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10:30 | 11:00 | 1.1.1 |
SMART CIVIL AVIATION TRANSPORTATION SYSTEM S. Yin, China | ||||
11:00 | 11:30 | 1.1.2 |
FLIGHT TEST ON THE ICING OF CIVIL AIRCRAFT Y. Chen, China | ||||
11:30 | 12:00 | 1.1.3 |
CURRENT PROGRESS AND FUTURE PROSPECTS OF CHINESE COMMERCIAL AIRCRAFT ENGINE DEVELOPMENT C. Shao, China |
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10:30 | 11:00 | 2.1.1 |
PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY Z.-L. Chen¹, Y.-C. Chen², S. Zhang, Beijing Aeronautical Science & Technology Research Institute, China; L.-X. Wang, Beihang University, China; Z.-G. Tan², B. Chen, AVIC Aerodynamics Research Institute, China; S.-W. Zhao, AVIC The First Aircraft Institute, China; L. Wang, AVIC Huiyang Aviation Propeller Co., LTD., China; J. Li¹, C.-S. Yuan¹, Y.-J. Zhang¹, Y.-Z. Zhang¹, W.-M. Sang¹, Y.-J. Tao¹, D. Li¹, B.-Q. Zhang¹; ¹Northwestern Polytechnical University, China ;²Shanghai Aircraft Design and Research Institute, COMAC, China | ||||
11:00 | 11:30 | 2.1.2 |
STUDY ON ADJOINT OPTIMIZATION OF BWB CONFIGURATION CONSIDERING THE INFLUENCE OF INTAKE AND EXHAUST SYSTEM J.-T. Huang¹, Z. Zhou¹, Z.-H. Gao, Northwestern Polytechnical University, China; X. Chen¹, S.-D. Zhong¹; ¹China Aerodynamics Research and Development Center, China | ||||
11:30 | 12:00 | 2.1.3 |
THE USE OF REVERSE ENGINEERING AND COMPUTATIONAL FLUID DYNAMICS METHODS IN THE PRELIMINARY DESIGN OF A LOW COST SATELLITE LAUNCH SYSTEM L. Kiszkowiak¹, A. Olejnik¹, A. Dziubinski, Lukasiewicz Research Network – Institute of Aviation, Poland; P. Zalewski¹; ¹Military University of Technology, Poland |
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10:30 | 11:00 | 3.1.1 |
RESEARCH ON OPTIMIZATION TECHNOLOGY FOR CONTROL PARAMETERS OF EJECTION SEAT BASED ON PSO ALGORITHM L. Jin¹, M. Wu¹, H. Yang¹, L. Wu¹, D. Cui, AVIC The First Aircraft Institute, China; ¹AVIC Aerospace Life-support Industries, Ltd., China | ||||
11:00 | 11:30 | 3.1.2 |
RESEARCH ON THE PRESSURE COMFORT OF PILOT HELMETS X.J. Wang¹, J. Xu¹, J.H. Wang¹, J.C. Mi, Intel Engineering Simulation Technology Co.,Ltd, China; Y.M. Jiang, Tiangong University, China; ¹Aerospace Life-support Industries LTD, China |
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10:30 | 11:00 | 4.1.1 |
NONLINEAR UNSTEADY AERODYNAMIC DESCRIPTIONS BASED ON IMPROVED GOMAN’S MODEL J. Yu¹, X.-J. Wu¹, D. Hao¹, H.-Y. Jia¹, S.-S. Liu¹; ¹CARDC, China | ||||
11:00 | 11:30 | 4.1.2 |
DATA FUSION UNSTEADY AERODYNAMIC MODELING BASED ON EXPERIMENTAL DATA X. Wang¹, W.W. Zhang¹; ¹Northwestern Polytechnical University, China | ||||
11:30 | 12:00 | 4.1.3 |
INVESTIGATION OF AERODYNAMIC INTERACTIONS BETWEEN NACA0012 AIRFOILS IN TANDEM M. Li, No.2 High School of East China Normal University, China; H. Xu, Fudan University, China |
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10:30 | 11:00 | 5.1.1 |
A DEEP-LEARNING-BASED METHOD FOR DAMAGE IDENTIFICATION OF COMPOSITE LAMINATES Y. Yang¹, B. Wang¹, S. Lv¹, Y. Zhou, Peking University, China; L. Wang¹, G. Liu¹; ¹Aircraft Strength Research Institute of ChinaAffiliation, China | ||||
11:00 | 11:30 | 5.1.2 |
IN-SITU LASER ASSISTED DIRECT IMPREGNATION, LAMINATION AND PLACEMENT OF CFRTP T. Ikeda, Chubu University, Japan; T. Sakai, Tottori University, Japan; A. Yokosu¹, Y. Fujii¹, H. Takenami¹, M. Arai¹, T. Ishikawa¹; ¹Nagoya University, Japan | ||||
11:30 | 12:00 | 5.1.3 |
A TWO PHASES COUPLING FREE AND POROUS FLOW NUMERICAL SIMULATION METHOD OF LCM PROCESS C. Li, China; C. Chen, China; L.M. Gao, China; J.F. Xu, China |
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10:30 | 11:00 | 6.1.1 |
COMPUTATIONAL STUDY OF THREE-DIMENSIONAL OPEN CAVITY FLOWS Y. Luo, China; C.H. Wu, China; S.Q. Yuan, China; H. Tian, China; H. Li, China; S.H. Zhang, China | ||||
11:00 | 11:30 | 6.1.2 |
EXPERIMENTAL STUDY ON SUPERSONIC CAVITY ACOUSTICS M. Jiang¹, M. Wang¹, F. He¹; ¹AVIC Chengdu Aircraft Design & Research Institute, China |
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10:30 | 11:00 | 7.1.1 |
SNGR BASED FAST ANALYSIS OF SLAT TRACK NOISE SOURCES W.H. Wang, China; Q.C. Wang, China; C. Breard, China; Y.F. Sun, China | ||||
11:00 | 11:30 | 7.1.2 |
AERODYNAMIC NOISE SIMULATION OF CIVIL AIRCRAFT LANDING GEARS BASED ON LES-SMARGORINSKY MODEL Q. Li, Chinese Aeronautical Establishment, China; P. Wang ¹, B. Chen ¹; ¹AVIC Aerodynamics Research Institute, China |
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10:30 | 11:00 | 8.1.1 |
RESEARCH ON ATTITUDE CONTROL AND CONSTRAINT SYSTEM DESIGN OF FULL-SCALE AIRCRAFT STATIC TEST BASED ON BARYCENTER J.-J. Zheng¹, B.-W. Wang¹, L.-G. Zhu, Shanghai Aircraft Design and Research Institute, China; J.-Y. Tang¹; ¹Aircraft Strength Research Institute of China, China | ||||
11:00 | 11:30 | 8.1.2 |
DESIGN OF A VERTICAL DITCHING TEST G. Nicolosi¹, F. Valpiani¹, G. Grilli¹, A. Saponaro Piacente¹, L. Di Ianni¹, E. Cestino¹, V. Sapienza¹, A. Polla, Aeronautical Consultant, Italy; P. Piana, TescoGo, Italy; ¹Politecnico di Torino, Italy | ||||
11:30 | 12:00 | 8.1.3 |
A SUBJECTIVE EVALUATION METHOD OF AIRCRAFT VIBRATION IN FLIGHT TEST H. Wang, COMAC Flight test Center, China |
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10:30 | 10:50 | 9.1.1 |
HOW CAN A CAMBER MORPHING WINGLET CONTRIBUTE TO MAKING AVIATION GREENER J.P. Eguea | ||||
10:50 | 11:10 | 9.1.2 |
A STUDY ON DEEP LEARNING BASED AUTOMATED AERIAL DOCKING SYSTEM J. Choi | ||||
11:10 | 11:30 | 9.1.3 |
TASK ALLOCATION ALGORITHMS FOR A COOPERATIVE DRONE PARCEL DELIVERY SYSTEM T.M.B. Bastos | ||||
11:30 | 12:00 | 9.1.3 |
UNPRECEDENTED TRANSITIONAL CHARACTERISTICS IN WAKE – BOUNDARY LAYER INTERACTION D. Veerasamy |
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10:30 | 11:00 | 10.1.1 |
DECOUPLING CONTROL LAW DESIGN FOR OBLIQUE-WING AIRCRAFT BASED ON EIGENSTRUCTURE ASSIGNMENT AND MODEL FOLLOWING L. Qiu, Chinese Flight Test Establishment, China; Z.H. Gao¹, Y. Liu¹; ¹Northwestern Polytechnical University, China | ||||
11:00 | 11:30 | 10.1.2 |
A REDUNDANT ADAPTIVE NAVIGATION METHOD BASED ON DYNAMIC PERFORMANCE EVALUATION FOR AEROSPACE VEHICLE T.-Y. Nie¹, R. Wang¹, J.-Y. Liu¹, Z. Xiong¹; ¹Nanjing University of Aeronautics and Astronautics, China |
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10:30 | 11:00 | 11.1.1 |
ON AIRCRAFT OPERATIONAL INTEGRITY Y. He, Air Force Engineering University, China | ||||
11:00 | 11:30 | 11.1.2 |
INTEGRATION OF SPACE VEHICLE OPERATIONS INTO THE UNITED ARAB EMIRATES AIR TRAFFIC MANAGEMENT - AN IMPACT ANALYSIS O. Lehmann¹, R. El-Jabi¹, K. Webster¹, A. Rachdi¹, Z. Malik¹; ¹Abu Dhabi University, United Arab Emirates |
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13:00 | 13:30 | 1.2.1 |
SHAPE MORPHING SMART STRUCTURES: MECHANICS, MATERIALS AND APPLICATIONS J. Leng, China | ||||
13:30 | 14:00 | 1.2.2 |
AN OVERVIEW OF HELICOPTER DEVELOPMENT IN CHINA AND SOME NEW HELICOPTER TECHNOLOGIES P. Xia, China | ||||
14:00 | 14:30 | 1.2.3 |
IMPLEMENTATION MECHANISM OF UAS INTEROPERABILITY BASED ON ARCHITECTURE META-MODEL X.H. Gao, China |
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13:00 | 13:30 | 2.2.1 |
AERODYNAMIC AND STRUCTURAL MODELING IN THE ROTORCRAFT MULTI-PHYSICS SIMULATION VAST J. Hofmann¹, M. Mindt¹, F. Weiss¹; ¹German Aerospace Center (DLR), Germany | ||||
13:30 | 14:00 | 2.2.2 |
HELICOPTER FLIGHT DYNAMICS MODELLING WITH FREE-WAKE METHOD EMBEDDED FOR ROTOR ICING ANALYSES G. Li, Chinese Aeronautical Establishment, China; G. Zhang¹, S. Chu¹; ¹Aviation Industry Development Research Center of China, China | ||||
14:00 | 14:30 | 2.2.3 |
TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55X L. Di Ianni¹, L. Loiodice¹, D. Celestini¹, D. Tiberti¹, C. Baldon¹, P. Iavecchia¹, A. Saponaro Piacente¹, M. Prodan¹, S. Grendene¹, B. Barberis¹, L. Santoro¹; ¹Politecnico di Torino, Italy |
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13:00 | 13:30 | 3.2.1 |
DYNAMIC PERFORMANCE ANALYSIS AND WEIGHTED-BASED FAULT DIAGNOSIS SCHEME FOR AIRCRAFT ELECTRIC POWER SYSTEM H. Li¹, Z. Zhao¹, Y. Zhang¹, S. Zhao¹, L. Xu¹; ¹Chengdu Aircraft Industrial (Group) Company Limited, China | ||||
13:30 | 14:00 | 3.2.2 |
INTEGRATED ON-BOARD NETWORKS FOR NEXT GENERATION AVIONICS E. Suvorova¹, V. Olenev¹; ¹St. Petersburg State University of Aerospace Instrumentation, Russia |
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13:00 | 13:30 | 4.2.1 |
NUMERICAL SIMULATIONS OF TRANSONIC BUFFET ON A HALF WING-BODY CONFIGURATION F. Sartor¹, M. Martin¹, C. Riveiro Moreno¹, J. Dandois¹; ¹ONERA, France | ||||
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 | ||||
14:00 | 14:30 | 4.2.3 |
NUMERICAL SIMULATION OF A BIO-INSPIRED FLEXIBLE FLAPPING-WING BASED ON EXPERIMENTAL MEASURED DEFORMATION X.-W. Yang¹, Y. Pei¹, W.-Q. Yang¹, P. Nian¹, B.-F. Song¹; ¹Northwestern Polytechnical University, China |
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13:00 | 13:30 | 5.2.1 |
THE NOISE REDUCTION STUDY OF COMPOSITE ACOUSTIC LINER ON HIGH BYPASS RATIO TURBOFAN AEROENGINE P. Hou¹, X.-J. Shang¹, Y. Dong¹; ¹Shenyang Aero Engine Research Institute, China | ||||
13:30 | 14:00 | 5.2.2 |
DYNAMIC RESPONSE AND DAMAGE OF THE FAN BLADES DURING UAV INGESTION INTO AN AERO-ENGINE N. Hou, China; X.H. Meng, China; J. Liu, China; Y.L. Li, China |
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13:00 | 13:30 | 6.2.1 |
VIBRATION INDUCED EXCITATION OF INSTABILITY WAVES IN A BLASIUS FLOW E.R. Gowree, ISAE-SUPAERO, France; C.J. Atkin, University of East Anglia, United Kingdom | ||||
13:30 | 14:00 | 6.2.2 |
STUDY ON THE STATISTICAL CHARACTERISTICS OF SKIN FRICTION OF SHOCK WAVE/ TURBULENT BOUDARY LAYER INTERATION IN A HOLLOW FLARE CONFIGURATION AT MACH 6 P.F. Shen ¹, H.Y. Cai, School of Aeronautics, Northwestern Polytechnical University, China; P.X. Liu¹, D. Sun¹, X.X. Yuan¹; ¹State Key Laboratory of Aerodynamics, China |
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13:00 | 13:30 | 7.2.1 |
ROBUST DESIGN OF 3D SHOCK CONTROL BUMPS TO TRANSPORT AIRCRAFT UNDER REALISTIC UNCERTAINTIES C. Sabater¹, S. Goertz¹; ¹German Aerospace Center (DLR), Germany | ||||
13:30 | 14:00 | 7.2.2 |
DRAG REDUCTION ANALYSIS IN CLOSE-FORMATION FLIGHT X.-X. Meng¹, M. Chang², J.-Q. Bai², M. Li¹; ¹School of Aeronautics, Northwestern Polytechnical University, China ;²Unmanned System Research Institute, Northwestern Polytechnical U, China | ||||
14:00 | 14:30 | 7.2.3 |
INCREASING THE EFFECTIVENESS OF AN AERODYNAMICALLY BALANCED CONTROL SURFACE ON A MODIFIED AIRFOIL WITH REDUCED DRAG V. Bogatyrev, TsAGI, Russia |
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13:00 | 13:30 | 8.2.1 |
STATIC AEROELASTIC TAILORING OF A HIGH-ASPECT-RATIO-WING FOR A SAILPLANE WITH A FORWARD MORPHING WING SECTION F. Sturm¹, G. Illenberger¹, D. Techmer¹, M. Hornung¹; ¹Technical University of Munich, Germany | ||||
13:30 | 14:00 | 8.2.2 |
AEROSERVOELASTIC OPTIMIZATION OF A HIGH ASPECT TRANSPORT WING WITH MORPHING TRAILING EDGE Z.-K. Zhang¹, Y.-J. Yang¹, S. Ricci², A. De Gaspari², C. Song¹, C. Yang¹; ¹Beihang University, China ;²Politecnico di Milano, Italy | ||||
14:00 | 14:30 | 8.2.3 |
A COMPREHENSIVE FRAMEWORK FOR THE COUPLED NONLINEAR AEROELASTIC AND FLIGHT DYNAMIC ANALYSES OF HIGHLY FLEXIBLE AIRCRAFT C. Zhang¹, X.F. Li¹, J.W. Chen¹, Z. Zhou², L. Qiao²; ¹Xi'an Modern Control Technology Research Institute, China ;²Northwestern Polytechnical University, China |
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13:00 | 13:30 | 9.2.1 |
HYBRID IGNITION PROBABILITY METHOD TO PREDICT THE IGNITION PERFORMANCE OF A GAS TURBINE COMBUSTOR W. Xiao, AECC Hunan Aviation Powerplant Research Institute, China; Y. Cheng, HUNAN MECHANICAL & ELECTRICAL POLYTECHNIC, China; K. Wang, Aero Engine Academy of China (AECC), China; Z. Ren, Tsinghua University, China | ||||
13:30 | 14:00 | 9.2.2 |
LARGE-EDDY SIMULATION OF A SWIRLING AVIATION KEROSENE SPRAY FLAME USING 3-COMPONENT SURROGATE FUELS K.D. Wan¹, Y.Z. Huang¹, Z.X. Gao¹, Y. He, Zhejiang University, China; C.W. Jiang¹; ¹Ningbo Institute of Technology, Beihang University, China |
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13:00 | 13:30 | 10.2.1 |
DECENTRALIZED CONFLICT DETECTION AND RESOLUTION METHOD ACCOUNTING FOR UNCERTAINTIES OF TRAJECTORIES N. Yokoyama, National Defense Academy of Japan, Japan | ||||
13:30 | 14:00 | 10.2.2 |
AN ALTERNATIVE BUT EQUIVALENT REALIZATION OF FINITE-HORIZON SUBOPTIMAL CONTROL FOR VEHICLE LANDING S. Zhang, China; X. Du, China; F. Liao, China; J.-T. Huang, China |
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13:00 | 13:30 | 11.2.1 |
DESIGN OF SIMULATION-BASED PILOT TRAINING SYSTEMS USING MACHINE LEARNING AGENTS J. Källström¹, R. Granlund, RISE SICS East, Sweden; F. Heintz¹; ¹Linköping University, Sweden | ||||
13:30 | 14:00 | 11.2.2 |
A STUDY ON TRAINING NEEDS ANALYSIS (TNA) METHOD FOR MILITARY AIRCRAFT Q. Wang¹, C. Sun¹, B. Hao¹; ¹ Chengdu Aircraft Design and Research Institute, AVIC, China | ||||
14:00 | 14:30 | 11.2.3 |
INFORMATION DISTRIBUTION METHOD FOR MULTI-AIRCRAFT COOPERATION BASED ON COLLABORATIVE FILTERING ALGORITHM Y.H. Wang, China; Z.J. Zhan, China; B. Xue, China; P.Y. Deng, China |
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15:00 | 15:30 | 1.3.1 |
TOWARDS AGILE SYSTEMS ENGINEERING: AN ITERATIVE & COLLABORATIVE APPROACH FOR COMPLEX SYSTEMS DEVELOPMENT D. Krob, France | ||||
15:30 | 16:00 | 1.3.2 |
DEPLOY SYSTEM ENGINEERING METHODS IN AIRBORNE GUIDANCE NAVIGATION CONTROL DOMAIN F. Wu, China | ||||
16:00 | 16:30 | 1.3.3 |
MODEL BASED DESIGN AND PRACTICE FOR AVIONICS SYSTEM L. Gao, China |
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15:00 | 15:30 | 2.3.1 |
ICAS DIGITAL PIONEERING INITIATIVE AND FUTURE PERSPECTIVES ON MDO & MBSE P.D. Ciampa, Germany | ||||
15:30 | 16:00 | 2.3.2 |
FUTURE PERSPECTIVES ON KBE & AI G. La Rocca, Netherlands | ||||
16:00 | 16:30 | 2.3.3 |
FUTURE PERSPECTIVES ON VR & AR S. Bagassi, Italy | ||||
16:30 | 17:00 | 2.3.4 |
FUTURE PERSPECTIVES ON SOSE C. Jouannet, Sweden |
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15:00 | 15:30 | 3.3.1 |
RESEARCH ON THE ENVIRONMENTAL WORTHINESS OF THE CIVIL AIRCRAFT USING THE FUZZY THEORY H. Zhang¹, J.T. Wu¹, P.Q. Tian¹, Z.P. Ren¹; ¹Aircraft Strength Research Institute of China, China | ||||
15:30 | 16:00 | 3.3.2 |
EXPERIMENTAL STUDY OF THE DYNAMICS CHARACTERISTICS OF AN IMPACT WATER DROPLET ON SUPERHYDROPHOBIC SURFACE J.X. Wang¹, C.L. Zhu¹, Z. Yang¹, C.X. Zhu, Nanjing University of Aeronautics and Astronautics,, China; ¹Nanjing University of Aeronautics and Astronautics, China | ||||
16:00 | 16:30 | 3.3.3 |
STUDY ON CLOSED-LOOP CROSS COMPENSATION CONTROL TECHNOLOGY IN ACCELERATED FATIGUE TESTING H. Zhao, Aircraft Strength Research Institute of China, Xi’an jiaotong Un, China; H. Tao¹, Z. Gu, Chongqing Hongyu Precision Industrial Co., Ltd., China; G. Shi, Shenyang Aircraft Design & Research Institute of China, China; S. Duan¹, J. Feng¹; ¹Aircraft Strength Research Institute of China, China | ||||
16:30 | 17:00 | 3.3.4 |
RESEARCH AND VALIDATION OF SYSTEM MODELING AND SIMULATION OF INTAKE AIR MIXER ALTITUDE TEST BED F. Wu, Northwestern Polytechnical,AECC Sichuan Gas Turbine Establishmen, China; X.-D. Feng¹, L.-T. Leng¹, T. Liu¹, C.-Q. Yang¹; ¹AECC Sichuan Gas Turbine Establishment, China |
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15:00 | 15:30 | 4.3.1 |
ON THE ASSESSMENT OF CFD METHODS FOR VORTICAL FLOWS R.C. Gonzalez, Cranfield Unversity, United Kingdom; S.A. Prince, Cranfield University, United Kingdom | ||||
15:30 | 16:00 | 4.3.2 |
RESEARCH OF TURBULENCE MODELING BASED ON MACHINE LEARNING Y.-H. Yin¹, Y.-F. Zhang¹; ¹Tsinghua University, China | ||||
16:00 | 16:30 | 4.3.3 |
TURBULENCE MODEL ASSESSMENT OF THE SEPARATED FLOW IN THE STANFORD DIFFUSER M. Bonnici¹, S. Prince¹, K. Garry¹; ¹Cranfield University, United Kingdom | ||||
16:30 | 17:00 | 4.3.4 |
RESEARCH OF THE HYPERSONIC BOUNDARY LAYER INSTABILITIES AND TRANSITION WITH THERMAL-CHEMICAL NON-EQUILIBRIUM EFFECTS X.L. Chen¹, F. Song¹; ¹Tsinghua University, China |
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15:00 | 15:30 | 5.3.1 |
STUDY OF COMPOSITE SKIN-STRINGER FATIGUE BEHAVIOR UNDER BROADBAND RANDOM VIBRATION S. Dubinskii¹, F. Sevastyanov¹, V. Kostenko¹, S. Denisov¹, I. Zharenov¹; ¹The Central Aerohydrodynamic Institute (TsAGI), Russia | ||||
15:30 | 16:00 | 5.3.2 |
MODEL CURVES: A SIMPLE WAY TO ACCOUNT FOR COMPLEX EFFECTS A. Bautin¹, Y. Svirsky¹, V. Basov¹, Y. Melnikov¹; ¹1Central Aerohydrodynamic Institute (TsAGI), Russia | ||||
16:00 | 16:30 | 5.3.3 |
A DIGITAL EQUIVALENT DEVELOPMENT FOR FATIGUE AND DAMAGE TOLERANCE IN AIRCRAFT STRUCTURES L. Zaplana Manzano¹, J. Romero Arana¹, J. Gómez-Escalonilla Martín¹; ¹AIRBUS DS, Spain | ||||
16:30 | 17:00 | 5.3.4 |
FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSURE S. Olsson, Quintus Technologies AB, Sweden; B. Carlsson¹, M. Bergkvist, Quintus Teachnologies AB, Sweden; R. He¹; ¹Quintus Technologies, China |
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15:00 | 15:30 | 6.3.1 |
HIGH-LIFT NOISE REDUCTION USING PLASMA ACTUATORS G.P.G. Silva¹, J.P. Eguea¹, J.A.G. Croce, Federal Institute of Education, Science and Technology of São Pa, Brazil; F.M. Catalano¹; ¹Department of Aeronautical Engineering, University of São Paulo, Brazil | ||||
15:30 | 16:00 | 6.3.2 |
ENERGY HARVESTING FROM PIEZOELECTRIC FRINGES AT THE TRAILING-EDGE OF A FINITE WING WITH LEADING-EDGE TUBERCLES E.P. Pereira¹, A. Esmaeili, Ferdowsi University of Mashhad, Iran; J.M.M. Sousa¹; ¹Instituto Superior Técnico, Portugal | ||||
16:00 | 16:30 | 6.3.3 |
SUBSONIC WIND TUNNEL SMALL RIBLETS DRAG REDUCTION EXPERIMENT ON C919 FUSELAGE MODEL H.W. Wang¹, Z. Huang¹, M.L. Yuan¹, X.H. Li¹, M. Zhang, Shanghai Aircraft Design and Research Institute, China; ¹China Academy of Aerospace Aerodynamics, China | ||||
16:30 | 17:00 | 6.3.4 |
HYBRID LAMINAR FLOW CONTROL (HLFC) RESEARCH AT AIRCRAFT RESEARCH ASSOCIATION (ARA), PAST, PRESENT AND FUTURE P.W.C. Wong, IHS Markit ESDU, United Kingdom; M. Maina¹, S. Lawson¹; ¹ARA, United Kingdom |
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15:00 | 15:30 | 7.3.1 |
PROPELLER WAKE - OBJECT INTERACTION USING A FREE WAKE MODEL UTILIZING LOCAL MESH SEPARATION M. Thiele¹, D. Salassidis¹, M. Hornung¹; ¹Institute of Aircraft Design, Technical University of Munich, Germany | ||||
15:30 | 16:00 | 7.3.2 |
NUMERICAL STUDY OF QUAD-ROTOR AIRCRAFT PERFORMANCE UNDER ADVERSE SITUATIONS T. Wan¹, M.-H. Tsai¹; ¹Tamkang Univ., Taiwan, China | ||||
16:00 | 16:30 | 7.3.3 |
AERODYNAMIC ANALYSIS OF A HIGH SPEED TEST RIG FOR USE IN ENGINE TEST FACILITIES F. Rasimarzabadi¹, M. Neuteboom¹, C. Clark¹, H. Martensson, GKN Aerospace Engine Systems, Sweden; ¹NRC, Canada |
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15:00 | 15:30 | 8.3.1 |
BIRD STRIKE SIMULATIONS IN MSC.SOFTWARE: CORRELATION BETWEEN THE EXPERIMENTS AND SIMULATIONS V. Symonov¹, J. Juracka¹; ¹Brno University of Technology, Czech Republic | ||||
15:30 | 16:00 | 8.3.2 |
MODELS AND METHODS FOR DRONE STRIKE LOAD PREDICTIONS F. Franke¹, U. Burger¹, C. Hühne, DLR, Germany; ¹Technische Hochschule Ingolstadt, Germany | ||||
16:00 | 16:30 | 8.3.3 |
EXPERIMENTAL STUDY ON ATTENUATION PERFORMANCE OF SHOCK-ABSORBING INSERT H.-S. Park¹, D.-H. Hwang¹, J. Yang, University of Washington, United States; J.-H. Han¹; ¹KAIST, South Korea | ||||
16:30 | 17:00 | 8.3.4 |
REVIEW OF PREDICTIVE METHODS FOR CAPTURING ONSET OF DAMAGE AND INITIAL DELAMINATION IN CARBON FIBRE REINFORCED POLYMER LAMINATES SUBJECT TO IMPACT H. Raza¹, O. Rodera Garcia², K. Carpenter¹, T. Pärnänen², J. Jokinen², M. Kanerva², J. Bayandor¹; ¹CRASH Lab, University at Buffalo, United States ;²Tampere University , Finland |
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15:00 | 15:30 | 9.3.1 |
THE USE OF SOFTWARE “VIRTUAL ENGINE” FOR TIMELY GAS-TURBINE ENGINE FAULT LOCALIZATIONS F.D. Golberg¹, M.P. Sokolov¹, V.E. Volkov¹, A.A. Petukhov¹; ¹Central Institute of Aviation Motors, Russia | ||||
15:30 | 16:00 | 9.3.2 |
AN IMPROVED IDENTIFICATION METHOD FOR ACTUATOR LOOP OF AIRCRAFT ENGINE CONTROL SYSTEM N. Liu, Shanghai Aircraft Design & Research Institute, Commercial Aircra, China | ||||
16:00 | 16:30 | 9.3.3 |
METHODS OF PROGRAMMED THRUST MANAGEMENT FOR NOISE REDUCTION OF SUPERSONIC CIVIL AIRCRAFT A. Mirzoyan¹, I. Khaletskii¹; ¹CIAM, Russia | ||||
16:30 | 17:00 | 9.3.4 |
RESEARCH ON CIVIL AIRCRAFT POWERPLANT SYSTEM EICAS MESSAGES DESIGN APPROACH Y. Shang, Shanghai Aircraft Design and Research Institute, China |
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15:00 | 15:30 | 10.3.1 |
SYSTEM ARCHITECTURE DESIGN SPACE MODELING AND OPTIMIZATION ELEMENTS J.H. Bussemaker¹, P.D. Ciampa¹, B. Nagel¹; ¹DLR, Germany | ||||
15:30 | 16:00 | 10.3.2 |
AIRCRAFT CRUISE PERFORMANCE DESIGN INTEGRATION BASED ON SYSTEM ENGINEERING H. Bihai¹, H. Zhen¹; ¹COMAC, China | ||||
16:00 | 16:30 | 10.3.3 |
RESEARCH ON AERO-ENGINE COLLABORATIVE DESIGN PROCESS BASED ON SYSTEM ENGINEERING Y.-G. Chai¹, J. Tao¹, S.-P. Guo¹; ¹AECC Commercial Aero Engine co. LTD, China | ||||
16:30 | 17:00 | 10.3.4 |
STRATEGIES TO ENHANCE CONFIGURATIONS FOR HIGH-PRECISION MULTI-DISCIPLINARY OPTIMIZATION H. Liu¹, M. Li¹, R. Zhu¹, Q. Ding², L. Zhou²; ¹Science and Technology on Electro-optic Control Laboratory, China ;²Beijing Institute of Technology, China |
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15:00 | 15:30 | 11.3.1 |
RESEARCH ON SAFETY ASSESSMENT APPROACH FOR UAS OPERATIONS OVER UNINHABITED AREAS Q. Zhang¹, Z. Zhou¹; ¹Northwestern Polytechnical University, China | ||||
15:30 | 16:00 | 11.3.2 |
EXPERIMENTAL STUDY ON CRITICAL HEAT FLUX CHARACTERISTICS OF R134A FLOW BOILING IN A HORIZONTAL 2.1 MM TUBE UNDER HYPERGRAVITY J.J. Han, Nanjing engineering Institute of Aircraft System, Jincheng, AVIC, China; G. Li, Nanjing University of Aeronautics and Astronautics, China | ||||
16:00 | 16:30 | 11.3.3 |
ULTRASONIC DE-ICING SYSTEM DESIGN METHODS BASED ON RESONANCE AND IMPEDANCE MATCHING B. Miao¹, M.-X. Bao¹, C.-L. Zhu¹; ¹Nanjing University of Aeronautics and Astronautics, China | ||||
16:30 | 17:00 | 11.3.4 |
A NUMEIRCAL PREDICTION OF THE AIRCRAFT ICING METEOROLOGICAL ENVIRONMENT Q.-L. Guo¹, W.-M. Sang¹, J.-J. Niu¹, A.-X. Qiu¹; ¹Northwestern Polytechnical University, China |
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08:00 | 08:30 | 1.4.1 |
APPLICATION OF ARTIFICIAL NEURAL NETWORKS FOR EFFICIENT RELIABILITY-BASED DESIGN OPTIMIZATION X. Chen¹, A. Riaz¹, S. El Fassi¹; ¹Cranfield University, United Kingdom | ||||
08:30 | 09:00 | 1.4.2 |
VALIDATING SURROGATE MODELS AND ICORPORATING UNCERTAINTY QUANTIFICATION IN MULTI-ELEMENTS AIRFOIL DESIGN OPTIMISATION D. Di Pasquale¹, C. Bolart¹; ¹Cranfield University, United Kingdom | ||||
09:00 | 09:30 | 1.4.3 |
EFFICIENT ADAPTIVE SURROGATE-BASED OPTIMIZATION USING FUZZY CLUSTERING FOR COMPLEX SYSTEM OPTIMIZATIONS C. Li¹, W. Ji¹, C. Gong¹, H. Fang, Shanghai Electro-Mechanical Engineering Institute, China; ¹Northwestern Polytechnical University, China | ||||
09:30 | 10:00 | 1.4.4 |
A NOVEL RBF DATA TRANSFER METHOD BASED ON PCA GEOMETRIC FEATURE EXTRACTION S.S. Liu¹, Q. You¹, Z.K. Liu², X. Liu², Y.W. Gui²; ¹State Key Laboratory of Aerodynamics, China ;²China Aerodynamics Research and Development Center, China |
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08:00 | 08:30 | 2.4.1 |
H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS N. Viola¹, R. Fusaro¹, D. Ferretto¹, O. Gori¹, B. Saracoglu², A.C. Ispir², C. Schram², V. Grewe³, J.F. Plezer³, J. Martinez³, M. Marini*, L. Cutrone*, G. Saccone*, S. Hernandez, University of La Coruna, Spain; K. Lammers, Netherlands Aerospace Centre, Netherlands; A. Vincent, The French Aerospace Lab ONERA, France; D. Hauglustaine, CNRS, France; B. Liebhardtº, F. Linkeº, D. Bodmerº; ¹Politecnico di Torino, Italy ;²Von Karman Institute for Fluid Dynamics, Belgium ;³Deutsches Zentrum für Luft- und Raumfahrt, Germany ;*Centro Italiano Ricerche Aerospaziali, Italy ;ºTechnical University of Hamburg Harburg, Germany | ||||
08:30 | 09:00 | 2.4.2 |
THERMAL PROTECTION SYSTEM PRELIMINARY DESIGN OF STRATOFLY HIGH-SPEED PROPELLED VEHICLE R. Scigliano¹, V. De Simone¹, M. Marini¹, R. Fusaro², D. Ferretto², N. Viola²; ¹Italian Aerospace Research Centre (CIRA), Italy ;²Politecnico di Torino (PoliTO), Italy | ||||
09:00 | 09:30 | 2.4.3 |
AERODYNAMIC DESIGN THEORY AND METHODOLOGY FOR AN AIRFRAME-INLET INTEGRATED FULL-WAVERIDER VEHICLE F. Ding¹, J. Liu¹, W. Huang¹, S. Guo, Air Force Engineering University, China; ¹National University of Defense Technology, China | ||||
09:30 | 10:00 | 2.4.4 |
INTEGRATION OF AN INCREASING-FIDELITY AERODYNAMIC MODELLING APPROACH IN THE CONCEPTUAL DESIGN OF HYPERSONIC CRUISER R. Fusaro¹, O. Gori¹, D. Ferretto¹, N. Viola¹, P. Roncioni², M. Marini²; ¹Politecnico di Torino, Italy ;²CIRA, Italy |
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08:00 | 08:30 | 3.4.1 |
MULTIROTOR VEHICLES DESIGN BASED ON DYNAMIC MANIPULABILITY FOR UNDERACTUATED FLYING SYSTEMS Y. Matsumura¹, M. Bando¹, S. Hokamoto¹; ¹Kyushu Univ., Japan | ||||
08:30 | 09:00 | 3.4.2 |
LANDING SYSTEM USING EXTENDED DYNAMIC WINDOW APPROACH FOR FIXED-WING UAV S. Ishioka¹, K. Uchiyama¹, K. Masuda¹; ¹Nihon University, Japan | ||||
09:00 | 09:30 | 3.4.3 |
OPTIMIZATION OF LONGITUDINAL CONTROL OF AN AGRICULTURAL UAV USING LQR-PID CONTROL A. Gomes Pereira Sarmento¹, A. Giacobini de Souza¹, A. Muniz Neves, CENIC Aeronáutica, Brazil; L.C. Sandoval Góes¹, R. Gil Annes da Silva¹; ¹Instituto Tecnológico de Aeronáutica (ITA), Brazil |
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08:00 | 08:30 | 4.4.1 |
MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF A CIVIL AIRCRAFT FUSELAGE S.V. Rohani¹, A. Jahangirian¹; ¹Amirkabir University of Technology, Iran | ||||
08:30 | 09:00 | 4.4.2 |
OPTIMISATION OF VORTEX GENERATORS FOR STALL SPEED REDUCTION J. Meyer¹, P. Okfen¹, C. Bil¹; ¹RMIT University, Australia | ||||
09:00 | 09:30 | 4.4.3 |
MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF A CIVIL AIRCRAFT WINGLET M. Heidari Soreshjani, Amirkabir University of Technology, Iran; A. Jahangirian, Amirkabir university of technology, Iran | ||||
09:30 | 10:00 | 4.4.4 |
OPTIMAL DESIGN OF A NEXT GENERATION HIGH-LIFT REUSABLE RE-ENTRY VEHICLE A. Aprovitola, University of Campania , Italy; L. Iuspa¹, G. Pezzella¹, A. Viviani¹; ¹University of Campania, Engineering Department., Italy |
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08:00 | 08:30 | 5.4.1 |
IMPACT OF ENROUTE TIME-BASED METERING ON EQUITY IN DELAY DISTRIBUTION A. Andreeva-Mori¹, Y. Matsuno¹; ¹Japan Aerospace Exploration Agency, Japan | ||||
08:30 | 09:00 | 5.4.2 |
ARTIFICIAL INTELLIGENCE AND HUMAN-MACHINE INTERACTIONS FOR STREAM-BASED AIR TRAFFIC FLOW MANAGEMENT P. Lertworawanich¹, N. Pongsakornsathien¹, Y. Xie¹, A. Gardi¹, R. Sabatini¹; ¹RMIT University, Australia | ||||
09:00 | 09:30 | 5.4.3 |
RESEARCH ON TRAJECTORY OPTIMIZATION TECHNOLOGY CONSIDERING METEOROLOGICAL INFORMATION PREDICTION W. Guo¹, R.Y. Zhang¹; ¹China National Aeronautical Radio Electronics Research Institute, China | ||||
09:30 | 10:00 | 5.4.4 |
POINT MERGE SYSTEM AND ARRIVAL METERING SYNERGY EFFECT ESTIMATION OF INBOUND FLIGHT EFFICIENCY AT TOKYO INTERNATIONAL (HANEDA) AIRPORT T. Mori, Osaka Prefecture University, Japan |
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08:00 | 08:30 | 6.4.1 |
EXPERIMENTAL INVESTIGATION, NUMERICAL AND MATHEMATICAL SIMULATION OF DISPERSE FLOWS IMPINGING ON AIRCRAFT SURFACE I.A. Amelyushkin¹, M.A. Kudrov¹, A.B. Miller¹, Y.F. Potapov¹, A.L. Stasenko¹, V.A. Zhbanov¹; ¹Central Aerohydrodynamic Institute, Russia | ||||
08:30 | 09:00 | 6.4.2 |
MODIFICATION OF TURBULENCE MODELS FOR PRESSURE-INDUCED SEPARATION ON SMOOTH SURFACES USING THE DLR VICTORIA EXPERIMENT T. Knopp¹, M. Novara¹, D. Schanz¹, W. Lühder¹, E. Schülein¹, R. Geisler¹, F. Philipp¹, M. Schroll², A. Krumbein¹, C. Willert², A. Schröder¹; ¹DLR AS, Germany ;²DLR AT, Germany | ||||
09:00 | 09:30 | 6.4.3 |
SINGULARITIES IN THE NEAR-WALL REGION OF 3D BOUNDARY LAYER AND THE FLOW STRUCTURE IN ITS VICINITY V.I. Shalaev, Moscow Institute of Physics and Technology, Russia |
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08:00 | 08:30 | 7.4.1 |
ESTIMATION OF THREE-DIMENSIONAL BOUNDARY LAYER VELOCITY PROFILES ON SWEPT WINGS AND BLENDED WING BODIES K. Ma¹, S. Prince¹; ¹Cranfield University, United Kingdom | ||||
08:30 | 09:00 | 7.4.2 |
NUMERICAL INVESTIGATION ON FLOW INTERFERENCE BETWEEN BLENDED-WING-BODY AIRCRAFT AND OVERHANGING NACELLE A.X. Qiu¹, W.M. Sang¹, R. Pang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | ||||
09:00 | 09:30 | 7.4.3 |
AN OPTIMIZATION OF ANTI-ICING CHAMBER BASED ON POD AND KRIGING J. Niu¹, W. Sang¹, A. Qiu¹, Q. Guo¹, D. Li¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | ||||
09:30 | 10:00 | 7.4.4 |
NUMERICAL INVESTIGATION OF THE EFFECT OF WALL TEMPERATURE ON THERMAL ENVIRONMENT OF TWO-DIMENSIONAL TRANSVERSE GAP B. Qiu, State Key Laboratory of Aerodynamics, China Aerodynamic Research, China; R. Li, Computational Aerodynamics Institute China Aerodynamic Research, China; X. Liu¹, J. Yao¹, B. Jiang¹, Y. Zhu, School of Chemical Engineering, China; ¹Computational Aerodynamics Institute, China Aerodynamic Research, China |
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08:00 | 08:30 | 8.4.1 |
COMPUTATIONAL FLUID-STRUCTURE INTERACTIONS OF A 3D FLEXIBLE FLAPPING WING Y. Guo¹, W. Yang¹, Y. Dong¹, X. Lang¹; ¹Northwestern Polytechnical University, China | ||||
08:30 | 09:00 | 8.4.2 |
FLUID-STRUCTURE INTERACTION ANALYSIS OF ELASTIC EFFECTS OF A TRANSPORT AIRCRAFT FITTED WITH WINGLETS W.M. Alves, Embraer, Brazil; B.S. Mattos¹, J.A. Hernandes¹; ¹ITA, Brazil | ||||
09:00 | 09:30 | 8.4.3 |
EFFECTS OF ELASTICITY, VISCOSITY AND BOUNDARY LAYER TRANSITION ON AEROELASTICITY CHARACTERISTICS OF LAMINAR WINGS S. Kuzmina¹, F. Ishmuratov¹, O. Karas¹; ¹TsAGI, Russia | ||||
09:30 | 10:00 | 8.4.4 |
AEROELASTIC RESPONSE CALCULATION USING DUHAMEL INTEGRAL AND ITS APPLICATIONS L. Bortolotto¹, R.G.A. Silva¹, M.H.J. Pedras, Embraer, Brazil; ¹Instituto Tecnológico de Aeronáutica, Brazil |
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08:00 | 08:30 | 9.4.1 |
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 | ||||
08:30 | 09:00 | 9.4.2 |
ANALYSIS OF AERODYNAMIC CHARACTERISTICS OF PROPELLER AT LOW ADVANCE RATIO USING A WHIRING ARM Y. Itoh¹, A. Satoh¹; ¹Iwate university, Japan | ||||
09:00 | 09:30 | 9.4.3 |
EXPERIMENTAL STUDIES OF SLOT-TYPE CASING TREATMENTS FOR MODEL FANS WITH THE AIM OF AERODYNAMIC AND ACOUSTIC IMPROVEMENTS V. Mileshin¹, S. Markov¹, V. Korzhnev¹, I. Pochkin¹; ¹CIAM, Russia | ||||
09:30 | 10:00 | 9.4.4 |
ANALYSIS OF THRUST-SCALED ACOUSTIC EMISSIONS OF AIRCRAFT PROPELLERS AND THEIR DEPENDENCE ON PROPULSIVE EFFICIENCY X. Geng¹, T. Hu¹, P. Liu¹, T. Sinnige², G. Eitelberg²; ¹Beihang University, China ;²Delft University of Technology, Netherlands |
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08:00 | 08:30 | 10.4.1 |
ARCHITECTURE INTEGRATION OF FUTURE ATM SYSTEM BASED ON META-MODEL J. Wang¹, J. Mao¹, Q. Zhou¹; ¹Chinese Aeronautical Radio and Electronics Research Institute, China | ||||
08:30 | 09:00 | 10.4.2 |
TECHNOLOGY ROADMAPS FOR THE DEVELOPMENT OF FUTURE HIGH-SPEED TRANSPORTATION SYSTEMS V. Vercella¹, R. Fusaro¹, N. Viola¹; ¹Politecnico di Torino, Italy | ||||
09:00 | 09:30 | 10.4.3 |
ARCHITECTURE OF PRODUCT RESEARCH AND DEVELOPMENT SYSTEM FOR COMPLICATED PRODUCTS ENGINEERING L. Su¹, H. Zhou¹, Y. Cheng¹, L. Du¹; ¹AEAC, China | ||||
09:30 | 10:00 | 10.4.4 |
GREENER ATM SYSTEM ARCHITECTURE RESEARCH BASED ON COMPLEX SYSTEM ENGINEERING METHOD H. Hu¹, J. Mao¹, D. Hu¹; ¹China Aeronautical Radio Electronics Research Institute, China |
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08:00 | 08:30 | 11.4.1 |
ATTENTION: TARGET AND ACTUAL - THE CONTROLLER FOCUS J. Rataj¹, O. Ohneiser¹, G. Marin², R. Postaru²; ¹DLR, Germany ;²ROMATSA, Romania | ||||
08:30 | 09:00 | 11.4.2 |
ANALYSIS OF PILOT OPERATIONAL STRATEGY DIFFERENCE USING NEURAL NETWORK R. Mori, Electronic Navigation Research Institute, Japan | ||||
09:00 | 09:30 | 11.4.3 |
OBJECTIVE MEASUREMENT OF HUMAN FACTORS FOR SUPPORTING THE OPERATOR’S LOAD SIMULATION AND MANAGEMENT U. Kale¹, O. Alharasees¹, F. Kling, Research, Development and Simulation Department, HungaroControl, Hungary; D. Rohacs¹; ¹Budapest University of Technology and Economics, Hungary | ||||
09:30 | 10:00 | 11.4.4 |
MACHINE LEARNING ENABLED TURBULENCE PREDICTION USING FLIGHT DATA FOR SAFETY ANALYSIS M. Emara¹, M. dos Santos¹, N. Chartier¹, J. Ackley¹, T.G. Puranik¹, A. Payan¹, M. Kirby¹, O.J. Pinon¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States |
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10:30 | 11:00 | 1.5.1 |
PRELIMINARY DESIGN AND EXPERIMENTAL INVESTIGATION OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT Y. Ma¹, W. Zhang¹, Y. Zhang¹, Y. Ma¹, Z. Bai¹; ¹Northwestern Polytechnical University, China | ||||
11:00 | 11:30 | 1.5.2 |
UNMANNED FIRE-FIGHTING AMPHIBIOUS AIRCRAFT WITH DISTRIBUTED TURBOELECTRIC PROPULSION SYSTEM A.N. Varyukhin¹, M.A. Ovdienko¹, A.V. Vlasov, Central Institute of Aviation Motors, Russia; V.S. Zakharchenko¹; ¹CENTRAL INSTITUTE OF AVIATION MOTORS, Russia | ||||
11:30 | 12:00 | 1.5.3 |
VALIDATION OF AN AERODYNAMIC MODEL FOR THE ANALYSIS OF SUBSCALE TEST AIRCRAFT WITH DISTRIBUTED ELECTRICAL PROPULSION O. Luderer¹, M. Jünemann¹, F. Thielecke¹; ¹Hamburg University of Technology, Germany |
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10:30 | 11:00 | 2.5.1 |
FLEET LEVEL DIRECT OPERATING COST ASSESSMENT OF ADVANCED ALL NEW MID-RANGE TRANSPORT AIRCRAFT J. Hartmann¹, S. Woehler¹, B. Liebhardt¹, F. Presto, Hamburg University of Technology (TUHH), Germany; ¹German Aerospace Center (DLR), Germany | ||||
11:00 | 11:30 | 2.5.2 |
BASED ON THE CHARACTERISTIC PARAMETERS ESTIMATE MANUFACTURING COST FOR COMPOSITE STRUCTURES H.H. Feng¹, F. Liu¹, H.F. Wei¹, J.M. Wu¹; ¹Aviation industry Development Research Center of China, China | ||||
11:30 | 12:00 | 2.5.3 |
ASSESSMENT OF NEW TECHNOLOGIES IN A MULTI-DISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION ENVIRONMENT INCLUDING RAMS AND COST DISCIPLINES C. Cabaleiro¹, M. Fioriti¹, L. Boggero², S. Corpino¹, P.D. Ciampa², B. Nagel²; ¹Politecnico di Torino, Spain ;²German Aerospace Center (DLR), Germany |
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10:30 | 11:00 | 3.5.1 |
AUTONOMOUS CONFLICT RESOLUTION ALGORITHM BASED ON ELLIPTIC GEOMETRY S.S. Rawikara¹, R.A. Sasongko¹, S.A. Munthahar¹; ¹Institut Teknologi Bandung, Indonesia | ||||
11:00 | 11:30 | 3.5.2 |
A NOVEL DETECT-AND-AVOID APPROACH FOR UAS IN URBAN ENVIRONMENTS S. Bijjahalli¹, A. Gardi¹, S. Hilton¹, R. Sabatini¹; ¹RMIT University, Australia | ||||
11:30 | 12:00 | 3.5.3 |
MULTI-UAV TRAJECTORY PLANNING BASED ON COORDINATION VARIABLES X. Zheng¹, S. He¹, D. Lin¹; ¹Beijing Institute of Technology, China |
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10:30 | 11:00 | 4.5.1 |
EFFECT OF DROPLET MVD ON ICING COLLECTION EFFICIENCY FOR A HELICOPTER BLADE W.B. Li¹, K.C. Li, Aviation Industry Corporation of China, China; C. Song¹, H.L. Ma¹, Y.Y. Wang¹; ¹China Aerodynamics Research and Development Center, China | ||||
11:00 | 11:30 | 4.5.2 |
NUMERICAL SIMULATION OF RIDGE ICE AND AERODYNAMIC EFFECT UNDER THERMAL ANTI-ICE L.B. Guo¹, G.Z. Cao, Nanjing University of Aeronautics and Astronautics, China; H.P. Zhang¹; ¹Shanghai Aircraft Design and Research Institute, China | ||||
11:30 | 12:00 | 4.5.3 |
COUPLED HEAT TRANSFER CHARACTERISTICS ON CHEMICALLY REACTING INTERFACE OF HIGH-SPEED AIRCRAFT CONSIDERING WALL INJECTION Q. You¹, X.-F. Yang¹, L. Zeng¹, Y.-W. Gui¹, Y.-X. Du¹, L. Liu¹, G.-M. Xiao¹; ¹China Aerodynamics Research and Development Center, China |
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10:30 | 11:00 | 5.5.1 |
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 | ||||
11:00 | 11:30 | 5.5.2 |
A NOVEL APPROACH FOR TURNAROUND TIME ALLOCATION BASED ON REINFORCEMENT LEARNING A. Rodriguez-Sanz, Universidad Politecnica de Madrid (UPM), Spain; J. Herrera de la Cruz , Universidad Complutense de Madrid (UCM), Spain |
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10:30 | 11:00 | 6.5.1 |
EFFECTS OF ADVERSE PRESSURE GRADIENT ON THE BEHAVIOURS OF RESOLVENT MODE C. Chen, China; J.-T. Huang, China; X. Chen, China | ||||
11:00 | 11:30 | 6.5.2 |
NUMERICAL SIMULATION STUDY ON BOUNDARY LAYER FLOW AND DRAG REDUCTION CHARACTERISTICS OF RIBLETS S.Y. Du¹, R. Pang, AVIC Xi’an Flight Automatic Control Research Institute, China; W.M. Sang¹, G.J. Yang¹; ¹Northwestern Polytechnical University, China | ||||
11:30 | 12:00 | 6.5.3 |
STUDY ON THE HEAT FLUX OF HYPERSONIC SHOCK WAVE BOUNDARY LAYER INTERACTION CONTROLLED BY A MICRO-RAMP VORTEX GENERATOR D. Sun¹, C. Li¹, H.-Y. Cai, School of Aeronautics, Northwestern Polytechnical University, China; Q.-L. Guo¹, P.-X. Liu¹, X.-X. Yuan¹; ¹State Key Laboratory of Aerodynamics, China |
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10:30 | 11:00 | 7.5.1 |
TRANSPORT AIRCRAFT WING INVESTIGATIONS AIMED ON WAKE VORTEX IMPACT BY OSCILLATING FLAPS J. Ruhland¹, F.M. Heckmeier¹, C. Breitsamter¹; ¹Technical University of Munich, Germany | ||||
11:00 | 11:30 | 7.5.2 |
AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATION M. Zhong¹, J. Hua¹, X. Sun¹, S. Zheng¹, G. Wang¹, G. Zhang¹, H. Wang¹, Y. Li¹, X. Li¹, J. Bai, Northwestern Polytechnical University, China; ¹Chinese Aeronautical Establishment, China |
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10:30 | 11:00 | 8.5.1 |
ACCURATE MODELS FOR THE PREDICTION OF FREE-EDGE STRESSES OF COMPOSITE STRUCTURES UNDER THERMAL LOADS E. Zappino¹, E. Carrera¹; ¹Politecnico di Torino, Italy | ||||
11:00 | 11:30 | 8.5.2 |
TEMPERATURE-INDUCED LOAD OF BOLTED HYBRID COMPOSITE/METAL JOINT K. Lei¹, B.-W. Wang¹, J.-T. Wu¹, W.-L. Deng¹; ¹Aircraft Strength Research Institute of China, China | ||||
11:30 | 12:00 | 8.5.3 |
DEVELOPMENT OF LIGHTWEIGHT HYBRID AIRFRAMES BASED ON UNIDIRECTIONAL COMPOSITE STRUCTURE CONCEPTS A. Shanygin, Russia |
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10:30 | 11:00 | 9.5.1 |
DESIGN TECHNIQUE OF INTEGRAL ALGORITHMS OF HELICOPTER FBW CONTROL SYSTEM V.M. Kuvshinov¹, A.Y. Voronin¹; ¹TsAGI, Russia | ||||
11:00 | 11:30 | 9.5.2 |
TRAJECTORY GENERATION AND CONTROL FOR PERCHING MANEUVERING WITH QUADROTOR Y. Sun¹, M. Chang¹, J.Q. Bai¹; ¹NWPU, China |
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10:30 | 11:00 | 10.5.1 |
STRUCTURAL HEALTH MONITORING - THE ROUTE TO CONDITION BASED MAINTENANCE J. van Doeselaar¹, D. Daverschot¹; ¹Airbus, France | ||||
11:00 | 11:30 | 10.5.2 |
COST AND BENEFIT OF SCHEDULED STRUCTURAL HEALTH MONITORING FOR COMMERCIAL AIRCRAFT D.M. Steinweg¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany | ||||
11:30 | 12:00 | 10.5.3 |
REAL TIME IMPACT LOCALIZATION USING MODAL SUPERPOSITION - APPLICATION TO A COMPOSITE AIRCRAFT FUSELAGE D. Goutaudier, CNRS, France; D. Gendre, Airbus, France |
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10:30 | 11:00 | 11.5.1 |
AIRCRAFT INFLIGHT ICING DETECTION AND DIAGNOSIS METHODS D. Ding¹, W.-Q. Qian¹, Q. Wang¹; ¹China Aerodynamics Research and Development Center, China | ||||
11:00 | 11:30 | 11.5.2 |
DESIGN AND RESEARCH ON SAFETY ANALYSIS TOOL FOR AVIONICS SYSTEM Y. Liu, Shanghai Aircraft Design and Research Institute, China | ||||
11:30 | 12:00 | 11.5.3 |
PROTOTYPE WHIRL TOWER FOR TESTING INSOLATED ROTOR SYSTEMS IN HOVER M. Wojtas¹, K. Raczko¹, L. Czajkowski¹; ¹Institute of Aviation, Poland |
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13:00 | 13:30 | 1.6.1 |
ATTENUATION OF NOISE IN THE CABIN OF A REGIONAL AIRCRAFT BY METAMATERIAL TRIM PANELS M.C. Moruzzi, University of Bologna, Italy; M. Cinefra, Italy; S. Bagassi, Italy; E. Carrera, Italy | ||||
13:30 | 14:00 | 1.6.2 |
GAZE-BASED INTERFACE FOR FLIGHT CONTROL: RESULTS OF INITIAL EXPERIMENTS WITH THE SYSTEM M.A. Rodriguez Diaz¹, E. Villani¹, P. Krus, Linköping University, Sweden; ¹Aeronautics Institute of Technology, Brazil | ||||
14:00 | 14:30 | 1.6.3 |
ESTIMATION OF STATIC AND DYNAMIC FLOATATION CHARACTERISTICS DURING AIRCRAFT DITCHING Y. Zhao¹, P. Liu¹, Q. Qu¹; ¹Beihang University, China |
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13:00 | 13:30 | 2.6.1 |
PROPOSAL FOR INTERNATIONAL FIRE AVIATION SERVICE UNDER THE AUSPICES OF ICAO TO IMPROVE WORLD WILDFIRE MANAGEMENT A. Mirzoyan, Russia | ||||
13:30 | 14:00 | 2.6.2 |
ICAO ADDRESSING CLIMATE CHANGE AND WILDFIRES J. Hupe, Canada | ||||
14:00 | 14:30 | 2.6.3 |
EXPERIENCE OF BELARUS IN USING HELICOPTER TECHNOLOGY FOR FOREST FIREFIGHTING I. Labzin, Belarus |
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13:00 | 13:30 | 3.6.1 |
FORMALIZED KNOWLEDGE MANAGEMENT FOR THE AIRCRAFT CABIN DESIGN PROCESS M. Fuchs¹, C. Hesse¹, J. Biedermann¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany | ||||
13:30 | 14:00 | 3.6.2 |
SOS BEHAVIOR MODEL TRANSFORMATION FOR AIRCRAFT TOP-LEVEL DEMONSTRATION J. Zang¹, J.Q. Zhu¹; ¹Chinese Aeronautical Establishment, China | ||||
14:00 | 14:30 | 3.6.3 |
CONNECTING SYSTEM SIMULATION TO AIRCRAFT CONCEPT DEVELOPMENT A. Oprea¹, R. Hällqvist¹, L. Knöös Franzén², M. Eek¹, I. Staack², H. Gavel¹; ¹Saab Aeronautics, Sweden ;²Linköping University, Sweden |
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13:00 | 13:30 | 4.6.1 |
LONGITUDINAL VORTEX FORMATION IN HYPERSONIC BOUNDARY LAYER ON BLUNTED DELTA WING AND ITS EFFECT ON FLOW CHARACTERISTICS V.I. Shalaev¹, S.V. Alexandrov¹, A.V. Vaganov², M.A. Starodubtsev²; ¹Moscow Institute of Physics and Technology, Russia ;²Central aerohydrodynamic Institute, Russia | ||||
13:30 | 14:00 | 4.6.2 |
LONGITUDINAL AND LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE HIGH-SPEED VEHICLE T. Bykerk, Honorary Associate, the University of Sydney, Australia, Australia; G. Pezzella, University of Campania, Engineering Department. , Italy; D. Verstraete, University of Sydney, School of Aerospace, Australia; A. Viviani, University of Campania, Engineering Department., Italy | ||||
14:00 | 14:30 | 4.6.3 |
MULTI-SCALE CFD/MD MODELLING OF HIGH-ENTHALPY FLOW/TPS INTERACTION AND ITS PRELIMINARY AERONAUTICAL APPLICATION X.F. Yang¹, Q. Li, Shanghai Jiao Tong University, China; Y.X. Du¹, G.M. Xiao¹, L. Liu¹, D. Wei¹, Y.W. Gui¹; ¹China Aerodynamics Research and Development Center, China |
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13:00 | 13:30 | 5.6.1 |
DESIGNING AIRCRAFT TRAFFIC FLOWS USING DATA-DRIVEN QUEUING MODELS E. Itoh, The University of Tokyo/ENRI, Japan; F. Kato¹, K. Higasa¹, M. Schultz, Technische Universität Dresden, Germany; ¹The University of Tokyo, Japan | ||||
13:30 | 14:00 | 5.6.2 |
ON THE MINIMUM SEPARATION BETWEEN ANY PAIR OF FLIGHT PATHS L.M.B.C. Campos, IDMEC/CCTAE/IST, Portugal; J.M.G. Marques, Escola de Ciências e Tecnologias, Universidade de Évora, Portugal |
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13:00 | 13:30 | 6.6.1 |
ADJUSTED SHAPES OF ADHESIVELY BONDED REPAIR PATCHES FOR THE EARLY INDICATION OF DEBOND IN FIGHTER AIRCRAFT STRUCTURES J. Jokinen¹, M. Wallin, Patria Aviation, Finland; M. Kanerva¹; ¹Tampere University, Finland | ||||
13:30 | 14:00 | 6.6.2 |
THE INFLUENCE OF THE NUMBER OF ADHESIVE PLIES (FM 300-2) ON FRACTURE PROPERTIES J. Jokinen¹, M. Wallin, Patria Aviation, Finland; M. Kanerva¹; ¹Tampere University, Finland | ||||
14:00 | 14:30 | 6.6.3 |
STATISTICS AND ANALYSIS OF MANUFACTURING DEFECTS AND DAMAGE OF HELICOPTER COMPOSITE STRUCTURES J. Li¹, J. Guo¹, H. Huang, Hafei Aviation Industry CO.,Ltd., China; H.F. Peng¹; ¹China Helicopter Research and Development Institute, China |
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13:00 | 13:30 | 7.6.1 |
RESEARCH ON UNSTEADY AERODYNAMIC MODELS AT HIGH ANGLES OF ATTACK BASED ON NONLINEAR REGRESSION J.A. Cheng¹, H. Zhan¹, B.G. Mi¹; ¹School of Aeronautics,Northwestern Polytechnical University, China | ||||
13:30 | 14:00 | 7.6.2 |
RESEARCH ON THE TRIGGERING CONDITIIONS OF EJECTABLE RECORDER FOR CIVIL AIRCRAFT S.M. Pu¹, H.F. Wang¹, L.K. Cheng¹; ¹Northwestern Polytechnical University, China |
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13:00 | 13:30 | 8.6.1 |
METHODS FOR CALCULATING THE FATIGUE DAMAGE OF A STRUCTURE FOR VARIOUS SPECTRA OF VIBRO-ACOUSTIC LOADS P. Bessonov¹, Y. Svirsky¹, I. Sidorov¹, S. Dubinskii¹; ¹TsAGI, Russia | ||||
13:30 | 14:00 | 8.6.2 |
ITERATIVE GLOBAL/LOCAL NON-INTRUSIVE MODEL COUPLING METHOD FOR STRUCTURE FAILURE ANALYSIS Y.J. Liu¹, S.Q. Liang¹, R.J. Sun¹, M.Q. Li, China; ¹AVIC THE FIRST AIRCRAFT INSTITUTE, China | ||||
14:00 | 14:30 | 8.6.3 |
A STRUCTURE DESIGN OF CFRP REAR PRESSURE BULKHEAD WITHOUT STIFFENERS Z.Y. Li¹, Y.Z. Han¹, X.H. Yao¹; ¹AVIC the First Aircraft Institute, China |
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13:00 | 13:30 | 9.6.1 |
EFFECTS OF COOLANT BUILD DIRECTION ON ADDITIVELY MANUFACTURED FAN-SHAPED COOLING HOLES Q. Zeng, School of Aeronautics and Astronautics, Zhejiang University, China; C. Li¹, J. Cao¹, B. Wang¹, G. Wang, ZHEJIANG UNIVERSITY, China; ¹AECC HAPRI, China | ||||
13:30 | 14:00 | 9.6.2 |
APPLICATION OF ADDITIVE MANUFACTURING TO THE PRODUCTION OF RPAV COMPONENTS P. Iavecchia¹, G. Campolo¹, G. Maritano¹, M. Coppola¹, E. Cestino¹, G. Frulla¹, V. Sapienza, 2Aeronautical Consultant, Italy; P. Piana, TescoGO, Italy; ¹Politecnico di Torino, Italy | ||||
14:00 | 14:30 | 9.6.3 |
AN EFFICIENT FINITE ELEMENT SIMULATION METHOD FOR ADDITIVE MANUFACTURING PROCESS Q.Y. Liu¹, C.Y. Wang¹, P. Yan¹, H. Ruan¹, H.Z. Xue¹, L.T. Dong¹; ¹Beihang University, China |
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13:00 | 13:30 | 10.6.1 |
CONDITION BASED MAINTENANCE (CBM) IN THE DIGITAL TRANSFORMATION STREAM V. Gros¹, P.-C. Rolland¹, S. Veron¹, B. Ordy¹, F. Dessertenne, AIRBUS OPERATIONS SAS, France; ¹AIRBUS SAS, France | ||||
13:30 | 14:00 | 10.6.2 |
TOTAL LIFE CYCLE COST AND EMISSION OF ELECTRIC, HYBRID-ELECTRIC AIRCRAFT D.D. Nguyen¹, U. Kale¹, A.W. Wangai¹; ¹Budapest University of Technology and Economics, Hungary | ||||
14:00 | 14:30 | 10.6.3 |
A METHOD FOR EVALUATING THE APPLICABILITY OF MAINTENANCE TASKS BASED ON HELICOPTER HEALTH AND USAGE MONITORING SYSTEM D.N. Dong¹, Z.Y. Jia¹, Y. Zhou¹; ¹AVIC China Aero-Polytechnology Establishment, China |
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13:00 | 13:30 | 11.6.1 |
ACTIVITY CHARACTERISTICS AND THE MECHANISM OF MESO-MICRO SCALE DISTURBANCES IN THE EAST ASIAN SUBTROPICAL UPPER-LEVEL JET STREAM X. Chen¹, J. Huang¹, M. Meng, Wenzhou Meteorological Burea, China; C. Chen¹, Q. Chen¹; ¹China Aerodynamics Research and Development Center, China | ||||
13:30 | 14:00 | 11.6.2 |
RESEARCH ON FAULT DIAGNOSIS AND FAILURE RECONFIGURATION OF FLUSH AIR DATA SENSING Q. Jia¹, W. Zhang¹, J. Shi¹, J. Hu¹, E. Safwat, Military Technical College, Egypt; ¹Northwestern Polytechnical University, China | ||||
14:00 | 14:30 | 11.6.3 |
CONCEPT OF A NEW SYSTEM SYNTHESIZING METEOROLOGICAL AND OROGRAPHIC INFLUENCES ON THE AIRPLANE SAFE ENERGY ENVELOPE X. Liu¹, L. Manfriani, Centre for Aviation, Zurich University of Applied Sciences, Switzerland; Y. Fu¹; ¹Lab. of Aerosp. Servo Actuation and Transmission, Beihang Univ., China |
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08:00 | 08:30 | 1.7.1 |
CONCEPTUAL DESIGN OF SILENT ELECTRIC COMMUTER AIRCRAFT P. Wassink¹, G. Atanasov¹, C. Hesse¹, B. Froehler¹; ¹German Aerospace Center (DLR), Germany | ||||
08:30 | 09:00 | 1.7.2 |
DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: CONTROL, ALIMENTATION, AND PROPULSION SYSTEMS P. Gili¹, M. Civera¹, R. Roy¹, S. Cibrario Bertolotti¹, D. Cosenza¹, A. Gili¹, C. Surace, Department of Structural, Geotechnical and Building Engineering,, Italy; ¹Department of Mechanical and Aerospace Engineering, Politecnico , Italy | ||||
09:00 | 09:30 | 1.7.3 |
EXPERIMENTAL RESEARCH ON PROPULSION AND AERODYNAMIC CHARACTERISTICS OF A DUAL-BODY DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT X.-Y. Zhang¹, Z.-H. Gao¹, T. Lei¹, X.-B. Zhang¹, W. Zhang¹; ¹Northwestern Polytechnical University, China | ||||
09:30 | 10:00 | 1.7.4 |
ON-BOARD SYSTEM ARCHITECTURES FOR HYBRID/ALL-ELECTRIC REGIONAL AIRCRAFT M. Fioriti¹, F. Di Fede¹, S. Corpino¹, P. Iodice², G. Cerino²; ¹Politecnico di Torino, Italy ;²LEONARDO Aircraft Division, Italy |
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08:00 | 08:30 | 2.7.1 |
COLLABORATIVE AIRCRAFT DESIGN TECHNIQUES IN RESEARCH B. Nagel¹, E. Moerland¹; ¹German Aerospace Center, Germany | ||||
08:30 | 09:00 | 2.7.2 |
IFAR-X COLLABORATIVE AIRCRAFT DESIGN EXERCISE ON ENVIRONMENTALLY COMPATIBLE TRANSPORT AIRCRAFT T. Nunes, CEIIA, Portugal | ||||
09:00 | 09:30 | 2.7.3 |
COLLABORATIVE AIRCRAFT DESIGN EXERCISE BEYOND IFAR P. Novelli, ONERA, France | ||||
09:30 | 10:00 | 2.7.4 |
HARMONIZING SUSTAINABLE AVIATION RESEARCH AMONG IFAR ORGANIZATIONS E. Campillo-Borras, Germany |
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08:00 | 08:30 | 3.7.1 |
FLIGHT TEST OF AN ADVANCED HYBRID-LAMINAR-FLOW-CONTROL (HLFC) SYSTEM ON AN A320 VERTICAL TAIL PLANE G. Ernst, German Aerospace Center, Germany; S. Pawellek¹, A. Büscher¹; ¹Airbus Operations GmbH, Germany | ||||
08:30 | 09:00 | 3.7.2 |
NOISE REDUCTION AT FLAP SIDE EDGE AND UNDERCARRIAGE M. Pott-Pollenske, Germany | ||||
09:00 | 09:30 | 3.7.3 |
MAIN LANDING GEAR DOORS VIBRATION REDUCTION BASED ON FLIGHT TEST R. Abarca López¹, C. Aquilini¹, P. Lubrina, ONERA, France; S.-H. Peng, FOI, Sweden; J. Schwochow, DLR, Germany; ¹Airbus, Spain | ||||
09:30 | 10:00 | 3.7.4 |
TOWARDS THE INDUSTRIAL APPLICATION OF ACTIVE FLOW CONTROL AT THE PYLON/WING JUNCTION OF CIVIL AIRCRAFT V. Soudakov, TsAGI, Russia; P. Schlösser¹, P. Weigel, Fraunhofer-Gesellschaft, Germany; T. ter Meer, NLR, Netherlands; A. Gebhardt, DLR, Germany; M. Meyer¹, M. Wahlich¹; ¹Airbus, Germany |
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08:00 | 08:30 | 4.7.1 |
FURTHER DEVELOPMENT OF COMPUTATIONAL STUDY ON COANDA BLANKET CURVATURE EFFECTS ON HALF SPHERICAL COANDA DEVICE H. Djojodihardjo, The Institute for the Advancement of Aerospace Science and Techn, Indonesia; M.A. Andira¹, R. Julistina¹, M.A. Moeljadi, Institute of Technology Bandung, Indonesia; ¹CCIT Group Indonesia, Indonesia | ||||
08:30 | 09:00 | 4.7.2 |
AERODYNAMIC MODELING AND FLIGHT PERFORMANCE RESEARCH OF THE COAXIAL RIGID HELICOPTER IN POP-UP PROCESS H.-Y. Li¹, X. Zhao¹, K. You¹, S.-Z. Zhao¹, Y.-F. Lin, China Helicopter Research and Development Institute, China; ¹Northwestern Polytechnical University, China | ||||
09:00 | 09:30 | 4.7.3 |
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 | ||||
09:30 | 10:00 | 4.7.4 |
NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING WITH SLOTTED-TIP D. Liu, School of Aeronautics,Northwestern Polytechnical University, China; W.Q. Yang¹, B.F. Song¹; ¹Research & Development Institute of NWPU in Shenzhen, China |
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08:00 | 08:30 | 5.7.1 |
AIRLINE NETWORK-AIRPLANE INTEGRATED OPTIMIZATION CONSIDERING MANUFACTURER'S PROGRAM COST J.A.T.G. Fregnani, Airbus, Brazil; B.S. Mattos¹, J.A. Hernandes¹; ¹ITA, Brazil | ||||
08:30 | 09:00 | 5.7.2 |
AIR TRAFFIC MANAGEMENT OF DRONES INTEGRATED INTO THE SMART CITIES D. Dinh Nguyen¹, D. Rohacs¹; ¹Budapest University of Technology and Economics, Hungary | ||||
09:00 | 09:30 | 5.7.3 |
VERTIPORT PLACEMENT METHOD BASED ON MOBILITY SURVEY DATA K. Lippoldt¹, L. Preis, Bauhaus Luftfahrt e.V., Germany; K. Bogenberger¹; ¹Technical University Munich, Germany | ||||
09:30 | 10:00 | 5.7.4 |
ASSESSING THE ENVIRONMENTAL IMPACT OF AIRCRAFT TAXIING TECHNOLOGIES R. Camilleri¹, A. Batra¹; ¹Institute of Aerospace Technologies, University of Malta, Malta |
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08:00 | 08:30 | 6.7.1 |
BLADE - NATURAL LAMINAR FLOW FLIGHT TESTING T. Gibson¹, B. Soucheleau¹, N. Rogers¹; ¹Airbus, United Kingdom | ||||
08:30 | 09:00 | 6.7.2 |
METHODICAL STUDIES OF THE POSSIBILITY TO APPLY A NUMERICAL METHOD WITH BUILD-IN EMPIRICAL CRITERIA FOR DETERMIMING THE LAMINAR-TO-TURBULENT TRANSITION ON THE CONE SURFACE AT HIGH MACH NUMBERS N.V. Voevodenko¹, Y.G. Shvalev¹; ¹TsAGI, Russia | ||||
09:00 | 09:30 | 6.7.3 |
NATURAL-LAMINAR-FLOW AIRFOIL DESIGN OPTIMIZATION CONSIDERING CROSSFLOW INSTABILITY WHEN CONFIGURED ON A SWEPT WING Z.-M. Xu¹, Z.-H. Han¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China | ||||
09:30 | 10:00 | 6.7.4 |
MULTIPOINT OPTIMIZATION OF TRANSONIC NATURAL LAMINAR FLOW NACELLES C.Y. Yan¹, Y.F. Zhang¹, M.H. Zhang, Shanghai Aircraft Design and Research Institute, China; ¹School of Aerospace, Tsinghua University, China |
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08:00 | 08:30 | 7.7.1 |
FAILURE PROCESS IDENTIFICATION IN C/SIC SAMPLES WITH A RANGE OF TENSILE PERFORMANCE USING ACOUSTIC EMISSION Y.Z. Zhang¹, X.Y. Tong¹, L.J. Yao¹, A.T. Augousti, Kingston University London, United Kingdom; ¹Northwestern Polytechnical University, China | ||||
08:30 | 09:00 | 7.7.2 |
EXPERIMENTAL INVESTIGATION AND LIFE PREDICTION FOR DEFECT INDUCED CRACK OF A P/M NICKEL BASED SUPERALLOY Y. Shi, China; X. Yang, China; D. Shi, China; D. Yang, China; G. Miao, China; S. Lv, China |
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08:00 | 08:30 | 8.7.1 |
RESEARCH OF LABYRINTH SEALS MEASUREMENT-BASED PROBABILITISTIC ANALYSIS METHOD FOR TURBOFAN INTERNAL AIR SYSTEM C.-X. Song¹, M.-C. Deng¹, Y. Fan¹, Y.-Q. Liang¹, Y. Shen¹; ¹AECC Shenyang Engine Research Institute, China | ||||
08:30 | 09:00 | 8.7.2 |
AXIAL ASSEMBLAGE DEVIATION ON PERFORMANCE OF ONE TRANSONIC CENTRIFUGAL COMPRESSOR W. Zhang¹, K. Luo¹, Q. Wen², F.-M. Tang²; ¹AECC HAPRI, China ;²AECC AEAC, China | ||||
09:00 | 09:30 | 8.7.3 |
THE POTENTIAL OF CASING TREATMENTS FOR TRANSONIC COMPRESSORS: EVALUATION BASED ON AXIAL-SLOT AND ROTOR BLADE OPTIMIZATION G. Goinis¹, C. Voß¹, E. Nicke¹; ¹German Aerospace Center (DLR), Germany | ||||
09:30 | 10:00 | 8.7.4 |
APPLICATION OF REINFORCEMENT LEARNING IN 1-D AERODYNAMIC DESIGN OF AXIAL COMPRESSOR Y. Liu¹, X. Hang¹, C. Jiang¹; ¹Beihang University, China |
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08:00 | 08:30 | 9.7.1 |
TOWARDS AN ONLINE PREDICTIVE MODEL OF AIRCRAFT ENERGY STATE USING SUPERVISED MACHINE LEARNING H.K. Lee¹, T.G. Puranik¹, O.J. Pinon Fischer¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States | ||||
08:30 | 09:00 | 9.7.2 |
AN OVERVIEW OF FLARE TECHNIQUES AND FLARE TRAINING METHODS K. Okubo¹, J.O. Entzinger¹; ¹The University of Tokyo, Japan | ||||
09:00 | 09:30 | 9.7.3 |
FLIGHT PERFORMANCE AND TRAJECTORY PREDICTION OF THE COAXIAL HELICOPTER IN AUTOROTATION S.-Z. Zhao¹, X. Zhao¹, R. Yao¹, Y.-F. Lin, China Helicopter Research and Development Institute, China; ¹Northwestern Polytechnical University, China | ||||
09:30 | 10:00 | 9.7.4 |
NUMERICAL STUDY OF DITCHING CHARACTERISTICS OF BWB AIRCRAFT S.L. Ding¹, Q.L. Qu¹, P.Q. Liu¹; ¹Beihang University, China |
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08:00 | 08:30 | 10.7.1 |
ANALYTICAL MODELLING OF A HOVERABLE X-SHAPE FLAPPING WING AIRCRAFT CONSIDERING WING-TAIL INTERACTION L.F. Zhao, Beihang University, Research Institute for Frontier Science, China; W.S. Wang, Beihang University, School of Automation Science and Electrical , China; Y.X. Chen, Beihang University, School of Aeronautic Science and Engineering, China; Z.X. Jiao, Beihang University, Ningbo Institute of Technology, China | ||||
08:30 | 09:00 | 10.7.2 |
MODELING AND CONTROL OF A HOVERABLE FLAPPING WING AIRCRAFT CONSIDERING FLAPPING WING INDUCED FLOW L. Wang¹, L.F. Zhao¹, W.Y. Jiang¹, Z.X. Jiao¹; ¹Beihang University, China | ||||
09:00 | 09:30 | 10.7.3 |
SIMULATION ON THE EFFECT OF AIRCRAFT LOCAL STRUCTURE DAMAGES ON THE DYNAMIC DERIVATIVE COUPLING CHARACTERISTICS B.-G. Mi¹, H. Zhan¹, X. Bai¹, J.-Y. Yu¹; ¹Northwestern Polytechnical University, China | ||||
09:30 | 10:00 | 10.7.4 |
INFLUENCE OF AERODYNAMIC ASYMMETRY ON SPIN PARAMETERS OF THE COMMON RESEARCH MODEL A.N. Khrabrov¹, M.E. Sidoryuk¹; ¹TsAGI, Russia |
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10:30 | 11:00 | 1.8.1 |
COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN S. Görtz¹, C. Ilic¹, M. Abu-Zurayk¹, T. Wunderlich¹, M. Schulze¹, T. Klimmek¹, Ö. Süelözgen¹, T. Kier¹, A. Schuster¹, S. Dähne¹, M. Petsch¹, J. Häßy¹, R.-G. Becker¹, M. Siggel¹, J. Kleinert¹, R. Mischke¹, S. Gottfried¹; ¹DLR, Germany | ||||
11:00 | 11:30 | 1.8.2 |
BLENDED WING BODY (BWB) PLANFORM MULTIDISCIPLINARY OPTIMISATION (MDO) FOR EARLY STAGE AIRCRAFT DESIGN USING MODEL BASED ENGINEERING D. DI Pasquale¹, D. Verma¹, G. Pagliuca¹; ¹Cranfield University, United Kingdom | ||||
11:30 | 12:00 | 1.8.3 |
TOPOLOGY OPTIMIZATION FOR WING STRUCTURE OF HYPERSONIC VEHICLE S.S. Zhang¹, Z.Q. Wan¹, X.Z. Wang, Institute of Unmanned System, Beihang University, China; Y.Z. Liu, China North Ind Grp Corp, Nav & Control Technol Inst, China; ¹School of Aeronautic Science and Engineering, Beihang University, China |
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10:30 | 11:00 | 2.8.1 |
DESIGN AND TEST OF A HIGH SLOPE ANGLE INTERMEDIATE DUCT BETWEEN LOW-PRESSURE COMPRESSOR AND HIGH-PRESSURE COMPRESSOR H.-L. Jin¹, J. Zhang¹, J.-F. Wu¹, D.-B. Qiu¹, Y.-Q. Yin¹; ¹AECC Hunan Aviation Powerplant Research Institute, China | ||||
11:00 | 11:30 | 2.8.2 |
NUMERICAL STUDY ON COOLING CHARACTERISTICS IN CHANNELS WITH PIN FIN ARRAYS UNDER HIGH TEMPERATURE/PRESSURE CONDITIONS S.-E. Peng¹, W. Jin¹, J.-M. Wu¹; ¹Xi’an Jiaotong University, China | ||||
11:30 | 12:00 | 2.8.3 |
THE FLOW AND HEAT TRANSFER OF ANALYSIS TO ANNULAR CAVITY IN ENGINE CASE G.Y. Pan¹, X. Yu¹, Y. Ii¹, Y.X. Zhao¹; ¹AECC SHENYANG ENGINE RESEACH INSTITUE, China |
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10:30 | 11:00 | 3.8.1 |
IMPROVED DESIGN OF AIRCRAFT NOSEWHEEL STEERING SYSTEM X. Li¹, Z.J. Wang¹, X.B. Ding ¹, Z.B. Wei¹; ¹FAI AVIC, China | ||||
11:00 | 11:30 | 3.8.2 |
INVESTIGATIONS ON LANDING GEAR SHOCK ABSORBER ACTIVE FORCE CONTROL Z. Skorupka¹, R. Harla¹; ¹Lukasiewicz Research Network - Institute of Aviation, Poland | ||||
11:30 | 12:00 | 3.8.3 |
A STOCHASTIC ROBUSTNESS VERIFICATION OF NLG SIMPLE ADAPTIVE SHIMMY SUPPRESSION SYSTEM A. Alaimo¹, C. Orlando¹; ¹Università di Enna Kore, Italy |
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10:30 | 11:00 | 4.8.1 |
VALIDATION OF A DISCONTINUOUS GALERKIN BASED DES SOLVER IN FLOW PROBLEMS USING HIGH PERFORMANCE COMPUTING I. Bosnyakov¹, S. Bosnyakov¹, S. Mikhaylov¹, V. Podaruev¹, A. Troshin¹, A. Wolkov¹; ¹Central Aerohydrodynamic Institute, Russia | ||||
11:00 | 11:30 | 4.8.2 |
ADVANCED WEAK SOLUTIONS IN FLUID DYNAMICS AND THEIR NUMERICAL COMPUTATIONS WITH AERODYNAMIC HEATING M. Ivanov¹, V. Mamaev¹, J. Li², G. Zheng²; ¹CIAM, Russia ;²NWPU, China | ||||
11:30 | 12:00 | 4.8.3 |
A BENCHMARK METHOD FOR PREDICTING OBLIQUE SHOCK STRUCTURE A. Shi, NORTHWESTERN POLYTECHNICAL UNIVERSITY, China; E. Dowell, DUKE UNIVERSITY, United States |
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10:30 | 11:00 | 5.8.1 |
FLIGHT TESTING OF 65KG T-FLEX SUBSCALE DEMONSTRATOR J. Bartasevicius¹, S.J. Koeberle¹, D. Teubl¹, C. Roessler¹, M. Hornung¹; ¹ Institute of Aircraft Design, Technical University of Munich, Germany | ||||
11:00 | 11:30 | 5.8.2 |
THE STUDY OF UNMANNED AERIAL VEHICLE FLYING QUALITIES FLIGHT TEST METHOD BASED ON TIME-DELAY EVALUATION S.-J. Qi¹, F. Wang¹, L. Jing¹; ¹Chinese Flight Test Establishment, China | ||||
11:30 | 12:00 | 5.8.3 |
STUDY OF SMALL UAVS DISTURBED MOTION NATURAL FREQUENCIES USING EXTENDED EXPERIMENTAL DATASETS M. El-Salamony, Peking University, China; S. Serokhvostov, Moscow Institute of Physics and Technology, Russia |
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10:30 | 11:00 | 6.8.1 |
STABILIZATION OF SUPERSONIC BOUNDARY LAYERS IN THE PRESENCE OF FAVORABLE PRESSURE GRADIENT P.V. Chuvakhov, Central Aerohydrodynamic Institue (TsAGI), Russia | ||||
11:00 | 11:30 | 6.8.2 |
NUMERICAL SIMULATION OF THREE-DIMENSIONAL DISTURBANCES EVOLUTION IN SUPERSONIC FLOW OVER A WAVY SURFACE A. Novikov, TsAGI, MIPT, Russia; A. Fedorov, MIPT, Russia | ||||
11:30 | 12:00 | 6.8.3 |
MECHANISMS OF NATURAL LAMINAR-TURBULENT TRANSITION ON AN UNSWEPT WING IN SUPERSONIC FLIGHT P.V. Chuvakhov, Central Aerohydrodynamic Institue (TsAGI), Russia; A.V. Fedorov¹, I.O. Pogorelov¹; ¹Moscow Institute of Physics and Technology (MIPT), Russia |
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10:30 | 11:00 | 7.8.1 |
AERODYNAMIC OPTIMIZATION DESIGN OF DOUBLE BLUNT ROTOR AIRFOIL WITH LARGE THICKNESS IN FORWARD AND REVERSE FLOW Y.M. Yao¹, X.D. Yang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | ||||
11:00 | 11:30 | 7.8.2 |
PARETO FRONT EXPLORATION USING MANIFOLD RECONSTRUCTION APPROACH FOR ROTORCRAFT AIRFOILS DESIGN C. Song, China; W.-B. Li, China; Z. Zhou, China; H.-Y. Liu, China; X. Luo, China | ||||
11:30 | 12:00 | 7.8.3 |
AERODYNAMIC DESIGN OPTIMIZAITON OF HYPERSONIC WING OVER WIDE MACH-NUMBER RANGE CONSIDERING LIFT MATCHING Y. Zhang¹, Z.-H. Han¹, F. Liu¹, C.-Z. Xu¹; ¹Northwestern Polytechnical University, China |
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10:30 | 11:00 | 8.8.1 |
MULTI-AXIS MANEUVER SIMULATION FOR SYSTEM IDENTIFICATION OF FLEXIBLE TRANSPORT AIRCRAFT BY HIGH-FIDELITY METHODS M. Ritter¹, M.S. Roeser¹, S. Görtz¹; ¹German Aerospace Center (DLR), Germany | ||||
11:00 | 11:30 | 8.8.2 |
THEORETICAL AND EXPERIMENTAL INVESTIGATION OF THE AEROELASTIC CHARACTERISTICS OF THE AFLONEXT PROJECT BIG-SIZE DEMONSTRATOR G.A. Amiryants¹, A.V. Chedrik¹, V.A. Malyutin¹, S.E. Paryshev¹, V.G. Soudakov¹; ¹Central Aerohydrodynamic Institute , Russia | ||||
11:30 | 12:00 | 8.8.3 |
ACTUATION MECHANISM USING SHAPE MEMORY ALLOY WIRES IN SPIRAL ARRANGEMENT FOR MORPHING WINGS R. Tsukamoto¹, A. Senba¹, T. Ikeda, Chubu University, Japan; M. Tamayama², H. Arizono²; ¹Meijo University, Japan ;²JAXA, Japan |
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10:30 | 11:00 | 10.8.1 |
THE APPLICATION OF THE PILOT-AIRCRAFT SYSTEM APPROACH FOR OPTIMIZING 3D DISPLAY PARAMETERS A.V. Efremov¹, M.S. Tiaglik¹, I.K. Irgaleev¹; ¹Moscow Aviation Institute, Russia | ||||
11:00 | 11:30 | 10.8.2 |
ON THE MAXIMIZATION OF CONTROL POWER IN LOW-SPEED FLIGHT FOR A BWB CONFIGURATION L.M.B.C. Campos, IDMEC/CCTAE/IST, Portugal; J.M.G. Marques, Escola de Ciências e Tecnologias, Universidade de Évora, Portugal |
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10:30 | 11:00 | 11.8.1 |
EXPERIMENT AND THEORETICAL ANALYSIS OF A TYPE OF NON-SYNCHRONOUS VIBRATION IN A HIGH PRESSURE COMPRESSOR F.L. Gao¹, M.S. Yang¹, Z.B. Zhang¹, Y. Chen¹; ¹AECC Shenyang Engine Research Institute, China | ||||
11:00 | 11:30 | 11.8.2 |
MEASUREMENT AND ANALYSIS OF INTER-STAGE FLOW FIELD IN A HIGH-LOAD AXIAL MULTISTAGE COMPRESSOR Z.-B. Zhang¹, F.-L. Gao¹, H. Wu¹, Y.-H. Chen¹; ¹Shenyang Engine Research Institute, China | ||||
11:30 | 12:00 | 11.8.3 |
ANALYSIS OF A WING-TIP-MOUNTED SMALL-SCALE PROPELLER CONFIGURATION UNDER NON-AXIAL INFLOW CONDITIONS M. Cerny¹, N. Herzog, Rolls-Royce Deutschland Ltd & Co KG, Germany; C. Breitsamter¹; ¹Technical University of Munich, Germany |
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13:00 | 13:30 | 1.9.1 |
EXPLORATION OF AERIAL FIREFIGHTING FLEET EFFECTIVENESS AND COST BY SYSTEM OF SYSTEMS SIMULATIONS P. Shiva Prakasha¹, N. Naeem¹, N. Cigal¹, P. Ratei¹, B. Nagel¹; ¹German Aerospace Center, Germany | ||||
13:30 | 14:00 | 1.9.2 |
BENEFIT ANALYSIS OF AIR REFUELING IN ULTRA LONG ROUTE AIRLINER OPERATION C. Ma¹, J.T. Si¹, Y.C. Chen, Commercial Aircraft Corporation of China, China; ¹Shanghai Aircraft Design and Research Institute, China | ||||
14:00 | 14:30 | 1.9.3 |
CLOUD-BASED ENVIRONMENT FOR AIRCRAFT DESIGN COLLABORATION X. Chen¹, A. Riaz¹, M.D. Guenov¹; ¹Cranfield University, United Kingdom | ||||
14:30 | 15:00 | 1.9.4 |
QUANTIFICATION OF OPERATIONAL EFFECTIVENESS FOR TECHNOLOGY EVALUATION A. Hull¹, A. Sudol¹, D. Mavris¹; ¹Georgia Institute of Technology, United States |
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13:00 | 13:30 | 2.9.1 |
METHODOLOGY FOR OBTAINING AN OPTIMIZED BAFFLED AIRFOIL FOR AN INFLATABLE WING S.R. Mistri¹, R.S. Pant¹, C.S. Yerramalli¹, A. Guha¹; ¹Indian Institute of Technology- Bombay, India | ||||
13:30 | 14:00 | 2.9.2 |
INTEGRATED AERODYNAMIC DESIGN OF PROPELLER POSITION AND WING SHAPE AT A LOW REYNOLDS NUMBER W. Yang, National University of Defense Technology, China; L. Yu¹, W.H. Wu¹, Z.L. Fan¹; ¹China Aerodynamics Research and Development Center, China | ||||
14:00 | 14:30 | 2.9.3 |
LIGHTWEIGHT UAV FOR EMERGENCY MEDICAL SERVICE T. Goetzendorf-Grabowski¹, J. Mieloszyk¹, M. Figat¹, A. Tarnowski¹, B. Hernik¹; ¹Warsaw University of Technology, Poland | ||||
14:30 | 15:00 | 2.9.4 |
DESIGN OF A HYBRID VTOL LOGISTICS UAV SYSTEM INTEGRATED INTO CIVIL AVIATION AIR TRAFFIC CONTROL SYSTEM J. Hanjie¹, M. Yi , Xi’an Institute of Space Radio Technology, China; Z. Ye ¹; ¹School of Aerospace Engineering, Universiti Sains Malaysia, Malaysia | ||||
15:00 | 15:30 | 2.9.5 |
DESIGN OPTIMIZATION OF MULTIROTOR DRONES IN FORWARD FLIGHT F. Pollet¹, S. Delbecq¹, M. Budinger, INSA Toulouse/ICA, France; J.-M. Moschetta¹; ¹ISAE-SUPAERO, France |
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13:00 | 13:30 | 3.9.1 |
RESEARCH ON AIRCRAFT-LEVEL PHYSICAL INTEGRATION VERIFICATION TEST TECHNOLOGY Z.C. Yao¹, L.B. Liu¹; ¹Shanghai Aircraft Design and Research Institute, Shanghai, China | ||||
13:30 | 14:00 | 3.9.2 |
THE APPLICATION OF THE AGILE 4.0 MBSE ARCHITECTURAL FRAMEWORK FOR THE MODELING OF SYSTEM STAKEHOLDERS, NEEDS AND REQUIREMENTS L. Boggero¹, P.D. Ciampa¹, B. Nagel¹; ¹DLR, Germany | ||||
14:00 | 14:30 | 3.9.3 |
HYBRID MODELLING FOR FULL MISSION SIMULATION P. Krus, Linköping university, Sweden; R. Braun, ICAS2020_0980, Sweden; E. Villani, Instituto Tecnológico de Aeronáutica, Brazil | ||||
14:30 | 15:00 | 3.9.4 |
MODEL-BASED VIRTUAL INTEGRATED TEST METHOD FOR AVIONICS SYSTEM S.F. Zhu¹, P.P. Xing¹; ¹COMAC Beijing Aircraft Technology Research Institute, China | ||||
15:00 | 15:30 | 3.9.5 |
A DEEP LEARNING AND ONTOLOGY BASED FRAMEWORK FOR TEXTUAL REQUIREMENTS ANALYSIS AND CONCEPTUAL MODEL GENERATION A. Liu, China |
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13:00 | 13:30 | 4.9.1 |
EXPERIMENTAL VALIDATION OF NUMERICAL PREDICTION OF WING-PROPELLER AERODYNAMIC INTERACTION S. De Lucas Bodas¹, J. Narbona Gonzalez¹, V. Ossorio Contreras¹, J.J. Guerra Crespo¹, D.E. Funes Sebastian¹, L.P. Ruiz Calavera¹; ¹Airbus Defence & Space, Spain | ||||
13:30 | 14:00 | 4.9.2 |
STATIC AEROELASTIC COMPUTATIONS OF WING CONFIGURATIONS IN TRANSONIC FLOWS AT HIGH REYNOLDS NUMBERS J.A.A. Lyrio¹, J.L.F. Azevedo², D.A. Rade¹, R.G. da Silva²; ¹Instituto Tecnológico de Aeronáutica, Brazil ;²Instituto de Aeronáutica e Espaço, Brazil | ||||
14:00 | 14:30 | 4.9.3 |
NUMERICAL INVESTIGATION OF WING ROCK PHENOMENON ON LOW ASPECT RATIO RECTANGULAR WINGS AT LOW REYNOLDS NUMBER A. Sultan¹, A. Maqsood¹, T.H. Go, Raytheon Missile Systems, United States; R. Riaz¹; ¹National University of Sciences & Technology, Pakistan | ||||
14:30 | 15:00 | 4.9.4 |
S55 PROJECT - CFD ANALYSIS OF AN HISTORICAL SEAPLANE C. Baldon¹, R. Indelicato¹, N. Bottino¹, M. Sinisi¹, F. Carrone¹, G. Cantanna¹, E. Cestino¹, V. Sapienza, Aeronautical Consultant, Italy; ¹Politecnico di Torino, Italy | ||||
15:00 | 15:30 | 4.9.5 |
RESEARCH ON FSI DYNAMIC CHARACTERISTICS OF PARAFOIL TRAILING EDGE DEFLECTION X.L. Gao¹, Q.B. Zhang, National Defense Technology University, China; Z.H. Li, Beijing Pioneering Innovation Center of China Aerodynamics Resea, China; Q. Chen¹, W.K. Wang, AVIC Aerospace Life-Support Industries. Ltd, China; ¹China Aerodynamic R&D Center, China |
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13:00 | 13:30 | 5.9.1 |
ACHIEVEMENTS IN THE BUCKLING OF THIN-WALLED COMPOSITE LAUNCHER STRUCTURES R. Degenhardt¹, F. Franzoni¹, S.G.P. Castro, TU-Delft, Netherlands; ¹DLR, Germany | ||||
13:30 | 14:00 | 5.9.2 |
THE VIBRATION CORRELATION TECHNIQUE – A RELIABLE NONDESTRUCTIVE TOOL TO PREDICT BUCKLING LOADS H. Abramovich, Technion, I.I.T.,, Israel | ||||
14:00 | 14:30 | 5.9.3 |
KINEMATIC MODEL OF REFINED THEORY AND EXACT ANALYTICAL SOLUTIONS OF STATIC AND BUCKLING PROBLEMS OF STRUCTURALLY-ANISOTROPIC COMPOSITE PANELS OF AIRCRAFT L.M. Gavva, Moscow Aviation Institute (NRU) , Russia | ||||
14:30 | 15:00 | 5.9.4 |
STUDY ON THE OUT-OF-PLANE COMPRESSION PROPERTIES OF MULTISTAGE TITANIUM ALLOY LATTICE METAMATERIALS AT 350°C H.Y. Huang¹, D. Wang¹, X.F. Du¹, Y.X. Xu¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | ||||
15:00 | 15:30 | 5.9.5 |
ACCURATE BUCKLING AND POST-BUCKLING ANALYSIS OF COMPOSITE STIFFENED PANELS E. Carrera¹, A. Pagani¹, R. Augello¹, D. Scano¹; ¹Politecnico di Torino, Italy |
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13:00 | 13:30 | 6.9.1 |
ANALYSIS AND CONTROL OF DYNAMIC STALL CHARACTERISTICS OF S809 AIRFOIL L.-S. Hao¹, Y.-W. Gao¹, B.-B. Wei¹, B. Hu¹; ¹Northwestern Polytechnical University, China | ||||
13:30 | 14:00 | 6.9.2 |
PHISICAL AND MATHEMATICAL MODELS OF THE BUFFET ONSET A.M. Lipanov, Institute of Applied Mathematics RAS, Russia; I.I. Lipatov, TsAGI, Russia; S.A. Karskanov, Instiute of Mechanics, Germany | ||||
14:00 | 14:30 | 6.9.3 |
IMPROVEMENT OF HELICOPTER PERFORMANCE THROUGH PULSE AIR JETS BLOWN FROM THE TRAILING EDGE OF MAIN ROTOR BLADES W. Stalewski, Lukasiewicz Research Network- Institute of Aviation, Poland | ||||
14:30 | 15:00 | 6.9.4 |
STUDY ON THE EFFECTS OF PROPLET GEOMETRIC PARAMETERS ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLER B. Wang¹, X.D. Yang¹, B.F. Song¹, J.H. Xu¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | ||||
15:00 | 15:30 | 6.9.5 |
ANALYSIS OF AERODYNAMIC COUPLING EFFECT IN CLOSE FORMATION FOR FLAPPING WINGS Z.T. Chen ¹, Z.X. Jiao¹, Y.X. Shang¹, L.F. Zhao¹; ¹Beihang University, China |
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13:00 | 13:30 | 7.9.1 |
AN EXERCISE IN DEVELOPING A SUPERVISED ANOMALY DETECTION MODEL WITH AUTOMATICALLY ENGINEERED FEATURES R. Rameshbabu¹, D. Rajaram¹, O.J. Pinon Fischer¹, T.G. Puranik¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States | ||||
13:30 | 14:00 | 7.9.2 |
INCORPORTING KNOWLEDGE COVERAGE MEASUREMENT INTO KNOWLEDGE TRANSFORMATION FROM DATA FOR KNOWLEDGE ACCUMULATION Y. Fan, Nanchang Hangkong University, China; C. Liu¹, J. Wang¹; ¹Northwestern Polytechnical University, China | ||||
14:00 | 14:30 | 7.9.3 |
DESIGN AND BEST PRACTICES OF SUPPLIER PERFORMANCE EVALUATION IN SUPPLY CHAIN H. Li¹, Y. Xu¹, Y. Chen¹; ¹AECC SHANGHAI COMMERCIAL AIRCRAFT ENGINE MANUFACTURING CO.,LTD., China | ||||
14:30 | 15:00 | 7.9.4 |
AUTOMATIC DETECTION TECHNOLOGY OF LARGE CIVIL AIRCRAFT BASED ON IMAGE RECOGNITION T.L. Shen, Automatic Detection Technology of Large Civil Aircraft Based on, China | ||||
15:00 | 15:30 | 7.9.5 |
ENABLING THE SMART SHOP FLOOR THROUGH THE INTEGRATION OF IOT AND AUTONOMOUS INTELLIGENCE A. Xu, Chengdu Aircraft Industrial (Group) Co., Ltd., China |
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13:00 | 13:30 | 8.9.1 |
AN INVERSE APPROACH BASED ON EUCLIDEAN SPACE FOR DETERMINING STRUCTURAL LOAD DISTRIBUTION FROM STRAIN MEASUREMENTS H.N. Dui, China; D.L. Liu, China; Z.X. Zhang, China; S.Z. Pan, China; L.X. Zhang, China | ||||
13:30 | 14:00 | 8.9.2 |
THERMOPLASTIC APPLICATIONS FOR AEROSTRUCTURES: TOWARDS SUSTAINABLE AND WEIGHT EFFICIENT APPLICATIONS M. Herman¹, E. Dupuy¹, C. Paris¹, E. Petiot¹, J.-P. Cabanac¹, C. Fualdes¹, G. Masse², M.-A. Celli²; ¹Airbus Operations, France ;²Airbus Helicopters, France | ||||
14:00 | 14:30 | 8.9.3 |
RATIONAL DETERMINATION OF WING JIG SHAPE OF A LONG-RANGE AIRCRAFT WITH TRANSONIC CRUISE REGIME A.V. Bezuevsky¹, A.V. Grigorev¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia | ||||
14:30 | 15:00 | 8.9.4 |
AIRCRAFT ENGINE ROTOR DYNAMICS ANALYSIS AFTER FAN BLADE-OUT WITH ACCOUNT OF ROTOR-CASING CONTACT INTERACTIONS V.Y. Myasnikov¹, I.I. Ivanov¹, B.S. Blinnik¹; ¹CIAM, Russia | ||||
15:00 | 15:30 | 8.9.5 |
STRUCTURAL HEALTH MONITORING OF SANDWICH STRUCTURES WITH LATTICE CORES IN AIRCRAFT DESIGN: CHALLENGES AND POTENTIAL T. Huang, Nanjing University of Aeronautics and Astronautics, China; M. Nuño ¹, K.-U. Schröder¹; ¹RWTH Aachen University, Germany |
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13:00 | 13:30 | 9.9.1 |
CERTIFICATION CONSIDERATIONS FOR EVTOL AIRCRAFT Y. Mou¹, M. Jiang¹, G. Zhu¹; ¹Nanjing Engineering Institute of Aircraft Systems, China | ||||
13:30 | 14:00 | 9.9.2 |
APPLICATION OF DEVELOPMENT ASSURANCE METHODOLOGIES TO ELECTRONIC ENGINE CONTROL SYSTEM (EECS) Q. Zhu¹, C.X. Wang¹; ¹AECC Commercial Aircraft Engine Co. Ltd, China | ||||
14:00 | 14:30 | 9.9.3 |
RESEARCH ON CERTIFICATION MANAGEMENT OF AIRCRAFT ENGINE BASED ON RISK ANALYSIS C.X. Wang¹, Q. Zhu¹, X.K. Wang¹, X.H. Tang¹; ¹AECC Commercial Aircraft Engine Co. Ltd, China | ||||
14:30 | 15:00 | 9.9.4 |
STUDY ON THE AIRWORTHINESS AND COMFORTABLENESS REQUIREMENTS OF AIRCRAFT CABIN AIR CONTAMINATIONS H. Tao, CAPEChina Aero-Polytechnology Establishment, China; L. Haixia¹, Y. Ning¹; ¹China Aero-Polytechnology Establishment, China | ||||
15:00 | 15:30 | 9.9.5 |
NUMERICAL ANALYSIS METHOD OF CIVIL AIRCRAFT DITCHING FLOATING PERFORMANCE H. Wang¹, H. Wang¹; ¹Shanghai Aircraft Design and Research Institute, China |
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13:00 | 13:30 | 10.9.1 |
VIRTUAL FLIGHT TEST OF A BWB AIRCRAFT IN LOW SPEED WIND TUNNEL B. Nie¹, F. Cen¹, Z. Liu¹, T. Guo¹, H. Sun¹; ¹China Aerodynamics Research and Development Center, China | ||||
13:30 | 14:00 | 10.9.2 |
BAYESIAN APPROACH TO SIMULTANEOUS STATIC AND DYNAMIC FLIGHT CHARACTERISTICS MODELING M. Naruoka, JAXA, Japan | ||||
14:00 | 14:30 | 10.9.3 |
THE ANALYSIS OF TAKEOFF ROTATION OF SUBSCALE FREE-FLIGHT K. Ma¹, L.-B. Wang¹, H. Du¹, W. Wang¹, W.-T. Gu¹; ¹AVIC THE FIRST AIRCRAFT INSTITUTE, China | ||||
14:30 | 15:00 | 10.9.4 |
ESTIMATION OF WIND BY ESTIMATING DERIVATIVES OF A LATERAL-DIRECTIONAL MOTION MODEL L.H. Son¹, Y. Ochi¹; ¹National Defense Academy, Japan |
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13:00 | 13:30 | 11.9.1 |
AN OBJECTIVE APPROACH FOR MEASURING INTERMITTENCY IN THE TRANSITIONAL BOUNDARY LAYER D. Veerasamy, Khalifa University, United Arab Emirates; C. Atkin, University of East Anglia, United Kingdom | ||||
13:30 | 14:00 | 11.9.2 |
DYNAMIC TRAILING-EDGE FLAP MOVEMENT AS A NON-CONVENTIONAL AERODYNAMIC LIFT MECHANISM M. Bremm¹, R. Stephan¹, R. Hörnschemeyer¹, E. Stumpf¹; ¹RWTH Aachen University, Germany | ||||
14:00 | 14:30 | 11.9.3 |
APPLIED RESEARCH ON SUPERVISED LEARNING IN THE JUDGMENT OF AIRFOIL TRANSITION B.B. Wei¹, Y.W. Gao¹, D. Li¹; ¹Northwestern Polytechnical University, China | ||||
14:30 | 15:00 | 11.9.4 |
TOTAL TEMPERATURE MEASUREMENTS IN WATER INJECTION AND PRE-COMPRESSOR COOLING TECHNOLOGY X. Geng¹, X.P. Liu¹, Z.Y. Song¹, L. Zhang¹; ¹AECC Shenyang Engine Research Institute, China | ||||
15:00 | 15:30 | 11.9.5 |
MICROPHONE ARRAY TECHNIQUES FOR TRAILING EDGE NOISE BASED ON CONVOLUTIONAL NEUTRAL NETWORK Z.C. Song¹, P.Q. Liu¹, H. Guo¹; ¹Beihang Univerisity, China |
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08:00 | 08:30 | 1.10.1 |
STUDY OF THE BENEFITS OF A SEMI-MORPHING WING CONCEPT L.P. Ruiz Calavera¹, S. De Lucas Bodas¹, D.E. Funes Sebastian¹; ¹Airbus Defence & Space, Spain | ||||
08:30 | 09:00 | 1.10.2 |
LANDING PLATFORM FOR URBAN AIR MOBILITY VEHICLES INTEGRATED INTO PARKING LOT INFRASTRUCTURE IN DENSELY BUILT-UP AREAS P. Brusberg¹, A.C. Doberts¹, T.M. Jansen¹, T. Witt¹; ¹HAW Hamburg, Germany | ||||
09:00 | 09:30 | 1.10.3 |
CIRCULATION CONTROL AIRCRAFT: RECENT DEVELOPMENTS OF THE CHANNEL-WING DESIGN M.F. Abdul Hamid¹, A.R. Abu Talib¹, A.S. Mohd Rafie¹, H. Djojodihardjo, The Institute for the Advancement of Aerospace Science and Tech, Indonesia; ¹Universiti Putra Malaysia, Malaysia |
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08:00 | 08:30 | 2.10.1 |
IFAR - INFRASTRUCTURE DATABASE R. Degenhardt, DLR, Germany; D. Paraschivoiu, NRC, Canada | ||||
08:30 | 09:00 | 2.10.2 |
SOL-GEL BASED ORGANIC-INORGANIC HYBRID COATINGS FOR CORROSION PROTECTION OF AEROSPACE ALUMINIUM ALLOY R.V. Lakshmi¹, S.T. Aruna¹, S. Sampath, Indian Institute of Science, India; ¹CSIR-National Aerospace Laboratories, India |
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08:00 | 08:30 | 3.10.1 |
APPLICATION OF A SKEWED-SLOT CASING TREATMENT IN A HIGH-LOADING AXIAL-CENTRIFUGAL COMPRESSOR H.-L. Jin, China; D.-B. Qiu, China; Y.-Q. Yin, China; X.-Q. Zou, China | ||||
08:30 | 09:00 | 3.10.2 |
DISTORTION PLATE DESIGN, SIMULATION VALIDATION AND TEST SCHEME FOR STABILITY ANALYSIS ON A FAN COMPONENT OF AN AEROENGINE Z.-P. Li, AECC Shenyang Engine Research Institute, China | ||||
09:00 | 09:30 | 3.10.3 |
EFFECT OF INTER-STAGE BLEEDING ON FLOW STABILITY OF A MULTI-STAGE COMPRESSOR X. Liu, China; H. Jin, China; D. Qiu, China; Y. Yin, China |
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08:00 | 08:30 | 4.10.1 |
GEOMETRICAL PARAMETER STUDY OF A HYPERSONIC VERTICAL GAP FLOW H.-Y. Zhang, State Key Laboratory of Aerodynamics, China; W.-G. Zong¹, Y.-H. Zhu¹, Y.-W. Gui, Computational Aerodynamics Institute, CARDC, China; B. Qiu, State Key Laboratory of Aerodynamics, China; ¹University of Sichuan, China | ||||
08:30 | 09:00 | 4.10.2 |
ATMOSPHERIC TURBULENCE EFFECTS ON SONIC BOOM PROPAGATION Z. Qian¹, Y. Leng¹; ¹AVIC Aerodynamics Research Institute, China | ||||
09:00 | 09:30 | 4.10.3 |
NUMERICAL SIMULATION OF PITCHING MOTION EFFECTS ON THE AERODYNAMIC PERFORMANCE OF DRAGONFLY-LIKE FLAPPING WING X.-Y. Lang¹, B.-F. Song¹, W.-Q. Yang¹; ¹Northwestern Polytechnical University, China |
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08:00 | 08:30 | 5.10.1 |
INFLUENCE OF VARIABLE WALL PERFORATION RATIO ON BOUNDARY LAYER PARAMETERS AT TRANSONIC SPEEDS S.L. Osipova, Russia |
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08:00 | 08:30 | 6.10.1 |
TRAJECTORY GENERATION AND CONTROL FOR PERCHING MANEUVERING WITH QUADROTOR Y. Sun, Northwestern Polytechnical University, China; M. Chang¹, J. Bai¹; ¹NWPU, China | ||||
08:30 | 09:00 | 6.10.2 |
DEVELOPMENTS TOWARDS A TOOLCHAIN FOR UAV FLIGHT DYNAMIC MODELS IN EARLY DESIGN S.J. Koeberle¹, M. Hornung¹; ¹Institute of Aircraft Design, TUM, Germany | ||||
09:00 | 09:30 | 6.10.3 |
NEW ROLL-SPIRAL COUPLING MODE CRITERION FOR HIGH-SPEED VEHICLES G.H. Dou¹, Y.J. Yang¹, A.L. Gong¹, W.J. Zhou¹; ¹China Academy of Aerospace Aerodynamics, China |
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08:00 | 08:30 | 7.10.1 |
NUMERICAL EVALUATION OF DYNAMIC STABILITY DERIVATIVES FOR HIGH LIFT DEVICES H. Ur Rahman¹, A. Maqsood¹, R. Riaz¹, L. Dala, Northumbria University, United Kingdom; ¹National University of Sciences & Technology, Pakistan | ||||
08:30 | 09:00 | 7.10.2 |
ADJOINT-BASED STUDY OF THE AERODYNAMIC CENTER SHIFT IN THE TRANSONIC FLOW REGIME A. Cato¹, M. Hayashi, Federal University of ABC, Brazil; J. Cavalcante¹, J. Qasem, Technical University of Munich, Germany; L. Kavabata¹, U. Costa¹, E. Volpe¹; ¹University of São Paulo, Brazil | ||||
09:00 | 09:30 | 7.10.3 |
NASA-CRM LATERAL-DIRECTIONAL STABILITY DERIVATIVES COMPARISON BETWEEN SEMI-EMPIRICAL, VORTEX LATTICE AND PANEL METHOD R. Sorbilli Cardoso de Sousa¹, R.G. Annes da Silva¹; ¹Instituto Tecnologico de Aeronautica, Brazil |
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08:00 | 08:30 | 8.10.1 |
MATHEMATICAL MODELS FOR ANALYSIS AND OPTIMIZATION OF AIRCRAFT STRUCTURAL COMPONENTS TAKING INTO CONSIDERATION OF LOCAL STRESS DISTRIBUTION V. Chedrik¹, S. Tuktarov¹, K. Balunov¹, N. Nguyen, Moscow Institute of Physics and Technology, Russia; ¹Central Aerohydrodynamic Institute, Russia | ||||
08:30 | 09:00 | 8.10.2 |
A METHOD FOR CALCULATING TORSION ANGLE OF FLEXIBLE RETICULAR TUBE AT DIFFERENT POSITIONS Y.C. Deng, SADRI, China; Y. Yang, ASRI, China; Y.Q. He, SIA, China; C. Sun, CAE, China; F. Qui, SAU, China | ||||
09:00 | 09:30 | 8.10.3 |
SPECIALIZED SOFTWARE DEVELOPMENT FOR BUILDING BLOCK APPROACH INTEGRATION IN FULL-SCALE STATIC TESTS E.M. Kolman¹, D.V. Kurulyuk¹, E.A. Levchenko¹, M.V. Limonin¹; ¹Central Aerohydrodynamic Institute named after N.E. Zhukovsky, Russia |
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08:00 | 08:30 | 9.10.1 |
FITT’S LAW WITH EYE TRACKING ON A FLIGHT SIMULATOR COCKPIT M.A. Rodriguez Diaz¹, E. Villani¹, P. Krus, Linköping University, Sweden; ¹Aeronautics Institute of Technology, Brazil | ||||
08:30 | 09:00 | 9.10.2 |
ANALYSIS AND SOLUTION RESEARCH OF THE AIR DATA LOSSFROM AIRCRAFT FOR ENGINE CONTROL L. Jing, COMAC Sadri, China | ||||
09:00 | 09:30 | 9.10.3 |
AN AGILE PRACTICE OF AVIONICS SYSTEM DEVELOPMENT L. Dong¹, W.-M. Song¹; ¹China Aeronautical Radio Electronics Research Institute, China |
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08:00 | 08:30 | 10.10.1 |
AERODYNAMICS DESIGN, OPTIMIZATION AND FLOW FIELD INVESTIGATION OF A CONTRA-ROTATING PROPFAN AT HIGH FLIGHT MACH NUMBERS T. Wu¹, Z. Li¹, W. Dong¹; ¹Shanghai Jiao Tong University, China | ||||
08:30 | 09:00 | 10.10.2 |
STUDY OF NON-ROTATING MICROPHONE ARRAY FOR SPINNING DUCT MODE DETECTION J.Y. Ying¹, X.B. Wang¹, J. Kang¹, M.H. Lu¹; ¹AECC commercial Aircraft Engine Co.,Ltd., China | ||||
09:00 | 09:30 | 10.10.3 |
MODELING OF COUNTER-ROTATING LIFT FAN/MAIN ENGINE COMBINED PROPULSION SYSTEM AND LIFT FAN AERODYNAMIC DESIGN H.-L. Jin, China; X. Chen, China; D.-B. Qiu, China; Y.-Q. Yin, China |
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08:00 | 08:30 | 11.10.1 |
LEARNING FLIGHT CONTROL SKILLS BY IMITATING EXPERT DEMONSTRATIONS R. Takase, The University of Tokyo, Japan | ||||
08:30 | 09:00 | 11.10.2 |
FEEDBACK ERROR LEARNING WITH ENHANCED SAMPLING: NEURAL FAULT TOLERANT CONTROLLER OF AIRCRAFT N. Yoshikawa, Mitsubishi Electric, Japan; S. Suzuki, The university of Tokyo, Germany |
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10:00 | 10:30 | 1.11.1 |
VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WING G. Song¹, W. Cheng¹, Y. Yang², Z. Qian³, W. Ge*, Y. Zhang*, Z. Wang², S. Zhang², X. Shi², C. Li³; ¹Aviation Industry Development Research Center of China, China ;²Aircraft strength research Institute of China, China ;³AVCI Aerodynamics Research Institute, China ;*Northwestern Polytechnical University, China | ||||
10:30 | 11:00 | 1.11.2 |
EVALUATION AND VALIDATION OF AEROELASTIC ANALYSIS PROGRAM FOR THE “AEROSTRUCT” WING OPTIMIZATION PLATFORM S.-B. Ling¹, K.-S. Zhang, Northwestern polytechnical university, China; Z.-H. Han¹, Z.-J. Gao, Xiantianjihangtong Technology CO. Ltd., China; ¹Northwestern Polytechnical university, China | ||||
11:00 | 11:30 | 1.11.3 |
ON WINGS WITH NON-ELLIPTIC LIFT DISTRIBUTIONS E. Bragado-Aldana¹, M.M. Lone¹, A. Riaz¹; ¹Cranfield University, United Kingdom | ||||
11:30 | 12:00 | 1.11.4 |
A HIERARCHICAL STRUCTURAL MODEL FOR CONCEPTUAL DESIGN OF TRANSPORT AIRCRAFT WING Y.K. Yin¹, W.B. Song¹; ¹Shanghai Jiao Tong University, China | ||||
12:00 | 12:30 | 1.11.5 |
MULTIFIDELITY AERODYNAMIC/STEALTH DESIGN OPTIMIZATION METHOD FOR FLYING WING AIRCRAFT Z.-Q. Liu¹, W.-P. Song¹, Z.-H. Han¹, Y. Wang¹; ¹Northwestern Polytechnical University, China |
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10:00 | 10:30 | 2.11.1 |
IMPACT OF NEW TECHNOLOGIES ON AIRCRAFT SYSTEMS A. Berres¹, P. Niemeyer¹; ¹German Aerospace Center (DLR), Germany | ||||
10:30 | 11:00 | 2.11.2 |
FAST METHOD AND AN INTEGRATED CODE FOR SONIC BOOM PREDICTION OF SUPERSONIC COMMERCIAL AIRCRAFT Y.-L. Ding¹, Z.-H. Han¹, J.-L. Qiao¹, W.-P. Song¹, B.-F. Song¹; ¹Northwestern Polytechnical University, China | ||||
11:00 | 11:30 | 2.11.3 |
INTEGRATION OF FUSELAGE-MOUNTED OVER-WING ENGINES ON A MID-RANGE AIRCRAFT P. Wegener, DLR - German Aerospace Center, Germany | ||||
11:30 | 12:00 | 2.11.4 |
AERODYNAMIC DESIGN OPTIMIZATION OF WAVERIDER-DERIVED VEHICLE W. Su ¹, C. Dong¹, X.P. Wang, Shanghai Electro-Mechanical Engineering Institute, Shanghai, China; Y.T. Zuo, National Key Laboratory of Aerodynamic Design and Research, Nort, China; ¹Beijing Institute of Space Long March Vehicle, China | ||||
12:00 | 12:30 | 2.11.5 |
MULTI-MISSION TANKER-TRANSPORT CONVERSION I. Berlowitz, IBAero Engineering, Israel |
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10:00 | 10:30 | 3.11.1 |
TRANSITION PREDICTION FOR TRANSPORT AIRCRAFT CONFIGURATIONS BASED ON OVERSET GRID Y.-M. Du, Shenyang Aerospace University, China; Z.-H. Gao¹, C. Pang¹; ¹Northwestern Polytechnical University, China | ||||
10:30 | 11:00 | 3.11.2 |
A CONTRIBUTION TO THE SIMULATION OF TRANSITIONAL FLOWS OVER AEROSPACE CONFIGURATIONS L.M.M.O. Carvalho, Instituto Tecnologico de Aeronautica, Brazil; R.G. da Silva¹, J.L.F. Azevedo¹; ¹Instituto de Aeronautica e Espaco, Brazil | ||||
11:00 | 11:30 | 3.11.3 |
AERODYNAMICS CHARACTERISTICS STUDY ON A NATURE LAMINAR FLOW AIRFOIL OF NEAR-SPACE VEHICLE AT LOW REYNOLDS NUMBERS F. Cui, Innovation & Research Institute of HIWING Technology Academy, China; H. Zhang, HIWING Technology Academy, China | ||||
11:30 | 12:00 | 3.11.4 |
HYBRID NUMERICAL SCHEMES IN PREDICTION OF HIGH-SPEED LAMINAR-TURBULENT TRANSITION I.V. Egorov, Russia; A.V. Novikov, Russia; N.K. Nguen, Vietnam | ||||
12:00 | 12:30 | 3.11.5 |
A LOCAL CORRELATION-BASED ALGEBRAIC TRANSITION MODEL WITH COMPRESSIBILITY AND CROSSFLOW CORRECTION R.X. Xie¹, W.M. Sang¹; ¹Northwestern Polytechnical University, China |
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10:00 | 10:30 | 4.11.1 |
MODELING AND SIMULATION OF DUSTY GAS FLOW IN AERODYNAMICS Y.M. Tsirkunov¹, D.A. Romanyuk¹, S.V. Panfilov¹; ¹Baltic State Technical University, Russia | ||||
10:30 | 11:00 | 4.11.2 |
AN INTELLIGENT STRUCTURED CHIMERA GRID APPROACH FOR MOVING OBJECTIVES L. Li, Northwestern Polytechnical University, China; Y. Liang¹, Y. Huai¹; ¹AVIC Aeronautics Computing Technique Research Institute , China | ||||
11:00 | 11:30 | 4.11.3 |
METHODS OF DIRECTIONAL COARSENING FOR UNSTRUCTURED GRIDS AND APPLICATIONS Z.-Y. Xiao¹, L. Zhang¹, X.-D. Cui¹, B. Mou¹; ¹China aerodynamics research and development center , China | ||||
11:30 | 12:00 | 4.11.4 |
AN ACCELERATION METHODOLOGY BASED ON DISTURBANCE REGION UPDATE METHOD FOR STEADY COMPRESSIBLE FLOWS S. Hu¹, C. Jiang¹, Z. Gao¹, C.-H. Lee¹; ¹Beihang University, China |
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10:00 | 10:30 | 5.11.1 |
EXPERIMENTAL INVESTIGATION OF DAMAGE WING IMPACT ON THE AIRLINER AERODYNAMIC CHARACTERISTICS A. Krzysiak, Lukasiewicz Research Network – Institute of Aviation, Poland; A. Olejnik¹, L. Kiszkowiak¹; ¹Faculty of Mechatronics, Armament & Aerospace; Military Universi, Poland | ||||
10:30 | 11:00 | 5.11.2 |
WIND-TUNNEL INVESTIGATION OF COMMERCIAL TRANSPORT AIRCRAFT STATIC AND DYNAMIC AERODYNAMIC CHARACTERISTICS AT EXTREME FLIGHT CONDITIONS L. Zhang, Beihang University, China; Z. Liu¹, F. Cen¹, Y. Jiang¹, H. Sun¹; ¹China Aerodynamic Research and Development Center, China | ||||
11:00 | 11:30 | 5.11.3 |
EXPERIMENTAL INVESTIGATION OF THE CHN-T1 MODEL IN FL-13 WIND TUNNEL OF CARDC AND DNW-LLF FACILITY L. Fan¹, H. Zhang¹; ¹China Aerodynamics Research and Development Center, China | ||||
11:30 | 12:00 | 5.11.4 |
STUDY ON AERODYNAMIC CHARACTERISTICS OF LIGHT CONVERTIBLE AIRCRAFT MODEL V.I. Chernousov¹, A.A. Krutov¹, E.A. Pigusov¹; ¹Central Aerohydrodinamic Institute (TsAGI), Russia | ||||
12:00 | 12:30 | 5.11.5 |
EXPERIMENTAL INVESTIGATIONS OF A FULL MODEL WITH ADAPTIVE ELASTO-FLEXIBLE MEMBRANE WINGS J. Pflüger¹, K. Hirschmann¹, C. Breitsamter¹; ¹Chair of Aerodynamics and Fluid Mechanics, TUM, Germany |
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10:00 | 10:30 | 6.11.1 |
RESEARCH ON STRUCTURAL DESIGN OF TAIL BOOM FOR AN UNMANNED HELICOPTER C.-G. Yang¹, Z.-Q. Tian¹; ¹China Helicopter Design and Research Institute, China | ||||
10:30 | 11:00 | 6.11.2 |
ON THE DEVELOPMENT OF FUSELAGE WEIGHT ESTIMATION TOOL INTO AIRCRAFT MULTIDISCIPLINARY DESIGN ENVIRONMENT H. Wang¹, H. Wang¹; ¹Shanghai Aircraft Design and Research Institute, China | ||||
11:00 | 11:30 | 6.11.3 |
AN INTEGRATED AERODYNAMIC/THERMAL/STRUCTURAL DESIGN FRAMEWORK FOR HYPERSONIC VEHICLES C. Li¹, Z.Q. Wan¹, X. Wang¹; ¹Beihang University, China | ||||
11:30 | 12:00 | 6.11.4 |
A DYNAMIC SELF-CONTROL ERR STRATEGY FOR BI-DIRECTIONAL EVOLUTIONARY STRUCTURAL OPTIMIZATION H. Zhang¹, Q. Zhang¹; ¹Sun Yat-sen University, China | ||||
12:00 | 12:30 | 6.11.5 |
DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: STRUCTURAL DESIGN AND OPTIMIZATION C. Surace¹, R. Roy¹, M. Civera¹, D. Allaio¹, R. Barbieri¹, A. Grava¹, R. Tufilli¹, P. Gili¹; ¹Politecnico di Torino, Italy |
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10:00 | 10:30 | 7.11.1 |
SPARSE POLYNOMIAL CHAOS EXPANSION BASED ON FULLY ADAPTIVE FORWARD-BACKWARD SELECTION METHOD H. Zhao, Sun Yat-sen University, China; Z.H. Gao¹, L. Xia¹; ¹Northwestern Polytechnical University, China | ||||
10:30 | 11:00 | 7.11.2 |
RAPID THEORETICAL EVALUATION OF FORMATION FLIGHT PERFORMANCE R. Vilumbrales-Garcia¹, M. Lone¹; ¹Cranfield University, United Kingdom | ||||
11:00 | 11:30 | 7.11.3 |
IMPROVED WEIGHTED GRADIENT-ENHANCED KRIGING MODEL FOR HIGH-DIMENSIONAL AERODYNAMIC MODELING PROBLEMS C.-Z. Xu¹, Z.-H. Han¹, K.-S. Zhang¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China | ||||
11:30 | 12:00 | 7.11.4 |
DESIGN OPTIMIZATION OF AIRFOILS AT ULTRA-LOW REYNOLDS NUMBERS J.-H. Xu¹, D. Li¹, W.-P. Song¹, Z.-H. Han¹, H.-J. Li¹; ¹Northwestern Polytechnical University, China | ||||
12:00 | 12:30 | 7.11.5 |
THE AERODYNAMIC OPTIMIZATION AND TRIM CHARACTERISTICS RESEARCH ON VARIABLE CAMBER WING OF WIDE-BODY CIVIL TRANSPORT X. Hao¹, C. Su¹, B. Wang¹, Q.Q. Zhang¹; ¹China Academy of Aerospace Aerodynamics, China |
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10:00 | 10:30 | 8.11.1 |
STRUCTURAL VIBRATION CONTROL BY USING THE ENERGY FROM DIFFERENT MODES K. Li¹, C. Bai¹; ¹Aircraft strength research institute, China | ||||
10:30 | 11:00 | 8.11.2 |
MODEL REDUCTION AND STOCHASTIC UPDATING OF A VIBRATING SYSTEM I. Isnardi¹, E. Menga, Airbus Operations S.L, Spain; J.E. Mottershead¹, S. Fichera¹; ¹University of Liverpool, United Kingdom | ||||
11:00 | 11:30 | 8.11.3 |
MODAL DAMPING PARAMETER IDENTIFICATION METHOD BASED ON IMPROVED VMD AND ENVELOPE FITTING AND ITS APPLICATION J. Bian¹, Y.-N. Chen¹, Q. Mei¹, Y.-L. Xu¹, Y.-H. Lu¹; ¹AECC Hunan Aviation Powerplant Research Institute, China | ||||
11:30 | 12:00 | 8.11.4 |
A PERTURBATION ANALYSIS OF NONLINEARITY IN LANDING-GEAR SHIMMY OF A FLEET AIRCRAFT M. Kou, AECC CAE, China; J. Zhang¹, J. Lu¹, S. Tan¹; ¹AVIC The First Aircraft Institute, China | ||||
12:00 | 12:30 | 8.11.5 |
NUMERICAL SIMULATION AND EXPERIMENTAL INVESTIGATION ON FLUTTER AND NON-SYNCHRONOUS VIBRATION Y.X. Liu¹, D. Mo¹, Q. Du¹, Y.Z. Chen¹, M. Wang¹; ¹AECC Shenyang Engine Research Institute, China |
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10:00 | 10:30 | 9.11.1 |
CONCEPTUAL STUDY OF THE DIGITAL HYDRAULIC ACTUATOR WITH PROPORTIONAL CONTROL FOR FLIGHT CONTROL ACTUATION SYSTEMS A. Dell'Amico, Saab AB/Linköping University, Sweden; F. Larsson¹, C. Johansson¹, V. De Negri, Federal University of Santa Catarina, Brazil; P. Krus, Linköping University, Sweden; ¹Saab AB, Sweden | ||||
10:30 | 11:00 | 9.11.2 |
VIRTUAL PROTOTYPING OF ELECTRICAL THSA FOCUSED ON MECHANICAL POWER TRANSMISSION FUNCTIONS J. Fu¹, C. Zheng¹, J.-C. Mare, Institute Clément Ader (CNRS UMR 5312), INSA-Toulouse, France; W. Zhang¹; ¹School of Mechanical Engineering and Automation, Beihang Univ., China | ||||
11:00 | 11:30 | 9.11.3 |
THE DEVELOPMENT OF ALGORITHMS FOR EMA FAULT EARLY DETECTION SYSTEM S. Bazhenov¹, A. Skryabin¹, G. Veresnikov, Institute of Control Science of Russian Academy of Science, Russia; ¹Central Aerohydrodynamic Institute of Russia, Russia | ||||
11:30 | 12:00 | 9.11.4 |
AN ONTOLOGICAL APPROACH FOR CLASSIFYING AIRCRAFT ACTUATORS F. Larsson¹, C. Reichenwallner², A. Dell'Amico¹, P. Krus²; ¹Saab AB, Sweden ;²Linköping University, Sweden | ||||
12:00 | 12:30 | 9.11.5 |
EVALUATION ASPECT MAPPING FOR ACTUATION SYSTEM DESIGN C. Reichenwallner¹, F. Larsson², A. Dell 'Amico², P. Krus¹; ¹Linköping university, Sweden ;²Saab AB, Sweden |
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10:00 | 10:30 | 10.11.1 |
RESEARCH OF PROPULSION-SYSTEM-SURROGATE-MODELING METHOD USING INFILL CRITERION SAMPLES D.-C. Wang¹, B.-F. Song¹, H.-F. Wang¹, J. Jiao, Chinese Academy of Sciences, China; ¹Northwestern Polytehnical University, China | ||||
10:30 | 11:00 | 10.11.2 |
THE CAPABILITIES OF AUTOMATION OF MDAO PROBLEM STATEMENT AT COLLABORATIVE CONCEPTUAL DESIGN OF THE PROPULSION SYSTEM USING OPEN SOURCE SOFTWARE TOOLS L. Mirzoyan¹, A. Mirzoyan¹, A. Isyanov¹; ¹CIAM, Russia | ||||
11:00 | 11:30 | 10.11.3 |
CONCEPTUAL STUDIES OF DIFFERENT TYPE OF HYBRID ELECTRIC PROPULSION SYSTEMS FOR COMMUTER AIRLINERS V.S. Zakharchenko¹, A.N. Varyukhin¹, D.Y. Rakhmankulov¹, P.S. Suntsov¹, M.A. Ovdienko¹, M.V. Gordin¹; ¹Central Institute of Aviation Motors (CIAM), Russia | ||||
11:30 | 12:00 | 10.11.4 |
IMPLEMENTATION OF DISTRIBUTED ELECTRIC PROPULSION ON A GENERAL AVIATION AIRCRAFT M.A. Gallani¹, L.C.S. Góes¹, L.A.R. Nerosky, Embraer, Brazil; ¹Instituto Tecnológico de Aeronáutica, Brazil | ||||
12:00 | 12:30 | 10.11.5 |
INVESTIGATION OF VARIABLE GEOMETRIES ON THE OPERABILITY AND AIRCRAFT LEVEL PERFORMANCE OF A THREE-SHAFT TURBOFAN ENGINE FOR ENTRY INTO SERVICE 2050 D. Mo¹, Y.X. Liu¹, I. Roumeliotis², D. Nalianda²; ¹AECC Shenyang Engine Research Institute, China ;²Cranfield University, United Kingdom |
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10:00 | 10:30 | 11.11.1 |
AIRCRAFT AUTOPILOT DESIGN USING ASYMMETRIC VARIABLE-SPAN WING MORPHING J. Lee¹, S. Kim¹, S. Jung¹, H. Lee¹, Y. Kim¹; ¹Seoul National University, South Korea | ||||
10:30 | 11:00 | 11.11.2 |
AUTONOMOUS FLIGHT CONTROL BASED ON NEURAL NETWORKS AND FUZZY DECISION P.C. Wen, China; C.H. Zou, China; Z. Gao, China; J.G. Sun, China | ||||
11:00 | 11:30 | 11.11.3 |
TWISTOR BASED 6-DOF DISTRIBUTED ADAPTIVE LEADER-FOLLOWING CONTROL FOR MULTIPLE RIGID SPACECRAFT FORMATION B. Zhang¹, F. Li, China Academy of Launch Vehicle Technology, China; J. Bai¹; ¹Northwestern Polytechnical University, China | ||||
11:30 | 12:00 | 11.11.4 |
DEVELOPMENT OF A HUMAN PILOTED AIR COMBAT ENGAGEMENT DATABASE T. Xue¹, J.Y. Ma¹, J.R. Wen¹, X.H. Yang, Science and Technology on Avionics Integration Laboratory, China; Y.Q. Dong¹, J.L. Ai¹; ¹Fudan University, China | ||||
12:00 | 12:30 | 11.11.5 |
LEARNING-BASED MIDCOURSE GUIDANCE FOR VELOCITY MAXIMIZATION WITH ANGULAR CONSTRAINT T. Jin¹, H. Li¹, S. He¹, Y. Li¹; ¹Beijing Institute of Technology, China |