ICAS 2020: TOPICS AND TITLES |
1 - Aircraft Design and Integrated Systems |
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ICAS2020_0010: I. Berlowitz, IBAero Engineering, Israel no paper provided |
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ICAS2020_0030: T. Goetzendorf-Grabowski¹, J. Mieloszyk¹, M. Figat¹, A. Tarnowski¹, B. Hernik¹; ¹Warsaw University of Technology, Poland LIGHTWEIGHT UAV FOR EMERGENCY MEDICAL SERVICE |
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ICAS2020_0050: A. Berres¹, P. Niemeyer¹; ¹German Aerospace Center (DLR), Germany IMPACT OF NEW TECHNOLOGIES ON AIRCRAFT SYSTEMS |
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ICAS2020_0085: S.R. Mistri¹, R.S. Pant¹, C.S. Yerramalli¹, A. Guha¹; ¹Indian Institute of Technology- Bombay, India METHODOLOGY FOR OBTAINING AN OPTIMIZED BAFFLED AIRFOIL FOR AN INFLATABLE WING |
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ICAS2020_0096: G. Li, Chinese Aeronautical Establishment, China; G. Zhang¹, S. Chu¹; ¹Aviation Industry Development Research Center of China, China HELICOPTER FLIGHT DYNAMICS MODELLING WITH FREE-WAKE METHOD EMBEDDED FOR ROTOR ICING ANALYSES |
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ICAS2020_0145: O. Luderer¹, M. Jünemann¹, F. Thielecke¹; ¹Hamburg University of Technology, Germany VALIDATION OF AN AERODYNAMIC MODEL FOR THE ANALYSIS OF SUBSCALE TEST AIRCRAFT WITH DISTRIBUTED ELECTRICAL PROPULSION |
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ICAS2020_0147: C. Li¹, W. Ji¹, C. Gong¹, H. Fang, Shanghai Electro-Mechanical Engineering Institute, China; ¹Northwestern Polytechnical University, China EFFICIENT ADAPTIVE SURROGATE-BASED OPTIMIZATION USING FUZZY CLUSTERING FOR COMPLEX SYSTEM OPTIMIZATIONS |
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ICAS2020_0154: D. Chen¹, Y. Li¹, Y. Li¹, L. Guan, Tsinghua University, China; Q. Wang, Beijing Aerospace Technology Institute, China; ¹Northwestern Polytechnical University, China CONCEPTUAL DESIGN OF A FIXED-WING AQUATIC UAV USING KNOWLEDGE BASED ENGINEERING |
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ICAS2020_0155: W. Wang, School of Aeronautics, Northwestern Polytechnical University, China; W. Yang¹, B. Song¹; ¹Research & Development Institute of NWPU, China NUMERICAL SIMULATION ON AERODYNAMIC CHARACTERISTICS OF BIONIC CORRUGATED FLAPPING WING |
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ICAS2020_0185: P. Wassink¹, G. Atanasov¹, C. Hesse¹, B. Froehler¹; ¹German Aerospace Center (DLR), Germany CONCEPTUAL DESIGN OF SILENT ELECTRIC COMMUTER AIRCRAFT |
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ICAS2020_0216: L.P. Ruiz Calavera¹, S. De Lucas Bodas¹, D.E. Funes Sebastian¹; ¹Airbus Defence & Space, Spain STUDY OF THE BENEFITS OF A SEMI-MORPHING WING CONCEPT |
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ICAS2020_0238: J. Hartmann¹, S. Woehler¹, B. Liebhardt¹, F. Presto, Hamburg University of Technology (TUHH), Germany; ¹German Aerospace Center (DLR), Germany FLEET LEVEL DIRECT OPERATING COST ASSESSMENT OF ADVANCED ALL NEW MID-RANGE TRANSPORT AIRCRAFT |
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ICAS2020_0244: D. DI Pasquale¹, D. Verma¹, G. Pagliuca¹; ¹Cranfield University, United Kingdom BLENDED WING BODY (BWB) PLANFORM MULTIDISCIPLINARY OPTIMISATION (MDO) FOR EARLY STAGE AIRCRAFT DESIGN USING MODEL BASED ENGINEERING |
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ICAS2020_0248: D. Di Pasquale¹, C. Bolart¹; ¹Cranfield University, United Kingdom VALIDATING SURROGATE MODELS AND ICORPORATING UNCERTAINTY QUANTIFICATION IN MULTI-ELEMENTS AIRFOIL DESIGN OPTIMISATION |
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ICAS2020_0253: E. Bragado-Aldana¹, M.M. Lone¹, A. Riaz¹; ¹Cranfield University, United Kingdom ON WINGS WITH NON-ELLIPTIC LIFT DISTRIBUTIONS |
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ICAS2020_0256: Y.K. Yin¹, W.B. Song¹; ¹Shanghai Jiao Tong University, China A HIERARCHICAL STRUCTURAL MODEL FOR CONCEPTUAL DESIGN OF TRANSPORT AIRCRAFT WING |
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ICAS2020_0284: G. Song¹, W. Cheng¹, Y. Yang², Z. Qian³, W. Ge*, Y. Zhang*, Z. Wang², S. Zhang², X. Shi², C. Li³; ¹Aviation Industry Development Research Center of China, China; ²Aircraft strength research Institute of China, China; ³AVCI Aerodynamics Research Institute, China; *Northwestern Polytechnical University, China VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WING |
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ICAS2020_0317: J. Guo¹, Y. Li, School of Aeronautics, Northwestern Polytechnical University, China; M. Xu¹; ¹School of Astronautics, Northwestern Polytechnical University, China AN ADJOINT-BASDF AERO-STRUCTURAL DESIGN OPTIMIZATION METHOD USING DYNAMIC MESH TECHNOLOGY |
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ICAS2020_0333: Y. Li¹, W. Yang ¹, A. Chen¹, R. Zhang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China MECHANISM DESIGN AND AERODYNAMIC RESEARCH OF RETRACTABLE FOLDING FLAPPING WING |
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ICAS2020_0350: S.-B. Ling¹, K.-S. Zhang, Northwestern polytechnical university, China; Z.-H. Han¹, Z.-J. Gao, Xiantianjihangtong Technology CO. Ltd., China; ¹Northwestern Polytechnical university, China EVALUATION AND VALIDATION OF AEROELASTIC ANALYSIS PROGRAM FOR THE “AEROSTRUCT” WING OPTIMIZATION PLATFORM |
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ICAS2020_0352: X. Chen¹, A. Riaz¹, S. El Fassi¹; ¹Cranfield University, United Kingdom APPLICATION OF ARTIFICIAL NEURAL NETWORKS FOR EFFICIENT RELIABILITY-BASED DESIGN OPTIMIZATION |
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ICAS2020_0366: J.-T. Huang¹, Z. Zhou¹, Z.-H. Gao, Northwestern Polytechnical University, China; X. Chen¹, S.-D. Zhong¹; ¹China Aerodynamics Research and Development Center, China STUDY ON ADJOINT OPTIMIZATION OF BWB CONFIGURATION CONSIDERING THE INFLUENCE OF INTAKE AND EXHAUST SYSTEM |
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ICAS2020_0398: Y. Ma¹, W. Zhang¹, Y. Zhang¹, Y. Ma¹, Z. Bai¹; ¹Northwestern Polytechnical University, China PRELIMINARY DESIGN AND EXPERIMENTAL INVESTIGATION OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT |
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ICAS2020_0451: A.N. Varyukhin¹, M.A. Ovdienko¹, A.V. Vlasov, Central Institute of Aviation Motors, Russia; V.S. Zakharchenko¹; ¹CENTRAL INSTITUTE OF AVIATION MOTORS, Russia UNMANNED FIRE-FIGHTING AMPHIBIOUS AIRCRAFT WITH DISTRIBUTED TURBOELECTRIC PROPULSION SYSTEM |
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ICAS2020_0468: J. Hanjie¹, M. Yi , Xi’an Institute of Space Radio Technology, China; Z. Ye ¹; ¹School of Aerospace Engineering, Universiti Sains Malaysia, Malaysia DESIGN OF A HYBRID VTOL LOGISTICS UAV SYSTEM INTEGRATED INTO CIVIL AVIATION AIR TRAFFIC CONTROL SYSTEM |
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ICAS2020_0493: R. Scigliano¹, V. De Simone¹, M. Marini¹, R. Fusaro², D. Ferretto², N. Viola²; ¹Italian Aerospace Research Centre (CIRA), Italy; ²Politecnico di Torino (PoliTO), Italy THERMAL PROTECTION SYSTEM PRELIMINARY DESIGN OF STRATOFLY HIGH-SPEED PROPELLED VEHICLE |
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ICAS2020_0495: Z.-L. Chen¹, Y.-C. Chen², S. Zhang, Beijing Aeronautical Science & Technology Research Institute, China; L.-X. Wang, Beihang University, China; Z.-G. Tan², B. Chen, AVIC Aerodynamics Research Institute, China; S.-W. Zhao, AVIC The First Aircraft Institute, China; L. Wang, AVIC Huiyang Aviation Propeller Co., LTD., China; J. Li¹, C.-S. Yuan¹, Y.-J. Zhang¹, Y.-Z. Zhang¹, W.-M. Sang¹, Y.-J. Tao¹, D. Li¹, B.-Q. Zhang¹; ¹Northwestern Polytechnical University, China; ²Shanghai Aircraft Design and Research Institute, COMAC, China PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY |
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ICAS2020_0508: M.C. Moruzzi, University of Bologna, Italy; M. Cinefra, Italy; S. Bagassi, Italy; E. Carrera, Italy ATTENUATION OF NOISE IN THE CABIN OF A REGIONAL AIRCRAFT BY METAMATERIAL TRIM PANELS |
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ICAS2020_0574: H.H. Feng¹, F. Liu¹, H.F. Wei¹, J.M. Wu¹; ¹Aviation industry Development Research Center of China, China BASED ON THE CHARACTERISTIC PARAMETERS ESTIMATE MANUFACTURING COST FOR COMPOSITE STRUCTURES |
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ICAS2020_0584: J. Hofmann¹, M. Mindt¹, F. Weiss¹; ¹German Aerospace Center (DLR), Germany AERODYNAMIC AND STRUCTURAL MODELING IN THE ROTORCRAFT MULTI-PHYSICS SIMULATION VAST |
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ICAS2020_0600: Y.-L. Ding¹, Z.-H. Han¹, J.-L. Qiao¹, W.-P. Song¹, B.-F. Song¹; ¹Northwestern Polytechnical University, China FAST METHOD AND AN INTEGRATED CODE FOR SONIC BOOM PREDICTION OF SUPERSONIC COMMERCIAL AIRCRAFT |
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ICAS2020_0620: X.-Y. Zhang¹, Z.-H. Gao¹, T. Lei¹, X.-B. Zhang¹, W. Zhang¹; ¹Northwestern Polytechnical University, China EXPERIMENTAL RESEARCH ON PROPULSION AND AERODYNAMIC CHARACTERISTICS OF A DUAL-BODY DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT |
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ICAS2020_0645: M.A. Rodriguez Diaz¹, E. Villani¹, P. Krus, Linköping University, Sweden; ¹Aeronautics Institute of Technology, Brazil GAZE-BASED INTERFACE FOR FLIGHT CONTROL: RESULTS OF INITIAL EXPERIMENTS WITH THE SYSTEM |
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ICAS2020_0663: F. Ding¹, J. Liu¹, W. Huang¹, S. Guo, Air Force Engineering University, China; ¹National University of Defense Technology, China AERODYNAMIC DESIGN THEORY AND METHODOLOGY FOR AN AIRFRAME-INLET INTEGRATED FULL-WAVERIDER VEHICLE |
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ICAS2020_0693: S. Görtz¹, C. Ilic¹, M. Abu-Zurayk¹, T. Wunderlich¹, M. Schulze¹, T. Klimmek¹, Ö. Süelözgen¹, T. Kier¹, A. Schuster¹, S. Dähne¹, M. Petsch¹, J. Häßy¹, R.-G. Becker¹, M. Siggel¹, J. Kleinert¹, R. Mischke¹, S. Gottfried¹; ¹DLR, Germany COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN |
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ICAS2020_0766: L. Di Ianni¹, L. Loiodice¹, D. Celestini¹, D. Tiberti¹, C. Baldon¹, P. Iavecchia¹, A. Saponaro Piacente¹, M. Prodan¹, S. Grendene¹, B. Barberis¹, L. Santoro¹; ¹Politecnico di Torino, Italy TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55X |
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ICAS2020_0781: F. Pollet¹, S. Delbecq¹, M. Budinger, INSA Toulouse/ICA, France; J.-M. Moschetta¹; ¹ISAE-SUPAERO, France DESIGN OPTIMIZATION OF MULTIROTOR DRONES IN FORWARD FLIGHT |
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ICAS2020_0840: N. Viola¹, R. Fusaro¹, D. Ferretto¹, O. Gori¹, B. Saracoglu², A.C. Ispir², C. Schram², V. Grewe³, J.F. Plezer³, J. Martinez³, M. Marini*, L. Cutrone*, G. Saccone*, S. Hernandez, University of La Coruna, Spain; K. Lammers, Netherlands Aerospace Centre, Netherlands; A. Vincent, The French Aerospace Lab ONERA, France; D. Hauglustaine, CNRS, France; B. Liebhardtº, F. Linkeº, D. Bodmerº; ¹Politecnico di Torino, Italy; ²Von Karman Institute for Fluid Dynamics, Belgium; ³Deutsches Zentrum für Luft- und Raumfahrt, Germany; *Centro Italiano Ricerche Aerospaziali, Italy; ºTechnical University of Hamburg Harburg, Germany H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS |
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ICAS2020_0851: H.-L. Liu¹, M.-H. Tang¹, A.-Y. Zhu¹, W. Kong¹, H.-C. Shi, The First Military Representative Office of the Air Force Equipm, China; ¹Chengdu Aircraft Industrial (Group) Co., Ltd, China RESEARCH ON BARYCENTER MEASUREMENT METHOD IN LAUNCH OF ROCKET-BOOSTED UNMANNED AERIAL VEHICLES |
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ICAS2020_0878: Z.-Q. Liu¹, W.-P. Song¹, Z.-H. Han¹, Y. Wang¹; ¹Northwestern Polytechnical University, China MULTIFIDELITY AERODYNAMIC/STEALTH DESIGN OPTIMIZATION METHOD FOR FLYING WING AIRCRAFT |
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ICAS2020_0970: S. Bijjahalli¹, A. Gardi¹, S. Hilton¹, R. Sabatini¹; ¹RMIT University, Australia A NOVEL DETECT-AND-AVOID APPROACH FOR UAS IN URBAN ENVIRONMENTS |
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ICAS2020_0997: P. Shiva Prakasha¹, N. Naeem¹, N. Cigal¹, P. Ratei¹, B. Nagel¹; ¹German Aerospace Center, Germany EXPLORATION OF AERIAL FIREFIGHTING FLEET EFFECTIVENESS AND COST BY SYSTEM OF SYSTEMS SIMULATIONS |
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ICAS2020_1101: C. Ma¹, J.T. Si¹, Y.C. Chen, Commercial Aircraft Corporation of China, China; ¹Shanghai Aircraft Design and Research Institute, China BENEFIT ANALYSIS OF AIR REFUELING IN ULTRA LONG ROUTE AIRLINER OPERATION |
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ICAS2020_1110: S.S. Zhang¹, Z.Q. Wan¹, X.Z. Wang, Institute of Unmanned System, Beihang University, China; Y.Z. Liu, China North Ind Grp Corp, Nav & Control Technol Inst, China; ¹School of Aeronautic Science and Engineering, Beihang University, China TOPOLOGY OPTIMIZATION FOR WING STRUCTURE OF HYPERSONIC VEHICLE |
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ICAS2020_1123: X. Chen¹, A. Riaz¹, M.D. Guenov¹; ¹Cranfield University, United Kingdom CLOUD-BASED ENVIRONMENT FOR AIRCRAFT DESIGN COLLABORATION |
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ICAS2020_1144: W. Su ¹, C. Dong¹, X.P. Wang, Shanghai Electro-Mechanical Engineering Institute, Shanghai, China; Y.T. Zuo, National Key Laboratory of Aerodynamic Design and Research, Nort, China; ¹Beijing Institute of Space Long March Vehicle, China AERODYNAMIC DESIGN OPTIMIZATION OF WAVERIDER-DERIVED VEHICLE |
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ICAS2020_1154: G.P. Qian¹, Y.H. Wang¹, C. Ma¹; ¹COMAC, China THE STUDY ON ANTI-ICING AREAS OF LEADING-EDGE SLATS IN MODERN CIVIL AIRCRAFT |
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ICAS2020_1155: C. Ma¹, Z.Y. Chen¹, C.H. Kong¹; ¹Shanghai Aircraft Design and Research Institute, China FAST ITERATIVE SIMULATION OF AIRLINER WING PLANFORM CONCEPTUAL DESIGN |
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ICAS2020_1160: S.S. Liu¹, Q. You¹, Z.K. Liu², X. Liu², Y.W. Gui²; ¹State Key Laboratory of Aerodynamics, China; ²China Aerodynamics Research and Development Center, China A NOVEL RBF DATA TRANSFER METHOD BASED ON PCA GEOMETRIC FEATURE EXTRACTION |
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ICAS2020_1185: W. Yang, National University of Defense Technology, China; L. Yu¹, W.H. Wu¹, Z.L. Fan¹; ¹China Aerodynamics Research and Development Center, China INTEGRATED AERODYNAMIC DESIGN OF PROPELLER POSITION AND WING SHAPE AT A LOW REYNOLDS NUMBER |
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ICAS2020_1194: P. Wegener, DLR - German Aerospace Center, Germany INTEGRATION OF FUSELAGE-MOUNTED OVER-WING ENGINES ON A MID-RANGE AIRCRAFT |
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ICAS2020_1195: R. Fusaro¹, O. Gori¹, D. Ferretto¹, N. Viola¹, P. Roncioni², M. Marini²; ¹Politecnico di Torino, Italy; ²CIRA, Italy INTEGRATION OF AN INCREASING-FIDELITY AERODYNAMIC MODELLING APPROACH IN THE CONCEPTUAL DESIGN OF HYPERSONIC CRUISER |
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ICAS2020_1217: P. Brusberg¹, A.C. Doberts¹, T.M. Jansen¹, T. Witt¹; ¹HAW Hamburg, Germany LANDING PLATFORM FOR URBAN AIR MOBILITY VEHICLES INTEGRATED INTO PARKING LOT INFRASTRUCTURE IN DENSELY BUILT-UP AREAS |
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ICAS2020_1219: P. Gili¹, M. Civera¹, R. Roy¹, S. Cibrario Bertolotti¹, D. Cosenza¹, A. Gili¹, C. Surace, Department of Structural, Geotechnical and Building Engineering,, Italy; ¹Department of Mechanical and Aerospace Engineering, Politecnico , Italy DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: CONTROL, ALIMENTATION, AND PROPULSION SYSTEMS |
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ICAS2020_1221: L. Kiszkowiak¹, A. Olejnik¹, A. Dziubinski, Lukasiewicz Research Network – Institute of Aviation, Poland; P. Zalewski¹; ¹Military University of Technology, Poland THE USE OF REVERSE ENGINEERING AND COMPUTATIONAL FLUID DYNAMICS METHODS IN THE PRELIMINARY DESIGN OF A LOW COST SATELLITE LAUNCH SYSTEM |
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ICAS2020_1241: A. Hull¹, A. Sudol¹, D. Mavris¹; ¹Georgia Institute of Technology, United States QUANTIFICATION OF OPERATIONAL EFFECTIVENESS FOR TECHNOLOGY EVALUATION |
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ICAS2020_1255: Y. Zhao¹, P. Liu¹, Q. Qu¹; ¹Beihang University, China ESTIMATION OF STATIC AND DYNAMIC FLOATATION CHARACTERISTICS DURING AIRCRAFT DITCHING |
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ICAS2020_1258: M. Fioriti¹, F. Di Fede¹, S. Corpino¹, P. Iodice², G. Cerino²; ¹Politecnico di Torino, Italy; ²LEONARDO Aircraft Division, Italy ON-BOARD SYSTEM ARCHITECTURES FOR HYBRID/ALL-ELECTRIC REGIONAL AIRCRAFT |
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ICAS2020_1259: C. Cabaleiro¹, M. Fioriti¹, L. Boggero², S. Corpino¹, P.D. Ciampa², B. Nagel²; ¹Politecnico di Torino, Spain; ²German Aerospace Center (DLR), Germany ASSESSMENT OF NEW TECHNOLOGIES IN A MULTI-DISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION ENVIRONMENT INCLUDING RAMS AND COST DISCIPLINES |
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ICAS2020_1310: M.F. Abdul Hamid¹, A.R. Abu Talib¹, A.S. Mohd Rafie¹, H. Djojodihardjo, The Institute for the Advancement of Aerospace Science and Tech, Indonesia; ¹Universiti Putra Malaysia, Malaysia CIRCULATION CONTROL AIRCRAFT: RECENT DEVELOPMENTS OF THE CHANNEL-WING DESIGN |
2 - Systems Engineering and Integration |
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ICAS2020_0053: H. Bihai¹, H. Zhen¹; ¹COMAC, China AIRCRAFT CRUISE PERFORMANCE DESIGN INTEGRATION BASED ON SYSTEM ENGINEERING |
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ICAS2020_0077: W. Cheng¹, C. Xing¹, J. Xu¹, G. Song¹; ¹Aviation Industry Development Research Center of China , China RESEARCH ON ARCHITECTURE FRAMEWORK MODEL BASED EVALUATION INDEX FOR AVIATION SCIENCE & TECHNOLOGY MANAGEMENT |
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ICAS2020_0134: M. Fuchs¹, C. Hesse¹, J. Biedermann¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany FORMALIZED KNOWLEDGE MANAGEMENT FOR THE AIRCRAFT CABIN DESIGN PROCESS |
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ICAS2020_0168: L. Liu¹, X.F. Yang¹, G.M. Xiao¹, Q. Li, School of Mechanical Engineering, Shanghai Jiao Tong University, China; D. Wei¹, W. Tang, Southwest University of Science and Technology, China; ¹State Key Laboratory of Aerodynamics, CARDC, China AN ENERGY BASED WEIGHT ESTIMATION TECHNIQUE OF TWO-STAGE-TO-ORBIT REUSABLE LAUNCH VEHICLES |
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ICAS2020_0193: L. Boggero¹, P.D. Ciampa¹, B. Nagel¹; ¹DLR, Germany THE APPLICATION OF THE AGILE 4.0 MBSE ARCHITECTURAL FRAMEWORK FOR THE MODELING OF SYSTEM STAKEHOLDERS, NEEDS AND REQUIREMENTS |
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ICAS2020_0200: J. Wang¹, J. Mao¹, Q. Zhou¹; ¹Chinese Aeronautical Radio and Electronics Research Institute, China ARCHITECTURE INTEGRATION OF FUTURE ATM SYSTEM BASED ON META-MODEL |
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ICAS2020_0203: J.H. Bussemaker¹, P.D. Ciampa¹, B. Nagel¹; ¹DLR, Germany SYSTEM ARCHITECTURE DESIGN SPACE MODELING AND OPTIMIZATION ELEMENTS |
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ICAS2020_0252: W.Y. Cheng¹, C.G. Xing¹, G. Song¹; ¹Aviation Industry Development Research Center of China , China A CONTRASTIVE STUDY OF STANDARD SPECIFICATION FOR TECHNOLOGY READINESS ASSESSMENT |
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ICAS2020_0416: H. Liu¹, M. Li¹, R. Zhu¹, Q. Ding², L. Zhou²; ¹Science and Technology on Electro-optic Control Laboratory, China; ²Beijing Institute of Technology, China STRATEGIES TO ENHANCE CONFIGURATIONS FOR HIGH-PRECISION MULTI-DISCIPLINARY OPTIMIZATION |
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ICAS2020_0433: L. Su¹, H. Zhou¹, Y. Cheng¹, L. Du¹; ¹AEAC, China ARCHITECTURE OF PRODUCT RESEARCH AND DEVELOPMENT SYSTEM FOR COMPLICATED PRODUCTS ENGINEERING |
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ICAS2020_0485: C.-J. He¹, L.-I. Wang¹, J.-H. Yang¹; ¹xi’an aircraft design institute, China COMPREHENSIVE REDUNDANCY MANAGEMENT AND VERIFICATION STRATEGY FOR TASK-BASED AIR MANAGEMENT SYSTEM |
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ICAS2020_0489: H. Hu¹, J. Mao¹, D. Hu¹; ¹China Aeronautical Radio Electronics Research Institute, China GREENER ATM SYSTEM ARCHITECTURE RESEARCH BASED ON COMPLEX SYSTEM ENGINEERING METHOD |
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ICAS2020_0549: J. Zang¹, J.Q. Zhu¹; ¹Chinese Aeronautical Establishment, China SOS BEHAVIOR MODEL TRANSFORMATION FOR AIRCRAFT TOP-LEVEL DEMONSTRATION |
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ICAS2020_0581: Y. Guo¹, C. Ma¹, X. Dong¹; ¹Northwestern Polytechnical University, China RESEARCH ON SELECTION METHODS FOR AIRCRAFT LANDING GEAR SYSTEM HEALTH FEATURE PARAMETERS |
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ICAS2020_0633: Y.-G. Chai¹, J. Tao¹, S.-P. Guo¹; ¹AECC Commercial Aero Engine co. LTD, China RESEARCH ON AERO-ENGINE COLLABORATIVE DESIGN PROCESS BASED ON SYSTEM ENGINEERING |
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ICAS2020_0720: Y.X. Che, Liaoning, China APPLICATION OF MBSE IN AERO-ENGINE STRUCTURAL PARAMETER CALCULATING SYSTEM |
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ICAS2020_0744: S. Chang¹, D.W. Xia¹, Z.K. Yan¹, X. Jiang¹, J. Tang¹, H.T. Zhong¹; ¹COMAC, China SYSTEM ENGINEERING THINKING ON COMMERCIAL AIRCRAFT FLIGHT TEST |
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ICAS2020_0795: Q. Li¹, Y. An¹; ¹AVIC Xi'an Aircraft Industry Group Company LTD., China RESEARCH ON FUNCTIONAL HAZARD ASSESSMENT TECHNOLOGY OF MILITARY AIRCRAFT |
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ICAS2020_0803: J. Shen¹, Q. Zhou¹, B.F. Li¹, C. Chen¹; ¹Chinese Aeronautical Radio and Electronics Research Institute, China CO-SIMULATION OF SYSML AND SIMULINK/MODELICA USING FMI |
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ICAS2020_0857: V.I. Budzko, FRC, Russia; A.V. Kan¹, G.G. Kazarinov¹, I.S. Mikhalyn ¹; ¹NRC Zhukovsky, Russia CREATING A MULTI-FUNCTIONAL EXPERT ANALYTICAL SYSTEM IN THE AIRCRAFT INDUSTRY AND THE FORMATION OF GENERAL REQUIREMENTS |
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ICAS2020_0958: V. Vercella¹, R. Fusaro¹, N. Viola¹; ¹Politecnico di Torino, Italy TECHNOLOGY ROADMAPS FOR THE DEVELOPMENT OF FUTURE HIGH-SPEED TRANSPORTATION SYSTEMS |
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ICAS2020_0980: P. Krus, Linköping university, Sweden; R. Braun, ICAS2020_0980, Sweden; E. Villani, Instituto Tecnológico de Aeronáutica, Brazil HYBRID MODELLING FOR FULL MISSION SIMULATION |
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ICAS2020_1212: S.F. Zhu¹, P.P. Xing¹; ¹COMAC Beijing Aircraft Technology Research Institute, China MODEL-BASED VIRTUAL INTEGRATED TEST METHOD FOR AVIONICS SYSTEM |
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ICAS2020_1229: A. Oprea¹, R. Hällqvist¹, L. Knöös Franzén², M. Eek¹, I. Staack², H. Gavel¹; ¹Saab Aeronautics, Sweden; ²Linköping University, Sweden CONNECTING SYSTEM SIMULATION TO AIRCRAFT CONCEPT DEVELOPMENT |
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ICAS2020_1232: Z.C. Yao¹, L.B. Liu¹; ¹Shanghai Aircraft Design and Research Institute, Shanghai, China RESEARCH ON AIRCRAFT-LEVEL PHYSICAL INTEGRATION VERIFICATION TEST TECHNOLOGY |
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ICAS2020_1244: B. Wu¹, X.D. Qui¹; ¹NUAA, COMAC SADRI, China THE CIVIL AIRCRAFT DEVELOPMENT PROJECT RISK MANAGEMENT RESEARCH |
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ICAS2020_1293: A. Liu, China A DEEP LEARNING AND ONTOLOGY BASED FRAMEWORK FOR TEXTUAL REQUIREMENTS ANALYSIS AND CONCEPTUAL MODEL GENERATION |
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ICAS2020_1309: B. Xue, China; B. Luo, China; Z.J. Zhan, China; Y.H. Wang, China A NEW SERVICE-ORIENTED ARCHITECTURE DESIGN METHOD FOR AVIONICS SOS |
3.1 - Aerodynamics – CFD Methods and Validation |
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ICAS2020_0021: F. Cui, Innovation & Research Institute of HIWING Technology Academy, China; H. Zhang, HIWING Technology Academy, China AERODYNAMICS CHARACTERISTICS STUDY ON A NATURE LAMINAR FLOW AIRFOIL OF NEAR-SPACE VEHICLE AT LOW REYNOLDS NUMBERS |
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ICAS2020_0033: I. Bosnyakov¹, S. Bosnyakov¹, S. Mikhaylov¹, V. Podaruev¹, A. Troshin¹, A. Wolkov¹; ¹Central Aerohydrodynamic Institute, Russia VALIDATION OF A DISCONTINUOUS GALERKIN BASED DES SOLVER IN FLOW PROBLEMS USING HIGH PERFORMANCE COMPUTING |
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ICAS2020_0037: M. Ivanov¹, V. Mamaev¹, J. Li², G. Zheng²; ¹CIAM, Russia; ²NWPU, China ADVANCED WEAK SOLUTIONS IN FLUID DYNAMICS AND THEIR NUMERICAL COMPUTATIONS WITH AERODYNAMIC HEATING |
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ICAS2020_0072: A. Shi, NORTHWESTERN POLYTECHNICAL UNIVERSITY, China; E. Dowell, DUKE UNIVERSITY, United States A BENCHMARK METHOD FOR PREDICTING OBLIQUE SHOCK STRUCTURE |
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ICAS2020_0080: R.C. Gonzalez, Cranfield Unversity, United Kingdom; S.A. Prince, Cranfield University, United Kingdom ON THE ASSESSMENT OF CFD METHODS FOR VORTICAL FLOWS |
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ICAS2020_0081: M. Bonnici¹, S. Prince¹, K. Garry¹; ¹Cranfield University, United Kingdom TURBULENCE MODEL ASSESSMENT OF THE SEPARATED FLOW IN THE STANFORD DIFFUSER |
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ICAS2020_0102: D. Liu, School of Aeronautics,Northwestern Polytechnical University, China; W.Q. Yang¹, B.F. Song¹; ¹Research & Development Institute of NWPU in Shenzhen, China NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING WITH SLOTTED-TIP |
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ICAS2020_0107: V.I. Shalaev¹, S.V. Alexandrov¹, A.V. Vaganov², M.A. Starodubtsev²; ¹Moscow Institute of Physics and Technology, Russia; ²Central aerohydrodynamic Institute, Russia LONGITUDINAL VORTEX FORMATION IN HYPERSONIC BOUNDARY LAYER ON BLUNTED DELTA WING AND ITS EFFECT ON FLOW CHARACTERISTICS |
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ICAS2020_0164: A. Aprovitola, University of Campania , Italy; L. Iuspa¹, G. Pezzella¹, A. Viviani¹; ¹University of Campania, Engineering Department., Italy OPTIMAL DESIGN OF A NEXT GENERATION HIGH-LIFT REUSABLE RE-ENTRY VEHICLE |
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ICAS2020_0165: T. Bykerk, Honorary Associate, the University of Sydney, Australia, Australia; G. Pezzella, University of Campania, Engineering Department. , Italy; D. Verstraete, University of Sydney, School of Aerospace, Australia; A. Viviani, University of Campania, Engineering Department., Italy LONGITUDINAL AND LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE HIGH-SPEED VEHICLE |
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ICAS2020_0171: S. De Lucas Bodas¹, J. Narbona Gonzalez¹, V. Ossorio Contreras¹, J.J. Guerra Crespo¹, D.E. Funes Sebastian¹, L.P. Ruiz Calavera¹; ¹Airbus Defence & Space, Spain EXPERIMENTAL VALIDATION OF NUMERICAL PREDICTION OF WING-PROPELLER AERODYNAMIC INTERACTION |
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ICAS2020_0232: S.V. Rohani¹, A. Jahangirian¹; ¹Amirkabir University of Technology, Iran MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF A CIVIL AIRCRAFT FUSELAGE |
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ICAS2020_0285: J. Su, China; Z. Tang, China; J. Tian, China; B. Pan, China; S. Luo, China CFD OPTIMUM DESIGN OF SUPERSONIC EJECTOR SYSTEM STRUCTURE OF TEST CELL |
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ICAS2020_0286: Y.-M. Du, Shenyang Aerospace University, China; Z.-H. Gao¹, C. Pang¹; ¹Northwestern Polytechnical University, China TRANSITION PREDICTION FOR TRANSPORT AIRCRAFT CONFIGURATIONS BASED ON OVERSET GRID |
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ICAS2020_0291: X. Liu, China; H. Jin, China; D. Qiu, China; Y. Yin, China EFFECT OF INTER-STAGE BLEEDING ON FLOW STABILITY OF A MULTI-STAGE COMPRESSOR |
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ICAS2020_0311: J. Meyer¹, P. Okfen¹, C. Bil¹; ¹RMIT University, Australia OPTIMISATION OF VORTEX GENERATORS FOR STALL SPEED REDUCTION |
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ICAS2020_0315: H. Chen, China; X. Yuan, China; S. Meng, China; R. Hua, China; Z. Tang, China; L. Bi, China SIMULATION OF HIGH REYNOLDS NUMBER VISCOUS FLOW BASED ON ADAPTIVE CARTESIAN GRID |
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ICAS2020_0349: Z. Qian¹, Y. Leng¹; ¹AVIC Aerodynamics Research Institute, China ATMOSPHERIC TURBULENCE EFFECTS ON SONIC BOOM PROPAGATION |
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ICAS2020_0388: Y.-H. Yin¹, Y.-F. Zhang¹; ¹Tsinghua University, China RESEARCH OF TURBULENCE MODELING BASED ON MACHINE LEARNING |
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ICAS2020_0402: M. Heidari Soreshjani, Amirkabir University of Technology, Iran; A. Jahangirian, Amirkabir university of technology, Iran MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF A CIVIL AIRCRAFT WINGLET |
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ICAS2020_0441: Y.M. Tsirkunov¹, D.A. Romanyuk¹, S.V. Panfilov¹; ¹Baltic State Technical University, Russia MODELING AND SIMULATION OF DUSTY GAS FLOW IN AERODYNAMICS |
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ICAS2020_0455: C. Baldon¹, R. Indelicato¹, N. Bottino¹, M. Sinisi¹, F. Carrone¹, G. Cantanna¹, E. Cestino¹, V. Sapienza, Aeronautical Consultant, Italy; ¹Politecnico di Torino, Italy S55 PROJECT - CFD ANALYSIS OF AN HISTORICAL SEAPLANE |
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ICAS2020_0529: I.V. Egorov, Russia; A.V. Novikov, Russia; N.K. Nguen, Vietnam HYBRID NUMERICAL SCHEMES IN PREDICTION OF HIGH-SPEED LAMINAR-TURBULENT TRANSITION |
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ICAS2020_0543: H.-L. Jin, China; D.-B. Qiu, China; Y.-Q. Yin, China; X.-Q. Zou, China APPLICATION OF A SKEWED-SLOT CASING TREATMENT IN A HIGH-LOADING AXIAL-CENTRIFUGAL COMPRESSOR |
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ICAS2020_0555: A. Sultan¹, A. Maqsood¹, T.H. Go, Raytheon Missile Systems, United States; R. Riaz¹; ¹National University of Sciences & Technology, Pakistan NUMERICAL INVESTIGATION OF WING ROCK PHENOMENON ON LOW ASPECT RATIO RECTANGULAR WINGS AT LOW REYNOLDS NUMBER |
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ICAS2020_0612: F. Sartor¹, M. Martin¹, C. Riveiro Moreno¹, J. Dandois¹; ¹ONERA, France NUMERICAL SIMULATIONS OF TRANSONIC BUFFET ON A HALF WING-BODY CONFIGURATION |
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ICAS2020_0632: H.-L. Jin¹, J. Zhang¹, J.-F. Wu¹, D.-B. Qiu¹, Y.-Q. Yin¹; ¹AECC Hunan Aviation Powerplant Research Institute, China DESIGN AND TEST OF A HIGH SLOPE ANGLE INTERMEDIATE DUCT BETWEEN LOW-PRESSURE COMPRESSOR AND HIGH-PRESSURE COMPRESSOR |
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ICAS2020_0636: Z.-P. Li, AECC Shenyang Engine Research Institute, China DISTORTION PLATE DESIGN, SIMULATION VALIDATION AND TEST SCHEME FOR STABILITY ANALYSIS ON A FAN COMPONENT OF AN AEROENGINE |
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ICAS2020_0677: T. Imamura, The University of Tokyo, Japan; Y. Tamaki, Tohoku University, Japan UNSTEADY FLOW SIMULATION AROUND MAIN LANDING GEAR USING HIERARCHICAL CARTESIAN GRID METHOD WITH IMMERSED BOUNDARY METHOD |
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ICAS2020_0686: J. Tang¹, J. Zhang¹, N.-C. Zhou¹, B. Li¹, P.-C. Cui¹; ¹China Aerodynamics Research and Development Center, China STALL PREDICTION OF AIRCRAFT WITH ADAPTIVE HYBRID MESH |
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ICAS2020_0704: W.B. Li¹, K.C. Li, Aviation Industry Corporation of China, China; C. Song¹, H.L. Ma¹, Y.Y. Wang¹; ¹China Aerodynamics Research and Development Center, China EFFECT OF DROPLET MVD ON ICING COLLECTION EFFICIENCY FOR A HELICOPTER BLADE |
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ICAS2020_0725: J.A.A. Lyrio¹, J.L.F. Azevedo², D.A. Rade¹, R.G. da Silva²; ¹Instituto Tecnológico de Aeronáutica, Brazil; ²Instituto de Aeronáutica e Espaço, Brazil STATIC AEROELASTIC COMPUTATIONS OF WING CONFIGURATIONS IN TRANSONIC FLOWS AT HIGH REYNOLDS NUMBERS |
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ICAS2020_0734: L.M.M.O. Carvalho, Instituto Tecnologico de Aeronautica, Brazil; R.G. da Silva¹, J.L.F. Azevedo¹; ¹Instituto de Aeronautica e Espaco, Brazil A CONTRIBUTION TO THE SIMULATION OF TRANSITIONAL FLOWS OVER AEROSPACE CONFIGURATIONS |
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ICAS2020_0794: L. Li, Northwestern Polytechnical University, China; Y. Liang¹, Y. Huai¹; ¹AVIC Aeronautics Computing Technique Research Institute , China AN INTELLIGENT STRUCTURED CHIMERA GRID APPROACH FOR MOVING OBJECTIVES |
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ICAS2020_0796: J. Yu¹, X.-J. Wu¹, D. Hao¹, H.-Y. Jia¹, S.-S. Liu¹; ¹CARDC, China NONLINEAR UNSTEADY AERODYNAMIC DESCRIPTIONS BASED ON IMPROVED GOMAN’S MODEL |
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ICAS2020_0805: X.F. Yang¹, Q. Li, Shanghai Jiao Tong University, China; Y.X. Du¹, G.M. Xiao¹, L. Liu¹, D. Wei¹, Y.W. Gui¹; ¹China Aerodynamics Research and Development Center, China MULTI-SCALE CFD/MD MODELLING OF HIGH-ENTHALPY FLOW/TPS INTERACTION AND ITS PRELIMINARY AERONAUTICAL APPLICATION |
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ICAS2020_0826: X.-W. Yang¹, Y. Pei¹, W.-Q. Yang¹, P. Nian¹, B.-F. Song¹; ¹Northwestern Polytechnical University, China NUMERICAL SIMULATION OF A BIO-INSPIRED FLEXIBLE FLAPPING-WING BASED ON EXPERIMENTAL MEASURED DEFORMATION |
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ICAS2020_0842: X. Wang¹, W.W. Zhang¹; ¹Northwestern Polytechnical University, China DATA FUSION UNSTEADY AERODYNAMIC MODELING BASED ON EXPERIMENTAL DATA |
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ICAS2020_0845: H. Chen¹, Y.F. Yang¹, P. Xue¹, X.X. Li¹, C. Dong¹, S.Z. Wang¹, M.X. Zhang¹; ¹Beijing Institute of Space Long March Vehicle, China INVESTIGATION ON DIFFERENT NUMERICAL SIMULATION METHODS OF ROCKET ENGINE |
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ICAS2020_0899: G.Y. Li, AVIC Xi'an Aircraft Industry Group Company LTD., China; T. Miao¹, B. Chen¹, F. Liu¹; ¹China Aerodynamics Research and Development Center, China AERODYNAMIC COEFFICIENT RESPONSE OF RECEIVER DURING AERIAL REFUELING PROCESS |
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ICAS2020_0906: H. Djojodihardjo, The Institute for the Advancement of Aerospace Science and Techn, Indonesia; M.A. Andira¹, R. Julistina¹, M.A. Moeljadi, Institute of Technology Bandung, Indonesia; ¹CCIT Group Indonesia, Indonesia FURTHER DEVELOPMENT OF COMPUTATIONAL STUDY ON COANDA BLANKET CURVATURE EFFECTS ON HALF SPHERICAL COANDA DEVICE |
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ICAS2020_0909: X.L. Gao¹, Q.B. Zhang, National Defense Technology University, China; Z.H. Li, Beijing Pioneering Innovation Center of China Aerodynamics Resea, China; Q. Chen¹, W.K. Wang, AVIC Aerospace Life-Support Industries. Ltd, China; ¹China Aerodynamic R&D Center, China RESEARCH ON FSI DYNAMIC CHARACTERISTICS OF PARAFOIL TRAILING EDGE DEFLECTION |
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ICAS2020_0944: X.L. Chen¹, F. Song¹; ¹Tsinghua University, China RESEARCH OF THE HYPERSONIC BOUNDARY LAYER INSTABILITIES AND TRANSITION WITH THERMAL-CHEMICAL NON-EQUILIBRIUM EFFECTS |
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ICAS2020_1063: M. Li, No.2 High School of East China Normal University, China; H. Xu, Fudan University, China INVESTIGATION OF AERODYNAMIC INTERACTIONS BETWEEN NACA0012 AIRFOILS IN TANDEM |
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ICAS2020_1073: H.-Y. Zhang, State Key Laboratory of Aerodynamics, China; W.-G. Zong¹, Y.-H. Zhu¹, Y.-W. Gui, Computational Aerodynamics Institute, CARDC, China; B. Qiu, State Key Laboratory of Aerodynamics, China; ¹University of Sichuan, China GEOMETRICAL PARAMETER STUDY OF A HYPERSONIC VERTICAL GAP FLOW |
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ICAS2020_1098: R.X. Xie¹, W.M. Sang¹; ¹Northwestern Polytechnical University, China A LOCAL CORRELATION-BASED ALGEBRAIC TRANSITION MODEL WITH COMPRESSIBILITY AND CROSSFLOW CORRECTION |
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ICAS2020_1106: W. Jin¹, S.E. Peng¹, J.M. Wu¹, J. Lei¹, W.T. Ji¹; ¹Xian Jiaotong University, China FLOW AND HEAT TRANSFER MECHANISM OF JET IMPINGEMENT COOLING ONTO MID-CHORD REGINE OF TWISTED BLADE |
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ICAS2020_1118: H.-Y. Li¹, X. Zhao¹, K. You¹, S.-Z. Zhao¹, Y.-F. Lin, China Helicopter Research and Development Institute, China; ¹Northwestern Polytechnical University, China AERODYNAMIC MODELING AND FLIGHT PERFORMANCE RESEARCH OF THE COAXIAL RIGID HELICOPTER IN POP-UP PROCESS |
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ICAS2020_1125: S.-Z. Zhao¹, X. Zhao¹, K. You¹, M.-H. Kang¹, Y.-F. Lin, China Helicopter Research and Development Institute, China; ¹Northwestern Polytechnical University, China HELICOPTER ROTOR AERODYNAMIC PERFORMANCE PREDICTION BASED ON FLOW SIMULATION AROUND AIRFOILS |
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ICAS2020_1150: X.-Y. Lang¹, B.-F. Song¹, W.-Q. Yang¹; ¹Northwestern Polytechnical University, China NUMERICAL SIMULATION OF PITCHING MOTION EFFECTS ON THE AERODYNAMIC PERFORMANCE OF DRAGONFLY-LIKE FLAPPING WING |
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ICAS2020_1151: S.-E. Peng¹, W. Jin¹, J.-M. Wu¹; ¹Xi’an Jiaotong University, China NUMERICAL STUDY ON COOLING CHARACTERISTICS IN CHANNELS WITH PIN FIN ARRAYS UNDER HIGH TEMPERATURE/PRESSURE CONDITIONS |
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ICAS2020_1167: Z.C. Zhu¹, B.F. Song¹, W.Q. Yang¹, X.Y. Lang¹; ¹Northwestern Polytechnical University, China NUMERICAL SIMULATION OF SWEEPING MOTION EFFECTS ON THE HOVERING DRAGONFLIES |
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ICAS2020_1172: C. Tang¹, W.Q. Yang¹, B.F. Song¹, X.Y. Lang¹; ¹Northwestern Polytechnical University, China AERODYNAMIC ANALYSIS OF DRAGONFLY WINGS SPACE DISTRIBUTION ON THREE-DIMENSIONAL DURING HOVERING FLIGHT |
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ICAS2020_1176: Q. You¹, X.-F. Yang¹, L. Zeng¹, Y.-W. Gui¹, Y.-X. Du¹, L. Liu¹, G.-M. Xiao¹; ¹China Aerodynamics Research and Development Center, China COUPLED HEAT TRANSFER CHARACTERISTICS ON CHEMICALLY REACTING INTERFACE OF HIGH-SPEED AIRCRAFT CONSIDERING WALL INJECTION |
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ICAS2020_1179: L.B. Guo¹, G.Z. Cao, Nanjing University of Aeronautics and Astronautics, China; H.P. Zhang¹; ¹Shanghai Aircraft Design and Research Institute, China NUMERICAL SIMULATION OF RIDGE ICE AND AERODYNAMIC EFFECT UNDER THERMAL ANTI-ICE |
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ICAS2020_1251: G.Y. Pan¹, X. Yu¹, Y. Ii¹, Y.X. Zhao¹; ¹AECC SHENYANG ENGINE RESEACH INSTITUE, China THE FLOW AND HEAT TRANSFER OF ANALYSIS TO ANNULAR CAVITY IN ENGINE CASE |
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ICAS2020_1261: Z.-Y. Xiao¹, L. Zhang¹, X.-D. Cui¹, B. Mou¹; ¹China aerodynamics research and development center , China METHODS OF DIRECTIONAL COARSENING FOR UNSTRUCTURED GRIDS AND APPLICATIONS |
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ICAS2020_1263: S. Hu¹, C. Jiang¹, Z. Gao¹, C.-H. Lee¹; ¹Beihang University, China AN ACCELERATION METHODOLOGY BASED ON DISTURBANCE REGION UPDATE METHOD FOR STEADY COMPRESSIBLE FLOWS |
3.2 - Experimental Aerodynamics |
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ICAS2020_0040: Q. Liu¹, Z. Luo¹, Z. Liu¹, X. Deng¹, P. Cheng¹; ¹National University of Defense Technology, China EXPERIMENTAL INVESTIGATION ON SUPERSONIC BOUNDARY LAYER TRANSITION INDUCED BY SINGLE/MULTI- ROUGHNESS ELEMENTS |
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ICAS2020_0101: A. Krzysiak, Lukasiewicz Research Network – Institute of Aviation, Poland; A. Olejnik¹, L. Kiszkowiak¹; ¹Faculty of Mechatronics, Armament & Aerospace; Military Universi, Poland EXPERIMENTAL INVESTIGATION OF DAMAGE WING IMPACT ON THE AIRLINER AERODYNAMIC CHARACTERISTICS |
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ICAS2020_0116: M. Cerny¹, N. Herzog, Rolls-Royce Deutschland Ltd & Co KG, Germany; C. Breitsamter¹; ¹Technical University of Munich, Germany ANALYSIS OF A WING-TIP-MOUNTED SMALL-SCALE PROPELLER CONFIGURATION UNDER NON-AXIAL INFLOW CONDITIONS |
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ICAS2020_0138: Z.-B. Zhang¹, F.-L. Gao¹, H. Wu¹, Y.-H. Chen¹; ¹Shenyang Engine Research Institute, China MEASUREMENT AND ANALYSIS OF INTER-STAGE FLOW FIELD IN A HIGH-LOAD AXIAL MULTISTAGE COMPRESSOR |
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ICAS2020_0140: Z.-B. Zhang¹, M.-S. Yang¹, H. Wu¹, M. Wang¹; ¹Shenyang Engine Research Institute, China EXPERIMENTAL INVESTIGATION ON FLOW CHARACTERISTICS IN COMPRESSOR ACOUSTIC-CAVITY RESONANCE TEST FACILITY BY PIV |
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ICAS2020_0149: D. Veerasamy, Khalifa University, United Arab Emirates; C. Atkin, University of East Anglia, United Kingdom AN OBJECTIVE APPROACH FOR MEASURING INTERMITTENCY IN THE TRANSITIONAL BOUNDARY LAYER |
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ICAS2020_0182: X.W. Xu¹, S.H. Yi¹, J.H. Han¹, W.P. Zheng¹, Z.H. Xia¹; ¹National University of Defense Technology, China EXPERIMENTAL INVESTIGATION OF HYPERSONIC BOUNDARY LAYER TRANSITION ON A SHARP CONE UNDER DIFFERENT ANGLES-OF-ATTACK |
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ICAS2020_0227: J. Pflüger¹, K. Hirschmann¹, C. Breitsamter¹; ¹Chair of Aerodynamics and Fluid Mechanics, TUM, Germany EXPERIMENTAL INVESTIGATIONS OF A FULL MODEL WITH ADAPTIVE ELASTO-FLEXIBLE MEMBRANE WINGS |
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ICAS2020_0249: S.L. Osipova, Russia INFLUENCE OF VARIABLE WALL PERFORATION RATIO ON BOUNDARY LAYER PARAMETERS AT TRANSONIC SPEEDS |
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ICAS2020_0264: B.B. Wei¹, Y.W. Gao¹, D. Li¹; ¹Northwestern Polytechnical University, China APPLIED RESEARCH ON SUPERVISED LEARNING IN THE JUDGMENT OF AIRFOIL TRANSITION |
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ICAS2020_0429: F.L. Gao¹, M.S. Yang¹, Z.B. Zhang¹, Y. Chen¹; ¹AECC Shenyang Engine Research Institute, China EXPERIMENT AND THEORETICAL ANALYSIS OF A TYPE OF NON-SYNCHRONOUS VIBRATION IN A HIGH PRESSURE COMPRESSOR |
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ICAS2020_0483: L. Zhang, Beihang University, China; Z. Liu¹, F. Cen¹, Y. Jiang¹, H. Sun¹; ¹China Aerodynamic Research and Development Center, China WIND-TUNNEL INVESTIGATION OF COMMERCIAL TRANSPORT AIRCRAFT STATIC AND DYNAMIC AERODYNAMIC CHARACTERISTICS AT EXTREME FLIGHT CONDITIONS |
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ICAS2020_0492: L. Fan¹, H. Zhang¹; ¹China Aerodynamics Research and Development Center, China EXPERIMENTAL INVESTIGATION OF THE CHN-T1 MODEL IN FL-13 WIND TUNNEL OF CARDC AND DNW-LLF FACILITY |
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ICAS2020_0500: X. Li¹, Z. Liu¹, Z. Qian¹; ¹AVIC Aerodynamics Research Institute, China A STUDY OF SONIC BOOM TEST WITH NOZZLE PLUME INTERACTIONS |
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ICAS2020_0810: V.I. Chernousov¹, A.A. Krutov¹, E.A. Pigusov¹; ¹Central Aerohydrodinamic Institute (TsAGI), Russia STUDY ON AERODYNAMIC CHARACTERISTICS OF LIGHT CONVERTIBLE AIRCRAFT MODEL |
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ICAS2020_0849: Z.C. Song¹, P.Q. Liu¹, H. Guo¹; ¹Beihang Univerisity, China MICROPHONE ARRAY TECHNIQUES FOR TRAILING EDGE NOISE BASED ON CONVOLUTIONAL NEUTRAL NETWORK |
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ICAS2020_0863: M. Bremm¹, R. Stephan¹, R. Hörnschemeyer¹, E. Stumpf¹; ¹RWTH Aachen University, Germany DYNAMIC TRAILING-EDGE FLAP MOVEMENT AS A NON-CONVENTIONAL AERODYNAMIC LIFT MECHANISM |
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ICAS2020_1170: X. Geng¹, X.P. Liu¹, Z.Y. Song¹, L. Zhang¹; ¹AECC Shenyang Engine Research Institute, China TOTAL TEMPERATURE MEASUREMENTS IN WATER INJECTION AND PRE-COMPRESSOR COOLING TECHNOLOGY |
3.3 - Basic Fluid Dynamics and Flow Control |
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ICAS2020_0108: V.I. Shalaev, Moscow Institute of Physics and Technology, Russia SINGULARITIES IN THE NEAR-WALL REGION OF 3D BOUNDARY LAYER AND THE FLOW STRUCTURE IN ITS VICINITY |
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ICAS2020_0114: Y. Luo, China; C.H. Wu, China; S.Q. Yuan, China; H. Tian, China; H. Li, China; S.H. Zhang, China COMPUTATIONAL STUDY OF THREE-DIMENSIONAL OPEN CAVITY FLOWS |
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ICAS2020_0236: P.W.C. Wong, IHS Markit ESDU, United Kingdom; M. Maina¹, S. Lawson¹; ¹ARA, United Kingdom HYBRID LAMINAR FLOW CONTROL (HLFC) RESEARCH AT AIRCRAFT RESEARCH ASSOCIATION (ARA), PAST, PRESENT AND FUTURE |
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ICAS2020_0301: W. Stalewski, Lukasiewicz Research Network- Institute of Aviation, Poland IMPROVEMENT OF HELICOPTER PERFORMANCE THROUGH PULSE AIR JETS BLOWN FROM THE TRAILING EDGE OF MAIN ROTOR BLADES |
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ICAS2020_0305: D. Sun¹, C. Li¹, H.-Y. Cai, School of Aeronautics, Northwestern Polytechnical University, China; Q.-L. Guo¹, P.-X. Liu¹, X.-X. Yuan¹; ¹State Key Laboratory of Aerodynamics, China STUDY ON THE HEAT FLUX OF HYPERSONIC SHOCK WAVE BOUNDARY LAYER INTERACTION CONTROLLED BY A MICRO-RAMP VORTEX GENERATOR |
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ICAS2020_0414: C. Chen, China; J.-T. Huang, China; X. Chen, China EFFECTS OF ADVERSE PRESSURE GRADIENT ON THE BEHAVIOURS OF RESOLVENT MODE |
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ICAS2020_0436: B. Wang¹, X.D. Yang¹, B.F. Song¹, J.H. Xu¹; ¹School of Aeronautics, Northwestern Polytechnical University, China STUDY ON THE EFFECTS OF PROPLET GEOMETRIC PARAMETERS ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLER |
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ICAS2020_0516: L.-S. Hao¹, Y.-W. Gao¹, B.-B. Wei¹, B. Hu¹; ¹Northwestern Polytechnical University, China ANALYSIS AND CONTROL OF DYNAMIC STALL CHARACTERISTICS OF S809 AIRFOIL |
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ICAS2020_0523: T. Knopp¹, M. Novara¹, D. Schanz¹, W. Lühder¹, E. Schülein¹, R. Geisler¹, F. Philipp¹, M. Schroll², A. Krumbein¹, C. Willert², A. Schröder¹; ¹DLR AS, Germany; ²DLR AT, Germany MODIFICATION OF TURBULENCE MODELS FOR PRESSURE-INDUCED SEPARATION ON SMOOTH SURFACES USING THE DLR VICTORIA EXPERIMENT |
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ICAS2020_0656: P.V. Chuvakhov, Central Aerohydrodynamic Institue (TsAGI), Russia STABILIZATION OF SUPERSONIC BOUNDARY LAYERS IN THE PRESENCE OF FAVORABLE PRESSURE GRADIENT |
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ICAS2020_0657: P.V. Chuvakhov, Central Aerohydrodynamic Institue (TsAGI), Russia; A.V. Fedorov¹, I.O. Pogorelov¹; ¹Moscow Institute of Physics and Technology (MIPT), Russia MECHANISMS OF NATURAL LAMINAR-TURBULENT TRANSITION ON AN UNSWEPT WING IN SUPERSONIC FLIGHT |
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ICAS2020_0708: M. Jiang¹, M. Wang¹, F. He¹; ¹AVIC Chengdu Aircraft Design & Research Institute, China EXPERIMENTAL STUDY ON SUPERSONIC CAVITY ACOUSTICS |
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ICAS2020_0890: E.R. Gowree, ISAE-SUPAERO, France; C.J. Atkin, University of East Anglia, United Kingdom VIBRATION INDUCED EXCITATION OF INSTABILITY WAVES IN A BLASIUS FLOW |
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ICAS2020_0894: I.A. Amelyushkin¹, M.A. Kudrov¹, A.B. Miller¹, Y.F. Potapov¹, A.L. Stasenko¹, V.A. Zhbanov¹; ¹Central Aerohydrodynamic Institute, Russia EXPERIMENTAL INVESTIGATION, NUMERICAL AND MATHEMATICAL SIMULATION OF DISPERSE FLOWS IMPINGING ON AIRCRAFT SURFACE |
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ICAS2020_0928: H.W. Wang¹, Z. Huang¹, M.L. Yuan¹, X.H. Li¹, M. Zhang, Shanghai Aircraft Design and Research Institute, China; ¹China Academy of Aerospace Aerodynamics, China SUBSONIC WIND TUNNEL SMALL RIBLETS DRAG REDUCTION EXPERIMENT ON C919 FUSELAGE MODEL |
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ICAS2020_0949: A.M. Lipanov, Institute of Applied Mathematics RAS, Russia; I.I. Lipatov, TsAGI, Russia; S.A. Karskanov, Instiute of Mechanics, Germany PHISICAL AND MATHEMATICAL MODELS OF THE BUFFET ONSET |
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ICAS2020_0968: A. Novikov, TsAGI, MIPT, Russia; A. Fedorov, MIPT, Russia NUMERICAL SIMULATION OF THREE-DIMENSIONAL DISTURBANCES EVOLUTION IN SUPERSONIC FLOW OVER A WAVY SURFACE |
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ICAS2020_0979: E.P. Pereira¹, A. Esmaeili, Ferdowsi University of Mashhad, Iran; J.M.M. Sousa¹; ¹Instituto Superior Técnico, Portugal ENERGY HARVESTING FROM PIEZOELECTRIC FRINGES AT THE TRAILING-EDGE OF A FINITE WING WITH LEADING-EDGE TUBERCLES |
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ICAS2020_0988: G.P.G. Silva¹, J.P. Eguea¹, J.A.G. Croce, Federal Institute of Education, Science and Technology of São Pa, Brazil; F.M. Catalano¹; ¹Department of Aeronautical Engineering, University of São Paulo, Brazil HIGH-LIFT NOISE REDUCTION USING PLASMA ACTUATORS |
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ICAS2020_1140: S.Y. Du¹, R. Pang, AVIC Xi’an Flight Automatic Control Research Institute, China; W.M. Sang¹, G.J. Yang¹; ¹Northwestern Polytechnical University, China NUMERICAL SIMULATION STUDY ON BOUNDARY LAYER FLOW AND DRAG REDUCTION CHARACTERISTICS OF RIBLETS |
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ICAS2020_1171: Z.T. Chen ¹, Z.X. Jiao¹, Y.X. Shang¹, L.F. Zhao¹; ¹Beihang University, China ANALYSIS OF AERODYNAMIC COUPLING EFFECT IN CLOSE FORMATION FOR FLAPPING WINGS |
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ICAS2020_1189: J.J. Yang¹, Y.D. Zhang¹, P. Lv¹, T. Pagliaroli, Università Niccolò Cusano, Italy; ¹China Academy of Aerospace Aerodynamics, China NUMERICAL SIMULATION OF LOCAL LONG SHALLOW CAVITY EFFECT ON THE STABILITY OF A HYPERSONIC BOUNDARY LAYER |
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ICAS2020_1224: P.F. Shen ¹, H.Y. Cai, School of Aeronautics, Northwestern Polytechnical University, China; P.X. Liu¹, D. Sun¹, X.X. Yuan¹; ¹State Key Laboratory of Aerodynamics, China STUDY ON THE STATISTICAL CHARACTERISTICS OF SKIN FRICTION OF SHOCK WAVE/ TURBULENT BOUDARY LAYER INTERATION IN A HOLLOW FLARE CONFIGURATION AT MACH 6 |
3.4 - Applied Aerodynamics |
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ICAS2020_0016: F. Rasimarzabadi¹, M. Neuteboom¹, C. Clark¹, H. Martensson, GKN Aerospace Engine Systems, Sweden; ¹NRC, Canada AERODYNAMIC ANALYSIS OF A HIGH SPEED TEST RIG FOR USE IN ENGINE TEST FACILITIES |
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ICAS2020_0071: M. Zhong¹, J. Hua¹, X. Sun¹, S. Zheng¹, G. Wang¹, G. Zhang¹, H. Wang¹, Y. Li¹, X. Li¹, J. Bai, Northwestern Polytechnical University, China; ¹Chinese Aeronautical Establishment, China AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATION |
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ICAS2020_0078: K. Ma¹, S. Prince¹; ¹Cranfield University, United Kingdom ESTIMATION OF THREE-DIMENSIONAL BOUNDARY LAYER VELOCITY PROFILES ON SWEPT WINGS AND BLENDED WING BODIES |
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ICAS2020_0094: H. Zhao, Sun Yat-sen University, China; Z.H. Gao¹, L. Xia¹; ¹Northwestern Polytechnical University, China SPARSE POLYNOMIAL CHAOS EXPANSION BASED ON FULLY ADAPTIVE FORWARD-BACKWARD SELECTION METHOD |
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ICAS2020_0209: M. Thiele¹, D. Salassidis¹, M. Hornung¹; ¹Institute of Aircraft Design, Technical University of Munich, Germany PROPELLER WAKE - OBJECT INTERACTION USING A FREE WAKE MODEL UTILIZING LOCAL MESH SEPARATION |
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ICAS2020_0220: T. Gibson¹, B. Soucheleau¹, N. Rogers¹; ¹Airbus, United Kingdom BLADE - NATURAL LAMINAR FLOW FLIGHT TESTING |
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ICAS2020_0279: C. Sabater¹, S. Goertz¹; ¹German Aerospace Center (DLR), Germany ROBUST DESIGN OF 3D SHOCK CONTROL BUMPS TO TRANSPORT AIRCRAFT UNDER REALISTIC UNCERTAINTIES |
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ICAS2020_0351: Q. Li, Chinese Aeronautical Establishment, China; P. Wang ¹, B. Chen ¹; ¹AVIC Aerodynamics Research Institute, China AERODYNAMIC NOISE SIMULATION OF CIVIL AIRCRAFT LANDING GEARS BASED ON LES-SMARGORINSKY MODEL |
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ICAS2020_0417: A.X. Qiu¹, W.M. Sang¹, R. Pang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China NUMERICAL INVESTIGATION ON FLOW INTERFERENCE BETWEEN BLENDED-WING-BODY AIRCRAFT AND OVERHANGING NACELLE |
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ICAS2020_0424: Y.M. Yao¹, X.D. Yang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China AERODYNAMIC OPTIMIZATION DESIGN OF DOUBLE BLUNT ROTOR AIRFOIL WITH LARGE THICKNESS IN FORWARD AND REVERSE FLOW |
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ICAS2020_0435: N.V. Voevodenko¹, Y.G. Shvalev¹; ¹TsAGI, Russia METHODICAL STUDIES OF THE POSSIBILITY TO APPLY A NUMERICAL METHOD WITH BUILD-IN EMPIRICAL CRITERIA FOR DETERMIMING THE LAMINAR-TO-TURBULENT TRANSITION ON THE CONE SURFACE AT HIGH MACH NUMBERS |
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ICAS2020_0463: C. Song, China; W.-B. Li, China; Z. Zhou, China; H.-Y. Liu, China; X. Luo, China PARETO FRONT EXPLORATION USING MANIFOLD RECONSTRUCTION APPROACH FOR ROTORCRAFT AIRFOILS DESIGN |
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ICAS2020_0472: Z.-M. Xu¹, Z.-H. Han¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China NATURAL-LAMINAR-FLOW AIRFOIL DESIGN OPTIMIZATION CONSIDERING CROSSFLOW INSTABILITY WHEN CONFIGURED ON A SWEPT WING |
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ICAS2020_0476: Y. Zhang¹, Z.-H. Han¹, F. Liu¹, C.-Z. Xu¹; ¹Northwestern Polytechnical University, China AERODYNAMIC DESIGN OPTIMIZAITON OF HYPERSONIC WING OVER WIDE MACH-NUMBER RANGE CONSIDERING LIFT MATCHING |
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ICAS2020_0482: T. Wan¹, M.-H. Tsai¹; ¹Tamkang Univ., Taiwan, China NUMERICAL STUDY OF QUAD-ROTOR AIRCRAFT PERFORMANCE UNDER ADVERSE SITUATIONS |
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ICAS2020_0501: C.Y. Yan¹, Y.F. Zhang¹, M.H. Zhang, Shanghai Aircraft Design and Research Institute, China; ¹School of Aerospace, Tsinghua University, China MULTIPOINT OPTIMIZATION OF TRANSONIC NATURAL LAMINAR FLOW NACELLES |
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ICAS2020_0556: H. Ur Rahman¹, A. Maqsood¹, R. Riaz¹, L. Dala, Northumbria University, United Kingdom; ¹National University of Sciences & Technology, Pakistan NUMERICAL EVALUATION OF DYNAMIC STABILITY DERIVATIVES FOR HIGH LIFT DEVICES |
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ICAS2020_0595: J. Ruhland¹, F.M. Heckmeier¹, C. Breitsamter¹; ¹Technical University of Munich, Germany TRANSPORT AIRCRAFT WING INVESTIGATIONS AIMED ON WAKE VORTEX IMPACT BY OSCILLATING FLAPS |
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ICAS2020_0648: R. Vilumbrales-Garcia¹, M. Lone¹; ¹Cranfield University, United Kingdom RAPID THEORETICAL EVALUATION OF FORMATION FLIGHT PERFORMANCE |
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ICAS2020_0676: X. Hao¹, C. Su¹, B. Wang¹, Q.Q. Zhang¹; ¹China Academy of Aerospace Aerodynamics, China THE AERODYNAMIC OPTIMIZATION AND TRIM CHARACTERISTICS RESEARCH ON VARIABLE CAMBER WING OF WIDE-BODY CIVIL TRANSPORT |
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ICAS2020_0706: S.M. Pu¹, H.F. Wang¹, L.K. Cheng¹; ¹Northwestern Polytechnical University, China RESEARCH ON THE TRIGGERING CONDITIIONS OF EJECTABLE RECORDER FOR CIVIL AIRCRAFT |
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ICAS2020_0714: X.-X. Meng¹, M. Chang², J.-Q. Bai², M. Li¹; ¹School of Aeronautics, Northwestern Polytechnical University, China; ²Unmanned System Research Institute, Northwestern Polytechnical U, China DRAG REDUCTION ANALYSIS IN CLOSE-FORMATION FLIGHT |
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ICAS2020_0743: W.H. Wang, China; Q.C. Wang, China; C. Breard, China; Y.F. Sun, China SNGR BASED FAST ANALYSIS OF SLAT TRACK NOISE SOURCES |
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ICAS2020_0784: V. Bogatyrev, TsAGI, Russia INCREASING THE EFFECTIVENESS OF AN AERODYNAMICALLY BALANCED CONTROL SURFACE ON A MODIFIED AIRFOIL WITH REDUCED DRAG |
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ICAS2020_0787: C.-Z. Xu¹, Z.-H. Han¹, K.-S. Zhang¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China IMPROVED WEIGHTED GRADIENT-ENHANCED KRIGING MODEL FOR HIGH-DIMENSIONAL AERODYNAMIC MODELING PROBLEMS |
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ICAS2020_0839: J.-H. Xu¹, D. Li¹, W.-P. Song¹, Z.-H. Han¹, H.-J. Li¹; ¹Northwestern Polytechnical University, China DESIGN OPTIMIZATION OF AIRFOILS AT ULTRA-LOW REYNOLDS NUMBERS |
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ICAS2020_0985: A. Cato¹, M. Hayashi, Federal University of ABC, Brazil; J. Cavalcante¹, J. Qasem, Technical University of Munich, Germany; L. Kavabata¹, U. Costa¹, E. Volpe¹; ¹University of São Paulo, Brazil ADJOINT-BASED STUDY OF THE AERODYNAMIC CENTER SHIFT IN THE TRANSONIC FLOW REGIME |
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ICAS2020_1132: J. Niu¹, W. Sang¹, A. Qiu¹, Q. Guo¹, D. Li¹; ¹School of Aeronautics, Northwestern Polytechnical University, China AN OPTIMIZATION OF ANTI-ICING CHAMBER BASED ON POD AND KRIGING |
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ICAS2020_1149: B. Qiu, State Key Laboratory of Aerodynamics, China Aerodynamic Research, China; R. Li, Computational Aerodynamics Institute China Aerodynamic Research, China; X. Liu¹, J. Yao¹, B. Jiang¹, Y. Zhu, School of Chemical Engineering, China; ¹Computational Aerodynamics Institute, China Aerodynamic Research, China NUMERICAL INVESTIGATION OF THE EFFECT OF WALL TEMPERATURE ON THERMAL ENVIRONMENT OF TWO-DIMENSIONAL TRANSVERSE GAP |
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ICAS2020_1152: J.A. Cheng¹, H. Zhan¹, B.G. Mi¹; ¹School of Aeronautics,Northwestern Polytechnical University, China RESEARCH ON UNSTEADY AERODYNAMIC MODELS AT HIGH ANGLES OF ATTACK BASED ON NONLINEAR REGRESSION |
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ICAS2020_1183: J.X. Gao¹, W.Q. Yang¹, R. Zhang¹, Y.B. Li¹; ¹Northwestern Polytechnical University, China NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING LEADING EDGE COVERTS |
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ICAS2020_1190: R. Sorbilli Cardoso de Sousa¹, R.G. Annes da Silva¹; ¹Instituto Tecnologico de Aeronautica, Brazil NASA-CRM LATERAL-DIRECTIONAL STABILITY DERIVATIVES COMPARISON BETWEEN SEMI-EMPIRICAL, VORTEX LATTICE AND PANEL METHOD |
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ICAS2020_1240: R. Zhang¹, W.Q. Yang¹, Y.B. Li¹, J.X. Gao¹; ¹School of Aeronautics, Northwestern Polytechnical University, China NUMERICAL SIMULATION OF VARIABLE WINGSPAN EFFECTS ON A BIONIC FLAPPING WING |
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ICAS2020_1260: V. Soudakov, TsAGI, Russia; P. Schlösser¹, P. Weigel, Fraunhofer-Gesellschaft, Germany; T. ter Meer, NLR, Netherlands; A. Gebhardt, DLR, Germany; M. Meyer¹, M. Wahlich¹; ¹Airbus, Germany TOWARDS THE INDUSTRIAL APPLICATION OF ACTIVE FLOW CONTROL AT THE PYLON/WING JUNCTION OF CIVIL AIRCRAFT |
4.1 - Material Issues, Fatigue and Damage Tolerance |
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ICAS2020_0036: C. Li, China; C. Chen, China; L.M. Gao, China; J.F. Xu, China A TWO PHASES COUPLING FREE AND POROUS FLOW NUMERICAL SIMULATION METHOD OF LCM PROCESS |
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ICAS2020_0089: A. Bautin¹, Y. Svirsky¹, V. Basov¹, Y. Melnikov¹; ¹1Central Aerohydrodynamic Institute (TsAGI), Russia MODEL CURVES: A SIMPLE WAY TO ACCOUNT FOR COMPLEX EFFECTS |
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ICAS2020_0095: P. Hou¹, X.-J. Shang¹, Y. Dong¹; ¹Shenyang Aero Engine Research Institute, China THE NOISE REDUCTION STUDY OF COMPOSITE ACOUSTIC LINER ON HIGH BYPASS RATIO TURBOFAN AEROENGINE |
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ICAS2020_0106: S. Dubinskii¹, F. Sevastyanov¹, V. Kostenko¹, S. Denisov¹, I. Zharenov¹; ¹The Central Aerohydrodynamic Institute (TsAGI), Russia STUDY OF COMPOSITE SKIN-STRINGER FATIGUE BEHAVIOR UNDER BROADBAND RANDOM VIBRATION |
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ICAS2020_0118: S. Su¹, W. Zhang¹, L. Li¹; ¹Aircraft Strength Research Institute, China FRACTURE CRITERION ANALYSIS AND CRACK GROWTH PROPERTY OF MIXED-MODE CRACK EXPERIMENTS |
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ICAS2020_0188: J. Li¹, J. Guo¹, H. Huang, Hafei Aviation Industry CO.,Ltd., China; H.F. Peng¹; ¹China Helicopter Research and Development Institute, China STATISTICS AND ANALYSIS OF MANUFACTURING DEFECTS AND DAMAGE OF HELICOPTER COMPOSITE STRUCTURES |
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ICAS2020_0272: Y. Yang¹, B. Wang¹, S. Lv¹, Y. Zhou, Peking University, China; L. Wang¹, G. Liu¹; ¹Aircraft Strength Research Institute of ChinaAffiliation, China A DEEP-LEARNING-BASED METHOD FOR DAMAGE IDENTIFICATION OF COMPOSITE LAMINATES |
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ICAS2020_0295: J. Jokinen¹, M. Wallin, Patria Aviation, Finland; M. Kanerva¹; ¹Tampere University, Finland THE INFLUENCE OF THE NUMBER OF ADHESIVE PLIES (FM 300-2) ON FRACTURE PROPERTIES |
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ICAS2020_0297: J. Jokinen¹, M. Wallin, Patria Aviation, Finland; M. Kanerva¹; ¹Tampere University, Finland ADJUSTED SHAPES OF ADHESIVELY BONDED REPAIR PATCHES FOR THE EARLY INDICATION OF DEBOND IN FIGHTER AIRCRAFT STRUCTURES |
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ICAS2020_0364: Y.Z. Zhang¹, X.Y. Tong¹, L.J. Yao¹, A.T. Augousti, Kingston University London, United Kingdom; ¹Northwestern Polytechnical University, China FAILURE PROCESS IDENTIFICATION IN C/SIC SAMPLES WITH A RANGE OF TENSILE PERFORMANCE USING ACOUSTIC EMISSION |
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ICAS2020_0400: Y. Shi, China; X. Yang, China; D. Shi, China; D. Yang, China; G. Miao, China; S. Lv, China EXPERIMENTAL INVESTIGATION AND LIFE PREDICTION FOR DEFECT INDUCED CRACK OF A P/M NICKEL BASED SUPERALLOY |
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ICAS2020_0401: N. Hou, China; X.H. Meng, China; J. Liu, China; Y.L. Li, China DYNAMIC RESPONSE AND DAMAGE OF THE FAN BLADES DURING UAV INGESTION INTO AN AERO-ENGINE |
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ICAS2020_0557: T. Ikeda, Chubu University, Japan; T. Sakai, Tottori University, Japan; A. Yokosu¹, Y. Fujii¹, H. Takenami¹, M. Arai¹, T. Ishikawa¹; ¹Nagoya University, Japan IN-SITU LASER ASSISTED DIRECT IMPREGNATION, LAMINATION AND PLACEMENT OF CFRTP |
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ICAS2020_0562: L. Zaplana Manzano¹, J. Romero Arana¹, J. Gómez-Escalonilla Martín¹; ¹AIRBUS DS, Spain A DIGITAL EQUIVALENT DEVELOPMENT FOR FATIGUE AND DAMAGE TOLERANCE IN AIRCRAFT STRUCTURES |
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ICAS2020_0713: Y.L. Su¹, Z.L. Fan¹, W.H. Wu¹, S. Lu, Northwestern Polytechnical University, China; X.M. Chen, Aircraft Strength Research Institute of AVIC, China; ¹China Aerodynamics Research and Development Center, China DESIGN METHOD FOR THE FATIGUE-SIMULATING SPECIMEN OF TWIN-WEB TURBINE DISK |
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ICAS2020_0833: D. Wei¹, Y. Cui¹, Y.A. Shi¹, G.M. Xiao¹, Y.X. Du¹, Y.W. Gui¹; ¹China Aerodynamics Research and Development Center, China A NEW METHOD FOR ESTIMATING THE THERMOS-PHYSICAL PARAMETERS OF THERMAL PROTECTION MATERIALS BY ULTRASONIC MEASUREMENTS |
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ICAS2020_0904: Y.J. Wang¹, Y. Liao¹, H. Dui¹, J. Dong¹; ¹Chengdu Aircraft Design and Research Institute, China STUDY ON THE FATIGUE SCATTER FACTOR UNDER SEVERE LOAD SPECTRUM |
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ICAS2020_1032: S. Olsson, Quintus Technologies AB, Sweden; B. Carlsson¹, M. Bergkvist, Quintus Teachnologies AB, Sweden; R. He¹; ¹Quintus Technologies, China FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSURE |
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ICAS2020_1065: D. Jin¹, G.P. Qian¹, K. Feng¹; ¹Shanghai Aircraft Design and Research Institute, China STUDY ON THE METHOD OF DETERMINING SKIN WAVINESS REQUIREMENT OF CIVIL AIRCRAFT |
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ICAS2020_1203: L.F. Wang¹, L. Liu², C. Liu, Jiangsu Aero-XY Technology Co., Ltd, China; X.L. Pan¹, Z.H. Zhao², L.C. Zhou¹; ¹Air Force Engineering University, China; ²Nanjing University of Aeronautics and Astronautics, China RESEARCH ON FATIGUE STRENGTH PREDICTION MODEL OF AERO-ENGINE BLADES SUBJECTED TO FOREIGN OBJECT DAMAGE |
4.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity |
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ICAS2020_0017: V. Symonov¹, J. Juracka¹; ¹Brno University of Technology, Czech Republic BIRD STRIKE SIMULATIONS IN MSC.SOFTWARE: CORRELATION BETWEEN THE EXPERIMENTS AND SIMULATIONS |
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ICAS2020_0019: F. Franke¹, U. Burger¹, C. Hühne, DLR, Germany; ¹Technische Hochschule Ingolstadt, Germany MODELS AND METHODS FOR DRONE STRIKE LOAD PREDICTIONS |
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ICAS2020_0086: P. LI, Aircraft Strength Research Institute, China TRANSFER PATH ANALYSIS OF RANDOM VIBRATION LOADS |
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ICAS2020_0097: M. Kou, AECC CAE, China; J. Zhang¹, J. Lu¹, S. Tan¹; ¹AVIC The First Aircraft Institute, China A PERTURBATION ANALYSIS OF NONLINEARITY IN LANDING-GEAR SHIMMY OF A FLEET AIRCRAFT |
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ICAS2020_0109: Z.Y. Li¹, Y.Z. Han¹, X.H. Yao¹; ¹AVIC the First Aircraft Institute, China A STRUCTURE DESIGN OF CFRP REAR PRESSURE BULKHEAD WITHOUT STIFFENERS |
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ICAS2020_0157: H.-S. Park¹, D.-H. Hwang¹, J. Yang, University of Washington, United States; J.-H. Han¹; ¹KAIST, South Korea EXPERIMENTAL STUDY ON ATTENUATION PERFORMANCE OF SHOCK-ABSORBING INSERT |
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ICAS2020_0187: C. Chang¹, J. Li¹; ¹China helicopter research and development institute, China DESIGN AND VERIFICATION OF ENERGY-ABSORBING STRUCTURE OF CORRUGATED BEAM BASED ON SPECIFIC FAILURE MODE |
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ICAS2020_0206: M. Ritter¹, M.S. Roeser¹, S. Görtz¹; ¹German Aerospace Center (DLR), Germany MULTI-AXIS MANEUVER SIMULATION FOR SYSTEM IDENTIFICATION OF FLEXIBLE TRANSPORT AIRCRAFT BY HIGH-FIDELITY METHODS |
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ICAS2020_0208: X.Y. Pang, China; W.W. Men, China; J.F. Huang, China DESIGN AND PERFORMANCE RESEARCH OF ARTIFICIAL ELECTROMAGNETIC STRUCTURE WITH TRANSMISSION AND ABSORPTION CHARACTERISTICS |
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ICAS2020_0212: G.A. Amiryants¹, A.V. Chedrik¹, V.A. Malyutin¹, S.E. Paryshev¹, V.G. Soudakov¹; ¹Central Aerohydrodynamic Institute , Russia THEORETICAL AND EXPERIMENTAL INVESTIGATION OF THE AEROELASTIC CHARACTERISTICS OF THE AFLONEXT PROJECT BIG-SIZE DEMONSTRATOR |
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ICAS2020_0269: Y.J. Liu¹, S.Q. Liang¹, R.J. Sun¹, M.Q. Li, China; ¹AVIC THE FIRST AIRCRAFT INSTITUTE, China ITERATIVE GLOBAL/LOCAL NON-INTRUSIVE MODEL COUPLING METHOD FOR STRUCTURE FAILURE ANALYSIS |
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ICAS2020_0270: H. Abramovich, Technion, I.I.T.,, Israel THE VIBRATION CORRELATION TECHNIQUE – A RELIABLE NONDESTRUCTIVE TOOL TO PREDICT BUCKLING LOADS |
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ICAS2020_0271: K. Lei¹, B.-W. Wang¹, J.-T. Wu¹, W.-L. Deng¹; ¹Aircraft Strength Research Institute of China, China TEMPERATURE-INDUCED LOAD OF BOLTED HYBRID COMPOSITE/METAL JOINT |
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ICAS2020_0294: L.M. Gavva, Moscow Aviation Institute (NRU) , Russia KINEMATIC MODEL OF REFINED THEORY AND EXACT ANALYTICAL SOLUTIONS OF STATIC AND BUCKLING PROBLEMS OF STRUCTURALLY-ANISOTROPIC COMPOSITE PANELS OF AIRCRAFT |
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ICAS2020_0304: J.-J. Zheng¹, B.-W. Wang¹, L.-G. Zhu, Shanghai Aircraft Design and Research Institute, China; J.-Y. Tang¹; ¹Aircraft Strength Research Institute of China, China RESEARCH ON ATTITUDE CONTROL AND CONSTRAINT SYSTEM DESIGN OF FULL-SCALE AIRCRAFT STATIC TEST BASED ON BARYCENTER |
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ICAS2020_0308: Z. Jia, China; L. Xuan, China; T. Su., China; L. Chen, China BROADBAND MICROWAVE ABSORBING HONEYCOMB CORE MATERIAL WITH ACTIVE CARBON AS DELEGATES |
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ICAS2020_0337: R. Degenhardt¹, F. Franzoni¹, S.G.P. Castro, TU-Delft, Netherlands; ¹DLR, Germany ACHIEVEMENTS IN THE BUCKLING OF THIN-WALLED COMPOSITE LAUNCHER STRUCTURES |
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ICAS2020_0340: A. Shanygin, Russia DEVELOPMENT OF LIGHTWEIGHT HYBRID AIRFRAMES BASED ON UNIDIRECTIONAL COMPOSITE STRUCTURE CONCEPTS |
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ICAS2020_0360: D. Gueraiche¹, S. Popov¹, A. Guelailia, Space mechanical research development, Algeria; ¹Moscow Aviation Institute, Russia PASSIVE FLEXIBLE WINGTIP AREA FOR IMPROVING AIRLINERS CRUISE EFFICIENCY AND GUST ALLEVIATION |
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ICAS2020_0383: K. Li¹, C. Bai¹; ¹Aircraft strength research institute, China STRUCTURAL VIBRATION CONTROL BY USING THE ENERGY FROM DIFFERENT MODES |
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ICAS2020_0391: W.-J. Nie¹, W.-Q. Deng¹, Y.-N. Chen¹, L. Zou¹; ¹AECC Hunan Aviation Powerplant Research Institute , China TURBINE STRUCTURE ANALYSIS AND IMPROVEMENT OF A HIGH-SPEED ROTOR WITH MULTI-DISK AND MULTI-SUPPORT |
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ICAS2020_0392: Y. Liu¹, D. Zhou¹, S. Feng¹, C. Yang¹, H. Xie¹; ¹Chengdu Aircraft Industry (Group) Corporation Ltd., China PROCESS RESEARCH AND OPTIMINZATION OF PINHOLE HOLE AND NAIL HEAD DAMAGE ON COMPOSITE PARTS |
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ICAS2020_0393: K. Yuan¹, M. Cheng¹; ¹Beijing Electro-Mechanical Engineering Institute, China SUPERSONIC AEROELASTIC ANALYSIS OF AN ALL-MOVABLE WING WITH FREE PLAY |
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ICAS2020_0397: J. Bian¹, Y.-N. Chen¹, Q. Mei¹, Y.-L. Xu¹, Y.-H. Lu¹; ¹AECC Hunan Aviation Powerplant Research Institute, China MODAL DAMPING PARAMETER IDENTIFICATION METHOD BASED ON IMPROVED VMD AND ENVELOPE FITTING AND ITS APPLICATION |
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ICAS2020_0479: E. Zappino¹, E. Carrera¹; ¹Politecnico di Torino, Italy ACCURATE MODELS FOR THE PREDICTION OF FREE-EDGE STRESSES OF COMPOSITE STRUCTURES UNDER THERMAL LOADS |
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ICAS2020_0518: T. Huang, Nanjing University of Aeronautics and Astronautics, China; M. Nuño ¹, K.-U. Schröder¹; ¹RWTH Aachen University, Germany STRUCTURAL HEALTH MONITORING OF SANDWICH STRUCTURES WITH LATTICE CORES IN AIRCRAFT DESIGN: CHALLENGES AND POTENTIAL |
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ICAS2020_0540: R. Tsukamoto¹, A. Senba¹, T. Ikeda, Chubu University, Japan; M. Tamayama², H. Arizono²; ¹Meijo University, Japan; ²JAXA, Japan ACTUATION MECHANISM USING SHAPE MEMORY ALLOY WIRES IN SPIRAL ARRANGEMENT FOR MORPHING WINGS |
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ICAS2020_0575: F. Sturm¹, G. Illenberger¹, D. Techmer¹, M. Hornung¹; ¹Technical University of Munich, Germany STATIC AEROELASTIC TAILORING OF A HIGH-ASPECT-RATIO-WING FOR A SAILPLANE WITH A FORWARD MORPHING WING SECTION |
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ICAS2020_0576: P. Bessonov¹, Y. Svirsky¹, I. Sidorov¹, S. Dubinskii¹; ¹TsAGI, Russia METHODS FOR CALCULATING THE FATIGUE DAMAGE OF A STRUCTURE FOR VARIOUS SPECTRA OF VIBRO-ACOUSTIC LOADS |
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ICAS2020_0593: V. Chedrik¹, S. Tuktarov¹, K. Balunov¹, N. Nguyen, Moscow Institute of Physics and Technology, Russia; ¹Central Aerohydrodynamic Institute, Russia MATHEMATICAL MODELS FOR ANALYSIS AND OPTIMIZATION OF AIRCRAFT STRUCTURAL COMPONENTS TAKING INTO CONSIDERATION OF LOCAL STRESS DISTRIBUTION |
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ICAS2020_0599: F. Chen¹, P. Chen¹, Y.Q. Zhao¹; ¹Shanghai Aircraft Manufacturing Corporation Ltd, China DEFORMATION ANALYSIS OF C-SPAR COMPOSITE STRUCTURE DURING THE PREFORMING PROCESSING |
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ICAS2020_0631: Z.-K. Zhang¹, Y.-J. Yang¹, S. Ricci², A. De Gaspari², C. Song¹, C. Yang¹; ¹Beihang University, China; ²Politecnico di Milano, Italy AEROSERVOELASTIC OPTIMIZATION OF A HIGH ASPECT TRANSPORT WING WITH MORPHING TRAILING EDGE |
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ICAS2020_0650: C. Zhang¹, X.F. Li¹, J.W. Chen¹, Z. Zhou², L. Qiao²; ¹Xi'an Modern Control Technology Research Institute, China; ²Northwestern Polytechnical University, China A COMPREHENSIVE FRAMEWORK FOR THE COUPLED NONLINEAR AEROELASTIC AND FLIGHT DYNAMIC ANALYSES OF HIGHLY FLEXIBLE AIRCRAFT |
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ICAS2020_0684: H. Wang, COMAC Flight test Center, China A SUBJECTIVE EVALUATION METHOD OF AIRCRAFT VIBRATION IN FLIGHT TEST |
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ICAS2020_0712: Y.C. Deng, SADRI, China; Y. Yang, ASRI, China; Y.Q. He, SIA, China; C. Sun, CAE, China; F. Qui, SAU, China A METHOD FOR CALCULATING TORSION ANGLE OF FLEXIBLE RETICULAR TUBE AT DIFFERENT POSITIONS |
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ICAS2020_0731: Y. Ding, China; Z. Zhou, China; H.J. Liu, China BIONIC LIGHT-WEIGHT GRID SURFACE WING STRUCTURE DESIGN FOR A SOLAR-POWERED UAV |
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ICAS2020_0763: G. Nicolosi¹, F. Valpiani¹, G. Grilli¹, A. Saponaro Piacente¹, L. Di Ianni¹, E. Cestino¹, V. Sapienza¹, A. Polla, Aeronautical Consultant, Italy; P. Piana, TescoGo, Italy; ¹Politecnico di Torino, Italy DESIGN OF A VERTICAL DITCHING TEST |
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ICAS2020_0780: H.-C. Qiu¹, W.-C. Fan¹, Y.-N. Fang¹; ¹COMAC Shanghai Aircraft Manufacturing Co., Ltd., China IMPROVED STOCHASTIC PERTURBATION ALGORITHM FOR GENERALIZED REPEATED EIGENVALUES PROBLEM BASED ON SURROGATE MODEL |
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ICAS2020_0836: Y. Guo¹, W. Yang¹, Y. Dong¹, X. Lang¹; ¹Northwestern Polytechnical University, China COMPUTATIONAL FLUID-STRUCTURE INTERACTIONS OF A 3D FLEXIBLE FLAPPING WING |
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ICAS2020_0880: S.Q. Bi¹, H. Cui¹, L.Y. Liu¹; ¹Shenyang Aircraft Design and Research Institute of AVIC, China THE FINITE ELEMENT MODELLING OF BOLTED STRUCTURE BETWEEN SELECTIVE LASER MELTING ALUMINIUM AND COMPOSITE PLATES |
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ICAS2020_0916: I. Isnardi¹, E. Menga, Airbus Operations S.L, Spain; J.E. Mottershead¹, S. Fichera¹; ¹University of Liverpool, United Kingdom MODEL REDUCTION AND STOCHASTIC UPDATING OF A VIBRATING SYSTEM |
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ICAS2020_0924: L. Magerramova, Central Institute of Aviation Motors, Russia; E. Kratt, Laboratory of New Technology, Russia DEVELOPMENT OF ADVANCED DESIGNS OF GAS TURBINE ENGINES FROM POWDER COMPOSITIONS |
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ICAS2020_0939: H.N. Dui, China; D.L. Liu, China; Z.X. Zhang, China; S.Z. Pan, China; L.X. Zhang, China AN INVERSE APPROACH BASED ON EUCLIDEAN SPACE FOR DETERMINING STRUCTURAL LOAD DISTRIBUTION FROM STRAIN MEASUREMENTS |
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ICAS2020_0961: S. Kuzmina¹, F. Ishmuratov¹, O. Karas¹; ¹TsAGI, Russia EFFECTS OF ELASTICITY, VISCOSITY AND BOUNDARY LAYER TRANSITION ON AEROELASTICITY CHARACTERISTICS OF LAMINAR WINGS |
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ICAS2020_0963: A.V. Bezuevsky¹, A.V. Grigorev¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia RATIONAL DETERMINATION OF WING JIG SHAPE OF A LONG-RANGE AIRCRAFT WITH TRANSONIC CRUISE REGIME |
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ICAS2020_0999: W.M. Alves, Embraer, Brazil; B.S. Mattos¹, J.A. Hernandes¹; ¹ITA, Brazil FLUID-STRUCTURE INTERACTION ANALYSIS OF ELASTIC EFFECTS OF A TRANSPORT AIRCRAFT FITTED WITH WINGLETS |
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ICAS2020_1014: H. Raza¹, O. Rodera Garcia², K. Carpenter¹, T. Pärnänen², J. Jokinen², M. Kanerva², J. Bayandor¹; ¹CRASH Lab, University at Buffalo, United States; ²Tampere University , Finland REVIEW OF PREDICTIVE METHODS FOR CAPTURING ONSET OF DAMAGE AND INITIAL DELAMINATION IN CARBON FIBRE REINFORCED POLYMER LAMINATES SUBJECT TO IMPACT |
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ICAS2020_1062: C.-G. Yang¹, Z.-Q. Tian¹; ¹China Helicopter Design and Research Institute, China RESEARCH ON STRUCTURAL DESIGN OF TAIL BOOM FOR AN UNMANNED HELICOPTER |
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ICAS2020_1068: H. Wang¹, H. Wang¹; ¹Shanghai Aircraft Design and Research Institute, China ON THE DEVELOPMENT OF FUSELAGE WEIGHT ESTIMATION TOOL INTO AIRCRAFT MULTIDISCIPLINARY DESIGN ENVIRONMENT |
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ICAS2020_1072: H.Y. Huang¹, D. Wang¹, X.F. Du¹, Y.X. Xu¹; ¹School of Aeronautics, Northwestern Polytechnical University, China STUDY ON THE OUT-OF-PLANE COMPRESSION PROPERTIES OF MULTISTAGE TITANIUM ALLOY LATTICE METAMATERIALS AT 350°C |
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ICAS2020_1109: C. Li¹, Z.Q. Wan¹, X. Wang¹; ¹Beihang University, China AN INTEGRATED AERODYNAMIC/THERMAL/STRUCTURAL DESIGN FRAMEWORK FOR HYPERSONIC VEHICLES |
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ICAS2020_1117: E.M. Kolman¹, D.V. Kurulyuk¹, E.A. Levchenko¹, M.V. Limonin¹; ¹Central Aerohydrodynamic Institute named after N.E. Zhukovsky, Russia SPECIALIZED SOFTWARE DEVELOPMENT FOR BUILDING BLOCK APPROACH INTEGRATION IN FULL-SCALE STATIC TESTS |
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ICAS2020_1124: E. Carrera¹, A. Pagani¹, R. Augello¹, D. Scano¹; ¹Politecnico di Torino, Italy ACCURATE BUCKLING AND POST-BUCKLING ANALYSIS OF COMPOSITE STIFFENED PANELS |
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ICAS2020_1126: L. Bortolotto¹, R.G.A. Silva¹, M.H.J. Pedras, Embraer, Brazil; ¹Instituto Tecnológico de Aeronáutica, Brazil AEROELASTIC RESPONSE CALCULATION USING DUHAMEL INTEGRAL AND ITS APPLICATIONS |
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ICAS2020_1153: H. Zhang¹, Q. Zhang¹; ¹Sun Yat-sen University, China A DYNAMIC SELF-CONTROL ERR STRATEGY FOR BI-DIRECTIONAL EVOLUTIONARY STRUCTURAL OPTIMIZATION |
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ICAS2020_1222: C. Surace¹, R. Roy¹, M. Civera¹, D. Allaio¹, R. Barbieri¹, A. Grava¹, R. Tufilli¹, P. Gili¹; ¹Politecnico di Torino, Italy DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: STRUCTURAL DESIGN AND OPTIMIZATION |
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ICAS2020_1235: M. Herman¹, E. Dupuy¹, C. Paris¹, E. Petiot¹, J.-P. Cabanac¹, C. Fualdes¹, G. Masse², M.-A. Celli²; ¹Airbus Operations, France; ²Airbus Helicopters, France THERMOPLASTIC APPLICATIONS FOR AEROSTRUCTURES: TOWARDS SUSTAINABLE AND WEIGHT EFFICIENT APPLICATIONS |
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ICAS2020_1242: V.Y. Myasnikov¹, I.I. Ivanov¹, B.S. Blinnik¹; ¹CIAM, Russia AIRCRAFT ENGINE ROTOR DYNAMICS ANALYSIS AFTER FAN BLADE-OUT WITH ACCOUNT OF ROTOR-CASING CONTACT INTERACTIONS |
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ICAS2020_1250: Y.X. Liu¹, D. Mo¹, Q. Du¹, Y.Z. Chen¹, M. Wang¹; ¹AECC Shenyang Engine Research Institute, China NUMERICAL SIMULATION AND EXPERIMENTAL INVESTIGATION ON FLUTTER AND NON-SYNCHRONOUS VIBRATION |
5 - Propulsion |
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ICAS2020_0027: N. Liu, Shanghai Aircraft Design & Research Institute, Commercial Aircra, China AN IMPROVED IDENTIFICATION METHOD FOR ACTUATOR LOOP OF AIRCRAFT ENGINE CONTROL SYSTEM |
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ICAS2020_0055: Y. Shang, Shanghai Aircraft Design and Research Institute, China RESEARCH ON CIVIL AIRCRAFT POWERPLANT SYSTEM EICAS MESSAGES DESIGN APPROACH |
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ICAS2020_0160: X. Yang¹, Q. Yang¹, W. Dong¹; ¹Shanghai Jiao Tong University, China A SIMPLIFIED MODEL FOR THE SIMULATION OF SYNERGISTIC AIR-BREATHING ROCKET ENGINE |
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ICAS2020_0162: D.-C. Wang¹, B.-F. Song¹, H.-F. Wang¹, J. Jiao, Chinese Academy of Sciences, China; ¹Northwestern Polytehnical University, China RESEARCH OF PROPULSION-SYSTEM-SURROGATE-MODELING METHOD USING INFILL CRITERION SAMPLES |
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ICAS2020_0257: Y.F. Li¹, Z.Z. Na¹, Y. Chen¹, Y.B. Wang¹; ¹AECC, China EFFECT OF COMPLEX FLOW PROFILES AT COMBUSTOR EXIT ON TURBINE CHARACTERISTICS |
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ICAS2020_0259: W. Xiao, AECC Hunan Aviation Powerplant Research Institute, China; Y. Cheng, HUNAN MECHANICAL & ELECTRICAL POLYTECHNIC, China; K. Wang, Aero Engine Academy of China (AECC), China; Z. Ren, Tsinghua University, China HYBRID IGNITION PROBABILITY METHOD TO PREDICT THE IGNITION PERFORMANCE OF A GAS TURBINE COMBUSTOR |
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ICAS2020_0290: H. Li, Aero Engine Corporation of China, China; C. Liang¹, X. Li¹; ¹AECC Shenyang Engine Research Institute, China MODELING AND SIMULATION APPLICATION THROUGHOUT THE AERO-ENGINE LIFE CYCLE |
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ICAS2020_0470: Y. Itoh¹, A. Satoh¹; ¹Iwate university, Japan ANALYSIS OF AERODYNAMIC CHARACTERISTICS OF PROPELLER AT LOW ADVANCE RATIO USING A WHIRING ARM |
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ICAS2020_0504: M. Zhang, AECC Commercial Aircraft Engine, China NUMERICAL INVESTIGATION OF NACELLE INTAKE FLOW DISTORTION AT CROSSWIND CONDITIONS |
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ICAS2020_0531: C.-X. Song¹, M.-C. Deng¹, Y. Fan¹, Y.-Q. Liang¹, Y. Shen¹; ¹AECC Shenyang Engine Research Institute, China RESEARCH OF LABYRINTH SEALS MEASUREMENT-BASED PROBABILITISTIC ANALYSIS METHOD FOR TURBOFAN INTERNAL AIR SYSTEM |
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ICAS2020_0538: W. Zhang¹, K. Luo¹, Q. Wen², F.-M. Tang²; ¹AECC HAPRI, China; ²AECC AEAC, China AXIAL ASSEMBLAGE DEVIATION ON PERFORMANCE OF ONE TRANSONIC CENTRIFUGAL COMPRESSOR |
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ICAS2020_0541: T. Wu¹, Z. Li¹, W. Dong¹; ¹Shanghai Jiao Tong University, China AERODYNAMICS DESIGN, OPTIMIZATION AND FLOW FIELD INVESTIGATION OF A CONTRA-ROTATING PROPFAN AT HIGH FLIGHT MACH NUMBERS |
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ICAS2020_0544: C. Hu¹, J. Gu¹, F. Gao¹; ¹AVIC The First Aircraft Institute, China THE RESEARCH ON PROPELLER NOISE PREDICTION METHOD FOR TURBOPROP AIRCRAFT |
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ICAS2020_0598: J.Y. Ying¹, X.B. Wang¹, J. Kang¹, M.H. Lu¹; ¹AECC commercial Aircraft Engine Co.,Ltd., China STUDY OF NON-ROTATING MICROPHONE ARRAY FOR SPINNING DUCT MODE DETECTION |
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ICAS2020_0678: Y. Liu¹, X. Hang¹, C. Jiang¹; ¹Beihang University, China APPLICATION OF REINFORCEMENT LEARNING IN 1-D AERODYNAMIC DESIGN OF AXIAL COMPRESSOR |
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ICAS2020_0722: J. Jiao¹, X.-P. Ma¹, B.-F. Song, Northwestern Polytechnical University, China; J.-B. Yang, China Electronics Technology Group Corporation 38th Research Ins, China; ¹Chinese Academy of Sciences, China AERODYNAMIC AND STRUCTURAL DESIGN OF THE COMPOSITE PROPELLER FOR NEAR SPACE VEHICLES |
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ICAS2020_0750: V. Mileshin¹, S. Markov¹, V. Korzhnev¹, I. Pochkin¹; ¹CIAM, Russia EXPERIMENTAL STUDIES OF SLOT-TYPE CASING TREATMENTS FOR MODEL FANS WITH THE AIM OF AERODYNAMIC AND ACOUSTIC IMPROVEMENTS |
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ICAS2020_0751: X. Geng¹, T. Hu¹, P. Liu¹, T. Sinnige², G. Eitelberg²; ¹Beihang University, China; ²Delft University of Technology, Netherlands ANALYSIS OF THRUST-SCALED ACOUSTIC EMISSIONS OF AIRCRAFT PROPELLERS AND THEIR DEPENDENCE ON PROPULSIVE EFFICIENCY |
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ICAS2020_0881: F.D. Golberg¹, M.P. Sokolov¹, V.E. Volkov¹, A.A. Petukhov¹; ¹Central Institute of Aviation Motors, Russia THE USE OF SOFTWARE “VIRTUAL ENGINE” FOR TIMELY GAS-TURBINE ENGINE FAULT LOCALIZATIONS |
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ICAS2020_0965: H.-L. Jin, China; X. Chen, China; D.-B. Qiu, China; Y.-Q. Yin, China MODELING OF COUNTER-ROTATING LIFT FAN/MAIN ENGINE COMBINED PROPULSION SYSTEM AND LIFT FAN AERODYNAMIC DESIGN |
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ICAS2020_0974: V.S. Zakharchenko¹, A.N. Varyukhin¹, D.Y. Rakhmankulov¹, P.S. Suntsov¹, M.A. Ovdienko¹, M.V. Gordin¹; ¹Central Institute of Aviation Motors (CIAM), Russia CONCEPTUAL STUDIES OF DIFFERENT TYPE OF HYBRID ELECTRIC PROPULSION SYSTEMS FOR COMMUTER AIRLINERS |
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ICAS2020_1017: A. Mirzoyan¹, I. Khaletskii¹; ¹CIAM, Russia METHODS OF PROGRAMMED THRUST MANAGEMENT FOR NOISE REDUCTION OF SUPERSONIC CIVIL AIRCRAFT |
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ICAS2020_1022: L. Mirzoyan¹, A. Mirzoyan¹, A. Isyanov¹; ¹CIAM, Russia THE CAPABILITIES OF AUTOMATION OF MDAO PROBLEM STATEMENT AT COLLABORATIVE CONCEPTUAL DESIGN OF THE PROPULSION SYSTEM USING OPEN SOURCE SOFTWARE TOOLS |
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ICAS2020_1025: M.A. Gallani¹, L.C.S. Góes¹, L.A.R. Nerosky, Embraer, Brazil; ¹Instituto Tecnológico de Aeronáutica, Brazil IMPLEMENTATION OF DISTRIBUTED ELECTRIC PROPULSION ON A GENERAL AVIATION AIRCRAFT |
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ICAS2020_1099: S.C. Xu¹, Y. Wang¹, Z.G. Wang¹, X.Q. Fan¹, B. Xiong¹; ¹National University of Defense Technology, China A DESIGN METHOD OF AN AXISYMMETRIC HYPERSONIC INLET INTERGRATED WITH A LONG FOREBODY |
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ICAS2020_1100: Y.-H. Wang¹, G.-P. Qian¹; ¹Shanghai Aircraft Design and Research Institute, China NUMERICAL STUDY OF HIGH TEMPERATURE TRANSVERSE PULSE JET IN THE SUPERSONIC COMBUSTION CHAMBER |
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ICAS2020_1122: C.-H. Liang¹, M.-B. Sun¹, Y.-X. Yang¹, Y. Liu, China Aerodynamics Research and Development Center, China; T.-Y. Wang¹, G.-W. Ma¹, F. Li¹, C. Wang¹; ¹National University of Defense Technology, China EXPERIMENTAL STUDY ON THE CHARACTERISTICS OF SONIC GAS INJECTION INTO SUPERSONIC CROSSFLOW WITH MA2.0 AND MA3.0 |
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ICAS2020_1146: X. Yang¹, Z.-W. Wang¹, Y.-B. Niu¹, H.-Y. Miao¹; ¹college of aerospace science and engineering,national university, China INFLUENCE OF SHOCK TRAIN ON HEAT FLUX DISTRIBUTION OF A CIRCULAR CONSTANT-AREA ISOLATOR |
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ICAS2020_1249: D. Mo¹, Y.X. Liu¹, I. Roumeliotis², D. Nalianda²; ¹AECC Shenyang Engine Research Institute, China; ²Cranfield University, United Kingdom INVESTIGATION OF VARIABLE GEOMETRIES ON THE OPERABILITY AND AIRCRAFT LEVEL PERFORMANCE OF A THREE-SHAFT TURBOFAN ENGINE FOR ENTRY INTO SERVICE 2050 |
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ICAS2020_1264: K.D. Wan¹, Y.Z. Huang¹, Z.X. Gao¹, Y. He, Zhejiang University, China; C.W. Jiang¹; ¹Ningbo Institute of Technology, Beihang University, China LARGE-EDDY SIMULATION OF A SWIRLING AVIATION KEROSENE SPRAY FLAME USING 3-COMPONENT SURROGATE FUELS |
6.1 - Flight Dynamics and Control (Control & Modelling) |
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ICAS2020_0073: T. Rogalski¹, P. Rzucidlo¹, J. Prusik, Doctoral School of Engineering and Technical Sciences at Rzeszo, Poland; ¹Rzeszow University of Technology, , Poland AIRCRAFT FLIGHT CONTROL SYSTEM FOR AEROBATIC FLIGHT |
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ICAS2020_0176: A.V. Efremov¹, M.S. Tiaglik¹, I.K. Irgaleev¹; ¹Moscow Aviation Institute, Russia THE APPLICATION OF THE PILOT-AIRCRAFT SYSTEM APPROACH FOR OPTIMIZING 3D DISPLAY PARAMETERS |
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ICAS2020_0181: K. Ma¹, L.-B. Wang¹, H. Du¹, W. Wang¹, W.-T. Gu¹; ¹AVIC THE FIRST AIRCRAFT INSTITUTE, China THE ANALYSIS OF TAKEOFF ROTATION OF SUBSCALE FREE-FLIGHT |
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ICAS2020_0197: C. Qi, China Aeronautical Radio Electronics Research Institute, China L1 ADAPTIVE CONTROL AUGMENTATION FOR A FLEXIBLE AIR-BREATHING HYPERSONIC VEHICLE MODEL |
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ICAS2020_0313: B. Nie¹, F. Cen¹, Z. Liu¹, T. Guo¹, H. Sun¹; ¹China Aerodynamics Research and Development Center, China VIRTUAL FLIGHT TEST OF A BWB AIRCRAFT IN LOW SPEED WIND TUNNEL |
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ICAS2020_0348: S. Zhang, China; X. Du, China; F. Liao, China; J.-T. Huang, China AN ALTERNATIVE BUT EQUIVALENT REALIZATION OF FINITE-HORIZON SUBOPTIMAL CONTROL FOR VEHICLE LANDING |
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ICAS2020_0384: L. Qiu, Chinese Flight Test Establishment, China; Z.H. Gao¹, Y. Liu¹; ¹Northwestern Polytechnical University, China DECOUPLING CONTROL LAW DESIGN FOR OBLIQUE-WING AIRCRAFT BASED ON EIGENSTRUCTURE ASSIGNMENT AND MODEL FOLLOWING |
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ICAS2020_0418: D.-N. Liu¹, W.-K. Wang¹, B.-D. Zhao¹, X.-Z. Hu¹, B.-W. Nie¹; ¹China Aerodynamics Research and Development Center, China PRELIMINARY VIRTUAL FLIGHT VALIDATION OF A QUAD TILT ROTOR UAV IN WIND TUNNEL |
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ICAS2020_0448: S.V. Serokhvostov, MIPT, Russia; T.E. Churkina, MAI, Russia OPTIMAL TRAJECTORY DEPENDENCE ON THE ATMOSPHERE MODEL FOR THE SUN-POWERED AIRPLANE |
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ICAS2020_0525: Y. Liu¹, B.-G. Mi, Shanghai Aircraft Airworthiness Certification Center, China; X. Liu¹, H. Zhan¹; ¹Northwestern Polytechnical University, China MODELING AND DYNAMICS STABILITY ANALYSIS FOR A BLENDED-WING-BODY AIRCRAFT |
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ICAS2020_0532: A.N. Khrabrov¹, M.E. Sidoryuk¹; ¹TsAGI, Russia INFLUENCE OF AERODYNAMIC ASYMMETRY ON SPIN PARAMETERS OF THE COMMON RESEARCH MODEL |
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ICAS2020_0534: V.M. Kuvshinov¹, A.Y. Voronin¹; ¹TsAGI, Russia DESIGN TECHNIQUE OF INTEGRAL ALGORITHMS OF HELICOPTER FBW CONTROL SYSTEM |
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ICAS2020_0591: P.C. Wen, China; C.H. Zou, China; Z. Gao, China; J.G. Sun, China AUTONOMOUS FLIGHT CONTROL BASED ON NEURAL NETWORKS AND FUZZY DECISION |
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ICAS2020_0613: N. Yoshikawa, Mitsubishi Electric, Japan; S. Suzuki, The university of Tokyo, Germany FEEDBACK ERROR LEARNING WITH ENHANCED SAMPLING: NEURAL FAULT TOLERANT CONTROLLER OF AIRCRAFT |
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ICAS2020_0752: L.H. Son¹, Y. Ochi¹; ¹National Defense Academy, Japan ESTIMATION OF WIND BY ESTIMATING DERIVATIVES OF A LATERAL-DIRECTIONAL MOTION MODEL |
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ICAS2020_0814: M. Naruoka, JAXA, Japan BAYESIAN APPROACH TO SIMULTANEOUS STATIC AND DYNAMIC FLIGHT CHARACTERISTICS MODELING |
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ICAS2020_0865: H.Y. Shi¹, H. Xie², X. Hu¹, Y.M. Liu¹, Z.Y. Cai², H.J. Zhao², Y.M. Zhou¹; ¹Beihang University, China; ²AVIC General Huanan Aircraft Industry Co., Ltd., China RESEARCH AND DESIGN OF AMPHIBIOUS AIRCRAFT FIRE-EXTINGUISHING SIMULATION MANAGEMENT SYSTEM BASED ON DIS |
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ICAS2020_0885: N. Yokoyama, National Defense Academy of Japan, Japan DECENTRALIZED CONFLICT DETECTION AND RESOLUTION METHOD ACCOUNTING FOR UNCERTAINTIES OF TRAJECTORIES |
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ICAS2020_0948: L.-F. Chang¹, G.-L. Xue¹, Z.-W. Liu¹; ¹China Aeronautical Radio Electronics Research Institute, China A METHOD OF MANEUVER IDENTIFICATION AND TRAJECTORY PREDICTION FOR AGILE TARGET |
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ICAS2020_0959: J. Lee¹, S. Kim¹, S. Jung¹, H. Lee¹, Y. Kim¹; ¹Seoul National University, South Korea AIRCRAFT AUTOPILOT DESIGN USING ASYMMETRIC VARIABLE-SPAN WING MORPHING |
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ICAS2020_0978: L. Zheng¹, Z. Bai¹, Z. Zhou¹, R. Wang¹; ¹Northwastern Polytechnical University, China APPLICATION OF VECTOR JET CONTROL TECHNOLOGY ON AIRCRAFT LONGITUDINAL CONTROL |
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ICAS2020_0989: L.M.B.C. Campos, IDMEC/CCTAE/IST, Portugal; J.M.G. Marques, Escola de Ciências e Tecnologias, Universidade de Évora, Portugal ON THE MAXIMIZATION OF CONTROL POWER IN LOW-SPEED FLIGHT FOR A BWB CONFIGURATION |
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ICAS2020_1001: O. Kreerenko, Moscow Aviation Institute, Beriev Aircraft Company, Russia SYNERGETIC CONTROLS OF THE SYSTEM “CARRIER AIRCRAFT - UPPER-STAGE ROCKET“ |
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ICAS2020_1074: L.F. Zhao, Beihang University, Research Institute for Frontier Science, China; W.S. Wang, Beihang University, School of Automation Science and Electrical , China; Y.X. Chen, Beihang University, School of Aeronautic Science and Engineering, China; Z.X. Jiao, Beihang University, Ningbo Institute of Technology, China ANALYTICAL MODELLING OF A HOVERABLE X-SHAPE FLAPPING WING AIRCRAFT CONSIDERING WING-TAIL INTERACTION |
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ICAS2020_1078: L. Wang¹, L.F. Zhao¹, W.Y. Jiang¹, Z.X. Jiao¹; ¹Beihang University, China MODELING AND CONTROL OF A HOVERABLE FLAPPING WING AIRCRAFT CONSIDERING FLAPPING WING INDUCED FLOW |
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ICAS2020_1080: R. Takase, The University of Tokyo, Japan LEARNING FLIGHT CONTROL SKILLS BY IMITATING EXPERT DEMONSTRATIONS |
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ICAS2020_1089: B. Zhang¹, F. Li, China Academy of Launch Vehicle Technology, China; J. Bai¹; ¹Northwestern Polytechnical University, China TWISTOR BASED 6-DOF DISTRIBUTED ADAPTIVE LEADER-FOLLOWING CONTROL FOR MULTIPLE RIGID SPACECRAFT FORMATION |
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ICAS2020_1104: Y. Kong¹, K. He¹, M.H. Lowenberg², S.A. Neild², F. Cen¹; ¹China Aerodynamics Research and Development Center, China; ²University of Bristol, United Kingdom NONLINEAR UNSTEADY AERODYNAMIC MODELING AND LONGITUDINAL STABILITY ANALYSIS FOR AN AIRCRAFT MODEL |
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ICAS2020_1134: B.-G. Mi¹, H. Zhan¹, X. Bai¹, J.-Y. Yu¹; ¹Northwestern Polytechnical University, China SIMULATION ON THE EFFECT OF AIRCRAFT LOCAL STRUCTURE DAMAGES ON THE DYNAMIC DERIVATIVE COUPLING CHARACTERISTICS |
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ICAS2020_1135: T. Xue¹, J.Y. Ma¹, J.R. Wen¹, X.H. Yang, Science and Technology on Avionics Integration Laboratory, China; Y.Q. Dong¹, J.L. Ai¹; ¹Fudan University, China DEVELOPMENT OF A HUMAN PILOTED AIR COMBAT ENGAGEMENT DATABASE |
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ICAS2020_1145: T. Jin¹, H. Li¹, S. He¹, Y. Li¹; ¹Beijing Institute of Technology, China LEARNING-BASED MIDCOURSE GUIDANCE FOR VELOCITY MAXIMIZATION WITH ANGULAR CONSTRAINT |
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ICAS2020_1180: T.-Y. Nie¹, R. Wang¹, J.-Y. Liu¹, Z. Xiong¹; ¹Nanjing University of Aeronautics and Astronautics, China A REDUNDANT ADAPTIVE NAVIGATION METHOD BASED ON DYNAMIC PERFORMANCE EVALUATION FOR AEROSPACE VEHICLE |
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ICAS2020_1247: Y. Sun¹, M. Chang¹, J.Q. Bai¹; ¹NWPU, China TRAJECTORY GENERATION AND CONTROL FOR PERCHING MANEUVERING WITH QUADROTOR |
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ICAS2020_1266: Z.-Y. Wang¹, P. Chen¹, Y.-L. Wang¹, W.-D. Huang¹; ¹Aerospace Engineering University, China ASCENT TRAJECTORY OPTIMIZATION OF HYPERSONIC VEHICLE USING SWARM INTELLIGENT METHOD |
6.2 - Flight Dynamics and Control (UAV related) |
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ICAS2020_0150: S. Ishioka¹, K. Uchiyama¹, K. Masuda¹; ¹Nihon University, Japan LANDING SYSTEM USING EXTENDED DYNAMIC WINDOW APPROACH FOR FIXED-WING UAV |
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ICAS2020_0282: G.F. Yu, School of Software, Northwestern Polytechnical University, China; L. Zhang¹, C.H. Zou¹, Y.C. Liu, Beijing Aerospace Automatic Control Institute, China; Y. Cheng¹; ¹AVIC Xi’an Aeronautics Computing Technique Research Institute, China A ROBUST AND REAL-TIME VISUAL-INERTIAL POSE ESTIMATION FOR FIX-WING AIRCRAFT LANDING |
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ICAS2020_0357: Y. Sun, Northwestern Polytechnical University, China; M. Chang¹, J. Bai¹; ¹NWPU, China TRAJECTORY GENERATION AND CONTROL FOR PERCHING MANEUVERING WITH QUADROTOR |
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ICAS2020_0498: M. El-Salamony, Peking University, China; S. Serokhvostov, Moscow Institute of Physics and Technology, Russia STUDY OF SMALL UAVS DISTURBED MOTION NATURAL FREQUENCIES USING EXTENDED EXPERIMENTAL DATASETS |
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ICAS2020_0552: S.J. Koeberle¹, M. Hornung¹; ¹Institute of Aircraft Design, TUM, Germany DEVELOPMENTS TOWARDS A TOOLCHAIN FOR UAV FLIGHT DYNAMIC MODELS IN EARLY DESIGN |
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ICAS2020_0619: R. Wang¹, J.-N. Du¹, Z. Xiong¹, J.-Y. Liu¹, Y. Rui¹, T.-Y. Nie¹; ¹Nanjing University of Aeronautics and Astronautics, China EXPERIMENTAL RESEARCH OF COOPERATIVE NAVIGATION METHOD FOR CLUSTER AIRCRAFTS BASED ON MUTUAL DISTANCE DIFFERENCE MODEL |
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ICAS2020_0651: M.H. Sadraey, Southern New Hampshire University, United States ROCKETS HYBRID LAUNCH SYSTEM USING LINEAR SYNCHRONOUS ELECTRIC MOTORS |
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ICAS2020_0707: J. Bartasevicius¹, S.J. Koeberle¹, D. Teubl¹, C. Roessler¹, M. Hornung¹; ¹ Institute of Aircraft Design, Technical University of Munich, Germany FLIGHT TESTING OF 65KG T-FLEX SUBSCALE DEMONSTRATOR |
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ICAS2020_0710: S.-J. Qi¹, F. Wang¹, L. Jing¹; ¹Chinese Flight Test Establishment, China THE STUDY OF UNMANNED AERIAL VEHICLE FLYING QUALITIES FLIGHT TEST METHOD BASED ON TIME-DELAY EVALUATION |
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ICAS2020_0735: S.S. Rawikara¹, R.A. Sasongko¹, S.A. Munthahar¹; ¹Institut Teknologi Bandung, Indonesia AUTONOMOUS CONFLICT RESOLUTION ALGORITHM BASED ON ELLIPTIC GEOMETRY |
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ICAS2020_0769: A. Satoh, Iwate University, Japan; M. Watanabe, O.T.Techno Research Co., Ltd., Japan; K. Hozumi¹, A. Watanabe¹; ¹Japan Aerospace Technology Foundation (JAST), Japan ENDURANCE ANALYSIS OF BATTERY-POWERED MULTICOPTERS: DERIVATION OF PROPER CUT-OFF VOLTAGE USING DC MOTOR MODEL |
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ICAS2020_0945: Y. Matsumura¹, M. Bando¹, S. Hokamoto¹; ¹Kyushu Univ., Japan MULTIROTOR VEHICLES DESIGN BASED ON DYNAMIC MANIPULABILITY FOR UNDERACTUATED FLYING SYSTEMS |
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ICAS2020_1006: T.L. Costa¹, J.C. Vendrichoski¹, E.S. El'Youssef¹, E.R. De Pieri¹; ¹Federal University of Santa Catarina, Brazil ROBUST CONTROL OF UNMANNED AERIAL VEHICLE WITH TILT ROTORS AND CAMERA |
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ICAS2020_1088: W.Y. Zhou¹, S.M. He¹, M.M. Tian¹; ¹AVIC Xi’an Flight Automatic Control Research Institute, China ADRC BASED HIGH MANEUVERING FLIGHT CONTROL LAW DESIGN FOR UAV |
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ICAS2020_1139: X. Zheng¹, S. He¹, D. Lin¹; ¹Beijing Institute of Technology, China MULTI-UAV TRAJECTORY PLANNING BASED ON COORDINATION VARIABLES |
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ICAS2020_1157: G.H. Dou¹, Y.J. Yang¹, A.L. Gong¹, W.J. Zhou¹; ¹China Academy of Aerospace Aerodynamics, China NEW ROLL-SPIRAL COUPLING MODE CRITERION FOR HIGH-SPEED VEHICLES |
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ICAS2020_1187: A. Gomes Pereira Sarmento¹, A. Giacobini de Souza¹, A. Muniz Neves, CENIC Aeronáutica, Brazil; L.C. Sandoval Góes¹, R. Gil Annes da Silva¹; ¹Instituto Tecnológico de Aeronáutica (ITA), Brazil OPTIMIZATION OF LONGITUDINAL CONTROL OF AN AGRICULTURAL UAV USING LQR-PID CONTROL |
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ICAS2020_1228: D. Ning¹, Y. Wang¹, S. Jia¹; ¹China Academy of Aerospace Aerodynamics, Beijing, China, China A POLE CONFIGURATION CONTROLLER FOR FIXED HEIGHT CONTROL OF TILT ROTOR AIRCRAFT |
7 - Systems, Subsystems and Equipment |
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ICAS2020_0004: L. Jing, COMAC Sadri, China ANALYSIS AND SOLUTION RESEARCH OF THE AIR DATA LOSSFROM AIRCRAFT FOR ENGINE CONTROL |
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ICAS2020_0039: H. Zhao, Aircraft Strength Research Institute of China, Xi’an jiaotong Un, China; H. Tao¹, Z. Gu, Chongqing Hongyu Precision Industrial Co., Ltd., China; G. Shi, Shenyang Aircraft Design & Research Institute of China, China; S. Duan¹, J. Feng¹; ¹Aircraft Strength Research Institute of China, China STUDY ON CLOSED-LOOP CROSS COMPENSATION CONTROL TECHNOLOGY IN ACCELERATED FATIGUE TESTING |
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ICAS2020_0110: A. Dell'Amico, Saab AB/Linköping University, Sweden; F. Larsson¹, C. Johansson¹, V. De Negri, Federal University of Santa Catarina, Brazil; P. Krus, Linköping University, Sweden; ¹Saab AB, Sweden CONCEPTUAL STUDY OF THE DIGITAL HYDRAULIC ACTUATOR WITH PROPORTIONAL CONTROL FOR FLIGHT CONTROL ACTUATION SYSTEMS |
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ICAS2020_0180: X.J. Wang¹, J. Xu¹, J.H. Wang¹, J.C. Mi, Intel Engineering Simulation Technology Co.,Ltd, China; Y.M. Jiang, Tiangong University, China; ¹Aerospace Life-support Industries LTD, China RESEARCH ON THE PRESSURE COMFORT OF PILOT HELMETS |
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ICAS2020_0196: J. Fu¹, C. Zheng¹, J.-C. Mare, Institute Clément Ader (CNRS UMR 5312), INSA-Toulouse, France; W. Zhang¹; ¹School of Mechanical Engineering and Automation, Beihang Univ., China VIRTUAL PROTOTYPING OF ELECTRICAL THSA FOCUSED ON MECHANICAL POWER TRANSMISSION FUNCTIONS |
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ICAS2020_0239: S. Bazhenov¹, A. Skryabin¹, G. Veresnikov, Institute of Control Science of Russian Academy of Science, Russia; ¹Central Aerohydrodynamic Institute of Russia, Russia THE DEVELOPMENT OF ALGORITHMS FOR EMA FAULT EARLY DETECTION SYSTEM |
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ICAS2020_0273: W.-J. Mo¹, X.-X. Huang¹, J.-A. Cao, School of Electrical Engineering, Xi’an Jiaotong University, China; Q. Yin¹, X.-H. Wu¹; ¹Chengdu Aircraft Industrial (Group) Co. Ltd, China RESEARCH ON AIRBORNE RF SYSTEM TESTING TECHNOLOGY USING TDR TECHNIQUE |
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ICAS2020_0292: C.-L. Han¹, F. Chen¹, X.-M. Sun¹, W.-H. Li¹; ¹China National Aeronautical Radio Electronics Research Institute, China FLIGHT MANAGEMENT SYSTEM REQUIREMENT ANALYSIS FOR TRAJECTORY BASED OPERATION |
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ICAS2020_0344: Z. Liu¹, P. Chen¹, X. Wei¹; ¹Xi'an Flight Automatic Control Research Institute, China MEMS-BASED DISTRIBUTED NAVIGATION SYSTEM |
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ICAS2020_0386: H. Li¹, Z. Zhao¹, Y. Zhang¹, S. Zhao¹, L. Xu¹; ¹Chengdu Aircraft Industrial (Group) Company Limited, China DYNAMIC PERFORMANCE ANALYSIS AND WEIGHTED-BASED FAULT DIAGNOSIS SCHEME FOR AIRCRAFT ELECTRIC POWER SYSTEM |
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ICAS2020_0413: L. Jin¹, M. Wu¹, H. Yang¹, L. Wu¹, D. Cui, AVIC The First Aircraft Institute, China; ¹AVIC Aerospace Life-support Industries, Ltd., China RESEARCH ON OPTIMIZATION TECHNOLOGY FOR CONTROL PARAMETERS OF EJECTION SEAT BASED ON PSO ALGORITHM |
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ICAS2020_0513: Z. Skorupka¹, R. Harla¹; ¹Lukasiewicz Research Network - Institute of Aviation, Poland INVESTIGATIONS ON LANDING GEAR SHOCK ABSORBER ACTIVE FORCE CONTROL |
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ICAS2020_0514: H. Zhang¹, J.T. Wu¹, P.Q. Tian¹, Z.P. Ren¹; ¹Aircraft Strength Research Institute of China, China RESEARCH ON THE ENVIRONMENTAL WORTHINESS OF THE CIVIL AIRCRAFT USING THE FUZZY THEORY |
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ICAS2020_0577: E. Suvorova¹, V. Olenev¹; ¹St. Petersburg State University of Aerospace Instrumentation, Russia INTEGRATED ON-BOARD NETWORKS FOR NEXT GENERATION AVIONICS |
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ICAS2020_0609: L. Dong¹, W.-M. Song¹; ¹China Aeronautical Radio Electronics Research Institute, China AN AGILE PRACTICE OF AVIONICS SYSTEM DEVELOPMENT |
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ICAS2020_0661: F. Wu, Northwestern Polytechnical,AECC Sichuan Gas Turbine Establishmen, China; X.-D. Feng¹, L.-T. Leng¹, T. Liu¹, C.-Q. Yang¹; ¹AECC Sichuan Gas Turbine Establishment, China RESEARCH AND VALIDATION OF SYSTEM MODELING AND SIMULATION OF INTAKE AIR MIXER ALTITUDE TEST BED |
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ICAS2020_0662: A. Alaimo¹, C. Orlando¹; ¹Università di Enna Kore, Italy A STOCHASTIC ROBUSTNESS VERIFICATION OF NLG SIMPLE ADAPTIVE SHIMMY SUPPRESSION SYSTEM |
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ICAS2020_0723: X. Li¹, Z.J. Wang¹, X.B. Ding ¹, Z.B. Wei¹; ¹FAI AVIC, China IMPROVED DESIGN OF AIRCRAFT NOSEWHEEL STEERING SYSTEM |
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ICAS2020_0808: C. Chen¹, J.S. Shen¹, Q.C. Liu¹, B. Xue¹; ¹China Aeronautical Radio Electronics Research Institute, China PRECISION ANALYSIS AND INDEX DISTRIBUTION SYSTEM DESIGN OF AVIONICS SYSTEM BASED ON BP NEURAL NETWORK |
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ICAS2020_0822: K.T. Li¹, H.S. Ma¹, D. Wang¹; ¹China National Aeronautical Radio Electronics Research Institute, China DESIGN OF UAV NAVIGATION ALGORITHM IN SINGLE SATELLITE ENVIRONMENT BASED ON HIGH PRECISION TIMING |
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ICAS2020_0982: M.A. Rodriguez Diaz¹, E. Villani¹, P. Krus, Linköping University, Sweden; ¹Aeronautics Institute of Technology, Brazil FITT’S LAW WITH EYE TRACKING ON A FLIGHT SIMULATOR COCKPIT |
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ICAS2020_1018: B. Wu¹, X. Qui¹, Y. Zhu, COMAC SADRI, China; ¹NUAA, COMAC SADRI, China BASED ON SYSTEMS ENGINEERING PROCESS THE CIVIL AIRCRAFT PROJECT PRODUCT BREAKDOWN STRUCTURE DEVELOPMENT RESEARCH |
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ICAS2020_1114: X.C. Li¹, H.F. Wei¹, J.M. Wu¹, F. Liu¹; ¹ADR (Aviation Industry Development Research Center of China), China A MANUFACTURING COST ESTIMATION MODEL WITH RELIABILITY FOR CIVIL AERO-ENGINE |
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ICAS2020_1138: J.X. Wang¹, C.L. Zhu¹, Z. Yang¹, C.X. Zhu, Nanjing University of Aeronautics and Astronautics,, China; ¹Nanjing University of Aeronautics and Astronautics, China EXPERIMENTAL STUDY OF THE DYNAMICS CHARACTERISTICS OF AN IMPACT WATER DROPLET ON SUPERHYDROPHOBIC SURFACE |
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ICAS2020_1209: F. Larsson¹, C. Reichenwallner², A. Dell'Amico¹, P. Krus²; ¹Saab AB, Sweden; ²Linköping University, Sweden AN ONTOLOGICAL APPROACH FOR CLASSIFYING AIRCRAFT ACTUATORS |
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ICAS2020_1210: C. Reichenwallner¹, F. Larsson², A. Dell 'Amico², P. Krus¹; ¹Linköping university, Sweden; ²Saab AB, Sweden EVALUATION ASPECT MAPPING FOR ACTUATION SYSTEM DESIGN |
8 - Manufacturing and Supply Chain Management |
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ICAS2020_0093: Q. Zeng, School of Aeronautics and Astronautics, Zhejiang University, China; C. Li¹, J. Cao¹, B. Wang¹, G. Wang, ZHEJIANG UNIVERSITY, China; ¹AECC HAPRI, China EFFECTS OF COOLANT BUILD DIRECTION ON ADDITIVELY MANUFACTURED FAN-SHAPED COOLING HOLES |
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ICAS2020_0310: A. Xu, Chengdu Aircraft Industrial (Group) Co., Ltd., China ENABLING THE SMART SHOP FLOOR THROUGH THE INTEGRATION OF IOT AND AUTONOMOUS INTELLIGENCE |
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ICAS2020_0343: Y. Fan, Nanchang Hangkong University, China; C. Liu¹, J. Wang¹; ¹Northwestern Polytechnical University, China INCORPORTING KNOWLEDGE COVERAGE MEASUREMENT INTO KNOWLEDGE TRANSFORMATION FROM DATA FOR KNOWLEDGE ACCUMULATION |
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ICAS2020_0454: P. Iavecchia¹, G. Campolo¹, G. Maritano¹, M. Coppola¹, E. Cestino¹, G. Frulla¹, V. Sapienza, 2Aeronautical Consultant, Italy; P. Piana, TescoGO, Italy; ¹Politecnico di Torino, Italy APPLICATION OF ADDITIVE MANUFACTURING TO THE PRODUCTION OF RPAV COMPONENTS |
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ICAS2020_0467: R. Rameshbabu¹, D. Rajaram¹, O.J. Pinon Fischer¹, T.G. Puranik¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States AN EXERCISE IN DEVELOPING A SUPERVISED ANOMALY DETECTION MODEL WITH AUTOMATICALLY ENGINEERED FEATURES |
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ICAS2020_0503: H. Li¹, Y. Xu¹, Y. Chen¹; ¹AECC SHANGHAI COMMERCIAL AIRCRAFT ENGINE MANUFACTURING CO.,LTD., China DESIGN AND BEST PRACTICES OF SUPPLIER PERFORMANCE EVALUATION IN SUPPLY CHAIN |
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ICAS2020_0542: X. Zhu¹, H. Wang¹, L. Liu¹; ¹Chengdu Aircraft Industrial (Group) Co., Ltd, China ASSEMBLY QUALITY OPTIMIZATION APPROACH FOR LARGE-SCALE ACTIVE COMPONENTS BASED ON REVERSE ENGINEERING |
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ICAS2020_0675: T.L. Shen, Automatic Detection Technology of Large Civil Aircraft Based on, China AUTOMATIC DETECTION TECHNOLOGY OF LARGE CIVIL AIRCRAFT BASED ON IMAGE RECOGNITION |
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ICAS2020_0774: Q.Y. Liu¹, C.Y. Wang¹, P. Yan¹, H. Ruan¹, H.Z. Xue¹, L.T. Dong¹; ¹Beihang University, China AN EFFICIENT FINITE ELEMENT SIMULATION METHOD FOR ADDITIVE MANUFACTURING PROCESS |
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ICAS2020_1223: L.S. Luna¹, G.A.P. Caurin¹, M.L. Tronco¹; ¹University of São Paulo, Brazil USAGE OF MQTT, ROS, AND AWS IN THE MANUFACTURING PROCESS OF AIRCRAFTS |
9 - Air Transport System Efficiency |
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ICAS2020_0032: E. Itoh, The University of Tokyo/ENRI, Japan; F. Kato¹, K. Higasa¹, M. Schultz, Technische Universität Dresden, Germany; ¹The University of Tokyo, Japan DESIGNING AIRCRAFT TRAFFIC FLOWS USING DATA-DRIVEN QUEUING MODELS |
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ICAS2020_0202: A. Andreeva-Mori¹, Y. Matsuno¹; ¹Japan Aerospace Exploration Agency, Japan IMPACT OF ENROUTE TIME-BASED METERING ON EQUITY IN DELAY DISTRIBUTION |
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ICAS2020_0207: V. Papantoni¹, J. Scherer¹, P. Wassink¹, G. Atanasov¹; ¹German Aerospace Center (DLR), Germany ASSESSMENT OF THREE COMMUTER AIRCRAFT CONCEPTS FROM A TRANSPORT SYSTEM PERSPECTIVE |
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ICAS2020_0409: B. Moberg, Vernamack AB, Sweden; P. Näsman, KTH Royal Institute of Technology, Sweden; U. Ziverts, Infobahn AB, Sweden ERAS- EVALUATION OF REALISTIC APPROACH SCENARIOS FOR MINIMAL NOISE - PRELIMINARY FINDINGS |
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ICAS2020_0456: D. Dinh Nguyen¹, D. Rohacs¹; ¹Budapest University of Technology and Economics, Hungary AIR TRAFFIC MANAGEMENT OF DRONES INTEGRATED INTO THE SMART CITIES |
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ICAS2020_0823: W. Guo¹, R.Y. Zhang¹; ¹China National Aeronautical Radio Electronics Research Institute, China RESEARCH ON TRAJECTORY OPTIMIZATION TECHNOLOGY CONSIDERING METEOROLOGICAL INFORMATION PREDICTION |
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ICAS2020_0990: L.M.B.C. Campos, IDMEC/CCTAE/IST, Portugal; J.M.G. Marques, Escola de Ciências e Tecnologias, Universidade de Évora, Portugal ON THE MINIMUM SEPARATION BETWEEN ANY PAIR OF FLIGHT PATHS |
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ICAS2020_1005: J.A.T.G. Fregnani, Airbus, Brazil; B.S. Mattos¹, J.A. Hernandes¹; ¹ITA, Brazil AIRLINE NETWORK-AIRPLANE INTEGRATED OPTIMIZATION CONSIDERING MANUFACTURER'S PROGRAM COST |
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ICAS2020_1009: P. Lertworawanich¹, N. Pongsakornsathien¹, Y. Xie¹, A. Gardi¹, R. Sabatini¹; ¹RMIT University, Australia ARTIFICIAL INTELLIGENCE AND HUMAN-MACHINE INTERACTIONS FOR STREAM-BASED AIR TRAFFIC FLOW MANAGEMENT |
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ICAS2020_1015: A. Rodriguez-Sanz, Universidad Politecnica de Madrid (UPM), Spain; J. Herrera de la Cruz , Universidad Complutense de Madrid (UCM), Spain A NOVEL APPROACH FOR TURNAROUND TIME ALLOCATION BASED ON REINFORCEMENT LEARNING |
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ICAS2020_1133: K. Lippoldt¹, L. Preis, Bauhaus Luftfahrt e.V., Germany; K. Bogenberger¹; ¹Technical University Munich, Germany VERTIPORT PLACEMENT METHOD BASED ON MOBILITY SURVEY DATA |
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ICAS2020_1162: R. Camilleri¹, A. Batra¹; ¹Institute of Aerospace Technologies, University of Malta, Malta ASSESSING THE ENVIRONMENTAL IMPACT OF AIRCRAFT TAXIING TECHNOLOGIES |
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ICAS2020_1205: T. Mori, Osaka Prefecture University, Japan POINT MERGE SYSTEM AND ARRIVAL METERING SYNERGY EFFECT ESTIMATION OF INBOUND FLIGHT EFFICIENCY AT TOKYO INTERNATIONAL (HANEDA) AIRPORT |
10 - Safety and Security |
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ICAS2020_0012: J. Rataj¹, O. Ohneiser¹, G. Marin², R. Postaru²; ¹DLR, Germany; ²ROMATSA, Romania ATTENTION: TARGET AND ACTUAL - THE CONTROLLER FOCUS |
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ICAS2020_0163: D. Ding¹, W.-Q. Qian¹, Q. Wang¹; ¹China Aerodynamics Research and Development Center, China AIRCRAFT INFLIGHT ICING DETECTION AND DIAGNOSIS METHODS |
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ICAS2020_0186: Y. Liu, Shanghai Aircraft Design and Research Institute, China DESIGN AND RESEARCH ON SAFETY ANALYSIS TOOL FOR AVIONICS SYSTEM |
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ICAS2020_0219: Q. Zhang¹, Z. Zhou¹; ¹Northwestern Polytechnical University, China RESEARCH ON SAFETY ASSESSMENT APPROACH FOR UAS OPERATIONS OVER UNINHABITED AREAS |
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ICAS2020_0231: Y. Mou¹, M. Jiang¹, G. Zhu¹; ¹Nanjing Engineering Institute of Aircraft Systems, China CERTIFICATION CONSIDERATIONS FOR EVTOL AIRCRAFT |
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ICAS2020_0268: Q. Zhu¹, C.X. Wang¹; ¹AECC Commercial Aircraft Engine Co. Ltd, China APPLICATION OF DEVELOPMENT ASSURANCE METHODOLOGIES TO ELECTRONIC ENGINE CONTROL SYSTEM (EECS) |
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ICAS2020_0378: X. Chen¹, J. Huang¹, M. Meng, Wenzhou Meteorological Burea, China; C. Chen¹, Q. Chen¹; ¹China Aerodynamics Research and Development Center, China ACTIVITY CHARACTERISTICS AND THE MECHANISM OF MESO-MICRO SCALE DISTURBANCES IN THE EAST ASIAN SUBTROPICAL UPPER-LEVEL JET STREAM |
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ICAS2020_0510: J.J. Han, Nanjing engineering Institute of Aircraft System, Jincheng, AVIC, China; G. Li, Nanjing University of Aeronautics and Astronautics, China EXPERIMENTAL STUDY ON CRITICAL HEAT FLUX CHARACTERISTICS OF R134A FLOW BOILING IN A HORIZONTAL 2.1 MM TUBE UNDER HYPERGRAVITY |
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ICAS2020_0533: R. Mori, Electronic Navigation Research Institute, Japan ANALYSIS OF PILOT OPERATIONAL STRATEGY DIFFERENCE USING NEURAL NETWORK |
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ICAS2020_0638: U. Kale¹, O. Alharasees¹, F. Kling, Research, Development and Simulation Department, HungaroControl, Hungary; D. Rohacs¹; ¹Budapest University of Technology and Economics, Hungary OBJECTIVE MEASUREMENT OF HUMAN FACTORS FOR SUPPORTING THE OPERATOR’S LOAD SIMULATION AND MANAGEMENT |
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ICAS2020_0649: H.K. Lee¹, T.G. Puranik¹, O.J. Pinon Fischer¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States TOWARDS AN ONLINE PREDICTIVE MODEL OF AIRCRAFT ENERGY STATE USING SUPERVISED MACHINE LEARNING |
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ICAS2020_0715: C.X. Wang¹, Q. Zhu¹, X.K. Wang¹, X.H. Tang¹; ¹AECC Commercial Aircraft Engine Co. Ltd, China RESEARCH ON CERTIFICATION MANAGEMENT OF AIRCRAFT ENGINE BASED ON RISK ANALYSIS |
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ICAS2020_0747: M. Wojtas¹, K. Raczko¹, L. Czajkowski¹; ¹Institute of Aviation, Poland PROTOTYPE WHIRL TOWER FOR TESTING INSOLATED ROTOR SYSTEMS IN HOVER |
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ICAS2020_0761: H. Tao, CAPEChina Aero-Polytechnology Establishment, China; L. Haixia¹, Y. Ning¹; ¹China Aero-Polytechnology Establishment, China STUDY ON THE AIRWORTHINESS AND COMFORTABLENESS REQUIREMENTS OF AIRCRAFT CABIN AIR CONTAMINATIONS |
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ICAS2020_0919: K. Okubo¹, J.O. Entzinger¹; ¹The University of Tokyo, Japan AN OVERVIEW OF FLARE TECHNIQUES AND FLARE TRAINING METHODS |
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ICAS2020_1061: K. Tong¹, Y. Song¹, X.-F. Kong¹, K.-W. Zhang¹, Z.-J. Chen¹; ¹Civil Aviation University of China, China AN INTEGRATED METHOD FOR ACCURATE IDENTIFICATION AND DYNAMIC MONITORING OF BUILDINGS IN AERODROME OBSTACLE FREE SPACE |
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ICAS2020_1064: Q. Jia¹, W. Zhang¹, J. Shi¹, J. Hu¹, E. Safwat, Military Technical College, Egypt; ¹Northwestern Polytechnical University, China RESEARCH ON FAULT DIAGNOSIS AND FAILURE RECONFIGURATION OF FLUSH AIR DATA SENSING |
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ICAS2020_1069: H. Wang¹, H. Wang¹; ¹Shanghai Aircraft Design and Research Institute, China NUMERICAL ANALYSIS METHOD OF CIVIL AIRCRAFT DITCHING FLOATING PERFORMANCE |
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ICAS2020_1127: S.-Z. Zhao¹, X. Zhao¹, R. Yao¹, Y.-F. Lin, China Helicopter Research and Development Institute, China; ¹Northwestern Polytechnical University, China FLIGHT PERFORMANCE AND TRAJECTORY PREDICTION OF THE COAXIAL HELICOPTER IN AUTOROTATION |
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ICAS2020_1148: B. Miao¹, M.-X. Bao¹, C.-L. Zhu¹; ¹Nanjing University of Aeronautics and Astronautics, China ULTRASONIC DE-ICING SYSTEM DESIGN METHODS BASED ON RESONANCE AND IMPEDANCE MATCHING |
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ICAS2020_1156: Q.-L. Guo¹, W.-M. Sang¹, J.-J. Niu¹, A.-X. Qiu¹; ¹Northwestern Polytechnical University, China A NUMEIRCAL PREDICTION OF THE AIRCRAFT ICING METEOROLOGICAL ENVIRONMENT |
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ICAS2020_1178: S.L. Ding¹, Q.L. Qu¹, P.Q. Liu¹; ¹Beihang University, China NUMERICAL STUDY OF DITCHING CHARACTERISTICS OF BWB AIRCRAFT |
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ICAS2020_1193: X. Liu¹, L. Manfriani, Centre for Aviation, Zurich University of Applied Sciences, Switzerland; Y. Fu¹; ¹Lab. of Aerosp. Servo Actuation and Transmission, Beihang Univ., China CONCEPT OF A NEW SYSTEM SYNTHESIZING METEOROLOGICAL AND OROGRAPHIC INFLUENCES ON THE AIRPLANE SAFE ENERGY ENVELOPE |
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ICAS2020_1237: M. Emara¹, M. dos Santos¹, N. Chartier¹, J. Ackley¹, T.G. Puranik¹, A. Payan¹, M. Kirby¹, O.J. Pinon¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States MACHINE LEARNING ENABLED TURBULENCE PREDICTION USING FLIGHT DATA FOR SAFETY ANALYSIS |
11 - Operations and Sustainment |
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ICAS2020_0052: R.P. Liu, China; Q. Wang, China; G.Y. He, China; M.T. Tang, China; J.X. Ren, China THE DATABASE DESIGN OF UNMANNED AERIAL VEHICLE |
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ICAS2020_0117: D.M. Steinweg¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany COST AND BENEFIT OF SCHEDULED STRUCTURAL HEALTH MONITORING FOR COMMERCIAL AIRCRAFT |
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ICAS2020_0125: D. Goutaudier, CNRS, France; D. Gendre, Airbus, France REAL TIME IMPACT LOCALIZATION USING MODAL SUPERPOSITION - APPLICATION TO A COMPOSITE AIRCRAFT FUSELAGE |
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ICAS2020_0130: J. Källström¹, R. Granlund, RISE SICS East, Sweden; F. Heintz¹; ¹Linköping University, Sweden DESIGN OF SIMULATION-BASED PILOT TRAINING SYSTEMS USING MACHINE LEARNING AGENTS |
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ICAS2020_0225: Y. He, Air Force Engineering University, China ON AIRCRAFT OPERATIONAL INTEGRITY |
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ICAS2020_0347: J. van Doeselaar¹, D. Daverschot¹; ¹Airbus, France STRUCTURAL HEALTH MONITORING - THE ROUTE TO CONDITION BASED MAINTENANCE |
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ICAS2020_0408: Y.H. Wang, China; Z.J. Zhan, China; B. Xue, China; P.Y. Deng, China INFORMATION DISTRIBUTION METHOD FOR MULTI-AIRCRAFT COOPERATION BASED ON COLLABORATIVE FILTERING ALGORITHM |
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ICAS2020_0602: Q. Wang¹, C. Sun¹, B. Hao¹; ¹ Chengdu Aircraft Design and Research Institute, AVIC, China A STUDY ON TRAINING NEEDS ANALYSIS (TNA) METHOD FOR MILITARY AIRCRAFT |
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ICAS2020_0635: D.D. Nguyen¹, U. Kale¹, A.W. Wangai¹; ¹Budapest University of Technology and Economics, Hungary TOTAL LIFE CYCLE COST AND EMISSION OF ELECTRIC, HYBRID-ELECTRIC AIRCRAFT |
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ICAS2020_0659: V. Gros¹, P.-C. Rolland¹, S. Veron¹, B. Ordy¹, F. Dessertenne, AIRBUS OPERATIONS SAS, France; ¹AIRBUS SAS, France CONDITION BASED MAINTENANCE (CBM) IN THE DIGITAL TRANSFORMATION STREAM |
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ICAS2020_0764: D.N. Dong¹, Z.Y. Jia¹, Y. Zhou¹; ¹AVIC China Aero-Polytechnology Establishment, China A METHOD FOR EVALUATING THE APPLICABILITY OF MAINTENANCE TASKS BASED ON HELICOPTER HEALTH AND USAGE MONITORING SYSTEM |
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ICAS2020_1213: O. Lehmann¹, R. El-Jabi¹, K. Webster¹, A. Rachdi¹, Z. Malik¹; ¹Abu Dhabi University, United Arab Emirates INTEGRATION OF SPACE VEHICLE OPERATIONS INTO THE UNITED ARAB EMIRATES AIR TRAFFIC MANAGEMENT - AN IMPACT ANALYSIS |
12 - Host nation |
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ICAS2020_1281: J. Leng, China SHAPE MORPHING SMART STRUCTURES: MECHANICS, MATERIALS AND APPLICATIONS |
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ICAS2020_1282: P. Xia, China AN OVERVIEW OF HELICOPTER DEVELOPMENT IN CHINA AND SOME NEW HELICOPTER TECHNOLOGIES |
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ICAS2020_1283: S. Yin, China SMART CIVIL AVIATION TRANSPORTATION SYSTEM |
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ICAS2020_1284: Y. Chen, China FLIGHT TEST ON THE ICING OF CIVIL AIRCRAFT |
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ICAS2020_1285: C. Shao, China CURRENT PROGRESS AND FUTURE PROSPECTS OF CHINESE COMMERCIAL AIRCRAFT ENGINE DEVELOPMENT |
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ICAS2020_1294: D. Krob, France TOWARDS AGILE SYSTEMS ENGINEERING: AN ITERATIVE & COLLABORATIVE APPROACH FOR COMPLEX SYSTEMS DEVELOPMENT |
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ICAS2020_1296: F. Wu, China DEPLOY SYSTEM ENGINEERING METHODS IN AIRBORNE GUIDANCE NAVIGATION CONTROL DOMAIN |
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ICAS2020_1298: L. Gao, China MODEL BASED DESIGN AND PRACTICE FOR AVIONICS SYSTEM |
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ICAS2020_1308: X.H. Gao, China IMPLEMENTATION MECHANISM OF UAS INTEROPERABILITY BASED ON ARCHITECTURE META-MODEL |
14 - Education and Training |
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ICAS2020_1304: J.P. Eguea, please select... HOW CAN A CAMBER MORPHING WINGLET CONTRIBUTE TO MAKING AVIATION GREENER |
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ICAS2020_1305: J. Choi, Germany A STUDY ON DEEP LEARNING BASED AUTOMATED AERIAL DOCKING SYSTEM |
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ICAS2020_1306: T.M.B. Bastos, Germany TASK ALLOCATION ALGORITHMS FOR A COOPERATIVE DRONE PARCEL DELIVERY SYSTEM |
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ICAS2020_1314: D. Veerasamy UNPRECEDENTED TRANSITIONAL CHARACTERISTICS IN WAKE – BOUNDARY LAYER INTERACTION |
15 - Guest lectures |
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ICAS2020_1047: M. Pott-Pollenske, Germany NOISE REDUCTION AT FLAP SIDE EDGE AND UNDERCARRIAGE |
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ICAS2020_1048: G. Ernst, German Aerospace Center, Germany; S. Pawellek¹, A. Büscher¹; ¹Airbus Operations GmbH, Germany FLIGHT TEST OF AN ADVANCED HYBRID-LAMINAR-FLOW-CONTROL (HLFC) SYSTEM ON AN A320 VERTICAL TAIL PLANE |
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ICAS2020_1049: R. Abarca López¹, C. Aquilini¹, P. Lubrina, ONERA, France; S.-H. Peng, FOI, Sweden; J. Schwochow, DLR, Germany; ¹Airbus, Spain MAIN LANDING GEAR DOORS VIBRATION REDUCTION BASED ON FLIGHT TEST |
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ICAS2020_1051: R. Degenhardt, DLR, Germany; D. Paraschivoiu, NRC, Canada IFAR - INFRASTRUCTURE DATABASE |
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ICAS2020_1052: R.V. Lakshmi¹, S.T. Aruna¹, S. Sampath, Indian Institute of Science, India; ¹CSIR-National Aerospace Laboratories, India SOL-GEL BASED ORGANIC-INORGANIC HYBRID COATINGS FOR CORROSION PROTECTION OF AEROSPACE ALUMINIUM ALLOY |
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ICAS2020_1054: G. Goinis¹, C. Voß¹, E. Nicke¹; ¹German Aerospace Center (DLR), Germany THE POTENTIAL OF CASING TREATMENTS FOR TRANSONIC COMPRESSORS: EVALUATION BASED ON AXIAL-SLOT AND ROTOR BLADE OPTIMIZATION |
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ICAS2020_1058: R. Schnell, German Aerospace Center (DLR), Germany; E. Goldhahn, Airbus Operations GmbH, Germany; M. Julian, Airbus Operations SAS, France DESIGN AND PERFORMANCE OF A LOW FAN-PRESSURE-RATIO PROPULSION SYSTEM |
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ICAS2020_1257: M. Wahlich, Airbus, Germany ACTIVE FLOW- LOADS & NOISE CONTROL ON NEXT GENERATION WING (AFLONEXT): OVERVIEW AND RESULTS |
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ICAS2020_1288: P.D. Ciampa, Germany ICAS DIGITAL PIONEERING INITIATIVE AND FUTURE PERSPECTIVES ON MDO & MBSE |
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ICAS2020_1289: G. La Rocca, Netherlands FUTURE PERSPECTIVES ON KBE & AI |
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ICAS2020_1290: S. Bagassi, Italy FUTURE PERSPECTIVES ON VR & AR |
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ICAS2020_1291: C. Jouannet, Sweden FUTURE PERSPECTIVES ON SOSE |
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ICAS2020_1299: B. Nagel¹, E. Moerland¹; ¹German Aerospace Center, Germany COLLABORATIVE AIRCRAFT DESIGN TECHNIQUES IN RESEARCH |
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ICAS2020_1300: T. Nunes, CEIIA, Portugal IFAR-X COLLABORATIVE AIRCRAFT DESIGN EXERCISE ON ENVIRONMENTALLY COMPATIBLE TRANSPORT AIRCRAFT |
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ICAS2020_1301: P. Novelli, ONERA, France COLLABORATIVE AIRCRAFT DESIGN EXERCISE BEYOND IFAR |
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ICAS2020_1302: E. Campillo-Borras, Germany HARMONIZING SUSTAINABLE AVIATION RESEARCH AMONG IFAR ORGANIZATIONS |
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ICAS2020_1307: A. Mirzoyan, Russia PROPOSAL FOR INTERNATIONAL FIRE AVIATION SERVICE UNDER THE AUSPICES OF ICAO TO IMPROVE WORLD WILDFIRE MANAGEMENT |
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ICAS2020_1311: J. Hupe, Canada ICAO ADDRESSING CLIMATE CHANGE AND WILDFIRES |
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ICAS2020_1313: I. Labzin, Belarus EXPERIENCE OF BELARUS IN USING HELICOPTER TECHNOLOGY FOR FOREST FIREFIGHTING |