Preliminary Programme - Session List
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Attention: Be advised that there might be changes till the congress, so please do not adjust your travel plans based on this preliminary programme.
"(invited)" behind a session means that those presentation were invited by the programme committee. They can, of course, be attended by everyone without "invitation
Thursday, 08. Sep 2022
0.8 | General lecture V: ICAS/IFAR „Transforming Aviation towards Zero Emission - to mitigate the climate impact“ I. Yimer, NRC Canada, B. Sainjon, ONERA France, M. Fischer, DLR Germany, Y. Watanabe, JAXA Japan, P. Krus, SARC Sweden Chair: D. Mavris ICAS PC Chair | |||
08. Sep 22 | 08:00 | 09:30 |
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09:30 - 10:00 | Coffee Break |
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08. Sep 22 | 10:00 | 10:30 | 1.10.1 |
CLEAN SKY 2 PROGRAMME OVERVIEW S. Dubois, Clean Aviation JU, Belgium | |||
08. Sep 22 | 10:30 | 11:00 | 1.10.2 |
SUSTAINABLE TECHNOLOGIES FOR COMMERCIAL AIRCRAFT OF TOMORROW - INTEGRATED MULTIFUNCTIONAL FUSELAGE DEMONSTRATOR Y.C. Roth, Airbus, Germany | |||
08. Sep 22 | 11:00 | 11:30 | 1.10.3 |
OPEN FAN ENGINE ARCHITECTURE FOR NEXT GENERATION SMR C. Diette, Safran Aircraft Engines, France | |||
08. Sep 22 | 11:30 | 12:00 | 1.10.4 |
PROGRESS IN WING DESIGN, STATUS AND PERSPECTIVES J. Lery, Dassault Aviation, France; M. Werner, Airbus, Germany; E. Coustols, ONERA, France | |||
08. Sep 22 | 12:00 | 12:30 | 1.10.5 |
THE CLEAN SKY 2 TECHNOLOGY EVALUATOR 1ST GLOBAL ASSESSMENT (invited) J.-F. Brouckaert, Belgium | |||
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08. Sep 22 | 10:00 | 10:30 | 2.10.1 |
COMBINED APPLICATION OF HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER IN PRELIMINARY AIRCRAFT DESIGN T. Effing¹, V. Schmitz¹, F. Schültke¹, F. Peter, Bauhaus Luftfahrt e.V, Germany; E. Stumpf¹; ¹RWTH Aachen University, Germany | |||
08. Sep 22 | 10:30 | 11:00 | 2.10.2 |
CLEAN-SKY 2 LARGE PASSENGER AIRCRAFT PLATFORM 1 ADVANCED ENGINE AND AIRCRAFT CONFIGURATIONS D. Kierbel, AIRBUS, France | |||
08. Sep 22 | 11:00 | 11:30 | 2.10.3 |
AERODYNAMIC DESIGN AND ANALYSIS OF HLFC WINGS WITHIN THE EUROPEAN PROJECT HLFC-WIN T. Streit¹, M. Kruse¹, T. Kilian¹, J. v. Geyr, DLRK, Germany; I. Petropoulos, ONERA, France; ¹DLR, Germany | |||
08. Sep 22 | 11:30 | 12:00 | 2.10.4 |
ECONOMICS OF SUSTAINABLE REGIONAL AIR MOBILITY P. De Felipe¹, D. Yang¹; ¹Imperial College London, United Kingdom | |||
08. Sep 22 | 12:00 | 12:30 | 2.10.5 |
TOWARD A GREENER AIRCRAFT ARCHITECTURE F. Vidal de Saint Jean, Dassault Aviation, France | |||
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08. Sep 22 | 10:00 | 10:30 | 3.10.1 |
SCALABILITY ANALYSIS OF RADICAL TECHNOLOGIES TO VARIOUS AIRCRAFT CLASS - PART I: INITIAL DESIGNS M.F.M. Hoogreef¹, V.O. Bonnin¹; ¹Delft University of Technology, Netherlands | |||
08. Sep 22 | 10:30 | 11:00 | 3.10.2 |
SCALABILITY ANALYSIS OF RADICAL TECHNOLOGIES TO VARIOUS AIRCRAFT CLASS - PART II: SENSITIVITY ANALYSIS V.O. Bonnin¹, M.F.M. Hoogreef¹; ¹Delft University of Technology, Netherlands | |||
08. Sep 22 | 11:00 | 11:30 | 3.10.3 |
REGIONAL TRANSPORT AIRCRAFT DESIGN USING TURBO-ELECTRIC DISTRIBUTED PROPULSION (TEDIP) SYSTEM V. Polepeddi¹, P. Raj¹, M. Emeneth, PACE America, United States; ¹Virginia Tech, United States | |||
08. Sep 22 | 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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08. Sep 22 | 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 | |||
08. Sep 22 | 10:30 | 11:00 | 4.10.2 |
LARGE EDDY SIMULATION OF A LYNX HELICOPTER LANDING IN THE BARROSO CORVETTE SHIP D.M. Pio¹, C.F. Rafael¹, P.S.C. Villela¹, G.A.L. da Silva¹, M. Ferro, Laboratorio Nacional de Computacao Cientifica -, Brazil; M.J.M. Guedes, Marinha do Brasil, Brazil; ¹Aerothermal Solutions - ATS, Brazil | |||
08. Sep 22 | 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 | |||
08. Sep 22 | 11:30 | 12:00 | 4.10.4 |
TRANSONIC FLOW OVER DELTA WING USING ENTROPIC LATTICE BOLTZMANN METHOD M. Dhake¹, C. Thantanapally¹, S. Arcidiacono¹, S. Ansumali¹; ¹SankhyaSutra Labs Ltd, India Presenter: Chakradhar Thantanapally, SankhyaSutra Labs Limited | |||
08. Sep 22 | 12:00 | 12:30 | 4.10.5 |
CFD TAKE-OFF ANALYSIS OF A SEAPLANE HULL THROUGH A DYNAMIC MULTIPHASE MODEL M. Sinisi¹, G. Cantanna¹, G. Occhipinti¹, A. Caramazza¹, G. Dilonardo¹, E. Cestino¹; ¹Politecnico di Torino, Italy Presenter: Gaetano Dilonardo, Politecnico di Torino | |||
Reserve Paper (interactive) | 4.10.R |
VALIDATING AIRSPACE CFD MODELS FOR DRONE OPERATION WITH FLIGHT TEST DATA D. Standingford¹, C. Sequeira², M. Allan¹, C. Rider², G. Furse², J. Sharpe¹; ¹Zenotech, United Kingdom ;²Flare Bright, United Kingdom | |||||
Reserve Paper (interactive) | 4.10.R |
COMPARATIVE ANALYSIS OF AERODYNAMIC CHARACTERISTICS OBTAINED BY ANALYTICAL, PANEL AND CFD METHOD G. Muchla¹, A. Kwiecien¹; ¹Faculty of Power and Aeronautical Engineering, WUT, Poland Presenter: Adrianna Kwiecien, Faculty of Power and Aeronautical Engineering, WUT | |||||
Reserve Paper (interactive) | 4.10.R |
REDESIGNING AND SIMULATION EVALUATION ON LARGE-FLOW HIGH-TEMPERATURE HIGH-PRESSURE BYPASS SURGE-OUT SYSTEM Z.-P. Li, AECC Shenyang Engine Research Institute, China | |||||
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08. Sep 22 | 10:00 | 10:30 | 5.10.1 |
AERONAUTICAL CFD AND TURBULENCE - PROGRESS AND CHALLENGES (invited) A. Rizzi¹, D. Henningson¹; ¹KTH, Sweden | |||
08. Sep 22 | 10:30 | 11:00 | 5.10.2 |
AERONAUTICAL CFD AND TURBULENCE - PROGRESS AND CHALLENGES PART 2 (invited) A. Rizzi¹, D. Henningson¹; ¹KTH, Sweden | |||
08. Sep 22 | 11:00 | 11:30 | 5.10.3 |
OPEN CAVITY SIMULATIONS UNDER SIDESLIP FLOW CONDITIONS K. Rajkumar¹, J. Radtke¹, E. Tangermann¹, M. Klein¹; ¹University of the Bundeswehr Munich, Germany | |||
08. Sep 22 | 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 Presenter: Umberto Armani | |||
08. Sep 22 | 12:00 | 12:30 | 5.10.5 |
UNSTEADY SIMULATIONS OF MASSIVELY SEPARATED FLOW AROUND NACA0021 AIRFOIL USING A TRANSITIONAL IDDES MODEL Y. Wang, China; S.-Q. Zhang, China; W.-P. Song, China; Z.-H. Han, China | |||
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08. Sep 22 | 10:00 | 10:30 | 6.10.1 |
EXPERIMENTAL INVESTIGATIONS OF AN AEROELASTIC WIND TUNNEL MODEL FOR TAIL BUFFETING ANALYSIS J. Stegmüller¹, S. Hayböck¹, P. Hartl¹, C. Breitsamter¹; ¹Technical University of Munich, Germany | |||
08. Sep 22 | 10:30 | 11:00 | 6.10.2 |
OPTIMIZATION OF AN ACTIVE DAMPING SYSTEM FOR USE WITH A SINGLE STRUT MOUNT J. Pereira, National Research Council Canada, Canada | |||
08. Sep 22 | 11:00 | 11:30 | 6.10.3 |
WIND-TUNNEL TEST ON LEADING-EDGE VORTEX OF LOW-ASPECT-RATIO FLAPPING PLATES J.-S. Han¹, C. Breitsamter¹; ¹Technical University of Munich, Germany | |||
08. Sep 22 | 11:30 | 12:00 | 6.10.4 |
POWERED WIND TUNNEL TESTING WITH HYDRAULIC MOTORS D. Steiling¹, P. Aschwanden¹, J. Müller¹, T. Jax¹; ¹RUAG AG, Switzerland Presenter: Peter Aschwanden, RUAG AG | |||
08. Sep 22 | 12:00 | 12:30 | 6.10.5 |
EXPERIMENTING ROTORCRAFT FLIGHT IN COMPLEX ENVIRONMENTAL CONDITIONS USING THE WIND TUNNEL: HELICOPTER SHIP LANDING CASE N. Taymourtash¹, A. Zanotti¹, G. Gibertini¹, G. Quaranta¹; ¹Politecnico di Milano, Italy | |||
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08. Sep 22 | 10:00 | 10:30 | 7.10.1 |
INCREMENTAL FATIGUE DAMAGE MODEL: APPLICATION TO PLANE PROBLEMS WITH NON-PROPORTIONAL LOADING Z. Kapidzic¹, S.B. Lindström, Linköping University, Sweden; J. Lundgren¹; ¹Saab AB, Sweden | |||
08. Sep 22 | 10:30 | 11:00 | 7.10.2 |
FATIGUE OF 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 | |||
08. Sep 22 | 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 | |||
08. Sep 22 | 11:30 | 12:00 | 7.10.4 |
FATIGUE CHARACTERIZATION OF ADHESIVE JOINTS IN AEROPLANES-THE DEVELOPMENT OF A NEGATIVE LOAD RATIO (R<0) TESTING METHOD O. Orell¹, J. Jokinen¹, M. Kanerva¹; ¹Tampere University, Finland | |||
08. Sep 22 | 12:00 | 12:30 | 7.10.5 |
FATIGUE DAMAGE MODEL OF HIGH TEMPERATURE POLYMER COMPOSITES IN AERO-ENGINES V.R. Pakkam Gabriel¹, P. Fernberg¹; ¹Luleå University of Technology, Sweden | |||
Reserve Paper | 7.10.R |
FATIGUE CRACK PROPAGATION IN ADDITIVELY MANUFACTURED POLYMER PARTS H. El Fazani¹, J. Coil¹, J. Laliberté¹; ¹Carleton University , Canada | |||||
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08. Sep 22 | 10:00 | 10:30 | 8.10.1 |
DEVELOPMENT OF A PREDICTIVE DAMAGE METHODOLOGY FOR HYBRID WING BODY AIRCRAFT STRUCTURES H. Raza¹, C. Harey¹, P. Vaghela¹, J. Bayandor¹; ¹CRASH Lab, University at Buffalo, United States Presenter: Christopher Harley, CRASH Lab, Dept. of MAE, University at Buffalo | |||
08. Sep 22 | 10:30 | 11:00 | 8.10.2 |
NUMERICAL ANALYSIS AND COMPARISON WITH RESULTS OF FRACTURE TESTS OF LUG MANUFACTURED IN COMPOSITE MATERIAL G.C. Fonseca, Embraer Minas Gerais, Brazil; S.F.M. Almeida, Instituto Tecnológico de Aeronáutica, Brazil | |||
08. Sep 22 | 11:00 | 11:30 | 8.10.3 |
ENHANCEMENT OF FLEXIBLE STRATEGY FOR AUGMENTING DESIGN POINTS FOR COMPUTER EXPERIMENTS AND APPLICATION TO A MDO OF A FAN-BLISK A. Tamkan¹, P. Flassig¹, M. Meyer, Rolls-Royce Deutschland, Germany; ¹Technische Hochschule Brandenburg, Germany | |||
08. Sep 22 | 11:30 | 12:00 | 8.10.4 |
TRANSIENT AND FREE-VIBRATION ANALYSIS OF LAMINATED SHELLS THROUGH THE DISCONTINUOUS GALERKIN METHOD G. Guarino¹, V. Gulizzi¹, A. Milazzo¹; ¹1University of Palermo, Department of Engineering, Italy Presenter: Vincenzo Gulizzi, University of Palermo - Department of Engineering | |||
08. Sep 22 | 12:00 | 12:30 | 8.10.5 |
DESIGN AND STUDY ON NOISE REDUCTION PROPERTIES OF A MULTISTAGE BIONIC MEMBRANE-TYPE ACOUSTIC METAMATERIAL X.J. Zhang¹, D. Guo¹, H.Y. Huang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | |||
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08. Sep 22 | 10:00 | 10:30 | 9.10.1 |
AEROELASTIC TAILORING OF COMPRESSOR BLADES A.-P. Chalke¹, N. Glodic¹, M. Gutierrez Salas¹; ¹KTH Royal Institute of Technology, Sweden | |||
08. Sep 22 | 10:30 | 11:00 | 9.10.2 |
RAPID AEROACOUSTIC PLANFORM DESIGN OPTIMIZATION OF INSTALLED PROPELLERS T. Sinnige¹, W. de Gruijl¹, W. de Haan¹, G. Eitelberg¹; ¹Delft University of Technology, Netherlands | |||
08. Sep 22 | 11:00 | 11:30 | 9.10.3 |
PERFORMANCE BENEFITS OF A FAN ON BLADE – FLADE – FOR A VARIABLE CYCLE ENGINE 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 | |||
08. Sep 22 | 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 Presenter: Lars Ellbrant, GKN Aerospace Sweden AB | |||
08. Sep 22 | 12:00 | 12:30 | 9.10.5 |
STUDY ON THE OBJECTIVE FUNCTION OF THE PROFILED ENDWALL OPTIMIZATION OF AN EMBEDDED COMPRESSOR STATOR J. Wang¹, D. Meng¹, D. Feng¹, Q. Zhao¹; ¹Shenyang Engine Research Institute of AECC, China | |||
Reserve Paper | 9.10.R |
DESIGN AND EFFICIENCY ANALYSIS OF EVTOL CONTRA-ROTATING PROPELER N.-X. Qiao¹, T.-L. Ma¹, X.-S. Wang¹, J.-C. Fu¹; ¹Beihang University, China | |||||
Reserve Paper | 9.10.R |
EXPERIMENTAL STUDY ON THE EFFECT OF INTERSTAGE BLEEDING ON THE PERFORMANCE OF FULL-SCALE MULTISTAGE AXIAL COMPRESSOR Z.-B. Zhang¹, Y.-H. Zhang¹, Y.-H. Chen¹; ¹Shenyang Engine Research Institute, China | |||||
Reserve Paper | 9.10.R |
EXPERIMENTAL STUDY OF FLAT BAFFLE INLET TOTAL-PRESSURE DISTORTION IN A THREE-STAGE FAN Y. Chen¹, Z. Zhang¹, A. Wang¹; ¹AECC Shenyang Engine Institute, China Presenter: Yehui CHEN, AECC Shenyang Engine Institute | |||||
Reserve Paper (interactive) | 9.10.R |
SURGE CHARACTERISTICS IN FRONT OF EACH STAGE FOR A HIGH PRESSURE FIVE STAGE COMPRESSOR B.-B. Jia¹, Z.-B. Zhang¹, H.-X. Li, AECC, China; ¹AECC Shenyang Engine Institute, China | |||||
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08. Sep 22 | 10:00 | 10:30 | 10.10.1 |
INCREMENTAL NONLINEAR DYNAMIC CONTROL WITH SPARSE NON-PARAMETRIC BAYESIAN REGRESSION OF DAMAGED AIRCRAFT L. Kim¹, D. Lee¹, H. Bang¹; ¹Korea Advanced Institute of Science and Technology, South Korea | |||
08. Sep 22 | 10:30 | 11:00 | 10.10.2 |
FAULT-TOLERANT CONTROL FOR AIRCRAFT WITH STRUCTURAL DAMAGE USING GAUSSIAN PROCESS REGRESSION D.-W. Lee¹, L.-S. Kim¹, H.-C. Bang¹; ¹KAIST, South Korea | |||
08. Sep 22 | 11:00 | 11:30 | 10.10.3 |
EFFECTIVENESS ANALYSIS OF DOBC Q-FILTER PARAMETERS FOR A MULTICOPTER UAV H.J. Jeaong¹, C. Roh¹, Y.H. Jang¹, J.Y Suk¹, S.K. Kim¹; ¹Department of Aerospace Engineering, Chungnam National Universit, South Korea | |||
08. Sep 22 | 11:30 | 12:00 | 10.10.4 |
CONVEX PROGRAMMING-BASED OPTIMAL THREE-DIMENSIONAL MID-COURSE GUIDANCE WITH LOSSLESS CONVEXIFICATION C.-G. Jung¹, C.-H. Lee¹, M.-J. Tahk¹; ¹KAIST, South Korea | |||
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08. Sep 22 | 10:00 | 10:30 | 11.10.1 |
TOWARDS CORRECT-BY-CONSTRUCTION DESIGN OF SAFETY-CRITICAL EMBEDDED AVIONICS SYSTEMS I. Sander¹, I. Söderquist², M. Ekman², R. Jordao¹, F. Bahrami¹, R. Chen¹, A. Åhlander²; ¹KTH Royal Institute of Technology, Sweden ;²Saab AB, Sweden | |||
08. Sep 22 | 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 | |||
08. Sep 22 | 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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08. Sep 22 | 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 | |||
08. Sep 22 | 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 Presenter: Gabriele Enea, MIT Lincoln Laboratory | |||
08. Sep 22 | 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 | |||
08. Sep 22 | 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 | |||
08. Sep 22 | 12:00 | 12:30 | 13.10.5 |
AIRCRAFT MASS ESTIMATION USING CRUISE FLIGHT PROFILE R. Mori, ENRI, Japan | |||
Reserve Paper | 13.10.R |
KINETIC ENERGY RECOVERY FROM A LANDING AIRCRAFT: ENERGY ANALYSIS, ENVIRONMENTAL AND ECONOMIC PROSPECTS R. Camilleri¹, A. Batra¹; ¹Institute of Aerospace Technologies (IAT), University of Malta, Malta | |||||
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08. Sep 22 | 10:00 | 10:30 | 14.10.1 |
MODEL-BASED SYSTEMS ENGINEERING FOR FUTURE DIGITAL FLIGHT LINES (invited) M.A. Kelly, Lockheed Martin Aeronautics, United States | |||
08. Sep 22 | 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 | |||
08. Sep 22 | 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 |
12:30 - 13:30 | Lunch Break |
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08. Sep 22 | 13:30 | 14:00 | 1.11.1 |
CLEAN AVIATION PROGRAMME RATIONALE AND OVERVIEW (invited) R. van Manen, Clean Aviation, Belgium | |||
08. Sep 22 | 14:00 | 14:30 | 1.11.2 |
ULTRA-EFFICIENT AIRCRAFT AND PROPULSION ARCHITECTURES FOR LOW-EMISSION SHORT/MEDIUM RANGE [SMR] AIRCRAFT (invited) M. Calvo Blanco, Belgium | |||
08. Sep 22 | 14:30 | 15:00 | 1.11.3 |
HYBRID-ELECTRIC AND FULL ELECTRIC ARCHITECTURES FOR LOW-EMISSION HYBRID-ELECTRIC REGIONAL [REG] AIRCRAFT (invited) A. Marino, Belgium | |||
08. Sep 22 | 15:00 | 15:30 | 1.11.4 |
DISRUPTIVE TECHNOLOGIES TO ENABLE ZERO-CARBON HYDROGEN–POWERED [HPA] SHORT RANGE AIRCRAFT (invited) P. Trinchieri, Belgium | |||
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08. Sep 22 | 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 | |||
08. Sep 22 | 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 | |||
08. Sep 22 | 14:30 | 15:00 | 2.11.3 |
CS2 – MANTA – MULTI-FUNCTIONAL FLAP MECHANISM OFFERING A SECOND DEGREE OF FREEDOM M. Desmet¹, J. Vervliet¹, D. De Wit¹, R. Seidler, Deutsches Zentrum Fuer Luft und Raumfahrt E.V., Germany; J. Docter, Netherlands Aerospace Centre, Netherlands; B. Everaert¹; ¹Asco Industries nv/sa, Belgium | |||
08. Sep 22 | 15:00 | 15:30 | 2.11.4 |
INFLUENCES OF CHANGING THE INSTALLING POSITIONS OF MULTIPLE WINGLETS ON AERODYNAMIC CHARACTERISTICS E. Kobayashi¹, K. Chiba¹; ¹The University of Electro-Communications, Japan | |||
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08. Sep 22 | 13:30 | 14:00 | 3.11.1 |
COOLING SYSTEM OF STRATOFLY HYPERSONIC VEHICLE: CONCEPTUAL DESIGN, NUMERICAL ANALYSIS AND VERIFICATION R. Scigliano¹, V. De Simone¹, R. Fusaro², D. Ferretto², M. Marini¹, N. Viola²; ¹Italian Aerospace Research Center - CIRA scpa, Italy ;²Politecnico di Torino (PoliTo), Italy | |||
08. Sep 22 | 14:00 | 14:30 | 3.11.2 |
HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONS N. Viola¹, R. Fusaro¹, D. Ferretto¹, O. Gori¹, M. Marini², P. Roncioni², B.O. Cakir³, A.C. Ispir³, B.H. Saracoglu³; ¹Politecnico di Torino, Italy ;²CIRA, Italy ;³VKI, Belgium Presenter: Oscar Gori, Politecnico di Torino | |||
08. Sep 22 | 14:30 | 15:00 | 3.11.3 |
LTO NOISE AND SONIC BOOM PREDICTIONS IN EARLY CONCEPTUAL DESIGN PHASES G. Piccirillo¹, S. Graziani¹, R. Fusaro¹, N. Viola¹; ¹Politecnico di Torino, Italy | |||
08. Sep 22 | 15:00 | 15:30 | 3.11.4 |
SIMPLIFIED MODELS FOR THE PRELIMINARY AERODYNAMIC CHARACTERIZATION OF HIGH-SPEED VEHICLES TO SUPPORT MISSION ANALYSIS O. Gori, Politecnico di Torino, Italy | |||
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08. Sep 22 | 13:30 | 14:00 | 4.11.1 |
ACCURATE TWO-DIMENSIONAL STEADY-STATES FOR THE SUPERSONIC FLOW OVER A COMPRESSION CORNER R. Santos¹, L. Alves¹, N. Cerulus², H. Quintanilha Jr², V. Theofilis²; ¹UFF, Brazil ;²UoL, United Kingdom | |||
08. Sep 22 | 14:00 | 14:30 | 4.11.2 |
NUMERICAL MODELING OF LAMINAR-TURBULENT TRANSITION IN AN INTERCONNECTING COMPRESSOR DUCT A. Capitao Patrao¹, B. González Lozano¹, I. Jonsson¹, C. Xisto¹; ¹Chalmers University of Technology, Sweden | |||
08. Sep 22 | 14:30 | 15:00 | 4.11.3 |
ANALYSIS OF A LAMINAR SEPARATION BUBBLE ON A NACA0009 AIRFOIL AT DIFFERENT BACKGROUND DISTURBANCE LEVELS J.S. Kern¹, A. Hanifi¹, D.S. Henningson¹; ¹FLOW, Department of Engineering Mechanics, KTH Royal Institute o, Sweden | |||
08. Sep 22 | 15:00 | 15:30 | 4.11.4 |
A STUDY ON THE NUMERICAL SIMULATION OF FLOW TRANSITION INCLUDING CROSSFLOW EFFECTS A.R.S. Righi, ITA, Brazil; G.L.O. Halila¹, J.L.F. Azevedo¹; ¹IAE, Brazil | |||
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08. Sep 22 | 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 | |||
08. Sep 22 | 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 | |||
08. Sep 22 | 14:30 | 15:00 | 5.11.3 |
NUMERICAL PREDICTION OF FOCUS BOOM GENERATED BY MANEUVERS S. Han¹, Y. Xu¹; ¹Chinese Aeronautical Establishment, China | |||
08. Sep 22 | 15:00 | 15:30 | 5.11.4 |
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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08. Sep 22 | 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 | |||
08. Sep 22 | 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 | |||
08. Sep 22 | 14:30 | 15:00 | 6.11.3 |
RECENT ACTIVITIES ON FLOW QUALITY ASSESSMENT AT THE EUROPEAN TRANSONIC WINDTUNNEL J.H. You¹, M.C.N. Wright¹, H. Quix¹; ¹European Transonic Windtunnel GmbH, Germany | |||
08. Sep 22 | 15:00 | 15:30 | 6.11.4 |
INVESTIGATION ON CORRECTION OF TUNNEL WALL INTERFERENCE FOR DYNAMIC AIRFOIL TEST IN LOW-SPEED WIND TUNNEL Y. Jiao, China; H. Zou, China; B. Chen, China; C. Xiao, China Presenter: Yuqin Jiao | |||
Reserve Paper | 6.11.R |
DEVELOPMENT AND VERIFICATION OF OSCILLATING BLADE GUST GENERATOR IN LOW-SPEED WIND TUNNEL C. Bu¹, Z. Ma¹, Y. Zhang¹, L. Li¹; ¹AVIC Aerodynamics Research Institute, China | |||||
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08. Sep 22 | 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 | |||
08. Sep 22 | 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 | |||
08. Sep 22 | 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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08. Sep 22 | 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 Presenter: Pedro J. González, TU-Berlin | |||
08. Sep 22 | 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 | |||
08. Sep 22 | 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 | |||
08. Sep 22 | 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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08. Sep 22 | 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 Presenter: Christophe DIETTE, Safran Aircraft Engines | |||
08. Sep 22 | 14:00 | 14:30 | 9.11.2 |
NOVEL AIRCRAFT PROPULSION AND AVAILABILITY OF ALTERNATIVE, SUSTAINABLE AVIATION FUELS IN 2050 J. Kos¹, J. 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 | |||
08. Sep 22 | 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 | |||
08. Sep 22 | 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 | |||
Reserve Paper (interactive) | 9.11.R |
ANALYSIS AND SIZING OF GREEN PROPULSION SYSTEM FOR A SUBORBITAL AIRCRAFT M. Bruno¹, R. Cambertoni¹, A. Pellegrino¹, P. Petrachi¹, C. Spampinato¹; ¹Polytechnic of Turin, Italy Presenter: Cristina Spampinato, Polytechnic of Turin | |||||
Reserve Paper (interactive) | 9.11.R |
TESTING AND MODELLING OF A DUCTED FAN MOTOR FOR UAV APPLICATIONS B.-O. Schröder¹, P.J. González¹, F.J. Silvestre¹; ¹TU Berlin, Germany Presenter: Pedro González, TU Berlin | |||||
Reserve Paper (interactive) | 9.11.R |
COMPARISON OF ANALYTICAL SEMI-EMPIRICAL MODEL FOR JET NOISE PREDICTION F. Petrosino¹, M. Barbarino¹; ¹CIRA, Italy | |||||
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08. Sep 22 | 13:30 | 14:00 | 10.11.1 |
ON LATERAL-LONGITUDINAL CONTROL COUPLING FOR SHORT- AND LONG-FUSELAGE BWB AIRCRAFT CONFIGURATIONS L.M.B.C. Campos, Instituto Superior Técnico, Universidade de Lisboa, Portugal; J.M.G. Marques, Universidade de Évora, Portugal | |||
08. Sep 22 | 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 Presenter: Clécio Fischer | |||
08. Sep 22 | 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 | |||
08. Sep 22 | 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 Presenter: Adrianna Kwiecien, Faculty of Power and Aeronautical Engineering, WUT | |||
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08. Sep 22 | 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 | |||
08. Sep 22 | 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 | |||
08. Sep 22 | 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 | |||
08. Sep 22 | 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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08. Sep 22 | 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 | |||
08. Sep 22 | 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 | |||
08. Sep 22 | 14:30 | 15:00 | 12.11.3 |
STRESS AND ENERGY RELEASE RATE INFLUENCE ON ICE SHEDDING WITH RESONANT ELECTROMECHANICAL DE-ICING SYSTEMS G. Gastaldo¹, V. Palanque, ISAE-Supaero and ONERA, France; M. Budinger, INSA/ICA, France; V. Pommier-Budinger¹; ¹ISAE-Supaero, France | |||
08. Sep 22 | 15:00 | 15:30 | 12.11.4 |
NUMERICAL SIMULATION OF ICE ACCRETION ON A PITOT TUBE K. Szilder¹, P. Forsyth¹; ¹National Research Council, Canada | |||
Reserve Paper | 12.11.R |
EFFECTS OF ANISOTROPIC THERMAL CONDUCTIVITY OF COMPOSITE SHIELD ON THE ELECTROTHERMAL ANTI-ICING SYSTEMS X. Guo¹, Q. Yang¹, H. Zheng¹, W. Dong¹; ¹Shanghai Jiaotong University, China | |||||
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08. Sep 22 | 13:30 | 14:00 | 13.11.1 |
NEW ENTRANTS’ AIRSPACE INTEGRATION IN JAPAN: JAXA’S ONGOING CONTRIBUTION N. Matayoshi, Japan Aerospace Exploration Agency, Japan | |||
08. Sep 22 | 14:00 | 14:30 | 13.11.2 |
ON KEY PARAMETERS FOR THE ATTRACTIVENESS OF ON-DEMAND INTER-CITY AIR MOBILITY T. Ehlers¹, S. Hagemann², V. Gollnick², K. Lütjens¹; ¹German Aerospace Center, Germany ;²Hamburg University of Technology, Germany | |||
08. Sep 22 | 14:30 | 15:00 | 13.11.3 |
THE AUTOMATION EVOLVES: CONCEPT FOR A HIGHLY AUTOMATED CONTROLLER WORKING POSITION I. Gerdes¹, M. Jameel¹, R. Hunger¹, L. Christoffels¹, H. Gürlük¹; ¹German Aerospace Center DLR, Germany | |||
08. Sep 22 | 15:00 | 15:30 | 13.11.4 |
AN OPERATIONAL CONCEPT FOR THE INTEGRATION OF URBAN AIR MOBILITY VEHICLES INTO THE AIR TRAFFIC CONTROL PROCESSES I.C. Metz¹, S. Schier-Morgenthal¹; ¹German Aerospace Center DLR, Germany | |||
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15:30 - 16:00 | Break |
0.9 | 16:00-17:00 ICAS von Karman Lecture: “Clean Sky Programme Achievements and Clean Aviation Outlook” S.Klauke CTO Airbus , E. Dalbies CTO SAFRAN, M. Protti Head of Advanced Research Leonardo Aircraft Chair: A. Krein Executive Director Clean Aviation JU GER, J.L. Azevedo, ICAS President BRA | |||
08. Sep 22 | 16:00 | 17:00 |
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17:00 - 17:30 | Closing Ceremony |