| |||||||
| 10:30 | 11:00 | 1.1.1 |
FLYZERO: THE UK VISION FOR ZERO-CARBON EMISSION AIR TRAVEL S. Pendry, ATI, United Kingdom | ||||
| 11:00 | 11:30 | 1.1.2 |
IMPACT OF NASCENT TECHNOLOGIES ON THE SUSTAINABILITY ATTRIBUTES OF AN EVOLUTIONARY SINGLE-AISLE AIRCRAFT N.J. Allen, Aerospace Technology Institute, United Kingdom; M.R. Schofield, Ellondee Ltd, United Kingdom | ||||
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| 10:30 | 11:00 | 2.1.1 |
LARGE-SCALE MULTIFIDELITY AEROSTRUCTURAL OPTIMIZATION OF A TRANSPORT AIRCRAFT N. Wu¹, C.A. Mader¹, J.R.R.A. Martins¹; ¹University of Michigan, United States | ||||
| 11:00 | 11:30 | 2.1.2 |
REGIONAL JET RETROFITTING DESIGN: FROM STAKEHOLDERS’ NEEDS AND SYSTEM’S REQUIREMENTS TO MDAO WORKFLOW FORMULATION M. Mandorino¹, P. Della Vecchia¹, F. Nicolosi¹, S. Corcione¹, V. Trifari¹, G. Cerino, Leonardo Aircraft Division, Italy; M. Fioriti², C. Cabailero², T. Lefebvre, ONERA/DTIS, Université de Toulouse, France; ¹University of Naples Federico II, Italy ;²Politecnico di Torino, Italy | ||||
| 11:30 | 12:00 | 2.1.3 |
COAST - A SIMULATION AND CONTROL FRAMEWORK TO SUPPORT MULTIDISCIPLINARY OPTIMIZATION AND AIRCRAFT DESIGN WITH CPACS D. Kiehn¹, J. Autenrieb¹, N. Fezans¹; ¹German Aerospace Center (DLR), Germany | ||||
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| 10:30 | 11:00 | 3.1.1 |
HIGH-SPEED COMPOUND HELICOPTER RESEARCH AT JAXA M. Sugiura¹, Y. Tanabe¹, N. Kobiki¹, H. Sugawara¹, K. Kimura¹; ¹JAXA, Japan | ||||
| 11:00 | 11:30 | 3.1.2 |
DESIGN OF A FLYING V SUBSONIC TRANSPORT J. Benad¹, R. Vos¹; ¹Delft University of Technology, Netherlands | ||||
| 11:30 | 12:00 | 3.1.3 |
DESIGN AND WIND TUNNEL TESTING OF A GENERAL AVIATION BLENDED WING BODY AIRCRAFT F. Staub¹, T. Tsuchiya¹; ¹The University of Tokyo, Japan | ||||
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| 10:30 | 11:00 | 4.1.1 |
UNSTEADY TURBULENT FLOW SIMULATION OF ROTOR BLADES ON MOVING CARTESIAN GRIDS USING RECURSIVE FITTING APPROACH K. Sugaya¹, T. Imamura¹; ¹The University of Tokyo, Japan | ||||
| 11:00 | 11:30 | 4.1.2 |
COMPUTATIONAL ANALYSIS OF SUPERSONIC FLOW AROUND A WEDGE AND A CYLINDER USING BUILDING-CUBE METHOD K. Abe¹, S. Miyazaki¹, D. Sasaki¹, S. Takahashi², G. Yamada²; ¹Kanazawa Institute of Technology, Japan ;²Tokai University, Japan | ||||
| 11:30 | 12:00 | 4.1.3 |
ON THE INFLUENCE OF GRADIENT RECONSTRUCTION PROCEDURES OVER THE ACCURACY OF FINITE VOLUME BASED SCHEMES F.B. Oliveira, Instituto Tecnológico de Aeronáutica, Brazil; J.L.F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil | ||||
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| 10:30 | 11:00 | 5.1.1 |
GARTEUR: NEARLY HALF A CENTURY OF EUROPEAN COLLABORATION IN AERONAUTICS P. Renzoni, Centro Italiano Ricerche Aerospaziali, Italy | ||||
| 11:00 | 11:30 | 5.1.2 |
THE GROUP OF RESPONSABLES "AERODYNAMICS (GOR AD)" AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES G. Mingione, CIRA, Italy; P. Coustols, ONERA, France; F. Monge, INTA, Spain; H. van der Ven, NLR, Netherlands; K. Richter, DLR, Germany; M. Tormalm, FOI, Sweden; L.R. Calavera¹, B. Stefes¹, D. Pagan, MBDA, France; P. Eliasson, SAAB, Sweden; M. Mallet, DASSAULT, France; R. Gemma, LEONARDO, Italy; ¹AIRUBS, Spain | ||||
| 11:30 | 12:00 | 5.1.3 |
THE GROUP OF RESPONSABLES "STRUCTURES AND MATERIALS (GOR SM)": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES H.G.S.J. Thuis, NLR, Netherlands | ||||
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| 10:30 | 11:00 | 6.1.1 |
EXPERIMENTAL INVESTIGATION OF THE EFFECT OF THE YAW ANGLE ON THE DRAG REDUCTION RATE FOR TRAPEZOIDAL RIBLETS A. Inasawa¹, R. Taniguchi¹, M. Asai¹, M. Sasamori², M. Kurita²; ¹Tokyo Metropolitan University, Japan ;²JAXA, Japan | ||||
| 11:00 | 11:30 | 6.1.2 |
STABILTY AND TRANSITION OF A LAMINAR SEPARATION BUBBLE SUBJECTED TO FREESTREAM TURBULENCE T. Jaroslawski¹, O. Vermeersch¹, J.-M. Moschetta², M. Forte¹, E. Gowree²; ¹ONERA, France ;²ISAE-SUPAERO, France | ||||
| 11:30 | 12:00 | 6.1.3 |
UNIFORM MOMENTUM ZONES IN A TURBULENT BOUNDARY LAYER OVER PERFORATED WALLS F. Scarano¹, M.C. Jacob, Université de Lyon, France; X. Carbonneau¹, E.R. Gowree¹; ¹ISAE - SUPAERO, France | ||||
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| 10:30 | 11:00 | 7.1.1 |
METHODOLOGIES AND EXAMPLE OF CONCEPTUAL DESIGN FOR A FOOT-LAUNCHABLE SPORT SAILPLANE L.M.F. Barbosa, Heart Aerospace, Sweden | ||||
| 11:00 | 11:30 | 7.1.2 |
AIRFOIL DESIGN BY MULTI-ADDITIONAL SAMPLING MULTI-FIDELITY EFFICIENT GLOBAL OPTIMIZATION K. Khankwa¹, T. Phiboon¹, A. Ariyarit¹, R. Kasemsri¹, M. Kanazaki, Tokyo Metropolitan University, Japan; ¹Suranaree University of Technology, Thailand | ||||
| 11:30 | 12:00 | 7.1.3 |
STRUCTURAL DESIGN AND FLUTTER ANALYSIS OF SWEPT BAFFLED INFLATABLE WING N. Ma¹, F.-M. Meng¹, J.-H. Meng¹, L. Liu¹; ¹Beijing Institute of Technology, China | ||||
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| 10:30 | 11:00 | 8.1.1 |
A REDUCED ORDER MODEL FOR FULL-SCALE DRONE COLLISIONS F. Franke¹, U. Burger¹, C. Hühne, German Aerospace Center, Germany; ¹Technische Hochschule Ingolstadt, Germany | ||||
| 11:00 | 11:30 | 8.1.2 |
HIGH FIDELITY AIRWORTHINESS BIRD AND DRONE STRIKE ANALYSIS OF ON-DEMAND AIR MOBILITY SERVICE AIRCRAFT P. Vaghela¹, H. Raza¹, E. Stumpf, Institute for Aerospace Systems, RWTH Aachen University, Germany; J. Bayandor¹; ¹CRASH Lab, University at Buffalo - The State Univ. of New York, United States | ||||
| 11:30 | 12:00 | 8.1.3 |
XRF1 HIGH LIFT LOAD ANALYSIS OF WING AND HIGH LIFT SYSTEM S. Pülm¹, V. Handojo¹, R.B. Seidler¹; ¹German Aerospace Center (DLR) e.V., Germany | ||||
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| 10:30 | 11:00 | 9.1.1 |
SERIES-HYBRID RETROFIT OF AN XV-15 TILTROTOR AND EMERGENCY PROCEDURE ENERGETIC ANALYSIS G. Avanzini, University of Salento, Italy; G. Bernardini¹, S. Moretti¹, J. Serafini¹; ¹Roma Tre University, Italy | ||||
| 11:00 | 11:30 | 9.1.2 |
DEVELOPMENT OF A CONTROLS APPROACH FOR FUEL CELL-POWERED ALL-ELECTRIC AERO ENGINES BASED ON AN FHA S. de Graaf¹, S. Kazula¹; ¹DLR e.V., Germany | ||||
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| 10:30 | 11:00 | 10.1.1 |
USING ACTIVE FLOW CONTROL TO IMPROVE THE AERODYNAMIC PERFORMANCE OF THE NEXT GENERATION CIVIL TILT ROTOR AIRCRAFT J.B. Vos¹, A. Gehri¹, H. Truong², A. Marouf², Y. Hoarau²; ¹CFS Engineering, Switzerland ;²University of Strasbourg, ICUBE Research Institute, France | ||||
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| 10:30 | 11:00 | 11.1.1 |
A SEMANTIC KNOWLEDGE BASED ENGINEERING FRAMEWORK FOR THE RAPID GENERATION OF NOVEL AIR VEHICLE CONFIGURATIONS J. Zamboni¹, A. Zamfir¹, E. Moerland¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany | ||||
| 11:00 | 11:30 | 11.1.2 |
RULE-BASED VERIFICATION OF A GEOMETRIC DESIGN USING THE CODEX FRAMEWORK B. Boden¹, Y. Cabac¹, T. Burschyk¹, B. Nagel¹; ¹DLR, Germany | ||||
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| 10:30 | 11:00 | 12.1.1 |
REAL-TIME CALCULATION AND ADAPTION OF CONFLICT-FREE AIRCRAFT GROUND TRAJECTORIES L. Nöhren¹, M. Schaper¹, L. Tyburzy¹, K. Muth¹; ¹German Aerospace Center (DLR), Germany | ||||
| 11:00 | 11:30 | 12.1.2 |
DEVELOPING A DEPARTURE QUEUE MODEL FOR INTEGRATED ARRIVAL AND DEPARTURE OPERATION OF RUNWAYS E. Itoh, The University of Tokyo/ENRI, Japan; D. Iwata, The University of Tokyo, Japan; M. Schultz, Bundeswehr University Munich, Germany | ||||
| 11:30 | 12:00 | 12.1.3 |
ASSESSMENT AND CONTROL OF ARRIVAL FLOW AND WAITING TIME APPLYING GT/GI/ST+GI TIME-VARYING QUEUING MODEL K. Higasa, The University of Tokyo, Japan; E. Itoh, Electronic Navigation Research Institute, Japan | ||||
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| 10:30 | 11:00 | 13.1.1 |
LONG TOUCHDOWN THROUGH A SAFETY-II PERSPECTIVE C. Reiser, Embraer, Brazil; E. Villani¹, M. Machado Cardoso Junior¹; ¹ITA, Brazil | ||||
| 11:00 | 11:30 | 13.1.2 |
DECISION LADDER APPLICATION ANALYZING A HELICOPTER EMERGENCY B.R. Teixeira¹, L.G.L. de Paula¹, A.C.S. Freitas¹, R.G. Cortes², M.Y.D. Ribeiro², M.M.C. Júnior², E. Vilani²; ¹Brazilian Air Force Flight Test and Research Institute, Brazil ;²Instituto Tecnológico de Aeronáutica , Brazil | ||||
| 11:30 | 12:00 | 13.1.3 |
SYSTEM SAFETY-BASED SUSTAINABLE AVIATION FUEL SAFETY ASSESSMENT METHOD AND AIRWORTHINESS CERTIFICATION S. Ding, Civil Aviation University of China, China; C. Gan¹, T. Qiu¹, P. Liu¹, Q. Ma¹; ¹Beihang University, China | ||||
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| 10:30 | 11:00 | 14.1.1 |
OPERATIONAL FEASIBILITY STUDY OF AIR TAXI SERVICE USING EVTOL H. Takizawa¹, Z. Lei¹; ¹Suwa University of Science, Japan | ||||
| 11:00 | 11:30 | 14.1.2 |
NEW GENERATION SPACE VEHICLE OPERATIONS IN THE UNITED ARAB EMIRATES – AN AIRSPACE AND RISK ASSESSMENT O. Lehmann¹, R. El-Jabi¹, K. Webster¹, A. Rachdi¹; ¹Abu Dhabi University, United Arab Emirates | ||||
| 11:30 | 12:00 | 14.1.3 |
EQUIVALENT CALCULATION METHOD OF FLYOVER NOISE LEVEL OF CUTBACK TAKE-OFF FOR CIVIL JET AIRPLANE AIRWORTHINESS CERTIFICATION Y.-H. Song¹, X.-L. Zhang¹, Q.-H. Liu, Northwestern Polytechnical University, China; Y.-L. Thang¹; ¹Chinese Flight Test Establishment, China | ||||
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| 14:10 | 14:40 | 1.2.1 |
A ROADMAP TOWARDS ENVIRONMENTALLY SUSTAINABLE AVIATION B. Loxton, United States | ||||
| 14:40 | 15:10 | 1.2.2 |
HYBRID ELECTRIC PROPULSION DEVELOPMENT FOR COMMERCIAL AVIATION C. Andrews¹, A. Simpson¹; ¹GE, United States | ||||
| 15:10 | 15:40 | 1.2.3 |
TOWARD A COMMUNITY NOISE ASSESSMENT OF SINGLE-AISLE AIRCRAFT WITH HYBRID-ELECTRIC PROPULSION M.R. Khorrami, United States | ||||
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| 14:10 | 14:40 | 2.2.1 |
DESIGN OF AN ADVANCED EMPENNAGE AND REAR FUSELAGE CONCEPT FOR A COMMERCIAL AIRCRAFT R.C. Llamas-Sandin¹, C.D. Handal-Rivera¹; ¹Airbus OSL, Spain | ||||
| 14:40 | 15:10 | 2.2.2 |
SYSTEMS ARCHITECTING: A PRACTICAL EXAMPLE OF DESIGN SPACE MODELING AND SAFETY-BASED FILTERING WITHIN THE AGILE 4.0 PROJECT A.K. Jeyaraj¹, J.H. Bussemaker², S. Liscouët-Hanke¹, L. Boggero²; ¹Concordia University, Canada ;²DLR, Germany | ||||
| 15:10 | 15:40 | 2.2.3 |
AN EFFICIENT SOLUTION FOR AERODYNAMIC SHAPE OPTIMIZATION WITHIN THE MID-RANGE APPROXIMATION FRAMEWORK Y. Zhang¹, F. Qu¹, J.Q. Bai¹, D.S. Jia², E.K. Bontoft², V.V. Toropov²; ¹Northwestern Polytechnical University, China ;²Queen Mary University of London, United Kingdom | ||||
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| 14:10 | 14:40 | 3.2.1 |
UNMANNED AERIAL VEHICLE – HUMAN PERFORMANCE EVALUTION UNDER CRITICAL OPERATIONAL SCENARIO E.T. da Silva¹, A.G.P. Sarmento¹, T.R. de Paula¹, A.S. Oliveira¹, J. Possamai¹, H.C. Marques¹, M.M. Cardoso¹, E. Villani¹; ¹Aeronautics Institute of Technology, Brazil | ||||
| 14:40 | 15:10 | 3.2.2 |
RESEARCH ON THE OVERALL DESIGN OF A HIGH-SPEED MORPHING UAV C. Ding, School of Aeronautic Science and Engineering,Beihang University, China; T.-L. Ma, Institute of Unmanned System, Beihang University, China; J.-C. Fu, School of Transportation ScienceandEngineering,BeihangUniversity, China; X.-S. Wang, School of Aeronautic Science and Engineering, Beihang University, China | ||||
| 15:10 | 15:40 | 3.2.3 |
COOPERATIVE THREAT ENGAGEMENT WITH HETEROGENEOUS DRONE SWARMS L. Giacomossi¹, J.A. Ricardo Jr¹, J.F.B. Brancalion, EMBRAER, Brazil; M.R.O.A. Maximo¹, D.A. Santos¹; ¹ITA, Brazil | ||||
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| 14:10 | 14:40 | 4.2.1 |
VALIDATION STUDY OF BLUNTED AND SHARP CONES AT HYPERSONIC SPEED E.K.T. Carias¹, S.A. Prince¹; ¹Cranfield University, United Kingdom | ||||
| 14:40 | 15:10 | 4.2.2 |
AERODATABASE DEVELOPMENT AND INTEGRATION OF SUPERSONIC/HYPERSONIC CRUISER VEHICLES IN MORE&LESS PROJECT P. Roncioni¹, M. Marini¹, R. Fusaro², N. Viola²; ¹CIRA, Italy ;²POLITO, Italy | ||||
| 15:10 | 15:40 | 4.2.3 |
TURBULENCE MODELLING STUDIES OF SHOCK-WAVE/BOUNDARY-LAYER INTERACTIONS ON HIFIRE-1 AXISYMMETRIC CONE CYLINDER FLARE IN HYPERSONIC FLOWS R.O. Bura, Republic of Indonesia Defense University, Indonesia; F.A. Maulana, Indonesia | ||||
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| 14:10 | 14:40 | 5.2.1 |
THE GROUP OF RESPONSABLES "FLIGHT MECHANICS, SYSTEMS AND INTEGRATION (GOR FM)": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES B. Korn, DLR, Germany; M. Hagström, FOI, Sweden | ||||
| 14:40 | 15:10 | 5.2.2 |
THE GROUP OF RESPONSABLES "ROTORCRAFT (RC-GOR)": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES A. Visingardi, CIRA, Italy; R. Heger, Airbus Helicopters, Germany; A. Le Pape, ONERA, France; R. Markiewicz, DSTL, United Kingdom; B. Ohlenforst, NLR, Netherlands; K. Pahlke, DLR, Germany; M. White, University of Liverpool, United Kingdom | ||||
| 15:10 | 15:40 | 5.2.3 |
AVIATION SECURITY CONCERNS A. Vozella, Italian Aerospace Research Centre, Italy; P. Bieber, ONERA, France | ||||
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| 14:10 | 14:40 | 6.2.1 |
STRAKE SECTION IMPACT ON HYBRID-DELTA-WING AERODYNAMICS D. Sedlacek¹, C. Breitamter¹; ¹Technical University of Munich, Germany | ||||
| 14:40 | 15:10 | 6.2.2 |
VOLUMETRIC VELOCITY MEASUREMENTS OF A HELICAL VORTEX PAIR D. Schröder¹, T. Leweke, CNRS, Aix-Marseille Université, Centrale Marseille, France; R. Hörnschemeyer¹, E. Stumpf¹; ¹Institute of Aerospace Systems, RWTH Aachen University, Germany | ||||
| 15:10 | 15:40 | 6.2.3 |
NUMERICAL AND EXPERIMENTAL INVESTIGATIONS ON THE DLR-F23 COMBAT AIRCRAFT WIND TUNNEL MODEL J. Zastrow¹, F. Oberdieck¹, U. Henne¹, C. Klein¹; ¹DLR - German Aerospace Center, Germany | ||||
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| 14:10 | 14:40 | 7.2.1 |
APPLICATION OF THE VIRTUAL CRACK CLOSURE TECHNIQUE FOR CRACKS IN BUILT-UP PANELS W.R.P. Mendonca¹, M.R.B. Rodrigues¹; ¹Embraer S.A., Brazil | ||||
| 14:40 | 15:10 | 7.2.2 |
NUMERICAL AND EXPERIMENTAL STRUCTURAL CHARACTERIZATION OF COMPOSITE ADVANCED JOINT FOR ULTRA LIGHT AEROSPACE PLATFORMS A. Polla, Politecnico di Torino; Royal Melbourne Institute of Technology, Italy; G. Frulla¹, E. Cestino¹, R. Das², P. Marzocca²; ¹Politecnico di Torino, Italy ;²Royal Melbourne Institute of Technology, Australia | ||||
| 15:10 | 15:40 | 7.2.3 |
A DAMAGE RECOGNITION METHOD OF COMPOSITE STRUCTURES USING ARTIFICIAL DEFECTIONS Y. Yang¹, S. Lyu¹; ¹Aircraft Strength Research Institute, China | ||||
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| 14:10 | 14:40 | 8.2.1 |
WIND TUNNEL EXPERIMENT WITH AN EPP-WING TO INVESTIGATE AEROELASTIC EFFECTS OF NONLINEAR ELASTIC STIFFNESSES K. Bramsiepe¹, M. Braune¹, W. Krüger¹, L. Tichy¹; ¹DLR - Institute of Aeroelasticity, Germany | ||||
| 14:40 | 15:10 | 8.2.2 |
DESIGN OF AN INNOVATIVE WING TIP FOR AEROELASTIC CONTROL: FROM SCRATCH TO FLIGHT TEST F. Toffol¹, F. Fonte, Leonardo Helicopters, Italy; S. Ricci¹; ¹Politecnico di Milano, Italy | ||||
| 15:10 | 15:40 | 8.2.3 |
EVALUATION ENVIRONMENT FOR CASCADED AND PARTLY DECENTRALIZED MULTI-RATE LOAD ALLEVIATION CONTROLLERS C. Wallace¹, S. Schulz¹, N. Fezans¹, T. Kier¹, G. Weber, Liebherr-Aerospace, Germany; ¹German Aerospace Center (DLR), Germany | ||||
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| 14:10 | 14:40 | 9.2.1 |
ASSESSMENT OF A SERIAL COOLING CONCEPT FOR HTPEM FUEL CELL SYSTEMS FOR AVIATION APPLICATIONS A. Link¹, J. Ludowicy¹, M. Staggat¹; ¹German Aerospace Center (DLR), Germany | ||||
| 14:40 | 15:10 | 9.2.2 |
DEMONSTRATION FLIGHTS OF HYBRID ELECTRIC AIRCRAFT P. Bohnert, United Kingdom; S.X. Ying, United States; M. Selier, Netherlands | ||||
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| 14:10 | 14:40 | 10.2.1 |
TRANSONIC NACELLE DESIGN FOR FUTURE MEDIUM RANGE AERO-ENGINES B.D.J. Schreiner¹, D.G. MacManus¹, F. Tejero¹, F. Sanchez-Moreno¹, C. Sheaf, Rolls Royce, United Kingdom; ¹Cranfield University, United Kingdom | ||||
| 14:40 | 15:10 | 10.2.2 |
STUDY OF EFFECTS ON THE WING'S AERODYNAMIC CHARACTERISTICS DUE TO DISTRIBUTED PROPULSION OVER WINGSPAN G.J. Resende¹, V. Malatesta¹, M.C. Savio², B.M. Castro²; ¹ITA - Aeronautics Institute of Technology, Brazil ;²EMBRAER, Brazil | ||||
| 15:10 | 15:40 | 10.2.3 |
A NOVEL EMBEDDED INLET BASED ON THE INTEGRATED DESIGN CONCEPT OF FUSELAGE AND INLET P. Yan, Shenyang Aircraft Design and Research Institute, China; F. Liu, Shenyang Aircraft Design and Research Institute, Chinese Aeronau, China | ||||
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| 14:10 | 14:40 | 11.2.1 |
LANDING SIMULATION OF A HIGH-ALTITUDE PLATFORM WITH SKID-TYPE LANDING GEAR – FLIGHT PROCEDURE, CONTROLLER, AND LOADS Y.J. Hasan¹, N. Fezans¹, A. Voß, DLR, Institute of Aeroelasticity, Germany; ¹DLR, Institute of Flight Systems, Germany | ||||
| 14:40 | 15:10 | 11.2.2 |
ALTITUDE ESTIMATION BY WIDE-FIELD-INTEGRATION OF OPTIC FLOW H. Hiraiwa¹, M. Bando¹, S. Hokamoto¹; ¹Kyushu university, Japan | ||||
| 15:10 | 15:40 | 11.2.3 |
FIXED-WING UAVS CONTROL WITH MODEL UNCERTAINTIES M.R. Kartal¹, D. Ignatyev¹, A. Zolotas¹; ¹Cranfield University, United Kingdom | ||||
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| 14:10 | 14:40 | 12.2.1 |
MACHINE LEARNING METHODS ENSURING BOTH PERFORMANCE AND INTERPRETABILITY OF ESTIMATING AIRCRAFT ARRIVAL TIMES N. Morikawa, Faculty of Aerospace Engineering, The University of Tokyo, Japan; E. Itoh, Air Traffic Management Department, Electronic Navigation Researc, Japan | ||||
| 14:40 | 15:10 | 12.2.2 |
APPLYING MACHINE LEARNING TO TAXI-TIME PREDICTION ATTOKYO INTERNATIONAL AIRPORT F. Kato¹, E. Itoh¹; ¹The University of Tokyo, Japan | ||||
| 15:10 | 15:40 | 12.2.3 |
AN AUCTION-BASED MECHANISM FOR A PRIVACY-PRESERVING MARKETPLACE FOR ATFM SLOTS C.G. Schuetz, Johannes Kepler University Linz, Austria; S. Ruiz, EUROCONTROL Innovation Hub, France; E. Gringinger¹, C. Fabianek¹, T. Loruenser, AIT Austrian Institute of Technology, Austria; ¹Frequentis AG, Austria | ||||
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| 14:10 | 14:40 | 13.2.1 |
LOCALIZATION OF INTERROGATORS WITH A 1030/1090 MHZ SPECTRUM MONITORING SYSTEM L. Sarperi¹, M. Jäger¹, P. Müller¹, M. Felux¹; ¹ZHAW, Switzerland | ||||
| 14:40 | 15:10 | 13.2.2 |
A FEDERATED LEARNING BASED SECURITY FOR CONTROLLER-PILOT DATA LINK COMMUNICATION S. Khan¹, G. Singh Gaba¹, A. Gurtov¹; ¹Linköping University, Sweden | ||||
| 15:10 | 15:40 | 13.2.3 |
TECHNICAL CONCEPTS FOR INSPECTING UAVS FOR DAMAGE J. Eltgen¹, T. Schüppstuhl¹; ¹Hamburg University of Technology, Germany | ||||
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| 14:10 | 14:40 | 14.2.1 |
DATA-DRIVEN APPROACH TO OPTIMAL AIRCRAFT MAINTENANCE O.C. Okoro¹, M. Zaliskyi¹, D. Serhii , National Aviation University , Ukraine; S. Qudus, Tamara Niger Aviation, Niger; ¹National Aviation University, Ukraine | ||||
| 14:40 | 15:10 | 14.2.2 |
OPERABILITY PROJECTION OF MAJOR AIRCRAFT COMPONENTS DURING EARLY AIRCRAFT DESIGN S.S. Manikar, Airbus/ ISAE-SUPAERO, France; J. Jezegou¹, P. de Saqui-Sannes¹, P. Asseman, Airbus, France; E. Benard¹; ¹ISAE-SUPAERO, France | ||||
| 15:10 | 15:40 | 14.2.3 |
DIGITAL TWIN CONCEPT FOR AIRCRAFT COMPONENTS H. Meyer¹, A.-K. Koschlik¹, F. Raddatz¹; ¹German Aerospace Center, Germany | ||||
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| 16:00 | 16:30 | 1.3.1 |
THE SWEDISH AIR FORCE INTO THE FUTURE – AIMING FOR A HIGHER GROUND AND A SHARPER EDGE T. Petersson, Sweden | ||||
| 16:30 | 17:00 | 1.3.2 |
FUTURE COMBAT AIRCRAFT SYSTEM THE COMPLEXITY OF THE SKILLS EQUATION S. Hopkins, BAE Systems, United Kingdom; I. Noakes, BAe Systems, United Kingdom | ||||
| 17:00 | 17:30 | 1.3.3 |
FUTURE COMBAT AIR SYSTEMS: REQUIREMENTS AND TECHNOLOGIES G. Girard, France | ||||
| 17:30 | 18:00 | 1.3.4 |
POWER/THERMAL 2030 VISION - AIR PLATFORM ELECTRIFICATION J.G. Nairus, United States | ||||
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| 16:00 | 16:30 | 2.3.1 |
VALIDATION OF SCALED FLIGHT TESTING P. Schmollgruber¹, C. Toussaint¹, A. Lepage¹, F. Bremmers², H. Jentink², L. Timmermans², N. Genito³, A. Rispoli³, D. Meissner, 5Airbus Operations GmbH, Germany; D. Kierbel, Airbus S.A.S., France; ¹ONERA, France ;²NLR, Netherlands ;³CIRA, Italy | ||||
| 16:30 | 17:00 | 2.3.2 |
TECHNOLOGY INTEGRATION FOR FUTURE AIRCRAFT CONFIGURATIONS D. Reckzeh, Airbus, Germany | ||||
| 17:00 | 17:30 | 2.3.3 |
MARKET ANALYSIS, TLARS SELECTION AND PRELIMINARY DESIGN INVESTIGATIONS FOR A REGIONAL HYBRID-ELECTRIC AIRCRAFT V. Marciello¹, M. Ruocco, SmartUp Engineering s.r.l., Italy; F. Nicolosi¹, M. Di Stasio¹; ¹University of Naples Federico II, Italy | ||||
| 17:30 | 18:00 | 2.3.4 |
UNMANNED AEW/ISR PLATFORM CONCEPTUAL DESIGN AND TECHNOLOGY ASSESSMENT C. Jouannet¹, K. Amadori¹, M. Emeneth, PACE America Inc., United States; A. Papageorgiou, Linköpings University, Sweden; ¹Saab Aeronautics, Sweden | ||||
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| 16:00 | 16:30 | 3.3.1 |
A COMMON FRAMEWORK FOR THE DESIGN OPTIMIZATION OF FIXED-WING, MULTICOPTER AND VTOL UAV CONFIGURATIONS F. Pollet¹, S. Delbecq¹, M. Budinger, ICA, Université de Toulouse, ISAE-SUPAERO, MINES ALBI, UPS, INSA, France; J.-M. Moschetta¹, J. Liscouët, Concordia University, Canada; ¹ISAE-SUPAERO, France | ||||
| 16:30 | 17:00 | 3.3.2 |
DESIGN OF A HALE UAV FOR ATMOSPHERIC IMAGING V. Nan Fernandez-Ayala¹, L. Vimláti¹, A. Matoses Gimenez¹, H. Delmotte¹, M. Ivchenko¹, R. Mariani¹; ¹KTH Royal Institute of Technology, Sweden | ||||
| 17:00 | 17:30 | 3.3.3 |
ENHANCING UAS DESIGN PROCESS FOR SPECIFIC CATEGORY OPERATIONS USING SORA R. Kalra¹, P. Flores-Peña, Drone Hopper S.L., Spain; A. Sanchez-Carmona¹, C. Cuerno-Rejado¹; ¹Universidad Politécnica de Madrid, Spain | ||||
| 17:30 | 18:00 | 3.3.4 |
OPENVSP BASED AERODYNAMIC DESIGN OPTIMIZATION TOOL BUILDING METHOD AND ITS APPLICATION TO TAILLESS UAV J. Kim¹, T. Tsuchiya¹; ¹The University of Tokyo, Japan | ||||
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| 16:00 | 16:30 | 4.3.1 |
A MULTIFIDELITY MULTIDISCIPLINARY APPROACH TO UNCONVENTIONAL AIRCRAFT DEVELOPMENT AND ASSESSMENT WITH APPLICATION TO THE STRUT-BRACED-WING AND HYBRID-WING-BODY CONFIGURATIONS D.W. Zingg¹, T. Chau¹, A.L. Gray¹, T.A. Reist¹; ¹University of Toronto Institute for Aerospace Studies, Canada | ||||
| 16:30 | 17:00 | 4.3.2 |
OVERVIEW OF AERODYNAMIC DESIGN ACTIVITIES PERFORMED AT ONERA TO REDUCE AVIATION'S CLIMATE IMPACT M. Méheut¹, G. Arnoult¹, O. Atinault¹, Q. Bennehard¹, C. Francois¹; ¹ONERA, France | ||||
| 17:00 | 17:30 | 4.3.3 |
MDAO OF A TRANSONIC TRUSS-BRACED WING VISION VEHICLE D.S. Lazzara¹, N.A. Harrison¹; ¹Boeing, United States | ||||
| 17:30 | 18:00 | 4.3.4 |
APPLICATION OF AERODYNAMIC AND AERO-STRUCTURAL OPTIMIZATION FOR ENERGY EFFICIENT AIRCRAFT O. Brodersen, Germany; T. Wunderlich, Germany; M. Abu-Zurayk, Germany; S. Görtz, Germany; C. Ilic, Germany; L. Reimer, Germany | ||||
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| 16:00 | 16:30 | 5.3.1 |
MODEL-BASED PERFORMANCE EVALUATION OF AIRCRAFT ACTUATOR TECHNOLOGIES F. Larsson¹, C. Reichenwallner², A. Dell'Amico¹, P. Krus²; ¹Saab AB, Sweden ;²Linköping University, Sweden | ||||
| 16:30 | 17:00 | 5.3.2 |
A COMPARATIVE ANALYSIS OF INNOVATIVE DIGITAL HYDRAULIC ACTUATORS FOR PRIMARY FLIGHT CONTROL R. Simões Lopes Junior¹, D. Oliveira e Silva¹, M.P. Nostrani¹, A. Dell´Amico, Saab AB, Sweden; P. Krus, Linköping University, Sweden; V.J. De Negri¹; ¹Federal University of Santa Catarina, Brazil | ||||
| 17:00 | 17:30 | 5.3.3 |
AN EVALUATION METHOD FOR AIRCRAFT ACTUATION SYSTEMS OPERATIONAL COST C. Reichenwallner, Linköping university, Sweden; F. Larsson¹, A. Dell'Amico¹; ¹Saab AB, Sweden | ||||
| 17:30 | 18:00 | 5.3.4 |
DEVELOPMENT OF A HIGH EFFICIENT HYDRAULIC POWER PACK L.Z. Lima¹, M.N. Duval¹, T. Zantner¹, D. Metzler¹, T. Lammering¹, F. Thielecke², N. Trochelmann², P.S. Bischof²; ¹Liebherr-Aerospace Lindenberg GmbH, Germany ;²Hamburg University of Technology, Germany | ||||
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| 16:00 | 16:30 | 6.3.1 |
AERODYNAMIC AND AEROACOUSTIC CHARACTERISTICS OF THE NACA 0008 AIRFOIL F.L. dos Santos¹, L. Botero-Bolivar¹, C.H. Venner¹, L.D. de Santana¹; ¹University of Twente, Netherlands | ||||
| 16:30 | 17:00 | 6.3.2 |
EXPERIMENTAL STUDIES ON THE INTERACTION BETWEEN PROPELLERS AND WING G.P.G. Silva¹, M.V.R.J. Silva¹, J.P. Eguea¹, F.M. Catalano¹; ¹Department of Aeronautical Engineering, University of Sao Paulo, Brazil | ||||
| 17:00 | 17:30 | 6.3.3 |
IDENTIFICATION OF CRITICAL ACOUSTIC MODES FOR AN OPEN BOX CAVITY WITH ADJUSTABLE DEPTH S. Hammer¹, J. Fridh¹, M. Billson, GKN Aerospace Sweden, Sweden; ¹KTH Royal Institute of Technology, Sweden | ||||
| 17:30 | 18:00 | 6.3.4 |
AN OVERVIEW OF AERO-ACOUSTIC EXPERIMENTAL TECHNOLOGY IN AVIC FL-10 WIND TUNNEL Z. Guocheng¹, B. Anyu ¹, C. Bao¹, L. Xiangnan¹; ¹AVIC ARI, China | ||||
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| 16:00 | 16:30 | 7.3.1 |
TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES AEROSTRUCTURES I. Rivero¹, A. Palomar¹, N. Martin¹, M. Lozano¹, J. Romero¹, B. De Nicolas¹, M. Rebollo¹, J. Gomez-Escalonilla¹; ¹Airbus, Spain | ||||
| 16:30 | 17:00 | 7.3.2 |
VARIATIONS IN STRUCTURAL PROPERTIES OF LATTICE STRUCTURES DEPENDING ON UNIT CELL SHAPE FOR MORPHING WINGS Y. Nishijima¹, H. Tanaka¹, A. Biron, Special Military School of Saint-Cyr, France; T. Miura¹; ¹National Defense Academy, Japan | ||||
| 17:00 | 17:30 | 7.3.3 |
PROPOSITION OF A NEW QUALIFICATION IMPACT TEST FOR AEROSPACE SMART STRUCTURES G. Gastaldo, France; Y. Rafik, France; M. Budinger, France; V. Pommier-Budinger, France; P. Olivier, France; P. Navarro, France | ||||
| 17:30 | 18:00 | 7.3.4 |
PERIDYNAMIC SIMULATION PLATTFORM TO DETERMINE VIRTUAL ALLOWABLES OF MANUFACTURING DEVIATIONS C. Willberg¹, J.-T. Hesse¹, D. Krause¹; ¹German Aerospace Center, Germany | ||||
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| 16:00 | 16:30 | 8.3.1 |
AEROELASTIC ANALYSIS OF HIGH ASPECT RATIO AND STRUT-BRACED WINGS Y. Le Lamer¹, J. Morlier, ICA, Université de Toulouse, ISAE-SUPAERO, MINES ALBI, UPS, INSA, France; E. Benard¹, P. He, Iowa State University, United States; ¹ISAE-SUPAERO, Université de Toulouse, France | ||||
| 16:30 | 17:00 | 8.3.2 |
COMPARING REDUCED ORDER MODEL FORMS FOR NONLINEAR DYNAMICAL SYSTEMS D. Massegur¹, D. Clifford¹, A. Da Ronch¹, S. Symon¹; ¹University of Southampton, United Kingdom | ||||
| 17:00 | 17:30 | 8.3.3 |
NUMERICAL INVESTIGATION ON THE DOUBLE TRANSONIC DIP OF SUPERCRITICAL AIRFOIL FLUTTER T. Miyake¹, H. Terashima¹; ¹Hokkaido University, Japan | ||||
| 17:30 | 18:00 | 8.3.4 |
ANALYSIS OF THE HAMMERHEAD LAUNCH VEHICLE USING CFD-CAE COUPLED METHOD IN THE TRANSONIC REGION H.-G. Rho, Korea Aerospace Univeristy, South Korea; P.A. Nguyen¹, J.-S. Bae¹, S.-H. Park, Konkuk University, South Korea; K.-H. Byun, Korea Agency for Defense Development, South Korea; ¹Korea Aerospace University, Vietnam | ||||
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| 16:00 | 16:30 | 9.3.1 |
COUPLED AEROPROPULSIVE ANALYSIS AND OPTIMIZATION OF A HIGH BYPASS TURBOFAN ENGINE A.H.R. Lamkin¹, A. Yildirim¹, J.R.R.A. Martins¹; ¹University of Michigan, United States | ||||
| 16:30 | 17:00 | 9.3.2 |
A COMPARITIVE ASSESSMENT OF MULTI-OBJECTIVE OPTIMISATION METHODOLOGIES FOR AERO-ENGINE NACELLES A. Swarthout¹, D. MacManus¹, F. Tejero¹, J. Matesanz-Garcia¹, L. Boscagli¹, C. Sheaf, Rolls Royce Plc., United Kingdom; ¹Cranfield University, United Kingdom | ||||
| 17:00 | 17:30 | 9.3.3 |
KNOWLEDGE-BASED CONCEPTUAL DESIGN METHODS FOR GEOMETRY AND MASS ESTIMATION OF RUBBER AERO ENGINES J. Häßy¹, J. Schmeink¹; ¹DLR, Germany | ||||
| 17:30 | 18:00 | 9.3.4 |
MULTIDISCIPLINARY OPTIMIZATION OF COMBUSTION CHAMBER FOR SMALL GAS TURBINE ENGINES C.-A. Pham¹, Q.-H. Nguyen¹, T.-A. Vu¹, N.-V. Nguyen¹; ¹Viettel Aerospace Institute, Viettel Group, Vietnam | ||||
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| 16:00 | 16:30 | 10.3.1 |
FLIGHT DYNAMICS SIMULATION AND FCS AUTO-GENERATION IN THE CONCEPTUAL DESIGN PHASE OF AN UNSTABLE SUPERSONIC AIRCRAFT E. Johansson¹, P. Månsson¹, P. Sjöberg¹; ¹Saab Aeronautics, Sweden | ||||
| 16:30 | 17:00 | 10.3.2 |
VALIDATION OF A HYBRID LOADS OBSERVER FOR A SUBSCALE TEST AIRCRAFT WITH DISTRIBUTED ELECTRIC PROPULSION O. Luderer¹, F. Thielecke¹; ¹Hamburg University of Technology, Germany | ||||
| 17:00 | 17:30 | 10.3.3 |
A BI-LEVEL CO-DESIGN APPROACH FOR MULTICOPTERS J. Mabboux¹, S. Delbecq¹, V. Pommier-Budinger¹, J. Bordeneuve-Guibe¹, A. Truc-Hermel², J.-M. Kai²; ¹ISAE Supaero, France ;²SAFRAN, France | ||||
| 17:30 | 18:00 | 10.3.4 |
DEEP REINFORCEMENT LEARNING FOR EVTOL HOVERING CONTROL D.S. Alarcon¹, J.H. Bidinotto¹; ¹University of São Paulo, Brazil | ||||
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| 16:00 | 16:30 | 11.3.1 |
OPTIMAL HOVERING WING KINEMATICS OF FLAPPING-WING MODEL USING REINFORCEMENT LEARNING H.-H. Yang¹, S.-G. Lee¹, Y.-J. Han¹, J.-H. Han¹; ¹Korea Advanced Institute of Science and Technology, South Korea | ||||
| 16:30 | 17:00 | 11.3.2 |
PREFLIGHT DIAGNOSIS OF MULTICOPTER ACTUATOR FAULT USING SUPERVISED LEARNING WITH DISTURBANCE OBSERVER OUTPUTS T.G. Kim¹, Y.J. Kim¹, S.K. Kim¹; ¹Chungnam National University, South Korea | ||||
| 17:00 | 17:30 | 11.3.3 |
USING DEEP REINFORCEMENT LEARNING TO IMPROVE THE ROBUSTNESS OF UAV LATERAL-DIRECTIONAL CONTROL R. Wang¹, Z. Zhou¹, X. Zhu¹, L. Zheng, Delft University of Technology, Netherlands; ¹Northwestern Polytechnical University, China | ||||
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| 16:00 | 16:30 | 12.3.1 |
IMPROVED CONFIGURATION MANAGEMENT FOR GREENER APPROACHES – EVALUATION OF A NOVEL PILOT SUPPORT CONCEPT T. Bauer¹, F. Abdelmoula¹, J. Boyer, Thales, France; M. Gerber, Swiss Sklylab Foundation, Switzerland; J. Meister², J.M. Wunderli²; ¹DLR e.V., Germany ;²Empa, Swiss Fed. Laboratories for Materials Science & Technology, Switzerland | ||||
| 16:30 | 17:00 | 12.3.2 |
A COMPARISON OF CLIMATE-OPTIMISED AND FUEL-OPTIMISED INTERMEDIATE STOP OPERATIONS FOR SELECTED CASE STUDIES Z. Zengerling¹, F. Linke¹, C. Weder¹, K. Dahlmann¹; ¹Deutsches Zentrum für Luft- und Raumfahrt, Germany | ||||
| 17:00 | 17:30 | 12.3.3 |
IMPLICATIONS OF POTENTIAL NEW REGULATORY MEASURES TO ADDRESS AVIATION EMISSIONS A. Nieto¹, G. Alonso¹, J. Cubas¹; ¹Universidad Politécnica de Madrid, Spain | ||||
| 17:30 | 18:00 | 12.3.4 |
AN ENGINELESS TAXI OPERATIONS SYSTEM USING BATTERY-OPERATED AUTONOMOUS TOW TRUCKS S. Zaninotto¹, J. Gauci¹, B. Zammit¹; ¹University of Malta, Malta | ||||
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| 16:00 | 16:30 | 13.3.1 |
A NOVEL METHOD FOR DETECTING UAVS USING PARALLEL NEURAL NETWORKS WITH RE-INFERENCE H. Stepien, Saab Aeronautics, Sweden; M. Bilger, Saab Surveillance, Sweden; H. Forsberg¹, B. Lindgren, Saab Dynamics, Sweden; J. Hjorth¹; ¹Mälardalen University, Sweden | ||||
| 16:30 | 17:00 | 13.3.2 |
URBAN AIR TRAFFIC MANAGEMENT FOR COLLISION AVOIDANCE WITH NON-COOPERATIVE AIRSPACE USERS I. Panchal¹, I.C. Metz, German Aerospace Center, Germany; M. Ribeiro, TU Delft, Netherlands; S.F. Armanini¹; ¹TU Munich, Germany | ||||
| 17:00 | 17:30 | 13.3.3 |
A HUMAN-MACHINE INTERFACE ANALYSIS FOR TELEOPERATION OF UAV OVERTIME DELAY A.G.P. Sarmento¹, T. Rosado de Paula¹, A.S. Oliveira¹, E.T. da Silva¹, J. Possamai¹, H.C. Marques¹, M.M. Cardoso Junior¹, E. Villani¹; ¹Aeronautics Institute of Technology (ITA), Brazil | ||||
| 17:30 | 18:00 | 13.3.4 |
IMAGE SEGMENTATION BASED EMERGENCY LANDING FOR AUTONOMOUS AND AUTOMATED UNMANNED AERIAL VEHICLES P. Hausmann¹, H. Meeß, Fraunhofer IVI, Germany; G. Elger¹; ¹Technische Hochschule Ingolstadt, Germany | ||||
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| 16:00 | 16:30 | 14.3.1 |
THE ALBATROSS PROJECT – A EUROPEAN INITIATIVE TO REDUCE AVIATION’S CARBON DIOXIDE EMISSIONS IN LARGE SCALE F. Sachs¹, F. Abdelmoula¹, D. Vechtel¹; ¹DLR, Germany | ||||
| 16:30 | 17:00 | 14.3.2 |
ZERO-EMISSION REGIONAL AVIATION IN SWEDEN R.T. Sorrentino¹, R.C. Parello¹, M. Delage¹, C.Y. Justin¹, D.N. Mavris¹, C. Jouannet², K. Amadori²; ¹Georgia Institute of Technology, United States ;²Saab AB/Saab Aeronautics, Sweden | ||||
| 17:00 | 17:30 | 14.3.3 |
PERFORMANCE EVALUATION OF THE ARRIVAL OPERATIONS IN TERMINAL AREA H. Hardell¹, A. Lemetti¹, T. Polishchuk¹; ¹Linköping University, Sweden | ||||
| 17:30 | 18:00 | 14.3.4 |
AERODYNAMIC INVESTIGATION OF VERY CLOSELY FLYING FIGHTERS TO DEVELOP NEW FORMATION TYPES S.M. Aydin¹, A.G. Yavuz, Turkish Aerospace Industries, Turkey; M. Kaya¹; ¹Yildirim Beyazit University, Turkey | ||||
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| 10:30 | 11:00 | 1.4.1 |
CERTIFICATION BY ANALYSIS - SOME THOUGHTS U. Kerlin, Airbus, Germany | ||||
| 11:00 | 11:30 | 1.4.2 |
NEXT STEPS TOWARDS CERTIFICATION BY ANALYSIS - A DIGITAL THREAD PERSPECTIVE O. Pinon Fischer, United States; D. Mavris, United States | ||||
| 11:30 | 12:00 | 1.4.3 |
TOWARDS CERTIFICATION BY ANALYSIS FOR FLIGHT CHARACTERISTICS R. Gregg, Boeing, United States | ||||
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| 10:30 | 11:00 | 2.4.1 |
DEEP LEARNING TECHNIQUES FOR HIGH-DIMENSIONAL SURROGATE-BASED AERODYNAMIC DESIGN M.A. Hariansyah¹, K. Shimoyama¹; ¹Institute of Fluid Science, Tohoku University, Japan | ||||
| 11:00 | 11:30 | 2.4.2 |
SUCCESSIVE KNOWLEDGE BUILDUP AND TRANSFER DURING THE ANALYSIS OF SCALED UAV WINGS BY MEANS OF MACHINE LEARNING T. Klaproth¹, M. Hornung¹; ¹Technical University of Munich, Germany | ||||
| 11:30 | 12:00 | 2.4.3 |
AIRCRAFT DESIGN PARAMETER ESTIMATION USING DATA-DRIVEN MACHINE LEARNING MODELS S. Shin¹, S. Lee¹, C. Son, Cheongju University, South Korea; K. Yee, Seoul National University, South Korea; ¹Korea Institute of Industrial Technology, South Korea | ||||
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| 10:30 | 11:00 | 3.4.1 |
EXPLORATION OF BOX-WING AIRCRAFT CONCEPT USING HIGH-FIDELITY AERODYNAMIC SHAPE OPTIMIZATION P.D. Bravo-Mosquera¹, T. Chau², F.M. Catalano¹, D.W. Zingg²; ¹University of São Paulo, Brazil ;²University of Toronto, Canada | ||||
| 11:00 | 11:30 | 3.4.2 |
CONCEPTUAL STUDY OF HYBRID-ELECTRIC BOX-WING AIRCRAFT TOWARDS THE REDUCTION OF AVIATION EFFECTS ON LOCAL AIR QUALITY AND CLIMATE CHANGE K. Abu Salem¹, V. Cipolla¹, G. Palaia¹, V. Binante², D. Zanetti²; ¹University of Pisa, Italy ;²SkyBox Engineering, Italy | ||||
| 11:30 | 12:00 | 3.4.3 |
MULTIDISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION PROCESS DEDICATED TO BLENDED WING BODY CONFIGURATIONS J. Gauvrit-Ledogar¹, A. Tremolet¹, F. Moens¹, M. Méheut¹, S. Defoort¹, R. Liaboeuf¹, F. Morel¹, B. Paluch¹; ¹ONERA, France | ||||
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| 10:30 | 11:00 | 4.4.1 |
WING BUFFET PRESSURE LOAD PREDICTION BASED ON A HYBRID DEEP LEARNING MODEL R. Zahn¹, A. Weiner, Technical University of Braunschweig, Germany; C. Breitsamter¹; ¹Technical University of Munich (TUM), Germany | ||||
| 11:00 | 11:30 | 4.4.2 |
AN ASSESSMENT OF REDUCED-ORDER AND MACHINE LEARNING MODELS FOR STEADY TRANSONIC FLOW PREDICTION ON WINGS R. Castellanos¹, J. Bowen Varela¹, A. Gorgues¹, E. Andrés¹; ¹INTA, Spain | ||||
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| 10:30 | 11:00 | 5.4.1 |
ASSESSMENT OF THE SUSTAINABILITY OF THE IMPLEMENTATION OF CIRCULAR ECONOMY PRINCIPLES IN PRODUCING AIRCRAFT STRUCTURES D.N. Markatos¹, S.G. Pantelakis¹; ¹University of Patras, Greece | ||||
| 11:00 | 11:30 | 5.4.2 |
INVESTIGATION ON INTEGRATING RECYCLABILITY AS A FUNCTION AT THE DESIGN PHASE OF COMPLEX-LOADED STRUCTURAL COMPONENTS A. Filippatos¹, K. Abhyankar, Institute of Lightweight Engineering and Polymer Technology, Tec, Germany; G. Tzortzinis¹; ¹Dresden Center for Intelligent Materials (DCIM), Technische Univ, Germany | ||||
| 11:30 | 12:00 | 5.4.3 |
SIGMOIDAL SENSING DEVICES FOR MONITORING TO IMPROVE MAINTENANCE OPERATIONS IN AERONAUTICS H. Pfeiffer¹, H. Sekler, Deutsche Lufthansa AG, Germany; M. Wevers¹; ¹KU Leuven, Belgium | ||||
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| 10:30 | 11:00 | 6.4.1 |
ANALYSIS OF THE EFFECT OF FLOW TRANSITION OVER THE WINGS OF THE BLADE DEMONSTRATOR R. Larsson, Saab Aeronautics, Sweden | ||||
| 11:00 | 11:30 | 6.4.2 |
TO CFD OR NOT TO CFD? COMPARING RANS AND VISCOUS PANEL METHODS FOR AIRFOIL SHAPE OPTIMIZATION E.J. Adler¹, A.C. Gray¹, J.R.R.A. Martins¹; ¹University of Michigan, United States | ||||
| 11:30 | 12:00 | 6.4.3 |
PUSHER PROPELLER INFLUENCE ON A LAMINAR WING TRANSITION LOCATION USING INFRARED THERMOGRAPHY J.P. Eguea¹, G.P.G. Silva¹, F.M. Catalano¹; ¹USP, Brazil | ||||
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| 10:30 | 11:00 | 7.4.1 |
EFFECT OF NITRIDING ON MICROSTRUCTURE AND MECHANICAL PROPERTIES ON A TI64 ALLOY FOR AEROSPACE APPLICATIONS S. Stekovic¹, R. Romero-Ramirez¹, L. Selegård, Saab Aeronautics, Sweden; ¹Linköping University, Sweden | ||||
| 11:00 | 11:30 | 7.4.2 |
MECHANICAL CHARACTERIZATION OF A COMPOSITE STRUCTURAL BATTERY LAMINATE G. Di Mauro¹, P. Russo, Institute for Polymers, Composites and Biomaterials, C.N.R., Italy; M. Guida¹; ¹University of Naples Federico II – Department of Industrial Eng., Italy | ||||
| 11:30 | 12:00 | 7.4.3 |
DOPAMINE-COATED UHMWPE/HYDROGEN-RICH BENZOXAZINE COMPOSITES FOR SPACE RADIATION SHIELDING J.-H. Cha¹, C.-G. Kim¹; ¹KAIST, South Korea | ||||
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| 10:30 | 11:00 | 8.4.1 |
DEVELOPMENT OF INNOVATIVE AND ECO-FRIENDLY AIRFRAME TECHNOLOGIES TO IMPROVE AIRCRAFT LIFE CYCLE ENVIRONMENTAL FOOTPRINT – LIFE CYCLE ASSESSMENT ACTIVITIES AT ECOTECH / CLEANSKY 2 L.A.S.A Prado¹, T.S.G. Das¹, S. Coskun¹, A. Kötter¹; ¹Capgemini Engineering / Altran Deutschland und SAS KG, Germany | ||||
| 11:00 | 11:30 | 8.4.2 |
NUMERICAL MODELING OF FLUID-STRUCTURE INTERACTION OF A 3D WEDGE DURING WATER IMPACT WITH VARIATION OF VELOCITY AND PITCH ANGLE F. Valpiani¹, P. Cicolini¹, D. Esposto¹, A. Galletti¹, D. Guagliardo¹; ¹Politecnico di Torino, Italy | ||||
| 11:30 | 12:00 | 8.4.3 |
EFFICIENT SURROGATE-BASED MULTI-OBJECTIVE OPTIMIZATION ALGORITHM WITH A NEW ADAPTIVE WEIGHT VECTOR GENERATION Z. Lu¹, Z.-H. Han¹, Z. Zhou, Science and Technology on Scramjet Laboratory,CARDC, China; W.-P. Song¹, Y. Zhang¹; ¹Northwestern Polytechnical University, China | ||||
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| 10:30 | 11:00 | 9.4.1 |
DEVELOPMENT OF A CONCEPTUAL DESIGN TOOL TO PREDICT PERFORMANCE OF HYDROGEN FUELLED PRECOOLED AIRBREATHING ROCKET ENGINES G. Grimaldi, Politecnico di Torino, Italy | ||||
| 11:00 | 11:30 | 9.4.2 |
LARGE EDDY SIMULATION OF RAMJET TO SCRAMJET TRANSITION T. Nilsson¹, C. Fureby¹; ¹Lund University, Sweden | ||||
| 11:30 | 12:00 | 9.4.3 |
AEROPROPULSIVE CHARACTERIZATION OF THE HYPERSONIC CRUISER VEHICLE IN STRATOFLY PROJECT P. Roncioni¹, L. Cutrone¹, M. Marini¹; ¹CIRA, Italy | ||||
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| 10:30 | 11:00 | 10.4.1 |
ENVIRONMENTAL ASSESSMENT OF NOISE ABATEMENT APPROACH TRAJECTORIES E.M. Thoma¹, T. Grönstedt¹, E. Otero Sola, KTH, Royal Institute of Technology, Sweden; X. Zhao¹; ¹Chalmers University of Technology, Sweden | ||||
| 11:00 | 11:30 | 10.4.2 |
DESIGN OF A TYPICAL MANEUVERING PROCESS SIMULATION TEST CONTROL SYSTEM WITH CONTROLLABLE RUDDER SURFACE J.-F. Wang, China; H. Tan, China; H. Chen, China; S. Feng, China; M.-H. Wang, China | ||||
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| 10:30 | 11:00 | 11.4.1 |
A PREPARATORY RESEARCH FOR UAM COLLISION AVOIDACE USING ADSB S. Ahn¹, H. Choi¹, S. Kim¹, J. Kim¹, H. Ryu¹; ¹Korea Aerospace Research Institute, South Korea | ||||
| 11:00 | 11:30 | 11.4.2 |
SAFE REINFORCEMENT LEARNING BASED MULTI-ROTOR COLLISION AVOIDANCE WITH UNEXPECTED OBSTACLES H.J. Ahn¹, C.S. Lim¹, D.W. Lee¹, H.C. Bang¹; ¹Korea Advanced Institute of Science and Technology(KAIST), South Korea | ||||
| 11:30 | 12:00 | 11.4.3 |
INVESTIGATION OF SIMULATION FRAMEWORKS FOR THE EVALUATION OF AUTOMATED FLIGHT FUNCTIONS FOR EVTOL AIRCRAFT Y. Lemmens¹, C. Teirlink¹, A. Hegde¹, D. Pla Guerrero¹, G. Olivares², H. Shah²; ¹Siemens Digital Industries Software, Belgium ;²National Institute for Aviation Research, United States | ||||
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| 10:30 | 11:00 | 12.4.1 |
SMART SKIN FOR AEW AIRCRAFT P. Khanal, Chalmers University of Technology, Sweden; P. Hallander¹, R. Luo¹; ¹Saab AB, Sweden | ||||
| 11:00 | 11:30 | 12.4.2 |
CERTIFICATION ASPECTS OF AN EARTH OBSERVATION PAYLOAD INSTALLED ON COMMERCIAL TRANSPORT AIRCRAFT R. Lopez Pereira, Safran Engineering Services GmbH, Germany; L. Rammos, Skyflox Sarl, Luxembourg | ||||
| 11:30 | 12:00 | 12.4.3 |
DESIGN OF ELECTRONICALLY PHASE-TUNING REFLECTARRAY ANTENNA FOR AIRBORNE RADAR APPLICATION G. Kong, China; P. Cui, China; W. Du, China; R. Chen, China | ||||
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| 10:30 | 11:00 | 13.4.1 |
EXPECTED TEAMWORK ATTRIBUTES BETWEEN HUMAN OPERATOR AND AUTOMATION IN AIR TRAFFIC CONTROL Å. Svensson, LFV, Sweden; N. Rönnberg, Linköping University, Sweden | ||||
| 11:00 | 11:30 | 13.4.2 |
PILOT’S ATTENTION DISTRIBUTION MODELING USING HIDDEN MARKOV MODELS J. Hanak¹, J. Vlk¹, P. Chudy¹; ¹Brno University of Technology, Czech Republic | ||||
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| 10:30 | 11:00 | 14.4.1 |
AERODYNAMIC DEVELOPMENT OF SAAB FCAS UNMANNED SUPERSONIC COMBAT AIRCRAFT M. Hackström¹, F. Kållberg¹, P. Nordström¹; ¹Saab Aeronautics, Sweden | ||||
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| 14:00 | 14:30 | 1.5.1 |
ICAS DIGITAL PIONEERING INITIATIVE AND SYSTEM OF SYSTEM CHALLENGES N. Nagel, Germany; C. Jouannet, Sweden | ||||
| 14:30 | 15:00 | 1.5.2 |
CHALLENGES OF MULTIDISCIPLINARY DESIGN OPTIMIZATION FOR GREEN AVIATION P. Schmollgruber, France; I. Staack, Sweden | ||||
| 15:00 | 15:30 | 1.5.3 |
POTENTIAL OF EXTENDED REALITY IN ENGINEERING AND CHALLENGES OF UNCONVENTIONAL VEHICLE DESIGN S. Bagassi, Italy; L. Boggero, Germany | ||||
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| 14:00 | 14:30 | 2.5.1 |
MORE ELECTRIC AIRCRAFT (MEA) SCALING ASPECTS AND WEIGHT IMPACT E. Holmgren¹, D. Haldar¹, L. Bertling Tjernberg, School of Electrical Engineering and Computer Science, KTH Royal, Sweden; A. Johansson, SAAB, Sweden; ¹KTH Royal Institute of Technology, Sweden | ||||
| 14:30 | 15:00 | 2.5.2 |
SIZING AND OPTIMIZATION OF A MORE ELECTRIC AIRCRAFT INTEGRATING SHORT-TERM INCREMENTAL TECHNOLOGIES T. Planès¹, S. Delbecq¹, V. Pommier-Budinger¹, V. Palanque¹, E. Bénard¹; ¹ISAE-SUPAERO, France | ||||
| 15:00 | 15:30 | 2.5.3 |
IMPLEMENTATION OF WING ICE PROTECTION SYSTEM IN MORE ELECTRIC AIRCRAFT TECHNOLOGIES D. Haldar¹, E. Holmgren¹, A. Johansson¹; ¹KTH Royal Institute of Technology, Sweden | ||||
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| 14:00 | 14:30 | 3.5.1 |
AEROSHAPE AND TRAJECTORY DESIGN OF NEXT GENERATION RE-ENTRY VEHICLES N. Montella¹, A. Aprovitola¹, L. Iuspa¹, G. Pezzella¹; ¹University of Campania , Italy | ||||
| 14:30 | 15:00 | 3.5.2 |
A RAPID DESIGN METHOD FOR QUIET SPIKE OF SUPERSONIC TRANSPORT AIRCRAFT L.-W. Zhang¹, Z.-H. Han¹, J.-L. Qiao¹, Y.-L. Ding¹, Q. Chen¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China | ||||
| 15:00 | 15:30 | 3.5.3 |
“CONCORDE-NEO”: A BIOFUEL PROPELLED SUPERSONIC COMMERCIAL AIRCRAFT WITH CONCORDE CONFIGURATION M. Borghi¹, G. Clinca¹, F.A. D'Amico¹, F. Fornaseri¹, E. Versino¹; ¹Politecnico di Torino, Italy | ||||
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| 14:00 | 14:30 | 4.5.1 |
CAD DEFORMATION FOR THE CONSIDERATION OF AEROELASTIC EFFECTS P. Wegener¹, S. Keye¹; ¹DLR, Germany | ||||
| 14:30 | 15:00 | 4.5.2 |
AUTOMATIC FREE-FORM DEFORMATION AS GEOMETRIC PARAMETERIZATION FOR AERODYNAMIC DESIGN M.A.L. Matunaga, ITA - Instituto Tecnológico de Aeronáutica, Brazil; J.L.F Azevedo, IAE - Instituto de Aeronáutica e Espaço, Brazil | ||||
| 15:00 | 15:30 | 4.5.3 |
HEAT TRANSFER ENHANCEMENT BY SUSPENDED PARTICLES IN A TURBULENT SHEARLESS FLOW H.R. Zandi Pour¹, M. Iovieno¹; ¹Politecnico di Torino, Italy | ||||
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| 14:00 | 14:30 | 5.5.1 |
TRANSITIONAL FLOW MODELLING OF A HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER TRANSONIC TRANSPORT AIRCRAFT WING M.M. Jentys¹, C. Breitsamter¹; ¹Technical University of Munich, Germany | ||||
| 14:30 | 15:00 | 5.5.2 |
REACTIVE CONTROL OF BYPASS TRANSITION IN A WING BOUNDARY LAYER J.M. Faúndez Alarcón¹, K. Sasaki¹, A. Hanifi¹, R. Larsson, Saab Aeronautics, Sweden; D.S. Henningson¹; ¹KTH Royal Institute of Technology, Linné FLOW Centre, Sweden | ||||
| 15:00 | 15:30 | 5.5.3 |
DIRECT NUMERICAL SIMULATIONS OF A THICK, ROTATING AIRFOIL AT A LOW REYNOLDS NUMBER T. Coelho Leite Fava¹, D. Henningson¹, A. Hanifi¹; ¹KTH, Sweden | ||||
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| 14:00 | 14:30 | 6.5.1 |
PRELIMINARY AERODYNAMIC WING DESIGN OPTIMISATION FOR WING-IN-GROUND EFFECT AIRCRAFT R. Jesudasan¹, R. Mariani¹, A. Hanifi¹; ¹KTH Royal Institute of Technololgy, Stockholm, Sweden | ||||
| 14:30 | 15:00 | 6.5.2 |
ON THE APPLICABILITY ASSESSMENT OF VON KARMAN’S MOMENTUM THEORY IN PREDICTING THE WATER-ENTER LOAD OF V-SHAPED BODY Y. Lu, China; A. Del Buono, Italy; T. Xiao, China; A. Iafrati, Italy; J. Xu, China | ||||
| 15:00 | 15:30 | 6.5.3 |
AERODYNAMIC AND AEROTHERMODYNAMIC ASSESSMENT OF A LIFTING-BODY RE-ENTRY VEHICLE A. Aprovitola¹, N. Montella¹, L. Iuspa¹, G. Pezzella¹, A. Viviani¹; ¹University of Campania , Italy | ||||
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| 14:00 | 14:30 | 7.5.1 |
TI-6AL-4V ADDITIVE MANUFACTURING MEASURE OF QUALITY ACCORDING TO FATIGUE CRACK INITIATION VS. CRACK PROPAGATION C. Matias¹, A. Diskin¹, O. Golan, Afeka- Tel-Aviv Academic College of Engineering, Israel; A. Garkun², E. Strokin²; ¹Israel Aerospace Industries (IAI), Israel ;²The Israel Institute of Metals,, Israel | ||||
| 14:30 | 15:00 | 7.5.2 |
RVE-BASED HOMOGENIZATION OF ADDITIVELY MANUFACTURED POROUS METALS A. Alaimo¹, G. Mantegna¹, C. Orlando¹, D. Tumino¹, C.R. Vindigni¹; ¹Faculty of Engineering and Architecture Kore University of Enna, Italy | ||||
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| 14:00 | 14:30 | 8.5.1 |
AMPAIRE AND THE ELECTRIFIED PROPULSION JOURNEY S. Ying, AMPAIRE, United States | ||||
| 14:30 | 15:00 | 8.5.2 |
REALISTIC HYDROGEN-BASED SOLUTIONS FOR SUSTAINABLE AVIATION J.P. Clark, Universal Hydrogen, United States | ||||
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| 14:00 | 14:30 | 9.5.1 |
PROPULSION SYSTEM INTEGRATION FOR A FIRST GENERATION HYDROGEN CIVIL AIRLINER? J. Huete¹, D. Nalianda¹, P. Pilidis¹; ¹Cranfield University, United Kingdom | ||||
| 14:30 | 15:00 | 9.5.2 |
SAND EROSION MODELING IN GENERIC COMPRESSOR RIG TESTING L.-Y. Jiang¹, X. Wu¹, Q. Yang¹; ¹National Research Council Canada, Canada | ||||
| 15:00 | 15:30 | 9.5.3 |
MULTI-PLATFORM APP-EMBEDDED MODEL FOR HYBRID AIR-BREATHING ROCKET-CYCLE ENGINE IN HYPERSONIC ATMOSPHERIC ASCENT S.E. Tsentis, Greece; V.G. Gkoutzamanis, Greece; A.D. Gaitanis, Greece; A.I. Kalfas, Greece | ||||
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| 14:00 | 14:30 | 10.5.1 |
HANDLING QUALITIES OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT D. Planas, ONERA & ISAE SUPAERO, France; C. Döll, ONERA, France; P. Pastor, ISAE SUPAERO, France | ||||
| 14:30 | 15:00 | 10.5.2 |
PRELIMINARY STUDY ON A DESIGN OF A RETURN FLIGHT TRAJECTORY OF A SUBORBITAL VEHICLE A. Kwiek¹, M. Figat¹, T. Goetzendorf-Grabowski ¹; ¹Warsaw University of Technology, Poland | ||||
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| 14:00 | 14:30 | 11.5.1 |
UNMANNED AERIAL VEHICLE\\\'S TRAJECTORY OPTIMIZATION IN CONSTRAINED ENVIRONMENTS J. Novák ¹, P. Chudý¹; ¹Brno University of Technology, Czech Republic | ||||
| 14:30 | 15:00 | 11.5.2 |
NUMERICAL MODELLING OF PITCHING WINGS FOR GUST MITIGATION W. Yuan¹, A. Wall¹, X. Zhang², D. Poirel²; ¹National Research Council (NRC) Canada, Canada ;²Royal Military College of Canada (RMC),, Canada | ||||
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| 14:00 | 14:30 | 12.5.1 |
VISION-BASED LOCALISATION FOR AUTONOMOUS AERIAL NAVIGATION IN GNSS-DENIED SITUATIONS D. Sabel¹, A. Maki¹, T. Westin², D. Åsvärn²; ¹KTH Royal Institute of Technology, Sweden ;²Spacemetric AB, Sweden | ||||
| 14:30 | 15:00 | 12.5.2 |
INNOONBOARD FOR IMPROVED IMAGE HANDLING IN AIRBORNE COASTAL RECONNAISSANCE – A PROJECT PRESENTATION D. Åkerman¹, O. Fästh, ST Airborne Solutions, Sweden; M. Persson, Unibap, Sweden; D. Sabel¹, D. Åsvärn¹; ¹Spacemetric, Sweden | ||||
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| 14:00 | 14:30 | 13.5.1 |
MANUFACTURE OF LARGE-SCALE SPACE EXPLORATION COMPONENTS USING WIRE + ARC ADDITIVE MANUFACTURING C. Diao¹, E. Eimer¹, S. Mancini, Thales Alenia Space, Italy; S. Krishnaswamy¹, F. Schwarz¹, E. Pagone¹, J. Ding¹, S. Williams¹, Z. Pinter², F. Martina²; ¹Cranfield University, United Kingdom ;²WAAM3D, United Kingdom | ||||
| 14:30 | 15:00 | 13.5.2 |
LATEST DEVELOPMENTS IN HIGH PRESSURE HEAT TREATMENT OF AEROSPACE COMPONENTS J. Shipley¹, A. Magnusson¹, C. Beamer, Quintus Technologyes LLC, United States; ¹Quintus Technologies AB, Sweden | ||||
| 15:00 | 15:30 | 13.5.3 |
VIKA - CONCEPT OF A DIGITAL PLATFORM FOR IMPLICIT KNOWLEDGE AND VIRTUAL ASSISTANCE FOR ADDITIVE MANUFACTURED PARTS J. Steffen, HAW Hamburg, Germany | ||||
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| 14:00 | 14:30 | 14.5.1 |
A FRAMEWORK FOR INNOVATION WITHIN AEROSPACE SEGMENT A.G. Slongo¹, C. Jochims Lau¹, G.L. de Oliveirra¹, B.M. Ramos¹, T.B. Volkman¹; ¹AEL Sistemas, Brazil | ||||
| 14:30 | 15:00 | 14.5.2 |
INTEGRATE ONLINE QUERY&DEFENSE INTO PROJECT BASED LEARNING TO PROMPT ENGINEERING AUTHENTIC EXPERIENCES S. Sun, Civil Aviation University of China, China; R. Gong, University of Waterloo, Canada | ||||
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| 16:00 | 16:30 | 1.6.1 |
NATO AVT-297 DEVELOPMENT OF A FRAMEWORK FOR VALIDATION OF COMPUTATIONAL TOOLS FOR ANALYSIS OF AIR VEHICLES J. Morrison¹, M. Nikbay, Istanbul Technical University, Turkey; E. Walker¹; ¹NASA Langley Research Center, United States | ||||
| 16:30 | 17:00 | 1.6.2 |
CONNECTING SYSTEM DESIGN TO MODELING AND SIMULATION CAPABILITIES J.M. Luckring, NASA Langley Research Center, United States; S. Shaw, MBDA UK Ltd., United Kingdom; W.L. Oberkampf, WLO Consulting, Inc., United States; R. Graves, Air Force Research Laboratory, United States | ||||
| 17:00 | 17:30 | 1.6.3 |
SYSTEM LEVEL IDENTIFICATION OF CRITICAL UNCERTAINTIES TO ENABLE VALIDATION EXPERIMENTS D.N. Mavris¹, E.Y. Yarbasi¹, B. Bagdatli¹; ¹Georgia Institute of Technology, United States | ||||
| 17:30 | 18:00 | 1.6.4 |
OPEN PANEL DISCUSSION op panel, United States | ||||
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| 16:00 | 16:30 | 2.6.1 |
BOEING/SAAB CO-DEVELOPMENT PROGRAMME OF T-7A TRAINER - A JOINT DIGITAL JOURNEY D.C. Yates, Boeing, United States | ||||
| 16:30 | 17:00 | 2.6.2 |
TOWARDS A SEAMLESS SIMULATION OF THE AIR TRANSPORT SYSTEM E. Moerland¹, A. Mancini¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany | ||||
| 17:00 | 17:30 | 2.6.3 |
CERTIFICATION DRIVEN DESIGN FROM STAKEHOLDERS’ NEEDS TO MDAO FORMULATION WITHIN AGILE 4.0 PROJECT M. Fioriti, Politecnico di Torino, Italy; C. Cabaleiro, DLR, Germany; T. Lefebvre, ONERA, France; P. Della Vecchia¹, M. Mandorino¹, S. Liscouët-Hanke², A. Jeyarai²; ¹Università di Napoli Federico II, Italy ;²Concordia University, Canada | ||||
| 17:30 | 18:00 | 2.6.4 |
DIGITAL COLLABORATIVE DESIGN: AN INNOVATIVE FRAMEWORK IN AERONAUTICAL EDUCATION Z. Cui¹, M. Luo¹, H. Liu¹, X. Sun¹, Z. Ji¹, Y. Hua, China Academy of Launch Vehicle Technology, China; ¹Beihang University, China | ||||
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| 16:00 | 16:30 | 3.6.1 |
INNOVATIVE URBAN AIR MOBILITY FROM THE PERSPECTIVE OF THE HAMBURG METROPOLITAN REGION D. Kloock-Schreiber¹, M. Swaid², V. Gollnick¹, A. Fay, HSU, Institute of Automation Technology, Germany; M. Niklaß²; ¹TUHH, Institute of Air Transportation Systems, Germany ;²DLR, Institute of Air Transportation Systems, Germany | ||||
| 16:30 | 17:00 | 3.6.2 |
ESTIMATION OF EVTOL FLIGHT PERFORMANCE USING ROTORCRAFT THEORY Y. Fukumine¹, Z. Lei¹; ¹Suwa University of Science, Japan | ||||
| 17:00 | 17:30 | 3.6.3 |
MIXED INTEGER NONLINEAR PROGRAMMING FOR EVTOL AIRCRAFT DESIGN AND OPTIMIZATION T. Jiang¹, M. Li¹, Y. Liu¹, Y. Zheng¹; ¹School of Aeronautics and Astronautics, Zhejiang University, China | ||||
| 17:30 | 18:00 | 3.6.4 |
RESEARCH ON THE DESIGN OF UNMANNED AERIAL VERICLE FOR MINE INSPECTION Z.-K. Li¹, S.-G. Su, Aerospace Times Feihong Technology Co., Ltd. , China; Z.-Y. Li¹, F.-R. Li¹, G. Chao¹; ¹Northwestern Polytechnical University, China | ||||
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| 16:00 | 16:30 | 4.6.1 |
EFFECT OF LES LENGTH SCALE AND NUMERICAL SCHEME IN HYBRID RANS-LES OF FREE SHEAR LAYER FLOWS S. Arvidson¹, M. Carlsson, Chalmers University of Technology, Sweden; S. Nilsson¹; ¹Saab Aeronautics, Sweden | ||||
| 16:30 | 17:00 | 4.6.2 |
INVESTIGATION OF LEADING-EDGE VORTICES ON A TRIPLE-DELTA-WING CONFIGURATION USING SCALE-ADAPTIVE SIMULATION T. Di Fabbio¹, E. Tangermann¹, M. Klein¹; ¹Universität der Bundeswehr München, Germany | ||||
| 17:00 | 17:30 | 4.6.3 |
NUMERICAL INVESTIGATION OF HYPERSONIC TURBULENT BOUNDARY LAYERS WITH HIGH-TEMPERATURE EFFECTS D. Passiatore¹, L. Sciacovelli, ENSAM Paris, France; P. Cinnela , Sorbonne Université, France; G. Pascazio¹; ¹Politecnico di Bari, Italy | ||||
| 17:30 | 18:00 | 4.6.4 |
HYBRID RANS-LES MODELLING: SOME RECENT DEVELOPMENT AND AERODYNAMIC APPLICATIONS S.-H. Peng, Swedish Defence Research Agency, FOI, Sweden | ||||
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| 16:00 | 16:30 | 5.6.1 |
STABILITY OF A LAMINAR BOUNDARY LAYER OVER LOCALISED SURFACE INDENTATION E.R. Gowree, ISAE-SUPAERO, France; C.J. Atkin, University of East Anglia, United Kingdom | ||||
| 16:30 | 17:00 | 5.6.2 |
ANALYSIS OF THE STABILITY OF MULTIPLE HELICAL VORTICES USING COMPLEX-STEP LINEARIZATION V.G. Kleine, ITA, Brazil; A. Hanifi¹, D.S. Henningson¹; ¹KTH, Sweden | ||||
| 17:00 | 17:30 | 5.6.3 |
EXPERIMENTAL EVALUATION OF A PASSIVE FLOW-CONTROL DEVICE FOR A TILTROTOR AIRCRAFT A.R. Proenca¹, S.A. Prince¹, L. Banks-Davies¹, K.P. Garry¹; ¹Cranfield University, United Kingdom | ||||
| 17:30 | 18:00 | 5.6.4 |
RESEARCH ON PRESSURE LOAD OF AN EMBEDDED JET NOZZLE H. Li¹, X. Wang¹, D. Yu¹, F. Liu¹; ¹Shenyang Aircraft Design and Research Institute, China | ||||
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| 16:00 | 16:30 | 6.6.1 |
PREDICTING STEADY LIFT AND DRAG COEFFICIENT OF TANDEM AIRCRAFT USING PRANDTL’S EXTENDED LIFTING-LINE THEORY IMPLEMENTED UNDER ASWING R. Jan¹, J.-M. Moschetta¹, J.-P. Condomines, ENAC, France; ¹ISAE-SUPAERO, France | ||||
| 16:30 | 17:00 | 6.6.2 |
ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUP R. Boisard¹, L. Lefevre¹, T. Zhang², G. Barakos², A. Visingardi, CIRA, Italy; F. Lößle³, A. Kostek³, T. Andronikos, NTUA, Greece; M. Keßler*, R. Wickersheim*, A. Colliº, G. Gibertiniº, A. Zanottiº; ¹ONERA, France ;²University Of Glasgow, United Kingdom ;³DLR, Germany ;*University of Stuttgart, Germany ;ºPolitecnico di Milano, Italy | ||||
| 17:00 | 17:30 | 6.6.3 |
COMPARING POTENTIAL FLOW SOLVERS FOR AERODYNAMIC CHARACTERISTICS ESTIMATION OF THE T-FLEX UAV F. Yu¹, J. Bartasevicius¹, M. Hornung¹; ¹Technical University of Munich, Germany | ||||
| 17:30 | 18:00 | 6.6.4 |
INVESTIGATION FLAPPING-FLIGHT AERODYNAMICS OF A ROBOTIC BIRD H.W.M. Hoeijmakers¹, L.H. Groot Koerkamp¹, L.D. de Santana¹, C.H. Venner¹, S. Stramigioli¹, J.L. Mulder¹, A. Brentjes¹, F. Gijsman¹, S.A. Hartman¹; ¹University of Twente, Netherlands | ||||
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| 16:00 | 16:30 | 7.6.1 |
WING STATIC STRUCTURAL ANALYSIS AND EXPERIMENTAL TESTING OF A COMPOSITE 1:8 S55-X REPLICA G. Nicolosi¹, A. Lunghitano ¹, S. Lombardi ¹, T. Talamucci¹, A. Caivano¹, N. Simone¹, E. Cestino¹, V. Sapienza, Aeronautical Engineering Consultant, Italy; ¹Politecnico di Torino, Italy | ||||
| 16:30 | 17:00 | 7.6.2 |
ASSESSMENT OF FAILURE UNDER LONGITUDINAL COMPRESSION OF UNIDIRECTIONAL COMPOSITES WITH IN-PLANE FIBER MISALIGNMENT A.R. de Faria, ITA, Brazil | ||||
| 17:00 | 17:30 | 7.6.3 |
DAMAGE QUANTIFICATION ON COMPOSITE STRUCTURES USING NEURAL NETWORKS AND HYBRID DATA L.P.S. Ferreira¹, M.O. Yano², S. Silva², C.A. Cimini¹; ¹UFMG, Brazil ;²UNESP, Brazil | ||||
| 17:30 | 18:00 | 7.6.4 |
TRIBOLOGICAL AND STRUCTURAL EVALUATION OF 3D PRINTED EPOXY RESINS G.C. Cristea¹, A. Stefan¹, K. Krawczyk, Joanneum Research, Austria; C.-E. Pelin¹, S. Ilina¹; ¹INCAS, Romania | ||||
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| 16:00 | 16:30 | 8.6.1 |
AEROELASTIC MODELING, LOADS ANALYSIS AND STRUCTURAL DESIGN OF A FIGHTER AIRCRAFT A. Voß¹, T. Klimmek¹; ¹DLR Institute of Aeroelasticity , Germany | ||||
| 16:30 | 17:00 | 8.6.2 |
LOADS ANALYSIS AND STRUCTURAL OPTIMIZATION OF A LONG-RANGE TRANSPORT CONFIGURATION WITH HYBRID LAMINAR FLOW CONTROL V. Handojo¹, T. Klimmek¹, T. Streit, DLR - Institute of Aerodynamics and Flow Technology, Germany; ¹DLR - Institute of Aeroelasticity, Germany | ||||
| 17:00 | 17:30 | 8.6.3 |
LATERAL GUST BEHAVIOUR OF AIRCRAFT INCORPORATING FLARED FOLDING WINGTIPS R.C.M. Cheung¹, H. Gu¹, F. Healy¹, D. Rezgui¹, J.E. Cooper¹; ¹University of Bristol, United Kingdom | ||||
| 17:30 | 18:00 | 8.6.4 |
SET-BASED DESIGN COORDINATION BETWEEN COUPLED SYSTEMS: A WING AERO-STRUCTURAL DESIGN PERSPECTIVE X. Chen¹, A. Riaz¹, M.D. Guenov¹; ¹Cranfield University, United Kingdom | ||||
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| 16:00 | 16:30 | 9.6.1 |
LATTICE BOLTZMANN METHOD FOR BROADBAND NOISE PREDICTIONS ON A TURBULENCE-CASCADE TEST RIG INCLUDING SERRATED VANES M. Buszyk¹, L. Vienne², T. Le Garrec¹, J.-F. Boussuge², C. Polacsek¹, R. Barrier¹; ¹ONERA, France ;²CERFACS, France | ||||
| 16:30 | 17:00 | 9.6.2 |
OPTIMIZATION OF INSTALLED COMPACT AND ROBUST NACELLES USING SURROGATE MODELS F. Sánchez-Moreno¹, D. MacManus¹, J. Hueso-Rebassa¹, F. Tejero¹, C. Sheaf, Rolls Royce, United Kingdom; ¹Cranfield University, United Kingdom | ||||
| 17:00 | 17:30 | 9.6.3 |
AEROACOUSTIC PERFORMANCES OF A LOW-NOISE AIRFOIL CASCADE WITH SERRATED LEADING EDGES: PREDICTIONS AND MEASUREMENTS C. Polacsek¹, M. Buszyk¹, R. Barrier¹, V. Clair², E. Salze²; ¹ONERA, France ;²LMFA, France | ||||
| 17:30 | 18:00 | 9.6.4 |
EFFECT OF HEAT EXCHANGER INTEGRATION IN AERODYNAMIC OPTIMISATION OF AN AGGRESSIVE S-DUCT I. Jonsson¹, R. Ranman¹, A. Capitao¹, C. Xisto¹; ¹Chalmers Tekniska Hogskola AB, Sweden | ||||
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| 16:00 | 16:30 | 10.6.1 |
AUTOMATIC TAKE-OFF AND LANDING OF A VERY LIGHT ALL ELECTRIC OPTIONALLY PILOTED AIRCRAFT S. Scherer¹, M. Speckmaier¹, D. Gierszewski¹, C. Mishra¹, A. Steinert¹, R. Steffensen¹, S. Wulf¹, F. Holzapfel¹; ¹Technical University of Munich,, Germany | ||||
| 16:30 | 17:00 | 10.6.2 |
LPV/LFR CONTROL FOR ACTIVE FLUTTER SUPPRESSION OF A SMART AIRFOIL MODEL R.L. Pereira, ITA, Brazil; P.J. González¹, F.J. Silvestre¹; ¹TU Berlin, Germany | ||||
| 17:00 | 17:30 | 10.6.3 |
LQR BASED DIGITAL AUTOPILOT FOR LIGHT SPORT AIRCRAFT J. Vlk¹, P. Chudy¹, M. Prustomersky¹; ¹Brno University of Technology, Czech Republic | ||||
| 17:30 | 18:00 | 10.6.4 |
EXTENSION OF THE CAPABILITIES OF AN AUTOMATIC LANDING SYSTEM WITH PROCEDURES MOTIVATED BY VISUAL-FLIGHT-RULES S. Scherer¹, C. Mishra¹, F. Holzapfel¹; ¹Technical University of Munich, Germany | ||||
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| 16:00 | 16:30 | 11.6.1 |
FAULT DIAGNOSIS FOR SENSOR AND ACTUATOR OF HEXACOPTER UAV USING DUAL EXTENDED KALMAN FILTER Y.J. Kim¹, T.G. Kim¹, S.K. Kim¹; ¹Chungnam National University, South Korea | ||||
| 16:30 | 17:00 | 11.6.2 |
CONTROL AUGMENTATION SYSTEM DESIGN FOR THE QUAD TILT-WING UAV VIA H-INFINITY STRUCTURE WITH GWO K.K. Deveerasetty¹, K. Oka¹, A. Harada¹; ¹Kochi University of Technology, Japan | ||||
| 17:00 | 17:30 | 11.6.3 |
OPTIMIZATION OF ENERGY CONSUMPTION IN THE TRANSITION STATE OF A QUAD-PLANE T. Goetzendorf-Grabowski¹, D. Kacik¹, K. Pobikrowska, Lukasiewicz Research Network – Institute of Aviation, Poland; J. Mieloszyk¹; ¹Warsaw University of Technology, Poland | ||||
| 17:30 | 18:00 | 11.6.4 |
FLIGHT VERIFICATION OF AUTOMATIC TRANSITION FOR QUAD TILT WING SMALL UAV K. Muraoka¹, M. Sato¹; ¹Japan Aerospace Exploration Agency, Japan | ||||
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| 16:00 | 16:30 | 12.6.1 |
ELECTRICALLY POWERED LANDING GEAR SYSTEM FOR TRANSPORT AIRCRAFT TAXIING I. Berlowitz, IBAero Engineering, Israel | ||||
| 16:30 | 17:00 | 12.6.2 |
THE INFLUENCE OF THE MODEL PARAMETERS OF LI-ION BATTERIES ON THE WIRING HARNESS PERFORMANCE OF EVTOL AIRCRAFT S. Oberschwendtner¹, M. Hornung¹; ¹Technical University of Munich, Germany | ||||
| 17:00 | 17:30 | 12.6.3 |
ANALYSIS AND DEVELOPMENT OF INTEGRATED LOW-PRESSURE SHAFT GENERATOR A. Reinap¹, M. Genrup¹, R. Avellán², H. Mårtensson²; ¹Lund University, Sweden ;²GKN Aerospace, Sweden | ||||
| 17:30 | 18:00 | 12.6.4 |
AN INTEGRATED CONTROL SCHEME FOR STARTER/GENERATOR SYSTEM IN MORE ELECTRIC AIRCRAFT H. Li, China; Z. Zhao, China; Z. Wan, China; L. Xu, China; S. Zhao, China; P. Sun, China | ||||
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| 16:00 | 16:30 | 13.6.1 |
STUDY OF THE COST EFFICIENCY AND LAMINATE QUALITY USING DIFFERENT MOULD-MAKING TECHNOLOGIES L. Loiodice¹, S. Grendene¹, T. Binetti¹, I. Boni ¹, F. Lovero ¹, R. Piani¹; ¹Politecnico di Torino, Italy | ||||
| 16:30 | 17:00 | 13.6.2 |
A VALUE-DRIVEN QUANTITATIVE FRAMEWORK COUPLING AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN BY LEVERAGING THE AGILE 4.0 MBSE-MDO FRAMEWORK G. Donelli¹, J.M.G.D. Mello², F.I.K. Odaguil², T. Lefebvre³, N. Bartoli³, T. van der Laan, GKN Fokker, Netherlands; L. Boggero¹, B. Nagel¹; ¹DLR, Germany ;²Embraer, Brazil ;³ONERA, France | ||||
| 17:00 | 17:30 | 13.6.3 |
REAL-TIME IDENTIFICATION OF USER ACTIONS IN COMPUTER-AIDED MANUFACTURING USING MACHINE LEARNING AND COMPUTER VISION B. Peukert¹, J. Vesterberg¹, J. Birberg, Saab AB , Sweden; ¹KTH, Sweden | ||||
| 17:30 | 18:00 | 13.6.4 |
DOMAIN MODEL CONSTRUCTION METHOD OF AVIATION EQUIPMENT MANUFACTURING OPERATION MANAGEMENT L. Chen¹, X. Li¹, Z. Zhang¹, W. Huang¹, R. Wu¹, Y. Li¹; ¹AVIC Chengdu Aircraft Industrial (Group) Co., Ltd., China | ||||
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| 16:00 | 16:30 | 14.6.1 |
OVERVIEW OF JAXA AND NASA COLLABORATION ON MANNED AND UNMANNED AIRCRAFT OPERATION INTEGRATION IN DISASTER RESPONSE A. Andreeva-Mori¹, J. Homola², M. Johnson², K. Kobayashi¹, Y. Okuno¹, P. Kopardekar²; ¹JAXA, Japan ;²NASA, United States | ||||
| 16:30 | 17:00 | 14.6.2 |
INTEGRATED UAS TRAJECTORY OPTIMIZATION FOR DISASTER RESPONSE RECONNAISSANCE MISSIONS A. Andreeva-Mori¹, J. Homola², M. Johnson², K. Kobayashi¹, Y. Okuno¹, P. Kopardekar²; ¹JAXA, Japan ;²NASA, United States | ||||
| 17:00 | 17:30 | 14.6.3 |
DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFT J. Ritter¹, H. Kahlo¹, N. Mandry¹, A.G. Can¹, P. Modi¹, B. Knoblauch¹, J. Schneider¹, A. Stromayer¹, T. Dietl², P. Ratei², P. Shiva Prakasha², B. Nagel²; ¹University of Stuttgart, Germany ;²German Aerospace Center (DLR), Germany | ||||
| 17:30 | 18:00 | 14.6.4 |
DESIGNING FOR SECURITY: A CYBERSECURITY INTRODUCTION FOR AEROSPACE EDUCATION K. Roush, United States | ||||
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| 10:30 | 11:00 | 1.7.1 |
DYNAMIC PAIRWISE WAKE VORTEX SEPARATIONS FOR ARRIVALS USING PREDICTIVE MACHINE LEARNING MODELS L. Frigerio¹, I. De Visscher, Wake Prediction Technologies (WaPT), Belgium; G. Stempfel¹, R. Barragan Montes², C. Chalon Morgan²; ¹Euranova, Belgium ;²EUROCONTROL, Belgium | ||||
| 11:00 | 11:30 | 1.7.2 |
FLIGHT SIMULATION TO SUPPORT SAFETY CASE FOR PAIR-WISE WAKE TURBULENCE SEPARATION ON DEPARTURES I. De Visscher, WaPT, Belgium; M. Langer¹, K. Bayram¹, T. Feuerle², P. Hecker², F. Rooseleer³, C. Chalon Morgan³; ¹2CACTUS partners GmbH, Germany ;²TU Braunschweig, Germany ;³EUROCONTROL, Belgium | ||||
| 11:30 | 12:00 | 1.7.3 |
FLIGHT SIMULATION TO SUPPORT SAFETY CASE FOR PAIR-WISE WAKE TURBULENCE SEPARATION ON DEPARTURES M. Langer, Germany | ||||
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| 10:30 | 11:00 | 2.7.1 |
ZONAL MODEL BASED AIRCRAFT PASSENGER THERMAL COMFORT COMPARATIVE STUDY S. Tarroc Gil¹, J. Schminder¹, A. Guerrero i Almirall, UptimAI, Czech Republic; J.I. Tarraga Prieto, MAHLE Electronics S.L.U, Slovenia; R. Vaz Linn, Federal University of Rio Grande do Sul, Brazil; ¹Linköping University, Sweden | ||||
| 11:00 | 11:30 | 2.7.2 |
AURALIZATION OF NOISE IN A VIRTUAL REALITY AIRCRAFT CABIN FOR PASSENGER WELL-BEING USING HUMAN-CENTRED APPROACH S. Santhosh¹, M.C. Moruzzi¹, F. De Crescenzio¹, S. Bagassi¹; ¹University of Bologna, Italy | ||||
| 11:30 | 12:00 | 2.7.3 |
TRANSPORT AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM AIR QUALITY IMPROVEMENT I. Berlowitz, IBAero Engineering, Israel | ||||
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| 10:30 | 11:00 | 3.7.1 |
SERIES OR PARALLEL HYBRID-ELECTRIC AIRCRAFT PROPULSION SYSTEMS? CASE STUDIES OF THE ATR42 AND ATR72 A. Batra¹, R. Raute, Dept. Ind. Elec. Power Conv., University of Malta, Malta; R. Camilleri¹; ¹Institute of Aerospace Technologies (IAT), University of Malta , Malta | ||||
| 11:00 | 11:30 | 3.7.2 |
DEVELOPMENT OF A HYDROGEN-POWERED FUSELAGE-MOUNTED BLI PROPULSOR ADD-ON FOR PASSENGER AIRCRAFT A. Heidebrecht¹, K. Burger¹, M. Hoogreef¹, R. Vos¹, A.T. Isikveren, SAFRAN S.A. c/o Aerospace Embedded Solutions GmbH, Munich, Germany; A. Gangoli Rao¹; ¹TU Delft, Netherlands | ||||
| 11:30 | 12:00 | 3.7.3 |
TECHNOLOGY ROADMAP AND CONCEPTUAL DESIGN OF HYBRID AND ELECTRIC CONFIGURATIONS IN THE COMMUTER CLASS F. Nicolosi¹, V. Marciello¹, V. Cusati¹, F. Orefice¹; ¹University of Naples Federico II, Italy | ||||
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| 10:30 | 11:00 | 4.7.1 |
EFFECTS OF TWO WINGLET TIP GEOMETRIES ON THE FLOW AND AERODYNAMIC PERFORMANCE OF A HYDRAULIC AXIAL TURBINE D.S. Tonon¹, J.T. Tomita¹, C. Bringhenti¹, D.F.C. Barbosa¹, L.H.L. Whitacker¹, L.E.N. Almeida, AVIBRAS, Brazil; ¹Aeronautics Institute of Technology , Brazil | ||||
| 11:00 | 11:30 | 4.7.2 |
INVESTIGATION ON CRUISE PERFORMANCE OF A HAND-LAUNCHED SOLAR-POWERED UAV FOR ENVIRONMENTAL MONITORING IN TIBET K.-L. Wang¹, Z. Zhou¹; ¹Northwestern Polytechnical University, China | ||||
| 11:30 | 12:00 | 4.7.3 |
INVESTIGATION OF TWO-DIMENSIONAL VORTEX DYNAMICS IN THE V103 CASCADE Y. Zhao¹, Y. Liu¹, S. Zhu¹, H. Xu¹, D. Wang¹; ¹Department of Aeronautics and Astronautics, Fudan University, China | ||||
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| 10:30 | 11:00 | 5.7.1 |
INTERNATIONAL SCIENTIFIC ASSESSMENT ON URBAN AIR MOBILITY AS A CONTRIBUTION TO FUTURE AVIATION STANDARDS C. Eschmann, DLR, Germany; D.L. Hackenberg, National Aeronautics and Space Administration (NASA), United States; C. Vidal, National Research Council Canada (NRC), Canada | ||||
| 11:00 | 11:30 | 5.7.2 |
AN INTERNATIONAL RESEARCH PERSPECTIVE ON AIRSPACE INTEGRATION IN THE FRAMEWORK OF URBAN AIR MOBILITY A. Andreeva-Mori, JAXA, Japan; S. Sharma¹, S. Verma¹, B. Dziugiel, Lukasiewicz Research Network, Poland; D. Sziroczak, Budapest University of Technology and Economics, Hungary; ¹Ames Research Center, United States | ||||
| 11:30 | 12:00 | 5.7.3 |
KARI-DLR DIGITAL COLLABORATION TO BUILD A MDAO SYSTEM FOR THE PRELIMINARY DESIGN OF HYBRID EVTOL AIRCRAFT S.-K. Paek, Korea Aerospace Research Institute, South Korea | ||||
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| 10:30 | 11:00 | 6.7.1 |
WIND TUNNEL TESTS RESULTS AND PERFORMANCE OF THE MOTHIF BLOWN FLAP P. D'Alesio¹, G. Travostino¹, P. Planquart², G. Glabeke²; ¹Piaggio Aerospace, Italy ;²von Karman Institute, Belgium | ||||
| 11:00 | 11:30 | 6.7.2 |
A STUDY OF HIGH-LIFT DEVICES FOR LOW REYNOLDS NUMBER APPLICATIONS Y. Leng¹, K. Fayez, DELAIR, France; J.-M. Moschetta¹, M. Bronz, ENAC, France; ¹ISAE-SUPAÉRO, France | ||||
| 11:30 | 12:00 | 6.7.3 |
MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF 2D HIGH-LIFT DEVICE BASED ON DISTRIBUTED DEEP REINFORCEMENT LEARNING J.-H. Dai¹, P.-Q. Liu¹, L. Li¹; ¹Beihang University, China | ||||
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| 10:30 | 11:00 | 7.7.1 |
A GLOBAL/LOCAL ELEMENT-WISE APPROACH FOR THE BUCKLING AND POST-BUCKLING ANALYSIS OF THIN MULTILAYERED STRUCTURES R. Augello¹, E. Carrera¹, A. Pagani¹, M. Petrolo¹; ¹Politecnico di Torino, Italy | ||||
| 11:00 | 11:30 | 7.7.2 |
OPTIMAL DESIGN OF STIFFENED PANELS UNDER BUCKLING CONSTRAINTS: A DESIGN METHODOLOGY CONSIDERING CAD-BASED PARAMETERIZATION WITH SIMULTANEOUS LAYOUT AND SIZING OPTIMIZATION H. Rahman¹, R. De Breuker¹, S.G.P. Castro¹; ¹Delft University of Technology, Netherlands | ||||
| 11:30 | 12:00 | 7.7.3 |
INVESTIGATION OF BUCKLING RESPONSE OF CYLINDRICAL SHELLS USING 3D-PRINTING TECHNOLOGY C. Bisagni¹, E. Labans¹; ¹Delft University of Technology, Netherlands | ||||
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| 10:30 | 11:00 | 8.7.1 |
PARAMETER IDENTIFICATION BY UPDATING THE STRUCTURAL MODEL OF A UAV WITH FLEXIBLE WING T.R. De Paula¹, V.P. Fernandes¹, A.G.P. Sarmento¹, D.F.C. Zuñiga¹, A.G. Souza, Universidade de Lisboa, Portugal; R.G.A. Silva¹, L.C.S. Góes¹; ¹Aeronautics Institute of Technology, Brazil | ||||
| 11:00 | 11:30 | 8.7.2 |
RESEARCH ON THE EFFECT OF THE PROCESS FIRST SHOT PEENING STRENGTHENING THEN SHOT PEENING FORMING ON FATIGUE STRENGTH OF 7050 HIGH-STRENGTH ALUMINUM ALLOY G.-W. Li¹, T.-H. Luo¹, H.-Y. Hang¹; ¹Northwestern Polytechnical University, China | ||||
| 11:30 | 12:00 | 8.7.3 |
DESIGNING SUSTAINABLE AVIATION SOLUTIONS WITH DIGITAL TWIN APPROACH M. Grundström¹, S. Ferrari¹; ¹Tampere University, Finland | ||||
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| 10:30 | 11:00 | 9.7.1 |
FEASIBILITY STUDY OF SHORT SUBSONIC DIFFUSER CONCEPT FOR SUPERSONIC INLET H. Miki¹, J. Akatsuka¹, I. Kikura, Tokyo University of Agriculture and Technology, Japan; Y. Watanabe¹; ¹JAXA, Japan | ||||
| 11:00 | 11:30 | 9.7.2 |
A STUDY ON THE DEVELOPMENT OF THE FLOW DISTORTION DOWNSTREAM OF AN S-DUCT INTAKE M. Migliorini¹, P.K. Zachos¹, D.G. MacManus¹, V. Monnier¹; ¹Cranfield University, United Kingdom | ||||
| 11:30 | 12:00 | 9.7.3 |
STUDY OF THE IMPACT OF AZIMUTHAL FLOW DISTORTION ON IN-DUCT ACOUSTIC PROPAGATION USING A MULTIMODAL FORMULATION B. Mangin¹, M. Daroukh¹, G. Gabard, LAUM, France; ¹ONERA, France | ||||
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| 10:30 | 11:00 | 10.7.1 |
META-REINFORCEMENT LEARNING-BASED FAULT TOLERANT CONTROL FOR A QUADROTOR WITH A SEVERE LOSS OF ROTOR S.-H. Kim¹, Y. Jung¹, Y. Kim¹; ¹Seoul National University, South Korea | ||||
| 11:00 | 11:30 | 10.7.2 |
FLIGHT CONTROLLABILITY ANALYSIS IN TIGHT FORMATION AND CRUISE FLIGHT FOR FUEL SAVING D.B. Rossato, Faculdade de Tecnologia SENAI , Brazil; K.H. Kienitz, Instituto Tecnológico de Aeronáutica, Brazil | ||||
| 11:30 | 12:00 | 10.7.3 |
DESIGN OF STABILITY AUGMENTATION SYSTEMS FOR A FLEXIBLE AIRCRAFT USING LQ OUTPUT-FEEDBACK CONTROL VIA LMI R.L. Pereira, ITA, Brazil; P.J. González¹, F.J. Silvestre¹; ¹TU Berlin, Germany | ||||
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| 10:30 | 11:00 | 11.7.1 |
DOOR-TO-DOOR TRAVEL PLANNER FOR IMPROVED TRAVELER EXPERIENCE USING DIGITAL TWIN CONCEPT J. La¹, C. Bil¹, I. Heiets¹, K.A. Lau, Qatar Airways, Qatar; ¹RMIT University, Australia | ||||
| 11:00 | 11:30 | 11.7.2 |
ENVIRONMENTAL AGENT-BASED MODELLING FOR A FIREFIGHTING SYSTEM OF SYSTEMS J.L. Lovaco¹, I. Staack¹, P. Krus¹; ¹Linköpings Universitet, Sweden | ||||
| 11:30 | 12:00 | 11.7.3 |
REQUIREMENTS-BASED GENERATION OF OPTIMAL VERTICAL TAKEOFF AND LANDING TRAJECTORIES FOR ELECTRIC AIRCRAFT C. Krammer, Germany; F. Schweighofer, Germany; D. Gierszewski, Germany; S.P. Scherer, Germany; T. Akman, Germany; H. Hong, Germany; F. Holzapfel, Germany | ||||
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| 10:30 | 11:00 | 12.7.1 |
UK-AEROSPACE RESEARCH CONSORTIUM - EXPANDING THE VALUE OF UK ACADEMIC RESEARCH R. Gardner, UK - Aerospace Research Consortium, United Kingdom; I. Gray, Cranfield University, United Kingdom | ||||
| 11:00 | 11:30 | 12.7.2 |
MAXIMISING VALUE FROM UK ACADEMIC RESEARCH - THE UK-AEROSPACE RESEARCH CONSORTIUM THEME APPROACH R. Gardner, UK-Aerospace Research Consortium, United Kingdom | ||||
| 11:30 | 12:00 | 12.7.3 |
THE BENEFIT OF BILATERAL RESEARCH NETWORKS - THE SARC AND BARINET INITIATIVES AND THE BRAZILIAN SWEDISH COLLABORATION IN AERONAUTICS E. Villani, Aeronautics Institute of Technology (ITA), Brazil; P. Krus, Linköping University, Sweden; V.J. de Negri, Federal University of Santa Catarina (UFSC), Brazil; L. Pereira, Federal University of ABC (UFABC), Brazil; G. Caurin, University of São Paulo (USP), Brazil | ||||
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| 10:30 | 11:00 | 13.7.1 |
MOTION STROKE DESIGN ON FLEXIBLE ASSEMBLY TOOLING FOR MULTIPLE AIRCRAFT COMPONENTS F. Guo¹, C. Song¹, X. Zhang², Q. Xiao²; ¹University of Science and Technology Beijing, China ;²AVIC Manufacturing Technology Institute, China | ||||
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| 10:30 | 11:00 | 14.7.1 |
NON-INTRUSIVE AEROTHERMAL CHARACTERIZATION OF SURFACE HEAT EXCHANGERS FOR TURBOFAN AEROENGINES A. Broatch¹, J. García-Tíscar¹, A. Felgueroso¹, M. Gelain², A. Couilleaux²; ¹Universitat Politecnica de Valencia, Spain ;²Safran Aircraft Engines, France | ||||
| 11:00 | 11:30 | 14.7.2 |
ZONAL MODEL VALIDATION FOR AN ENVIRONMENTALLY FRIENDLY AIRCRAFT CARGO FIRE PROTECTION SYSTEM WITH CONTAINERIZED LOAD A. Pathak¹, M. Pschirer¹, M. Kienberger¹, V. Norrefeldt¹; ¹Fraunhofer IBP, Germany | ||||
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| 13:55 | 14:25 | 1.8.1 |
TOWARD DIRECT DRIVE ELECTRIFIED PROPULSION CONCEPTS FOR SUSTAINABLE AVIATION C. Tschida, United States | ||||
| 14:25 | 14:55 | 1.8.2 |
REGIONAL AIR MOBILITY MARKET STUDY C.Y. Justin¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States | ||||
| 14:55 | 15:25 | 1.8.3 |
UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATION R. Jansen¹, C.C. Kiris², T. Chau², L. Machado², T.P. Dever¹, J.S. Litt¹, J.J. Arthur³, M.N. Lynde³, J.W. Chapman¹, J.L. Kratz¹, M.G. Turner¹, A. Mirhashemi¹, C.L. Denham³, J.M. Wishart*, K. Mahavier*, M.J. Boucherº, N. Heersemaº, E.J. Stalcup¹; ¹NASA Glenn Research Center, United States ;²NASA Ames Research Center, United States ;³NASA Langley Research Center, United States ;*Volpe National Transportation Systems Center, United States ;ºNASA Armstrong Research Center, United States | ||||
| 15:25 | 15:55 | 1.8.4 |
EUROPEAN AVIATION RESEARCH AND INNOVATION TOWARDS CLIMATE NEUTRALITY M. Kyriakopoulos, Belgium | ||||
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| 13:55 | 14:25 | 2.8.1 |
A CREDIBILITY-BASED CRITERION FOR THE ASSESSMENT OF FUTURISTIC AIRCRAFT CONCEPTS N.F.M. Wahler¹, L. Radomsky², L.V. Hanisch², R. Mallwitz², M. Henke², A. Elham¹; ¹University of Southampton, United Kingdom ;²TU Braunschweig, Germany | ||||
| 14:25 | 14:55 | 2.8.2 |
INSTALLATION PENALTY OF AERO-ENGINES ON NARROW BODY AIRCRAFT T.E. Boogaart¹, M.F.M. Hoogreef¹, A. Gangoli Rao¹; ¹Delft University of Technology, Netherlands | ||||
| 14:55 | 15:25 | 2.8.3 |
FAST-OAD-GA: AN OPEN-SOURCE EXTENSION FOR OVERALL AIRCRAFT DESIGN OF GENERAL AVIATION AIRCRAFT F. Lutz¹, J. Jézégou¹, A. Reysset, INSA Toulouse, France; A. Busteros-Ramos¹, V. Pommier-Budinger¹; ¹ISAE-SUPAERO, France | ||||
| 15:25 | 15:55 | 2.8.4 |
THE USE OF COMPUTATIONAL FLUID DYNAMICS METHODS IN THE PRELIMINARY DESIGN OF A NEW GENERATION LIGHT COMBAT AIRPLANE L. Kiszkowiak¹, A. Olejnik¹, A. Dziubinski, Lukasiewicz Research Network – Institute of Aviation, Poland; ¹Military University of Technology, Poland | ||||
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| 13:55 | 14:25 | 3.8.1 |
A SCALABLE HYDROGEN PROPULSION SYSTEM FOR CIVIL TRANSPORT AIRCRAFT A.S.J. van Heerden¹, S. Sasi¹, R. Ghelani¹, D. Sanders¹, I. Roumeliotis¹; ¹Cranfield University, United Kingdom | ||||
| 14:25 | 14:55 | 3.8.2 |
AUTOMATED HYBRID PROPULSION MODEL CONSTRUCTION FOR CONCEPTUAL AIRCRAFT DESIGN AND OPTIMIZATION M. Fouda¹, E.J. Adler², J.H. Bussemaker¹, J.R.R.A. Martins², D.F. Kurtulus, Middle East Technical University, Turkey; L. Boggero¹, B. Nagel¹; ¹DLR, Germany ;²University of Michigan, United States | ||||
| 14:55 | 15:25 | 3.8.3 |
DESIGN AND PERFORMANCE OF LIQUID HYDROGEN FUELLED AIRCRAFT FOR YEAR 2050 EIS C. Xisto, Chalmers University of Technology, Sweden; A. Lundbladh, GKN Aerospace AB, Sweden | ||||
| 15:25 | 15:55 | 3.8.4 |
NUMERICAL INVESTIGATION ON THE AERO-PROPULSION EFFECT OF DISTRIBUTED PROPULSION FOR V/VTOL APPLICATION S. Song¹, S. Deng¹, Q. Li, AVIC General Aircraft Research Institute, China; H. Qiao¹, Y. Lu¹; ¹Nanjing University of Aeronautics and Astronautics, China | ||||
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| 13:55 | 14:25 | 4.8.1 |
DATA-DRIVEN ADAPTATION AND OPTIMIZATION OF TURBULENT FLOWS K.J. Fidkowski, University of Michigan, United States | ||||
| 14:25 | 14:55 | 4.8.2 |
HIGH-ORDER ACCURATE EMBEDDED-BOUNDARY DISCONTINUOUS GALERKIN METHODS FOR INVISCID GAS DYNAMICS V. Gulizzi, University of Palermo, Italy | ||||
| 14:55 | 15:25 | 4.8.3 |
HIGH-ACCURATE NUMERICAL SIMULATION FOR VORTEX FLOW OVER A SLENDER MISSILE AT HIGH ANGLE OF ATTACK C.-H. Gao¹, W.-P. Song¹, S.-Q. Han¹, K. Lu¹, Y. Wang¹, Z.-H. Han¹, B. Wu, Shanghai Electro-mechanical Engineering Institute, China; ¹Northwestern Polytechnical University, China | ||||
| 15:25 | 15:55 | 4.8.4 |
A COMPUTATIONAL STUDY ON BLADE-VORTEX INTERACTION FOR COAXIAL ROTORS IN HOVER USING A NOVEL HIGH-ORDER SCHEME S.-Q. Han, Sichuan University, China; W.-P. Song¹, Z.-H. Han¹; ¹Northwestern Polytechnical University, China | ||||
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| 13:55 | 14:25 | 7.8.1 |
ADAPTIVE PATH PLANNING FOR SPRAYING UAS IN VINEYARD UNDER VARIABLE WIND CONDITION L. Scagnellato¹, M. Lecce¹, N. Bloise¹, M. Carreño Ruiz¹, E. Capello¹, G. Guglieri¹; ¹Politecnico di Torino, Italy | ||||
| 14:25 | 14:55 | 7.8.2 |
DESIGN OF AN EFFICIENT CLIMBING FLIGHT TRAJECTORY FOR A FLAPPING-WING MICRO AIR VEHICLE S.-G. Lee¹, H.-H. Yang¹, Y.-J. Han¹, J.-H. Han¹; ¹Korea Advanced Institute of Science and Technology, South Korea | ||||
| 14:55 | 15:25 | 7.8.3 |
THREE DIMENSIONAL PATH FOLLOWING CONTROL FOR A FIXED-WING UAV ON SO(3) WITH INPUT SATURATION B. Zhang¹, W. Li, The Second Representative Office of Air Force Armament Departmen, China; Z. Miao¹, Y. Zhang, Beijing System Design Institute of Mechanical-Electrical Enginee, China; ¹Northwestern Polytechnical University, China | ||||
| 15:25 | 15:55 | 7.8.4 |
COOPERATIVE PATH PLANNING AND ADJUSTING STRATEGY FOR UAVS WITH STRICT TIME CONSTRAINS Y. Lu¹, Q. Chen¹, Y. Wang¹; ¹National University of Defense technology, China | ||||
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| 13:55 | 14:25 | 8.8.1 |
DESIGN AND EXPERIMENTAL TESTING OF A DROOP NOSE MORPHING FOR ADVANCED REGIONAL AIRCRAFT A. De Gaspari¹, V. Cavalieri¹, S. Ricci¹; ¹Politecnico di Milano, Italy | ||||
| 14:25 | 14:55 | 8.8.2 |
STRUCTURAL ANALYSIS OF TWISTED/CURVED BEAMS USING A HYBRID METHOD A. Siami¹, F. Nitzsche¹; ¹Carleton University, Canada | ||||
| 14:55 | 15:25 | 8.8.3 |
EXPERIMENTAL AND NUMERICAL ANALYSIS OF A PRE-STRESSED TENSEGRITY MEMBRANE V.A.S. Paiva¹, L.H.S. Teixeira¹, J.H. Izuka¹, P.G. Ramos¹, P.R.G. Kurka¹; ¹UNICAMP, Brazil | ||||
| 15:25 | 15:55 | 8.8.4 |
MORPHING FORWARD WING SECTION SKIN DESIGN FOR A SAILPLANE CONSIDERING WING BENDING F. Sturm¹, M. Hornung¹; ¹Technical University of Munich, Germany | ||||
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| 13:55 | 14:25 | 9.8.1 |
THERMODYNAMIC POTENTIAL OF TURBOFAN ENGINES WITH DIRECT COMBUSTION OF HYDROGEN A. Görtz, German Aerospace Center, Institute of Propulsion Technology, Germany; D. Silberhorn, German Aerospace Center, Institute of System Architectures in Ae, Germany | ||||
| 14:25 | 14:55 | 9.8.2 |
THE INFLUENCE OF THE VANE LEAN ON THE FLOW IN A TURBINE REAR STRUCTURE V. Vikhorev¹, V. Chernoray¹, A.M. Zuher², J. Larsson²; ¹Chalmers University of Technology, Sweden ;²GKN Aerospace Engine Systems, Sweden | ||||
| 14:55 | 15:25 | 9.8.3 |
DEVELOPMENT OF THE LOW-COST AND LIMITED SPACE SEA-LEVEL RAM AIR TEST (RAT) MACH 0.8 SYSTEM T.-G. Nguyen¹, Q.-H. Nghiem¹, Q.-H. Nguyen¹, N.-V. Nguyen¹, D.-L. Chu¹, P.-M. Nguyen¹; ¹Viettel Aerospace Institute, Vietnam | ||||
| 15:25 | 15:55 | 9.8.4 |
ANALYSIS OF THE OPERATION OF THE PULSEJET ENGINE J. Tegner, FOI, Sweden | ||||
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| 13:55 | 14:25 | 10.8.1 |
ESTIMATION OF STEPWISE VARYING WIND BASED ON DERIVATIVE ESTIMATION OF AIRCRAFT USING SLIDING WINDOW RECURSIVE LEAST SQUARES METHOD H.S. Luu¹, Y. Ochi¹; ¹National Defense Academy, Japan | ||||
| 14:25 | 14:55 | 10.8.2 |
A GENERALISED MULTI-OBJECTIVE ISLAND MODEL FOR FLIGHT CONTROL SYSTEM CLEARANCES P. Piprek¹, P.M. Dias¹, D. Schwalb¹; ¹Airbus Defence and Space GmbH, Germany | ||||
| 14:55 | 15:25 | 10.8.3 |
STATISTICAL DATA SELECTION FOR BETTER FLIGHT CHARACTERISTIC MODELING M. Naruoka¹, T. Ninomiya¹; ¹Japan Aerospace Exploration Agency, Japan | ||||
| 15:25 | 15:55 | 10.8.4 |
RESEARCH ON SERVO CONTROL METHOD AND DAMPING CHARACTERISTICS OF ACTIVE CONTROL DEVICE L. Yao¹, H. Yu¹, Z. Zhao¹, J. Zheng¹; ¹Shenyang Aircraft Design and Research Institute, China | ||||
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| 13:55 | 14:25 | 11.8.1 |
VIRTUAL RECONFIGURATION AND ASSESSMENT OF AIRCRAFT CABINS USING MODEL-BASED SYSTEMS ENGINEERING M. Fuchs¹, F. Beckert¹, F. Rauscher¹, C. Goetz¹, J. Biedermann¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany | ||||
| 14:25 | 14:55 | 11.8.2 |
MORE ELECTRIC AIRPLANE: CASE STUDY STOCKHOLM - COPENHAGEN A. Johansson, Saab Aeronautics, Sweden; M. Yildiz¹, L. Bertling-Tjernberg¹; ¹Royal Institute of Technology (KTH), Sweden | ||||
| 14:55 | 15:25 | 11.8.3 |
HMI-HUFLAB – A BRAZILIAN - SWEDISH INITIATIVE IN HUMAN FACTORS FOR AERONAUTICS E. Villani¹, J. Alfredsson², M. Bång³, B. Johansson³, U. Anderini², D. Arjoni¹; ¹Aeronautics Institute of Technology (ITA), Brazil ;²SAAB AB, Sweden ;³Linköping University, Sweden | ||||
| 15:25 | 15:55 | 11.8.4 |
CRITICALITY AND COMFORT ZONE SUPPORTING DESIGN CHOICES TO ACHIEVE SUSTAINABLE REQUIREMENTS: THE CASE OF ELECTRIC AIRCRAFT L. Pereira, Federal University of ABC, Brazil; P. Krus, Linköping University, Sweden | ||||
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| 13:55 | 14:25 | 12.8.1 |
PRELIMINARY STUDY ON A FLUIDIC DEVICE SUPPORTING AIRCRAFT-FLIGHT CONTROL W. Stalewski, Lukasiewicz Research Network- Institute of Aviation, Poland | ||||
| 14:25 | 14:55 | 12.8.2 |
EXPERIMENTS TO INVESTIGATE LIFT PRODUCTION MECHANISMS ON OSCILLATING TRAILING-EDGE FLAPS M. Bremm¹, R. Hörnschemeyer¹, E. Stumpf¹; ¹RWTH Aachen University, Germany | ||||
| 14:55 | 15:25 | 12.8.3 |
IMPROVING STALL CHARACTERISTICS OF UCAV WING WITH VORTEX GENERATORS P. Eliasson, Saab, Sweden; A. Rizzi¹, J. Oppelstrup¹, M. Zhang, Airinnova AB, Sweden; ¹KTH, Sweden | ||||
| 15:25 | 15:55 | 12.8.4 |
OPTIMIZATION STUDY ON THE FLOW SEPARATION CONTROL USING A SAWTOOTH PLASMA ACTUATOR L. Wang, Beihang University, China; C.W. Wong¹, Y. Zhou¹; ¹Harbin Institute of Technology, China | ||||
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| 13:55 | 14:25 | 13.8.1 |
REDUCED TRANSMISSION RISKS FOR PASSENGER OPERATIONS DURING COVID-19 PANDEMIC M. Schultz, Universität der Bundeswehr München, Germany; M. Soolaki, University of Westminster, United Kingdom; O. Michler, Dresden University of Technology, Germany; E. Itoh, University of Tokyo, Japan | ||||
| 14:25 | 14:55 | 13.8.2 |
QUANTUM ARRIVAL AND DEPARTURE MANAGEMENT N. Yoshikawa, Mitsubishi Electric, Japan | ||||
| 14:55 | 15:25 | 13.8.3 |
V/A-R AIR GESTURES HMI INTERACTION IN AIRPORT CONTROL TOWERS S. Bagassi¹, M. Corsi¹, F. Galuppi¹; ¹University of Bologna, Italy | ||||
| 15:25 | 15:55 | 13.8.4 |
DESIGN & VALIDATION OF A FLIGHT CENTRIC WORKLOAD MODEL INCLUDING ATC TASK CHANGE & CONSIDERING INFLUENCING FACTORS T. Finck¹, M.-C. Névir, Technische Universität Dresden, Germany; C. Kluenker¹; ¹German Aerospace Center, Germany | ||||
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| 13:55 | 14:25 | 14.8.1 |
MEASUREMENT OF NOISE AND INDOOR CLIMATE ON BOARD A TURBOPROP AIRPLANE FLIGHT B. Müller¹, A. Lindner¹, V. Norrefeldt¹, Y. Song, TU Delft, Netherlands; N. Mansfield, Nottingham Trent University, United Kingdom; P. Vink, vhp Human Performance, Netherlands; ¹Fraunhofer IBP, Germany | ||||
| 14:25 | 14:55 | 14.8.2 |
USE OF THE FLIGHT TEST FACILITY MOCK-UPS IN THE EUROPEAN CLEAN SKY 2 PROGRAM V. Norrefeldt¹, F. Mayer¹, A. Pathak¹, M. Pschirer¹, M. Kienberger¹, A. Lindner¹, S. Johann¹, A. Nagele-Renzl¹, M. Buschhaus¹, G. Grün¹; ¹Fraunhofer IBP, Germany | ||||
| 14:55 | 15:25 | 14.8.3 |
COMPUTATIONAL STUDY OF AIRFLOW AND DISPERSION OF AIRBORNE PATHOGENS INSIDE AN AIRCRAFT CABIN C.L.S. Raposo¹, J.M.M. Sousa¹; ¹IDMEC, Instituto Superior Técnico, Portugal | ||||
| 15:25 | 15:55 | 14.8.4 |
IMPACT OF MOTION-DEPENDENT ERRORS ON THE ACCURACY OF AN UNAIDED STRAPDOWN INERTIAL NAVIGATION SYSTEM K. Borodacz¹, C. Szczepanski¹; ¹Lukasiewicz Research Network - Institute of Aviation, Poland | ||||
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| 16:15 | 16:45 | 1.9.1 |
SYSTEM LEVEL STUDIES FOR NASA - MODEL DEVELOPMENT TOWARD ZERO EMISSIONS J. Tai, Georgia Tech, United States | ||||
| 16:45 | 17:15 | 1.9.2 |
TRANSONIC TRUSS-BRACED WING VISION VEHICLE TECHNOLOGY MATURATION N.A. Harrison, Boeing Research & Technology, United States; G.M. Gatlin, NASA Langley Research Center, United States; E.D. Dickey¹, A.M. Malone¹; ¹Boeing Commercial Airplanes, United States | ||||
| 17:15 | 17:45 | 1.9.3 |
AN INNOVATIVE HYDROGEN-POWERED PROPULSION SYSTEM FOR SINGLE-AISLE AIRCRAFT W. Orisamolu, United States | ||||
| 17:45 | 18:15 | 1.9.4 |
JETZERO BWB ENABLING TECHNOLOGIES M. Page, United States; J. Vassberg, United States | ||||
| 18:15 | 18:45 | 1.9.5 |
JETZERO BWB ENABLING TECHNOLOGIES M. Page, United States; J. Vassberg, United States | ||||
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| 16:15 | 16:45 | 2.9.1 |
DESIGN AND ECO-EFFICIENCY ASSESSMENT OF A PEOPLE-MOVER AIRCRAFT IN COMPARISON TO STATE-OF-THE-ART NARROW BODY AIRCRAFT S. Wöhler¹, J.-N. Walther¹, W. Grimme¹; ¹German Aerospace Center (DLR), Germany | ||||
| 16:45 | 17:15 | 2.9.2 |
MINIMIZING THE CLIMATE IMPACT OF THE NEXT GENERATION AIRCRAFT USING NOVEL CLIMATE FUNCTIONS FOR AIRCRAFT DESIGN K. Radhakrishnan, 1Institute of Air Transportation Systems, TUHH, Germany; K. Deck¹, P. Proesmans¹, F. Linke², F. Yin¹, V. Grewe¹, R. Vos¹, B. Lührs², M. Niklaß², I. Dedoussi¹; ¹Delft University of Technology, Netherlands ;²Air Transportation Systems, DLR, Germany | ||||
| 17:15 | 17:45 | 2.9.3 |
PROPELLER AIRCRAFT DESIGN OPTIMIZATION FOR CLIMATE IMPACT REDUCTION R. Thijssen¹, P. Proesmans¹, R. Vos¹; ¹Delft University of Technology, Netherlands | ||||
| 17:45 | 18:15 | 2.9.4 |
AIRCRAFT FLEET MODELS USING A BOTTOM-UP APPROACH FOR SIMULATING AVIATION TECHNOLOGICAL PROSPECTIVE SCENARIOS S. Delbecq¹, T. Planès¹, M. Delavenne¹, V. Pommier-Budinger¹, A. Joksimovic¹; ¹ISAE-SUPAERO, France | ||||
| 18:15 | 18:45 | 2.9.5 |
SUSTAINABLE AVIATION FOR SWEDEN - TECHNOLOGY & CAPABILITY ASSESSMENT TARGETING 2045 C. Jouannet, Saab Aeronautics, Sweden; I. Staack¹, T. Grönstedt², X. Zhao², P. Krus¹, A. Lundbladh, GKN Aerospace, Sweden; B. Nagel, DLR, Germany; ¹Linköpings University, Sweden ;²Chalmers, Sweden | ||||
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| 16:15 | 16:45 | 3.9.1 |
SORA-BASED RISK ASSESSMENT FOR CARGO UNMANNED AERIAL VEHICLES IN THE UAM FRAMEWORK L. Babetto¹, B. Kniebel¹, E. Stumpf¹; ¹ILR, RWTH Aachen University, Germany | ||||
| 16:45 | 17:15 | 3.9.2 |
MEDIUM SIZE UAV AS TEST PLATFORM FOR NEW TECHNOLOGIES J. Mieloszyk¹, A. Tarnowski¹, A. Kwiek¹, R. Topolewski¹, T. Goetzendorf-Grabowski¹; ¹Warsaw University of Technology, Poland | ||||
| 17:15 | 17:45 | 3.9.3 |
CONCEPTUAL DESIGN AND SIZING FOR A FIXED WING UAV FOR EXPLORATION OVER MARS P. Gupta, Manipal Institute of Technology, Manipal, India, India; R.S. Pant, Indian Institute of Technology Bombay, Mumbai, India, India | ||||
| 17:45 | 18:15 | 3.9.4 |
AN INVESTIGATION ON THE IMPROVEMENT FOR TANDEM WING PITCHING MOMENT CHARACTERISTICS X. Wang¹, T. Ma, Institude of Unmanned System, Beihang University, China; N. Qiao¹, J. Fu, SchoolofTransportationScienceandEngineering, Beihang University, China; ¹School of Aeronautic Science and Engineering, Beihang University, China | ||||
| 18:15 | 18:45 | 3.9.5 |
TASK ALLOCATION METHOD FOR COMPLEX RECONNAISSANCE AREA BY MULTIPLE UAVS Y. Yue¹, Y. Pei¹, P. Hou¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | ||||
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| 16:15 | 16:45 | 4.9.1 |
ENHANCING CFD PREDICTIONS FOR THE GRIPEN AIRCRAFT P. Eliasson¹, P. Weinerfelt¹, F. Bramkamp, NSC, Sweden; ¹Saab, Sweden | ||||
| 16:45 | 17:15 | 4.9.2 |
STUDY OF THE EFFECTS OF NUMERICAL MODEL ENHANCEMENTS FOR AEROSTRUCTURAL ANALYSIS IN TRANSONIC FLOWS J.A.A. Lyrio¹, J.L.F. Azevedo², D.A. Rade¹, R.G. da Silva², C. Breviglieri, Embraer, S. A., Brazil; ¹Instituto Tecnologico de Aeronautica, DCTA/ITA, Brazil ;²Instituto de Aeronautica e Espaço, DCTA/IAE/ALA, Brazil | ||||
| 17:15 | 17:45 | 4.9.3 |
A STATIC STABILITY COMPARISON OF WIND TUNNEL AND COMPUTATIONAL FLUID DYNAMICS METHODS L.K. Fitzgerald¹, A.J. Niven¹, P.C. Griffin¹; ¹University of Limerick, Ireland | ||||
| 17:45 | 18:15 | 4.9.4 |
EXTERNAL-INTERNAL AERODYNAMIC COUPLING ON A TURBOPROP ENGINE USING THE BODY-FORCE METHOD R. Moretti¹, J. Decours¹; ¹ONERA, France | ||||
| 18:15 | 18:45 | 4.9.5 |
DEVELOPMENT OF A CFD MODEL AND METHODOLOGY FOR THE INTERNAL FLOW SIMULATION IN A HYDROGEN-POWERED UAV A. Porcarelli, KTH - Royal Institute of Technology, Sweden | ||||
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| 16:15 | 16:45 | 5.9.1 |
WIND TUNNEL TEST OF A BLENDED WING BODY UNMANNED AERIAL VEHICLE R. Mariani¹, S. Suewatanakul¹, S. Ghika¹, L.A. Penela¹, P. Wennhage¹, B. Zang, University of Bristol, United Kingdom; ¹KTH Royal Institute of Technology, Sweden | ||||
| 16:45 | 17:15 | 5.9.2 |
WIND TUNNEL EXPERIMENT OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) AND BLACK KITE (MILVUS MIGRANS) N. Kishimoto, Setsunan University, Japan; D. Wada¹, M. Tamayama¹, Y. Iwami², N. Tomita², T. Ikeda³, Y. Tanahashi³, K. Katagiri, Osaka Research Institute of Science and Technology, Japan; ¹JAXA, Japan ;²Yamashina Institute for Ornithology, Japan ;³Chubu University, Japan | ||||
| 17:15 | 17:45 | 5.9.3 |
ANALYSIS OF LOW-SPEED AERODYNAMIC CHARACTERISTICS OF BUSEMANN BIPLANE AIRFOIL INSTALLED HIGH LIFT DEVICES T.D. Nguyen¹, M. Taguchi¹, M. Kashitani¹, K. Kusunose, Formerly Japan Aerospace Exploration Agency, Japan; ¹National Defense Academy of Japan, Japan | ||||
| 17:45 | 18:15 | 5.9.4 |
EXPERIMENTAL INVESTIGATION ON TRANSPORT AIRPLANE LONGITUDINAL STABILITY ENHANCEMENT IN CRITICAL ICING CONDITION L. Fan¹, T. Guo¹, L. Zhang¹, H. Zhang¹; ¹CARDC, China | ||||
| 18:15 | 18:45 | 5.9.5 |
INFLUENCE OF MANEUVERING PROCESS ON PERFORMANCE CHARACTERISTICS OF BELLY INLET OF AIRCRAFT B.-B. XU¹, C.J. Wu¹, F.Z. Sun¹, J.P. Tang¹, W.T. Xiong¹; ¹China Aerodynamics Research and Development Center, China | ||||
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| 16:15 | 16:45 | 7.9.1 |
FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSURE S. Olsson¹, B. Carlsson¹, B. Helgesen¹; ¹Quintus Technologies AB, Sweden | ||||
| 16:45 | 17:15 | 7.9.2 |
INFLUENCE OF KEYHOLE TIG WELDING PARAMETERS ON WELD GEOMETRY OF NEWLY-DEVELOPED SUPERALLOY VDM ALLOY 780 A. Ariaseta, Sweden; N. Sadeghinia, Sweden; J. Andersson, Sweden | ||||
| 17:15 | 17:45 | 7.9.3 |
USE OF FRICTION STIR WELDING ON PRIMARY STRUCTURES OF AIRCRAFTS INSTEAD OF RIVETED JUNCTION D. Desgaches, AIRBUS, France | ||||
| 17:45 | 18:15 | 7.9.4 |
EXPERIMENTAL INVESTIGATIONS ON TENSILE PROPERTIES OF ALUMINUM HONEYCOMB SANDWICH STRUCTURES WITH SINGLE-SIDED REPAIRING B. Yan¹, G. Zhang¹, M. Tong¹, L. Li¹, D. Yu¹, S. Zhu¹, Z. Wu², H. Wang², T. Jin, China Special Vehicle Research Institute, China; ¹Nanjing University of Aeronautics & Astronautics, China ;²Nanjing University of Aeronautics and Astronautics, China | ||||
| 18:15 | 18:45 | 7.9.5 |
RESEARCH ON THE DUCTILE FRACTURE OF AL7085 AND TC11 UNDER COMPLEX STRESS STATE Y.J. Liu, AVIC the First Aircraft Institute, China | ||||
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| 16:15 | 16:45 | 8.9.1 |
NONLINEAR VIBRATION-BUCKLING INVESTIGATION OF UNSTIFFENED AND STIFFENED STRUCTURES SUBJECTED TO MECHANICAL AND THERMAL LOADINGS R. Azzara¹, M. Filippi¹, A. Pagani¹, E. Carrera¹; ¹Politecnico di Torino, Italy | ||||
| 16:45 | 17:15 | 8.9.2 |
GROUND VIBRATION TESTING OF A HIGH ASPECT RATIO WING WITH REVOLVING CLAMP G. Dessena¹, D.I. Ignatyev¹, J.F. Whidborne¹, A. Pontillo, University of Bristol, United Kingdom; L. Zanotti Fragonara¹; ¹Cranfield University, United Kingdom | ||||
| 17:15 | 17:45 | 8.9.3 |
UPDATING OF JET TRAINER AIRCRAFT DYNAMIC MODEL TO RESULTS OF GROUND VIBRATION TEST J. Cecrdle, Czech Aerospace Research Centre (VZLU), Czech Republic | ||||
| 17:45 | 18:15 | 8.9.4 |
DYNAMIC STRESS SIMULATION AND ASYMMETRY STATOR DESIGN FOR A FAN BLISK Y. Liu¹, K. Xu, Aero Engine Academy of China, China; Y. Chen¹, Y. Wu¹, Q. Du¹, D. Mo¹; ¹AECC Shenyang Engine Research Institute, China | ||||
| 18:15 | 18:45 | 8.9.5 |
A NEW APPROACH TO SHAPING THE PUSHROD TUBE AS THE MAIN COMPONENT OF THE CONTROL SYSTEM, OPTIMIZATION, AND MANUFACTURING TECHNOLOGY. W. Grendysa, Warsaw University of Technology, Poland | ||||
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| 16:15 | 16:45 | 9.9.1 |
THE IMPACT OF REACTION MECHANISM COMPLEXITY IN LES MODELING OF LIQUID KEROSENE SPRAY COMBUSTION A. Åkerblom, Lund University, Sweden | ||||
| 16:45 | 17:15 | 9.9.2 |
NUMERICAL ANALYSIS OF PROPAGATION OF DETONATION WAVE PLUNGING ENTRY THE FUEL JET TRAIN INSIDE ROTATING DETONATION COMBUSTOR F. Wang¹, T. Mizukaki¹; ¹Tokai University, Japan | ||||
| 17:15 | 17:45 | 9.9.3 |
LES OF COMBUSTION DYNAMICS IN AN ETHYLENE-HYDROGEN-AIR RAMJET N. Zettervall¹, K. Nordin-Bates¹, C. Ibron¹, C. Fureby, Lund University, Sweden; ¹FOI, Sweden | ||||
| 17:45 | 18:15 | 9.9.4 |
HIGH PRESSURE HYDROGEN OXYGEN COMBUSTION KINETIC ASSESSMENT FOR AIR-BREATHING PROPULSION SUPERSONIC GREEN AVIATION G. Saccone¹, M. Marini¹; ¹Italian Aerospace Research Centre - CIRA, Italy | ||||
| 18:15 | 18:45 | 9.9.5 |
RESEARCH ON FLOW HEAT TRANSFER CHARACTERISTICS OF HEAT EXCHANGER BASED ON BIONIC FRACTAL STRUCTURE B.-W. Yu¹, X. Yu¹, M.-G. Cao¹, X.-Z. Zhang¹, C.-L. Zhang¹, H.-B. Ji, Institute of Metal Research, Chinese Academy of Sciences, China; W.-T. Tong, Avic GuZhou YongHong Aviation Machinery Co, China; ¹Shenyang Aeroengine Research Institute, China | ||||
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| 16:15 | 16:45 | 10.9.1 |
THE NEW RESEARCH AIRCRAFT ISTAR - EXPERIMENTAL FLIGHT CONTROL SYSTEM D. Niedermeier¹, K. Giese¹, D. Leißling¹; ¹DLR, Germany | ||||
| 16:45 | 17:15 | 10.9.2 |
RAPID PROTOTYPING IN AIRCRAFT DESIGN USING CFD, WIND TUNNEL AND FLIGHT TESTING R. Larsson¹, U. Ringertz, Royal Institute of Technology, KTH, Sweden; D. Lundström, Linköping University, LIU, Sweden; A. Sobron¹; ¹Saab Aeronautics, Sweden | ||||
| 17:15 | 17:45 | 10.9.3 |
SYNTHETIC AIR DATA - A COMPARATIVE PRACTICAL STUDY V.L.M. Veras, EMBRAER, Brazil; L.C.S. Góes, ITA, Brazil | ||||
| 17:45 | 18:15 | 10.9.4 |
FREE FLIGHT TEST IN HORIZONTAL WIND TUNNEL WITH POWERED AIRCRAFT J.-F. Wang¹, S.-G. Lu¹, S. Feng¹, M.-H. Wang¹; ¹AVIC Aerodynamics Research Institute, China | ||||
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| 16:15 | 16:45 | 11.9.1 |
THE AGILE 4.0 MBSE-MDAO DEVELOPMENT FRAMEWORK: OVERVIEW AND ASSESSMENT L. Boggero¹, T. Lefèbvre, ONERA/DTIS, France; J. Vankan, Royal Netherlands Aerospace Centre (NLR), Netherlands; B. Beijer, KE-works, Netherlands; V. Saluzzi, Bombardier Aviation, Canada; B. Nagel¹; ¹German Aerospace Center (DLR), Germany | ||||
| 16:45 | 17:15 | 11.9.2 |
EXPERIMENTAL INVESTIGATION OF FUEL SLOSH IN A GENERIC FIGHTER WING TANK CONFIGURATION L. Debschütz¹, A. Seefried², T. Westermeier¹, R. Kuchar², D. Schwalb¹; ¹Airbus Defence and Space, Germany ;²German Aerospace Center, Germany | ||||
| 17:15 | 17:45 | 11.9.3 |
COUPLING OF MODEL-BASED SYSTEMS ENGINEERING AND SAFETY ANALYSIS IN CONCEPTUAL AIRCRAFT SYSTEM DESIGN S.M. Lübbe¹, M. Schäfer¹, O. Bertram¹; ¹German Aerospace Center (DLR), Germany | ||||
| 17:45 | 18:15 | 11.9.4 |
ONTOLOGY-ASSISTED AIRCRAFT CONCEPT GENERATION L. Knöös Franzén¹, R. Chaitanya Munjulury¹, P. Krus¹; ¹Linköping University, Sweden | ||||
| 18:15 | 18:45 | 11.9.5 |
HYBRID ELECTRIC PROPULSION SYSTEM OPTIMIZATION FOR A COMMUTER AIRCRAFT P. Krus¹, I. Staack¹, A.A.M. Oliveira, Federal University of Santa Catharina, Brazil; ¹Linköping University, Sweden | ||||
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| 16:15 | 16:45 | 12.9.1 |
FIT FOR CHANGE - DLR STRATEGY TOWARDS ZERO-EMISSION AVIATION E. Campillo Borrás¹, M. Fischer¹, A. Kaysser-Pyzalla¹, A. Klöckner¹, D. Kügler¹, R. Mönig¹, B. Nagel¹, C.-C. Rossow¹, M. Wiedemann¹; ¹Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany | ||||
| 16:45 | 17:15 | 12.9.2 |
NOVEL PATHWAYS TO SUSTAINABLE AVIATION C. Voigt, Germany; M. Rapp, Germany; U. Herrmann, Germany | ||||
| 17:15 | 17:45 | 12.9.3 |
CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS A. Kuenz¹, J. Lieb¹, M. Rudolph¹, A. Volkert¹, D. Geister¹, N. Ammann¹, D. Zhukov¹, P. Feurich, FlyNex, Germany; J. Gonschorek¹, M. Gessner¹, T. Kraft¹, H. Hackbarth, KopterKraft OÜ, Estonia; G. Peklar, NXP Semiconductors, Germany; L. Schalk¹, D. Becker¹, D. Gerbeth¹, C. Zhu¹, O. Garcia Crespillo¹, K. Caprdja², H. Walther², Jan Pertz¹, Klaus Lütjens¹; ¹DLR, Germany ;²DFS, Germany | ||||
| 17:45 | 18:15 | 12.9.4 |
ELIMINATING CLIMATE IMPACT FROM AVIATION – REVIEW OF PROMISING AIRCRAFT CONCEPTS AND ENABLING TECHNOLOGY BRICKS J. Hartmann, German Aerospace Center (DLR), Germany | ||||
| 18:15 | 18:45 | 12.9.5 |
DESIGN,MANUFACTURING & CERTIFICATION STRATEGIES FOR INNOVATIVE HYDROGEN STORAGE SYSTEMS TO ENABLE ZERO EMISSION AVIATION M. Wiedemann¹, D. Wilckens¹, M. Kleineberg¹; ¹DLR, Germany | ||||
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| 16:15 | 16:45 | 13.9.1 |
CLUSTER STRUCTURE AND GATEWAY AVAILABILITY OF AD-HOC COMMUNICATION NETWORKS IN THE NORTH ATLANTIC AIRSPACE T. Marks¹, A. Hillebrecht¹; ¹German Aerospace Center, Germany | ||||
| 16:45 | 17:15 | 13.9.2 |
DEMAND PATTERN INFLUENCE ON RELATION OF TURNAROUND DURATION AND GATE OCCUPATION DEPENDING ON AVAILABLE RESOURCES M. Jameel, DLR, Germany | ||||
| 17:15 | 17:45 | 13.9.3 |
ASSESSMENT OF REAL-TIME DATA TRANSMISSION VIA AD-HOC COMMUNICATION NETWORKS IN THE NORTH ATLANTIC OCEANIC AIRSPACE A. Hillebrecht¹, T. Marks¹, V. Gollnick, Hamburg University of Technology, Germany; ¹German Aerospace Center, Air Transportation Systems, Germany | ||||
| 17:45 | 18:15 | 13.9.4 |
AIR TRAFFIC SIMULATION ACROSS FIR IN JAPAN USING CELLULAR AUTOMATON K. Sekine¹, T. Tatsukawa¹, K. Fujii¹, E. Itoh, The University of Tokyo, Japan; ¹Tokyo University of Science, Japan | ||||
| 18:15 | 18:45 | 13.9.5 |
OPTIMIZATION OF AIRCRAFT FLIGHT PATHS CONSIDERING THE CONFLICTING PARAMETERS OF ECONOMY AND SAFETY T. Nagashima¹, M. Ding, Institutes of Innovation for Future Society, Nagoya University, Japan; K. Fujii¹, K. Takeda¹; ¹Graduate School of Informatics, Nagoya University, Japan | ||||
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| 16:15 | 16:45 | 14.9.1 |
ENERGY-BASED SYSTEM ARCHITECTURE DESIGN - ENVIRONMENTAL CONTROL SYSTEM A. Joksimovic¹, X. Carbonneau¹, F. Brazier, Delft University of Technology, Netherlands; R. Vingerhoeds¹; ¹ISAE-SUPAERO, France | ||||
| 16:45 | 17:15 | 14.9.2 |
METHODOLOGY FOR THE AUTOMATED PRELIMINARY CERTIFICATION OF ON-BOARD SYSTEMS ARCHITECTURES THROUGH REQUIREMENTS ANALYSIS C. Cabaleiro¹, M. Fioriti, Politecnico di Torino, Italy; L. Boggero¹; ¹German Aerospace Center (DLR), Germany | ||||
| 17:15 | 17:45 | 14.9.3 |
A SYSTEM INTEGRATOR’S PERSPECTIVE ON VEHICLE SYSTEM EVALUATION AT THE AIRCRAFT CONCEPT STAGE A. Drego¹, S. Steinkellner¹; ¹Saab AB, Sweden | ||||
| 17:45 | 18:15 | 14.9.4 |
EXTENSIBLE AIRCRAFT FUSELAGE MODEL GENERATION FOR A MULTIDISCIPLINARY, MULTI-FIDELITY CONTEXT J.-N. Walther¹, C. Hesse¹, J. Biedermann¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany | ||||
| 18:15 | 18:45 | 14.9.5 |
MATHEMATICAL MODELLING AND ANALYSIS OF THERMAL MANAGEMENT SYSTEM ARCHITECTURE FOR HYPERSONIC AIRCRAFT S. Nambiar¹, D. Ferreto¹; ¹Politecnico di Torino, Italy | ||||
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| 10:00 | 10:30 | 1.10.1 |
CLEAN SKY 2 PROGRAMME OVERVIEW S. Dubois, Clean Aviation JU, Belgium | ||||
| 10:30 | 11:00 | 1.10.2 |
SUSTAINABLE TECHNOLOGIES FOR COMMERCIAL AIRCRAFT OF TOMORROW - INTEGRATED MULTIFUNCTIONAL FUSELAGE DEMONSTRATOR Y.C. Roth, Airbus, Germany | ||||
| 11:00 | 11:30 | 1.10.3 |
OPEN FAN ENGINE ARCHITECTURE FOR NEXT GENERATION SMR C. Diette, Safran Aircraft Engines, France | ||||
| 11:30 | 12:00 | 1.10.4 |
PROGRESS IN WING DESIGN, STATUS AND PERSPECTIVES J. Lery, Dassault Aviation, France; M. Werner, Airbus, Germany; E. Coustols, ONERA, France | ||||
| 12:00 | 12:30 | 1.10.5 |
THE CLEAN SKY 2 TECHNOLOGY EVALUATOR 1ST GLOBAL ASSESSMENT J.-F. Brouckaert, Belgium | ||||
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| 10:00 | 10:30 | 2.10.1 |
COMBINED APPLICATION OF HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER IN PRELIMINARY AIRCRAFT DESIGN T. Effing¹, V. Schmitz¹, F. Schültke¹, F. Peter, Bauhaus Luftfahrt e.V, Germany; E. Stumpf¹; ¹RWTH Aachen University, Germany | ||||
| 10:30 | 11:00 | 2.10.2 |
CLEAN-SKY 2 LARGE PASSENGER AIRCRAFT PLATFORM 1 ADVANCED ENGINE AND AIRCRAFT CONFIGURATIONS D. Kierbel, AIRBUS, France | ||||
| 11:00 | 11:30 | 2.10.3 |
AERODYNAMIC DESIGN AND ANALYSIS OF HLFC WINGS WITHIN THE EUROPEAN PROJECT HLFC-WIN T. Streit¹, M. Kruse¹, T. Kilian¹, J. v. Geyr, DLRK, Germany; I. Petropoulos, ONERA, France; ¹DLR, Germany | ||||
| 11:30 | 12:00 | 2.10.4 |
ECONOMICS OF SUSTAINABLE REGIONAL AIR MOBILITY P. De Felipe¹, D. Yang¹; ¹Imperial College London, United Kingdom | ||||
| 12:00 | 12:30 | 2.10.5 |
TOWARD A GREENER AIRCRAFT ARCHITECTURE F. Vidal de Saint Jean, Dassault Aviation, France | ||||
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| 10:00 | 10:30 | 3.10.1 |
SCALABILITY ANALYSIS OF RADICAL TECHNOLOGIES TO VARIOUS AIRCRAFT CLASS - PART I: INITIAL DESIGNS M.F.M. Hoogreef¹, V.O. Bonnin¹; ¹Delft University of Technology, Netherlands | ||||
| 10:30 | 11:00 | 3.10.2 |
SCALABILITY ANALYSIS OF RADICAL TECHNOLOGIES TO VARIOUS AIRCRAFT CLASS - PART II: SENSITIVITY ANALYSIS V.O. Bonnin¹, M.F.M. Hoogreef¹; ¹Delft University of Technology, Netherlands | ||||
| 11:00 | 11:30 | 3.10.3 |
REGIONAL TRANSPORT AIRCRAFT DESIGN USING TURBO-ELECTRIC DISTRIBUTED PROPULSION (TEDIP) SYSTEM V. Polepeddi¹, P. Raj¹, M. Emeneth, PACE America, United States; ¹Virginia Tech, United States | ||||
| 11:30 | 12:00 | 3.10.4 |
ARRIVING AT CERTIFIABLE NOVEL AIRLINER USING LIQUID HYDROGEN & EFFICIENCY METRICS R.K. Nangia, Nangia, United Kingdom; L. Hyde, Consulting, United Kingdom | ||||
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| 10:00 | 10:30 | 4.10.1 |
STEADY-STATE AERODYNAMICS TIP GAP INFLUENCE IN A TRANSONIC LINEAR CASCADE AT NEAR STALL C. Tavera Guerrero¹, N. Glodic¹, H. Mårtensson, GKN Aerospace Sweden AB, Sweden; ¹KTH, Sweden | ||||
| 10:30 | 11:00 | 4.10.2 |
LARGE EDDY SIMULATION OF A LYNX HELICOPTER LANDING IN THE BARROSO CORVETTE SHIP D.M. Pio¹, C.F. Rafael¹, P.S.C. Villela¹, G.A.L. da Silva¹, M. Ferro, Laboratorio Nacional de Computacao Cientifica -, Brazil; M.J.M. Guedes, Marinha do Brasil, Brazil; ¹Aerothermal Solutions - ATS, Brazil | ||||
| 11:00 | 11:30 | 4.10.3 |
NUMERICAL INVESTIGATION OF ROTORCRAFT PRESSURE ERROR CORRECTION BY UTILIZATION OF AIR DAMS A.-O. Sezer¹, M. Elfarra, Ankara Y?ld?r?m Beyaz?t University, Turkey; H.-I. Ünlü¹; ¹Turkish Aerospace, Turkey | ||||
| 11:30 | 12:00 | 4.10.4 |
TRANSONIC FLOW OVER DELTA WING USING ENTROPIC LATTICE BOLTZMANN METHOD M. Dhake¹, C. Thantanapally¹, S. Arcidiacono¹, S. Ansumali¹; ¹SankhyaSutra Labs Ltd, India | ||||
| 12:00 | 12:30 | 4.10.5 |
CFD TAKE-OFF ANALYSIS OF A SEAPLANE HULL THROUGH A DYNAMIC MULTIPHASE MODEL M. Sinisi¹, G. Cantanna¹, G. Occhipinti¹, A. Caramazza¹, G. Dilonardo¹, E. Cestino¹; ¹Politecnico di Torino, Italy | ||||
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| 10:00 | 10:30 | 5.10.1 |
AERONAUTICAL CFD AND TURBULENCE - PROGRESS AND CHALLENGES A. Rizzi¹, D. Henningson¹; ¹KTH, Sweden | ||||
| 10:30 | 11:00 | 5.10.2 |
AERONAUTICAL CFD AND TURBULENCE - PROGRESS AND CHALLENGES PART 2 A. Rizzi¹, D. Henningson¹; ¹KTH, Sweden | ||||
| 11:00 | 11:30 | 5.10.3 |
OPEN CAVITY SIMULATIONS UNDER SIDESLIP FLOW CONDITIONS K. Rajkumar¹, J. Radtke¹, E. Tangermann¹, M. Klein¹; ¹University of the Bundeswehr Munich, Germany | ||||
| 11:30 | 12:00 | 5.10.4 |
APPLICATION OF GENETIC PROGRAMMING AND ARTIFICIAL NEURAL NETWORK APPROACHES FOR RECONSTRUCTION OF TURBULENT JET FLOW FIELDS V. Gryazev, United Kingdom; U. Armani, United Kingdom; A.R. Murali, France; A.P. Markesteijn, United Kingdom; S.A. Karabasov, United Kingdom; V. Toropov, United Kingdom; S.E. Naghibi, United Kingdom; V. Riabov, Japan | ||||
| 12:00 | 12:30 | 5.10.5 |
UNSTEADY SIMULATIONS OF MASSIVELY SEPARATED FLOW AROUND NACA0021 AIRFOIL USING A TRANSITIONAL IDDES MODEL Y. Wang, China; S.-Q. Zhang, China; W.-P. Song, China; Z.-H. Han, China | ||||
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| 10:00 | 10:30 | 6.10.1 |
EXPERIMENTAL INVESTIGATIONS OF AN AEROELASTIC WIND TUNNEL MODEL FOR TAIL BUFFETING ANALYSIS J. Stegmüller¹, S. Hayböck¹, P. Hartl¹, C. Breitsamter¹; ¹Technical University of Munich, Germany | ||||
| 10:30 | 11:00 | 6.10.2 |
OPTIMIZATION OF AN ACTIVE DAMPING SYSTEM FOR USE WITH A SINGLE STRUT MOUNT J. Pereira, National Research Council Canada, Canada | ||||
| 11:00 | 11:30 | 6.10.3 |
WIND-TUNNEL TEST ON LEADING-EDGE VORTEX OF LOW-ASPECT-RATIO FLAPPING PLATES J.-S. Han¹, C. Breitsamter¹; ¹Technical University of Munich, Germany | ||||
| 11:30 | 12:00 | 6.10.4 |
POWERED WIND TUNNEL TESTING WITH HYDRAULIC MOTORS D. Steiling¹, P. Aschwanden¹, J. Müller¹, T. Jax¹; ¹RUAG AG, Switzerland | ||||
| 12:00 | 12:30 | 6.10.5 |
EXPERIMENTING ROTORCRAFT FLIGHT IN COMPLEX ENVIRONMENTAL CONDITIONS USING THE WIND TUNNEL: HELICOPTER SHIP LANDING CASE N. Taymourtash¹, A. Zanotti¹, G. Gibertini¹, G. Quaranta¹; ¹Politecnico di Milano, Italy | ||||
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| 10:00 | 10:30 | 7.10.1 |
INCREMENTAL FATIGUE DAMAGE MODEL: APPLICATION TO PLANE PROBLEMS WITH NON-PROPORTIONAL LOADING Z. Kapidzic¹, S.B. Lindström, Linköping University, Sweden; J. Lundgren¹; ¹Saab AB, Sweden | ||||
| 10:30 | 11:00 | 7.10.2 |
FATIGUE OF NOTCHED STANDARD SPECIMENS – THE INFLUENCE OF THE STRESS GRADIENT ON THE S-N CURVE IN AL2024 S. Sieberer¹, J. Homan, Fatec Engineering, Netherlands; M. Schagerl¹; ¹Johannes Kepler University Linz, Austria | ||||
| 11:00 | 11:30 | 7.10.3 |
FATIGUE LIFE ENHANCEMENT OF TYPICAL AERONAUTICAL JOINTS BY MEANS OF ENGINEERED RESIDUAL STRESSES D. Fanteria¹, L. Boni ¹, F. Bovecchi¹, D.O. Busse, IRBUS Operations GmbH, Germany; D. Furfari, AIRBUS Operations GmbH, Germany; ¹University of Pisa, Italy | ||||
| 11:30 | 12:00 | 7.10.4 |
FATIGUE CHARACTERIZATION OF ADHESIVE JOINTS IN AEROPLANES-THE DEVELOPMENT OF A NEGATIVE LOAD RATIO (R<0) TESTING METHOD O. Orell¹, J. Jokinen¹, M. Kanerva¹; ¹Tampere University, Finland | ||||
| 12:00 | 12:30 | 7.10.5 |
FATIGUE DAMAGE MODEL OF HIGH TEMPERATURE POLYMER COMPOSITES IN AERO-ENGINES V.R. Pakkam Gabriel¹, P. Fernberg¹; ¹Luleå University of Technology, Sweden | ||||
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| 10:00 | 10:30 | 8.10.1 |
DEVELOPMENT OF A PREDICTIVE DAMAGE METHODOLOGY FOR HYBRID WING BODY AIRCRAFT STRUCTURES H. Raza¹, C. Harey¹, P. Vaghela¹, J. Bayandor¹; ¹CRASH Lab, University at Buffalo, United States | ||||
| 10:30 | 11:00 | 8.10.2 |
NUMERICAL ANALYSIS AND COMPARISON WITH RESULTS OF FRACTURE TESTS OF LUG MANUFACTURED IN COMPOSITE MATERIAL G.C. Fonseca, Embraer Minas Gerais, Brazil; S.F.M. Almeida, Instituto Tecnológico de Aeronáutica, Brazil | ||||
| 11:00 | 11:30 | 8.10.3 |
ENHANCEMENT OF FLEXIBLE STRATEGY FOR AUGMENTING DESIGN POINTS FOR COMPUTER EXPERIMENTS AND APPLICATION TO A MDO OF A FAN-BLISK A. Tamkan¹, P. Flassig¹, M. Meyer, Rolls-Royce Deutschland, Germany; ¹Technische Hochschule Brandenburg, Germany | ||||
| 11:30 | 12:00 | 8.10.4 |
TRANSIENT AND FREE-VIBRATION ANALYSIS OF LAMINATED SHELLS THROUGH THE DISCONTINUOUS GALERKIN METHOD G. Guarino¹, V. Gulizzi¹, A. Milazzo¹; ¹1University of Palermo, Department of Engineering, Italy | ||||
| 12:00 | 12:30 | 8.10.5 |
DESIGN AND STUDY ON NOISE REDUCTION PROPERTIES OF A MULTISTAGE BIONIC MEMBRANE-TYPE ACOUSTIC METAMATERIAL X.J. Zhang¹, D. Guo¹, H.Y. Huang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | ||||
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| 10:00 | 10:30 | 9.10.1 |
AEROELASTIC TAILORING OF COMPRESSOR BLADES A.-P. Chalke¹, N. Glodic¹, M. Gutierrez Salas¹; ¹KTH Royal Institute of Technology, Sweden | ||||
| 10:30 | 11:00 | 9.10.2 |
RAPID AEROACOUSTIC PLANFORM DESIGN OPTIMIZATION OF INSTALLED PROPELLERS T. Sinnige¹, W. de Gruijl¹, W. de Haan¹, G. Eitelberg¹; ¹Delft University of Technology, Netherlands | ||||
| 11:00 | 11:30 | 9.10.3 |
PERFORMANCE BENEFITS OF A FAN ON BLADE – FLADE – FOR A VARIABLE CYCLE ENGINE M. Assato, IAE, Brazil; A. Altar Inceer¹, L. Moraes¹, J. Takachi Tomita², C. Bringhenti², P. Bravo-Mosquera, USP, Brazil; D. Rosell, SAAB Aeronautcs, Sweden; T. Grönstedt¹; ¹Chalmers University, Sweden ;²ITA, Brazil | ||||
| 11:30 | 12:00 | 9.10.4 |
STATUS OF GKN AEROSPACE\'S ENGINE MODULE DEMONSTRATORS IN THE CLEAN SKY-2 PROJECT R. Lundberg¹, L. Ellbrant¹, P. Johansson¹, U. Johansson¹, M. Billson¹, B. Gustafsson¹; ¹GKN Aerospace Sweden AB, Sweden | ||||
| 12:00 | 12:30 | 9.10.5 |
STUDY ON THE OBJECTIVE FUNCTION OF THE PROFILED ENDWALL OPTIMIZATION OF AN EMBEDDED COMPRESSOR STATOR J. Wang¹, D. Meng¹, D. Feng¹, Q. Zhao¹; ¹Shenyang Engine Research Institute of AECC, China | ||||
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| 10:00 | 10:30 | 10.10.1 |
INCREMENTAL NONLINEAR DYNAMIC CONTROL WITH SPARSE NON-PARAMETRIC BAYESIAN REGRESSION OF DAMAGED AIRCRAFT L. Kim¹, D. Lee¹, H. Bang¹; ¹Korea Advanced Institute of Science and Technology, South Korea | ||||
| 10:30 | 11:00 | 10.10.2 |
FAULT-TOLERANT CONTROL FOR AIRCRAFT WITH STRUCTURAL DAMAGE USING GAUSSIAN PROCESS REGRESSION D.-W. Lee¹, L.-S. Kim¹, H.-C. Bang¹; ¹KAIST, South Korea | ||||
| 11:00 | 11:30 | 10.10.3 |
EFFECTIVENESS ANALYSIS OF DOBC Q-FILTER PARAMETERS FOR A MULTICOPTER UAV H.J. Jeaong¹, C. Roh¹, Y.H. Jang¹, J.Y Suk¹, S.K. Kim¹; ¹Department of Aerospace Engineering, Chungnam National Universit, South Korea | ||||
| 11:30 | 12:00 | 10.10.4 |
CONVEX PROGRAMMING-BASED OPTIMAL THREE-DIMENSIONAL MID-COURSE GUIDANCE WITH LOSSLESS CONVEXIFICATION C.-G. Jung¹, C.-H. Lee¹, M.-J. Tahk¹; ¹KAIST, South Korea | ||||
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| 10:00 | 10:30 | 11.10.1 |
TOWARDS CORRECT-BY-CONSTRUCTION DESIGN OF SAFETY-CRITICAL EMBEDDED AVIONICS SYSTEMS I. Sander¹, I. Söderquist², M. Ekman², R. Jordao¹, F. Bahrami¹, R. Chen¹, A. Åhlander²; ¹KTH Royal Institute of Technology, Sweden ;²Saab AB, Sweden | ||||
| 10:30 | 11:00 | 11.10.2 |
CONCEPT LEVEL EXPLORATION OF IMA-BASED NETWORKED PLATFORMS WITH MIXED TIME-SENSITIVE COMMUNICATION REQUIREMENTS R. Saar de Moraes¹, S. Nadjm-Tehrani¹; ¹Linköping University, Sweden | ||||
| 11:00 | 11:30 | 11.10.3 |
SYSTEMS ARCHITECTING ASSISTANT (SARA) - ENABLING A SEAMLESS PROCESS CHAIN FROM REQUIREMENTS TO OVERALL SYSTEMS DESIGN N. Kuelper¹, J. Broehan¹, T. Bielsky¹, F. Thielecke¹; ¹Hamburg University of Technology, Germany | ||||
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| 10:00 | 10:30 | 13.10.1 |
ATCO STRATEGIES IN TACTICAL TBO: A SIMULATOR STUDY M. Nylin¹, J. Nilsson¹, J. Lundberg², M. Bång²; ¹LiU/LFV, Sweden ;²LiU, Sweden | ||||
| 10:30 | 11:00 | 13.10.2 |
TRAJECTORY-BASED OPERATIONS TO IMPROVE LONG-RANGE AIR TRAFFIC FLOW MANAGEMENT G. Enea, MIT Lincoln Laboratory, United States; J. Bronsvoort, Airservices Australia, Australia | ||||
| 11:00 | 11:30 | 13.10.3 |
ASSESSMENT OF ENERGY-EFFICIENT APPROACHES WITH INCREASED GLIDESLOPE ANGLES D. Vechtel¹, P. Pauly¹; ¹German Aerospace Center (DLR), Germany | ||||
| 11:30 | 12:00 | 13.10.4 |
COMPETITIVITY, STRATEGY AND VALUE ON AIRPORTS A METHOD OF DIAGNOSIS, SUGGESTIONS AND ACTIONS FOR INTERNATIONAL AIRPORTS WITH A CASE STUDY OF CNF A.H.O. Carvalho, Pontifícia Universidade Católica de Minas Gerais – PUC Minas, Brazil; E.M.M. Torga, Centro Universitário UNA, Brazil; F.R.V. Paiva, Universidade FUMEC - Fundação Mineira de Educação e Cultura, Brazil | ||||
| 12:00 | 12:30 | 13.10.5 |
AIRCRAFT MASS ESTIMATION USING CRUISE FLIGHT PROFILE R. Mori, ENRI, Japan | ||||
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| 10:00 | 10:30 | 14.10.1 |
MODEL-BASED SYSTEMS ENGINEERING FOR FUTURE DIGITAL FLIGHT LINES M.A. Kelly, Lockheed Martin Aeronautics, United States | ||||
| 10:30 | 11:00 | 14.10.2 |
GRAPH-BASED KNOWLEDGE REPRESENTATION AND ALGORITHMS FOR AIR AND MAINTENANCE OPERATIONS E. Olsson¹, O. Candell¹, P. Funk², R. Sohlberg², M. Castaño, Luleå University of Technology, Sweden; M. Gustafsson¹, P. Bladh¹; ¹Saab Aeronautics, Sweden ;²Mälardalen University, Sweden | ||||
| 11:00 | 11:30 | 14.10.3 |
AUGMENTED REALITY FOR AIRCRAFT FATIGUE NON-DESTRUCTIVE EVALUATION M.J. Scott¹, S. Koschel¹, W. Verhagen¹, O. Levinski, Defence Science and Technology Group, Australia; P. Marzocca¹; ¹RMIT University, Australia | ||||
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| 13:30 | 14:00 | 1.11.1 |
CLEAN AVIATION PROGRAMME RATIONALE AND OVERVIEW R. van Manen, Clean Aviation, Belgium | ||||
| 14:00 | 14:30 | 1.11.2 |
ULTRA-EFFICIENT AIRCRAFT AND PROPULSION ARCHITECTURES FOR LOW-EMISSION SHORT/MEDIUM RANGE [SMR] AIRCRAFT M. Calvo Blanco, Belgium | ||||
| 14:30 | 15:00 | 1.11.3 |
HYBRID-ELECTRIC AND FULL ELECTRIC ARCHITECTURES FOR LOW-EMISSION HYBRID-ELECTRIC REGIONAL [REG] AIRCRAFT A. Marino, Belgium | ||||
| 15:00 | 15:30 | 1.11.4 |
DISRUPTIVE TECHNOLOGIES TO ENABLE ZERO-CARBON HYDROGEN–POWERED [HPA] SHORT RANGE AIRCRAFT P. Trinchieri, Belgium | ||||
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| 13:30 | 14:00 | 2.11.1 |
AERODYNAMIC CHARACTERISTICS OF BOX WINGS FOR AN INNOVATIVE EVTOL CONFIGURATION E. Shima, Japan Aerospace Exploration Agency, Japan; K. Yonezawa, Central Research Institute of Electric Power Industry, Japan; R. Nishida¹, S. Honda¹, M. Sato¹; ¹Kogakuin University, Japan | ||||
| 14:00 | 14:30 | 2.11.2 |
IMPACT OF THE NUMBER OF WING STATIONS ON THE TWIST DISTRIBUTION OF A BWB CONCEPTUAL AIRCRAFT DESIGN IN A MDAO ENVIRONMENT TO MATCH TARGET LIFT DISTRIBUTION B. Fröhler¹, M. Iwanizki¹, P. Balack¹, J. Häßy¹, D. Silberhorn¹; ¹German Aerospace Center (DLR), Germany | ||||
| 14:30 | 15:00 | 2.11.3 |
CS2 – MANTA – MULTI-FUNCTIONAL FLAP MECHANISM OFFERING A SECOND DEGREE OF FREEDOM M. Desmet¹, J. Vervliet¹, D. De Wit¹, R. Seidler, Deutsches Zentrum Fuer Luft und Raumfahrt E.V., Germany; J. Docter, Netherlands Aerospace Centre, Netherlands; B. Everaert¹; ¹Asco Industries nv/sa, Belgium | ||||
| 15:00 | 15:30 | 2.11.4 |
INFLUENCES OF CHANGING THE INSTALLING POSITIONS OF MULTIPLE WINGLETS ON AERODYNAMIC CHARACTERISTICS E. Kobayashi¹, K. Chiba¹; ¹The University of Electro-Communications, Japan | ||||
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| 13:30 | 14:00 | 3.11.1 |
COOLING SYSTEM OF STRATOFLY HYPERSONIC VEHICLE: CONCEPTUAL DESIGN, NUMERICAL ANALYSIS AND VERIFICATION R. Scigliano¹, V. De Simone¹, R. Fusaro², D. Ferretto², M. Marini¹, N. Viola²; ¹Italian Aerospace Research Center - CIRA scpa, Italy ;²Politecnico di Torino (PoliTo), Italy | ||||
| 14:00 | 14:30 | 3.11.2 |
HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONS N. Viola¹, R. Fusaro¹, D. Ferretto¹, O. Gori¹, M. Marini², P. Roncioni², B.O. Cakir³, A.C. Ispir³, B.H. Saracoglu³; ¹Politecnico di Torino, Italy ;²CIRA, Italy ;³VKI, Belgium | ||||
| 14:30 | 15:00 | 3.11.3 |
LTO NOISE AND SONIC BOOM PREDICTIONS IN EARLY CONCEPTUAL DESIGN PHASES G. Piccirillo¹, S. Graziani¹, R. Fusaro¹, N. Viola¹; ¹Politecnico di Torino, Italy | ||||
| 15:00 | 15:30 | 3.11.4 |
SIMPLIFIED MODELS FOR THE PRELIMINARY AERODYNAMIC CHARACTERIZATION OF HIGH-SPEED VEHICLES TO SUPPORT MISSION ANALYSIS O. Gori, Politecnico di Torino, Italy | ||||
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| 13:30 | 14:00 | 4.11.1 |
ACCURATE TWO-DIMENSIONAL STEADY-STATES FOR THE SUPERSONIC FLOW OVER A COMPRESSION CORNER R. Santos¹, L. Alves¹, N. Cerulus², H. Quintanilha Jr², V. Theofilis²; ¹UFF, Brazil ;²UoL, United Kingdom | ||||
| 14:00 | 14:30 | 4.11.2 |
NUMERICAL MODELING OF LAMINAR-TURBULENT TRANSITION IN AN INTERCONNECTING COMPRESSOR DUCT A. Capitao Patrao¹, B. González Lozano¹, I. Jonsson¹, C. Xisto¹; ¹Chalmers University of Technology, Sweden | ||||
| 14:30 | 15:00 | 4.11.3 |
ANALYSIS OF A LAMINAR SEPARATION BUBBLE ON A NACA0009 AIRFOIL AT DIFFERENT BACKGROUND DISTURBANCE LEVELS J.S. Kern¹, A. Hanifi¹, D.S. Henningson¹; ¹FLOW, Department of Engineering Mechanics, KTH Royal Institute o, Sweden | ||||
| 15:00 | 15:30 | 4.11.4 |
A STUDY ON THE NUMERICAL SIMULATION OF FLOW TRANSITION INCLUDING CROSSFLOW EFFECTS A.R.S. Righi, ITA, Brazil; G.L.O. Halila¹, J.L.F. Azevedo¹; ¹IAE, Brazil | ||||
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| 13:30 | 14:00 | 5.11.1 |
COMPUTATIONALLY ECONOMICAL METHODS FOR LANDING GEAR NOISE SIMULATIONS R. Spencer, CFMS Ltd, United Kingdom; M. Allan, Zenotech Ltd, United Kingdom | ||||
| 14:00 | 14:30 | 5.11.2 |
PROPELLER AEROACOUSTIC MODELS IN VARIABLE-FIDELITY DESIGN OPTIMIZATION W. Klimczyk¹, A. Sieradzki¹; ¹Lukasiewicz Research Network - Institute of Aviation, Poland | ||||
| 14:30 | 15:00 | 5.11.3 |
NUMERICAL PREDICTION OF FOCUS BOOM GENERATED BY MANEUVERS S. Han¹, Y. Xu¹; ¹Chinese Aeronautical Establishment, China | ||||
| 15:00 | 15:30 | 5.11.4 |
IN-FLIGHT MEASUREMENTS AND ESTIMATION OF SONIC BOOM SIGNATURE OF SUPERSONIC AIRCRAFT L. Qu, China; S. Han, China; Y. Song, China; Y. Xu, China; Y. Zhang, China; Y. Wang, China | ||||
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| 13:30 | 14:00 | 6.11.1 |
WALL INTERFERENCE CORRECTIONS USING NONLINEAR LEAST-SQUARES OPTIMISATION S. Noel¹, D.M. Birch², J.J. Doherty², T. Tipnis¹; ¹QinetiQ, United Kingdom ;²University of Surrey, United Kingdom | ||||
| 14:00 | 14:30 | 6.11.2 |
A NEW FACILITY FOR HYPERSONIC FLOW SIMULATION DRIVEN BY A HIGH VELOCITY OXYGEN FUEL GUN A. Esposito, DEPT.OF INDUSTRIAL ENGINEERING UNIVERSITY OF NAPLES FEDERICO II, Italy; C. Allouis, STEMS-CNR, Italy; M. Lappa, Dept of Mech. and Aer.Engineering, University of Strathclyde, United Kingdom | ||||
| 14:30 | 15:00 | 6.11.3 |
RECENT ACTIVITIES ON FLOW QUALITY ASSESSMENT AT THE EUROPEAN TRANSONIC WINDTUNNEL J.H. You¹, M.C.N. Wright¹, H. Quix¹; ¹European Transonic Windtunnel GmbH, Germany | ||||
| 15:00 | 15:30 | 6.11.4 |
INVESTIGATION ON CORRECTION OF TUNNEL WALL INTERFERENCE FOR DYNAMIC AIRFOIL TEST IN LOW-SPEED WIND TUNNEL Y. Jiao, China; H. Zou, China; B. Chen, China; C. Xiao, China | ||||
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| 13:30 | 14:00 | 7.11.1 |
DEVELOPMENT OF MULTI-CANARD UAV FOR ACTIVE AEROELASTIC CONTROL TOWARD PSEUDO-SMALL SATELLITES N. Morita¹, S. Nakasuka¹, T. Tsuchiya¹, K. Takashima¹, Y. Taguchi¹, K. Suzuki¹, T. Koyama¹, R. Eto¹, I. Baba¹; ¹the University of Tokyo, Japan | ||||
| 14:00 | 14:30 | 7.11.2 |
INFLUENCE OF OVERALL LAYOUT DESIGN OF COMPOUND MULTI-ROTOR VEHICLES ON FLIGHT PERFORMANCE Y. Huang¹, M. Bando¹, S. Hokamoto¹; ¹Kyushu University, Japan | ||||
| 14:30 | 15:00 | 7.11.3 |
USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTION L.D. Jesus¹, A.J.D. Filho¹, M.A. Almeida¹, W. M. Martins¹, T.C. Pimenta¹, A.C.B. Ramos¹, L. A. Baldochi¹, L.O. Carvalho¹, P. Funk, Mälardalen University, Sweden; ¹Federal University of Itajubá, Brazil | ||||
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| 13:30 | 14:00 | 8.11.1 |
A PRELIMINARY STRUCTURAL DESIGN OF A FLEXIBLE FLYING DEMONSTRATOR P.J. González¹, G. Stavorinus¹, H. Shahi¹, Y.M. Meddaikar², S. Cumnuantip², A. Voß², T. Klimmek², W.R. Krüger², F.J. Silvestre¹; ¹TU-Berlin, Germany ;²DLR, Germany | ||||
| 14:00 | 14:30 | 8.11.2 |
DEVELOPMENT AND APPLICATIONS OF A VIRTUAL HYBRID PLATFORM FOR MULTISCALE ANALYSIS OF ADVANCED STRUCTURES OF AIRCRAFT (DEVISU) E. Carrera, Politecnico di Torino, Italy; U. Galvanetto, University of Padova, Italy; S. De Rosa, Università degli Studi di Napoli, Italy; P. Gardonio, University of Udine, Italy; A. Milazzo, Università degli Studi di Palermo, Italy; R. Vescovini, Politecnico di Milano, Italy; M. Zaccariotto, University of Padua, Italy | ||||
| 14:30 | 15:00 | 8.11.3 |
VIBRO-ACOUSTIC ANALYSIS OF MULTI-LAYER CYLINDRICAL SHELL-CAVITY SYSTEMS VIA CUF FINITE ELEMENTS M.C. Moruzzi¹, M. Cinefra, Poliecnico di Bari, Italy; S. Bagassi¹, E. Zappino, Politecnico di Torino, Italy; ¹Università di Bologna, Italy | ||||
| 15:00 | 15:30 | 8.11.4 |
WING LOADING PROCESS IN KNOWLEDGE-BASED AIRCRAFT DESIGN AND OPTIMIZATION FRAMEWORK S. Hosseini¹, H.R. Ovesy¹, M.A. Vaziri-Zanjani¹; ¹Amirkabir University of Technology, Iran | ||||
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| 13:30 | 14:00 | 9.11.1 |
TECHNOLOGY MATURATION IN CLEAN SKY 2 FOR NEXT GENERATION SMR ENGINE C. Diette, Safran Aircraft Engines, France; E. Obert, Safran, France; G. Marion, Safran Transmission Systems, France; H. De Franssu, Safran Nacelles, France; A. Frezet, Avio Aero, Italy; B. Walther, GE Deutschland, Germany; A. Sjunnesson, GKN Aeropsace Engie Systems, Sweden | ||||
| 14:00 | 14:30 | 9.11.2 |
NOVEL AIRCRAFT PROPULSION AND AVAILABILITY OF ALTERNATIVE, SUSTAINABLE AVIATION FUELS IN 2050 J. Kos¹, J. Posada-Duque², B. Peerlings¹, N. Ben Salah², N. Lim¹, W. Lammen¹, I. Stepchuk, TU Delft, Faculty of Technology and Policy Management, Netherlands; E. van der Sman¹, M. Palmeros-Parada²; ¹Royal Netherlands Aerospace Centre, Netherlands ;²TU Delft, Faculty of Applied Sciences, Netherlands | ||||
| 14:30 | 15:00 | 9.11.3 |
MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEM T. Grönstedt¹, C. Xisto¹, X. Zhao¹, I. Jonsson¹, A. Reinap², M. Genrup², N. Glodic³, M. Guiterrez Salas³, M. Lejon*, R. Avellan*, H. Mårtensson*; ¹Chalmers University, Sweden ;²Lund University, Sweden ;³Royal Institute of Technology, Sweden ;*GKN Aerospace, Sweden | ||||
| 15:00 | 15:30 | 9.11.4 |
LOW BPR TURBOFAN PERFORMANCE WITH POWER EXTRACTION D. Rosell, Saab Aeronautics, Sweden; T. Grönstedt, Chalmers Univerity of Technology, Sweden; P.D. Bravo-Mosquera¹, F. Martini Catalano¹; ¹University of Sao Paulo, Brazil | ||||
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| 13:30 | 14:00 | 10.11.1 |
ON LATERAL-LONGITUDINAL CONTROL COUPLING FOR SHORT- AND LONG-FUSELAGE BWB AIRCRAFT CONFIGURATIONS L.M.B.C. Campos, Instituto Superior Técnico, Universidade de Lisboa, Portugal; J.M.G. Marques, Universidade de Évora, Portugal | ||||
| 14:00 | 14:30 | 10.11.2 |
OPEN-LOOP SUBSPACE IDENTIFICATION OF A FLEXIBLE UNMANNED AERIAL SYSTEM R.C. Machado, Instituto de Fomento e Coordenação Industrial (IFI), Brazil; D.F.C. Zúniga, 2Universidade Estadual Paulista Júlio de Mesquita Filho, Brazil; A. Souza, Instituto Superior Técnico de Lisboa, Portugal; T. Rosado¹, L.C.S. Góes¹; ¹Instituto Tecnológico de Aeronáutica, Brazil | ||||
| 14:30 | 15:00 | 10.11.3 |
LATERAL-DIRECTIONAL AERODYNAMIC MODELLING FOR NUMERICAL RESULTS USING NEURO-FUZZY WITH DIFFERENTIAL EVOLUTION V.T. Sant'Ana¹, I. Staack, Linköping University, Sweden; R.M. Finzi Neto¹; ¹Federal University of Uberlândia, Brazil | ||||
| 15:00 | 15:30 | 10.11.4 |
COMPARATIVE ANALYSIS OF AERODYNAMIC CHARACTERISTICS OBTAINED BY ANALYTICAL, PANEL AND CFD METHOD G. Muchla¹, A. Kwiecien¹; ¹Faculty of Power and Aeronautical Engineering, WUT, Poland | ||||
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| 13:30 | 14:00 | 11.11.1 |
HETEROGENEOUS SYSTEMS MODELLING IN SUPPORT OF INCREMENTAL DEVELOPMENT R. Hällqvist¹, J. Naeser¹, J. Wallén Axehill¹, E. Herzog¹; ¹Saab AB, Sweden | ||||
| 14:00 | 14:30 | 11.11.2 |
A MODEL BASED SYSTEMS ENGINEERING APPROACH TO STREAMLINED NOISE CERTIFICATION OF TRANSPORT-TYPE AIRCRAFT D. Kim¹, F. Karagoz¹, S. Datta¹, M. Balchanos¹, D.H. Anvid¹, E.D. Harrison¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States | ||||
| 14:30 | 15:00 | 11.11.3 |
A HOLISTIC AIRCRAFT CABIN METAMODEL AS AN APPROACH TOWARDS AN INTERCONNECTED DIGITISED CABIN LIFECYCLE M.C. Berschik¹, M. Blecken¹, H. Kumawat¹, J.-E. Rath¹, D. Krause¹, R. God¹, T. Schüppstuhl¹; ¹Hamburg University of Technology, Germany | ||||
| 15:00 | 15:30 | 11.11.4 |
A COLLABORATIVE DESIGN METHOD FOR CIVIL AIRCRAFT BASED ON AN ENDURING AND EVOLUTIONARY AUTHORITATIVE SOURCE OF TRUTH X. Sun¹, M. Luo¹, Z. Cui¹, Z. Ji¹, H. Liu¹; ¹Beihang University, China | ||||
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| 13:30 | 14:00 | 12.11.1 |
EXPERIMENTAL ANALYSIS OF HEAT TRANSFER CHARACTERISTICS OF DIELECTRIC BARRIER DISCHARGE PLASMA ACTUATOR A. Hatamoto¹, K. Emori¹, H. Nishida¹; ¹Tokyo University of Agriculture and Technology, Japan | ||||
| 14:00 | 14:30 | 12.11.2 |
THE SENS4ICE EU PROJECT – SENSORS AND CERTIFIABLE HYBRID ARCHITECTURES FOR SAFER AVIATION IN ICING ENVIRONMENT – PROJECT OVERVIEW AND INITIAL RESULTS C.W. Schwarz, DLR, Germany | ||||
| 14:30 | 15:00 | 12.11.3 |
STRESS AND ENERGY RELEASE RATE INFLUENCE ON ICE SHEDDING WITH RESONANT ELECTROMECHANICAL DE-ICING SYSTEMS G. Gastaldo¹, V. Palanque, ISAE-Supaero and ONERA, France; M. Budinger, INSA/ICA, France; V. Pommier-Budinger¹; ¹ISAE-Supaero, France | ||||
| 15:00 | 15:30 | 12.11.4 |
NUMERICAL SIMULATION OF ICE ACCRETION ON A PITOT TUBE K. Szilder¹, P. Forsyth¹; ¹National Research Council, Canada | ||||
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| 13:30 | 14:00 | 13.11.1 |
NEW ENTRANTS’ AIRSPACE INTEGRATION IN JAPAN: JAXA’S ONGOING CONTRIBUTION N. Matayoshi, Japan Aerospace Exploration Agency, Japan | ||||
| 14:00 | 14:30 | 13.11.2 |
ON KEY PARAMETERS FOR THE ATTRACTIVENESS OF ON-DEMAND INTER-CITY AIR MOBILITY T. Ehlers¹, S. Hagemann², V. Gollnick², K. Lütjens¹; ¹German Aerospace Center, Germany ;²Hamburg University of Technology, Germany | ||||
| 14:30 | 15:00 | 13.11.3 |
THE AUTOMATION EVOLVES: CONCEPT FOR A HIGHLY AUTOMATED CONTROLLER WORKING POSITION I. Gerdes¹, M. Jameel¹, R. Hunger¹, L. Christoffels¹, H. Gürlük¹; ¹German Aerospace Center DLR, Germany | ||||
| 15:00 | 15:30 | 13.11.4 |
AN OPERATIONAL CONCEPT FOR THE INTEGRATION OF URBAN AIR MOBILITY VEHICLES INTO THE AIR TRAFFIC CONTROL PROCESSES I.C. Metz¹, S. Schier-Morgenthal¹; ¹German Aerospace Center DLR, Germany | ||||
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