUE-DRIVEN DECISION-MAKING FOR THE AIRCRAFT, MANUFACTURING AND SUPPLY CHAIN DESIGN G. Ascione¹, G. Donelli¹, L. Boggero¹, B. Nagel¹; ¹DLR, Germany | ||||
| 14:30 | 15:00 | 16.11.3 |
A SUPPORTING FRAMEWORK FOR AIRCRAFT MRO OPERATIONS. CAPACITY PLANNING, TASKS TRACEABILITY AND DISEMBARKED ITEMS TRACKING F. Martone¹, G. Zazzaro¹, M. Inverno¹, S. De Luca, Atitech S.p.A., Italy; F. Mainieri, Major Bit Consulting s.r.l., Italy; G. Romano¹; ¹C.I.R.A. Italian Aerospace Research Centre, Italy | ||||
| 15:00 | 15:30 | 16.11.4 |
COMPUTER VISION ALGORITHMS FOR THE IDENTIFICATION OF DAMAGES ON FULL-SCALE AIRCRAFT COMPONENTS S. Merola ¹, M. Guida¹, F. Marulo¹; ¹University of Naples Federico II, Italy | ||||
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| 13:30 | 14:00 | 17.11.1 |
VALIDATION OF ENERGY CHARACTERISTICS IN FLIGHT CONTROL SYSTEM BASED ON A MULTIDISCIPLINARY VIRTUAL PLATFORM Y. Wang¹, M. Sun¹, J. Fu¹; ¹Beihang University, China | ||||
| 14:00 | 14:30 | 17.11.2 |
RESULTS OF THE SCALED FLIGHT DEMONSTRATOR FLIGHT TESTS P. Schmollgruber¹, C. Toussaint¹, P. Iannelli, CIRA, Italy; H. Jentink, Royal NLR, Netherlands; D. Kierbel, Airbus S.A.S., France; ¹ONERA, France | ||||
| 14:30 | 15:00 | 17.11.3 |
FAULT DETECTION FOR AN AIRCRAFT ELEVATOR F.C. Antoniazzi¹, A.G.P. Sarmento¹, E. Villani¹; ¹Aeronautical Institute of Technology, Brazil | ||||
| 15:00 | 15:30 | 17.11.4 |
ENERGY PREDICTION DURING APPROACH AND LANDING BASED ON LONG SHORT-TERM MEMORY MODEL J.-Q. Yan, School of Aeronautics, Northwestern Polytechnical University, China | ||||
| additional information (interactive) | 17.11.R |
DATA ORIENTED EVALUATION OF FLIGHT CHARACTERISTIC MODELS BY USING BAYES FACTOR M. Naruoka¹, T. Ninomiya¹; ¹Japan Aerospace Exploration Agency, Japan | |||||