Preliminary Programme - Session List
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Attention: Be advised that there might be changes till the congress, so please do not adjust your travel plans based on this preliminary programme.
7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
Monday, 06. Sep 2021
7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
| 07:00 - 08:00 | Registration | |||
| 08:00 - 09:00 | Opening Ceremony | |||
| 0.1 | ICAS Daniel & Florence Guggenheim Memorial Lecture, Yesterday,Today & Tomorrow of AVIC, Yang Wei, China Chair: S. Suzuki ICAS President | |||
| 06. Sep 21 | 09:00 | 10:00 |
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| 10:00 - 10:30 | Break | |||
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| 06. Sep 21 | 10:30 | 11:00 | 1.1.1 |
TECHNOLOGY INTEGRATION FOR FUTURE AIRCRAFT CONFIGURATIONS D. Reckzeh, Airbus, Germany | |||
| 06. Sep 21 | 11:00 | 11:30 | 1.1.2 |
TECHNOLOGY INTEGRATION AND OVERALL AIRCRAFT PERFORMANCE ASSESSMENT FOR AN ADVANCED MID-RANGE AIRCRAFT S. Woehler, German Aerospace Center, Germany | |||
| 06. Sep 21 | 11:30 | 12:00 | 1.1.3 |
MAXIMIZING THE DEGREE OF SIMILITUDE OF SUB-SCALE MODELS TO SUPPORT SCALED FLIGHT TESTING A Raju Kulkarni, TU Delft, Netherlands | |||
| Reserve Paper | 1.1.R |
MULTI-ROLE TANKER-TRANSPORT CONVERSION Ilan Berlowitz, IBAero Engineering, Israel | |||||
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| 06. Sep 21 | 10:30 | 11:00 | 2.1.1 |
VAST – VERSATILE AEROMECHANICS SIMULATION PLATFORM FOR HELICOPTERS J. Hofmann, German Aerospace Center (DLR), Germany | |||
| 06. Sep 21 | 11:00 | 11:30 | 2.1.2 |
HELICOPTER FLIGHT DYNAMICS MODELLING WITH FREE-WAKE METHOD EMBEDDED FOR ROTOR ICING ANALYSES Guozhi Li¹, Guanglin Zhang¹, Shiyong Chu¹; ¹Aviation Industry Development Research Center of China, China | |||
| 06. Sep 21 | 11:30 | 12:00 | 2.1.3 |
DESIGN AND ANALYSIS METHOD OF HELICOPTER ANTI-BALLISTIC VULNERABILITY P. Hou, School of Aeronautics, Northwestern Polytechnical University, China | |||
| Reserve Paper | 2.1.R |
REGRESSION HIERARCHICAL KRIGING FOR NOISY DATA FUSION WITH APPLICATION TO ROTOR AERODYNAMIC DESIGN OPTIMIZATION sw Yang, Seoul National University, South Korea | |||||
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| 06. Sep 21 | 10:30 | 11:00 | 3.1.1 |
STRATEGIES TO ENHANCE CONFIGURATIONS FOR HIGH-PRECISION MULTI-DISCIPLINARY OPTIMIZATION L.-H. LIU, Science and Technology on Electro-optic Control Laboratory, Chin, China | |||
| 06. Sep 21 | 11:00 | 11:30 | 3.1.2 |
SYSTEM ARCHITECTING: THE ARCHITECTURE DESIGN PROBLEM AS A GRAPH J.H. Bussemaker, DLR, Germany | |||
| 06. Sep 21 | 11:30 | 12:00 | 3.1.3 |
AIRCRAFT CRUISE PERFORMANCE DESIGN INTEGRATION BASED ON SYSTEM ENGINEERING HBH BIHAI, COMAC/SADRI, China | |||
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| 06. Sep 21 | 10:30 | 11:00 | 4.1.1 |
A COMPARISON OF QUASI-STEADY STATE AND UNSTEADY COMPUTATIONAL METHODS FOR PITCH DAMPING DERIVATIVE ESTIMATES T Bykerk, Australia | |||
| 06. Sep 21 | 11:00 | 11:30 | 4.1.2 |
NONLINEAR UNSTEADY AERODYNAMIC DESCRIPTIONS BASED ON IMPROVED GOMAN\\\'S MODEL Xiao-jun WU¹, Dong HAO¹, Hong-yin JIA¹, Shen-shen LIU¹; ¹CARDC, China | |||
| 06. Sep 21 | 11:30 | 12:00 | 4.1.3 |
DATA FUSION UNSTEADY AERODYNAMIC MODELING BASED ON EXPERIMENTAL DATA X W Wang, China | |||
| Reserve Paper | 4.1.R |
HIGHER ORDER DERIVATIVES OF UNSTEADY AERODYNAMICS OF AIRFOIL ASSOCIATED WITH FORCED PITCHING/PLUNGING MOTIONS Q ZHANG, Xi'an Aeronautical University, China | |||||
| Reserve Paper | 4.1.R |
EFFECT OF MACH NUMBER AND ANGLE OF ATTACK ON AERODYNAMICS OF OA309 AIRFOIL Y. J. Jin, Northwestern Polytechnical University, China | |||||
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| 06. Sep 21 | 10:30 | 11:00 | 5.1.1 |
EXPERIMENTAL INVESTIGATIONS OF A FULL MODEL WITH ADAPTIVE ELASTO-FLEXIBLE MEMBRANE WINGS J Pflueger, Technical University Munich, Chair Aerodynamics/Fluidmechanics, Germany | |||
| 06. Sep 21 | 11:00 | 11:30 | 5.1.2 |
EXPERIMENTAL ANALYSIS OF A BLOWN-WING CONFIGURATION DURING TRANSITION FLIGHT Y Leng, ISAE, France | |||
| 06. Sep 21 | 11:30 | 12:00 | 5.1.3 |
WIND TUNNEL ASSESSMENT OF A PASSIVE-ADAPTIVE WING FOR DRAG REDUCTION C. B. York, Singapore Institute of Technology, Singapore | |||
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| 06. Sep 21 | 10:30 | 11:00 | 6.1.1 |
COMPUTATIONAL STUDY OF THREE-DIMENSIONAL OPEN CAVITY FLOWS Y Luo, China | |||
| 06. Sep 21 | 11:00 | 11:30 | 6.1.2 |
NUMERICAL STUDY OF THE SIDEWALL EFFECTS ON THE OSCILLATORY SHEAR LAYER IN THE CAVITY FLOW OF HIGH REYNOLDS NUMBER Q.-L. GUO, China | |||
| 06. Sep 21 | 11:30 | 12:00 | 6.1.3 |
DETACHED-EDDY SIMULATIONS OF LEADING EDGE PLATE FLOW CONTROL BEFORE HIGH-SPEED CAVITY PC.C Cui, China Aerodynamics Research and Development Center, China | |||
| Reserve Paper | 6.1.R |
EXPERIMENTAL STUDY ON SUPERSONIC CAVITY ACOUSTICS M. JIAN, CADI, China | |||||
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| 06. Sep 21 | 10:30 | 11:00 | 7.1.1 |
MEDIUM-FIDELITY NOISE ASSESSMENT OF NOVEL MID RANGE TRANSPORT AIRCRAFT M. Lummer, German Aerospace Center (DLR), Germany | |||
| 06. Sep 21 | 11:00 | 11:30 | 7.1.2 |
SNGR BASED FAST ANALYSIS OF SLAT TRACK NOISE SOURCES W Wang, Shanghai Aircraft Design and Research Institute, China | |||
| 06. Sep 21 | 11:30 | 12:00 | 7.1.3 |
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF A DRESSED NOSE LANDING GEAR L.-B. Botero-Bolívar, University of São Paulo, Brazil | |||
| Reserve Paper | 7.1.R |
AERODYNAMIC NOISE SIMULATION OF CIVIL AIRCRAFT LANDING GEARS BASED ON LATTICE BOLTZMANN LES-SMARGORINSKY MODEL Qing Li, Chinese Aeronautical Establishment, China; Bao Chen¹, Puyuan Wang¹; ¹AVIC Aerodynamics Research Institute, China | |||||
| Reserve Paper | 7.1.R |
INVESTIGATION OF FLOW ACOUSTIC CHARACTERISTICS OF ROTOR-ROTOR INTERACTION FOR MULTICOPTER Y. Jo, South Korea | |||||
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| 06. Sep 21 | 10:30 | 11:00 | 8.1.1 |
TESTING INVESTIGATION OF FLEXIBLE WING LIMIT CYCLES WITH AILERON FREEPLAY NONLINEARITY X.-F. He, Shanghai Aircraft Airworthiness Certification Center of CAAC, China | |||
| 06. Sep 21 | 11:00 | 11:30 | 8.1.2 |
EXPERIMENTAL AND THEORETICAL STUDY ON FLUTTER ANALYSIS OF A VERY FLEXIBLE WING Z.C FU , China Academy of Aerospace Aerodynamics (CAAA), China | |||
| 06. Sep 21 | 11:30 | 12:00 | 8.1.3 |
THEORETICAL AND EXPERIMENTAL INVESTIGATION OF THE AEROELASTIC CHARACTERISTICS OF THE AFLONEXT PROJECT DEMONSTRATOR G. A. Amiryants, TsAGI, Russia | |||
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| 06. Sep 21 | 10:30 | 11:00 | 9.1.1 |
AERODYNAMC PERFORMANCE IMPROVEMENT OF A TRANSONIC AXIAL COMPRESSOR BY SWEPT AND LEANED ROTORS K You, Northwestern Polytechnical University, China | |||
| 06. Sep 21 | 11:00 | 11:30 | 9.1.2 |
FLOW TURBULENCE INVESTIGATION AT THE LINEAR CASCADE’S OUTLET A.D. Nepomnyashchiy, Central Institute of Aviation Motors, Russia | |||
| 06. Sep 21 | 11:30 | 12:00 | 9.1.3 |
DESIGN EXPERIENCE OF PENETRATION COOLING SYSTEM FOR HIGH-TEMPERATURE TURBINE BLADES S. Kharkovskiy, CIAM, Russia | |||
| Reserve Paper | 9.1.R |
PROBABILISTIC ANALYSIS OF A TURBOFAN SECONDARY AIR SYSTEM BASED ON MEASURED DATA OF LABYRINTH SEALS C. -X Song, AECC Shenyang Engine Research Institute, China | |||||
| Reserve Paper | 9.1.R |
INFLUENCE OF THE AXIAL ASSEMBLAGE DEVIATION ON PERFORMANCE OF ONE TRANSONIC CENTRIFUGAL COMPRESSOR Z.-W. Zhang, AECC HAPRI, China | |||||
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| 06. Sep 21 | 10:30 | 11:00 | 10.1.1 |
A COMPUTATIONAL MODEL OF 3 D.O.F. AIRFOIL FOR FLUTTER ANALYSIS WITH CFD BASED AERODYNAMIC FORCES A.-O Alam, Dalian university of technology , China | |||
| 06. Sep 21 | 11:00 | 11:30 | 10.1.2 |
COMPUTATIONAL FLUID-STRUCTURE INTERACTIONS OF A 3D FLEXIBLE FLAPPING WING Y.-D. Dong, China | |||
| 06. Sep 21 | 11:30 | 12:00 | 10.1.3 |
COMPUTATION OD ELASTIC FOR A TRANSPORT AIRPLANE FITTED WITH WINGLETS BY FLUID-STRUCTURE INTERACTION Mattos, B. S. Mattos, Instituto Tecnologico de Aeronautica (ITA), Brazil | |||
| Reserve Paper | 10.1.R |
AEROELASTIC RESPONSE CALCULATION USING DUHAMEL INTEGRAL AND ITS APPLICATIONS L. Bortolotto, Brazil | |||||
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| 06. Sep 21 | 10:30 | 11:00 | 11.1.1 |
SYSTEM OF UNMANNED AERIAL VEHICLES FOR WILD BOARS WITH AFRICAN SWINE FEVER SYMPTOMS DETECTION K.-S. Sibilski, Air Force Institute of Technology, Poland | |||
| 06. Sep 21 | 11:00 | 11:30 | 11.1.2 |
EVALUATION OF AN OBSTACLE TRACKING SYSTEM FOR AIRCRAFT GROUND OPERATIONS K.T. Theuma, University of Malta, Malta | |||
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| 06. Sep 21 | 10:30 | 11:00 | 12.1.1 |
STRUCTURAL HEALTH MONITORING – THE ROUTE TO CONDITION BASED MAINTENANCE J van Doeselaar, Airbus, France | |||
| 06. Sep 21 | 11:00 | 11:30 | 12.1.2 |
COST AND BENEFIT OF STRUCTURAL HEALTH MONITORING FOR COMMERCIAL AIRCRAFT D. M. Steinweg, Bauhaus-Luftfahrt e.V., Germany | |||
| 06. Sep 21 | 11:30 | 12:00 | 12.1.3 |
REAL TIME IMPACT IDENTIFICATION TECHNIQUE USING MODAL SUPERPOSITION / APPLICATION ON AIRCRAFT FUSELAGE D GENDRE, AIRBUS, France | |||
| Reserve Paper | 12.1.R |
COMPOSITE RECYCLING – AN OVERVIEW OF A 21ST CENTURY CHALLENGE IN AEROSPACE INDUSTRY J. Mašek, Brno University of Technology, Faculty of Mechanical Engineering, Czech Republic | |||||
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| 12:00 - 13:00 | Lunch | |||
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| 06. Sep 21 | 13:00 | 13:30 | 1.2.1 |
SYSTEM OF SYSTEMS DRIVEN AIRCRAFT DESIGN FOR WILDFIRE SUPPRESSION P Shiva Prakasha, DLR - German Aerospace Center, Germany | |||
| 06. Sep 21 | 13:30 | 14:00 | 1.2.2 |
OPTIMAL AIRLINE FLEET COMPOSED BY A COMBINATION OF JET AND TURBOPROP AIRPLANES Mattos, B. S. Mattos, Instituto Tecnologico de Aeronautica (ITA), Brazil | |||
| 06. Sep 21 | 14:00 | 14:30 | 1.2.3 |
BENEFIT ANALYSIS OF AIR REFUELING SYSTEM IN ULTRA LONG RANGE ROUTE OPERATION M.C MA, COMAC, China | |||
| Reserve Paper | 1.2.R |
CLOUD-BASED ENVIRONMENT FOR AIRCRAFT DESIGN COLLABORATION X. Chen, Cranfield University, United Kingdom | |||||
| Reserve Paper | 1.2.R |
QUANTIFICATION OF OPERATIONAL EFFECTIVENESS FOR TECHNOLOGY EVALUATION A. Hull, Georgia Institute of Technology, United States | |||||
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| 06. Sep 21 | 13:00 | 13:30 | 2.2.1 |
A CONCEPTUAL DESIGN OF LSA CLASS AMPHIBIOUS AIRCRAFT S. Hanada, Sophia University, Japan | |||
| 06. Sep 21 | 13:30 | 14:00 | 2.2.2 |
AEROELASTIC OPTIMIZATION OF A BLENDED WING BODY AIRCRAFT CONSIDERING STABILITY/CONTROL CONSTRAINTS X.Z. Wang, Beihang University, China | |||
| 06. Sep 21 | 14:00 | 14:30 | 2.2.3 |
PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY Z. L. Chen, Northwestern Polytechnical University, China | |||
| Reserve Paper | 2.2.R |
STUDY ON ADJOINT BASED OPTIMIZATION OF BWB CONFIGURATION CONSIDERING THE INTAKE AND EXHAUST EFFECTS J.-T. Huang, China Aerodynamics Research and Development Center, China | |||||
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| 06. Sep 21 | 13:00 | 13:30 | 3.2.1 |
A COLLABORATIVE, DISTRIBUTED AND MULTILEVEL PROCESS TO SUPPORT THE DESIGN OF A NOVEL MID-RANGE AIRCRAFT CONFIGURATION B. Gerlinger, DLR, Germany | |||
| 06. Sep 21 | 13:30 | 14:00 | 3.2.2 |
ASTRID-H: A CONCEPTUAL DESIGN METHODOLOGY AND TOOL TO SUPPORT HIGH-SPEED VEHICLE DESIGN R. Fusaro, Politecnico di Torino, Italy | |||
| 06. Sep 21 | 14:00 | 14:30 | 3.2.3 |
RESEARCH ON AERO-ENGINE COLLABORATIVE DESIGN PROCESS BASED ON SYSTEM ENGINEERING C.-Y.G. YINGANG, AECC Commercial Aviation Engine .LITD, China | |||
| Reserve Paper | 3.2.R |
THE APPLICATION OF DIGITAL TWIN TECHNOLOGY IN INTELLIGENT OPERATION AND MAINTENANCE OF AERO-ENGINE W-P Wang, Aero-Engine Academy of China, China | |||||
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| 06. Sep 21 | 13:00 | 13:30 | 4.2.1 |
NUMERICAL SIMULATIONS OF TRANSONIC BUFFET ON A HALF WING-BODY CONFIGURATION F. Sartor, ONERA, France | |||
| 06. Sep 21 | 13:30 | 14:00 | 4.2.2 |
UNSTEADY FLOW SIMULATION AROUND MAIN LANDING GEAR USING HIERARCHICAL CARTESIAN GRID METHOD WITH IMMERSED BOUNDARY METHOD T. Imamura, The University of Tokyo, Japan; Y. Tamaki, Tohoku University, Japan | |||
| 06. Sep 21 | 14:00 | 14:30 | 4.2.3 |
NUMERICAL SIMULATION OF A BIO-INSPIRED FLEXIBLE FLAPPING-WING BASED ON EXPERIMENTAL MEASURED DEFORMATION X.-Y. Yang, School of Aeronautics, Northwestern Polytechnical University, China | |||
| Reserve Paper | 4.2.R |
ATMOSPHERIC TURBULENCE EFFECTS ON SONIC BOOM PROPAGATION Z-S Qian, AVIC Aerodynamics Research Institute, China | |||||
| Reserve Paper | 4.2.R |
INVESTIGTION OF AERODYNAMIC INTERACTIONS BETWEEN NACA0012 AIRFOILS IN TANDEM Hongyi Xu, Department of Aeronautics and Astronautics, Fudan University, China | |||||
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| 06. Sep 21 | 13:00 | 13:30 | 5.2.1 |
EXPERIMENTAL INVESTIGATION OF DAMAGE WING IMPACT ON THE AIRLINER AERODYNAMIC CHARACTERISTICS Andrzej. A. Krzysiak, ?ukasiewicz Research Network – Institute of Aviation, Poland | |||
| 06. Sep 21 | 13:30 | 14:00 | 5.2.2 |
WIND-TUNNEL INVESTIGATION OF AERODYNAMIC CHARACTERISTICS FOR COMMERCIAL TRANSPORT AIRCRAFT AT EXTREME FLIGHT CONDITIONS L. zhang, China Aerodynamics Research and Development Center , China | |||
| 06. Sep 21 | 14:00 | 14:30 | 5.2.3 |
EXPERIMANTAL INVESTIGATION OF THE CHN-T1 MODEL IN FL-13 WIND TUNNEL OF CARDC AND DNW-LLF FACILITY F.L.T Fan, CARDC, China | |||
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| 06. Sep 21 | 13:00 | 13:30 | 6.2.1 |
DECENTRALIZED CONFLICT DETECTION AND RESOLUTION METHOD ACCOUNTING FOR UNCERTAINTIES OF TRAJECTORIES N. Yokoyama, National Defense Academy, Japan | |||
| 06. Sep 21 | 13:30 | 14:00 | 6.2.2 |
AN ALTERNATIVE BUT EQUIVALENT REALIZATION OF FINITE-HORIZON SUBOPTIMAL CONTROL FOR VEHICLE LANDING S. Zhang, China Aerodynamics Research and Development Center, China | |||
| 06. Sep 21 | 14:00 | 14:30 | 6.2.3 |
A NEW PITCH STABILITY ENHANCEMENT SCHEME FOR AEROSPACE VEHICLE Guangming: G. M. XIAO, China Aerodynamics Research & Development Center, China | |||
| Reserve Paper | 6.2.R |
SENSITIVITY MINIMIZATION ON A PARAMETER INTERVAL FOR ROBUST DIRECT OPTIMAL CONTROL T. Akman, Technical University of Munich, Germany | |||||
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| 06. Sep 21 | 13:00 | 13:30 | 7.2.1 |
TRANSPORT AIRCRAFT WING INVESTIGATIONS AIMED ON CROW INSTABILITY EXCITATION AND HIGH LIFT INCREASE BY OSCILLATING FLAPS J. Ruhland, Chair of Aerodynamics and Fluid Mechanics (TU Munich), Germany | |||
| 06. Sep 21 | 13:30 | 14:00 | 7.2.2 |
NUMERICAL INVESTIGATIONS OF HINGED STRAKES AERODYNAMICS AT HIGH ANGLES OF ATTACK Z. F. Xia, China Academy of Aerospace Aerodynamics, China | |||
| 06. Sep 21 | 14:00 | 14:30 | 7.2.3 |
AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATION Min ZHONG¹, Jun HUA¹, Xiasheng SUN¹, Sui ZHENG¹, Ganglin WANG¹, Guoxin ZHANG¹, Hao WANG¹, Yan LI¹, Xiaofei LI¹, Junqiang BAI, Northwestern Polytechnical University, China; ¹Chinese Aeronautical Establishment, China | |||
| Reserve Paper | 7.2.R |
NUMERICAL STUDY ON WING ROCK MECHANISM OF A LOW-ASPECT-RATIO RECTANGULAR WING AT LOW REYNOLDS NUMBER Y. Huang, Beihang University, China | |||||
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| 06. Sep 21 | 13:00 | 13:30 | 8.2.1 |
STATIC AEROELASTIC TAILORING OF A HIGH-ASPECT-RATIO-WING FOR A SAILPLANE WITH A MORPHING FORWARD WING SECTION F. Sturm, Technical University of Munich, Germany | |||
| 06. Sep 21 | 13:30 | 14:00 | 8.2.2 |
AEROSERVOELASTIC OPTIMIZATION OF A HIGH ASPECT TRANSPORT WING WITH MORPHING TRAILING EDGE Z. Zhang, Beihang University, China | |||
| 06. Sep 21 | 14:00 | 14:30 | 8.2.3 |
A COMPREHENSIVE FRAMEWORK FOR THE COUPLED NONLINEAR AEROELASTIC AND FLIGHT DYNAMIC ANALYSES OF HIGHLY FLEXIBLE AIRCRAFT Z.-C. Zhang, Northwestern Ploytechnical University, China | |||
| Reserve Paper | 8.2.R |
ON THE AEROELASTICITY OF THE ACTIVE SPAN EXTENSION AND PASSIVE PITCH POLYMORPHING WING Z Haider, Khalifa University of Science and Technology, United Arab Emirates | |||||
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| 06. Sep 21 | 13:00 | 13:30 | 9.2.1 |
THE USE OF SOFTWARE “VIRTUAL ENGINE” FOR TIMELY GAS-TURBINE ENGINE FAULT LOCALIZATIONS V. Vladimir, CIAM, Russia | |||
| 06. Sep 21 | 13:30 | 14:00 | 9.2.2 |
AN IMPROVED IDENTIFICATION METHOD FOR ACTUATOR LOOP OF AIRCRAFT ENGINE CONTROL SYSTEM Nan Liu, Shanghai Aircraft Design & Research Institute, Commercial Aircra, China | |||
| 06. Sep 21 | 14:00 | 14:30 | 9.2.3 |
METHODS OF PROGRAMMED THRUST MANAGEMENT FOR NOISE REDUCTION OF SUPERSONIC CIVIL AIRCRAFT A. Mirzoyan, CIAM, Russia | |||
| Reserve Paper | 9.2.R |
RESEARCH ON CIVIL AIRCRAFT POWERPLANT SYSTEM EICAS MESSAGES DESIGN METHOD S.-Y. Yang, COMAC, China | |||||
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| 06. Sep 21 | 13:00 | 13:30 | 10.2.1 |
EFFECTS OF ELASTICITY, VISCOSITY AND BOUNDARY LAYER TRANSITION ON AEROELASTICITY CHARACTERISTICS OF LAMINAR WINGS S.I. Kuzmina, TsAGI, Russia | |||
| 06. Sep 21 | 13:30 | 14:00 | 10.2.2 |
STUDY ON THE MULTIPLE EQUILIBRIUM POINTS OF TRANSONIC FLUTTER IN VISCOUS FLOW G. Wang, Northwestern Polytechnical University, China | |||
| 06. Sep 21 | 14:00 | 14:30 | 10.2.3 |
AEROELASTIC STRUCTURAL DESIGN OF A MID-RANGE COMPOSITE WING AIRCRAFT USING CPACS-MONA K. Sinha, German Aerospace Center, Germany | |||
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| 06. Sep 21 | 13:00 | 13:30 | 11.2.1 |
CASCADE CONTROL OF AVIATION VARIABLE FREQUENCY AC GENERATION SYSTEM BASED ON SLIDING MODE ACTIVE DISTURBANCE REJECTION R.-Z.-X. RUAN, Nanjing University Of Aeronautics And Astronautics, China | |||
| 06. Sep 21 | 13:30 | 14:00 | 11.2.2 |
DYNAMIC PERFORMANCE ANALYSIS AND ADAPTIVE FAULT DIAGNOSIS OF AIRCRAFT POWER SYSTEM H Li, Chengdu Aircraft Industrial (Group) Corporation, China | |||
| 06. Sep 21 | 14:00 | 14:30 | 11.2.3 |
DESIGN AND APPLICATION OF 18-PULSE AUTO-COUPLING TRANSFORMER RECTIFIER FOR AVIATION WX.-C. CHEN¹, TY.-S. SUN¹, LX.-J. JIANG¹; ¹AVIC, China | |||
| Reserve Paper | 11.2.R |
INTEGRATED ON-BOARD NETWORKS FOR NEXT GENERATION AVIONICS Valentin: V Olenev, St. Petersburg State University of Aerospace Instrumentation, Russia | |||||
| Reserve Paper | 11.2.R |
AN AGILE PRACTICE OF AVIONICS SYSTEM DEVELOPMENT Lei: L Dong, China Aeronautical Radio Electronics Research Institute, China | |||||
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| 06. Sep 21 | 13:00 | 13:30 | 12.2.1 |
CONDITION BASED MAINTENANCE (CBM) IN THE DIGITAL TRANSFORMATION STREAM VG Gros, AIRBUS SAS, France | |||
| 06. Sep 21 | 13:30 | 14:00 | 12.2.2 |
ANALYSIS OF THE ECONOMIC PERFORMANCE FOR AIRCRAFT MAINTENANCE USING DATA DRIVEN APPROACH X Zhao, China | |||
| 06. Sep 21 | 14:00 | 14:30 | 12.2.3 |
TOTAL LIFE CYCLE COST AND EMISSION OF ELECTRIC, HYBRID – ELECTRIC AIRCRAFT N. D. Dung, Budapest University of Tech. and econ.;, Hungary | |||
| Reserve Paper | 12.2.R |
A METHOD FOR EVALUATING THE APPLICABILITY OF MAINTENANCE TASKS BASED ON HELICOPTER HEALTH AND USAGE MONITORING SYSTEM DN-D Dong, AVIC China Aero-Polytechnology Establishment, China | |||||
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| 06. Sep 21 | 13:00 | 13:30 | 13.2.1 |
DETECTION AND ANALYSIS OF AIRCRAFT’S LOW ENERGY STATE DURING THE FINAL APPROACH PHASE Xiaolong Wang¹, Florian Holzapfel¹; ¹Technische Universität München, Germany | |||
| 06. Sep 21 | 13:30 | 14:00 | 13.2.2 |
TOWARDS AN ONLINE PREDICTIVE MODEL OF AIRCRAFT ENERGY STATE USING SUPERVISED MACHINE LEARNING O Pinon Fischer, Georgia Institute of Technology, United States | |||
| 06. Sep 21 | 14:00 | 14:30 | 13.2.3 |
AN OVERVIEW OF FLARE TECHNIQUES AND FLARE TRAINING METHODS J.O. Entzinger, The University of Tokyo, Japan | |||
| Reserve Paper | 13.2.R |
MACHINE LEARNING BASED PREDICTION OF VEER-OFFS DURING LANDING PHASE S. Lagunas-Caballero, Airbus Defence and Space, Spain | |||||
| 14:30 - 15:00 | Break | |||
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| 06. Sep 21 | 15:00 | 15:30 | 1.3.1 |
ATTENUATION OF NOISE IN THE CABIN OF A REGIONAL AIRCRAFT BY METAMATERIAL TRIM PANELS M. Cinefra, Politecnico di Torino, Italy | |||
| 06. Sep 21 | 15:30 | 16:00 | 1.3.2 |
ACOUSTIC FLIGHT LAB – A UNIQUE INTEGRATION PLATFORM FOR OPTIMIZING OF VIBRO-ACOUSTIC PERFORMANCE OF AIRCRAFT M. Wandel, Airbus Operations GmbH, Germany | |||
| 06. Sep 21 | 16:00 | 16:30 | 1.3.3 |
DEVELOPMENT OF A GESTURE-BASED INTERFACE FOR FLIGHT CONTROLS: RESULTS OF INITIAL EXPERIMENTS WITH THE SYSTEM M.A. Rodriguez Diaz, Instituto Tecnologico de Aeronáutica, Brazil | |||
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| 06. Sep 21 | 15:00 | 15:30 | 3.3.1 |
FORMALIZED KNOWLEDGE MANAGEMENT FOR THE AIRCRAFT CABIN DESIGN PROCESS M. Fuchs¹, C. Hesse¹; ¹DLR, Germany | |||
| 06. Sep 21 | 15:30 | 16:00 | 3.3.2 |
A MODULAR KNOWLEDGE-BASED-ENGINEERING APPLICATION SUPPORTING THE PREDESIGN OF NOVEL AIRCRAFT CONFIGURATIONS A. Zamfir, German Aerospace Center (DLR), Germany | |||
| 06. Sep 21 | 16:00 | 16:30 | 3.3.3 |
IMPROVING CONCEPTUAL DESIGN SPACE EXPLORATION CAPABILITIES USING AN ADVANCED KNOWLEDGE-BASED-ENGINEERING TOOL J. Zamboni, German Aerospace Center (DLR), Germany | |||
| Reserve Paper | 3.3.R |
APPLICATION OF KNOWLEDGE ENGINEERING IN SPACECRAFT OVERALL DESIGN Zhao Zhao, Harbin Institute Technology, China | |||||
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| 06. Sep 21 | 15:00 | 15:30 | 4.3.1 |
LONGITUDINAL VORTEX FORMATION IN HYPERSONIC BOUNDARY LAYER ON BLUNTED DELTA WING AND ITS EFFECT ON FLOW CHARACTERISTICS V.I. Shalaev, Moscow Institute of Physics and Technology, Russia | |||
| 06. Sep 21 | 15:30 | 16:00 | 4.3.2 |
LONGITUDINAL AND LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE HIGH-SPEED VEHICLE G. Pezzella, University of Campania, Italy | |||
| 06. Sep 21 | 16:00 | 16:30 | 4.3.3 |
MULTI-SCALE CFD/MD MODELLING OF HIGH-ENTHALPY FLOW/TPS INTERACTION AND ITS PRELIMINARY AERONAUTICAL APPLICATION X. Yang, China Aerodynamics Research and Development Center, China | |||
| Reserve Paper | 4.3.R |
RESEARCH OF HYPERSONIC BOUNDARY LAYER INSTABILITY AND TRANSITION WITH THERMAL-CHEMICAL NON-EQUILIBRIUM EFFECTS X.-L. Chen, Tsinghua University, China | |||||
| Reserve Paper | 4.3.R |
INVESTIGATION OF A HYPERSONIC VERTICAL GAP FLOW H. Zhang, China | |||||
| Reserve Paper | 4.3.R |
COUPLED HEAT TRANSFER CHARACTERISTICS ON CHEMICALLY REACTING INTERFACE OF HIGH-SPEED AIRCRAFT CONSIDERING WALL INJECTION Q. -Y. You, State Key Laboratory of Aerodynamics, China | |||||
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| 06. Sep 21 | 15:00 | 15:30 | 5.3.1 |
EXPERIMENTAL AND NUMERICAL AERODYNAMIC LOAD RESULTS ACTIONG ON THE M5/ONERA/IAE AERONAUTICAL STANDARD MODEL M. S. Souza, IAE, Brazil | |||
| 06. Sep 21 | 15:30 | 16:00 | 5.3.2 |
OPTIMIZATION OF AN ACTIVE DAMPING SYSTEM FOR USE WITH A SINGLE STRUT MOUNT J.L. Pereira, National Research Council Canada, Canada | |||
| 06. Sep 21 | 16:00 | 16:30 | 5.3.3 |
STUDY ON AERODYNAMIC CHARACTERISTICS OF LIGHT CONVERTIBLE AIRCRAFT MODEL E.A. Pigusov, Central Aerohydrodinamic Institute, Russia | |||
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| 06. Sep 21 | 15:00 | 15:30 | 6.3.1 |
ADJUSTED SHAPES OF ADHESIVELY BONDED REPAIR PATCHES FOR THE EARLY INDICATION OF DEBOND IN FIGHTER AIRCRAFT STRUCTURES J Jokinen, Tampere University, Finland | |||
| 06. Sep 21 | 15:30 | 16:00 | 6.3.2 |
THE INFLUENCE OF THE NUMBER OF ADHESIVE PLIES (FM-300-2K) ON FRACTURE PROPERTIES J Jokinen, Tampere University, Finland | |||
| 06. Sep 21 | 16:00 | 16:30 | 6.3.3 |
STATISTICS AND ANALYSIS OF MANUFACTURE DEFECTS AND DAMAGE OF HELICOPTER COMPOSITE STRUCTURES Jun Li, China | |||
| Reserve Paper | 6.3.R |
DEVELOPMENT OF METHOD FOR DETERMINING THE SHEAR FRACTURE TOUGHNESS ON SPECIMENS WITHOUT A DELAMINATION INITIATOR MADE OF V. Tokar, TsAGI, Russia | |||||
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| 06. Sep 21 | 15:00 | 15:30 | 7.3.1 |
NUMERICAL VIRTUAL FLIGHT SIMULATION OF QUASI-COBRA MANEUVER OF A FIGHTER AIRCRAFT None Wang, China Aerodynamics Research and Development Center, China | |||
| 06. Sep 21 | 15:30 | 16:00 | 7.3.2 |
NUMERICAL SIMULATION OF AIRFOIL SPANWISE-RIDGE ICE FORMATION BASED ON HOT AIR ANTI-ICING SYSTEM J.-T Wang, Northwestern Polytechnical University, China | |||
| 06. Sep 21 | 16:00 | 16:30 | 7.3.3 |
VERIFICATION AND VALIDATION OF SONIC BOOM SIMULATION CAPABILITIES G. CARRIER, ONERA, France | |||
| Reserve Paper | 7.3.R |
RESEARCH ON UNSTEADY AERODYNAMIC MODELS AT HIGH ANGLE OF ATTACK BASED ON NONLINEAR REGRESSION J.A C Cheng, Northwestern Polytechnical University, China | |||||
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| 06. Sep 21 | 15:00 | 15:30 | 8.3.1 |
MULTI-AXIS MANEUVER SIMULATION FOR SYSTEM IDENTIFICATION OF FLEXIBLE TRANSPORT AIRCRAFT BY HIGH-FIDELITY METHODS M Ritter, German Aerospace Center (DLR), Germany | |||
| 06. Sep 21 | 15:30 | 16:00 | 8.3.2 |
STRUCTURAL DESIGN OF MILITARY AIRCRAFT VERTICAL TAIL INCLUDING DYNAMIC LOADS FROM WING AND AIRBRAKE SEPARATED FLOW W.G. LUBER, wgl-dynamics Consulting, Germany | |||
| 06. Sep 21 | 16:00 | 16:30 | 8.3.3 |
RECEPTANCE-BASED UNCERTAINTY QUANTIFICATION AND MINIMIZATION IN AEROSERVOELASTIC SYSTEMS L. J. Adamson, University of Liverpool, United Kingdom | |||
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| 06. Sep 21 | 15:00 | 15:30 | 9.3.1 |
THE POTENTIAL OF CASING TREATMENTS FOR TRANSONIC COMPRESSORS: EVALUATION BASED ON AXIAL-SLOT AND ROTOR BLADE OPTIMISATIO G. Goinis¹, C. Voß¹, E. Nicke¹; ¹German Aerospace Center (DLR), Germany | |||
| 06. Sep 21 | 15:30 | 16:00 | 9.3.2 |
CONJUGATE HEAT TRANSFER MODELLING OF A TURBINE VANE ENDWALL WITH THERMAL BARRIER COATINGS Z. Fen, China | |||
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| 06. Sep 21 | 15:00 | 15:30 | 10.3.1 |
STRUCTURAL VIBRATION CONTROL BY USING THE ENERGY FROM DIFFERENT MODE K.L LI, Aircraft strength research institute, China | |||
| 06. Sep 21 | 15:30 | 16:00 | 10.3.2 |
VERIFICATION AND VALIDATION IN AN UNCERTAIN ENVIRONMENT i Isnardi, University of Liverpool, United Kingdom | |||
| 06. Sep 21 | 16:00 | 16:30 | 10.3.3 |
MODAL DAMPING IDENTIFICATION METHOD BASED ON VARIATIONAL MODE DECOMPOSITION AND ENVELOPE FITTING AND ITS APPLICATIONS J. BIAN, AECC Hunan Aviation Powerplant Research Institute, China | |||
| Reserve Paper | 10.3.R |
A PERTURBATION ANALYSIS OF NONLINEARITY IN LANDING-GEAR SHIMMY OF A FLEET AIRCRAFT M.-L Kou, AECC CAE, China | |||||
| Reserve Paper | 10.3.R |
ANALYSIS OF WHIRL VIBRATION IN AN AIRCRAFT BRAKE SYSTEM DURING BRAKING D.Y.H Han, China | |||||
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| 06. Sep 21 | 15:00 | 15:30 | 11.3.1 |
RESEARCH ON OPTIMIZATION TECHNOLOGY FOR CONTROL PARAMETERS OF EJECTION SEAT BASED ON PSO ALGORITHM J-L Lou, Aerospace Life-support Industries,LTD., China | |||
| 06. Sep 21 | 15:30 | 16:00 | 11.3.2 |
MANOEUVRABLE AERIAL TARGET TRACKING IN THE PRESENCE OF STAND-OFF JAMMING C. Tian, School of Aeronautics, Northwestern Polytechnical University, China | |||
| 06. Sep 21 | 16:00 | 16:30 | 11.3.3 |
RESEARCH ON THE PRESSURE COMFORT OF PILOT’S HELMET X. Wang, AVIC Aerospace Life Support Industries LTD, China | |||
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| 06. Sep 21 | 15:00 | 15:30 | 12.3.1 |
MODELING THE CLIMATE IMPACT OF FORMATION FLIGHT T. Marks, German Aerospace Center (DLR), Germany | |||
| 06. Sep 21 | 15:30 | 16:00 | 12.3.2 |
A MULTI-CRITERIA SEQUENCING LOGIC FOR THE EXTENDED TERMINAL MANOEUVRING AREA CONSIDERING INTERDEPENDENT UNCERTAINTIES T. Zeh, Technische Universität Dresden, Germany | |||
| 06. Sep 21 | 16:00 | 16:30 | 12.3.3 |
ON THE AIRCRAFT OPERATIONAL INTEGRITY Yuting He He, Air Force Engineering University, China | |||
| Reserve Paper | 12.3.R |
INTEGRATION OF SPACE VEHICLE OPERATIONS INTO THE UNITED ARAB EMIRATES AIR TRAFFIC MANAGEMENT – AN IMPACT ANALYSIS O. Lehmann, Abu Dhabi University, United Arab Emirates | |||||
| Reserve Paper | 12.3.R |
ENHANCED UNDERSTANDING OF INTERMODAL PASSENGER BEHAVIOR THROUGH BIG DATA ANALYSIS AND FUSION TECHNIQUES J. B. P. Blasco Puyuelo, Nommon Solutions & Technologies, Spain | |||||
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| 06. Sep 21 | 15:00 | 15:30 | 13.3.1 |
ACTIVITY CHARACTERISTICS AND THE MECHANISM OF MESO-MICRO SCALE DISTURBANCES IN THE EAST ASIAN SUBTROPICAL UPPER-LEVEL JE X Chen¹, J Huang¹, M Meng, Wenzhou Meteorological Burea, China; C Chen¹, Q Chen¹; ¹China Aerodynamics Research and Development Center, China | |||
| 06. Sep 21 | 15:30 | 16:00 | 13.3.2 |
A METHODOLOGY FOR CHARACTERISING LOSS OF CONTROL IN FLIGHT ACCIDENTS J.P. Macedo, Univeristy of Sao Paulo, Brazil | |||
| 06. Sep 21 | 16:00 | 16:30 | 13.3.3 |
MAIN OUTCOMES FROM H2020 VISION PROJECT: EU-JAPAN COLLABORATIVE RESEARCH IN INTELLIGENT FLIGHT CONTROL STSTEMS Y. Watanabe, ONERA, France | |||
| Reserve Paper | 13.3.R |
ANALYSIS OF RISK FACTORS AND IDENTIFICATION OF PRECURSORS OF RUNWAY EXCURSIONS AT LANDING Nail: N. Khairullin, Central Aerohydrodynamic Institute (TsAGI), Russia | |||||
| Reserve Paper | 13.3.R |
RESEARCH ON FAULT DETECTION AND FAULT RECONFIGURATION OF FLUSH AIR DATA SENSING Q.-J Jia, Northwestern Polytechnical University, China | |||||
| Reserve Paper | 13.3.R |
CONCEPT OF A NEW SYSTEM SYNTHESIZING METEOROLOGICAL AND OROGRAPHIC INFLUENCES ON THE AIRPLANE SAFE ENERGY ENVELOPE X. Liu¹, L. Manfriani¹, Y. Fu, Lab. of Aerosp. Servo Actuation and Transmission, Beihang Univ., China; ¹Centre for Aviation, Zurich University of Applied Sciences, Switzerland | |||||
| 0.2 | General Lecture 1 - CTO Chair: J. Azevedo ICAS PC Chair | |||
| 06. Sep 21 | 16:35 | 18:35 |
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Tuesday, 07. Sep 2021
7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
| 0.3 | General Lecture 2 - Future needs you – the panel discussion of the skills for aeronautics Chair: M. Kanerva ECSC Chair | |||
| 07. Sep 21 | 08:00 | 09:00 |
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| 0.4 | Interactive Presentations Chair: | |||
| 07. Sep 21 | 09:00 | 10:00 |
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| 07. Sep 21 | 10:00 | 10:30 | 1.4.1 |
A HIERARCHICAL STRUCTURAL MODEL FOR CONCEPTUAL DESIGN OF TRANSPORT AIRCRAFT WING Y.K. Yin¹, W.B. Song¹; ¹Shanghai Jiao Tong University, China | |||
| 07. Sep 21 | 10:30 | 11:00 | 1.4.2 |
VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WING W.Y.CHENG CHENG, Aviation Industry Development Research Center of China (ADR), China | |||
| 07. Sep 21 | 11:00 | 11:30 | 1.4.3 |
EVALUATION AND VALIDATION OF AEROELASTIC ANALYSIS PROGRAM FOR AEROSTRUCT WING OPTIMIZATION PLATFORM S.B. Ling, Northwestern Polytechnical University, China | |||
| 07. Sep 21 | 11:30 | 12:00 | 1.4.4 |
ON WINGS WITH NON-ELLIPTIC LIFT DISTRIBUTIONS E. Bragado Aldana¹, M. M. Lone¹; ¹Cranfield University, United Kingdom | |||
| Reserve Paper | 1.4.R |
ON THE FLIGHT MECHANICS OF A TRANSPORT AIRCRAFT FITTED WITH FLARED-HINGE FOLDING WINGTIPS R Ajaj, Khalifa University, United Arab Emirates | |||||
| Reserve Paper | 1.4.R |
UNCERTAINTY ANALYSIS OF HYBRID LAMINAR FLOW CONTROL WINGS FOR WING-GLOVE FLIGHT TESTS T.Y. Yang, Northwestern Polytechnical University, China | |||||
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| 07. Sep 21 | 10:00 | 10:30 | 2.4.1 |
FLEET LEVEL DIRECT OPERATING COST ASSESSMENT OF ADVANCED ALL NEW MID-RANGE TRANSPORT AIRCRAFT J. Hartmann, DLR, Germany | |||
| 07. Sep 21 | 10:30 | 11:00 | 2.4.2 |
STATISTICAL APPROACH TO INDIRECT COST ASSESSMENT FOR AN AIRCRAFT FLEET G.-F. Ferrari, Politecnico di Torino, Italy | |||
| 07. Sep 21 | 11:00 | 11:30 | 2.4.3 |
DEVELOPMENT OF A PARAMETRIC COST MODEL ASSESSING THE IMPACT OF NEW TECHNOLOGIES ON A REGIONAL AIRCRAFT M. Fioriti, Politecnico di Torino, Italy | |||
| 07. Sep 21 | 11:30 | 12:00 | 2.4.4 |
LIFECYCLE COST-BENEFIT ASSESSMENT OF SELECTED TECHNOLOGIES CONSIDERING UNCERTAINTIES A.A. Pohya, DLR, Germany | |||
| Reserve Paper | 2.4.R |
BASED ON THE CHARACTERISTIC PARAMETERS ESTIMATE MANUFACTURING COST FOR COMPOSITE STRUCTURES H.-F. Feng, China | |||||
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| 07. Sep 21 | 10:00 | 10:30 | 4.4.1 |
FLOW CONTROL AT HIGH LIFT MISSION OF A CIVIL AIRCRAFTBY AN OPTIMUM MORPHING LEADING-EDGE DESIGN alireza jahangirian, aerospace engineering departmen, Iran | |||
| 07. Sep 21 | 10:30 | 11:00 | 4.4.2 |
OPTIMISATION OF VORTEX GENERATORS FOR STALL SPEED REDUCTION Jannek Meyer¹, Patrick Marcello Okfen¹, Cees Bil¹; ¹RMIT University, Australia | |||
| 07. Sep 21 | 11:00 | 11:30 | 4.4.3 |
AERODYNAMIC DESIGN OOPTIMIZATION OF A CIVIL AIRCRAFT WINGLET USING MULTI-OBJECTIVE EVOLUTIONARY ALGORITHM AND CFD SOLVER alireza jahangirian, aerospace engineering departmen, Iran | |||
| 07. Sep 21 | 11:30 | 12:00 | 4.4.4 |
DESIGN AND OPTIMIZATION OF A HIGH-ALTITUDE LONG ENDURANCE UAV PROPELLER K. Y. You, Northwestern Polytechnical University, China | |||
| Reserve Paper | 4.4.R |
OPTIMAL DESIGN OF A NEXT GENERATION HIGH-LIFT REUSABLE RE-ENTRY VEHICLE G. Pezzella, University of Campania, Italy | |||||
| Reserve Paper | 4.4.R |
MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF A CIVIL AIRCRAFT FUSELAGE alireza jahangirian, aerospace engineering departmen, Iran | |||||
| Reserve Paper | 4.4.R |
CFD SIMULATION OF A NEW REVERSE-HINGED SPOILER FOR LIFT/DRAG CONTROL K. Djidjeli, University of Southampton, United Kingdom | |||||
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| 07. Sep 21 | 10:00 | 10:30 | 5.4.1 |
AN OBJECTIVE APPROACH FOR MEASURING INTERMITTENCY IN THE TRANSITIONAL BOUNDARY LAYERS D Veerasamy, City, University of London, United Kingdom | |||
| 07. Sep 21 | 10:30 | 11:00 | 5.4.2 |
DYNAMIC TRAILING-EDGE FLAP MOVEMENT AS A NON-CONVENTIONAL LIFTING MECHANISM M. Bremm, RWTH Aachen University, Germany | |||
| 07. Sep 21 | 11:00 | 11:30 | 5.4.3 |
COMPUTATIONAL FLUID DYNAMIC STUDY ON LOW SPEED WIND TUNNEL DATA CORRECTIONS W. S. Stryczniewicz, Lukasiewicz Research Network - Institute of Aviation, Poland | |||
| 07. Sep 21 | 11:30 | 12:00 | 5.4.4 |
SKIN-FRICTION TOPOLOGY ON AXISYMMETRIC BOATTAIL MODELS BY AN OPTICAL-FLOW ALGORITHM WITH SUBGRID FUNCTION T. H. Tran, Le Quy Don Technical University, Vietnam | |||
| Reserve Paper | 5.4.R |
APPLIED RESEARCH ON SUPERVISED LEARNING IN THE JUDGMENT OF AIRFOIL TRANSITION W.-B.B. Wei, China | |||||
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| 07. Sep 21 | 10:00 | 10:30 | 6.4.1 |
EXPERIMENTAL INVESTIGATION, NUMERICAL AND MATHEMATICAL SIMULATION OF DISPERSE FLOWS IMPINGING ON AIRCRAFT SURFACE Ivan Alexeevich: Amelyushkin, TsAGI, Russia | |||
| 07. Sep 21 | 10:30 | 11:00 | 6.4.2 |
MODIFICATION OF TURBULENCE MODELS FOR PRESSURE-INDUCED SEPARATION ON SMOOTH SURFACES USING THE DLR VICTORIA EXPERIMENT A. M. Krumbein, DLR - German Aerospace Center, Germany | |||
| 07. Sep 21 | 11:00 | 11:30 | 6.4.3 |
A NETWORK-CENTROID BASED REDUCED-ORDER MODEL FOR A MIXING LAYER H. Li, National University of Defense Technology, China | |||
| 07. Sep 21 | 11:30 | 12:00 | 6.4.4 |
SINGULARITIES IN THE NEAR-WALL REGION OF 3D BOUNDARY LAYER AND ASYMPTOTIC FLOW STRUCTURE IN ITS VICINITY V.I. Shalaev, Moscow Institute of Physics and Technology, Russia | |||
| Reserve Paper | 6.4.R |
LOW ORDER MODELLING OF UNSTEADY AERODYNAMIC LIFT FORCES ON 2D FLAT-PLATE DURING SINUSOIDAL PITCHING R. Zeng, Beihang University, China | |||||
| Reserve Paper | 6.4.R |
EVOLUTION OF WAVEPACKETS ON THE WINDWARD SIDE OF AN INCLINED HYPERSONIC STRAIGHT CONE UNDER FLIGHT CONDITION P.-Y. Yang, China Aerodynamics Research And Debelopment Center, China | |||||
| Reserve Paper | 6.4.R |
STUDY ON THE STATISTICAL CHARACTERISTICS OF SKIN FRICTION OF SHOCK WAVE TURBULENT BOUNDARY LAYER AT MACH 6 Peng-fei:P.-F Shen, State Key Laboratory of Aerodynamics, China | |||||
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| 07. Sep 21 | 10:00 | 10:30 | 7.4.1 |
PROPELLER WAKE - OBJECT INTERACTION USING A FREE WAKE MODEL UTILIZING LOCAL MESH REFINEMENT M. Thiele, Technical University of Munich - Institute of Aircraft Design, Germany | |||
| 07. Sep 21 | 10:30 | 11:00 | 7.4.2 |
AERODYNAMIC INVESTIGATION OF ROTOR-ROTOR INTERACTION FOR DISTRIBUTED-PROPELLER SYSTEMS R. de Vries, Delft University of Technology, Netherlands | |||
| 07. Sep 21 | 11:00 | 11:30 | 7.4.3 |
NUMERICAL STUDY OF QUAD-ROTOR AIRCRAFT PERFORMANCE UNDER SEVERE WEATHER T. Wan, Tamkang University, Taiwan, China | |||
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| 07. Sep 21 | 10:00 | 10:30 | 8.4.1 |
LIGHTWEIGHT DESIGN OF THERMAL PROTECTION STRUCTURES WITH EFFECTS OF MESO-PROPERTIES OF MATERIALS S.-H.-A. You An, Computational Aerodynamic Institute(CAI), CARDC, China | |||
| 07. Sep 21 | 10:30 | 11:00 | 8.4.2 |
ACCURATE MODELS FOR THE PREDICTION OF FREE-EDGE STRESSES OF COMPOSITE STRUCTURES UNDER THERMAL LOADS E. Zappino, Italy | |||
| 07. Sep 21 | 11:00 | 11:30 | 8.4.3 |
TEMPERATURE-INDUCED LOAD OF BOLTED HYBRID COMPOSITE/METAL JOINT L.-K KAI, AVIC Aircraft Strength Research Institute, China | |||
| 07. Sep 21 | 11:30 | 12:00 | 8.4.4 |
DEVELOPMENT OF LIGHTWEIGHT HYBRID AIRFRAMES BASED ON UNIDIRECTIONAL COMPOSITE STRUCTURE CONCEPTS A. Shanygin, Central Aerohydrodynamic Institute (TsAGI), Russia | |||
| Reserve Paper | 8.4.R |
SEARCH OF RATIONAL LEVEL OF WING-FUSELAGE INTEGRATION TO INCREASE WEIGHT EFFICIENCY OF AIRCRAFT COMPOSITE STRUCTURES I. Kondakov, Central Aerohydrodynamic Institute (TsAGI), Russia | |||||
| Reserve Paper | 8.4.R |
STRUCTURAL INDICES-BASED OPTIMIZATION METHODOLOGY FOR LIGHT AIRCRAFT COMPOSITE WINGS M Nuño, RWTH Aachen University, Germany | |||||
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| 07. Sep 21 | 10:00 | 10:30 | 9.4.1 |
KNOWLEDGE-BASED CONCEPTUAL DESIGN METHODS FOR GEOMETRY AND WEIGHT ESTIMATION OF RUBBER AERO ENGINES J. Häßy, German Aerospace Center (DLR), Germany | |||
| 07. Sep 21 | 10:30 | 11:00 | 9.4.2 |
RESEARCH OF PROPULSION-SYSTEM-SURROGATE-MODELING METHOD USING INFILL CRITERION SAMPLES DC.W Wang, School of Aeronautics, Northwestern Polytechnical University, China | |||
| 07. Sep 21 | 11:00 | 11:30 | 9.4.3 |
ELABORATION OF DISTRIBUTED MDAO SYSTEM FOR CONCEPTUAL DESIGN OF SCA PROPULSION SYSTEM IN INTEGRATED DEVELOPMENT ENVIRONM L.A. Mirzoyan, CIAM, Russia | |||
| 07. Sep 21 | 11:30 | 12:00 | 9.4.4 |
AERODYNAMIC PROPULSION SYSTEM OPTIMIZATION: TOWARDS TO AGILE 4.0 K.S. Anisimov, Federal State Unitary Enterprise Central Aerohydrodynamic Instit, Russia | |||
| Reserve Paper | 9.4.R |
PARAMETRIC MODELLING TO SUPPORT PRELIMINARY DESIGN OF PROPULSION SYSTEMS FOR RE-USABLE ACCESS TO SPACE D. Ferretto, Politecnico di Torino, Italy | |||||
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| 07. Sep 21 | 10:00 | 10:30 | 10.4.1 |
VIRTUAL TESTING OF A MULTIFUNCTIONAL POWER CONTROL UNIT FOR HYDRAULIC SUPPLY AND HIGH LIFT ACTUATION L. Nordmann, Germany | |||
| 07. Sep 21 | 10:30 | 11:00 | 10.4.2 |
RESEARCH AND VALIDATION OF SYSTEM MODELING AND SIMULATION OF INTAKE AIR MIXER ALTITUDE TEST BED Feng-Wu: F. -W. Wu, AECC Sichuan Gas Turbine Establishment, China | |||
| 07. Sep 21 | 11:00 | 11:30 | 10.4.3 |
DESIGN AND DEVELOPMENT OF A MODULAR IRON BIRD TO TEST MOVABLE SURFACE ACTUATORS OF GENERAL AVIATION AIRCRAFT AND UAVS M. Mattei, Università della Campania "Luigi Vanvitelli", Italy | |||
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| 07. Sep 21 | 10:00 | 10:30 | 11.4.1 |
RESEARCH ON DYNAMIC MODELING AND TRANSITION FLIGHT STRATEGY OF INDUCED-LIFT VTOL UAV C.W Wang, Northwestern Polytechniacl University, China | |||
| 07. Sep 21 | 10:30 | 11:00 | 11.4.2 |
COMPARATIVE ANALYSIS OF METHODS USED TO ACTIVE CONTROL OF MICRO AERIAL VEHICLE K.-S. Sibilski, Warsaw University of Technology, Poland | |||
| 07. Sep 21 | 11:00 | 11:30 | 11.4.3 |
PERCHING PRINCIPLES ANALYSIS OF POST-STALL PERCHING UNMANNED AERIAL VEHICLE S.-Y Yang, NWPU, China | |||
| 07. Sep 21 | 11:30 | 12:00 | 11.4.4 |
DEVELOPMENT TOWARDS A TOOLCHAIN FOR ESTIMATING UAV FLIGHT DYNAMIC MODELS IN EARLY DESIGN S. Koeberle, Institute of Aircraft Design/Technical University of Munich, Germany | |||
| Reserve Paper | 11.4.R |
STUDY OF SMALL UAVS DISTURBED MOTION NATURAL FREQUENCIES USING EXTENDED EXPERIMENTAL DATASETS M. E. El-Salamony, Peking University, China | |||||
| Reserve Paper | 11.4.R |
AERODYNAMICS CHARACTERISTICS AND FLIGHT DYNAMICS ANALYSIS OF MULTI-BODY AIRCRAFT C. An, Beihang University, China | |||||
| Reserve Paper | 11.4.R |
OPTIMIZATION OF LONGITUDINAL CONTROL OF AN AGRICULTURAL UAV USING LQR-PID CONTROL A.G.P. Sarmento, Technological Institute of Aeronautics, Brazil | |||||
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| 07. Sep 21 | 10:00 | 10:30 | 12.4.1 |
A DEEP-LEARNING-BASED METHOD FOR DAMAGE IDENTIFICATION OF COMPOSITE LAMINATES Y Yu¹, W Binwen¹, L Shuaishuai¹, Z Yuxi, Peking University, China; W Li¹, L Guoqiang¹; ¹Aircraft Strength Research Institute of ChinaAffiliation, China | |||
| 07. Sep 21 | 10:30 | 11:00 | 12.4.2 |
IN-SITU LASER ASSISTED DIRECT IMPREGNATION, LAMINATION AND PLACEMENT OF CFRTP T. Ikeda, Chubu University, Japan | |||
| 07. Sep 21 | 11:00 | 11:30 | 12.4.3 |
MOISTURE ABSORPTION BEHAVIOR OF COMPOSITE STIFFENED PANELS IN HYGROTHERMAL ENVIRONMENT B-L Ma, China | |||
| 07. Sep 21 | 11:30 | 12:00 | 12.4.4 |
A TWO PHASES COUPLING FREE AND POROUS FLOW NUMERICAL SIMULATION METHOD OF LCM PROCESS C. Li, BASTRI of COMAC, China | |||
| Reserve Paper | 12.4.R |
RESEARCH OF THE MECHANICAL PROPERTIES OF CFRP OF THE HIGH THICKNESS A.A. Sviridov, The Central Aerohydrodynamic Institute, Russia | |||||
| Reserve Paper | 12.4.R |
DESIGN FOR MANUFACTURING APPROACH AND LOW COST METAL STRUCTURE LP PINTO, AIRBUS, France | |||||
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| 07. Sep 21 | 10:00 | 10:30 | 13.4.1 |
ATTENTION: TARGET AND ACTUAL – THE CONTROLLER FOCUS J. Rataj, DLR, Germany | |||
| 07. Sep 21 | 10:30 | 11:00 | 13.4.2 |
ANALYSIS OF PILOT OPERATIONAL STRATEGY DIFFERENCE USING NEURAL NETWORK R. Mori, Electronic Navigation Research Institute, Japan | |||
| 07. Sep 21 | 11:00 | 11:30 | 13.4.3 |
WORKLOAD EVALUATION USING OBJECTIVE AND SUBJECTIVE DATA MEASURED DURING SIMULATED FLIGHT C. Orlando, Kore University of Enna, Italy | |||
| 07. Sep 21 | 11:30 | 12:00 | 13.4.4 |
ENSURING HIGH NAVIGATION INTEGRITY FOR URBAN AIR MOBILITY USING TIGHTLY COUPLED GNSS/INS SYSTEM S.-Z Wang, Shanghai Jiao Tong University, China | |||
| Reserve Paper | 13.4.R |
OBJECTIVE MEASUREMENT OF HUMAN FACTORS FOR SUPPORTING THE OPERATOR’S LOAD SIMULATION AND MANAGEMENT U. Kale, Budapest University of Tech. and econ.;, Hungary | |||||
| Reserve Paper | 13.4.R |
MACHINE LEARNING ENABLED TURBULENCE PREDICTION USING FLIGHT DATA FOR SAFETY ANALYSIS T Puranik, Georgia Institute of Technology, United States | |||||
| 12:00 - 13:00 | Lunch | |||
| 0.5 | ICAS Lecture for Innovation in Aeronautics - Electrification - The third revolution in aviation, Cory Combs, USA Chair: | |||
| 07. Sep 21 | 13:00 | 13:45 |
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| 07. Sep 21 | 14:00 | 14:30 | 1.5.1 |
CONCURRENT OPTIMIZATION OF AIRFRAME AND ENERGY STORAGE AND CONVERSION SYSTEMS FOR HYBRID ELECTRIC PROPULSION AIRCRAFT A. Elham, TU Braunschweig, Germany | |||
| 07. Sep 21 | 14:30 | 15:00 | 1.5.2 |
PRELIMINARY DESIGN AND EXPERIMENTAL INVESTIGATION OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT Y.-M. Ma, Northwestern Polytechnical University, China | |||
| 07. Sep 21 | 15:00 | 15:30 | 1.5.3 |
UNMANNED FIRE-FIGHTING AMPHIBIOUS AIRCRAFT WITH DISTRIBUTED TURBOELECTRIC PROPULSION SYSTEM A.N. Varyukhin, CENTRAL INSTITUTE OF AVIATION MOTORS (CIAM), Russia | |||
| Reserve Paper | 1.5.R |
MULTIFIDELITY OPTIMISATION OF A BLENDED WING BODY MARTIAN GLIDER D. Verstraete, The University of Sydney, Australia | |||||
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| 07. Sep 21 | 14:00 | 14:30 | 2.5.1 |
MULTI-FIDELITY AND MULTI-POINT SIMULTANEOUS SHAPE AND SIZING OPTIMISATION FOR MAXIMUM AIRCRAFT PERFORMANCE A. Gastaldi, Airbus Defence and Space, Germany | |||
| 07. Sep 21 | 14:30 | 15:00 | 2.5.2 |
BWB CONFIGURATION’S AERODYNAMIC OPTIMIZATION DESIGN AND SHAPE PARAMETERIZATION BASED ON GRADIENT METHOD W.zy Wang, The First Aircraft Institute, China | |||
| 07. Sep 21 | 15:00 | 15:30 | 2.5.3 |
MULTIFIDELITY AERODYNAMIC/STEALTH SHAPE DESIGN OPTIMIZATION METHOD FOR FLYING WING AIRCRAFT Z.-Q. Liu, School of Aeronautics, Northwestern Polytechnical University, China | |||
| Reserve Paper | 2.5.R |
A GRADIENT-BASED AERO-STEALTH OPTIMIZATION DESIGN METHOD FOR THE LONG-ENDURANCE UAV SHAPE DESIGN L.-M. Ming, Northwestern Polytechnical University, China | |||||
| Reserve Paper | 2.5.R |
AN INTEGRATED OPTIMIZATION METHOD OF WING-TIP AERODYNAMIC/STEALTH BASED ON SURROGATE MODEL RC Wang, Institute of Engineering Thermophysics, Chinese Academy of Scien, China | |||||
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| 07. Sep 21 | 14:00 | 14:30 | 3.5.1 |
ARCHITECTURE INTEGRATION OF FUTURE ATM SYSTEM BASED ON META MODEL JY Wang, China Aeronautical Radio Electronics Research Institute, China | |||
| 07. Sep 21 | 14:30 | 15:00 | 3.5.2 |
TECHNOLOGY ROADMAPS FOR THE DEVELOPMENT OF FUTURE HIGH-SPEED TRANSPORTATION SYSTEMS N. Viola, Politecnico di Torino, Italy | |||
| 07. Sep 21 | 15:00 | 15:30 | 3.5.3 |
ARCHITECTURE OF PRODUCT RESEARCH AND DEVELOPMENT SYSTEM L. Su, Aero-Engine Academy of China, China | |||
| Reserve Paper | 3.5.R |
GREENER ATM SYSTEM ARCHITECTURE RESEARCH BASED ON COMPLEX SYSTEM ENGINEERING METHOD H. Hu, China Aeronautical Radio Electronics Research Institute, China | |||||
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| 07. Sep 21 | 14:00 | 14:30 | 4.5.1 |
NUMERICAL STUDY ON THE STALL CHARACTERISTICS AND SEPARATED FLOW AROUND ICED AIRFOILS USING LATTICE BOLTZMANN METHOD H.Y.G Gu, Northwestern Polytechnical University, China | |||
| 07. Sep 21 | 14:30 | 15:00 | 4.5.2 |
EFFECT OF DROPLET SIZE ON ICING RANGE FOR HELICOPTER BLADE Li Weibin, China | |||
| 07. Sep 21 | 15:00 | 15:30 | 4.5.3 |
THREE-EQUATION TTURBULENCE MODEL FOR SEPARATION PREDICTION OF ICE-ACCRETION AIRFOIL H.-L Li, Tsinghua University, China | |||
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| 07. Sep 21 | 14:00 | 14:30 | 5.5.1 |
INVESTIGATION OF A NOISE REDUCTION PROPELLER GEOMETRY BASED ON AERODYNAMIC AND AEROACOUSTIC OPTIMIZATION X GENG, BEIHANG UNIVERSITY, China | |||
| 07. Sep 21 | 14:30 | 15:00 | 5.5.2 |
MICROPHONE ARRAY TECHNIQUES FOR TRAILING EDGE NOISE BASED ON CONVOLUTIONAL NEUTRAL NETWORK ZC Song, BeiHang Univerisity, China | |||
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| 07. Sep 21 | 14:00 | 14:30 | 6.5.1 |
NUMERICAL SIMULATION OF BOUNDARY LAYER FLOW ON MICROSTRUCTURE SURFACE R.P. Pang, Northwestern Polytechnical University , China | |||
| 07. Sep 21 | 14:30 | 15:00 | 6.5.2 |
SUBSONIC WIND TUNNEL SMALL RIBLETS DRAG REDUCTION TEST ON C919 FUSELAGE MODEL H.W. Wang, China Academy of Aerospace Aerodynamics, China | |||
| 07. Sep 21 | 15:00 | 15:30 | 6.5.3 |
THE EFFECTS OF ADVERSE PRESSURE GRADIENT ON THE BEHAVIORS OF RESOLVENT MODE IN TURBULENT CHANNEL FLOWS Cheng Chen, CARDC, China | |||
| Reserve Paper | 6.5.R |
DIRECT SIMULATION OF THE HYPERSONIC SHOCK WAVE/BOUNDARY LAYER INTERACTION AND ITS HEATING LOAD CONTROL BY MICRO-RAMP VOR D. Sun, State Key Laboratory of Aerodynamics, China | |||||
| Reserve Paper | 6.5.R |
FLOW AND HEAT TRANSFER MECHANISMS OF SINGLE CIRCULAR JET IMPINGEMENT USING LARGE EDDY SIMULATION Q.-L. Li, China | |||||
| Reserve Paper | 6.5.R |
NUMERICAL SIMULATION STUDY ON BOUNDARY LAYER FLOW AND DRAG REDUCTION CHARACTERISTICS OF RIBLETS Du,S.Y. Du, Northwestern Polytechnical University, China | |||||
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| 07. Sep 21 | 14:00 | 14:30 | 7.5.1 |
AERODYNAMIC ANALYSIS OF AN AIR DRIVE EJECTOR FOR USE IN ENGINE TEST FACILITIES Faezeh Rasimarzabadi¹, Martin Neuteboom¹, Catherine Clark¹, Hans Martensson, GKN Aerospace Engine Systems, Sweden; ¹NRC, Canada | |||
| 07. Sep 21 | 14:30 | 15:00 | 7.5.2 |
LOW PARAMETRIZED MODELLING METHODOLOGY TO OPTIMIZE THE WING SURFACE OF AN AIRCRAFT WITH OVER_WING MOUNTED ENGINES PW WEGENER, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany | |||
| 07. Sep 21 | 15:00 | 15:30 | 7.5.3 |
AERODYNAMIC INTERFERENCE OPTIMIZATION OF THE FUSELAGE-PUSHING PROPELLER CONFIGURATION V. Gubskiy, TsAGI, Russia | |||
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| 07. Sep 21 | 14:00 | 14:30 | 8.5.1 |
OPTIMAL DESIGN OF FLUID-CONVEYING PIPE SUPPORT FOR CONTROLLING REACTION FORCE DURING VIBRATION R.T. tian, Aviation Industry Aircraft Strength Research Institute, China | |||
| 07. Sep 21 | 14:30 | 15:00 | 8.5.2 |
OPERATIONAL MODAL ANALYSIS AND ESTIMATION OF AERODYNAMIC PARAMETERS OF A FLEXIBLE AIRCRAFT L. Goes, ITA, Brazil | |||
| 07. Sep 21 | 15:00 | 15:30 | 8.5.3 |
PRELIMINARY DESIGN AND OPTIMIZATION OF A REFERENCE AIRCRAFT UNDER DYNAMIC LOADS H. Schmidt, RWTH University, Germany | |||
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| 07. Sep 21 | 14:00 | 14:30 | 9.5.1 |
CONCEPTUAL STUDIES OF DIFFERENT TYPE OF HYBRID ELECTRIC PROPULSION SYSTEMS FOR COMMUTER AIRLINERS V.S. Zakharchenko, CENTRAL INSTITUTE OF AVIATION MOTORS, Russia | |||
| 07. Sep 21 | 14:30 | 15:00 | 9.5.2 |
THERMAL MANAGEMENT FOR GASOLINE ENGINE-BATTERY HYBRID PROPULSION SYSTEM OF SMALL UAV PLATFORM H.R. Gwon, Korean Air R&D Center, South Korea | |||
| 07. Sep 21 | 15:00 | 15:30 | 9.5.3 |
COMPARATIVE ANALYSIS OF THE HWB WITH MECHANICAL AND ELECTRICAL DRIVEN M. Fioriti, Politecnico di Torino, Italy | |||
| Reserve Paper | 9.5.R |
DIGITAL SIMULATION OF STARTER/GENERATOR CONTROL FOR MORE ELECTRIC ENGINE J XU, AECC COMMERCIAL AIRCRAFT ENGINE CO., LTD., China | |||||
| Reserve Paper | 9.5.R |
IMPLEMENTATION OF DISTRIBUTED ELECTRIC PROPULSION ON A GENERAL AVIATION AIRCRAFT M Gallani, EMBRAER, Brazil | |||||
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| 07. Sep 21 | 14:00 | 14:30 | 10.5.1 |
INFLUENCE OF STABILITY AND CONTROL DERIVATIVES IN PIO PHENOMENON G.D.A.N. Daher de Alencar Neves, Escola de Engenharia de São Carlos, Brazil | |||
| 07. Sep 21 | 14:30 | 15:00 | 10.5.2 |
AIRCRAFT GROUND MOTION SIMULATION ORIENTED 6 DEGREE OF FREEDOM MODEL N. Bai Bai, Beihang University, China | |||
| 07. Sep 21 | 15:00 | 15:30 | 10.5.3 |
RE-ENTRY TRAJECTORY TRACKING CONTROL OF A MICRO-SATELLITE SYSTEM WITH A DEPLOYABLE FRONT STRUCTURE M. Mattei, Università della Campania "Luigi Vanvitelli", Italy | |||
| Reserve Paper | 10.5.R |
INFLUENCE OF AERODYNAMIC ASYMMETRY ON SPIN PARAMETERS OF THE COMMON RESEARCH MODEL M. Sidoryuk, Central Aerohydrodynamic Institute (TsAGI) , Russia | |||||
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| 07. Sep 21 | 14:00 | 14:30 | 11.5.1 |
IMPLEMENTATION OF VELOCITY OBSTACLE METHOD ON A QUADROTOR UNMANNED AERIAL VEHICLE FOR DYNAMIC CONFLICT AVOIDANCE Y.I. Jenie, FTMD - Institut Teknologi Bandung, Indonesia | |||
| 07. Sep 21 | 14:30 | 15:00 | 11.5.2 |
MPC BASED PARTIAL TRAJECTORY PLANNING FOR MULTIROTOR WITH POINT CLOUD OBSTACLES H. Ahn, KAIST, South Korea | |||
| 07. Sep 21 | 15:00 | 15:30 | 11.5.3 |
VELOCITY OBSTACLE METHOD IN OPTICAL FLOW FRAMEWORK FOR AUTOMATIC CONFLICT DETECTION AND RESOLUTION IN UAVS Y.I. Jenie, Faculty of Mechanical and Aerospace Engineering, ITB, Indonesia | |||
| Reserve Paper | 11.5.R |
MOTHERSHIP PLANE WITH SENSING DRONES SYSTEM FOR 3D MAPPING APPLICATIONS M.J. Modzelewski, Warsaw University of Technology, Poland | |||||
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| 07. Sep 21 | 14:00 | 14:30 | 12.5.1 |
THE NOISE REDUCTION STUDY OF COMPOSITE ACOUSTIC LINER ON HIGH BYPASS RATIO TURBOFAN AEROENGINE P-H Hou, Shenyang Aeroengine Research Institute, China | |||
| 07. Sep 21 | 14:30 | 15:00 | 12.5.2 |
DYNAMIC RESPONSE AND DAMAGE OF THE FAN BLADES DURING UAV INGESTION INTO AN AERO-ENGINE N.D Hou, China | |||
| 07. Sep 21 | 15:00 | 15:30 | 12.5.3 |
EXPERIMENTAL AND NUMERICAL STUDY ON BALLISTIC IMPACT OF ARAMID FABRIC H. Pei, China | |||
| Reserve Paper | 12.5.R |
ANALYSIS OF THE DYNAMIC RESPONSE AND FAILURE OF FABRIC SUBJECTED TO BLAST LOADING J.C Jiang, Civil Aviation University of China, China | |||||
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| 07. Sep 21 | 14:00 | 14:30 | 13.5.1 |
AIRCRAFT INFLIGHT ICING DETECTION AND DIAGNOSIS METHODS Di Ding¹, Wei-Qi Qian¹, Qing Wang¹; ¹China Aerodynamics Research and Development Center, China | |||
| 07. Sep 21 | 14:30 | 15:00 | 13.5.2 |
DESIGN AND RESEARCH ON SAFETY ANALYSIS TOOL FOR AVIONICS SYSTEM Yu Liu, Shanghai Aircraft Design and Research Institute, China | |||
| 07. Sep 21 | 15:00 | 15:30 | 13.5.3 |
A PROTOTYPE WHIRL TOWER FOR TESTING INSOLATED ROTOR SYSTEMS IN HOVER M. Wojtas, ?ukasiewicz Research Network - Institute of Aviation, Poland | |||
| Reserve Paper | 13.5.R |
EXPERIMENTAL STUDY ON CRITICAL HEAT FLUX CHARACTERISTICS OF R134A FOLW BOILING IN HORIZONTAL 2.1MM TUBE UNDER HYPERGRAVI H.JJ Jianjun, Nanjing engineering Institute of Aircraft System, Jincheng, AVIC, China | |||||
| Reserve Paper | 13.5.R |
DEVELOPMENT AND ASSESSMENT OF DURABLE ICEPHOBIC COATINGS FOR AIRCRAFT APPLICARIONS J. GARCIA, IRT SAINT EXUPERY, France | |||||
| Reserve Paper | 13.5.R |
ULTRASONIC DE-ICING SYSTEM DESIGN METHODS BASED ON RESONANCE AND IMPEDANCE MATCHING Bo Miao, Nanjing University of Aeronautics and Astronautics, China | |||||
| Reserve Paper | 13.5.R |
A NUMEIRCAL PREDICTION OF AIRCRAFT ICING SITUATION FIELD BASED WRF AND SVR G.-Q.L. Qilei, Northwestern Polytechnical University, China | |||||
| 15:30 - 16:00 | Break | |||
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| 07. Sep 21 | 16:00 | 16:30 | 1.6.1 |
ON ROBUST MULTI DISCIPLINARY ANALYSIS AND OPTIMISATION FOR NEW GENERATION FLEXIBLE AIRCRAFT M. Saporito, University of Southampton, United Kingdom | |||
| 07. Sep 21 | 16:30 | 17:00 | 1.6.2 |
APPLICATION OF ARTIFICIAL NEURAL NETWORKS FOR EFFICIENT RELIABILITY-BASED DESIGN OPTIMIZATION X. Chen, Cranfield University, United Kingdom | |||
| 07. Sep 21 | 17:00 | 17:30 | 1.6.3 |
VALIDATING SURROGATE MODELS AND ICORPORATING UNCERTAINTY QUANTIFICATION IN MULTI-ELEMENTS AIRFOIL DESIGN OPTIMISATION C. Bolart, Cranfield University, United Kingdom | |||
| 07. Sep 21 | 17:30 | 18:00 | 1.6.4 |
EFFICIENT ADAPTIVE SURROGATE-BASED OPTIMIZATION USING FUZZY CLUSTERING FOR COMPLEX SYSTEM OPTIMIZATIONS C.-N. Li, Northwestern Polytechnical University, China | |||
| Reserve Paper | 1.6.R |
A NOVEL RBF DATA TRANSFER METHOD BASED ON PCA GEOMETRIC FEATURE EXTRACTION S.S. Liu, China | |||||
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| 07. Sep 21 | 16:00 | 16:30 | 2.6.1 |
H2020 STRATOFLY PROJECT FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS N. Viola, Politecnico di Torino, Italy | |||
| 07. Sep 21 | 16:30 | 17:00 | 2.6.2 |
THERMAL PROTECTION SYSTEM PRELIMINARY DESIGN OF STRATOFLY HIGH-SPEED PROPELLED VEHICLE R. SCIGLIANO, Italian Aerospace Research Centre (CIRA), Italy | |||
| 07. Sep 21 | 17:00 | 17:30 | 2.6.3 |
HEXAFLY-INT HYPERSONIC VEHICLE THERMAL PROTECTION SYSTEM DESIGN R. SCIGLIANO, Italian Aerospace Research Centre (CIRA), Italy | |||
| 07. Sep 21 | 17:30 | 18:00 | 2.6.4 |
AERODYNAMIC DESIGN THEORY AND METHODOLOGY FOR AN AIRFRAME-INLET INTEGRATED FULL-WAVERIDER VEHICLE F. D. Ding, National University of Defense Technology, China | |||
| Reserve Paper | 2.6.R |
NOVEL OSCULATING AXISYMMETRIC DESIGN METHOD FOR A HYPERSONIC WAVERIDER VEHICLE DERIVED FROM A POINTED VON KARMAN OGIVE F. D. Ding, National University of Defense Technology, China | |||||
| Reserve Paper | 2.6.R |
INTEGRATION OF AN INCREASING-FIDELITY AERODYNAMIC MODELLING APPROACH IN THE CONCEPTUAL DESIGN OF HYPERSONIC CRUISER R. Fusaro, Politecnico di Torino, Italy | |||||
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| 07. Sep 21 | 16:00 | 16:30 | 4.6.1 |
ON THE ASSESSMENT OF TURBULENCE MODELS FOR THE SIMULATION OF VORTICAL FLOWS R. C. Gonzalez, Cranfield Unversity, United Kingdom; S. A. Prince, Cranfield University, United Kingdom | |||
| 07. Sep 21 | 16:30 | 17:00 | 4.6.2 |
RESEARCH OF TURBULENCE MODELING BASED ON MACHINE LEARNING Y. Y. Yin, Tsinghua University, China | |||
| 07. Sep 21 | 17:00 | 17:30 | 4.6.3 |
RESEARCH ON MACHINE LEARNING RECONSTRUCTION OF TURBULENCE MODEL DRIVEN BY EXPERIMENTAL DATA Y.-F. Wang, BUAA, China | |||
| 07. Sep 21 | 17:30 | 18:00 | 4.6.4 |
TURBULENCE MODEL ASSESSMENT OF THE SEPARATED FLOW IN THE STANFORD DIFFUSER M. Bonnici¹, S. A. Prince¹, K. P. Garry¹; ¹Cranfield University, United Kingdom | |||
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| 07. Sep 21 | 16:00 | 16:30 | 5.6.1 |
EXPERIMENT AND THEORETICAL ANALYSIS OF A TYPE OF NON-SYNCHRONOUS VIBRATION IN A HIGH PRESSURE COMPRESSOR GAO Fei-Long, Shenyang Engine Research Institute, China | |||
| 07. Sep 21 | 16:30 | 17:00 | 5.6.2 |
TSAGI’S EXPERIENCE IN THE DEVELOPMENT OF SIX-COMPONENT ROTATING SHAFT BALANCES V.S. Manvelyan, Central Aerohydrodynamic Institute (TsAGI), Russia | |||
| 07. Sep 21 | 17:00 | 17:30 | 5.6.3 |
JET FLAME RESEARCH BASED ON PHOSPHORESCENT IMAGING TECHNIQUE AND HILBERT-HUANG TRANSFORM METHOD P Tian, Shanghai Jiao Tong University, China | |||
| 07. Sep 21 | 17:30 | 18:00 | 5.6.4 |
MEASUREMENT AND ANALYSIS OF INTER-STAGE FLOW FIELD IN A HIGH-LOAD AXIAL MULTISTAGE COMPRESSOR Z.-Z. Zhang, AECC Shenyang Engine Research Institute, China | |||
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| 07. Sep 21 | 16:00 | 16:30 | 6.6.1 |
HYBRID LAMINAR FLOW CONTROL (HLFC) RESEARCH AT AIRCRAFT RESEARCH ASSOCIATION (ARA), PAST, PRESENT AND FUTURE A. Ciarella, ARA, United Kingdom | |||
| 07. Sep 21 | 16:30 | 17:00 | 6.6.2 |
INVESTIGATION OF LAMINARIZATION EFFICIENCY OF THE SECTIONED SUCTION SYSTEM ON THE SWEPT WING IN FAILURE CASE S.N. Tolkachev, Central Aerohydrodynamic Institute (TsAGI), Russia | |||
| 07. Sep 21 | 17:00 | 17:30 | 6.6.3 |
ENERGY HARVESTING FROM PIEZOELECTRIC FRINGES AT THE TRAILING EDGE OF A FINITE WING WITH LEADING-EDGE TUBERCLES M. Melo de Sousa, Instituto Superior Tecnico, Portugal | |||
| 07. Sep 21 | 17:30 | 18:00 | 6.6.4 |
HIGH-LIFT NOISE REDUCTION USING PLASMA ACTUATORS G. P. G. Silva, University of Sao Paulo, Brazil | |||
| Reserve Paper | 6.6.R |
INVESTIGATION OF ROLL ATTENUATION MECHANISM OF LOW-ASPECT-RATIO WINGS USING BIONIC FLOW CONTROL APPROACHES T. Hu, Beihang University, China | |||||
| Reserve Paper | 6.6.R |
MIXING CONTROL BY LASER PLASMA IN HELIUM JET/SHOCK WAVE INTERACTION Fan Liu¹, Hong Yan¹, Alexander Zheltovodov, Khristianovich Institute of Theoretical and Applied Mechanics, Russia; ¹Northwestern Polytechnical University, China | |||||
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| 07. Sep 21 | 16:00 | 16:30 | 7.6.1 |
INVESTIGATION AERODYNAMICS FLAPPING FLIGHT ROBOTIC BIRD H.W.M. Hoeijmakers, University of Twente, Netherlands | |||
| 07. Sep 21 | 16:30 | 17:00 | 7.6.2 |
DEFORMATION AND FLOWFIELD INVESTIGATION OF A FLAPING-WING MAV IN GROUND EFFECT J WANG, Northwestern Polytechnical University, China | |||
| 07. Sep 21 | 17:00 | 17:30 | 7.6.3 |
EFFECTS OF SPANWISE AREA DISTRIBUTION ON AERODYNAMIC PERFORMANCE OF FLAPPING WINGS IN HOVER Z CAO, Northwestern Polytechnical University, China | |||
| 07. Sep 21 | 17:30 | 18:00 | 7.6.4 |
THE INFLUENCE OF SWEEPING MOTION ON THREE-DIMENSIONAL FLOW PATTERNS AND AERODYNAMIC PERFORMANCE OF FLAPPING WINGS T.-W. Wu, Northwestern Polytechnical University, China | |||
| Reserve Paper | 7.6.R |
NEURAL MODEL OF FIXED WINGS MICRO AERIAL VEHICLE AERODYNAMICS K.-S. Sibilski, Warsaw University of Technology, Poland | |||||
| Reserve Paper | 7.6.R |
NUMERICAL SIMULATION OF SPANWISE FOLDING EFFECTS ON A BIRD-SCALE FLAPPING WING X.Y. Lang, School of Aeronautics, Northwestern Polytechnical University, China | |||||
| Reserve Paper | 7.6.R |
BIO-INSPIRED AERODYNAMIC OPTIMISATION OF BLUFF-BODIES E.R.G Gowree, ISAE-SUPAERO, France | |||||
| Reserve Paper | 7.6.R |
NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING LEADING EDGE COVERTS Jiangxin Gao Gao, Northwestern Polytechnical University, China | |||||
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| 07. Sep 21 | 16:00 | 16:30 | 8.6.1 |
ACHIEVEMENTS IN THE BUCKLING OF THIN-WALLED COMPOSITE LAUNCHER STRUCTURES RD Degenhardt, DLR, Germany | |||
| 07. Sep 21 | 16:30 | 17:00 | 8.6.2 |
THE VIBRATION CORRELATION TECHNIQUE – A RELIABLE NONDESTRUCTIVE METHOD TO PREDICTBUCKLING LOADS - Abramovich, Technion, I.I.T.,, Israel | |||
| 07. Sep 21 | 17:00 | 17:30 | 8.6.3 |
INVESTIGATION OF BUCKLING RESPONSE OF CYLINDRICAL SHELLS USING 3D-PRINTING TECHNOLOGY C. Bisagni, Delft University of Technology, Netherlands | |||
| 07. Sep 21 | 17:30 | 18:00 | 8.6.4 |
KINEMATIC MODEL OF REFINED THEORY AND EXACT ANALYTICAL SOLUTIONS OF STATIC AND BUCKLING PROBLEMS OF STRUCTURALLY-ANISOTR L M Liubov, Moscow Aviation Institute (NRU), Russia | |||
| Reserve Paper | 8.6.R |
OPTIMIZATION AND STRENGTH TESTS OF COMPRESSED COMPOSITE TUBE AS A MAIN ELEMENT OF MECHANICAL FLIGHT CONTROL SYSTEM. W. Grendysa, Warsaw University of Technology, Poland | |||||
| Reserve Paper | 8.6.R |
STUDY ON THE COMPRESSION PROPERTIES OF MULTISTAGE TITANIUM ALLOY LATTICE METAMATERIALS AT HIGH TEMPERUTURE H.HY HUANG, School of Aeronautics Northwestern Polytechnical University, China | |||||
| Reserve Paper | 8.6.R |
OPTIMIZATION AND STRENGTH TESTS OF COMPRESSED COMPOSITE TUBE AS A MAIN ELEMENT OF MECHANICAL FLIGHT CONTROL SYSTEM. W Grendysa, Warsaw University of Technology, Poland | |||||
| Reserve Paper | 8.6.R |
ADVANCED MODELS FOR THE POST-BUCKLING RESPONSE ANALYSIS OF AEROSPACE REINFOCED COMPOSITE PANELS A. Pagani, Politecnico di Torino, Italy | |||||
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| 07. Sep 21 | 16:00 | 16:30 | 9.6.1 |
EVOLUTION OF TOLLMIEN-SCHLICHTING DISTURBANCES OVER NATURALLY DISTRIBUTED ROUGH SURFACES S. Mughal, Imperial College London, United Kingdom | |||
| 07. Sep 21 | 16:30 | 17:00 | 9.6.2 |
VIBRATION INDUCED EXCITATION AND CONTROL OF TOLLMIEN-SCHLICHTING WAVES E.R.G Gowree, ISAE-SUPAERO, France | |||
| 07. Sep 21 | 17:00 | 17:30 | 9.6.3 |
NON-LINEAR BOUNDARY LAYER RECEPTIVITY TO FREE-STREAM TURBULENCE D. Sboev, Central Aerohydrodynamic Institute (TsAGI), Russia | |||
| 07. Sep 21 | 17:30 | 18:00 | 9.6.4 |
STABILITY ANALYSIS OF STREAMWISE CORNER FLOW D Xu, Tsinghua University, China | |||
| Reserve Paper | 9.6.R |
LINEAR GLOBAL STABILITY ANALYSIS OF ROUGHNESS-INDUCED TRANSITION Qiang Yang¹, Guohua Tu¹, Jianqiang Chen¹, Xianxu Yuan¹; ¹State Key Laboratory of Aerodynamics, China | |||||
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| 07. Sep 21 | 16:00 | 16:30 | 10.6.1 |
IMPACT OF CONTROL ALLOCATION METHODS ON THE OPTIMAL CONTROL SURFACE LAYOUT OF BOX-WING AIRCRAFT C. Varriale, Delft University of Technology, Netherlands | |||
| 07. Sep 21 | 16:30 | 17:00 | 10.6.2 |
DECISION-MAKING MODELLING: APPLICATION TO APPROACH PHASE IN AUTONOMOUS AIR TO AIR REFUELLING I Romo, Airbus, Spain | |||
| 07. Sep 21 | 17:00 | 17:30 | 10.6.3 |
ADVANCED REFUELING BOOM SYSTEM (ARBS) AUTOMATIC AIR TO AIR REFUELING FLIGHT CONTROL LAWS A. Sanz de Blas, Airbus Defence & Space, Spain | |||
| 07. Sep 21 | 17:30 | 18:00 | 10.6.4 |
DECOUPLING CONTROL LAW DESIGN FOR AN OBLIQUE-WING AIRCRAFT BASED ON EIGENSTRUCTURE ASSIGNMENT AND MODEL FOLLOWING L Qiu, Chinese Flight Test Establishment, China | |||
| Reserve Paper | 10.6.R |
GAIN SCHEDULING BY FREQUENCY SHAPED LINEAR QUADRATIC CONTROL OF FIXED-WING AIRCRAFT LONGITUDINAL MOTION. L.S. Kim, Korea Advanced Institute of Science and Technology, South Korea | |||||
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| 07. Sep 21 | 16:00 | 16:30 | 11.6.1 |
A VARIABLE-FIDELITY METHOD FOR UNMANNED AIRCRAFT WAKE VORTEX SAFETY AND CONTROL ANALYSIS V. Golubev, ERAU, United States | |||
| 07. Sep 21 | 16:30 | 17:00 | 11.6.2 |
MULTIROTOR VEHICLES DESIGN BASED ON DYNAMIC MANIPULABILITY FOR UNDERACTUATED FLYING SYSTEMS S. Hokamoto, Kyushu Univ., Japan | |||
| 07. Sep 21 | 17:00 | 17:30 | 11.6.3 |
LANDING SYSTEM USING EXTENDED DYNAMIC WINDOW APPROACH FOR FIXED-WING UAV S Ishioka, Nihon university, Japan | |||
| 07. Sep 21 | 17:30 | 18:00 | 11.6.4 |
MPPC OF MULTICOPTER WITH FAULT ROTOR IN COLLISION SITUATION Y Shimizu, Univerisity of Tokyo, Japan | |||
| Reserve Paper | 11.6.R |
AUTONOMOUS CONTROL OF FIXED-WING UNMANNED AERIAL SYSTEMS(UASS) BY REINFORCEMENT LEARNING H. Wang, AVIC Xi'an Flight Automatic Control Research Institute, China | |||||
| Reserve Paper | 11.6.R |
NEW ROLL-SPIRAL COUPLING MODE CRITERION FOR HIGH SPEED VEHICLES D-GH Dou, China Academy of Aerodynamic of Aerospace, China | |||||
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| 07. Sep 21 | 16:00 | 16:30 | 12.6.1 |
TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES AEROSTRUCTURES I. Rivero Arevalo, Airbus, Spain | |||
| 07. Sep 21 | 16:30 | 17:00 | 12.6.2 |
STUDY OF COMPOSITE SKIN-STRINGER FATIGUE BEHAVIOR UNDER BROADBAND RANDOM VIBRATION F. Sevastyanov, The Central Aerohydrodynamic Institute named after N.E.Zhukovsky, Russia | |||
| 07. Sep 21 | 17:00 | 17:30 | 12.6.3 |
APPROACH OF THE STATIC AND FATIGUE STRENGTH ESTIMATION OF THE COMPOSITE JOINTS A.A. Sviridov, The Central Aerohydrodynamic Institute, Russia | |||
| 07. Sep 21 | 17:30 | 18:00 | 12.6.4 |
FAILURE CRITERION OF CFRP FOR OPEN-HOLE FATIGUE TESTING A.G. Kalinin, TsAGI, Russia | |||
| Reserve Paper | 12.6.R |
MODEL CURVES: A SIMPLE WAY TO ACCOUNT FOR COMPLEX EFFECTS A.A. Bautin, TsAGI, Russia | |||||
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| 07. Sep 21 | 16:00 | 16:30 | 13.6.1 |
RESEARCH ON SAFETY ASSESSMENT APPROACH FOR UAS OPERATIONS OVER UNINHABITED AREAS ZQ Zhang, Northwestern Polytechnical University, China | |||
| 07. Sep 21 | 16:30 | 17:00 | 13.6.2 |
END TO END CYBERSECURITY IN CIVIL AVIATION ECO SYSTEM JC Jean-Claude, Airbus, France | |||
| 07. Sep 21 | 17:00 | 17:30 | 13.6.3 |
STUDY ON DYNAMIC RESPONSE AND INJURY OF FRONT ROW OCCUPANT UNDER HORIZONTAL IMPACT M.S.C. MA, Civil Aviation University of China, China | |||
| 07. Sep 21 | 17:30 | 18:00 | 13.6.4 |
STATISTICAL ANALYSIS OF AIRCRAFT INCIDENTS M-28 BRYZA J. Tomaszewska, Polish Air Force University, Poland | |||
| Reserve Paper | 13.6.R |
FIRE AND EXPLOSION ANALYSIS OF AIRCRAFT FUEL TANK BASED ON TNT EQUIVALENT METHOD AND FIREBALL EXPLOSION MODEL W K KAI, AVIC XI'AN AIRCRAFT INDUSTRY (GROUP) COMPANY LTD, China | |||||
| Reserve Paper | 13.6.R |
FLIGHT PERFORMANCE AND TRAJECTORY PREDICTION OF THE COAXIAL HELICOPTER IN AUTOROTATION S.-Z. Zhao, Northwestern Polytechnical University, China | |||||
Wednesday, 08. Sep 2021
7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
| 0.6 | General Lecture 3 - Trends in Aircraft Propulsion: Reflections on ISABE 2019 Chair: Ric Parker President ISABE | |||
| 08. Sep 21 | 08:00 | 09:00 |
Ric Parker, President ISABE | |
| 09:00 - 09:30 | Break | |||
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| 08. Sep 21 | 09:30 | 10:00 | 1.7.1 |
IMPACT OF NEW TECHNOLOGIES ON AIRCRAFT SYSTEMS A. Berres, German Aerospace Center, Germany | |||
| 08. Sep 21 | 10:00 | 10:30 | 1.7.2 |
APPLICATIONS OF FAST: AN OPEN SOURCE TOOL FOR AIRCRAFT CONCEPTUAL AND PRELIMINARY DESIGN S. M. Delbecq, ISAE-SUPAERO, France | |||
| 08. Sep 21 | 10:30 | 11:00 | 1.7.3 |
LAMBDA: A KNOWLEDGE-BASED MODULAR, MULTIFIDELITY AND MULTIDISCIPLINARY AIRCRAFT CONCEPTUAL DESIGN ENVIRONMENT S. Hosseini, Amirkabir University of Technology, Iran | |||
| 08. Sep 21 | 11:00 | 11:30 | 1.7.4 |
IMPROVED LINEAR METHOD FOR SONIC BOOM PREDICTION OF SUPERSONIC TRANSPORTS Y.-L. Ding, Northwestern Polytechnical University, China | |||
| 08. Sep 21 | 11:30 | 12:00 | 1.7.5 |
LOW SWEEP LAMINAR FLOW WING AT TRANSONIC SPEED N. Qin, The University of Sheffield, United Kingdom | |||
| Reserve Paper | 1.7.R |
AERODYNAMIC DESIGN OPTIMIZATION OF WAVERIDER-DERIVED VEHICLE S.W. Wei, Beijing Institute of Space Long March Vehicle, China | |||||
| Reserve Paper | 1.7.R |
ENGINE INTEGRATION AND WING OPTIMIZATION OF A MID-RANGE AIRCRAFT WITH OVER-WING MOUNTED ENGINE P. Wegener, German Aerospace Center, Germany | |||||
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| 08. Sep 21 | 09:30 | 10:00 | 2.7.1 |
MULTIDISCIPLINARY OPTIMISATION OF A FUEL-CELL-POWERED EVTOL FIXED-WING CARGO UAV D. Verstraete, The University of Sydney, Australia | |||
| 08. Sep 21 | 10:00 | 10:30 | 2.7.2 |
CONCEPTUAL DESIGN FOR LONG-ENDURANCE CONVERTIBLE UNMANNED AERIAL SYSTEM Y Leng, ISAE, France | |||
| 08. Sep 21 | 10:30 | 11:00 | 2.7.3 |
DESIGN OF A HYBRID-POWER VTOL LOGISTICS UAV SYSTEM INTEGRATED INTO THE CIVIL AVIATION AIR TRAFFIC MANAGEMENT SYSTEM H.-J. Jiang, Xi'an Tangyan Aviation Technology CO. LTD, China | |||
| 08. Sep 21 | 11:00 | 11:30 | 2.7.4 |
SURROGATE-BASED MULTIDISCIPLINARY DESIGN OPTIMIZATION OF MULTIROTOR DRONES S. M. Delbecq, ISAE-SUPAERO, France | |||
| 08. Sep 21 | 11:30 | 12:00 | 2.7.5 |
AERODYNAMIC ANALYSIS ON TAIL-SITTER UAV HOVERING UNDER CROSSWIND Chen Jiaojiao Jiaojiao, Northwestern Polytechnical University, China | |||
| Reserve Paper | 2.7.R |
LIGHTWEIGHT UAV FOR EMERGENCY MEDICAL SERVICE T. Goetzendorf-Grabowski, Warsaw University of Technology, Poland | |||||
| Reserve Paper | 2.7.R |
CONCEPTUAL DESIGN AND IMPLEMENTATION OF A NOVEL TRICOPTER FIXED-WING VTOL UAV CONFIGURATION P. Stahl, Technical University of Munich, Germany | |||||
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| 08. Sep 21 | 09:30 | 10:00 | 3.7.1 |
MODEL-BASED ENGINEERING OF A SYSTEM DIAGNOSTIC ENGINE FOR AN AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM F. Mardt, Hamburg University of Technology, Germany | |||
| 08. Sep 21 | 10:00 | 10:30 | 3.7.2 |
A MBSE DESIGN ARCHITECTURE FOR CONTROL SYSTEM BASED ON DEMAND ELEMENT TRANSFER P.J. Wang, Tsinghua University, China | |||
| 08. Sep 21 | 10:30 | 11:00 | 3.7.3 |
A DOCUMENT-BASED VS. MODEL-BASED APPLICATION OF THE NASA SYSTEMS ENGINEERING PROCESS L. Boggero, German Aerospace Center (DLR), Germany | |||
| 08. Sep 21 | 11:00 | 11:30 | 3.7.4 |
TOWARDS THE NEXT GENERATION OF COMPLEX SYSTEMS ARCHITECTING: A MBSE FRAMEWORK TO AIRCRAFT DEVELOPMENT P. D. Ciampa, DLR, Germany | |||
| 08. Sep 21 | 11:30 | 12:00 | 3.7.5 |
HYBRID MODELLING FOR FULL MISSION SIMULATION P Krus, Linköping university, Sweden | |||
| Reserve Paper | 3.7.R |
MODEL-BASED STAKEHOLDER REQUIREMENTS DEFINITION FOR JOINT MISSION PLANNING SYSTEM D.-Z. Du, Aviation Industry Development Research Center of China, China | |||||
| Reserve Paper | 3.7.R |
SOS BEHAVIOR MODEL TRANSFORMATION FOR AIRCRAFT TOP-LEVEL DEMONSTRATION J Zang, Aviation Industry Development Research Center of China, China | |||||
| Reserve Paper | 3.7.R |
MODEL-BASED VIRTUAL INTEGRATED TEST METHOD FOR AVIONICS SYSTEM S.F. Zhu, COMAC Beijing Aircraft Technology Research Institute, China | |||||
| Reserve Paper | 3.7.R |
CONNECTING SYSTEM SIMULATION TO AIRCRAFT CONCEPT DEVELOPMENT A. Oprea, SAAB Aeronautics, Sweden | |||||
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| 08. Sep 21 | 09:30 | 10:00 | 4.7.1 |
EXPERIMENTAL VALIDATION OF NUMERICAL PREDICTION OF WING-PROPELLER AERODYNAMIC INTERACTION L. P. Ruiz Calavera, Airbus Defence & Space, Spain | |||
| 08. Sep 21 | 10:00 | 10:30 | 4.7.2 |
FLOW STRUCTURE INVESTIGATION OF CONTRA-ROTATING WIND TURBINES BY CFD AND EXPERIMENTAL METHODS K You, Northwestern Polytechnical University, China | |||
| 08. Sep 21 | 10:30 | 11:00 | 4.7.3 |
STATIC AEROELASTIC COMPUTATIONS OF WING CONFIGURATIONS IN TRANSONIC FLOWS AT HIGH REYNOLDS NUMBERS J. A. A. Lyrio, Instituto Tecnológico de Aeronáutica, Brazil | |||
| 08. Sep 21 | 11:00 | 11:30 | 4.7.4 |
NUMERICAL INVESTIGATION OF WING ROCK PHENOMENON ON LOW ASPECT RATIO RECTANGULAR WINGS AT LOW REYNOLDS NUMBER N/A Maqsood, Pakistan | |||
| 08. Sep 21 | 11:30 | 12:00 | 4.7.5 |
A COMPUTATIONAL FLUID DYNAMICS ANALYSIS OF A HISTORICAL SEAPLANE CRUISE AND TAKE OFF PERFORMANCE E. Cestino, Politecnico di Torino, Italy | |||
| Reserve Paper | 4.7.R |
ADVANCED AIRCRAFT FIRE EXTINGUISHING NUMERICAL SIMULATION Y. SOMMERER, AIRBUS, France | |||||
| Reserve Paper | 4.7.R |
FLUID STRUCTURE INTERACTION OF RAM-AIR PARACHUTE TRAILING EDGE DEFLECTION Gao XL Gao, China Aerodynamics Research and Development Center, China | |||||
| Reserve Paper | 4.7.R |
AERODYNAMIC MODELING AND FLIGHT PERFORMANCE RESEARCH OF THE COAXIAL RIGID HELICOPTER IN POP-UP PROCESS H.-Y. Li, Northwestern Polytechnical University, China | |||||
| Reserve Paper | 4.7.R |
NUMERICAL SIMULATION OF PITCHING MOTION EFFECTS ON THE AERODYNAMIC PERFORMANCE OF DRAGONFLY-LIKE FLAPPING WING XY.-L Lang, China | |||||
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| 08. Sep 21 | 09:30 | 10:00 | 5.7.1 |
NEW INVESTIGATION METHOD OF THE SHOCK WAVE/BOUNDARY LAYER INTERACTION PATTERN AT TRANSONIC SPEEDS M.A. Brutyan, TsAGI, Russia | |||
| 08. Sep 21 | 10:00 | 10:30 | 5.7.2 |
INFLUENCE OF VARIABLE WALL PERFORATION RATIO ON BOUNDARY LAYER PARAMETERS AT TRANSONIC SPEEDS S.L. Osipova, Central Aerohydrodynamic Institute named after N.E. Zhukovsky, Russia | |||
| 08. Sep 21 | 10:30 | 11:00 | 5.7.3 |
RESEARCH OF HYBRID LAMINAR FLOW CONTROL TECHNOLOGY FOR CIVIL AIRCRAFT WING C. Shao, Shanghai Aircraft Design and Research Institute, COMAC, China | |||
| 08. Sep 21 | 11:00 | 11:30 | 5.7.4 |
STUDY OF SHOCK WAVE / LAMINAR BOUNDARY LAYER INTERACTION AREA BY PIV TECHNIQUE Oleg: O. Vishnyakov, Khristianovich Institute of Theoretical and Applied Mechanics SB, Russia | |||
| 08. Sep 21 | 11:30 | 12:00 | 5.7.5 |
DEVELOPMENT OF THE MODEL NEAR-FIELD STUDY TECHNIQUES INTHE SUPERSONIC WIND TUNNELS AIMED AT THE SONIC BOOM PREDICTION A.I. IVANOV, TSAGI, Russia | |||
| Reserve Paper | 5.7.R |
THE EXPERIMENTAL INVESTIGATION OF THE THROTTLING SECOND THROAT INFLUENCE ON TRANSONIC WIND TUNNEL FLOW QUALITY Z HaiYang, China Aerodynamics Research and Development Center, Facility des, China | |||||
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| 08. Sep 21 | 09:30 | 10:00 | 6.7.1 |
INVESTIGATIONS OF AERODYNAMIC CHARACTERISTICS AND LAMINAR-TURBULENT TRANSITION ON LARGE-SCALE TRANSONIC AIRFOIL V.G. Soudakov, TsAGI, Russia | |||
| 08. Sep 21 | 10:00 | 10:30 | 6.7.2 |
TYPES OF TRANSONIC BUFFET FOR A LAMINAR AIRFOILS P.A. Polivanov, Khristianovich Institute of Theoretical and Applied Mechanics SB, Russia | |||
| 08. Sep 21 | 10:30 | 11:00 | 6.7.3 |
BUFFET CONTROL ON STRUCT-BRACED WING AIRCRAFT USING TANGENTIAL BLOWING S Li, School of Aerospace Engineering, Tsinghua University, China | |||
| 08. Sep 21 | 11:00 | 11:30 | 6.7.4 |
HIGH-FIDELITY ANALYSIS OF ROBUST NONLINEAR 2-DOF AIRFOIL LCO CONTROL V. Golubev, ERAU, United States | |||
| 08. Sep 21 | 11:30 | 12:00 | 6.7.5 |
ANALYSIS AND CONTROL OF DYNAMIC STALL CHARACTERISTICS OF S809 AIRFOIL L-S Hao, Northwestern Polytechnical University, China | |||
| Reserve Paper | 6.7.R |
NUMERICAL STUDY ON HIGH-FREQUENCY RESPONSE OF WALL JETS FOR GUST LOAD CONTROL X. C. Xue, Nanjing University of Aeronautics and Astronautics, China | |||||
| Reserve Paper | 6.7.R |
PHISICAL AND MATHEMATICAL MODELS OF THE BUFFET ONSET A.M. Lipanov, Institute of Applied Mathematics, Russia | |||||
| Reserve Paper | 6.7.R |
ANALYSIS OF AERODYNAMIC COUPLING EFFECT IN CLOSE FORMATION FOR FLAPPING WINGS Z-LF Zhao, Beihang University, China | |||||
| |||||||
| 08. Sep 21 | 09:30 | 10:00 | 7.7.1 |
SPARSE POLYNOMIAL CHAOS EXPANSION BASED ON FULLY ADAPTIVE FORWARD-BACKWARD SELECTION METHOD H. Zhao, Northwestern Polytechnical University, China | |||
| 08. Sep 21 | 10:00 | 10:30 | 7.7.2 |
ON IMPROVING GRADIENT-ENHANCED KRIGING MODEL FOR AERODYNAMIC DESIGN OPTIMIZATION D.H.D. Dang, Northwestern Polytechnical University, China | |||
| 08. Sep 21 | 10:30 | 11:00 | 7.7.3 |
FAR-FIELD WAVEFORM DESIGN OPTIMIZATION BASED ON SONIC BOOM NOISE LEVEL J.-L. Qiao, Northwestern Polytechnical University, China | |||
| 08. Sep 21 | 11:00 | 11:30 | 7.7.4 |
PREDICTION OF FLIGHT DYNAMICS IN WAKE SURFING SCENARIOS MML Lone, Cranfield University, United Kingdom | |||
| 08. Sep 21 | 11:30 | 12:00 | 7.7.5 |
IMPROVED WEIGHTED GRADIENT-ENHANCED KRIGING MODEL FOR HIGH-DIMENSIONAL AERODYNAMIC DESIGN OPTIMIZATION PROBLEMS C.-Z. Xu, China | |||
| Reserve Paper | 7.7.R |
AERODYNAMIC EVALUATION OF FORWARD-SWEPT AND SWEPTBACK WING WITH OPTIMIZED PLANEFORMS Sei-ichiro Morizawa, National Institute of Technology, Okinawa College, Japan | |||||
| Reserve Paper | 7.7.R |
AERODYNAMIC DESIGN OPTIMIZATION OF WAVERIDER-DERIVED VEHICLE W. Su, Beijing Institute of Space Long March Vehicle, China | |||||
| Reserve Paper | 7.7.R |
APPLICATION OF TRANSFER LEARNING AND DEEP REINFORCEMENT LEARNING IN OPTIMIZATION OF HIGH-LIFT DEVICES JH.D. Dai, Beihang University, China | |||||
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| 08. Sep 21 | 09:30 | 10:00 | 8.7.1 |
AN INVERSE APPROACH BASED ON EUCLIDEAN SPACE FOR DETERMINING STRUCTURAL LOAD DISTRIBUTION FROM STRAIN MEASUREMENTS H.N. Dui, AVIC, Chengdu Aircraft Design & Research Institute, China | |||
| 08. Sep 21 | 10:00 | 10:30 | 8.7.2 |
DESIGN OF EXPERIMENTS TECHNIQUES TO INVESTIGATE LOAD SHARE STRATEGIES BETWEEN AERO ENGINE, NACELLE AND POWERPLANT COMPONENTS C.-M MARTIN , Queens University Belfast, United Kingdom | |||
| 08. Sep 21 | 10:30 | 11:00 | 8.7.3 |
THERMOPLASTIC APPLICATIONS FOR AEROSTRUCTURES: TOWARDS SUSTAINABLE AND WEIGHT EFFICIENT APPLICATIONS LLJ Herman, France | |||
| 08. Sep 21 | 11:00 | 11:30 | 8.7.4 |
RATIONAL DETERMINATION OF WING JIG SHAPE OF A LONG-RANGE AIRCRAFT WITH TRANSONIC CRUISE REGIME A.V. Bezuevsky, TsAGI, Russia | |||
| 08. Sep 21 | 11:30 | 12:00 | 8.7.5 |
AIRCRAFT ENGINE ROTOR DYNAMICS ANALYSIS AFTER FAN BLADE-OUT WITH ACCOUNT OF ROTOR-CASING CONTACT INTERACTIONS V. Myasnikov, Central Institute of Aviation Motors, Russia | |||
| Reserve Paper | 8.7.R |
THE METHOD OF AIRCRAFT MATHEMATICAL MODEL STIFFNESS PROPERTIES CORRECTION BASED ON EXPERIMENTAL RESEARCH RESULTS M.A. Pronin, Central Aerohydrodynamic Institute n.a. prof. N.E.Zhukovsky, Russia | |||||
| Reserve Paper | 8.7.R |
STRUCTURAL HEALTH MONITORING OF SANDWICH STRUCTURES WITH LATTICE CORES IN AIRCRAFT DESIGN: CHALLENGES AND POTENTIAL T. Huang, RWTH Aachen University, Germany | |||||
| Reserve Paper | 8.7.R |
RESEARCH ON STRUCTURAL DESIGN OF TAIL BOOM FOR AN UNMANNED HELICOPTER C.-G. Yang¹, Z.-Q. Tian¹; ¹China Helicopter Design and Research Institute, China | |||||
| Reserve Paper | 8.7.R |
AN INTEGRATED AERODYNAMIC/THERMAL/STRUCTURAL DESIGN FRAMEWORK FOR HYPERSONIC VEHICLES Li C. Li, Beihang University, China | |||||
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| 08. Sep 21 | 09:30 | 10:00 | 9.7.1 |
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF POST-MACHINING DISTORTION FOR LARGE AEROSPACE MONOLITHIC COMPONENTS BS SHI, National Research Council Canada, Canada | |||
| 08. Sep 21 | 10:00 | 10:30 | 9.7.2 |
RESEARCH ON THE DEVELOPMENT AND PERFORMANCE OF THE OBSTACLE-PASSING STRUCTURE OF THE CRAWLER INSPECTION ROBOT Pu Zhang¹, Jin Sun¹; ¹Beihang University, China | |||
| 08. Sep 21 | 10:30 | 11:00 | 9.7.3 |
SOFTWARE-BASED IMPROVING THE QUALITY OF HIGH-SPEED MACHINING S. Zietarski, Military University of Technology, Poland | |||
| 08. Sep 21 | 11:00 | 11:30 | 9.7.4 |
RESEARCH ON MANUFACTURING PROCESS AND MICROSTRUCTURE OF SIC/ALSI7MG COMPOSITE FABRICATED BY SELECTIVE LASER MELTING H Zhu, China | |||
| 08. Sep 21 | 11:30 | 12:00 | 9.7.5 |
EXPERIMENTAL STUDY ON PATH PLANNING OF BELT GRINDING FOR BIOMIMETIC SURFACE ON AERO-ENGINE BLADE Chongqing Univer Xiao, China | |||
| Reserve Paper | 9.7.R |
AUTOMATIC DETECTION TECHNOLOGYOF LARGE CIVIL AIRCRAFT BASED ON IMAGE RECOGNITION T.-L. SHEN, China | |||||
| Reserve Paper | 9.7.R |
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| Reserve Paper | 9.7.R |
RESEARCH ON SOLVING PROBLEM OF AIRCRAFT ASSEMBLY COORDINATION BASED ON 3D LASER SCANNING MEASUREMENT TECHNOLOGY W J JIAN, China | |||||
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| 08. Sep 21 | 09:30 | 10:00 | 10.7.1 |
VIRTUAL FLIGHT TEST OF A BWB AIRCRAFT IN LOW SPEED WIND TUNNEL B.W. NIE, National University of Defense Technology, China | |||
| 08. Sep 21 | 10:00 | 10:30 | 10.7.2 |
INVESTIGATION INTO FLIGHT DYNAMICS OF A BLENDED-WING-BODY AIRCRAFT F. CEN, China | |||
| 08. Sep 21 | 10:30 | 11:00 | 10.7.3 |
BAYESIAN APPROACH TO SIMULTANEOUS STATIC AND DYNAMIC FLIGHT CHARACTERISTICS MODELING M. Naruoka, Japan Aerospace Exploration Agency, Japan | |||
| 08. Sep 21 | 11:00 | 11:30 | 10.7.4 |
THE ANALYSIS OF TAKEOFF ROTATION OF SUBSCALE FREE-FLIGHT TESTS K.-M. MA, Xi’an Aircraft Design Institute, China | |||
| 08. Sep 21 | 11:30 | 12:00 | 10.7.5 |
SIMULTANEOUS ESTIMATION OF DERIVATIVES, TRIM STATES, AND WIND Yoshimasa: Y. Ochi, National Defense Academy, Japan | |||
| Reserve Paper | 10.7.R |
IDENTIFICATION OF AIRCRAFT MODEL CONSIDERING FREQUENCY CHARACTERISTICS OF MAXIMAL LENGTH SEQUENCE INPUT A. Fujimori, University of Yamanashi, Japan | |||||
| Reserve Paper | 10.7.R |
SEPARATE IDENTIFICATION OF AIRCRAFT THRUST AND DRAG FORCES THROUGH FLIGHT TEST DATA O. N. Korsun, Moscow Aviation Institute (National Research University), Russia | |||||
| Reserve Paper | 10.7.R |
ANALYTICAL MODELLING OF A HOVERABLE X-SHAPE FLAPPING WING AIRCRAFT CONSIDERING WING-TAIL INTERACTION LF Zhao, Beihang University, China | |||||
| Reserve Paper | 10.7.R |
MODELING AND CONTROL OF A HOVERABLE FLAPPING WING AIRCRAFT CONSIDERING FLAPPING WING INDUCED FLOW Z-LF Zhao, Beihang University, China | |||||
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| 08. Sep 21 | 09:30 | 10:00 | 11.7.1 |
LIEBHERR-AEROSPACE EHA TECHNOLOGY FOR FUTURE FLIGHT CONTROL APPLICATION T. Röben, Liebherr-Aerospace, Germany | |||
| 08. Sep 21 | 10:00 | 10:30 | 11.7.2 |
THE DEVELOPMENT OF ALGORITHMS FOR EMA FAULT EARLY DETECTION SYSTEM A.V. Skryabin, 1. Central Aerohydrodynamic Institute of Russia, Russia | |||
| 08. Sep 21 | 10:30 | 11:00 | 11.7.3 |
CONCEPTUAL STUDY OF THE DIGITAL HYDRAULIC ACTUATOR WITH PROPORTIONAL CONTROL FOR FLIGHT CONTROL ACTUATION SYSTEMS A. Dell'Amico, Saab AB, Sweden | |||
| 08. Sep 21 | 11:00 | 11:30 | 11.7.4 |
VIRTUAL PROTOTYPING OF ELECTRICAL THS ACTUATOR FOCUSED ON MECHANICAL POWER TRANSMISSION FUNCTIONS J. FU FU, BEIHANG UNIVERSITY, China | |||
| 08. Sep 21 | 11:30 | 12:00 | 11.7.5 |
DYNAMIC ANALYSIS AND CONTROL DESIGN OF A FAULT-TOLERANT ELECTRO-MECHANICAL ACTUATOR WITH DIFFERENTIAL BALL SCREWS G. Di Rito, Università di Pisa - Dipartimento di Ing. Civile ed Industriale, Italy; N. Borgarelli¹, M. Nardeschi¹, B. Luciano, AESIS s.r.l., Italy; ¹Umbra Group S.p.A., Italy | |||
| Reserve Paper | 11.7.R |
DESIGN AND CHARACTERIZATION OF A NOVEL DUAL REDUNDANCY ELECTRO-HYDROSTATIC ACTUATOR SYSTEM H.-Q. QI, Beihang University, China | |||||
| Reserve Paper | 11.7.R |
A RESEARCH ON POSITION CONTROL ACTUATORS FOR FIXEDWINGED RESEARCH UAVS D.T. Teubl, Institute of Aircraft Design TUM, Germany | |||||
| Reserve Paper | 11.7.R |
AN ONTOLOGICAL APPROACH FOR CLASSIFYING AIRCRAFT ACTUATORS F Larsson, Saab Aeronautics, Sweden | |||||
| Reserve Paper | 11.7.R |
MEASURE OF PERFORMANCE MAPPING FOR ACTUATION SYSTEM DESIGN C. Reichenwallner, Linköping university, Sweden | |||||
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| 08. Sep 21 | 09:30 | 10:00 | 12.7.1 |
IMPACT OF ENROUTE TIME-BASED METERING ON EQUITY IN DELAY DISTRIBUTION A. Andreeva-Mori, JAXA, Japan | |||
| 08. Sep 21 | 10:00 | 10:30 | 12.7.2 |
SPATIO-TEMPORALLY CORRELATED WIND MODELING AND PROBABILISTIC TRAJECTORY PREDICTION USING ENSEMBLE WEATHER FORECASTS Y Matsuno, Japan Aerospace Exploration Agency, Japan | |||
| 08. Sep 21 | 10:30 | 11:00 | 12.7.3 |
COGNITIVE HUMAN-MACHINE INTERFACES FOR ENROUTE AIR TRAFFIC FLOW MANAGEMENT A. Gardi, RMIT University, Australia | |||
| 08. Sep 21 | 11:00 | 11:30 | 12.7.4 |
RESEARCH ON TRAJECTORY OPTIMIZATION TECHNOLOGY CONSIDERING METEOROLOGICAL INFORMATION PREDICTION G.-W Guo, China National Aeronautical Radio Electronics Research Institute, China | |||
| 08. Sep 21 | 11:30 | 12:00 | 12.7.5 |
QUANTITATIVE ANALYSIS OF PMS AND ARRIVAL METERING SYNERGY EFFECT ON INBOUND FLIGHTS AT TOKYO INTERNATIONAL AIRPORT T. Mori, Osaka Prefecture University, Japan | |||
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| 08. Sep 21 | 09:30 | 10:00 | 13.7.1 |
GEARED FANS AND VARIABLE PITCH FANS - NUMERICAL AND EXPERIMENTAL INVESTIGATIONS OF THEIR AERODYNAMICS S.V. Pankov, Central Institute of Aviation Motors (CIAM), Russia | |||
| 08. Sep 21 | 10:00 | 10:30 | 13.7.2 |
ANALYSIS OF AERODYNAMIC CHARACTERISTICS OF PROPELLERS AT LOW ADVANCE RATIO USING A WHIRLING ARM Y.I. Itoh, Iwate university, Japan | |||
| 08. Sep 21 | 10:30 | 11:00 | 13.7.3 |
EXPERIMENTAL STUDIES OF SLOT-TYPE CASING TREATMENTS FOR MODEL FANS WITH THE AIM OF AERODYNAMIC AND ACOUSTIC IMPROVEMENTS V.I. Mileshin, Central Institute of Aviation Motors, Russia | |||
| 08. Sep 21 | 11:00 | 11:30 | 13.7.4 |
ANALYSIS OF THRUST-SCALED PROPELLER NOISE AND ITS TRADE-OFF WITH PROPELLER EFFICIENCY T. Sinnige, Netherlands | |||
| 08. Sep 21 | 11:30 | 12:00 | 13.7.5 |
MODELING OF COUNTER-ROTATING LIFT FAN/MAIN ENGINE COMBINED PROPULSION SYSTEM AND LIFT FAN AERODYNAMIC DESIGN H.-L JIN, AECC Hunan Aviation Powerplant Research Institute, China | |||
| Reserve Paper | 13.7.R |
AERODYNAMICS DESIGN, OPTIMIZATION AND FLOW FIELD INVESTIGATION OF A CONTRA-ROTATING PROPFAN AT HIGH FLIGHT MACH NUMBERS T Wu¹, W Dong¹; ¹Shanghai Jiao Tong University, China | |||||
| Reserve Paper | 13.7.R |
STUDY OF NON-ROTATING MICROPHONE ARRAY FOR SPINNING DUCT MODE DETECTION Y. Jiyong, AECC Commercial Aircraft Engine Co., Ltd., China | |||||
| 12:00 - 13:00 | Lunch | |||
| 0.7 | General Lecture 4 - Virtual Aircraft Technology Integration Platform – Results of DLR’s Project VicToria Chair: Björn Nagel DLR | |||
| 08. Sep 21 | 13:00 | 13:55 |
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| 08. Sep 21 | 14:00 | 14:30 | 1.8.1 |
EXPERIMENTAL RESEARCH ON PROPULSION AND AERODYNAMIC CHARACTERISTICS OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT X.-Y. ZHANG, Northwestern Polytechnical University, China | |||
| 08. Sep 21 | 14:30 | 15:00 | 1.8.2 |
PROPULSIVE FUSELAGE AIRCRAFT CONCEPT – A SUMMARY OF STRUCTURE ANALYSIS BASED ON CENTRELINE H2020 Z. Goraj, Warsaw University of Technology, Poland | |||
| 08. Sep 21 | 15:00 | 15:30 | 1.8.3 |
REQUIREMENTS AND LIMITATIONS FOR GENERAL AVIATION ELECTRIC AIRPLANES Z. Lei, Suwa University of Science, Japan | |||
| Reserve Paper | 1.8.R |
LANDING PLATFORM FOR URBAN AIR MOBILITY VEHICLES INTEGRATED INTO PARKING LOT INFRASTRUCTURE IN DENSELY BUILT-UP AREAS P. Brusberg, Germany | |||||
| Reserve Paper | 1.8.R |
DESIGN OF A PROTOTYPE LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: CONTROL, ALIMENTATION, AND PROPULSION SYSTEMS M. Civera, Politecnico di Torino, Italy | |||||
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| 08. Sep 21 | 14:00 | 14:30 | 2.8.1 |
TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55X L. Di Ianni, Politecnico di Torino, Italy | |||
| 08. Sep 21 | 14:30 | 15:00 | 2.8.2 |
INTERNATIONAL VIRTUAL COLLABORATION IN UNDERGRADUATE AERONAUTICAL ENGINEERING EDUCATION – CHALLENGES AND EXPERIENCES J. Abulawi, HAW Hamburg, Germany | |||
| 08. Sep 21 | 15:00 | 15:30 | 2.8.3 |
OPEN SCIENCE IN AVIATION RESEARCH: THE INDIVIDUAL ADVANTAGE OF SHARING KNOWLEDGE M. Spieck, Thelsys GmbH, Germany | |||
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| 08. Sep 21 | 14:00 | 14:30 | 3.8.1 |
A RECURRENT PLANNING STRATEGY FOR UAV PATH IDENTIFICATION IN A DYNAMIC ENVIRONMENT BASED ON BIT-CODED FLIGHT MANOEUVRES L. BLASI, UNIVERSITA' DELLA CAMPANIA "LUIGI VANVITELLI", Italy | |||
| 08. Sep 21 | 14:30 | 15:00 | 3.8.2 |
A NOVEL DETECT-AND-AVOID SYSTEM OF UAS IN URBAN ENVIRONMENT L.N. Nurhakim, RMIT University, Australia | |||
| 08. Sep 21 | 15:00 | 15:30 | 3.8.3 |
AUTONOMOUS CONFLICT RESOLUTION ALGORITHM BASED ON ELLIPTIC GEOMETRY R.A. Sasongko, Institut Teknologi Bandung, Indonesia | |||
| Reserve Paper | 3.8.R |
HYDRO ENVIRONMENTAL MAPPING TOOL USING SWARMS AND MACHINE LEARNING, UAV & USV R.K.R. Kuntz, Brazil | |||||
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| 08. Sep 21 | 14:00 | 14:30 | 4.8.1 |
VALIDATION OF A DISCONTINUOUS GALERKIN BASED DES SOLVER IN FLOW PROBLEMS USING HIGH PERFORMANCE COMPUTING A.V. Wolkov, TsAGI, Russia | |||
| 08. Sep 21 | 14:30 | 15:00 | 4.8.2 |
ADVANCED WEEK SOLUTIONS IN FLUID DYNAMICS AND THEIR NUMERICAL COMPUTATIONS WITH AERODYNAMIC HEATING M.Ja. Ivanov, Central Institute of Aviation Motors, Russia | |||
| 08. Sep 21 | 15:00 | 15:30 | 4.8.3 |
A BENCHMARK METHOD FOR PREDICTING OBLIQUE SHOCK STRUCTURE A. Shi, Northwestern Polytechnical University, China | |||
| Reserve Paper | 4.8.R |
ACCURATE SIMULATIONS OF AIRCRAFT WAKE VORTICES WITH HIGH-ORDER NUMERICAL METHOD S. Bosnyakov, TsAGI, Russia | |||||
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| 08. Sep 21 | 14:00 | 14:30 | 5.8.1 |
COMPARISON OF ISOLATED AND DUCTED FIXED-PITCH PROPELLERS UNDER NON-AXIAL INFLOW CONDITIONS M. Cerny, Germany | |||
| 08. Sep 21 | 14:30 | 15:00 | 5.8.2 |
INVESTIGATION OF THE CHARACTERISTICS OF THE HELICOPTER MAIN ROTOR WITH ELASTIC MOUNTING BLADES O.-E. Kirillov, Central Aerohydrodynamic Institute (TsAGI), Russia | |||
| 08. Sep 21 | 15:00 | 15:30 | 5.8.3 |
EXPERIMENTAL MEASUREMENTS ON BIOMIMETIC WIND TURBINE BLADES BY P. TOMENTOSA SEED L.-P Paiva, UFU, Brazil | |||
| Reserve Paper | 5.8.R |
EXPERIMENTAL INVESTIGATION OF PULSATION OF THE ROTOR SLIPSTREAM ACTING ON AN ELEVATED HELIPORT P. Ruchala, Institute of Aviation, Poland | |||||
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| 08. Sep 21 | 14:00 | 14:30 | 6.8.1 |
IMPROVEMENT OF HELICOPTER PERFORMANCE THROUGH PULSE AIR-JETS BLOWN FROM THE TRAILING EDGE OF MAIN ROTOR BLADES W.S. STALEWSKI, LUKASIEWICZ RESEARCH NETWORK - INSTITUTE OF AVIATION, Poland | |||
| 08. Sep 21 | 14:30 | 15:00 | 6.8.2 |
ENHANED STRAIGHT BLADED VAWT BY RETRACTABLE GURNEY FLAPS K. Song, Northwestern Polytechnical University, China | |||
| 08. Sep 21 | 15:00 | 15:30 | 6.8.3 |
STUDY ON THE EFFECTS OF PROPLET GEOMETRIC PARAMETERS ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLER B.W Wang, China | |||
| Reserve Paper | 6.8.R |
APPLICATION OF A LEADING-EDGE TIP EXTENSION ON DELTA WING WITH WINGLET FOR HIGH LIFT X.Y. Feng, Northwestern Polytechnical University, China | |||||
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| 08. Sep 21 | 14:00 | 14:30 | 7.8.1 |
AERODYNAMIC OPTIMIZATION DESIGN OF DOUBLE BLUNT ROTOR AIRFOIL WITH LARGE THICKNESS IN FORWARD AND REVERSE FLOW Y.-M. YAO, China | |||
| 08. Sep 21 | 14:30 | 15:00 | 7.8.2 |
PARETO FRONT EXPLORATION USING MANIFOLD LEARNING APPROACH FOR ROTORCRAFT AIRFOILS DESIGN C.-S. Song, Computational Aerodynamics Institute, China Aerodynamics Researc, China | |||
| 08. Sep 21 | 15:00 | 15:30 | 7.8.3 |
MULTI-OBJECTIVE AERODYNAMIC SHAPE OPTIMIZATION OF WIDE-MACH-NUMBER-RANGE WING CONSIDERING LIFT MATCHING Y Zhang, NORTHWESTERN POLYTECHNICAL UNIVERSITY, China | |||
| Reserve Paper | 7.8.R |
DESIGN OPTIMIZATION OF AIRFOILS AT ULTRA-LOW REYNOLDS NUMBERS J.-H. Xu, Northwestern Polytechnical University, China | |||||
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| 08. Sep 21 | 14:00 | 14:30 | 8.8.1 |
RESEARCH PROGRESS OF DISTRIBUTED OPTICAL FIBER SENSING DEFORMATION MEASUREMENT FOR MORPHING WING X-Jf Xue, Chinese Aeronautical Establishment, China | |||
| 08. Sep 21 | 14:30 | 15:00 | 8.8.2 |
ACTUATION MECHANISM USING SHAPE MEMORY ALLOY WIRES IN SPIRAL ARRANGEMENT R Tsukamoto, Meijo University, Japan | |||
| 08. Sep 21 | 15:00 | 15:30 | 8.8.3 |
MORPHING AIRCRAFT BASED ON SMART MATERIALS AND STRUCTURES J. Sun, Harbin Institute of Technology, China | |||
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| 08. Sep 21 | 14:00 | 14:30 | 9.8.1 |
EFFECTS OF COOLANT BUILD DIRECTION ON ADDITIVELY MANUFACTURED FAN-SHAPED COOLING HOLES Z.-Q QI, AECC HUNAN AVIATION POWERPLANT RESEARCH INSTITUTE, China | |||
| 08. Sep 21 | 14:30 | 15:00 | 9.8.2 |
APPLICATION OF ADDITIVE MANUFACTURING TO THE PRODUCTION OF RPAV COMPONENTS E. Cestino, Politecnico di Torino, Italy | |||
| 08. Sep 21 | 15:00 | 15:30 | 9.8.3 |
DESIGNING AERONAUTICAL PARTS FOR ADDITIVE MANUFACTURING – SUPPORTED BY A VIRTUAL DESIGN ADVISOR J. Abulawi, HAW Hamburg, Germany | |||
| Reserve Paper | 9.8.R |
AN EFFICIENT FINITE ELEMENT SIMULATION METHOD FOR ADDITIVE MANUFACTURING PROCESSES Q.-Y. Liu, Beihang University, China | |||||
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| 08. Sep 21 | 14:00 | 14:30 | 10.8.1 |
GUARANTEED FLYING QUALITIES UNDER REAL AND COMPLEX UNCERTAINTIES D. Seiferth, Technical University of Munich, Germany | |||
| 08. Sep 21 | 14:30 | 15:00 | 10.8.2 |
CONTROL ALLOCATION FOR ONERA\'S SMALL BUSINESS CONCEPT PLANE AMPERE WITH DISTRIBUTED ELECTRIC PROPULSION C. DÖLL, ONERA, France | |||
| 08. Sep 21 | 15:00 | 15:30 | 10.8.3 |
ON THE MAXIMIZATION OF CONTROL POWER IN LOW-SPEED FLIGHT FOR A BWB CONFIGURATION L.M.B.C. Campos, IDMEC/CCTAE/IST, Portugal | |||
| Reserve Paper | 10.8.R |
AN ACTIVE SIDESTICK CONTROLLER FOR AIRCRAFT GROUND OPERATIONS J Gauci, University of Malta, Malta | |||||
| Reserve Paper | 10.8.R |
THE APPLICATION OF THE PILOT-AIRCRAFT SYSTEM APPROACH FOR OPTIMIZING 3D DISPLAY PARAMETERS A. V. Efremov¹, M. S. Tiaglik¹, I. Kh. Irgaleev¹; ¹Moscow Aviation Institute, Russia | |||||
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| 08. Sep 21 | 14:00 | 14:30 | 11.8.1 |
DAMAGE DETECTION OF AERONAUTICAL PANELS BY USING CROSS-CORRELATION OF SPATIALLY SHIFTED DISTRIBUTED STRAIN SENSORS M. Ciminello, C.I.R.A. Italian Aerospace Research Center, Italy | |||
| 08. Sep 21 | 14:30 | 15:00 | 11.8.2 |
THEORETICAL AND EXPERIMENTAL STUDY FOR THE DEVELOPMENT OF SELF-POWERED MONITORING SYSTEMS WITH MFC PIEZOELECTRIC PATCHES G. Di Rito¹, M.-R. Chiarelli¹, V. Franchi¹, L. Bancallari, MBDA Italia S.p.A., Italy; B. Luciano, AESIS s.r.l., Italy; ¹Università di Pisa - Dipartimento di Ing. Civile ed Industriale, Italy | |||
| 08. Sep 21 | 15:00 | 15:30 | 11.8.3 |
STUDY ON CLOSED-LOOP CROSS COMPENSATION CONTROL TECHNOLOGY IN ACCELERATED FATIGUE TEST HONGWEI ZHAO¹, HONGWEI ZHAO, Xi’an jiaotong University, China; HAN TAO¹, ZHENZHONG GU, Chongqing Hongyu Precision Industrial Co., Ltd., China; GUANGSHENG SHI, Shenyang Aircraft Design & Research Institute of China, China; JIANMIN FENG¹, SHIHUI DUAN¹; ¹Aircraft Strength Research Institute of China, China | |||
| Reserve Paper | 11.8.R |
DESIGN OF DATA SERVICE ARCHITECTURE FOR AVIATION PHM SYSTEM BASED ON MULTI-LAYER PROTOCOL P.J. Wang, Tsinghua University, China | |||||
| Reserve Paper | 11.8.R |
RELIABILITY ANALYSIS AND EVALUATION METHOD FOR DESIGN APPRAISAL OF AIRBORNE EQUIPMENTS Z-J-L Zhang, AVIC XI’AN AIRCRAFT INDUSTRY (GROUP) COMPANY LTD., China | |||||
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| 08. Sep 21 | 14:00 | 14:30 | 12.8.1 |
ANGULAR 3D INSTRUMENT APPROACHES FOR GLS EQUIPPED AIRCRAFT USING A LIGHT AND MOBILE SBAS TO GBAS CONVERTER T. Dautermann, DLR , Germany | |||
| 08. Sep 21 | 14:30 | 15:00 | 12.8.2 |
ON THE MINIMUM SEPARATION BETWEEN ANY PAIR OF FLIGHT PATHS L.M.B.C. Campos, IDMEC/CCTAE/IST, Portugal | |||
| 08. Sep 21 | 15:00 | 15:30 | 12.8.3 |
AIRSPACE CAPACITY MANAGEMENT OPTIMISATION FOR TRAJECTORY BASED OPERATIONS D. Zheng Zhang¹, E. Puntero Parla¹, M. Sánchez Cidoncha¹, F. Gómez Comendador², R. Arnaldo Valdés²; ¹CRIDA A.I.E., Spain ;²Technical University of Madrid, Spain | |||
| Reserve Paper | 12.8.R |
DESIGNING AIRCRAFT TRAFFIC FLOWS USING DATA-DRIVEN QUEUING MODELS E. Itoh, ENRI, Japan | |||||
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| 08. Sep 21 | 14:00 | 14:30 | 13.8.1 |
DEVELOPMENT OF AIRFRAME DIGITAL TWIN TECHNOLOGY FOR AIRCRAFT STRUCTURAL INTEGRITY MANAGEMENT PROGRAM Min Liao, National Research Council Canada, Canada | |||
| 08. Sep 21 | 14:30 | 15:00 | 13.8.2 |
A DIGITAL EQUIVALENT DEVELOPMENT FOR FATIGUE AND DAMAGE TOLERANCE IN AIRCRAFT STRUCTURES L. ZAPLANA MANZANO, AIRBUS , Spain | |||
| 08. Sep 21 | 15:00 | 15:30 | 13.8.3 |
EXPERIMENTAL STUDY OF THE EFFECT OF BIAXIAL STRESS STATE ON THE GROWTH RATE OF FATIGUE CRACKS A.V. Kulemin, Central Aerohydrodynamic Institute n. a. N.E. Zhukovsky (TsAGI), Russia | |||
| Reserve Paper | 13.8.R |
INVESTIGATION OF THE INFLUENCE OF LOW AMPLITUDE LOADS ON THE FATIGUE LIFE OF CFRP SAMPLES WITH IMPACT DAMAGE UNDER IRRE V.G. Lukyanchuk, Central Aerohydrodynamic Institute, TsAGI, Russia, Russia | |||||
| 15:30 - 16:00 | Break | |||
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| 08. Sep 21 | 16:00 | 16:30 | 1.9.1 |
FUEL-CELL HYBRID-ELECTRIC AIRCRAFT: DESIGN, OPERATIONAL AND ENVIRONMENTAL IMPACT A. E. Scholz, Technical University of Munich, Germany | |||
| 08. Sep 21 | 16:30 | 17:00 | 1.9.2 |
DESIGN FOR DIRECTIONAL CONTROL AND STABILITY OF AIRCRAFT WITH DISTRIBUTED PROPULSION J.S.E. Soikkeli¹, M.F.M. Hoogreef¹; ¹Delft University of Technology, Netherlands | |||
| 08. Sep 21 | 17:00 | 17:30 | 1.9.3 |
VALIDATION OF AN AERODYNAMIC MODEL FOR THE DESIGN OF SUBSCALE TEST AIRCRAFT WITH DISTRIBUTED ELECTRICAL PROPULSION O. Luderer, Hamburg University of Technology, Germany | |||
| 08. Sep 21 | 17:30 | 18:00 | 1.9.4 |
CONCEPTUAL DESIGN OF SILENT ELECTRIC COMMUTER AIRCRAFT G. Atanasov, Germany | |||
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| 08. Sep 21 | 16:00 | 16:30 | 2.9.1 |
HYBRID POWER SYSTEM FOR NEW GENERATION OF VTOL UNMANNED AERIAL VEHICLES WITH A TAKE-OFF WEIGHT OF UP TO 300 KG L. Czajkowski, ?ukasiewicz Research Network - Institute of Aviation, Poland | |||
| 08. Sep 21 | 16:30 | 17:00 | 2.9.2 |
DEVELOPMENT OF A TURN-KEY, INTEGRATED RAPID DESIGN AND MANUFACTURING ENVIRONMENT FOR SUAS D. Verstraete, The University of Sydney, Australia | |||
| 08. Sep 21 | 17:00 | 17:30 | 2.9.3 |
DATABASE BASED MULTI-MISSION DESIGN FOR E-VTOL UAVS T. Seren, Institute of Aircraft Design - Technical University of Munich, Germany | |||
| 08. Sep 21 | 17:30 | 18:00 | 2.9.4 |
METHODOLOGY FOR OBTAINING AN OPTIMIZED BAFFLED AIRFOIL FOR AN INFLATABLE WING S.R.M. Mistri, Indian Institute of Technology- Bombay, India | |||
| Reserve Paper | 2.9.R |
INTEGRATED AERODYNAMIC DESIGN OF PROPELLER POSITION AND WING SHAPE AT A LOW REYNOLDS NUMBER W. YANG, CARDC, China | |||||
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| 08. Sep 21 | 16:00 | 16:30 | 3.9.1 |
FLIGHT TEST OF AN ADVANCED HYBRID-LAMINAR-FLOW-CONTROL (HLFC) SYSTEM ON AN A320 VERTICAL TAIL PLANE H. von Geyr, German Aerospace >Centre, DLR, Germany | |||
| 08. Sep 21 | 16:30 | 17:00 | 3.9.2 |
ACTIVE FLOW CONTROL (AFC) AT PYLON / WING JUNCTION OF CIVIL AIRCRAFT – A FULL-SCALE DEMONSTRATION T. M. Gibson, Airbus Operations Limited, United Kingdom | |||
| 08. Sep 21 | 17:00 | 17:30 | 3.9.3 |
NOISE REDUCTION AT FLAP SIDE EDGE AND UNDERCARRIAGE S Pott-Pollenske, DLR, Germany | |||
| 08. Sep 21 | 17:30 | 18:00 | 3.9.4 |
MAIN LANDING GEAR DOORS VIBRATION REDUCTION BASED ON FLIGHT TEST R Abarca Lopez, Airbus, Spain | |||
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| 08. Sep 21 | 16:00 | 16:30 | 4.9.1 |
STALL PREDICTION OF AIRCRAFT WITH ADAPTIVE HYBRID MESH J. Tang¹, J. Zhang¹, N.-C. Zhou¹, B. Li¹, P.-C. Cui¹; ¹China Aerodynamics Research and Development Center, China | |||
| 08. Sep 21 | 16:30 | 17:00 | 4.9.2 |
LATTICE BOLTZMANN SIMULATIONS OF STORE SEPARATION TRAJECTORIES G. Trapani, Dassault Systemes Spain, Spain | |||
| 08. Sep 21 | 17:00 | 17:30 | 4.9.3 |
TRAJECTORY PREDICTIONS FOR THE MK-82 STORE FROM A GENERIC CAVITY Alex CENKO, AIWS, United States | |||
| 08. Sep 21 | 17:30 | 18:00 | 4.9.4 |
COMPUTATIONAL STUDY ON COAND? BLANKET CURVATURE EFFECTS ON HALF-SPHERICAL COAND? DEVICE PERFORMANCE HD Djojodihardjo, Retired Professor, Indonesia | |||
| Reserve Paper | 4.9.R |
NUMERICAL SIMULATION AND ANALYSIS OF SECOND THROAT IN LARGE WIND TUNNELS B.-B.-X. Xu, CARDC, China | |||||
| Reserve Paper | 4.9.R |
A VALIDATION STUDY FOR EFFECT OF CAMBER IN A MULTI ELEMENT AIRFOIL IN SUBSONIC FLOW CONDITIONS E. GULRAIZ, RCMS, NUST, Pakistan | |||||
| Reserve Paper | 4.9.R |
HELICOPTER ROTOR AERODYNAMIC PERFORMANCE PREDICTION BASED ON FLOW SIMULATION AROUND AIRFOILS S.-Z. Zhao, Northwesn Polytechnical University, China | |||||
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| 08. Sep 21 | 16:00 | 16:30 | 5.9.1 |
INTAKE BOUNDARY LAYER PROFILE ESTIMATION FOR BLI PERFORMANCE PREDICTION ON A BLENDED WING BODY K. Ma¹, S. Prince¹; ¹Cranfield University, United Kingdom | |||
| 08. Sep 21 | 16:30 | 17:00 | 5.9.2 |
NUMERICAL STUDY OF HEAT TRANSFER ENHANCEMENT OF CONFINED JET IN AIRCRAFT ANTI-ICING CHAMBER J.-J Niu, Northwestern Polytechnical University, China | |||
| 08. Sep 21 | 17:00 | 17:30 | 5.9.3 |
NUMERICAL INVESTIGATION ON FLOW INTERFERENCE BETWEEN BLENDED-WING-BODY AIRCRAFT AND OVERHANGING NACELLE A.X.Q Qiu, China | |||
| 08. Sep 21 | 17:30 | 18:00 | 5.9.4 |
PRELIMINARY AERODYNAMIC DESIGN AND ANALYSIS OF TRUSS-BRACED WING REGIONAL AIRCRAFT USING HIGH-FIDELITY METHODS S. Hosseini, Amirkabir University of Technology, Iran | |||
| Reserve Paper | 5.9.R |
AN INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS FOR SAAB J-29 AIRCRAFT DESIGN USING HIGH FIDELITY CFD M. Zhang, Airinnova AB, Sweden | |||||
| Reserve Paper | 5.9.R |
AN OPTIMIZATION OF ANTI-ICING CHAMBER BASED ON POD AND KRIGING J Niu, Northwestern Polytechnical University, College of Aeronautics, China | |||||
| Reserve Paper | 5.9.R |
CONTROL OF RAMS-HORN VORTEX STALL ON SWEPT WINGS: A CFD STUDY M Zhang, Airinnova, Sweden | |||||
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| 08. Sep 21 | 16:00 | 16:30 | 6.9.1 |
STABILIZATION OF SUPERSONIC BOUNDARY LAYERS IN THE PRESENCE OF FAVORABLE PRESSURE GRADIENT P.V. Chuvakhov¹, A.V. Fedorov, Moscow Institute of Physics and Technology (MIPT), Russia; A.O. Obraz¹; ¹Central Aerohydrodynamic Institue (TsAGI), Russia | |||
| 08. Sep 21 | 16:30 | 17:00 | 6.9.2 |
NUMERICAL SIMULATION OF THREE-DIMENSIONAL DISTURBANCES EVOLUTION IN SUPERSONIC FLOW OVER A WAVY SURFACE A.V. Novikov, Central Aerohydrodynamic Institute, Russia | |||
| 08. Sep 21 | 17:00 | 17:30 | 6.9.3 |
MECHANISMS OF NATURAL LAMINAR-TURBULENT TRANSITION ON AN UNSWEPT WING IN SUPERSONIC FLIGHT P.V. Chuvakhov¹, A.V. Fedorov², A.O. Obraz¹, I.O. Pogorelov²; ¹Central Aerohydrodynamic Institue (TsAGI), Russia ;²Moscow Institute of Physics and Technology (MIPT), Russia | |||
| 08. Sep 21 | 17:30 | 18:00 | 6.9.4 |
TRIGGERING SUPERSONIC BOUNDARY-LAYER INSTABILITY BY SMALL-SCALE VORTEX SHEDDING G. Tu, State Key Laboratory of Aerodynamics, China | |||
| Reserve Paper | 6.9.R |
GLOBAL STABILITY ANALYSIS ON A LIFTING-BODY BOUNDARY LAYER X. Chen, China | |||||
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| 08. Sep 21 | 16:00 | 16:30 | 7.9.1 |
GRADIENT-BASED ROBUST DESIGN OF A WING WITH 3D SHOCK CONTROL BUMPS C. Sabater, German Aerospace Center (DLR), Germany | |||
| 08. Sep 21 | 16:30 | 17:00 | 7.9.2 |
AERODYNAMIC PERFORMANCE ANALYSIS USING AN EXERGY BALANCE METHOD I. Petropoulos, ONERA, France | |||
| 08. Sep 21 | 17:00 | 17:30 | 7.9.3 |
DRAG REDUCTION ANALYSIS IN CLOSE-FORMATION FLIGHT X.X. Meng, Northwestern Polytechnical University, China | |||
| 08. Sep 21 | 17:30 | 18:00 | 7.9.4 |
INCREASING THE EFFECTIVENESS OF AN AERODYNAMICALLY BALANCED CONTROL SURFACE ON A MODIFIED AIRFOIL WITH REDUCED DRAG V.V. Bogatyrev, TsAGI, Russia | |||
| Reserve Paper | 7.9.R |
DESIGN OF WINGTIP SAILS FOR A LARGE-ASPECT-RATIO WING Y. Liu¹, R. Zeng¹, L. Ping¹; ¹CETC Wuhu Diamond Aircraft Manufacture co., LTD, China | |||||
| Reserve Paper | 7.9.R |
AERODYNAMIC DESIGN AND ANALYSIS ON A NEW STEPPED WINGLET BASED ON THE DYNAMIC CHARACTERISTICS OF THE WINGTIP VORTEX J.Jin Jin, Shanghai Aircraft Design and Research Institute,COMAC, China | |||||
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| 08. Sep 21 | 16:00 | 16:30 | 8.9.1 |
RESEARCH ON ATTITUDE CONTROL AND CONSTRAINT SYSTEM DESIGN OF FULL-SCALE AIRCRAFT STATIC TEST BASED ON BARYCENTRE JJ ZHENG, AVICASRI, China | |||
| 08. Sep 21 | 16:30 | 17:00 | 8.9.2 |
NON-CONTACT MEASUREMENT OF SURFACE DEFORMATION FIELDS BY VIDEOGRAMMETRY METHOD K.A. Kuruliuk, Central Aerohydrodynamic Institute n. a. prof. N.E. Zhukovsky, Russia | |||
| 08. Sep 21 | 17:00 | 17:30 | 8.9.3 |
OPTIMIZATION FOR PROCESS AND MANAGEMENT IN MASSIVE STRAIN MEASUREMENT IN THE FULL SCALE AIRCRAFT STRUCTURE STRENGTH TEST J. Zuo, Aircraft Strength Research Institute of China, China | |||
| 08. Sep 21 | 17:30 | 18:00 | 8.9.4 |
DESIGN OF A VERTICAL DITCHING TEST E. Cestino, Politecnico di Torino, Italy | |||
| Reserve Paper | 8.9.R |
A SUBJECTIVE EVALUATION METHOD OF AIRCRAFT VIBRATION IN FLIGHT TEST H.G WANG, COMAC, China | |||||
| Reserve Paper | 8.9.R |
RESEARCH PROGRESS OF DISTRIBUTED OPTICAL FIBER SENSING DEFORMATION MEASUREMENT FOR MORPHING WING J F Xue, Chinese Aeronautical Establishment, China | |||||
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| 08. Sep 21 | 16:00 | 16:30 | 9.9.1 |
ASSESSING THE IMPACT OF PRODUCTION MODELING IN CONCEPTUAL AIRCRAFT DESIGN J. Page Risueno, German Aerospace Center (DLR), Germany | |||
| 08. Sep 21 | 16:30 | 17:00 | 9.9.2 |
A STRUCTURED AND SCALABLE APPROACH FOR THE DEFINITION OF DEEP LEARNING ARCHITECTURES FOR BEARING ANOMALY DETECTION O Pinon Fischer, Georgia Institute of Technology, United States | |||
| 08. Sep 21 | 17:00 | 17:30 | 9.9.3 |
INCORPORTING KNOWLEDGE COVERAGE MEASUREMENT INTO KNOWLEDGE TRANSFORMATION FROM DATA FOR KNOWLEDGE ACCUMULATION Y.-B. Fan, NanChang HangKong University, China | |||
| 08. Sep 21 | 17:30 | 18:00 | 9.9.4 |
DESIGN AND BEST PRACTICES OF SUPPLIER PERFORMANCE EVALUATION IN SUPPLY CHAIN HZ-L Li, AECC SHANGHAI COMMERCIAL AIRCRAFT ENGINE MANUFACTURING CO.,LTD., China | |||
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| 08. Sep 21 | 16:00 | 16:30 | 10.9.1 |
AIRCRAFT BRAKING DYNAMICS AND BRAKE SYSTEM MODELING FOR FAULT DETECTION AND ISOLATION L.C.N. Cardoso Navarro, ITA, Brazil | |||
| 08. Sep 21 | 16:30 | 17:00 | 10.9.2 |
LEARNING FLIGHT CONTROL SKILLS BY IMITATING EXPERT DEMONSTRATIONS R. Takase, The University of Tokyo, Japan | |||
| 08. Sep 21 | 17:00 | 17:30 | 10.9.3 |
TWO-LAYER ADAPTIVE AUGMENTATION FOR INCREMENTAL BACKSTEPPING FLIGHT CONTROL OF AIRCRAFT IN FAILURE CONDITIONS D. Ignatyev, Cranfield University, United Kingdom | |||
| 08. Sep 21 | 17:30 | 18:00 | 10.9.4 |
FEEDBACK ERROR LEARNING WITH ENHANCED SAMPLING: NEURAL FAULT TOLERANT CONTROL OF AIRCRAFT N. Yoshikawa, University of Tokyo, Japan | |||
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| 08. Sep 21 | 16:00 | 16:30 | 11.9.1 |
IMPROVED DESIGN OF AIRCRAFT NOSEWHEEL STEERING SYSTEM L.-X. Xin, FAI AVIC, China | |||
| 08. Sep 21 | 16:30 | 17:00 | 11.9.2 |
NEW SOLUTION OF A DAMPER WITH A MAGNETORHEOLOGICAL ELASTOMER P. Skalski, Institute of Aviation, Poland | |||
| 08. Sep 21 | 17:00 | 17:30 | 11.9.3 |
INVESTIGATIONS ON LANDING GEAR SHOCK ABSORBER ACTIVE FORCE CONTROL Z. Skorupka, ?ukasiewicz Research Network - Institute of Aviation, Poland | |||
| 08. Sep 21 | 17:30 | 18:00 | 11.9.4 |
A STOCHASTIC ROBUSTNESS VERIFICATION OF NLG SIMPLE ADAPTIVE SHIMMY SUPPRESSION SYSTEM C. Orlando, Italy | |||
| Reserve Paper | 11.9.R |
STUDY ON THE DYNAMIC COUPLING CHARACTERISTICS OF AIRCRAFT LOW SPEED BRAKE ZHAO HAO, Shanghai Aircraft Design And Research Institute , China | |||||
| Reserve Paper | 11.9.R |
RESEARCH ON DESIGN OF HYDRAULIC ACCUMULATOR FOR A CIVIL AIRCRAFT BRAKE SYSTEM G.-C Zhang, Shanghai Aircraft Design and Research Institute, China | |||||
| Reserve Paper | 11.9.R |
A NOVEL OF CONTROL METHOD BASED ON PWM FOR HIGH_SPEED ON/OFF VALVES ARRAY OF AIRCRAFT BRAKE SYSTEMS Renjie Li Li, Beihang unversity, China | |||||
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| 08. Sep 21 | 16:00 | 16:30 | 12.9.1 |
INTEGRATION AND EVALUATION OF AN AIRCRAFT TAXIING SOLUTION USING AUTONOMOUS TOW TRUCKS J Gauci, University of Malta, Malta | |||
| 08. Sep 21 | 16:30 | 17:00 | 12.9.2 |
ERAS - EVALUATION OF REALISTIC APPROACH SCENARIOS FOR MINIMAL NOISE - PRELIMINARY FINDINGS B Moberg, Vernamack AB, Sweden; P Näsman, KTH Royal Institute of Technology, Sweden; U Ziverts, Infobahn AB, Sweden | |||
| 08. Sep 21 | 17:00 | 17:30 | 12.9.3 |
DESIGN AND TRIALING OF A CONCEPT OF OPERATIONS (CONOPS) FOR OPTIMAL CLIMBS AND DESCENTS INTO MEDIUM DENSITY AIRFIELDS D. Zammit-Mangion, University of Malta, Malta | |||
| 08. Sep 21 | 17:30 | 18:00 | 12.9.4 |
A NOVEL APPROACH FOR TURNAROUND TIME ALLOCATION BASED ON REINFORCEMENT LEARNING A. Rodriguez-Sanz, Universidad Politecnica de Madrid (UPM), Spain | |||
| Reserve Paper | 12.9.R |
OPERATION PLANNING AIDED METHOD OF GENERAL AIRCRAFT BASED ON MULTI-CBR AND COMBINATION EVALUATION METHOD R.-X. Xie, Beihang University, China | |||||
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| 08. Sep 21 | 16:00 | 16:30 | 13.9.1 |
FAILURE PROCESS IDENTIFICATION OF C-SIC WITH DIFFERENT TENSILE PERFORMANCE Y.Z. Zhang, Northwestern Polytechnical University, China | |||
| 08. Sep 21 | 16:30 | 17:00 | 13.9.2 |
INVESTIGATION OF STOPPER STRAPS EFFECTS ON LONGITUDINAL CRACK GROWTH RATES IN A SKIN OF PRESSURIZED AIRCRAFT FUSELAGE A.S. Kim, TsAGI, Russia | |||
| 08. Sep 21 | 17:00 | 17:30 | 13.9.3 |
INFLUENCE OF NOTCH EFFECTS ON STATIC CHARACTERISTICS OF STEEL BASED ON THERMOGRAPHIC METHOD Junling Fan¹, Pengfei Yang¹, Shaozheng Zhan¹; ¹Aircraft Strength Research Institute, China | |||
| 08. Sep 21 | 17:30 | 18:00 | 13.9.4 |
EXPERIMENTAL INVESTIGATION AND NUMERICAL SIMULATION OF SINGLE LAP JOINTS OF ALLOY-ARAMID FIBER COMPOSITE BASED ON COHESI ZTC Zou, Civil Aviation University of China, China | |||
| Reserve Paper | 13.9.R |
A MICROPHONE POSITION CALIBRATION METHOD FOR A RANDOM ARRAY Q He, China | |||||
| Reserve Paper | 13.9.R |
EXPERIMENTAL INVESTIGATION AND LIFE PREDICTION FOR DEFECT INDUCED CRACK OF A P/M NICKEL BASED SUPERALLOY SHI Y. SHI, Beihang University, China | |||||
Thursday, 09. Sep 2021
7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
| 0.8 | General Lecture 5 - IFAR contribution to sustainable aviation - can we achieve zero emission aviation? IFAR Chair, Sergey Chernychev IFAR Vice Chair, Ibrahim Ymer IFAR Past Chair, Michel Peters CAE, tbd NASA, tbd DLR, Rolf Henke Chair: D. Mavris ICAS PPSC Chair | |||
| 09. Sep 21 | 08:00 | 09:30 |
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| 09:30 - 10:00 | Break | |||
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| 09. Sep 21 | 10:00 | 10:30 | 1.10.1 |
COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN S. Görtz, DLR - German Aerospace Center, Germany | |||
| 09. Sep 21 | 10:30 | 11:00 | 1.10.2 |
ASSESSMENT OF NEW TECHNOLOGIES IN A MDAO ENVIRONMENT INCLUDING RAMS AND COST DISCIPLINES M. Fioriti, Politecnico di Torino, Italy | |||
| 09. Sep 21 | 11:00 | 11:30 | 1.10.3 |
INTERACTIONS BETWEEN MULTIFUNCTIONAL FLIGHT CONTROL SYSTEMS AND HIGH ASPECT RATIO WINGS IN A MID-RANGE AIRCRAFT O.B. Bertram, German Aerospace Center DLR, Germany | |||
| 09. Sep 21 | 11:30 | 12:00 | 1.10.4 |
MDAX: AGILE GENERATION OF COLLABORATIVE MDO WORKFLOWS A. Makus, German Aerospace Center (DLR), Germany | |||
| 09. Sep 21 | 12:00 | 12:30 | 1.10.5 |
BLENDED WING BODY PLANFORM MULTIDSCIPLIANRY OPTIMISATION Davide DI Pasquale¹, Divyam Verma¹, Giampaolo Pagliuca¹; ¹Cranfield University, United Kingdom | |||
| Reserve Paper | 1.10.R |
TOPOLOGY OPTIMIZATION FOR WING STRUCTURE OF HYPERSONIC VEHICLE S. Zhang, School of Aeronautical Science and Engineering, Beihang Universi, China | |||||
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| 09. Sep 21 | 10:00 | 10:30 | 3.10.1 |
TRANSITION PREDICTION FOR TRANSPORT AIRCRAFT CONFIGURATIONS BASED ON OVERSET GRID Y.-M. Du, Northwestern Polytechnical University, China | |||
| 09. Sep 21 | 10:30 | 11:00 | 3.10.2 |
A CONTRIBUTION TO THE SIMULATION OF TRANSITIONAL FLOWS OVER AEROSPACE CONFIGURATIONS J. L. F. Azevedo, Instituto de Aeronautica e Espaco, Brazil | |||
| 09. Sep 21 | 11:00 | 11:30 | 3.10.3 |
AERODYNAMICS CHARACTERISTICS STUDY ON A NATURE LAMINAR FLOW AIRFOIL OF NEAR-SPACE VEHICLE AT LOW REYNOLDS NUMBERS Cui Fei, China; Zhang Hongkun, China | |||
| 09. Sep 21 | 11:30 | 12:00 | 3.10.4 |
EFFECT OF THE WALL PROPERTIES ON THE SHOCK WAVE / LAMINAR BOUNDARY LAYER INTERACTION A. Kutepova, Khristianovich Institute of Theoretical and Applied Mechanics, Russia | |||
| 09. Sep 21 | 12:00 | 12:30 | 3.10.5 |
TURBOFAN NACELLE DESIGN WITH TAKING INTO ACCOUNT LAMINAR-TURBULENT TRANSITION A. A. Savelyev, Central Aerohydrodynamic Institute, Russia | |||
| Reserve Paper | 3.10.R |
HYBRID NUMERICAL SCHEMES IN PREDICTION OF HIGH-SPEED LAMINAR-TURBULENT TRANSITION I. Egorov, TsAGI, Russia | |||||
| Reserve Paper | 3.10.R |
INFLUENCE OF RAREFACTION FAN ON RECEPTIVITY OF SUPERSONIC BOUNDARY LAYER TO FREE STREAM ACOUSTIC DISTURBANCES N.V. Palchekovskaya, Moscow Institute of Physics and Technology, Russia | |||||
| Reserve Paper | 3.10.R |
A LOCAL CORRELATION-BASED ALGEBRAIC TRANSITION MODEL WITH COMPRESSIBILITY AND CROSS-FLOW CORRECTION R. X. Xie, Northwestern Polytechnical University, China | |||||
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| 09. Sep 21 | 10:00 | 10:30 | 4.10.1 |
MODELING AND SIMULATION OF DUSTY GAS FLOW IN AERODYNAMICS Yu.M. Tsirkunov¹, D.A. Romanyuk¹, S.V. Panfilov¹; ¹Baltic State Technical University, Russia | |||
| 09. Sep 21 | 10:30 | 11:00 | 4.10.2 |
STUDY ON AN IMPROVED PRECONDITIONING METHOD FOR MIXED COMPRESSIBLE AND INCOMPRESSIBLE FLOW L-H Huan, China Aerodynamics Research and Development Center, China | |||
| 09. Sep 21 | 11:00 | 11:30 | 4.10.3 |
STUDY OF UNSTEADY NUMERICAL SIMULATIONS BASED ON UNSTRUCTURED MESH DEFORMATION TECHNIQUE H.-Y. Liu, China | |||
| 09. Sep 21 | 11:30 | 12:00 | 4.10.4 |
2D INCOMPRESSIBLE FLOW SOLVER IN VELOCITY-VORTICITY FORMULATION USING DC-PSE OPERATOR DISCRETIZATION L. R. Zuhal, Institut Teknologi Bandung, Indonesia | |||
| 09. Sep 21 | 12:00 | 12:30 | 4.10.5 |
ASSESSMENT OF CFD/K-FWH HYBRID METHOD FOR HELICOPTER ROTOR NOISE PREDICTION J.-B. Fu, Politecnico di Milano, Italy | |||
| Reserve Paper | 4.10.R |
ON THE POSSIBILITY OF APPLYING THE HYPERSONIC SMALL-DISTURBANCE THEORY IN AERODYNAMIC STUDIES OF HIGH-SPEED AIRCRAFT A.A. Gubanov, Central Aerohydrodynamic Institute n.a. Prof. N.E. Zhukovsky, Russia | |||||
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| 09. Sep 21 | 10:00 | 10:30 | 5.10.1 |
BIRD STRIKE SIMULATIONS IN MSC.SOFTWARE: CORRELATION BETWEEN THE EXPERIMENTS AND SIMULATIONS V. Symonov¹, J. Juracka¹; ¹Brno University of Technology, Czech Republic | |||
| 09. Sep 21 | 10:30 | 11:00 | 5.10.2 |
MODELS AND METHODS FOR DRONE STRIKE LOAD PREDICTIONS F. F. Franke, Technische Hochschule Ingolstadt, Germany | |||
| 09. Sep 21 | 11:00 | 11:30 | 5.10.3 |
EXPERIMENTAL STUDY ON ATTENUATION PERFORMANCE OF SHOCK ABSORBING INSERT H.-S Park, South Korea | |||
| 09. Sep 21 | 11:30 | 12:00 | 5.10.4 |
MULTISCALE ANALYSIS OF BALLISTIC IMPACT OF WOVEN COMPOSITE MATERIALS D SONG, China | |||
| 09. Sep 21 | 12:00 | 12:30 | 5.10.5 |
DEVELOPMENT OF A PREDICTIVE METHODOLOGY FOR FAST ESTIMATION OF IMPACT BEHAVIOR IN AEROSPACE GRADE COMPOSITES K Carpenter, United States | |||
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| 09. Sep 21 | 10:00 | 10:30 | 7.10.1 |
BLADE - NATURAL LAMINAR FLOW FLIGHT TESTING T. Gibson, Airbus, United Kingdom | |||
| 09. Sep 21 | 10:30 | 11:00 | 7.10.2 |
METODICAL STUDIES OF THE POSSIBILITY TO APPLY A NUMERICAL METHOD WITH BUILT-IN EMPIRICAL CRITERIA FOR DETERMINING THE LA N.V. Voevodenko, TsAGI, Russia | |||
| 09. Sep 21 | 11:00 | 11:30 | 7.10.3 |
NATURAL-LAMINAR-FLOW AIRFOIL DESIGN OPTIMIZATION CONSIDERING CROSSFLOW INSTABILITY Z.-M Xu, Northwestern Polytechnical University, China | |||
| 09. Sep 21 | 11:30 | 12:00 | 7.10.4 |
DESIGN OF TRANSONIC NATURAL LAMINAR FLOW NACELLE C.Y. Yan, Tsinghua University, China | |||
| 09. Sep 21 | 12:00 | 12:30 | 7.10.5 |
THE NUMERICAL AND EXPERIMENTAL STUDIES ON LAMINAR WING SHORT RANGE AIRCRAFT WITH REDUCED COMMUNITY NOISE A.L. Bolsunovsky, Central Aerohydrodynamic Institute n.a. prof. N.E.Zhukovsky (TsA, Russia | |||
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| 09. Sep 21 | 10:00 | 10:30 | 8.10.1 |
METHODS TO CALCULATE THE STRUCTURE FATIGUE DAMAGE UNDER VARIOUS SPECTRA OF VIBRO-ACOUSTIC LOADS I.S. Sidorov, TsAGI, Russia | |||
| 09. Sep 21 | 10:30 | 11:00 | 8.10.2 |
FAILURE PROPERTIES AND MACROSCOPIC MODELLING OF AERONAUTIC RIVETED CONNECTIONS ZY Yifan, Civil Aviation University of China, China | |||
| 09. Sep 21 | 11:00 | 11:30 | 8.10.3 |
ITERATIVE GLOBAL/LOCAL NON-INTRUSIVE MODEL COUPLING METHOD FOR STRUCTURE FAILURE ANALYSIS Y.J. LIU, AVIC the first aircraft institute, China | |||
| 09. Sep 21 | 11:30 | 12:00 | 8.10.4 |
NUMERICAL ANALYSIS AND COMPARISON WITH RESULTS OF FRACTURE TESTS OF LUG MANUFACTURED IN COMPOSITE MATERIAL G. C. Fonseca, Embraer - Minas Gerais, Brazil | |||
| 09. Sep 21 | 12:00 | 12:30 | 8.10.5 |
EFFECT OF CENTER HOLE ON SHEAR STABILITY AND BEARING CAPACITY OF SHEET METAL FORMING PLATE W.L. LI, AVIC Shengyang Aircraft Design & Research Institute, China | |||
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| 09. Sep 21 | 10:00 | 10:30 | 9.10.1 |
STUDY ON OPTIMIZATION OF SPRAY CONE ANGLE OF THE COMBINED ATOMIZER BY SIMULATION AND EXPERIMENT C. Q. Cheng Cheng, Beijing Precision Engineering Institute For Aircraft Industr, China | |||
| 09. Sep 21 | 10:30 | 11:00 | 9.10.2 |
INVESTIGATION OF MEASUREMENT CHARACTERISTICS OF PROPAGATING FLAME BY MULTIPLE-ION-PROBE METHOD T.Y. Yatsufusa, Hiroshima Institute of Technology, Japan | |||
| 09. Sep 21 | 11:00 | 11:30 | 9.10.3 |
STUDY ON THE INFLUENCE OF A NEW GLIDING ARC PLASMA ACTUATOR ON THE PERFORMANCE IN AN AERO-ENGINE COMBUSTION CHAMBER Y CHEN, Air Force Engineering University, China | |||
| 09. Sep 21 | 11:30 | 12:00 | 9.10.4 |
METHODS OF CHOOSING THE PARAMETERS AND DESIGN OF THE HEAT EXCHANGERS OF AVIATION GAS TURBINE ENGINES (GTE) A. Revanth Reddy, Moscow Aviation Institute (National Research University), Russia | |||
| 09. Sep 21 | 12:00 | 12:30 | 9.10.5 |
HYBRID KERNEL FORMATION AND TRACKING METHOD TO PREDICT IGNITION LIMITS ON LOW EMISSION COMBUSTORS Wei Xiao, AECC Hunan Aviation Powerplant Research Institute, China; Yajun Cheng, HUNAN MECHANICAL & ELECTRICAL POLYTECHNIC, China; Ke Wang, Aero Engine Academy of China (AECC), China; Zhuyin Ren, Tsinghua University, China | |||
| Reserve Paper | 9.10.R |
NONLINEAR DYNAMICS MEASUREMENT OF SELF-SUSTAINED THERMOACOUSTIC INSTABILITIES IN A PREMIXED SWIRLING COMBUSTOR D. Zhao, University of Canterbury, New Zealand | |||||
| Reserve Paper | 9.10.R |
DECISION PROBLEMS IN AN IDENTIFICATION OF FACTORS INFLUENCING ON THE EMISSION OF HARMFUL COMPOUNDS OF TRANSPORT MEANS M. JACYNA, Warsaw University of Technology, Poland | |||||
| Reserve Paper | 9.10.R |
ATOMIZATION OF COAXIAL SWIRLING LIQUID SHEETS USING TRANSFORMING ALGORITHM X. Sun, Northwestern Polytechnical University, China | |||||
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| 09. Sep 21 | 10:00 | 10:30 | 10.10.1 |
NONLINEAR CONTROL STRATEGY FOR QUAD-TILTROTOR IN TRANSITION MODE K.W. Jang, KAIST, South Korea | |||
| 09. Sep 21 | 10:30 | 11:00 | 10.10.2 |
NONLINEAR FAULT-TOLERANT FLIGHT CONTROL WITH CONTROL ALLOCATION OF NASA GTM T-2 MODEL WITH DIFFERENT DAMAGE SCENARIOS B. Ergocmen, Middle East Technical University, Turkey | |||
| 09. Sep 21 | 11:00 | 11:30 | 10.10.3 |
MACHINE LEARNING TECHNIQUES FOR AIRCRAFT STALL DETECTION AND RECOVERY J Gauci, University of Malta, Malta | |||
| 09. Sep 21 | 11:30 | 12:00 | 10.10.4 |
AIRCRAFT AUTOPILOT DESIGN USING ASYMMETRIC VARIABLE-SPAN WING MORPHING J. Lee, Seoul National University, South Korea | |||
| 09. Sep 21 | 12:00 | 12:30 | 10.10.5 |
AUTONOMOUS FLIGHT CONTROL BASED ON NEURAL NETWORKS AND FUZZY DECISION P.C. Wen, AVIC Xi’an Aeronautics Computing Technique Research Institute, China | |||
| Reserve Paper | 10.10.R |
ANALYSIS OF REENTRY TRAJECTORY OPTIMIZATION OF COMPLEX PATH CONSTRAINTS USING HERMIT SPLINE INTERPOLATION Y Kwak, Konkuk Univ., South Korea | |||||
| Reserve Paper | 10.10.R |
TWISTOR BASED 6-DOF DISTRIBUTED ADAPTIVE LEADER-FOLLOWING CONTROL FOR MULTIPLE RIGID SPACECRAFT FORMATION B. Zhang, Northwestern Polytechnical University, China | |||||
| Reserve Paper | 10.10.R |
DEVELOPMENT OF A HUMAN PILOTED AIR COMBAT ENGAGEMENT DATABASE T.-X Xue, Fudan university, China | |||||
| Reserve Paper | 10.10.R |
LEARNING-BASED MIDCOURSE GUIDANCE FOR VELOCITY MAXIMIZATION WITH ANGULAR CONSTRAINT H Li, Beijing Institute of Technology, China | |||||
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| 09. Sep 21 | 10:00 | 10:30 | 11.10.1 |
OPTIMALPOWER DISTRIBUTION ON A MORE ELECTRIC AIRCRAFT E. D'Amato, Università degli studi della Campania "Luigi Vanvitelli", Italy | |||
| 09. Sep 21 | 10:30 | 11:00 | 11.10.2 |
CONCEPTUAL SYSTEM-LEVEL MODELING OF CONVENTIONAL AND MEA SYSTEMS ARCHITECTURES FOR MODERN MIDRANGE TRANSPORT AIRCRAFT M. Jünemann, Hamburg University of Technology, Germany | |||
| 09. Sep 21 | 11:00 | 11:30 | 11.10.3 |
ICE THICKNESS IMPACT AND DETECTION IN RESONANT ELECTROMECHANICAL DEICING SYSTEMS M. Budinger, INSA Toulouse, France | |||
| 09. Sep 21 | 11:30 | 12:00 | 11.10.4 |
ANTI-PUMP-FORCE-FIGHT PRESSURE CONTROLLER FOR A REDUNDANT HYDRAULIC POWER PACKAGE WITH SPEED VARIABLE AC MOTOR PUMPS N. Trochelmann, TUHH/ Institute of Aircraft Systems Engineering, Germany | |||
| 09. Sep 21 | 12:00 | 12:30 | 11.10.5 |
ON-BOARD SYSTEM ARCHITECTURES FOR HYBRID/ALL-ELECTRIC REGIONAL AIRCRAFT M. Fioriti, Politecnico di Torino, Italy | |||
| Reserve Paper | 11.10.R |
SURROGATE MODELS OF PM BRUSHLESS MOTORS FOR THE PRELIMINARY DESIGN OF AIRCRAFT APPLICATION SYSTEMS F De Giorgi, INSA/ICA Toulouse, France | |||||
| Reserve Paper | 11.10.R |
NUMERICAL SIMULATION OF DE-ICING PROCESS ON COMPOSITE AIRFOIL WITH ANISOTROPIC CONDUCTIVITY X.F Guo, Shanghai Jiao Tong University, China | |||||
| Reserve Paper | 11.10.R |
RESEARCH ON 18 PULSE AUTOTRANSFORMER RECTIFIER DEVICE FOR AVIATION WX.-C Chen, China | |||||
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| 09. Sep 21 | 10:00 | 10:30 | 12.10.1 |
MISSION CONTROL WITH REAL-TIME FLIGHT PATH PLANNING FOR TILTWING UAVS TO SUPPORT RESCUE OPERATIONS I. Barz¹, P. Hartmann, flyXdrive GmbH, Germany; N. Voget¹, S. Seitz¹, D. Moormann¹; ¹Institute of Flight System Dynamics, RWTH Aachen University, Germany | |||
| 09. Sep 21 | 10:30 | 11:00 | 12.10.2 |
PATH PLANNING OF UNINHABITED AERIAL VEHICLE BASED A MODIFIED ANT ALGORITHM Y.-F Feng, China | |||
| 09. Sep 21 | 11:00 | 11:30 | 12.10.3 |
CONFLICT RESOLUTION ADVISORIES BY UAS TRAFFIC MANAGEMENT SYSTEMS P. Hartmann, RWTH Aachen University, Germany | |||
| 09. Sep 21 | 11:30 | 12:00 | 12.10.4 |
TEMPLATE MATCHING BASED ON SEGMENTED AERIAL IMAGES FOR VISION-AIDED NAVIGATION K Hong, South Korea | |||
| 09. Sep 21 | 12:00 | 12:30 | 12.10.5 |
TERRAIN INFORMATION MEASURE FOR VISION-BASED MAP-REFERENCED NAVIGATION S. Kim, Korea Advanced Institute of Science and Technology, South Korea | |||
| Reserve Paper | 12.10.R |
A COMPARATIVE STUDY OF 3-D GRAPH-SEARCH ALGORITHMS FOR UAVS’ SHORTEST FLIGHT PATHS A. T. Nguyen, Le Quy Don Technical University, Vietnam | |||||
| Reserve Paper | 12.10.R |
3D TRAJECTORY DESIGN AND TRACKING FOR MULTIROTOR UAVS INDOOR FLIGHT E. Capello, Italy | |||||
| Reserve Paper | 12.10.R |
MULTI-UAV TRAJECTORY PLANNING BASED ON COORDINATION VARIABLES X. Z. Zheng, Beijing Institute of Technology, China | |||||
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| 09. Sep 21 | 10:00 | 10:30 | 13.10.1 |
CERTIFICATION CONSIDERATIONS FOR EVTOL AIRCRAFT Yingkang MOU¹, Mei JIANG¹; ¹Nanjing Engineering Institute of Aircraft Systems, China | |||
| 09. Sep 21 | 10:30 | 11:00 | 13.10.2 |
APPLICATION OF DEVELOPMENT ASSURANCE METHODOLOGIES TO ELECTRONIC ENGINE CONTROL SYSTEM (EECS) Q ZHU, AECC COMMERCIAL AIRCRAFT ENGINE CO., LTD., China | |||
| 09. Sep 21 | 11:00 | 11:30 | 13.10.3 |
RESEARCH ON AIRWOTHINESS CERTIFICATION OF CIVIL AVIATION PRODCUTS BASED ON RISK ANALYSIS C.-X Wang, AECC COMMERCIAL AIRCRAFT ENGINE CO., LTD, China | |||
| 09. Sep 21 | 11:30 | 12:00 | 13.10.4 |
STUDY ON THE AIRWORTHINESS AND COMFORTABLENESS REQUIREMENTS OF AIRCRAFT CABIN AIR CONTAMINATIONS Hu Tao Tao, CAPE?CAPE?, China | |||
| 09. Sep 21 | 12:00 | 12:30 | 13.10.5 |
CRASHWORTHINESS EVALUATION OF AIRCRAFT FUSELAGE BASED ON BUILDING BLOCK APPROACH C.-K Kun, Civil Aviation University of China, China | |||
| Reserve Paper | 13.10.R |
RESEARCH ON THE TRIGGERING CONDITIIONS OF EJECTABLE RECORDER FOR CIVIL AIRCRAFT Shumin Pu, Northwestern Polytechnical University, China | |||||
| Reserve Paper | 13.10.R |
NUMERICAL ANALYSIS METHOD OF CIVIL AIRCRAFT DITCHING FLOATING PERFORMANCE H WANG, China | |||||
| Reserve Paper | 13.10.R |
NUMERICAL STUDY OF DITCHING CHARACTERISTICS OF BWB AIRCRAFT SL.D. Ding, Beihang University, China | |||||
| 12:30 - 14:00 | Lunch | |||
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| 09. Sep 21 | 14:00 | 14:30 | 1.11.1 |
STUDY OF THE BENEFITS OF A SEMI-MORPHING WING CONCEPT L. P. Ruiz Calavera, Airbus Defence & Space, Spain | |||
| 09. Sep 21 | 14:30 | 15:00 | 1.11.2 |
FLIGHT EXPERIMENTS FOR THE ALTAIR SEMI-REUSABLE AIR-LAUNCH SYSTEM WITH THE DEMONSTRATOR EOLE J. Gauvrit-Ledogar, ONERA, France | |||
| 09. Sep 21 | 15:00 | 15:30 | 1.11.3 |
CIRCULATION CONTROL AIRCRAFT: RECENT DEVELOPMENTS OF THE CHANNEL-WING DESIGN HD Djojodihardjo, Retired Professor, Indonesia | |||
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| 09. Sep 21 | 14:00 | 14:30 | 2.11.1 |
IFAR (INTERNATIONAL FORUM FOR AVIATION RESEARCH) INFRASTRUCTURE DATABASE rd Degenhardt, DLR, Germany | |||
| 09. Sep 21 | 14:30 | 15:00 | 2.11.2 |
SOL-GEL BASED ORGANIC-INORGANIC HYBRID COATINGS FOR CORROSION PROTECTION OF AEROSPACE ALUMINIUM ALLOY R.V. Lakshmi, India | |||
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| 09. Sep 21 | 14:00 | 14:30 | 3.11.1 |
APPLICATION OF A SKEWED SLOT CASING TREATMENT IN A HIGH-LOADING AXIAL-CENTRIFUGAL COMPRESSOR H. L. JIN, China | |||
| 09. Sep 21 | 14:30 | 15:00 | 3.11.2 |
DISTORTION PLATE DESIGN, SIMULATION VALIDATION AND TEST SCHEME FOR STABILITY ANALYSIS ON A FAN COMPONENT OF AEROENGINE ZP.-L Li, AECC Shenyang Engine Design Institute, China | |||
| 09. Sep 21 | 15:00 | 15:30 | 3.11.3 |
EFFECT OF INTER-STAGE BLEEDING ON FLOW STABILITY OF A MULTI-STAGE COMPRESSOR X. W. LIU, China | |||
| Reserve Paper | 3.11.R |
DESIGN AND TEST OF A HIGH SLOPE ANGLE INTERMEDIATE DUCT BETWEEN AN AXIAL-CENTRIFUGAL LOW PRESSURE AND HIGH PRESSURE COMP H. L. JIN, China | |||||
| Reserve Paper | 3.11.R |
EFFECT OF HEAT LOAD AND INLET FLOW CONDITIONS OF COOLING AIR ON HEAT TRANSFER IN CHANNEL PASSAGE WITH PIN FINS P.-S. Peng, Xi’an Jiaotong University, China | |||||
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| 09. Sep 21 | 14:00 | 14:30 | 4.11.1 |
AERODYNAMIC AND AEROACOUSTIC INVESTIGATION OF THE FLOW PAST THE 30P30N HIGH-LIFT MULTI-AIRFOIL Yao Jin Jin, China | |||
| 09. Sep 21 | 14:30 | 15:00 | 4.11.2 |
AN INTELLIGENT STRUCTURED CHIMERA GRID APPROACH FOR MOVING OBJECTIVES L. L. Li, AVIC Aeronautics Computing Technique Research Institute, China | |||
| 09. Sep 21 | 15:00 | 15:30 | 4.11.3 |
SUN CODE: AN AUTOMATIC AND FAST FLOW SIMULATION TOOL FOR AIRCRAFT AERODYNAMIC DESIGN Mingzhe Sun¹, Rongting Lin¹, Dongrun Wu¹, Jender Lee¹, Xi Du¹, Dakai Lin¹; ¹COMAC BATRI, China | |||
| Reserve Paper | 4.11.R |
INVESTIGATION OF NUMERICAL METHOD OF INTERNAL FLOW AND OIL CAPTURE EFFICIENCY OF UNDER-RACE LUBRICATION J.-L. Jiang, Northwestern Polytechnical University, China | |||||
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| 09. Sep 21 | 14:00 | 14:30 | 5.11.1 |
VALIDATION OF SCALED FLIGHT TESTING - OVERALL APPROACH AND FIRST RESULTS P. Schmollgruber, France | |||
| 09. Sep 21 | 14:30 | 15:00 | 5.11.2 |
COMPARISON OF ESTIMATED AND ACTUAL AERODYNAMIC PERFORMANCE OF A 65KG UAV J. Bartasevicius, Technical University of Munich, Germany | |||
| 09. Sep 21 | 15:00 | 15:30 | 5.11.3 |
BIO-INSPIRED SWARM CONTROL OF DRONES USING SIMPLE INTERACTION RULES J Kikuchi, Graduate School of Tokai University, Japan | |||
| Reserve Paper | 5.11.R |
THE STUDY OF UNMANNED AERIAL VEHICLE FLYING QUALITIES FLIGHT TEST METHOD BASED ON TIME-DELAY EVALUATION S.J.-Q. QI, Chinese Flight Test Establishment , China | |||||
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| 09. Sep 21 | 14:00 | 14:30 | 6.11.1 |
RESEARCH ON CIVIL AIRCRAFT EQUIPMENT QUALIFICATION TEST G.-C Zhang, Shanghai Aircraft Design and Research Institute, China | |||
| 09. Sep 21 | 14:30 | 15:00 | 6.11.2 |
EXPERIMENTAL STUDY OF A LOOP HEAT PIPE FOR COOLING AIRCRAFT NACELLE ENGINE EQUIPEMENT V. Ayel, ISAE-ENSMA, France | |||
| 09. Sep 21 | 15:00 | 15:30 | 6.11.3 |
RESEARCH ON THE ENVIRONMENTAL WORTHINESS OF THE CIVIL AIRCRAFT USING THE FUZZY THEORY WITH THE TEST RESULT Z-H hui, Aircraft Strength Institute Research, China | |||
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| 09. Sep 21 | 14:00 | 14:30 | 7.11.1 |
NUMERICAL EVALUATION OF DYNAMIC STABILITY DERIVATIVES FOR HIGH LIFT DEVICES Aamir Sultan¹, Adnan Maqsood¹, Tiauw Hiong Go, Raytheon Missile Systems, United States; Rizwan Riaz¹; ¹National University of Sciences & Technology, Pakistan | |||
| 09. Sep 21 | 14:30 | 15:00 | 7.11.2 |
THE AERODYNAMIC OPTIMIZATION AND TRIM CHARACTERISTICS RESEARCH ON VARIABLE CAMBER WING OF WIDEBODY CIVIL TRANSPORT Cheng Su¹, Xuan Hao¹, Bin Wang¹, Qingqing Zhang¹; ¹China Academy of Aerospace Aerodynamics, China | |||
| 09. Sep 21 | 15:00 | 15:30 | 7.11.3 |
EFFECT OF CANARD DEFLECTION ON MAIN WING FOR A CLOSE-COUPLED-CANARD CONFIGURATION DURING PITCHING OSCILLATIONS Q. Chen, Beihang University, China | |||
| Reserve Paper | 7.11.R |
DESIGN OF VORTEX GENERATORS OF HYBRID SIZES OF AN AIRCRAFT HORIZONTAL TAIL Y. Liu¹, L. Ping¹, R. Zeng¹; ¹CETC Wuhu Diamond Aircraft Manufacture co., LTD, China | |||||
| Reserve Paper | 7.11.R |
ADJOINT-BASED STUDY OF THE AERODYNAMIC CENTER SHIFT IN THE TRANSONIC FLOW REGIME M. Hayashi, Federal University of ABC, Brazil | |||||
| Reserve Paper | 7.11.R |
NASA-CRM LATERAL-DIRECTIONAL STABILITY DERIVATIVES COMPARISON BETWEEN SEMI-EMPIRICAL, VORTEX LATTICE AND PANEL METHOD R.S. Sorbilli Cardoso de Sousa, Instituto Tecnológico de Aeronáutica, Brazil | |||||
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| 09. Sep 21 | 14:00 | 14:30 | 8.11.1 |
MULTIDIMENSIONAL FINITE ELEMENT MODELS FOR ADVANCED HELICOPTER BLADES M. Filippi, Politecnico di Torino, Italy | |||
| 09. Sep 21 | 14:30 | 15:00 | 8.11.2 |
MATHEMATICAL MODELS FOR OPTIMIZATION OF AIRCRAFT STRUCTURES TAKING INTO CONSIDERATION OF LOCAL STRESS DISTRIBUTION S. A. Tuktarov, Central aerohydrodynamic institute, Russia | |||
| 09. Sep 21 | 15:00 | 15:30 | 8.11.3 |
THE BEAM MODEL OF A HAWKMOTH WING STRUCTURE A. T. Nguyen, Le Quy Don Technical University, Vietnam | |||
| Reserve Paper | 8.11.R |
INVESTIGATION ON PERFORMANCE OF PCM-BASED ORTHOTROPIC COOLING PLATE FOR THERMAL MANAGEMENT OF AVIONICS MODULE. B. Wu, Aeronautical Computing Technique Research Institute, China | |||||
| Reserve Paper | 8.11.R |
A METHOD FOR CALCULATING TORSION ANGLE OF FLEXIBLE RETICULAR TUBE AT DIFFERENT POSITIONS DENG Yangchen, SADRI, China; YANG Yu, ASRI, China; HE Yuqing, SIA, China; SUN Cong, CAE, China; QIU Fusheng, SAU, China | |||||
| Reserve Paper | 8.11.R |
SPECIALIZED SOFTWARE DEVELOPMENT FOR BUILDING BLOCK APPROACH INTEGRATION IN FULL-SCALE STATIC TESTS D.V. Kurulyuk, FSUE TsAGI, Russia | |||||
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| 09. Sep 21 | 14:00 | 14:30 | 9.11.1 |
KEY TECHNOLOGIES FOR THE NEXT GENERATION OF CIVIL AIRCRAFT ENGINES F. Haselbach, United Kingdom | |||
| 09. Sep 21 | 14:30 | 15:00 | 9.11.2 |
DESIGN AND PERFORMANCE OF A LOW FAN-PRESSURE-RATIO PROPULSION SYSTEM R. Schnell, German Aerospace Center (DLR), Germany; E. Goldhahn, Airbus Operations GmbH, Germany; M. Julian, Airbus Operations SAS, France | |||
| 09. Sep 21 | 15:00 | 15:30 | 9.11.3 |
AN EXPERIMENTAL-NUMERICAL METHOD FOR TRANSIENT INFRARED MEASUREMENT OF FILM COOLING EFFECTIVENESS N.E. Holgate, United Kingdom | |||
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| 09. Sep 21 | 14:00 | 14:30 | 10.11.1 |
MODELING OF HELICOPTER FLIGHT DYNAMICS AND ROTOR BLADES LOADS DURING EXTREME FLIGHTS Grzegorz Kowalec Kowaleczko, Air Force Institute of Technology, Poland | |||
| 09. Sep 21 | 14:30 | 15:00 | 10.11.2 |
DESIGN TECHNIQUE OF INTEGRAL ALGORITHMS FOR HELICOPTER FBW CONTROL SYSTEM V.M. Kuvshinov, Central Aero-Hydrodynamics Institute, Russia | |||
| 09. Sep 21 | 15:00 | 15:30 | 10.11.3 |
AERODYNAMIC PERFORMANCE CALCULATION OF XH-59A HELICOPTER IN MANEUVERING PROCESS K. Y. You, Northwestern Polytechnical University, China | |||
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| 09. Sep 21 | 14:00 | 14:30 | 11.11.1 |
EVALUATION OF A GESTURE-BASED PILOT-AIRCRAFT INTERFACE IN A SIMULATION ENVIRONMENT M.A. Rodriguez Diaz, Instituto Tecnologico de Aeronáutica, Brazil | |||
| 09. Sep 21 | 14:30 | 15:00 | 11.11.2 |
ANALYSIS AND SOLUTION RESEARCH OF THE AIR DATA LOSS FROM AIRCRAFT FOR ENGINE CONTROL J LI, COMAC, China | |||
| 09. Sep 21 | 15:00 | 15:30 | 11.11.3 |
REAL-TIME GNSS PRECISE POINT POSITIONING AND VISUAL-INERTIAL ODOMETRY COUPLED NAVIGATION SYSTEM FOR UAVS C.-C. Cheng, SJTU, China | |||
| Reserve Paper | 11.11.R |
DESIGN OF UAV NAVIGATION ALGORITHM IN SINGLE SATELLITE ENVIRONMENT BASED ON HIGH PRECISION TIMING L.KT Li, China National Aeronautical Radio Electronics Research Institute, China | |||||
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| 09. Sep 21 | 14:00 | 14:30 | 12.11.1 |
ON-DEMAND AIR MOBILITY FOR BEIJING: PREREQUISITES FOR COMPETITIVENESS X. Sun, Beihang University, China | |||
| 09. Sep 21 | 14:30 | 15:00 | 12.11.2 |
AIRLINE NETWORK-AIRPLANE INTEGRATED OPTIMIZATION CONSIDERING MANUFACTURER\'S PROGRAM COST Mattos, B. S. Mattos, Instituto Tecnologico de Aeronautica (ITA), Brazil | |||
| 09. Sep 21 | 15:00 | 15:30 | 12.11.3 |
ASSESSMENT OF THREE COMMUTER AIRCRAFT CONCEPTS FROM A TRANSPORT SYSTEM PERSPECTIVE V. Papantoni, German Aerospace Center (DLR), Germany | |||
| Reserve Paper | 12.11.R |
AIR TRAFFIC MANAGEMENT OF DRONES INTEGRATED INTO SMART CITIES D. Rohacs, B udapest University of Tech. and econ.;, Hungary | |||||
| Reserve Paper | 12.11.R |
VERTIPORT PLACEMENT METHOD BASED ON MOBILITY SURVEY DATA K Lippoldt, Technische Universität München, Germany | |||||
| Reserve Paper | 12.11.R |
ASSESSING THE ENVIRONMENTAL IMPACT OF AIRCRAFT TAXIING TECHNOLOGIES AND STRATEGIES N/A BATRA, Institute of Aerospace Technologies, University of Malta, Malta | |||||
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| 09. Sep 21 | 14:00 | 14:30 | 13.11.1 |
DESIGN OF SIMULATION-BASED PILOT TRAINING SYSTEMS USING MACHINE LEARNING AGENTS J. Källström¹, R. Granlund, RISE SICS East, Sweden; F. Heintz¹; ¹Linköping University, Sweden | |||
| 09. Sep 21 | 14:30 | 15:00 | 13.11.2 |
A STUDY ON TRAINING NEEDS ANALYSIS (TNA) METHOD FOR MILITARY AIRCRAFT Q WANG, Chengdu Aircraft Design and Research Institute, AVIC, China | |||
| 09. Sep 21 | 15:00 | 15:30 | 13.11.3 |
COMPARISON OF READINESS TO PERFORM THE TASK OF AIRCRAFT USED FOR CADET TRAINING J. Tomaszewska, Polish Air Force University, Poland | |||
| Reserve Paper | 13.11.R |
INFORMATION DISTRIBUTION METHOD FOR MULTI-AIRCRAFT COOPERATION BASED ON COLLABORATIVE FILTERING ALGORITHM Y Wang, AVIC, China | |||||
| 15:30 - 16:00 | Break | |||
| 0.9 | von Karman Lecture - Active Flow-, Loads- and Noise Control on Next Generation Wing (AFLoNext) - M.Wahlich Chair: C. Atkin ICAS MRSC Chair | |||
| 09. Sep 21 | 16:00 | 17:00 |
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| 17:00 - 17:30 | Closing Ceremony | |||