30th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

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Attention: Be advised that there might be changes till the congress, so please do not adjust your travel plans based on this preliminary programme.
7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room

Monday, 06. Sep 2021

7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
07:00 - 08:00Registration

08:00 - 09:00Opening Ceremony

0.1ICAS Daniel & Florence Guggenheim Memorial Lecture, Yesterday,Today & Tomorrow of AVIC, Yang Wei, China
Chair: S. Suzuki ICAS President
06. Sep 21 09:00 10:00

10:00 - 10:30Break

1.1China Aviation 1
Chair(s): ,
Track 1
12 - Host nation
2.1Unconventional Configuration
Chair(s): Kimmel, B.
Track 2
01 - Aircraft Design and Integrated Systems
06. Sep 21 10:30 11:00 2.1.1 A CONCEPTUAL DESIGN OF LSA CLASS AMPHIBIOUS AIRCRAFT
S. Hanada, Sophia University, Japan
06. Sep 21 11:00 11:30 2.1.2 AEROELASTIC OPTIMIZATION OF A BLENDED WING BODY AIRCRAFT CONSIDERING STABILITY/CONTROL CONSTRAINTS
X.Z. Wang, Beihang University, China
06. Sep 21 11:30 12:00 2.1.3 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
Reserve Paper 2.1.R STUDY ON ADJOINT BASED OPTIMIZATION OF BWB CONFIGURATION CONSIDERING THE INTAKE AND EXHAUST EFFECTS
J.-T. Huang¹, Z. Zhou¹, Z.-H. Gao, Northwestern Polytechnical University, China; X. Chen¹, S.-D. Zhong¹; ¹China Aerodynamics Research and Development Center, China
3.1Design architecture & integration methodology 1
Chair(s): Vian, J.
Track 3
02 - Systems Engineering and Integration
06. Sep 21 10:30 11:00 3.1.1 STRATEGIES TO ENHANCE CONFIGURATIONS FOR HIGH-PRECISION MULTI-DISCIPLINARY OPTIMIZATION
hua liu¹, ronggang zhu¹; ¹Science and Technology on Electro-optic Control Laboratory, China
06. Sep 21 11:00 11:30 3.1.2 SYSTEM ARCHITECTING: THE ARCHITECTURE DESIGN PROBLEM AS A GRAPH
J.H. Bussemaker¹, P.D. Ciampa¹, B. Nagel¹; ¹DLR, Germany
06. Sep 21 11:30 12:00 3.1.3 AIRCRAFT CRUISE PERFORMANCE DESIGN INTEGRATION BASED ON SYSTEM ENGINEERING
HE BIHAI¹, HUA ZHEN¹; ¹COMAC, China
4.1Unsteady Aerodynamics 1
Chair(s): Mello, O., Pezzella, G.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
06. Sep 21 10:30 11:00 4.1.1 A COMPARISON OF QUASI-STEADY STATE AND UNSTEADY COMPUTATIONAL METHODS FOR PITCH DAMPING DERIVATIVE ESTIMATES
T Bykerk, Australia
06. Sep 21 11:00 11:30 4.1.2 NONLINEAR UNSTEADY AERODYNAMIC DESCRIPTIONS BASED ON IMPROVED GOMAN\\\'S MODEL
Xiao-jun WU¹, Dong HAO¹, Hong-yin JIA¹, Shen-shen LIU¹; ¹CARDC, China
06. Sep 21 11:30 12:00 4.1.3 DATA FUSION UNSTEADY AERODYNAMIC MODELING BASED ON EXPERIMENTAL DATA
X W Wang, China
Reserve Paper 4.1.R HIGHER ORDER DERIVATIVES OF UNSTEADY AERODYNAMICS OF AIRFOIL ASSOCIATED WITH FORCED PITCHING/PLUNGING MOTIONS
Q ZHANG, Xi'an Aeronautical University, China
Reserve Paper 4.1.R EFFECT OF MACH NUMBER AND ANGLE OF ATTACK ON AERODYNAMICS OF OA309 AIRFOIL
Y. J. Jin, Northwestern Polytechnical University, China
5.1Full Configuration Test 1
Chair(s): Chen, Y., Ivanov, A.
Track 5
03.2 - Experimental Aerodynamics
06. Sep 21 10:30 11:00 5.1.1 EXPERIMENTAL INVESTIGATION OF DAMAGE WING IMPACT ON THE AIRLINER AERODYNAMIC CHARACTERISTICS
Andrzej: A Krzysiak, 1?ukasiewicz Research Network – Institute of Aviation, Poland; Aleksander: A Olejnik¹, ?ukasz: ? Kiszkowiak¹; ¹Faculty of Mechatronics, Armament & Aerospace; Military Universi, Poland
06. Sep 21 11:00 11:30 5.1.2 WIND-TUNNEL INVESTIGATION OF AERODYNAMIC CHARACTERISTICS FOR COMMERCIAL TRANSPORT AIRCRAFT AT EXTREME FLIGHT CONDITIONS
ZHANG Lei, Beihang University, China; LIU Zhitao¹, CEN Fei¹, JIANG Yong¹, SUN Haisheng¹; ¹China Aerodynamic Research and Development Center, China
06. Sep 21 11:30 12:00 5.1.3 EXPERIMANTAL INVESTIGATION OF THE CHN-T1 MODEL IN FL-13 WIND TUNNEL OF CARDC AND DNW-LLF FACILITY
F.L.T Fan, CARDC, China
6.1Cavity Flows
Chair(s): Breitsamter, C., Prince, S.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
06. Sep 21 10:30 11:00 6.1.1 COMPUTATIONAL STUDY OF THREE-DIMENSIONAL OPEN CAVITY FLOWS
Yong Luo, China; Conghai Wu, China; Hao Tian, China; Hu Li, China; Shuhai Zhang, China
06. Sep 21 11:00 11:30 6.1.2 NUMERICAL STUDY OF THE SIDEWALL EFFECTS ON THE OSCILLATORY SHEAR LAYER IN THE CAVITY FLOW OF HIGH REYNOLDS NUMBER
Q.-L. GUO, China
06. Sep 21 11:30 12:00 6.1.3 DETACHED-EDDY SIMULATIONS OF LEADING EDGE PLATE FLOW CONTROL BEFORE HIGH-SPEED CAVITY
Pengcheng Cui¹, Jing Tang ¹, Jiangtao Chen¹, Huan Li¹, Bin Li¹, Mingsheng Ma¹; ¹China Aerodynamics Research and Development Center , China
Reserve Paper 6.1.R EXPERIMENTAL STUDY ON SUPERSONIC CAVITY ACOUSTICS
MING JIAN¹, MING WANG¹, FEI HE¹; ¹AVIC Chengdu Aircraft Design & Research Institute, China
7.1Aero Acoustics
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
06. Sep 21 10:30 11:00 7.1.1 MEDIUM-FIDELITY NOISE ASSESSMENT OF NOVEL MID RANGE TRANSPORT AIRCRAFT
M. Lummer, German Aerospace Center (DLR), Germany
06. Sep 21 11:00 11:30 7.1.2 SNGR BASED FAST ANALYSIS OF SLAT TRACK NOISE SOURCES
W Wang, Shanghai Aircraft Design and Research Institute, China
06. Sep 21 11:30 12:00 7.1.3 NUMERICAL AND EXPERIMENTAL INVESTIGATION OF A DRESSED NOSE LANDING GEAR
L.-B. Botero-Bolívar, University of São Paulo, Brazil
Reserve Paper 7.1.R AERODYNAMIC NOISE SIMULATION OF CIVIL AIRCRAFT LANDING GEARS BASED ON LATTICE BOLTZMANN LES-SMARGORINSKY MODEL
Qing Li, Chinese Aeronautical Establishment, China; Puyuan Wang ¹, Bao Chen ¹; ¹AVIC Aerodynamics Research Institute, China
Reserve Paper 7.1.R INVESTIGATION OF FLOW ACOUSTIC CHARACTERISTICS OF ROTOR-ROTOR INTERACTION FOR MULTICOPTER
Y. Jo, South Korea
8.1Aeroelastic Experimental Investigation
Chair(s): Kuzmina, S., Luber, W.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
06. Sep 21 10:30 11:00 8.1.1 TESTING INVESTIGATION OF FLEXIBLE WING LIMIT CYCLES WITH AILERON FREEPLAY NONLINEARITY
X.-F. He, Shanghai Aircraft Airworthiness Certification Center of CAAC, China
06. Sep 21 11:00 11:30 8.1.2 EXPERIMENTAL AND THEORETICAL STUDY ON FLUTTER ANALYSIS OF A VERY FLEXIBLE WING
Z.C FU , China Academy of Aerospace Aerodynamics (CAAA), China
06. Sep 21 11:30 12:00 8.1.3 THEORETICAL AND EXPERIMENTAL INVESTIGATION OF THE AEROELASTIC CHARACTERISTICS OF THE AFLONEXT PROJECT DEMONSTRATOR
G.A. Amiryants¹, A.V. Chedrik¹, V.A. Malyutin¹, S.E. Paryshev¹, V.G. Soudakov¹; ¹Central Aerohydrodynamic Institute , Russia
9.1Compressors & Turbines
Chair(s): Yimer, I.
Track 9
05 - Propulsion
06. Sep 21 10:30 11:00 9.1.1 AERODYNAMC PERFORMANCE IMPROVEMENT OF A TRANSONIC AXIAL COMPRESSOR BY SWEPT AND LEANED ROTORS
K You, Northwestern Polytechnical University, China
06. Sep 21 11:00 11:30 9.1.2 FLOW TURBULENCE INVESTIGATION AT THE LINEAR CASCADE’S OUTLET
A.D. Nepomnyashchiy, Central Institute of Aviation Motors, Russia
06. Sep 21 11:30 12:00 9.1.3 DESIGN EXPERIENCE OF PENETRATION COOLING SYSTEM FOR HIGH-TEMPERATURE TURBINE BLADES
S. Kharkovskiy, CIAM, Russia
Reserve Paper 9.1.R PROBABILISTIC ANALYSIS OF A TURBOFAN SECONDARY AIR SYSTEM BASED ON MEASURED DATA OF LABYRINTH SEALS
C.-X. Song¹, M.-C. Deng¹, Y. Fan¹, Y.-Q. Liang¹, Y. Shen¹; ¹AECC Shenyang Engine Research Institute, China
Reserve Paper 9.1.R INFLUENCE OF THE AXIAL ASSEMBLAGE DEVIATION ON PERFORMANCE OF ONE TRANSONIC CENTRIFUGAL COMPRESSOR
Wen ZHANG¹, Kailin LUO¹, Quan WEN², Fangming TANG², Xiwu LIU¹; ¹AECC HAPRI, China ;²AECC AEAC, China
10.1Computational Aeroelasticity 1
Chair(s): Amiryants, G., Luber, W.
Track 10
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
06. Sep 21 10:30 11:00 10.1.1 A COMPUTATIONAL MODEL OF 3 D.O.F. AIRFOIL FOR FLUTTER ANALYSIS WITH CFD BASED AERODYNAMIC FORCES
A.-O Alam, Dalian university of technology , China
06. Sep 21 11:00 11:30 10.1.2 COMPUTATIONAL FLUID-STRUCTURE INTERACTIONS OF A 3D FLEXIBLE FLAPPING WING
Y Guo¹, W Yang¹, Y Dong¹, X Lang¹; ¹Northwestern Polytechnical University, China
06. Sep 21 11:30 12:00 10.1.3 COMPUTATION OD ELASTIC FOR A TRANSPORT AIRPLANE FITTED WITH WINGLETS BY FLUID-STRUCTURE INTERACTION
W. M. Alves, Embraer, Brazil; B. S. Mattos¹, J. A. Hernandes¹; ¹ITA, Brazil
11.1Military Technology
Chair(s): Fu, Y., Goes, L.
Track 11
07 - Systems, Subsystems and Equipment
06. Sep 21 10:30 11:00 11.1.1 RESEARCH ON OPTIMIZATION TECHNOLOGY FOR CONTROL PARAMETERS OF EJECTION SEAT BASED ON PSO ALGORITHM
Lou Jin¹, Ming Wu¹, Hui Yang¹, Liang Wu¹, Dongyue Cui, AVIC The First Aircraft Institute, China; ¹AVIC Aerospace Life-support Industries, Ltd., China
06. Sep 21 11:00 11:30 11.1.2 MANOEUVRABLE AERIAL TARGET TRACKING IN THE PRESENCE OF STAND-OFF JAMMING
C. Tian, School of Aeronautics, Northwestern Polytechnical University, China
06. Sep 21 11:30 12:00 11.1.3 RESEARCH ON THE PRESSURE COMFORT OF PILOT’S HELMET
X. Wang, AVIC Aerospace Life Support Industries LTD, China
12.1Flight Operations
Chair(s): Vincent, J., Da Cunha, S.
Track 12
11 - Operations and Sustainment
06. Sep 21 10:30 11:00 12.1.1 MODELING THE CLIMATE IMPACT OF FORMATION FLIGHT
T. Marks, German Aerospace Center (DLR), Germany
06. Sep 21 11:00 11:30 12.1.2 A MULTI-CRITERIA SEQUENCING LOGIC FOR THE EXTENDED TERMINAL MANOEUVRING AREA CONSIDERING INTERDEPENDENT UNCERTAINTIES
T. Zeh, Technische Universität Dresden, Germany
06. Sep 21 11:30 12:00 12.1.3 ON THE AIRCRAFT OPERATIONAL INTEGRITY
Yuting He, Air Force Engineering University, China
Reserve Paper 12.1.R INTEGRATION OF SPACE VEHICLE OPERATIONS INTO THE UNITED ARAB EMIRATES AIR TRAFFIC MANAGEMENT – AN IMPACT ANALYSIS
O. Lehmann¹, R. El-Jabi¹, K.-M. Webster¹, A.-K. Rachdi¹, Z.-H. Malik¹; ¹Abu Dhabi University, United Arab Emirates
13.1Education and industry processes
Chair(s): ,
Track 13
14 - Education and Training

12:00 - 13:00Lunch

1.2MDO
Chair(s): Bagassi, S.
Track 1
01 - Aircraft Design and Integrated Systems
06. Sep 21 13:00 13:30 1.2.1 COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN
S. Görtz, DLR - German Aerospace Center, Germany
06. Sep 21 13:30 14:00 1.2.2 BLENDED WING BODY PLANFORM MULTIDSCIPLIANRY OPTIMISATION
Davide DI Pasquale¹, Divyam Verma¹, Giampaolo Pagliuca¹; ¹Cranfield University, United Kingdom
06. Sep 21 14:00 14:30 1.2.3 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
2.2Rotorcraft
Chair(s): Melkert, J.
Track 2
01 - Aircraft Design and Integrated Systems
06. Sep 21 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
06. Sep 21 13:30 14:00 2.2.2 HELICOPTER FLIGHT DYNAMICS MODELLING WITH FREE-WAKE METHOD EMBEDDED FOR ROTOR ICING ANALYSES
Guozhi Li, Chinese Aeronautical Establishment, China; Guanglin Zhang¹, Shiyong Chu¹; ¹Aviation Industry Development Research Center of China, China
06. Sep 21 14:00 14:30 2.2.3 DESIGN AND ANALYSIS METHOD OF HELICOPTER ANTI-BALLISTIC VULNERABILITY
P. Hou, School of Aeronautics, Northwestern Polytechnical University, China
Reserve Paper 2.2.R REGRESSION HIERARCHICAL KRIGING FOR NOISY DATA FUSION WITH APPLICATION TO ROTOR AERODYNAMIC DESIGN OPTIMIZATION
sw Yang, Seoul National University, South Korea
3.2Design architecture & integration methodology 2
Chair(s): Nagel, B.
Track 3
02 - Systems Engineering and Integration
06. Sep 21 13:00 13:30 3.2.1 RESEARCH ON AERO-ENGINE COLLABORATIVE DESIGN PROCESS BASED ON SYSTEM ENGINEERING
Y.-G. Chai¹, J. Tao¹, S.-P. Guo¹, W.-W. Chen¹; ¹AECC Commercial Aero Engine co. LTD, China
06. Sep 21 13:30 14:00 3.2.2 ASTRID-H: A CONCEPTUAL DESIGN METHODOLOGY AND TOOL TO SUPPORT HIGH-SPEED VEHICLE DESIGN
R. Fusaro, Politecnico di Torino, Italy
06. Sep 21 14:00 14:30 3.2.3 THE APPLICATION OF DIGITAL TWIN TECHNOLOGY IN INTELLIGENT OPERATION AND MAINTENANCE OF AERO-ENGINE
W-P Wang, Aero-Engine Academy of China, China
4.2Unsteady Aerodynamics 2
Chair(s): Mello, O., Bykerk, T.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
06. Sep 21 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
06. Sep 21 13:30 14:00 4.2.2 UNSTEADY FLOW SIMULATION AROUND MAIN LANDING GEAR USING HIERARCHICAL CARTESIAN GRID METHOD WITH IMMERSED BOUNDARY METHOD
T. Imamura, The University of Tokyo, Japan; Y. Tamaki, Tohoku University, Japan
06. Sep 21 14:00 14:30 4.2.3 NUMERICAL SIMULATION OF A BIO-INSPIRED FLEXIBLE FLAPPING-WING BASED ON EXPERIMENTAL MEASURED DEFORMATION
X.-W. Yang¹, Y. Pei¹, W.-Q. Yang¹, P. Nian¹, B.-F. Song¹; ¹Northwestern Polytechnical University, China
Reserve Paper 4.2.R ATMOSPHERIC TURBULENCE EFFECTS ON SONIC BOOM PROPAGATION
Z-S Qian, AVIC Aerodynamics Research Institute, China
Reserve Paper 4.2.R INVESTIGTION OF AERODYNAMIC INTERACTIONS BETWEEN NACA0012 AIRFOILS IN TANDEM
Muyao Li, No.2 High School of East China Normal University, China; Hongyi Xu, Fudan University, China
5.2Full Configuration Test 2
Chair(s): Ivanov, A., Chen, Y.
Track 5
03.2 - Experimental Aerodynamics
06. Sep 21 13:00 13:30 5.2.1 EXPERIMENTAL AND NUMERICAL AERODYNAMIC LOAD RESULTS ACTIONG ON THE M5/ONERA/IAE AERONAUTICAL STANDARD MODEL
M. S. Souza, IAE, Brazil
06. Sep 21 13:30 14:00 5.2.2 STUDY ON AERODYNAMIC CHARACTERISTICS OF LIGHT CONVERTIBLE AIRCRAFT MODEL
E.A. Pigusov¹, A.A. Krutov¹, V.I. Chernousov¹; ¹Central Aerohydrodinamic Institute (TsAGI), Russia
6.2Robust Control
Chair(s): Naruoka, M.
Track 6
06.1 - Flight Dynamics and Control (Control & Modelling)
06. Sep 21 13:00 13:30 6.2.1 DECENTRALIZED CONFLICT DETECTION AND RESOLUTION METHOD ACCOUNTING FOR UNCERTAINTIES OF TRAJECTORIES
Nobuhiro Yokoyama, National Defense Academy of Japan, Japan
06. Sep 21 13:30 14:00 6.2.2 AN ALTERNATIVE BUT EQUIVALENT REALIZATION OF FINITE-HORIZON SUBOPTIMAL CONTROL FOR VEHICLE LANDING
S. Zhang, China; X. Du, China; F. Liao, China; J. T. Huang, China
06. Sep 21 14:00 14:30 6.2.3 A NEW PITCH STABILITY ENHANCEMENT SCHEME FOR AEROSPACE VEHICLE
Guangming: G. M. XIAO, China Aerodynamics Research & Development Center, China
Reserve Paper 6.2.R SENSITIVITY MINIMIZATION ON A PARAMETER INTERVAL FOR ROBUST DIRECT OPTIMAL CONTROL
T. Akman, Technical University of Munich, Germany
7.2tbd2
Chair(s): ,
Track 7
8.2Aeroelasticity of Morphing Structures
Chair(s): Ritter, M., Kuzmina, S.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
06. Sep 21 13:00 13:30 8.2.1 STATIC AEROELASTIC TAILORING OF A HIGH-ASPECT-RATIO-WING FOR A SAILPLANE WITH A MORPHING FORWARD WING SECTION
Fabian Sturm¹, Gerrit Illenberger¹, David Techmer¹, Mirko Hornung¹; ¹Technical University of Munich, Germany
06. Sep 21 13:30 14:00 8.2.2 AEROSERVOELASTIC OPTIMIZATION OF A HIGH ASPECT TRANSPORT WING WITH MORPHING TRAILING EDGE
Z. Zhang, Beihang University, China
06. Sep 21 14:00 14:30 8.2.3 A COMPREHENSIVE FRAMEWORK FOR THE COUPLED NONLINEAR AEROELASTIC AND FLIGHT DYNAMIC ANALYSES OF HIGHLY FLEXIBLE AIRCRAFT
Z.-C. Zhang, Northwestern Ploytechnical University, China
9.2Controls & Software
Chair(s): Remy, S.
Track 9
05 - Propulsion
06. Sep 21 13:00 13:30 9.2.1 THE USE OF SOFTWARE “VIRTUAL ENGINE” FOR TIMELY GAS-TURBINE ENGINE FAULT LOCALIZATIONS
V.E. Volkov¹, F.D. Golberg¹, M.P. Sokolov¹, A.A. Petukhov¹; ¹Central Institute of Aviation Motors, Russia
06. Sep 21 13:30 14:00 9.2.2 AN IMPROVED IDENTIFICATION METHOD FOR ACTUATOR LOOP OF AIRCRAFT ENGINE CONTROL SYSTEM
Nan Liu, Shanghai Aircraft Design & Research Institute, Commercial Aircra, China
06. Sep 21 14:00 14:30 9.2.3 METHODS OF PROGRAMMED THRUST MANAGEMENT FOR NOISE REDUCTION OF SUPERSONIC CIVIL AIRCRAFT
A. Mirzoyan, CIAM, Russia
Reserve Paper 9.2.R RESEARCH ON CIVIL AIRCRAFT POWERPLANT SYSTEM EICAS MESSAGES DESIGN METHOD
SHANG Yang, Shanghai Aircraft Design and Research Institute, China
10.2Computational Aeroelasticity 2
Chair(s): Ritter, M., Amiryants, G.
Track 10
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
06. Sep 21 13:00 13:30 10.2.1 EFFECTS OF ELASTICITY, VISCOSITY AND BOUNDARY LAYER TRANSITION ON AEROELASTICITY CHARACTERISTICS OF LAMINAR WINGS
S.I. Kuzmina, TsAGI, Russia
06. Sep 21 13:30 14:00 10.2.2 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
11.2Avionics
Chair(s): Viola, N., Fu, J.
Track 11
07 - Systems, Subsystems and Equipment
06. Sep 21 13:00 13:30 11.2.1 DYNAMIC PERFORMANCE ANALYSIS AND WEIGHTED-BASED FAULT DIAGNOSIS SCHEME FOR AIRCRAFT ELECTRIC POWER SYSTEM
Zhengda Zhao¹, Yongqiang Zhang¹, Shuangxin Zhao¹, Long Xu¹; ¹Chengdu Aircraft Industrial (Group) Company Limited, China
06. Sep 21 13:30 14:00 11.2.2 DESIGN AND APPLICATION OF 18-PULSE AUTO-COUPLING TRANSFORMER RECTIFIER FOR AVIATION
WX.-C. CHEN¹, TY.-S. SUN¹, LX.-J. JIANG¹; ¹AVIC, China
06. Sep 21 14:00 14:30 11.2.3 INTEGRATED ON-BOARD NETWORKS FOR NEXT GENERATION AVIONICS
Valentin: V Olenev, St. Petersburg State University of Aerospace Instrumentation, Russia
Reserve Paper 11.2.R AN AGILE PRACTICE OF AVIONICS SYSTEM DEVELOPMENT
Lei: L Dong, China Aeronautical Radio Electronics Research Institute, China
12.2Condition Based Maintenance 1
Chair(s): Molent, L., Li, D.
Track 12
11 - Operations and Sustainment
06. Sep 21 13:00 13:30 12.2.1 STRUCTURAL HEALTH MONITORING – THE ROUTE TO CONDITION BASED MAINTENANCE
John van Doeselaar¹, Derk Daverschot¹; ¹Airbus, France
06. Sep 21 13:30 14:00 12.2.2 COST AND BENEFIT OF STRUCTURAL HEALTH MONITORING FOR COMMERCIAL AIRCRAFT
D. M. Steinweg¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
06. Sep 21 14:00 14:30 12.2.3 REAL TIME IMPACT IDENTIFICATION TECHNIQUE USING MODAL SUPERPOSITION / APPLICATION ON AIRCRAFT FUSELAGE
Dimitri Goutaudier, CNRS, France; Didier Gendre, Airbus, France
13.2Flight Control During Approach
Chair(s): ,
Track 13
10 - Safety and Security
06. Sep 21 13:00 13:30 13.2.1 DETECTION AND ANALYSIS OF AIRCRAFT’S LOW ENERGY STATE DURING THE FINAL APPROACH PHASE
Xiaolong Wang¹, Florian Holzapfel¹; ¹Technische Universität München, Germany
06. Sep 21 13:30 14:00 13.2.2 TOWARDS AN ONLINE PREDICTIVE MODEL OF AIRCRAFT ENERGY STATE USING SUPERVISED MACHINE LEARNING
O Pinon Fischer, Georgia Institute of Technology, United States
06. Sep 21 14:00 14:30 13.2.3 AN OVERVIEW OF FLARE TECHNIQUES AND FLARE TRAINING METHODS
K Okubo¹, J.O. Entzinger¹; ¹The University of Tokyo, Japan
Reserve Paper 13.2.R MACHINE LEARNING BASED PREDICTION OF VEER-OFFS DURING LANDING PHASE
S. Lagunas-Caballero, Airbus Defence and Space, Spain

14:30 - 15:00Break

1.3China Aviation 2
Chair(s): ,
Track 1
12 - Host nation
2.3Shape Optimization
Chair(s): Rinoie, K.
Track 2
01 - Aircraft Design and Integrated Systems
06. Sep 21 15:00 15:30 2.3.1 BWB CONFIGURATION’S AERODYNAMIC OPTIMIZATION DESIGN AND SHAPE PARAMETERIZATION BASED ON GRADIENT METHOD
W.zy Wang, The First Aircraft Institute, China
06. Sep 21 15:30 16:00 2.3.2 MULTIFIDELITY AERODYNAMIC/STEALTH SHAPE DESIGN OPTIMIZATION METHOD FOR FLYING WING AIRCRAFT
Z.-Q Liu¹, W.-P Song¹, Z.-H Han¹, Y Wang¹; ¹Northwestern Polytechnical University, China
06. Sep 21 16:00 16:30 2.3.3 A GRADIENT-BASED AERO-STEALTH OPTIMIZATION DESIGN METHOD FOR THE LONG-ENDURANCE UAV SHAPE DESIGN
L.-M. Ming, Northwestern Polytechnical University, China
06. Sep 21 16:30 17:00 2.3.4 ESTIMATION OF STATIC AND DYNAMIC FLOATATION CHARACTERISTICS DURING AIRCRAFT DITCHING
Z.-Y. Zhao¹, Q.-Q. Qu¹, L.-P. Liu¹; ¹Beihang University, China
3.3Digital Pioneering - Where will MDO, MBSE, Digital Twins and AI bring engineering in 20 years?
Chair(s): ,
Track 3
4.3Turbulence Modeling
Chair(s): Bigarella, E., Wolf, W.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
06. Sep 21 15:00 15:30 4.3.1 ON THE ASSESSMENT OF TURBULENCE MODELS FOR THE SIMULATION OF VORTICAL FLOWS
R. C. Gonzalez, Cranfield Unversity, United Kingdom; S. A. Prince, Cranfield University, United Kingdom
06. Sep 21 15:30 16:00 4.3.2 RESEARCH OF TURBULENCE MODELING BASED ON MACHINE LEARNING
Y.-H. YIN¹, Y.-F. ZHANG¹; ¹Tsinghua University, China
06. Sep 21 16:00 16:30 4.3.3 RESEARCH ON MACHINE LEARNING RECONSTRUCTION OF TURBULENCE MODEL DRIVEN BY EXPERIMENTAL DATA
Y.-F. Wang, BUAA, China
06. Sep 21 16:30 17:00 4.3.4 TURBULENCE MODEL ASSESSMENT OF THE SEPARATED FLOW IN THE STANFORD DIFFUSER
M. Bonnici¹, S. A. Prince¹, K. P. Garry¹; ¹Cranfield University, United Kingdom
5.3Measurement Techniques & Data Analysis
Chair(s): Jujun, W., Xunmian, W.
Track 5
03.2 - Experimental Aerodynamics
06. Sep 21 15:00 15:30 5.3.1 AN OBJECTIVE APPROACH FOR MEASURING INTERMITTENCY IN THE TRANSITIONAL BOUNDARY LAYERS
D Veerasamy, City, University of London, United Kingdom
06. Sep 21 15:30 16:00 5.3.2 DYNAMIC TRAILING-EDGE FLAP MOVEMENT AS A NON-CONVENTIONAL LIFTING MECHANISM
M. J. Bremm¹, R. Stephan¹, R. G. Hörnschemeyer¹, E. Stumpf¹; ¹RWTH Aachen University, Germany
06. Sep 21 16:00 16:30 5.3.3 COMPUTATIONAL FLUID DYNAMIC STUDY ON LOW SPEED WIND TUNNEL DATA CORRECTIONS
W. S. Stryczniewicz, Lukasiewicz Research Network - Institute of Aviation, Poland
06. Sep 21 16:30 17:00 5.3.4 SKIN-FRICTION TOPOLOGY ON AXISYMMETRIC BOATTAIL MODELS BY AN OPTICAL-FLOW ALGORITHM WITH SUBGRID FUNCTION
T. H. Tran, Le Quy Don Technical University, Vietnam
Reserve Paper 5.3.R APPLIED RESEARCH ON SUPERVISED LEARNING IN THE JUDGMENT OF AIRFOIL TRANSITION
Binbin Wei¹, Yongwei Gao¹, Dong Li¹; ¹Northwestern Polytechnical University, China
Reserve Paper 5.3.R TOTAL TEMPERATURE MEASUREMENTS IN WATER INJECTION AND PRE-COMPRESSOR COOLING TECHNOLOGY
Geng Xin¹, Song Zhenyu¹, Zhang Long¹, Liu Xupeng¹; ¹AECC Shenyang Engine Design and Research Institute, China
6.3Flow Control Applications 1
Chair(s): Gowree, E., Prince, S.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
06. Sep 21 15:00 15:30 6.3.1 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
06. Sep 21 15:30 16:00 6.3.2 INVESTIGATION OF LAMINARIZATION EFFICIENCY OF THE SECTIONED SUCTION SYSTEM ON THE SWEPT WING IN FAILURE CASE
S.N. Tolkachev, Central Aerohydrodynamic Institute (TsAGI), Russia
06. Sep 21 16:00 16:30 6.3.3 ENERGY HARVESTING FROM PIEZOELECTRIC FRINGES AT THE TRAILING EDGE OF A FINITE WING WITH LEADING-EDGE TUBERCLES
E.P. Pereira¹, A Esmaeili¹, J.M.M. Sousa¹; ¹Instituto Superior Técnico, Portugal
06. Sep 21 16:30 17:00 6.3.4 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
Reserve Paper 6.3.R INVESTIGATION OF ROLL ATTENUATION MECHANISM OF LOW-ASPECT-RATIO WINGS USING BIONIC FLOW CONTROL APPROACHES
T. Hu, Beihang University, China
Reserve Paper 6.3.R MIXING CONTROL BY LASER PLASMA IN HELIUM JET/SHOCK WAVE INTERACTION
Fan Liu¹, Hong Yan¹, Alexander Zheltovodov, Khristianovich Institute of Theoretical and Applied Mechanics, Russia; ¹Northwestern Polytechnical University, China
7.3Propulsion Airframe Integration
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
06. Sep 21 15:00 15:30 7.3.1 PROPELLER WAKE - OBJECT INTERACTION USING A FREE WAKE MODEL UTILIZING LOCAL MESH REFINEMENT
M. Thiele¹, D. Salassidis¹, M. Hornung¹; ¹Institute of Aircraft Design, Technical University of Munich, Germany
06. Sep 21 15:30 16:00 7.3.2 NUMERICAL STUDY OF QUAD-ROTOR AIRCRAFT PERFORMANCE UNDER SEVERE WEATHER
T. Wan, Tamkang University, Taiwan, China
06. Sep 21 16:00 16:30 7.3.3 AERODYNAMIC ANALYSIS OF AN AIR DRIVE EJECTOR FOR USE IN ENGINE TEST FACILITIES
Faezeh Rasimarzabadi¹, Martin Neuteboom¹, Catherine Clark¹, Hans Martensson, GKN Aerospace Engine Systems, Sweden; ¹NRC, Canada
06. Sep 21 16:30 17:00 7.3.4 AERODYNAMIC INTERFERENCE OPTIMIZATION OF THE FUSELAGE-PUSHING PROPELLER CONFIGURATION
V. Gubskiy, TsAGI, Russia
8.3Buckling and Instability
Chair(s): Juracka, J., Cestino, E.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
06. Sep 21 15:00 15:30 8.3.1 ACHIEVEMENTS IN THE BUCKLING OF THIN-WALLED COMPOSITE LAUNCHER STRUCTURES
F. Franzoni, DLR, Germany; S. Castro, TU-Delft, Netherlands
06. Sep 21 15:30 16:00 8.3.2 THE VIBRATION CORRELATION TECHNIQUE – A RELIABLE NONDESTRUCTIVE METHOD TO PREDICTBUCKLING LOADS
Haim Abramovich, Technion, I.I.T.,, Israel
06. Sep 21 16:00 16:30 8.3.3 INVESTIGATION OF BUCKLING RESPONSE OF CYLINDRICAL SHELLS USING 3D-PRINTING TECHNOLOGY
C. Bisagni¹, E. Labans¹; ¹Delft University of Technology, Netherlands
06. Sep 21 16:30 17:00 8.3.4 KINEMATIC MODEL OF REFINED THEORY AND EXACT ANALYTICAL SOLUTIONS OF STATIC AND BUCKLING PROBLEMS OF STRUCTURALLY-ANISOTR
L M Gavva, Moscow Aviation Institute (NRU) , Russia
Reserve Paper 8.3.R STUDY ON THE COMPRESSION PROPERTIES OF MULTISTAGE TITANIUM ALLOY LATTICE METAMATERIALS AT HIGH TEMPERUTURE
H.Y. Huang¹, D. Wang¹, X.F. Du¹, Y.X Xu¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
Reserve Paper 8.3.R ADVANCED MODELS FOR THE POST-BUCKLING RESPONSE ANALYSIS OF AEROSPACE REINFOCED COMPOSITE PANELS
E. Carrera¹, A. Pagani¹, R. Augello¹, D. Scano¹; ¹Politecnico di Torino, Italy
9.3Transition Physics 1
Chair(s): Atkin, C., Sousa, J.
Track 9
03.3 - Basic Fluid Dynamics and Flow Control
06. Sep 21 15:00 15:30 9.3.1 EVOLUTION OF TOLLMIEN-SCHLICHTING DISTURBANCES OVER NATURALLY DISTRIBUTED ROUGH SURFACES
S. Mughal, Imperial College London, United Kingdom
06. Sep 21 15:30 16:00 9.3.2 VIBRATION INDUCED EXCITATION AND CONTROL OF TOLLMIEN-SCHLICHTING WAVES
E. R. Gowree, ISAE-SUPAERO, France; C. J. Atkin, University of East Anglia, United Kingdom
06. Sep 21 16:00 16:30 9.3.3 NON-LINEAR BOUNDARY LAYER RECEPTIVITY TO FREE-STREAM TURBULENCE
D. Sboev, Central Aerohydrodynamic Institute (TsAGI), Russia
06. Sep 21 16:30 17:00 9.3.4 STABILITY ANALYSIS OF STREAMWISE CORNER FLOW
D Xu, Tsinghua University, China
Reserve Paper 9.3.R LINEAR GLOBAL STABILITY ANALYSIS OF ROUGHNESS-INDUCED TRANSITION
Qiang Yang¹, Guohua Tu¹, Jianqiang Chen¹, Xianxu Yuan¹; ¹State Key Laboratory of Aerodynamics, China
10.3Decoupling Control
Chair(s): Wang, Q.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
06. Sep 21 15:00 15:30 10.3.1 DECISION-MAKING MODELLING: APPLICATION TO APPROACH PHASE IN AUTONOMOUS AIR TO AIR REFUELLING
I Romo, Airbus, Spain
06. Sep 21 15:30 16:00 10.3.2 ADVANCED REFUELING BOOM SYSTEM (ARBS) AUTOMATIC AIR TO AIR REFUELING FLIGHT CONTROL LAWS
A. Sanz de Blas, Airbus Defence & Space, Spain
06. Sep 21 16:00 16:30 10.3.3 DECOUPLING CONTROL LAW DESIGN FOR AN 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
06. Sep 21 16:30 17:00 10.3.4 GAIN SCHEDULING BY FREQUENCY SHAPED LINEAR QUADRATIC CONTROL OF FIXED-WING AIRCRAFT LONGITUDINAL MOTION.
L.S. Kim, Korea Advanced Institute of Science and Technology, South Korea
11.3UAV Dynamics and Control 1
Chair(s): Rui, W., Götzendorf Grabowski, T.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
06. Sep 21 15:00 15:30 11.3.1 RESEARCH ON DYNAMIC MODELING AND TRANSITION FLIGHT STRATEGY OF INDUCED-LIFT VTOL UAV
C.W Wang, Northwestern Polytechniacl University, China
06. Sep 21 15:30 16:00 11.3.2 COMPARATIVE ANALYSIS OF METHODS USED TO ACTIVE CONTROL OF MICRO AERIAL VEHICLE
K.-S. Sibilski, Warsaw University of Technology, Poland
06. Sep 21 16:00 16:30 11.3.3 PERCHING PRINCIPLES ANALYSIS OF POST-STALL PERCHING UNMANNED AERIAL VEHICLE
C.M Min ¹, B.JP Junqiang¹; ¹NWPU, China
06. Sep 21 16:30 17:00 11.3.4 DEVELOPMENT TOWARDS A TOOLCHAIN FOR ESTIMATING UAV FLIGHT DYNAMIC MODELS IN EARLY DESIGN
S. J. Koeberle¹, M. Hornung¹; ¹Institute of Aircraft Design, TUM, Germany
Reserve Paper 11.3.R STUDY OF SMALL UAVS DISTURBED MOTION NATURAL FREQUENCIES USING EXTENDED EXPERIMENTAL DATASETS
Mostafa El-Salamony, Peking University, China; Sergey Serokhvostov, Moscow Institute of Physics and Technology, Russia
Reserve Paper 11.3.R AERODYNAMICS CHARACTERISTICS AND FLIGHT DYNAMICS ANALYSIS OF MULTI-BODY AIRCRAFT
C. An, Beihang University, China
Reserve Paper 11.3.R OPTIMIZATION OF LONGITUDINAL CONTROL OF AN AGRICULTURAL UAV USING LQR-PID CONTROL
Andrew Gomes Pereira Sarmento¹, Alain Giacobini de Souza¹, Alexandre Muniz Neves, CENIC Aeronáutica, Brazil; Luiz Carlos Sandoval Góes¹, Roberto Gil Annes da Silva¹; ¹Instituto Tecnológico de Aeronáutica (ITA), Brazil
12.3Fatigue Assessment
Chair(s): van Doeselaar, J., Blom, A.
Track 12
04.1 - Material Issues, Fatigue and Damage Tolerance
06. Sep 21 15:00 15:30 12.3.1 TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES AEROSTRUCTURES
I. Rivero Arevalo, Airbus, Spain
06. Sep 21 15:30 16:00 12.3.2 STUDY OF COMPOSITE SKIN-STRINGER FATIGUE BEHAVIOR UNDER BROADBAND RANDOM VIBRATION
S.V. Dubinskii¹, F.S. Sevastyanov¹, V.M. Kostenko¹, S.L. Denisov¹, I.A. Zharenov¹; ¹The Central Aerohydrodynamic Institute (TsAGI), Russia
06. Sep 21 16:00 16:30 12.3.3 APPROACH OF THE STATIC AND FATIGUE STRENGTH ESTIMATION OF THE COMPOSITE JOINTS
A.A. Sviridov, The Central Aerohydrodynamic Institute, Russia
06. Sep 21 16:30 17:00 12.3.4 FAILURE CRITERION OF CFRP FOR OPEN-HOLE FATIGUE TESTING
A.G. Kalinin, TsAGI, Russia
Reserve Paper 12.3.R MODEL CURVES: A SIMPLE WAY TO ACCOUNT FOR COMPLEX EFFECTS
A. Bautin¹, Yu. Svirsky¹, V. Basov¹, Ya. Melnikov¹; ¹1Central Aerohydrodynamic Institute (TsAGI), Russia
Reserve Paper 12.3.R IMPROVED HIGH CYCLE FATIGUE PERFORMANCE OF TI6AL4V TITANIUM ALLOY BY WARM LASER SHOCK PEENING
X.L. Pan, Air Force Engineering University, China
13.3Safety and Security Analysis
Chair(s): ,
Track 13
10 - Safety and Security
06. Sep 21 15:00 15:30 13.3.1 RESEARCH ON SAFETY ASSESSMENT APPROACH FOR UAS OPERATIONS OVER UNINHABITED AREAS
QIAN ZHANG, Northwestern Polytechnical University, China
06. Sep 21 15:30 16:00 13.3.2 END TO END CYBERSECURITY IN CIVIL AVIATION ECO SYSTEM
JC Jean-Claude, Airbus, France
06. Sep 21 16:00 16:30 13.3.3 STUDY ON DYNAMIC RESPONSE AND INJURY OF FRONT ROW OCCUPANT UNDER HORIZONTAL IMPACT
M.S.C. MA, Civil Aviation University of China, China
06. Sep 21 16:30 17:00 13.3.4 STATISTICAL ANALYSIS OF AIRCRAFT INCIDENTS M-28 BRYZA
J. Tomaszewska, Polish Air Force University, Poland
Reserve Paper 13.3.R FIRE AND EXPLOSION ANALYSIS OF AIRCRAFT FUEL TANK BASED ON TNT EQUIVALENT METHOD AND FIREBALL EXPLOSION MODEL
W K KAI, AVIC XI'AN AIRCRAFT INDUSTRY (GROUP) COMPANY LTD, China
Reserve Paper 13.3.R 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

0.2Project Clean Sky - Axel Krein, GER
Chair:
06. Sep 21 17:05 18:00

Tuesday, 07. Sep 2021

7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
1.4Design Optimization under Uncertainty
Chair(s): Padulo, M.
Track 1
01 - Aircraft Design and Integrated Systems
07. Sep 21 08:00 08:30 1.4.1 ON ROBUST MULTI DISCIPLINARY ANALYSIS AND OPTIMISATION FOR NEW GENERATION FLEXIBLE AIRCRAFT
M. Saporito, University of Southampton, United Kingdom
07. Sep 21 08:30 09:00 1.4.2 APPLICATION OF ARTIFICIAL NEURAL NETWORKS FOR EFFICIENT RELIABILITY-BASED DESIGN OPTIMIZATION
X. Chen¹, Atif Riaz¹, S. El Fassi¹, A.S.J. van Heerden¹; ¹Cranfield University, United Kingdom
07. Sep 21 09:00 09:30 1.4.3 VALIDATING SURROGATE MODELS AND ICORPORATING UNCERTAINTY QUANTIFICATION IN MULTI-ELEMENTS AIRFOIL DESIGN OPTIMISATION
D. Di Pasquale¹, C Bolart¹; ¹Cranfield University, United Kingdom
07. Sep 21 09:30 10:00 1.4.4 EFFICIENT ADAPTIVE SURROGATE-BASED OPTIMIZATION USING FUZZY CLUSTERING FOR COMPLEX SYSTEM OPTIMIZATIONS
Chunna Li¹, Wen Ji¹, Chunlin Gong¹, Hai Fang, Shanghai Electro-Mechanical Engineering Institute, China; ¹Northwestern Polytechnical University, China
Reserve Paper 1.4.R A NOVEL RBF DATA TRANSFER METHOD BASED ON PCA GEOMETRIC FEATURE EXTRACTION
shenshen Liu, China; Xiao Liu, China; Bo Qiu, China; Yewei Gui, China; Zhikan Liu, China
2.4Hypersonics
Chair(s): Kimmel, B.
Track 2
01 - Aircraft Design and Integrated Systems
07. Sep 21 08:00 08:30 2.4.1 H2020 STRATOFLY PROJECT FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS
N. Viola, Politecnico di Torino, Italy
07. Sep 21 08:30 09:00 2.4.2 THERMAL PROTECTION SYSTEM PRELIMINARY DESIGN OF STRATOFLY HIGH-SPEED PROPELLED VEHICLE
R. SCIGLIANO, Italian Aerospace Research Centre (CIRA), Italy
07. Sep 21 09:00 09:30 2.4.3 HEXAFLY-INT HYPERSONIC VEHICLE THERMAL PROTECTION SYSTEM DESIGN
R. SCIGLIANO, Italian Aerospace Research Centre (CIRA), Italy
07. Sep 21 09:30 10:00 2.4.4 AERODYNAMIC DESIGN THEORY AND METHODOLOGY FOR AN AIRFRAME-INLET INTEGRATED FULL-WAVERIDER VEHICLE
Ding Feng¹, Liu Jun¹, Huang Wei¹, Guo Shanguang, Air Force Engineering University, China; ¹National University of Defense Technology, China
Reserve Paper 2.4.R NOVEL OSCULATING AXISYMMETRIC DESIGN METHOD FOR A HYPERSONIC WAVERIDER VEHICLE DERIVED FROM A POINTED VON KARMAN OGIVE
F. D. Ding, National University of Defense Technology, China
Reserve Paper 2.4.R 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
3.4Global Collaborative Digital Integration in Aviation / IFAR-X challenge
Chair(s): ,
Track 3
02 - Systems Engineering and Integration
4.4Aerodynamic Optimization
Chair(s): Wan, T., Gao, Z.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
07. Sep 21 08:00 08:30 4.4.1 FLOW CONTROL AT HIGH LIFT MISSION OF A CIVIL AIRCRAFTBY AN OPTIMUM MORPHING LEADING-EDGE DESIGN
alireza jahangirian, aerospace engineering departmen, Iran
07. Sep 21 08:30 09:00 4.4.2 OPTIMISATION OF VORTEX GENERATORS FOR STALL SPEED REDUCTION
Jannek Meyer¹, Patrick Marcello Okfen¹, Cees Bil¹; ¹RMIT University, Australia
07. Sep 21 09:00 09:30 4.4.3 AERODYNAMIC DESIGN OOPTIMIZATION OF A CIVIL AIRCRAFT WINGLET USING MULTI-OBJECTIVE EVOLUTIONARY ALGORITHM AND CFD SOLVER
M Heidari Soreshjani, Amirkabir University of Technology, Iran; A JAHANGIRIAN, Amirkabir university of technology, Iran
07. Sep 21 09:30 10:00 4.4.4 DESIGN AND OPTIMIZATION OF A HIGH-ALTITUDE LONG ENDURANCE UAV PROPELLER
K. Y. You, Northwestern Polytechnical University, China
Reserve Paper 4.4.R OPTIMAL DESIGN OF A NEXT GENERATION HIGH-LIFT REUSABLE RE-ENTRY VEHICLE
Andrea Aprovitola, University of Campania "L. Vanvitelli"., Italy; Luigi Iuspa¹, Giuseppe Pezzella¹, Antonio Viviani¹; ¹University of Campania, Engineering Department., Italy
Reserve Paper 4.4.R MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF A CIVIL AIRCRAFT FUSELAGE
Seyed Vahidreza Rohani¹, Alireza Jahangirian¹; ¹Amirkabir University of Technology, Iran
Reserve Paper 4.4.R CFD SIMULATION OF A NEW REVERSE-HINGED SPOILER FOR LIFT/DRAG CONTROL
K. Djidjeli, University of Southampton, United Kingdom
5.4Turbomechanics
Chair(s): Hui, D., Heng, L.
Track 5
03.2 - Experimental Aerodynamics
07. Sep 21 08:00 08:30 5.4.1 EXPERIMENT AND THEORETICAL ANALYSIS OF A TYPE OF NON-SYNCHRONOUS VIBRATION IN A HIGH PRESSURE COMPRESSOR
FeiLong GAO¹, MingSui Yang¹, ZhiBo Zhang¹, Yehui chen¹; ¹AECC Shenyang Engine Research Institute, China
07. Sep 21 08:30 09:00 5.4.2 TSAGI’S EXPERIENCE IN THE DEVELOPMENT OF SIX-COMPONENT ROTATING SHAFT BALANCES
V.S. Manvelyan, Central Aerohydrodynamic Institute (TsAGI), Russia
07. Sep 21 09:00 09:30 5.4.3 JET FLAME RESEARCH BASED ON PHOSPHORESCENT IMAGING TECHNIQUE AND HILBERT-HUANG TRANSFORM METHOD
P Tian, Shanghai Jiao Tong University, China
07. Sep 21 09:30 10:00 5.4.4 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
6.4Developments in Modelling
Chair(s): Atkin, C., Mughal, S.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
07. Sep 21 08:00 08:30 6.4.1 EXPERIMENTAL INVESTIGATION, NUMERICAL AND MATHEMATICAL SIMULATION OF DISPERSE FLOWS IMPINGING ON AIRCRAFT SURFACE
Ivan Alexeevich: Amelyushkin, TsAGI, Russia
07. Sep 21 08:30 09:00 6.4.2 MODIFICATION OF TURBULENCE MODELS FOR PRESSURE-INDUCED SEPARATION ON SMOOTH SURFACES USING THE DLR VICTORIA EXPERIMENT
Tobias Knopp¹, Matteo Novara¹, Daniel Schanz¹, Wieland Lühder¹, Erich Schülein¹, Reinhard Geisler¹, Florian Philipp¹, Michael Schroll², Andreas Krumbein¹, Christian Willert², Andreas Schröder¹; ¹DLR AS, Germany ;²DLR AT, Germany
07. Sep 21 09:00 09:30 6.4.3 A NETWORK-CENTROID BASED REDUCED-ORDER MODEL FOR A MIXING LAYER
H. Li, National University of Defense Technology, China
07. Sep 21 09:30 10:00 6.4.4 SINGULARITIES IN THE NEAR-WALL REGION OF 3D BOUNDARY LAYER AND ASYMPTOTIC FLOW STRUCTURE IN ITS VICINITY
V.I. Shalaev, Moscow Institute of Physics and Technology, Russia
Reserve Paper 6.4.R LOW ORDER MODELLING OF UNSTEADY AERODYNAMIC LIFT FORCES ON 2D FLAT-PLATE DURING SINUSOIDAL PITCHING
R. Zeng, Beihang University, China
Reserve Paper 6.4.R EVOLUTION OF WAVEPACKETS ON THE WINDWARD SIDE OF AN INCLINED HYPERSONIC STRAIGHT CONE UNDER FLIGHT CONDITION
P. Yang¹, Z. Tang¹, S. Dong¹, J. Chen¹, X. Yuan¹, X. Chen¹; ¹China Aerodynamics Research and Development Center, China
Reserve Paper 6.4.R STUDY ON THE STATISTICAL CHARACTERISTICS OF SKIN FRICTION OF SHOCK WAVE TURBULENT BOUNDARY LAYER AT MACH 6
Peng-fei:P.-F Shen, State Key Laboratory of Aerodynamics, China
7.4Flapping Wing/MAV
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
07. Sep 21 08:00 08:30 7.4.1 INVESTIGATION AERODYNAMICS FLAPPING FLIGHT ROBOTIC BIRD
H.W.M. Hoeijmakers, University of Twente, Netherlands
07. Sep 21 08:30 09:00 7.4.2 DEFORMATION AND FLOWFIELD INVESTIGATION OF A FLAPING-WING MAV IN GROUND EFFECT
J WANG, Northwestern Polytechnical University, China
07. Sep 21 09:00 09:30 7.4.3 EFFECTS OF SPANWISE AREA DISTRIBUTION ON AERODYNAMIC PERFORMANCE OF FLAPPING WINGS IN HOVER
Z CAO, Northwestern Polytechnical University, China
07. Sep 21 09:30 10:00 7.4.4 THE INFLUENCE OF SWEEPING MOTION ON THREE-DIMENSIONAL FLOW PATTERNS AND AERODYNAMIC PERFORMANCE OF FLAPPING WINGS
T.-W. Wu, Northwestern Polytechnical University, China
Reserve Paper 7.4.R NEURAL MODEL OF FIXED WINGS MICRO AERIAL VEHICLE AERODYNAMICS
K.-S. Sibilski, Warsaw University of Technology, Poland
Reserve Paper 7.4.R NUMERICAL SIMULATION OF SPANWISE FOLDING EFFECTS ON A BIRD-SCALE FLAPPING WING
X.Y. Lang, School of Aeronautics, Northwestern Polytechnical University, China
Reserve Paper 7.4.R NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING LEADING EDGE COVERTS
Jiangxin Gao¹, Wenqing Yang¹, Rui Zhang¹, Yuanbo Li¹; ¹Northwestern Polytechnical University, China
Reserve Paper 7.4.R COMPUTATIONAL INVESTIGATION OF CEILING PROXIMITY EFFECTS FOR MICRO QUADROTOR FLIGHT
Z.X. Xu, Northwestern Polytechnical University, China
8.4Composite Materials and Structures
Chair(s): Fichera, S., Li, K.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
07. Sep 21 08:00 08:30 8.4.1 LIGHTWEIGHT DESIGN OF THERMAL PROTECTION STRUCTURES WITH EFFECTS OF MESO-PROPERTIES OF MATERIALS
S.-H.-A. You An, Computational Aerodynamic Institute(CAI), CARDC, China
07. Sep 21 08:30 09:00 8.4.2 ACCURATE MODELS FOR THE PREDICTION OF FREE-EDGE STRESSES OF COMPOSITE STRUCTURES UNDER THERMAL LOADS
E. Zappino¹, E. Carrera¹; ¹Politecnico di Torino, Italy
07. Sep 21 09:00 09:30 8.4.3 TEMPERATURE-INDUCED LOAD OF BOLTED HYBRID COMPOSITE/METAL JOINT
L.-K KAI, AVIC Aircraft Strength Research Institute, China
07. Sep 21 09:30 10:00 8.4.4 DEVELOPMENT OF LIGHTWEIGHT HYBRID AIRFRAMES BASED ON UNIDIRECTIONAL COMPOSITE STRUCTURE CONCEPTS
A. Shanygin, Central Aerohydrodynamic Institute (TsAGI), Russia
Reserve Paper 8.4.R SEARCH OF RATIONAL LEVEL OF WING-FUSELAGE INTEGRATION TO INCREASE WEIGHT EFFICIENCY OF AIRCRAFT COMPOSITE STRUCTURES
I. Kondakov, Central Aerohydrodynamic Institute (TsAGI), Russia
9.4MDO for Collaborative Propulsion Design
Chair(s): Mirzoyan, A.
Track 9
05 - Propulsion
07. Sep 21 08:00 08:30 9.4.1 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
07. Sep 21 08:30 09:00 9.4.2 ELABORATION OF DISTRIBUTED MDAO SYSTEM FOR CONCEPTUAL DESIGN OF SCA PROPULSION SYSTEM IN INTEGRATED DEVELOPMENT ENVIRONM
L.A. Mirzoyan, CIAM, Russia
07. Sep 21 09:00 09:30 9.4.3 AERODYNAMIC PROPULSION SYSTEM OPTIMIZATION: TOWARDS TO AGILE 4.0
K.S. Anisimov, Federal State Unitary Enterprise Central Aerohydrodynamic Instit, Russia
07. Sep 21 09:30 10:00 9.4.4 DECISION PROBLEMS IN AN IDENTIFICATION OF FACTORS INFLUENCING ON THE EMISSION OF HARMFUL COMPOUNDS OF TRANSPORT MEANS
M. JACYNA, Warsaw University of Technology, Poland
10.4Virtual Testing
Chair(s): Stumpf, E., Peters, M.
Track 10
07 - Systems, Subsystems and Equipment
07. Sep 21 08:00 08:30 10.4.1 RESEARCH AND VALIDATION OF SYSTEM MODELING AND SIMULATION OF INTAKE AIR MIXER ALTITUDE TEST BED
Feng Wu, Northwestern Polytechnical,AECC Sichuan Gas Turbine Establishmen, China; Xu-dong Feng¹, Lin-tao Leng¹, Tao Liu¹, Cai-qiong Yang¹; ¹AECC Sichuan Gas Turbine Establishment, China
07. Sep 21 08:30 09:00 10.4.2 DESIGN AND DEVELOPMENT OF A MODULAR IRON BIRD TO TEST MOVABLE SURFACE ACTUATORS OF GENERAL AVIATION AIRCRAFT AND UAVS
M. Mattei, Università della Campania "Luigi Vanvitelli", Italy
11.4UAV Dynamics and Control 2
Chair(s): Bai, J., Krus, P.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
07. Sep 21 08:00 08:30 11.4.1 A VARIABLE-FIDELITY METHOD FOR UNMANNED AIRCRAFT WAKE VORTEX SAFETY AND CONTROL ANALYSIS
V. Golubev, ERAU, United States
07. Sep 21 08:30 09:00 11.4.2 MULTIROTOR VEHICLES DESIGN BASED ON DYNAMIC MANIPULABILITY FOR UNDERACTUATED FLYING SYSTEMS
Y Matsumura¹, M Bando¹, S Hokamoto¹; ¹Kyushu Univ., Japan
07. Sep 21 09:00 09:30 11.4.3 LANDING SYSTEM USING EXTENDED DYNAMIC WINDOW APPROACH FOR FIXED-WING UAV
S Ishioka¹, K Uchiyama¹, K Masuda¹; ¹Nihon University, Japan
07. Sep 21 09:30 10:00 11.4.4 MPPC OF MULTICOPTER WITH FAULT ROTOR IN COLLISION SITUATION
Y Shimizu, Univerisity of Tokyo, Japan
Reserve Paper 11.4.R AUTONOMOUS CONTROL OF FIXED-WING UNMANNED AERIAL SYSTEMS(UASS) BY REINFORCEMENT LEARNING
H. Wang, AVIC Xi'an Flight Automatic Control Research Institute, China
Reserve Paper 11.4.R NEW ROLL-SPIRAL COUPLING MODE CRITERION FOR HIGH SPEED VEHICLES
Guohui Dou¹, Yunjun Yang¹, Anlong Gong¹, Chuqun Ji¹; ¹China Academy of Aerodynamic of Aerospace, China
12.4Composite Characterization and Fabrication
Chair(s): , , Wallin, M.
Track 12
04.1 - Material Issues, Fatigue and Damage Tolerance
07. Sep 21 08:00 08:30 12.4.1 A DEEP-LEARNING-BASED METHOD FOR DAMAGE IDENTIFICATION OF COMPOSITE LAMINATES
Y Yu¹, W Binwen¹, L Shuaishuai¹, Z Yuxi, Peking University, China; W Li¹, L Guoqiang¹; ¹Aircraft Strength Research Institute of ChinaAffiliation, China
07. Sep 21 08:30 09:00 12.4.2 IN-SITU LASER ASSISTED DIRECT IMPREGNATION, LAMINATION AND PLACEMENT OF CFRTP
Tadashige Ikeda, Chubu University, Japan; Takeharu Sakai, Tottori University, Japan; Ayako Yokosu¹, Yasunari Fujii¹, Masahiro Arai¹, Takashi Ishikawa¹; ¹Nagoya University, Japan
07. Sep 21 09:00 09:30 12.4.3 MOISTURE ABSORPTION BEHAVIOR OF COMPOSITE STIFFENED PANELS IN HYGROTHERMAL ENVIRONMENT
B-L Ma, China
07. Sep 21 09:30 10:00 12.4.4 A TWO PHASES COUPLING FREE AND POROUS FLOW NUMERICAL SIMULATION METHOD OF LCM PROCESS
C. Chen, China; C. Chen, China; L.M. Gao, China; J.F. Xu, China
Reserve Paper 12.4.R RESEARCH OF THE MECHANICAL PROPERTIES OF CFRP OF THE HIGH THICKNESS
A.A. Sviridov, The Central Aerohydrodynamic Institute, Russia
Reserve Paper 12.4.R A METHODOLOGY TO GENERATE DESIGN ALLOWABLES OF COMPOSITE LAMINATES USING MACHINE LEARNING
P Camanho, Faculdade de Engenharia, Universidade do Porto, Portugal
13.4ATC, Pilot & Controller
Chair(s): ,
Track 13
10 - Safety and Security
07. Sep 21 08:00 08:30 13.4.1 ATTENTION: TARGET AND ACTUAL – THE CONTROLLER FOCUS
J. Rataj¹, O. Ohneiser¹, G. Marin², R. Postaru²; ¹DLR, Germany ;²ROMATSA, Romania
07. Sep 21 08:30 09:00 13.4.2 ANALYSIS OF PILOT OPERATIONAL STRATEGY DIFFERENCE USING NEURAL NETWORK
Ryota Mori, Electronic Navigation Research Institute, Japan
07. Sep 21 09:00 09:30 13.4.3 OBJECTIVE MEASUREMENT OF HUMAN FACTORS FOR SUPPORTING THE OPERATOR’S LOAD SIMULATION AND MANAGEMENT
U. Kale, Budapest University of Tech. and econ.;, Hungary
07. Sep 21 09:30 10:00 13.4.4 MACHINE LEARNING ENABLED TURBULENCE PREDICTION USING FLIGHT DATA FOR SAFETY ANALYSIS
M Emara¹, M dos Santos¹, N Chartier¹, J Ackley¹, T Puranik¹, A Payan¹, M Kirby¹, O Pinon¹, D Mavris¹; ¹Georgia Institute of Technology, United States

10:00 - 10:30Break

1.5Hybrid/Electric & Unconventional Aircraft 1
Chair(s): Prakasha, P.
Track 1
01 - Aircraft Design and Integrated Systems
07. Sep 21 10:30 11:00 1.5.1 CONCURRENT OPTIMIZATION OF AIRFRAME AND ENERGY STORAGE AND CONVERSION SYSTEMS FOR HYBRID ELECTRIC PROPULSION AIRCRAFT
A. Elham, TU Braunschweig, Germany
07. Sep 21 11:00 11:30 1.5.2 PRELIMINARY DESIGN AND EXPERIMENTAL INVESTIGATION OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT
Y Ma, Germany; W Zhang, China; Y Zhang, China; Y Ma, China; Z Bai, China
07. Sep 21 11:30 12:00 1.5.3 UNMANNED FIRE-FIGHTING AMPHIBIOUS AIRCRAFT WITH DISTRIBUTED TURBOELECTRIC PROPULSION SYSTEM
A.V. Vlasov¹, M.A. Ovdienko¹, V.S. Zakharchenko, Central Institute of Aviation Motors, Russia; A.N. Varyukhin¹; ¹CENTRAL INSTITUTE OF AVIATION MOTORS, Russia
2.5Cost Assessment
Chair(s): Bagassi, S.
Track 2
01 - Aircraft Design and Integrated Systems
07. Sep 21 10:30 11:00 2.5.1 FLEET LEVEL DIRECT OPERATING COST ASSESSMENT OF ADVANCED ALL NEW MID-RANGE TRANSPORT AIRCRAFT
J. Hartmann¹, F. Presto, Hamburg University of Technology (TUHH), Germany; S. Woehler¹, B. Liebhardt¹; ¹German Aerospace Center (DLR), Germany
07. Sep 21 11:00 11:30 2.5.2 LIFECYCLE COST-BENEFIT ASSESSMENT OF SELECTED TECHNOLOGIES CONSIDERING UNCERTAINTIES
A.A. Pohya, DLR, Germany
07. Sep 21 11:30 12:00 2.5.3 BASED ON THE CHARACTERISTIC PARAMETERS ESTIMATE MANUFACTURING COST FOR COMPOSITE STRUCTURES
H.-F. Feng, China
3.5System Architecture
Chair(s): Limouzy, J.C., Pan, D.P.
Track 3
02 - Systems Engineering and Integration
07. Sep 21 10:30 11:00 3.5.1 ARCHITECTURE INTEGRATION OF FUTURE ATM SYSTEM BASED ON META MODEL
Jinyan Wang¹, Zhou Qing¹, Li Bingfei¹; ¹Chinese Aeronautical Radio and Electronics Research Institute, China
07. Sep 21 11:00 11:30 3.5.2 TECHNOLOGY ROADMAPS FOR THE DEVELOPMENT OF FUTURE HIGH-SPEED TRANSPORTATION SYSTEMS
V. Vercella¹, R. Fusaro¹, N. Viola¹; ¹Politecnico di Torino, Italy
07. Sep 21 11:30 12:00 3.5.3 ARCHITECTURE OF PRODUCT RESEARCH AND DEVELOPMENT SYSTEM
Liyuan Su¹, Haoxiang Zhou¹; ¹AEAC, China
Reserve Paper 3.5.R GREENER ATM SYSTEM ARCHITECTURE RESEARCH BASED ON COMPLEX SYSTEM ENGINEERING METHOD
Haoliang Hu¹, Jizhi Mao¹, Dezhen Hu¹; ¹China Aeronautical Radio Electronics Research Institute, China
4.5Ice Accretion
Chair(s): Gao, Z., Santos, L.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
07. Sep 21 10:30 11:00 4.5.1 NUMERICAL STUDY ON THE STALL CHARACTERISTICS AND SEPARATED FLOW AROUND ICED AIRFOILS USING LATTICE BOLTZMANN METHOD
H.Y.G Gu, Northwestern Polytechnical University, China
07. Sep 21 11:00 11:30 4.5.2 EFFECT OF DROPLET SIZE ON ICING RANGE FOR HELICOPTER BLADE
Li Kaicheng, China; Song Chao, China; Ma Honglin, China; Wang YIngyu, China
07. Sep 21 11:30 12:00 4.5.3 THREE-EQUATION TTURBULENCE MODEL FOR SEPARATION PREDICTION OF ICE-ACCRETION AIRFOIL
H.-L Li, Tsinghua University, China
5.5Aeroacoustics & Noise
Chair(s): Bao, C., Rasuo, B.
Track 5
03.2 - Experimental Aerodynamics
07. Sep 21 10:30 11:00 5.5.1 INVESTIGATION OF A NOISE REDUCTION PROPELLER GEOMETRY BASED ON AERODYNAMIC AND AEROACOUSTIC OPTIMIZATION
X GENG, BEIHANG UNIVERSITY, China
07. Sep 21 11:00 11:30 5.5.2 MICROPHONE ARRAY TECHNIQUES FOR TRAILING EDGE NOISE BASED ON CONVOLUTIONAL NEUTRAL NETWORK
Zhangchen SONG¹, Peiqing LIU¹, Hao GUO¹; ¹Beihang Univerisity, China
6.5Turbulent Flows
Chair(s): Breitsamter, C., Fu, S.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
07. Sep 21 10:30 11:00 6.5.1 NUMERICAL SIMULATION OF BOUNDARY LAYER FLOW ON MICROSTRUCTURE SURFACE
R.P. Pang, Northwestern Polytechnical University , China
07. Sep 21 11:00 11:30 6.5.2 SUBSONIC WIND TUNNEL SMALL RIBLETS DRAG REDUCTION TEST ON C919 FUSELAGE MODEL
H.W. Wang, China Academy of Aerospace Aerodynamics, China
07. Sep 21 11:30 12:00 6.5.3 THE EFFECTS OF ADVERSE PRESSURE GRADIENT ON THE BEHAVIORS OF RESOLVENT MODE IN TURBULENT CHANNEL FLOWS
Cheng Chen, China; J.-T. Huang, China; Xian Chen, China
Reserve Paper 6.5.R DIRECT SIMULATION OF THE HYPERSONIC SHOCK WAVE/BOUNDARY LAYER INTERACTION AND ITS HEATING LOAD CONTROL BY MICRO-RAMP VOR
D Sun¹, C Li¹, Q-L Guo¹, P-X Liu¹, X-X Yuan¹; ¹State Key Laboratory of Aerodynamics, China
Reserve Paper 6.5.R FLOW AND HEAT TRANSFER MECHANISMS OF SINGLE CIRCULAR JET IMPINGEMENT USING LARGE EDDY SIMULATION
Q.-L. Li, China
Reserve Paper 6.5.R NUMERICAL SIMULATION STUDY ON BOUNDARY LAYER FLOW AND DRAG REDUCTION CHARACTERISTICS OF RIBLETS
S. Y. Du¹, R. Pang, AVIC Xi’an Flight Automatic Control Research Institute, China; W. M. Sang¹, G. J. Yang¹; ¹Northwestern Polytechnical University, China
7.5Low Speed Aero
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
07. Sep 21 10:30 11:00 7.5.1 TRANSPORT AIRCRAFT WING INVESTIGATIONS AIMED ON CROW INSTABILITY EXCITATION AND HIGH LIFT INCREASE BY OSCILLATING FLAPS
J. Ruhland¹, F.M. Heckmeier¹, C. Breitsamter¹; ¹Technical University of Munich, Germany
07. Sep 21 11:00 11:30 7.5.2 NUMERICAL INVESTIGATIONS OF HINGED STRAKES AERODYNAMICS AT HIGH ANGLES OF ATTACK
Z. F. Xia, China Academy of Aerospace Aerodynamics, China
07. Sep 21 11:30 12:00 7.5.3 AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATION
Min ZHONG¹, Jun HUA¹, Xiasheng SUN¹, Sui ZHENG¹, Ganglin WANG¹, Guoxin ZHANG¹, Hao WANG¹, Yan LI¹, Xiaofei LI¹, Junqiang BAI, Northwestern Polytechnical University, China; ¹Chinese Aeronautical Establishment, China
Reserve Paper 7.5.R NUMERICAL STUDY ON WING ROCK MECHANISM OF A LOW-ASPECT-RATIO RECTANGULAR WING AT LOW REYNOLDS NUMBER
Y. Huang, Beihang University, China
8.5Fluid Structure Interaction
Chair(s): Schmidt, H., Zheng, J.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
07. Sep 21 10:30 11:00 8.5.1 OPTIMAL DESIGN OF FLUID-CONVEYING PIPE SUPPORT FOR CONTROLLING REACTION FORCE DURING VIBRATION
R.T. tian, Aviation Industry Aircraft Strength Research Institute, China
07. Sep 21 11:00 11:30 8.5.2 OPERATIONAL MODAL ANALYSIS AND ESTIMATION OF AERODYNAMIC PARAMETERS OF A FLEXIBLE AIRCRAFT
L. Goes, ITA, Brazil
07. Sep 21 11:30 12:00 8.5.3 PRELIMINARY DESIGN AND OPTIMIZATION OF A REFERENCE AIRCRAFT UNDER DYNAMIC LOADS
H. Schmidt, RWTH University, Germany
9.5More / Hybrid / Electric Propulsion
Chair(s): ,
Track 9
05 - Propulsion
07. Sep 21 10:30 11:00 9.5.1 THERMAL MANAGEMENT FOR GASOLINE ENGINE-BATTERY HYBRID PROPULSION SYSTEM OF SMALL UAV PLATFORM
H.R. Gwon, Korean Air R&D Center, South Korea
07. Sep 21 11:00 11:30 9.5.2 CONCEPTUAL STUDIES OF DIFFERENT TYPE OF HYBRID ELECTRIC PROPULSION SYSTEMS FOR COMMUTER AIRLINERS
V.S. Zakharchenko, CENTRAL INSTITUTE OF AVIATION MOTORS, Russia
07. Sep 21 11:30 12:00 9.5.3 IMPLEMENTATION OF DISTRIBUTED ELECTRIC PROPULSION ON A GENERAL AVIATION AIRCRAFT
M Gallani, EMBRAER, Brazil
Reserve Paper 9.5.R DIGITAL SIMULATION OF STARTER/GENERATOR CONTROL FOR MORE ELECTRIC ENGINE
J XU, AECC COMMERCIAL AIRCRAFT ENGINE CO., LTD., China
10.5Boundary Control
Chair(s): Itoh, E.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
07. Sep 21 10:30 11:00 10.5.1 INFLUENCE OF STABILITY AND CONTROL DERIVATIVES IN PIO PHENOMENON
G.D.A.N. Daher de Alencar Neves, Escola de Engenharia de São Carlos, Brazil
07. Sep 21 11:00 11:30 10.5.2 AIRCRAFT GROUND MOTION SIMULATION ORIENTED 6 DEGREE OF FREEDOM MODEL
N. Bai Bai, Beihang University, China
07. Sep 21 11:30 12:00 10.5.3 INFLUENCE OF AERODYNAMIC ASYMMETRY ON SPIN PARAMETERS OF THE COMMON RESEARCH MODEL
A.N. Khrabrov¹, M.E. Sidoryuk¹; ¹TsAGI, Russia
11.5UAV Conflict Avoidance 1
Chair(s): Sabatini, R., Goraj, Z.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
07. Sep 21 10:30 11:00 11.5.1 IMPLEMENTATION OF VELOCITY OBSTACLE METHOD ON A QUADROTOR UNMANNED AERIAL VEHICLE FOR DYNAMIC CONFLICT AVOIDANCE
Y.I. Jenie, FTMD - Institut Teknologi Bandung, Indonesia
07. Sep 21 11:00 11:30 11.5.2 MPC BASED PARTIAL TRAJECTORY PLANNING FOR MULTIROTOR WITH POINT CLOUD OBSTACLES
H. Ahn, KAIST, South Korea
07. Sep 21 11:30 12:00 11.5.3 VELOCITY OBSTACLE METHOD IN OPTICAL FLOW FRAMEWORK FOR AUTOMATIC CONFLICT DETECTION AND RESOLUTION IN UAVS
Y.I. Jenie, Faculty of Mechanical and Aerospace Engineering, ITB, Indonesia
12.5Dynamics and Noise
Chair(s): Jokinen, J., Bayandor, J.
Track 12
04.1 - Material Issues, Fatigue and Damage Tolerance
07. Sep 21 10:30 11:00 12.5.1 THE NOISE REDUCTION STUDY OF COMPOSITE ACOUSTIC LINER ON HIGH BYPASS RATIO TURBOFAN AEROENGINE
P-H Hou, Shenyang Aeroengine Research Institute, China
07. Sep 21 11:00 11:30 12.5.2 DYNAMIC RESPONSE AND DAMAGE OF THE FAN BLADES DURING UAV INGESTION INTO AN AERO-ENGINE
N.D. Hou, China; X.H. Meng, China; J. Liu, China; Y.L. Li, China
07. Sep 21 11:30 12:00 12.5.3 EXPERIMENTAL AND NUMERICAL STUDY ON BALLISTIC IMPACT OF ARAMID FABRIC
H. Pei, China
Reserve Paper 12.5.R ANALYSIS OF THE DYNAMIC RESPONSE AND FAILURE OF FABRIC SUBJECTED TO BLAST LOADING
J.C Jiang, Civil Aviation University of China, China
13.5Systems & Components Safety
Chair(s): ,
Track 13
10 - Safety and Security
07. Sep 21 10:30 11:00 13.5.1 AIRCRAFT INFLIGHT ICING DETECTION AND DIAGNOSIS METHODS
Di Ding¹, Wei-Qi Qian¹, Qing Wang¹; ¹China Aerodynamics Research and Development Center, China
07. Sep 21 11:00 11:30 13.5.2 DESIGN AND RESEARCH ON SAFETY ANALYSIS TOOL FOR AVIONICS SYSTEM
Yu Liu, Shanghai Aircraft Design and Research Institute, China
07. Sep 21 11:30 12:00 13.5.3 A PROTOTYPE WHIRL TOWER FOR TESTING INSOLATED ROTOR SYSTEMS IN HOVER
M.-M. Wojtas¹, L. Czajkowski¹, K. Raczko¹; ¹Institute of Aviation, Poland
Reserve Paper 13.5.R EXPERIMENTAL STUDY ON CRITICAL HEAT FLUX CHARACTERISTICS OF R134A FOLW BOILING IN HORIZONTAL 2.1MM TUBE UNDER HYPERGRAVI
H.JJ Jianjun, Nanjing engineering Institute of Aircraft System, Jincheng, AVIC, China
Reserve Paper 13.5.R DEVELOPMENT AND ASSESSMENT OF DURABLE ICEPHOBIC COATINGS FOR AIRCRAFT APPLICARIONS
J. GARCIA, IRT SAINT EXUPERY, France
Reserve Paper 13.5.R ULTRASONIC DE-ICING SYSTEM DESIGN METHODS BASED ON RESONANCE AND IMPEDANCE MATCHING
B Miao¹, M.-X. Bao¹, C.-L. Zhu¹; ¹Nanjing University of Aeronautics and Astronautics, China
Reserve Paper 13.5.R A NUMEIRCAL PREDICTION OF AIRCRAFT ICING SITUATION FIELD BASED WRF AND SVR
Q.-L. Guo¹, W.-M. Sang¹, J.-J. Niu¹, A.-X. Qiu¹; ¹Northwestern Polytechnical University, China

12:00 - 13:00Lunch

1.6HMI & Cabin Design
Chair(s): Nagel, B.
Track 1
01 - Aircraft Design and Integrated Systems
07. Sep 21 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
07. Sep 21 13:30 14:00 1.6.2 ACOUSTIC FLIGHT LAB – A UNIQUE INTEGRATION PLATFORM FOR OPTIMIZING OF VIBRO-ACOUSTIC PERFORMANCE OF AIRCRAFT
M. Wandel, Airbus Operations GmbH, Germany
07. Sep 21 14:00 14:30 1.6.3 DEVELOPMENT OF A GESTURE-BASED INTERFACE FOR FLIGHT CONTROLS: RESULTS OF INITIAL EXPERIMENTS WITH THE SYSTEM
M. A. Rodriguez Diaz¹, E. Villani¹, P. Krus, Linköping University, Sweden; ¹Aeronautics Institute of Technology, Brazil
2.6AVIATION AND WORLD WILDFIRES
Chair(s): Mirzoyan, A.
Track 2
15 - Guest lectures
3.6Knowledge based Engineering
Chair(s): Conway, S., Stezycki, P.
Track 3
02 - Systems Engineering and Integration
07. Sep 21 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
07. Sep 21 13:30 14:00 3.6.2 A MODULAR KNOWLEDGE-BASED-ENGINEERING APPLICATION SUPPORTING THE PREDESIGN OF NOVEL AIRCRAFT CONFIGURATIONS
A. Zamfir, German Aerospace Center (DLR), Germany
07. Sep 21 14:00 14:30 3.6.3 APPLICATION OF KNOWLEDGE ENGINEERING IN SPACECRAFT OVERALL DESIGN
Zhao Zhao, Harbin Institute Technology, China
4.6High Speed Flows
Chair(s): Alves, L., Liu, H.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
07. Sep 21 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. Shalaev, Moscow Institute of Physics and Technology, Russia
07. Sep 21 13:30 14:00 4.6.2 LONGITUDINAL AND LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE HIGH-SPEED VEHICLE
Tamás Bykerk, Honorary Associate, the University of Sydney, Australia, Australia; Giuseppe Pezzella, University of Campania, Engineering Department. , Italy; Dries Verstraete, University of Sydney, School of Aerospace, Australia; Antonio Viviani, University of Campania, Engineering Department., Italy
07. Sep 21 14:00 14:30 4.6.3 MULTI-SCALE CFD/MD MODELLING OF HIGH-ENTHALPY FLOW/TPS INTERACTION AND ITS PRELIMINARY AERONAUTICAL APPLICATION
Xiaofeng Yang¹, Yanxia Du¹, Guangming Xiao¹, Lei Liu¹, Dong Wei¹, Qin Li¹, Yewei Gui¹; ¹China Aerodynamics Research and Development Center, China
Reserve Paper 4.6.R RESEARCH OF HYPERSONIC BOUNDARY LAYER INSTABILITY AND TRANSITION WITH THERMAL-CHEMICAL NON-EQUILIBRIUM EFFECTS
X.-L. Chen, Tsinghua University, China
Reserve Paper 4.6.R GEOMETRICAL PARAMETER STUDY OF A HYPERSONIC VERTICAL GAP FLOW
H. -Y. Zhang, State Key Laboratory of Aerodynamics, China; W.-G. Zong, University of Sichuan, China; Y.-W. Gui, Computational Aerodynamics Institute, CARDC, China; B. Qiu, State Key Laboratory of Aerodynamics, China
Reserve Paper 4.6.R COUPLED HEAT TRANSFER CHARACTERISTICS ON CHEMICALLY REACTING INTERFACE OF HIGH-SPEED AIRCRAFT CONSIDERING WALL INJECTION
Q. You, China; X.-F. Yang, China; L. Zeng, China; Y.-W. Gui, China; Y.-X. Du, China; L. Liu, China; G.-M. Xiao, China
5.6Adaptive Wings
Chair(s): Dakai, L., Gowree, E.
Track 5
03.2 - Experimental Aerodynamics
07. Sep 21 13:00 13:30 5.6.1 EXPERIMENTAL INVESTIGATIONS OF A FULL MODEL WITH ADAPTIVE ELASTO-FLEXIBLE MEMBRANE WINGS
J Pflueger, Technical University Munich, Chair Aerodynamics/Fluidmechanics, Germany
07. Sep 21 13:30 14:00 5.6.2 EXPERIMENTAL ANALYSIS OF A BLOWN-WING CONFIGURATION DURING TRANSITION FLIGHT
Y Leng, ISAE, France
07. Sep 21 14:00 14:30 5.6.3 WIND TUNNEL ASSESSMENT OF A PASSIVE-ADAPTIVE WING FOR DRAG REDUCTION
C. B. York, Singapore Institute of Technology, Singapore
6.6Composite Defect and Damage
Chair(s): Herman, M., Ikeda, T.
Track 6
04.1 - Material Issues, Fatigue and Damage Tolerance
07. Sep 21 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
07. Sep 21 13:30 14:00 6.6.2 THE INFLUENCE OF THE NUMBER OF ADHESIVE PLIES (FM-300-2K) ON FRACTURE PROPERTIES
J Jokinen¹, M Wallin, Patria Aviation, Finland; M Kanerva¹; ¹Tampere University, Finland
07. Sep 21 14:00 14:30 6.6.3 STATISTICS AND ANALYSIS OF MANUFACTURE 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
Reserve Paper 6.6.R DEVELOPMENT OF METHOD FOR DETERMINING THE SHEAR FRACTURE TOUGHNESS ON SPECIMENS WITHOUT A DELAMINATION INITIATOR MADE OF
V. Tokar, TsAGI, Russia
7.6Simulation
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
07. Sep 21 13:00 13:30 7.6.1 NUMERICAL VIRTUAL FLIGHT SIMULATION OF QUASI-COBRA MANEUVER OF A FIGHTER AIRCRAFT
None Wang, China Aerodynamics Research and Development Center, China
07. Sep 21 13:30 14:00 7.6.2 NUMERICAL SIMULATION OF AIRFOIL SPANWISE-RIDGE ICE FORMATION BASED ON HOT AIR ANTI-ICING SYSTEM
J.-T Wang, Northwestern Polytechnical University, China
07. Sep 21 14:00 14:30 7.6.3 VERIFICATION AND VALIDATION OF SONIC BOOM SIMULATION CAPABILITIES
G. CARRIER, ONERA, France
Reserve Paper 7.6.R RESEARCH ON UNSTEADY AERODYNAMIC MODELS AT HIGH ANGLE OF ATTACK BASED ON NONLINEAR REGRESSION
J A Cheng¹, H Zhan¹, B G Mi¹; ¹School of Aeronautics,Northwestern Polytechnical University, China
8.6Aeroservoelasticity
Chair(s): Degenhardt, R., Schmidt, H.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
07. Sep 21 13:00 13:30 8.6.1 MULTI-AXIS MANEUVER SIMULATION FOR SYSTEM IDENTIFICATION OF FLEXIBLE TRANSPORT AIRCRAFT BY HIGH-FIDELITY METHODS
M. R. Ritter¹, M. S. Roeser¹, S. Görtz¹; ¹German Aerospace Center (DLR), Germany
07. Sep 21 13:30 14:00 8.6.2 STRUCTURAL DESIGN OF MILITARY AIRCRAFT VERTICAL TAIL INCLUDING DYNAMIC LOADS FROM WING AND AIRBRAKE SEPARATED FLOW
W.G. LUBER, wgl-dynamics Consulting, Germany
07. Sep 21 14:00 14:30 8.6.3 RECEPTANCE-BASED UNCERTAINTY QUANTIFICATION AND MINIMIZATION IN AEROSERVOELASTIC SYSTEMS
L. J. Adamson, University of Liverpool, United Kingdom
9.6ISABE 1
Chair(s): ,
Track 9
15 - Guest lectures
07. Sep 21 13:00 13:30 9.6.1 THE POTENTIAL OF CASING TREATMENTS FOR TRANSONIC COMPRESSORS: EVALUATION BASED ON AXIAL-SLOT AND ROTOR BLADE OPTIMISATIO
G. Goinis¹, C. Voß¹, E. Nicke¹; ¹German Aerospace Center (DLR), Germany
07. Sep 21 13:30 14:00 9.6.2 CONJUGATE HEAT TRANSFER MODELLING OF A TURBINE VANE ENDWALL WITH THERMAL BARRIER COATINGS
Z. Fen, China
10.6Vibration and Damping
Chair(s): Zappino, E., Bisagni, C.
Track 10
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
07. Sep 21 13:00 13:30 10.6.1 STRUCTURAL VIBRATION CONTROL BY USING THE ENERGY FROM DIFFERENT MODE
K.L LI, Aircraft strength research institute, China
07. Sep 21 13:30 14:00 10.6.2 VERIFICATION AND VALIDATION IN AN UNCERTAIN ENVIRONMENT
i Isnardi, University of Liverpool, United Kingdom
07. Sep 21 14:00 14:30 10.6.3 MODAL DAMPING IDENTIFICATION METHOD BASED ON VARIATIONAL MODE DECOMPOSITION AND ENVELOPE FITTING AND ITS APPLICATIONS
J. BIAN¹, Y.-N. CHEN¹, Q. MEI¹, Y.-L XU¹, Y.-H. LU¹; ¹AECC Hunan Aviation Powerplant Research Institute, China
Reserve Paper 10.6.R A PERTURBATION ANALYSIS OF NONLINEARITY IN LANDING-GEAR SHIMMY OF A FLEET AIRCRAFT
M.-L Kou, AECC CAE, China
Reserve Paper 10.6.R ANALYSIS OF WHIRL VIBRATION IN AN AIRCRAFT BRAKE SYSTEM DURING BRAKING
D.Y.H Han, China
Reserve Paper 10.6.R NUMERICAL SIMULATION AND EXPERIMENTAL INVESTIGATION ON FLUTTER AND NON-SYNCHRONOUS VIBRATION
Yuzhi Chen¹, Da Mo¹, Qing Du¹, Lin Yang¹, Mingsui Yang¹; ¹AECC Shenyang Engine Research Institute, China
11.6Aircraft & UAV as Sensor Platform
Chair(s): Goes, L., Fu, J.
Track 11
07 - Systems, Subsystems and Equipment
07. Sep 21 13:00 13:30 11.6.1 SYSTEM OF UNMANNED AERIAL VEHICLES FOR WILD BOARS WITH AFRICAN SWINE FEVER SYMPTOMS DETECTION
K.-S. Sibilski, Air Force Institute of Technology, Poland
07. Sep 21 13:30 14:00 11.6.2 EVALUATION OF AN OBSTACLE TRACKING SYSTEM FOR AIRCRAFT GROUND OPERATIONS
K.T. Theuma, University of Malta, Malta
12.6Condition Based Maintenance 2
Chair(s): , , Kecen, H.
Track 12
11 - Operations and Sustainment
07. Sep 21 13:00 13:30 12.6.1 CONDITION BASED MAINTENANCE (CBM) IN THE DIGITAL TRANSFORMATION STREAM
V GROS¹, P.-Ch ROLLAND¹, S VERON¹, B ORDY¹, F DESSERTENNE, AIRBUS OPERATIONS SAS, France; ¹AIRBUS SAS, France
07. Sep 21 13:30 14:00 12.6.2 ANALYSIS OF THE ECONOMIC PERFORMANCE FOR AIRCRAFT MAINTENANCE USING DATA DRIVEN APPROACH
X Zhao, China
07. Sep 21 14:00 14:30 12.6.3 TOTAL LIFE CYCLE COST AND EMISSION OF ELECTRIC, HYBRID – ELECTRIC AIRCRAFT
N. D. Dung, Budapest University of Tech. and econ.;, Hungary
Reserve Paper 12.6.R A METHOD FOR EVALUATING THE APPLICABILITY OF MAINTENANCE TASKS BASED ON HELICOPTER HEALTH AND USAGE MONITORING SYSTEM
DN DONG¹, ZY JIA¹, Y ZHOU¹; ¹AVIC China Aero-Polytechnology Establishment, China
13.6Flight Control and Critical Situations
Chair(s): ,
Track 13
10 - Safety and Security
07. Sep 21 13:00 13:30 13.6.1 ACTIVITY CHARACTERISTICS AND THE MECHANISM OF MESO-MICRO SCALE DISTURBANCES IN THE EAST ASIAN SUBTROPICAL UPPER-LEVEL JE
X Chen¹, J Huang¹, M Meng, Wenzhou Meteorological Burea, China; C Chen¹, Q Chen¹; ¹China Aerodynamics Research and Development Center, China
07. Sep 21 13:30 14:00 13.6.2 A METHODOLOGY FOR CHARACTERISING LOSS OF CONTROL IN FLIGHT ACCIDENTS
J.P. Macedo, Univeristy of Sao Paulo, Brazil
07. Sep 21 14:00 14:30 13.6.3 MAIN OUTCOMES FROM H2020 VISION PROJECT: EU-JAPAN COLLABORATIVE RESEARCH IN INTELLIGENT FLIGHT CONTROL STSTEMS
Y. Watanabe, ONERA, France
Reserve Paper 13.6.R ANALYSIS OF RISK FACTORS AND IDENTIFICATION OF PRECURSORS OF RUNWAY EXCURSIONS AT LANDING
Nail: N. Khairullin, Central Aerohydrodynamic Institute (TsAGI), Russia
Reserve Paper 13.6.R RESEARCH ON FAULT DETECTION AND FAULT RECONFIGURATION OF FLUSH AIR DATA SENSING
Jia Qianlei, China; Zhang Weiguo, China; Hu Jiayue, China; Safwat Ehab, Egypt
Reserve Paper 13.6.R CONCEPT OF A NEW SYSTEM SYNTHESIZING METEOROLOGICAL AND OROGRAPHIC INFLUENCES ON THE AIRPLANE SAFE ENERGY ENVELOPE
X. Liu¹, L. Manfriani¹, Y. Fu, Lab. of Aerosp. Servo Actuation and Transmission, Beihang Univ., China; ¹Centre for Aviation, Zurich University of Applied Sciences, Switzerland

0.3Interactive presentations
Chair:
07. Sep 21 14:30 16:00

16:00 - 16:10Break

0.4General Lecture 2 - Future needs you-the panel discussion of the skills of aeronautics C.Combs, USA T.Ito, Japan
Chair: M. Kanerva ICAS ECSC Chair
07. Sep 21 16:10 17:00

0.5ICAS Lecture for Innovation in Aeronautics - Electrification - The third revolution in aviation, Corey Combs, USA
Chair:
07. Sep 21 17:00 18:00

Wednesday, 08. Sep 2021

7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
1.7Hybrid/Electric & Unconventional Aircraft 2
Chair(s): Prakasha, P.
Track 1
01 - Aircraft Design and Integrated Systems
08. Sep 21 08:00 08:30 1.7.1 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
08. Sep 21 08:30 09:00 1.7.2 CONCEPTUAL DESIGN OF SILENT ELECTRIC COMMUTER AIRCRAFT
P. Wassink, German Aerospace Center (DLR), Germany; G. Atanasov¹, C. Hesse¹, B. Froehler¹; ¹German Aerospace Ce, Germany
08. Sep 21 09:00 09:30 1.7.3 MULTIFIDELITY OPTIMISATION OF A BLENDED WING BODY MARTIAN GLIDER
D. Verstraete, The University of Sydney, Australia
08. Sep 21 09:30 10:00 1.7.4 DESIGN OF A PROTOTYPE 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
2.7UAS 1
Chair(s): Gerhards, R.
Track 2
01 - Aircraft Design and Integrated Systems
08. Sep 21 08:00 08:30 2.7.1 HYBRID POWER SYSTEM FOR NEW GENERATION OF VTOL UNMANNED AERIAL VEHICLES WITH A TAKE-OFF WEIGHT OF UP TO 300 KG
L. Czajkowski, ?ukasiewicz Research Network - Institute of Aviation, Poland
08. Sep 21 08:30 09:00 2.7.2 DEVELOPMENT OF A TURN-KEY, INTEGRATED RAPID DESIGN AND MANUFACTURING ENVIRONMENT FOR SUAS
D. Verstraete, The University of Sydney, Australia
08. Sep 21 09:00 09:30 2.7.3 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
08. Sep 21 09:30 10:00 2.7.4 INTEGRATED AERODYNAMIC DESIGN OF PROPELLER POSITION AND WING SHAPE AT A LOW REYNOLDS NUMBER
Wei YANG, National University of Defense Technology, China; Lei YU¹, Wenhua WU¹, Zhaolin FAN¹; ¹China Aerodynamics Research and Development Center, China
3.7AFLoNext
Chair(s): ,
Track 3
15 - Guest lectures
08. Sep 21 08:00 08:30 3.7.1 FLIGHT TEST OF AN ADVANCED HYBRID-LAMINAR-FLOW-CONTROL (HLFC) SYSTEM ON AN A320 VERTICAL TAIL PLANE
H. von Geyr, German Aerospace >Centre, DLR, Germany
08. Sep 21 08:30 09:00 3.7.2 ACTIVE FLOW CONTROL (AFC) AT PYLON / WING JUNCTION OF CIVIL AIRCRAFT – A FULL-SCALE DEMONSTRATION
T. M. Gibson, Airbus Operations Limited, United Kingdom
08. Sep 21 09:00 09:30 3.7.3 NOISE REDUCTION AT FLAP SIDE EDGE AND UNDERCARRIAGE
S Pott-Pollenske, DLR, Germany
08. Sep 21 09:30 10:00 3.7.4 MAIN LANDING GEAR DOORS VIBRATION REDUCTION BASED ON FLIGHT TEST
R Abarca Lopez, Airbus, Spain
4.7Applied CFD 1
Chair(s): Wan, T., Liu, P.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
08. Sep 21 08:00 08:30 4.7.1 TRAJECTORY PREDICTIONS FOR THE MK-82 STORE FROM A GENERIC CAVITY
Alex CENKO, AIWS, United States
08. Sep 21 08:30 09:00 4.7.2 STALL PREDICTION OF AIRCRAFT WITH ADAPTIVE HYBRID MESH
J. Tang¹, J. Zhang¹, N.-C. Zhou¹, B. Li¹, P.-C. Cui¹; ¹China Aerodynamics Research and Development Center, China
08. Sep 21 09:00 09:30 4.7.3 COMPUTATIONAL STUDY ON COAND? BLANKET CURVATURE EFFECTS ON HALF-SPHERICAL COAND? DEVICE PERFORMANCE
Harijono Djojodihardjo, The Institute for the Advancement of Aerospace Science and Techn, Indonesia; M.Arif Andira¹, Ratih Julistina¹, M.Agoes Moeljadi, Institute of Technology Bandung, Indonesia; ¹CCIT Group Indonesia, Indonesia
08. Sep 21 09:30 10:00 4.7.4 NUMERICAL SIMULATION AND ANALYSIS OF SECOND THROAT IN LARGE WIND TUNNELS
D.-X. LIAO¹, J.-M. CHEN¹, H.-G. QIN¹; ¹CARDC, China
Reserve Paper 4.7.R A VALIDATION STUDY FOR EFFECT OF CAMBER IN A MULTI ELEMENT AIRFOIL IN SUBSONIC FLOW CONDITIONS
E. GULRAIZ, RCMS, NUST, Pakistan
Reserve Paper 4.7.R HELICOPTER ROTOR AERODYNAMIC PERFORMANCE PREDICTION BASED ON FLOW SIMULATION AROUND AIRFOILS
S.-Z. Zhao¹, X. Zhao¹, K. You¹, M.-H. Kang¹, Y.-F. Lin, China Helicopter Research and Development Institute, China; ¹Northwestern Polytechnical University, China
5.7Configurations
Chair(s): ,
Track 5
03.4 - Applied Aerodynamics
08. Sep 21 08:00 08:30 5.7.1 INTAKE BOUNDARY LAYER PROFILE ESTIMATION FOR BLI PERFORMANCE PREDICTION ON A BLENDED WING BODY
K. Ma¹, S. Prince¹; ¹Cranfield University, United Kingdom
08. Sep 21 08:30 09:00 5.7.2 NUMERICAL INVESTIGATION ON FLOW INTERFERENCE BETWEEN BLENDED-WING-BODY AIRCRAFT AND OVERHANGING NACELLE
Aoxiang Qiu¹, Weimin sang¹, Run Pang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
08. Sep 21 09:00 09:30 5.7.3 PRELIMINARY AERODYNAMIC DESIGN AND ANALYSIS OF TRUSS-BRACED WING REGIONAL AIRCRAFT USING HIGH-FIDELITY METHODS
S. Hosseini, Amirkabir University of Technology, Iran
08. Sep 21 09:30 10:00 5.7.4 AN OPTIMIZATION OF ANTI-ICING CHAMBER BASED ON POD AND KRIGING
Junjie: J Niu¹, Weimin: W Sang¹, Aoxiang:A Qiu¹, Qilei: Q Guo¹, Dong: D Li¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
Reserve Paper 5.7.R AN INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS FOR SAAB J-29 AIRCRAFT DESIGN USING HIGH FIDELITY CFD
M. Zhang, Airinnova AB, Sweden
6.7Transition Physics 2
Chair(s): Atkin, C., Mugal, S.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
08. Sep 21 08:00 08:30 6.7.1 STABILIZATION OF SUPERSONIC BOUNDARY LAYERS IN THE PRESENCE OF FAVORABLE PRESSURE GRADIENT
P.V. Chuvakhov¹, A.V. Fedorov, Moscow Institute of Physics and Technology (MIPT), Russia; A.O. Obraz¹; ¹Central Aerohydrodynamic Institue (TsAGI), Russia
08. Sep 21 08:30 09:00 6.7.2 NUMERICAL SIMULATION OF THREE-DIMENSIONAL DISTURBANCES EVOLUTION IN SUPERSONIC FLOW OVER A WAVY SURFACE
A.V. Novikov, TsAGI, MIPT, Russia; A.V. Fedorov, MIPT, Russia
08. Sep 21 09:00 09:30 6.7.3 MECHANISMS OF NATURAL LAMINAR-TURBULENT TRANSITION ON AN UNSWEPT WING IN SUPERSONIC FLIGHT
P.V. Chuvakhov¹, A.V. Fedorov², A.O. Obraz¹, I.O. Pogorelov²; ¹Central Aerohydrodynamic Institue (TsAGI), Russia ;²Moscow Institute of Physics and Technology (MIPT), Russia
08. Sep 21 09:30 10:00 6.7.4 TRIGGERING SUPERSONIC BOUNDARY-LAYER INSTABILITY BY SMALL-SCALE VORTEX SHEDDING
G. Tu, State Key Laboratory of Aerodynamics, China
Reserve Paper 6.7.R GLOBAL STABILITY ANALYSIS ON A LIFTING-BODY BOUNDARY LAYER
X. Chen, China
7.7Performance
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
08. Sep 21 08:00 08:30 7.7.1 ROBUST DESIGN OF 3D SHOCK CONTROL BUMPS TO TRANSPORT AIRCRAFT UNDER REALISTIC UNCERTAINTIES
C. Sabater¹, S. Goertz¹; ¹German Aerospace Center (DLR), Germany
08. Sep 21 08:30 09:00 7.7.2 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
08. Sep 21 09:00 09:30 7.7.3 INCREASING THE EFFECTIVENESS OF AN AERODYNAMICALLY BALANCED CONTROL SURFACE ON A MODIFIED AIRFOIL WITH REDUCED DRAG
V.V. Bogatyrev, TsAGI, Russia
08. Sep 21 09:30 10:00 7.7.4 DESIGN OF WINGTIP SAILS FOR A LARGE-ASPECT-RATIO WING
Y. Liu¹, R. Zeng¹, L. Ping¹; ¹CETC Wuhu Diamond Aircraft Manufacture co., LTD, China
Reserve Paper 7.7.R AERODYNAMIC DESIGN AND ANALYSIS ON A NEW STEPPED WINGLET BASED ON THE DYNAMIC CHARACTERISTICS OF THE WINGTIP VORTEX
J.Jin Jin, Shanghai Aircraft Design and Research Institute,COMAC, China
8.7Testing and Measurement
Chair(s): Bisagni, C., Li, K.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
08. Sep 21 08:00 08:30 8.7.1 RESEARCH ON ATTITUDE CONTROL AND CONSTRAINT SYSTEM DESIGN OF FULL-SCALE AIRCRAFT STATIC TEST BASED ON BARYCENTRE
JJ ZHENG, AVICASRI, China
08. Sep 21 08:30 09:00 8.7.2 NON-CONTACT MEASUREMENT OF SURFACE DEFORMATION FIELDS BY VIDEOGRAMMETRY METHOD
K.A. Kuruliuk, Central Aerohydrodynamic Institute n. a. prof. N.E. Zhukovsky, Russia
08. Sep 21 09:00 09:30 8.7.3 OPTIMIZATION FOR PROCESS AND MANAGEMENT IN MASSIVE STRAIN MEASUREMENT IN THE FULL SCALE AIRCRAFT STRUCTURE STRENGTH TEST
J. Zuo, Aircraft Strength Research Institute of China, China
08. Sep 21 09:30 10:00 8.7.4 DESIGN OF A VERTICAL DITCHING TEST
G. Nicolosi¹, F. Valpiani¹, A. Polla¹, G. Grilli¹, A. Saponaro Piacente¹, L. Di Ianni¹, E. Cestino¹, V. Sapienza, Aeronautical Consultant, Italy; P. Piana, TescoGo, Italy; ¹Politecnico di Torino, Italy
Reserve Paper 8.7.R A SUBJECTIVE EVALUATION METHOD OF AIRCRAFT VIBRATION IN FLIGHT TEST
Haigang Wang, COMAC Flight test Center, China
Reserve Paper 8.7.R RESEARCH PROGRESS OF DISTRIBUTED OPTICAL FIBER SENSING DEFORMATION MEASUREMENT FOR MORPHING WING
J F Xue, Chinese Aeronautical Establishment, China
9.7Advanced Manufacturing Management
Chair(s): Wang, S.
Track 9
08 - Manufacturing and Supply Chain Management
08. Sep 21 08:00 08:30 9.7.1 ASSESSING THE IMPACT OF PRODUCTION MODELING IN CONCEPTUAL AIRCRAFT DESIGN
J. Page Risueno, German Aerospace Center (DLR), Germany
08. Sep 21 08:30 09:00 9.7.2 A STRUCTURED AND SCALABLE APPROACH FOR THE DEFINITION OF DEEP LEARNING ARCHITECTURES FOR BEARING ANOMALY DETECTION
O Pinon Fischer, Georgia Institute of Technology, United States
08. Sep 21 09:00 09:30 9.7.3 INCORPORTING KNOWLEDGE COVERAGE MEASUREMENT INTO KNOWLEDGE TRANSFORMATION FROM DATA FOR KNOWLEDGE ACCUMULATION
Yubin Fan, Nanchang Hangkong University, China; Chuang Liu¹, Junbiao Wang¹; ¹Northwestern Polytechnical University, China
08. Sep 21 09:30 10:00 9.7.4 DESIGN AND BEST PRACTICES OF SUPPLIER PERFORMANCE EVALUATION IN SUPPLY CHAIN
HZ-L Li, AECC SHANGHAI COMMERCIAL AIRCRAFT ENGINE MANUFACTURING CO.,LTD., China
10.7Fault Detection
Chair(s): Wang, Y.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
08. Sep 21 08:00 08:30 10.7.1 AIRCRAFT BRAKING DYNAMICS AND BRAKE SYSTEM MODELING FOR FAULT DETECTION AND ISOLATION
L.C.N. Cardoso Navarro, ITA, Brazil
08. Sep 21 08:30 09:00 10.7.2 LEARNING FLIGHT CONTROL SKILLS BY IMITATING EXPERT DEMONSTRATIONS
R. Takase, The University of Tokyo, Japan
08. Sep 21 09:00 09:30 10.7.3 TWO-LAYER ADAPTIVE AUGMENTATION FOR INCREMENTAL BACKSTEPPING FLIGHT CONTROL OF AIRCRAFT IN FAILURE CONDITIONS
D. Ignatyev, Cranfield University, United Kingdom
08. Sep 21 09:30 10:00 10.7.4 FEEDBACK ERROR LEARNING WITH ENHANCED SAMPLING: NEURAL FAULT TOLERANT CONTROL OF AIRCRAFT
Y Nobuyuki, Mitsubishi Electric, Japan; S Shinji, The university of Tokyo, Germany
11.7Aspects of More electric Aircraft
Chair(s): Peters, M., Viola, N.
Track 11
07 - Systems, Subsystems and Equipment
08. Sep 21 08:00 08:30 11.7.1 OPTIMALPOWER DISTRIBUTION ON A MORE ELECTRIC AIRCRAFT
E. D'Amato, Università degli studi della Campania "Luigi Vanvitelli", Italy
08. Sep 21 08:30 09:00 11.7.2 ANTI-PUMP-FORCE-FIGHT PRESSURE CONTROLLER FOR A REDUNDANT HYDRAULIC POWER PACKAGE WITH SPEED VARIABLE AC MOTOR PUMPS
N. Trochelmann, TUHH/ Institute of Aircraft Systems Engineering, Germany
08. Sep 21 09:00 09:30 11.7.3 SURROGATE MODELS OF PM BRUSHLESS MOTORS FOR THE PRELIMINARY DESIGN OF AIRCRAFT APPLICATION SYSTEMS
F De Giorgi, INSA/ICA Toulouse, France
08. Sep 21 09:30 10:00 11.7.4 RESEARCH ON 18 PULSE AUTOTRANSFORMER RECTIFIER DEVICE FOR AVIATION
WX.-C Chen, China
12.7Airport/Aircraft Operation
Chair(s): Itoh, E.
Track 12
09 - Air Transport System Efficiency
08. Sep 21 08:00 08:30 12.7.1 INTEGRATION AND EVALUATION OF AN AIRCRAFT TAXIING SOLUTION USING AUTONOMOUS TOW TRUCKS
J Gauci, University of Malta, Malta
08. Sep 21 08:30 09:00 12.7.2 ERAS - EVALUATION OF REALISTIC APPROACH SCENARIOS FOR MINIMAL NOISE - PRELIMINARY FINDINGS
B Moberg, Vernamack AB, Sweden; P Näsman, KTH Royal Institute of Technology, Sweden; U Ziverts, Infobahn AB, Sweden
08. Sep 21 09:00 09:30 12.7.3 DESIGN AND TRIALING OF A CONCEPT OF OPERATIONS (CONOPS) FOR OPTIMAL CLIMBS AND DESCENTS INTO MEDIUM DENSITY AIRFIELDS
D. Zammit-Mangion, University of Malta, Malta
08. Sep 21 09:30 10:00 12.7.4 A NOVEL APPROACH FOR TURNAROUND TIME ALLOCATION BASED ON REINFORCEMENT LEARNING
A. Rodriguez-Sanz, Universidad Politecnica de Madrid (UPM), Spain; J. Herrera, Universidad Complutense de Madrid (UCM), Spain
Reserve Paper 12.7.R OPERATION PLANNING AIDED METHOD OF GENERAL AIRCRAFT BASED ON MULTI-CBR AND COMBINATION EVALUATION METHOD
R.-X. Xie, Beihang University, China
13.7Failure And Fracture Mechanics
Chair(s): Liao, M., Kanerva, M.
Track 13
04.1 - Material Issues, Fatigue and Damage Tolerance
08. Sep 21 08:00 08:30 13.7.1 FAILURE PROCESS IDENTIFICATION OF C-SIC WITH DIFFERENT TENSILE PERFORMANCE
Y.Z. Zhang¹, X.Y. Tong¹, L.J. Yao¹, A.T. Augousti, Kingston University London, United Kingdom; ¹Northwestern Polytechnical University, China
08. Sep 21 08:30 09:00 13.7.2 INVESTIGATION OF STOPPER STRAPS EFFECTS ON LONGITUDINAL CRACK GROWTH RATES IN A SKIN OF PRESSURIZED AIRCRAFT FUSELAGE
A.S. Kim, TsAGI, Russia
08. Sep 21 09:00 09:30 13.7.3 INFLUENCE OF NOTCH EFFECTS ON STATIC CHARACTERISTICS OF STEEL BASED ON THERMOGRAPHIC METHOD
Junling Fan¹, Wei Zhang¹; ¹Aircraft Strength Research Institute, China
08. Sep 21 09:30 10:00 13.7.4 EXPERIMENTAL INVESTIGATION AND NUMERICAL SIMULATION OF SINGLE LAP JOINTS OF ALLOY-ARAMID FIBER COMPOSITE BASED ON COHESI
ZTC Zou, Civil Aviation University of China, China
Reserve Paper 13.7.R A MICROPHONE POSITION CALIBRATION METHOD FOR A RANDOM ARRAY
Q He, China
Reserve Paper 13.7.R EXPERIMENTAL INVESTIGATION AND LIFE PREDICTION FOR DEFECT INDUCED CRACK OF A P/M NICKEL BASED SUPERALLOY
YI SHI, China; XIAOGUANG YANG, China; DUOQI SHI, China; DIDI YANG, China; GUOLEI MIAO, China; SHUANGQI LV, China

10:00 - 10:30Break

1.8Hybrid/Electric & Unconventional Aircraft 3
Chair(s): Melkert, J.
Track 1
01 - Aircraft Design and Integrated Systems
08. Sep 21 10:30 11:00 1.8.1 EXPERIMENTAL RESEARCH ON PROPULSION AND AERODYNAMIC CHARACTERISTICS OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT
X.-Y. Zhang¹, Z.-H. Gao¹, T. Lei¹, X.-B. Zhang¹, W. Zhang¹; ¹Northwesyern Polytechnical University, China
08. Sep 21 11:00 11:30 1.8.2 PROPULSIVE FUSELAGE AIRCRAFT CONCEPT – A SUMMARY OF STRUCTURE ANALYSIS BASED ON CENTRELINE H2020
Z. Goraj, Warsaw University of Technology, Poland
2.8Technology Integration & Education
Chair(s): Fusaro, R.
Track 2
01 - Aircraft Design and Integrated Systems
08. Sep 21 10:30 11:00 2.8.1 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; ¹Politecnico di Torino, Italy
08. Sep 21 11:00 11:30 2.8.2 OPEN SCIENCE IN AVIATION RESEARCH: THE INDIVIDUAL ADVANTAGE OF SHARING KNOWLEDGE
M. Spieck, Thelsys GmbH, Germany
08. Sep 21 11:30 12:00 2.8.3 MULTI-ROLE TANKER-TRANSPORT CONVERSION
Ilan Berlowitz, IBAero Engineering, Israel
3.8UAV Conflict Avoidance 2
Chair(s): Bang, H., Bil, C.
Track 3
06.2 - Flight Dynamics and Control (UAV related)
08. Sep 21 10:30 11:00 3.8.1 A NOVEL DETECT-AND-AVOID SYSTEM OF UAS IN URBAN ENVIRONMENT
L.N. Nurhakim, RMIT University, Australia
08. Sep 21 11:00 11:30 3.8.2 AUTONOMOUS CONFLICT RESOLUTION ALGORITHM BASED ON ELLIPTIC GEOMETRY
R.A. Sasongko, Institut Teknologi Bandung, Indonesia
08. Sep 21 11:30 12:00 3.8.3 MOTHERSHIP PLANE WITH SENSING DRONES SYSTEM FOR 3D MAPPING APPLICATIONS
M.J. Modzelewski, Warsaw University of Technology, Poland
4.8Numerical Methods 1
Chair(s): Viviani, A., Moura, R.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
08. Sep 21 10:30 11:00 4.8.1 VALIDATION OF A DISCONTINUOUS GALERKIN BASED DES SOLVER IN FLOW PROBLEMS USING HIGH PERFORMANCE COMPUTING
A. V. Wolkov¹, I.S. Bosnyakov¹, S.M. Bosnyakov¹, S.V. Mikhaylov¹, V.Y. Podaruev¹, A.I. Troshin¹; ¹Central Aerohydrodynamic Institute, Russia
08. Sep 21 11:00 11:30 4.8.2 ADVANCED WEEK SOLUTIONS IN FLUID DYNAMICS AND THEIR NUMERICAL COMPUTATIONS WITH AERODYNAMIC HEATING
Mikhail Ivanov¹, Vadim Mamaev¹, Jaling Li², Guanghua Zheng²; ¹CIAM, Russia ;²NWPU, China
08. Sep 21 11:30 12:00 4.8.3 A BENCHMARK METHOD FOR PREDICTING OBLIQUE SHOCK STRUCTURE
A. Shi, Northwestern Polytechnical University, China
Reserve Paper 4.8.R ACCURATE SIMULATIONS OF AIRCRAFT WAKE VORTICES WITH HIGH-ORDER NUMERICAL METHOD
S. Bosnyakov, TsAGI, Russia
5.8UAV Flight Testing
Chair(s): Wong, K.C., Monk, J.
Track 5
06.2 - Flight Dynamics and Control (UAV related)
08. Sep 21 10:30 11:00 5.8.1 VALIDATION OF SCALED FLIGHT TESTING - OVERALL APPROACH AND FIRST RESULTS
P. Schmollgruber, France
08. Sep 21 11:00 11:30 5.8.2 FLIGHT TESTING OF 65KG FLEXOP SUBSCALE DEMONSTRATOR
J. Bartasevicius¹, S. Koeberle¹, D. Teubl¹, C. Roessler¹, M. Hornung¹; ¹ Institute of Aircraft Design, Technical University of Munich, Germany
08. Sep 21 11:30 12:00 5.8.3 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
6.8Flow Control Applications 2
Chair(s): Goraj, Z., Prince, S.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
08. Sep 21 10:30 11:00 6.8.1 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
08. Sep 21 11:00 11:30 6.8.2 ENHANED STRAIGHT BLADED VAWT BY RETRACTABLE GURNEY FLAPS
K. Song, Northwestern Polytechnical University, China
08. Sep 21 11:30 12:00 6.8.3 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
Reserve Paper 6.8.R APPLICATION OF A LEADING-EDGE TIP EXTENSION ON DELTA WING WITH WINGLET FOR HIGH LIFT
X.Y. Feng, Northwestern Polytechnical University, China
7.8Optimization 1
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
08. Sep 21 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
08. Sep 21 11:00 11:30 7.8.2 PARETO FRONT EXPLORATION USING MANIFOLD LEARNING APPROACH FOR ROTORCRAFT AIRFOILS DESIGN
C. Song, China; W.-B. Li, China; Z. Zhou, China; H.-Y. Liu, China; X. Luo, China
08. Sep 21 11:30 12:00 7.8.3 MULTI-OBJECTIVE AERODYNAMIC SHAPE OPTIMIZATION OF WIDE-MACH-NUMBER-RANGE WING CONSIDERING LIFT MATCHING
Y Zhang¹, Z, -H. Han¹, F Liu¹, C.-Z. Xu¹; ¹Northwestern Polytechnical University, China
Reserve Paper 7.8.R 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
8.8Morphing Structures
Chair(s): Franke, F., Abramovich, H.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
08. Sep 21 10:30 11:00 8.8.1 RESEARCH PROGRESS OF DISTRIBUTED OPTICAL FIBER SENSING DEFORMATION MEASUREMENT FOR MORPHING WING
X-Jf Xue, Chinese Aeronautical Establishment, China
08. Sep 21 11:00 11:30 8.8.2 ACTUATION MECHANISM USING SHAPE MEMORY ALLOY WIRES IN SPIRAL ARRANGEMENT
Ryota Tsukamoto¹, Atsuhiko Senba¹, Tadashige Ikeda, Chubu University, Japan; Masato Tamayama², Hitoshi Arizono²; ¹Meijo University, Japan ;²JAXA, Japan
08. Sep 21 11:30 12:00 8.8.3 MORPHING AIRCRAFT BASED ON SMART MATERIALS AND STRUCTURES
J. Sun, Harbin Institute of Technology, China
9.8Additive Manufacturing
Chair(s): Zhang, J.
Track 9
08 - Manufacturing and Supply Chain Management
08. Sep 21 10:30 11:00 9.8.1 EFFECTS OF COOLANT BUILD DIRECTION ON ADDITIVELY MANUFACTURED FAN-SHAPED COOLING HOLES
Qi Zeng¹, Chaochao Li¹, Jun Cao¹, Buming Wang¹; ¹AECC HAPRI, China
08. Sep 21 11:00 11:30 9.8.2 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
08. Sep 21 11:30 12:00 9.8.3 AN EFFICIENT FINITE ELEMENT SIMULATION METHOD FOR ADDITIVE MANUFACTURING PROCESSES
Liu Qingyi¹, Wang Zhaoyang¹, Yan Peng¹, Ruan Hui¹, Xue Haozhou¹, Dong Leiting¹; ¹Beihang University, China
10.8Flying Quality
Chair(s): Yokoyama, N.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
08. Sep 21 10:30 11:00 10.8.1 CONTROL ALLOCATION FOR ONERA\'S SMALL BUSINESS CONCEPT PLANE AMPERE WITH DISTRIBUTED ELECTRIC PROPULSION
C. DÖLL, ONERA, France
08. Sep 21 11:00 11:30 10.8.2 ON THE MAXIMIZATION OF CONTROL POWER IN LOW-SPEED FLIGHT FOR A BWB CONFIGURATION
LMBC Campos, IDMEC/CCTAE/IST, Portugal; Joaquim Marques, Escola de Ciências e Tecnologias, Universidade de Évora, Portugal
08. Sep 21 11:30 12:00 10.8.3 AN ACTIVE SIDESTICK CONTROLLER FOR AIRCRAFT GROUND OPERATIONS
J Gauci, University of Malta, Malta
Reserve Paper 10.8.R THE APPLICATION OF THE PILOT-AIRCRAFT SYSTEM APPROACH FOR OPTIMIZING 3D DISPLAY PARAMETERS
A. V. Efremov¹, M. S. Tiaglik¹, I. Kh. Irgaleev¹; ¹Moscow Aviation Institute, Russia
11.8System Health Monitoring
Chair(s): Mare, J., Stumpf, E.
Track 11
07 - Systems, Subsystems and Equipment
08. Sep 21 10:30 11:00 11.8.1 DAMAGE DETECTION OF AERONAUTICAL PANELS BY USING CROSS-CORRELATION OF SPATIALLY SHIFTED DISTRIBUTED STRAIN SENSORS
M. Ciminello, C.I.R.A. Italian Aerospace Research Center, Italy
08. Sep 21 11:00 11:30 11.8.2 THEORETICAL AND EXPERIMENTAL STUDY FOR THE DEVELOPMENT OF SELF-POWERED MONITORING SYSTEMS WITH MFC PIEZOELECTRIC PATCHES
G. Di Rito¹, M.-R. Chiarelli¹, V. Franchi¹, L. Bancallari, MBDA Italia S.p.A., Italy; B. Luciano, AESIS s.r.l., Italy; ¹Università di Pisa - Dipartimento di Ing. Civile ed Industriale, Italy
08. Sep 21 11:30 12:00 11.8.3 STUDY ON CLOSED-LOOP CROSS COMPENSATION CONTROL TECHNOLOGY IN ACCELERATED FATIGUE TEST
HONGWEI ZHAO¹, HONGWEI ZHAO, Xi’an jiaotong University, China; HAN TAO¹, ZHENZHONG GU, Chongqing Hongyu Precision Industrial Co., Ltd., China; GUANGSHENG SHI, Shenyang Aircraft Design & Research Institute of China, China; JIANMIN FENG¹, SHIHUI DUAN¹; ¹Aircraft Strength Research Institute of China, China
Reserve Paper 11.8.R DESIGN OF DATA SERVICE ARCHITECTURE FOR AVIATION PHM SYSTEM BASED ON MULTI-LAYER PROTOCOL
P.J. Wang, Tsinghua University, China
Reserve Paper 11.8.R RELIABILITY ANALYSIS AND EVALUATION METHOD FOR DESIGN APPRAISAL OF AIRBORNE EQUIPMENTS
Z-J-L Zhang, AVIC XI’AN AIRCRAFT INDUSTRY (GROUP) COMPANY LTD., China
12.8Airspace Management
Chair(s): Andreeva Mori, A.
Track 12
09 - Air Transport System Efficiency
08. Sep 21 10:30 11:00 12.8.1 ANGULAR 3D INSTRUMENT APPROACHES FOR GLS EQUIPPED AIRCRAFT USING A LIGHT AND MOBILE SBAS TO GBAS CONVERTER
T. Dautermann, DLR , Germany
08. Sep 21 11:00 11:30 12.8.2 ON THE MINIMUM SEPARATION BETWEEN ANY PAIR OF FLIGHT PATHS
LMBC Campos, IDMEC/CCTAE/IST, Portugal; Joaquim Marques, Escola de Ciências e Tecnologias, Universidade de Évora, Portugal
08. Sep 21 11:30 12:00 12.8.3 DESIGNING AIRCRAFT TRAFFIC FLOWS USING DATA-DRIVEN QUEUING MODELS
E. Itoh, ENRI, Japan
13.8Structural Integrity and Fatigue
Chair(s): Liao, M., Blom, A.
Track 13
04.1 - Material Issues, Fatigue and Damage Tolerance
08. Sep 21 10:30 11:00 13.8.1 DEVELOPMENT OF AIRFRAME DIGITAL TWIN TECHNOLOGY FOR AIRCRAFT STRUCTURAL INTEGRITY MANAGEMENT PROGRAM
Min Liao, National Research Council Canada, Canada
08. Sep 21 11:00 11:30 13.8.2 A DIGITAL EQUIVALENT DEVELOPMENT FOR FATIGUE AND DAMAGE TOLERANCE IN AIRCRAFT STRUCTURES
Laura Zaplana Manzano¹, Javier Romero Arana¹, Javier Gómez-Escalonilla Martín¹; ¹AIRBUS DS, Spain
08. Sep 21 11:30 12:00 13.8.3 EXPERIMENTAL STUDY OF THE EFFECT OF BIAXIAL STRESS STATE ON THE GROWTH RATE OF FATIGUE CRACKS
A.V. Kulemin, Central Aerohydrodynamic Institute n. a. N.E. Zhukovsky (TsAGI), Russia
Reserve Paper 13.8.R INVESTIGATION OF THE INFLUENCE OF LOW AMPLITUDE LOADS ON THE FATIGUE LIFE OF CFRP SAMPLES WITH IMPACT DAMAGE UNDER IRRE
V.G. Lukyanchuk, Central Aerohydrodynamic Institute, TsAGI, Russia, Russia

12:00 - 13:00Lunch

1.9System of Systems
Chair(s): Padulo, M.
Track 1
01 - Aircraft Design and Integrated Systems
08. Sep 21 13:00 13:30 1.9.1 SYSTEM OF SYSTEMS DRIVEN AIRCRAFT DESIGN FOR WILDFIRE SUPPRESSION
Prajwal Shiva Prakasha¹, Bjoern Nagel¹; ¹German Aerospace Center, Germany
08. Sep 21 13:30 14:00 1.9.2 OPTIMAL AIRLINE FLEET COMPOSED BY A COMBINATION OF JET AND TURBOPROP AIRPLANES
Mattos, B. S. Mattos, Instituto Tecnologico de Aeronautica (ITA), Brazil
08. Sep 21 14:00 14:30 1.9.3 BENEFIT ANALYSIS OF AIR REFUELING SYSTEM IN ULTRA LONG RANGE ROUTE OPERATION
C. MA¹, J.T. SI¹, Y.C. CHEN, Commercial Aircraft Corporation of China, China; ¹Shanghai Aircraft Design and Research Institute, China
08. Sep 21 14:30 15:00 1.9.4 CLOUD-BASED ENVIRONMENT FOR AIRCRAFT DESIGN COLLABORATION
X. Chen¹, A. Riaz¹, M. D. Guenov¹; ¹Cranfield University, United Kingdom
08. Sep 21 15:00 15:30 1.9.5 QUANTIFICATION OF OPERATIONAL EFFECTIVENESS FOR TECHNOLOGY EVALUATION
A Hull, United States; A Sudol, United States; D Mavris, United States
2.9UAS 2
Chair(s): Gerhards, R.
Track 2
01 - Aircraft Design and Integrated Systems
08. Sep 21 13:00 13:30 2.9.1 MULTIDISCIPLINARY OPTIMISATION OF A FUEL-CELL-POWERED EVTOL FIXED-WING CARGO UAV
D. Verstraete, The University of Sydney, Australia
08. Sep 21 13:30 14:00 2.9.2 CONCEPTUAL DESIGN FOR LONG-ENDURANCE CONVERTIBLE UNMANNED AERIAL SYSTEM
Y Leng, ISAE, France
08. Sep 21 14:00 14:30 2.9.3 DESIGN OF A HYBRID-POWER VTOL LOGISTICS UAV SYSTEM INTEGRATED INTO THE CIVIL AVIATION AIR TRAFFIC MANAGEMENT SYSTEM
Jiang Hanjie¹, Zhou Ye¹; ¹School of Aerospace Engineering, Universiti Sains Malaysia, Malaysia
08. Sep 21 14:30 15:00 2.9.4 DESIGN OPTIMIZATION OF MULTIROTOR DRONES IN FORWARD FLIGHT
F. Pollet¹, S. Delbecq¹, M. Budinger, INSA Toulouse/ICA, France; J.-M. Moschetta¹; ¹ISAE-SUPAERO, France
08. Sep 21 15:00 15:30 2.9.5 AERODYNAMIC ANALYSIS ON TAIL-SITTER UAV HOVERING UNDER CROSSWIND
Chen Jiaojiao Jiaojiao, Northwestern Polytechnical University, China
Reserve Paper 2.9.R LIGHTWEIGHT UAV FOR EMERGENCY MEDICAL SERVICE
Tomasz Goetzendorf-Grabowski¹, Jacek Mieloszyk¹, Marcin Figat¹, Andrzej Tarnowski¹, Bogdan Hernik¹; ¹Warsaw University of Technology, Poland
Reserve Paper 2.9.R CONCEPTUAL DESIGN AND IMPLEMENTATION OF A NOVEL TRICOPTER FIXED-WING VTOL UAV CONFIGURATION
P. Stahl, Technical University of Munich, Germany
3.9Model Based Systems Engineering
Chair(s): Vijgen, P., Müller Wiesner, D.
Track 3
02 - Systems Engineering and Integration
08. Sep 21 13:00 13:30 3.9.1 MODEL-BASED ENGINEERING OF A SYSTEM DIAGNOSTIC ENGINE FOR AN AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM
F. Mardt, Hamburg University of Technology, Germany
08. Sep 21 13:30 14:00 3.9.2 A MBSE DESIGN ARCHITECTURE FOR CONTROL SYSTEM BASED ON DEMAND ELEMENT TRANSFER
P.J. Wang, Tsinghua University, China
08. Sep 21 14:00 14:30 3.9.3 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
08. Sep 21 14:30 15:00 3.9.4 TOWARDS THE NEXT GENERATION OF COMPLEX SYSTEMS ARCHITECTING: A MBSE FRAMEWORK TO AIRCRAFT DEVELOPMENT
P. D. Ciampa, DLR, Germany
08. Sep 21 15:00 15:30 3.9.5 HYBRID MODELLING FOR FULL MISSION SIMULATION
P Krus, Linköping university, Sweden; R Braun, ICAS2020_0980, Sweden; E Villani, Instituto Tecnológico de Aeronáutica, Brazil
Reserve Paper 3.9.R MODEL-BASED STAKEHOLDER REQUIREMENTS DEFINITION FOR JOINT MISSION PLANNING SYSTEM
D.-Z. Du, Aviation Industry Development Research Center of China, China
Reserve Paper 3.9.R SOS BEHAVIOR MODEL TRANSFORMATION FOR AIRCRAFT TOP-LEVEL DEMONSTRATION
Jing Zang¹, Jiaqiang Zhu¹; ¹Chinese Aeronautical Establishment, China
Reserve Paper 3.9.R MODEL-BASED VIRTUAL INTEGRATED TEST METHOD FOR AVIONICS SYSTEM
Shaofan Zhu¹, Peipei Xing¹; ¹COMAC Beijing Aircraft Technology Research Institute, China
Reserve Paper 3.9.R 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
4.9Applied CFD 2
Chair(s): Wei, S., Azevedo, J.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
08. Sep 21 13:00 13:30 4.9.1 EXPERIMENTAL VALIDATION OF NUMERICAL PREDICTION OF WING-PROPELLER AERODYNAMIC INTERACTION
S. De Lucas Bodas¹, J. Narbona Gonzalez¹, Victor Ossorio Contreras¹, J. J. Guerra Crespo¹, D. E. Funes Sebastian¹, L. P. Ruiz Calavera¹; ¹Airbus Defence & Space, Spain
08. Sep 21 13:30 14:00 4.9.2 FLOW STRUCTURE INVESTIGATION OF CONTRA-ROTATING WIND TURBINES BY CFD AND EXPERIMENTAL METHODS
K You, Northwestern Polytechnical University, China
08. Sep 21 14:00 14:30 4.9.3 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
08. Sep 21 14:30 15:00 4.9.4 NUMERICAL INVESTIGATION OF WING ROCK PHENOMENON ON LOW ASPECT RATIO RECTANGULAR WINGS AT LOW REYNOLDS NUMBER
Aamir Sultan¹, Adnan Maqsood¹, Tiauw Hiong Go, Raytheon Missile Systems, United States; Rizwan Riaz¹; ¹National University of Sciences & Technology, Pakistan
08. Sep 21 15:00 15:30 4.9.5 A COMPUTATIONAL FLUID DYNAMICS ANALYSIS OF A HISTORICAL SEAPLANE CRUISE AND TAKE OFF PERFORMANCE
C. Baldon¹, R. Indelicato¹, M. Sinisi¹, N. Bottino¹, F. Carrone¹, G. Cantanna¹, E. Cestino¹, V. Sapienza, Aeronautical Consultant, Italy; ¹Politecnico di Torino, Italy
Reserve Paper 4.9.R ADVANCED AIRCRAFT FIRE EXTINGUISHING NUMERICAL SIMULATION
Y. SOMMERER, AIRBUS, France
Reserve Paper 4.9.R FLUID STRUCTURE INTERACTION OF RAM-AIR PARACHUTE TRAILING EDGE DEFLECTION
Gao XL Gao, China Aerodynamics Research and Development Center, China
Reserve Paper 4.9.R 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
Reserve Paper 4.9.R 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
5.9Impact
Chair(s): Han, J., Bayandor, J.
Track 5
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
08. Sep 21 13:00 13:30 5.9.1 BIRD STRIKE SIMULATIONS IN MSC.SOFTWARE: CORRELATION BETWEEN THE EXPERIMENTS AND SIMULATIONS
V. Symonov¹, J. Juracka¹; ¹Brno University of Technology, Czech Republic
08. Sep 21 13:30 14:00 5.9.2 MODELS AND METHODS FOR DRONE STRIKE LOAD PREDICTIONS
Florian Franke¹, Uli Burger¹, Christian Hühne, DLR, Germany; ¹Technische Hochschule Ingolstadt, Germany
08. Sep 21 14:00 14:30 5.9.3 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
08. Sep 21 14:30 15:00 5.9.4 MULTISCALE ANALYSIS OF BALLISTIC IMPACT OF WOVEN COMPOSITE MATERIALS
D SONG, China
08. Sep 21 15:00 15:30 5.9.5 DEVELOPMENT OF A PREDICTIVE METHODOLOGY FOR FAST ESTIMATION OF IMPACT BEHAVIOR IN AEROSPACE GRADE COMPOSITES
H. Raza¹, O. R. Garcia², K. Carpenter¹, T. Pärnänen², J. Jokinen², M. Kanerva², J. Bayandor¹; ¹CRASH Lab, University at Buffalo, United States ;²Tampere University , Finland
6.9Unsteady Flow Phenomena
Chair(s): Breitsamter, C., Wong, P.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
08. Sep 21 13:00 13:30 6.9.1 INVESTIGATIONS OF AERODYNAMIC CHARACTERISTICS AND LAMINAR-TURBULENT TRANSITION ON LARGE-SCALE TRANSONIC AIRFOIL
V.G. Soudakov, TsAGI, Russia
08. Sep 21 13:30 14:00 6.9.2 TYPES OF TRANSONIC BUFFET FOR A LAMINAR AIRFOILS
P.A. Polivanov, Khristianovich Institute of Theoretical and Applied Mechanics SB, Russia
08. Sep 21 14:00 14:30 6.9.3 BUFFET CONTROL ON STRUCT-BRACED WING AIRCRAFT USING TANGENTIAL BLOWING
S Li, School of Aerospace Engineering, Tsinghua University, China
08. Sep 21 14:30 15:00 6.9.4 HIGH-FIDELITY ANALYSIS OF ROBUST NONLINEAR 2-DOF AIRFOIL LCO CONTROL
V. Golubev, ERAU, United States
08. Sep 21 15:00 15:30 6.9.5 ANALYSIS AND CONTROL OF DYNAMIC STALL CHARACTERISTICS OF S809 AIRFOIL
L-S Hao, Northwestern Polytechnical University, China
Reserve Paper 6.9.R NUMERICAL STUDY ON HIGH-FREQUENCY RESPONSE OF WALL JETS FOR GUST LOAD CONTROL
X. C. Xue, Nanjing University of Aeronautics and Astronautics, China
Reserve Paper 6.9.R PHISICAL AND MATHEMATICAL MODELS OF THE BUFFET ONSET
A.M. Lipanov, Institute of Applied Mathematics, Russia
Reserve Paper 6.9.R ANALYSIS OF AERODYNAMIC COUPLING EFFECT IN CLOSE FORMATION FOR FLAPPING WINGS
Zhaotong Chen ¹, Zongxia Jiao¹, Yaoxing Shang¹, Longfei Zhao¹; ¹Beihang University, China
7.9Laminar Flow
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
08. Sep 21 13:00 13:30 7.9.1 BLADE - NATURAL LAMINAR FLOW FLIGHT TESTING
Tom Gibson¹, Bertrand Soucheleau¹, Nick Rogers¹; ¹Airbus, United Kingdom
08. Sep 21 13:30 14:00 7.9.2 METODICAL STUDIES OF THE POSSIBILITY TO APPLY A NUMERICAL METHOD WITH BUILT-IN EMPIRICAL CRITERIA FOR DETERMINING THE LA
N.V. Voevodenko, TsAGI, Russia
08. Sep 21 14:00 14:30 7.9.3 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
08. Sep 21 14:30 15:00 7.9.4 DESIGN OF TRANSONIC NATURAL LAMINAR FLOW NACELLE
C. Y. Yan¹, Y. F. Zhang¹, M. H. Zhang, Shanghai Aircraft Design and Research Institute, China; ¹School of Aerospace, Tsinghua University, China
08. Sep 21 15:00 15:30 7.9.5 THE NUMERICAL AND EXPERIMENTAL STUDIES ON LAMINAR WING SHORT RANGE AIRCRAFT WITH REDUCED COMMUNITY NOISE
A.L. Bolsunovsky, Central Aerohydrodynamic Institute n.a. prof. N.E.Zhukovsky (TsA, Russia
8.9Design of Aircraft Structures 1
Chair(s): Cestino, E., Alaimo, A.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
08. Sep 21 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
08. Sep 21 13:30 14:00 8.9.2 DESIGN OF EXPERIMENTS TECHNIQUES TO INVESTIGATE LOAD SHARE STRATEGIES BETWEEN AERO ENGINE, NACELLE AND POWERPLANT COMPONENTS
C.-M MARTIN , Queens University Belfast, United Kingdom
08. Sep 21 14:00 14:30 8.9.3 THERMOPLASTIC APPLICATIONS FOR AEROSTRUCTURES: TOWARDS SUSTAINABLE AND WEIGHT EFFICIENT APPLICATIONS
M. HERMAN¹, E. DUPUY¹, E. PETIOT¹, C. PARIS¹, J.-P. CABANAC¹, C. FUALDES¹, G. MASSE², M.-A. CELLI²; ¹Airbus Operations, France ;²Airbus Helicopters, France
08. Sep 21 14:30 15:00 8.9.4 RATIONAL DETERMINATION OF WING JIG SHAPE OF A LONG-RANGE AIRCRAFT WITH TRANSONIC CRUISE REGIME
A.V. Bezuevsky, TsAGI, Russia
08. Sep 21 15:00 15:30 8.9.5 AIRCRAFT ENGINE ROTOR DYNAMICS ANALYSIS AFTER FAN BLADE-OUT WITH ACCOUNT OF ROTOR-CASING CONTACT INTERACTIONS
V. Myasnikov¹, I. Ivanov¹, B. Blinnik¹; ¹CIAM, Russia
Reserve Paper 8.9.R THE METHOD OF AIRCRAFT MATHEMATICAL MODEL STIFFNESS PROPERTIES CORRECTION BASED ON EXPERIMENTAL RESEARCH RESULTS
M.A. Pronin, Central Aerohydrodynamic Institute n.a. prof. N.E.Zhukovsky, Russia
Reserve Paper 8.9.R STRUCTURAL HEALTH MONITORING OF SANDWICH STRUCTURES WITH LATTICE CORES IN AIRCRAFT DESIGN: CHALLENGES AND POTENTIAL
T. Huang, RWTH Aachen University, Germany
9.9Advanced Manufacturing
Chair(s): Rupeng, L.
Track 9
08 - Manufacturing and Supply Chain Management
08. Sep 21 13:00 13:30 9.9.1 NUMERICAL AND EXPERIMENTAL INVESTIGATION OF POST-MACHINING DISTORTION FOR LARGE AEROSPACE MONOLITHIC COMPONENTS
BS SHI, National Research Council Canada, Canada
08. Sep 21 13:30 14:00 9.9.2 RESEARCH ON THE DEVELOPMENT AND PERFORMANCE OF THE OBSTACLE-PASSING STRUCTURE OF THE CRAWLER INSPECTION ROBOT
Pu Zhang¹, Jin Sun¹; ¹Beihang University, China
08. Sep 21 14:00 14:30 9.9.3 SOFTWARE-BASED IMPROVING THE QUALITY OF HIGH-SPEED MACHINING
S. Zietarski, Military University of Technology, Poland
08. Sep 21 14:30 15:00 9.9.4 RESEARCH ON MANUFACTURING PROCESS AND MICROSTRUCTURE OF SIC/ALSI7MG COMPOSITE FABRICATED BY SELECTIVE LASER MELTING
H Zhu, China
08. Sep 21 15:00 15:30 9.9.5 EXPERIMENTAL STUDY ON PATH PLANNING OF BELT GRINDING FOR BIOMIMETIC SURFACE ON AERO-ENGINE BLADE
Chongqing Univer Xiao, China
Reserve Paper 9.9.R AUTOMATIC DETECTION TECHNOLOGYOF LARGE CIVIL AIRCRAFT BASED ON IMAGE RECOGNITION
yu liu, China
Reserve Paper 9.9.R ???????????????????????????
M.B.L ??, ????????, China
Reserve Paper 9.9.R RESEARCH ON SOLVING PROBLEM OF AIRCRAFT ASSEMBLY COORDINATION BASED ON 3D LASER SCANNING MEASUREMENT TECHNOLOGY
W J JIAN, China
10.9Nonlinear Control
Chair(s): Rogalski, T.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
08. Sep 21 13:00 13:30 10.9.1 NONLINEAR CONTROL STRATEGY FOR QUAD-TILTROTOR IN TRANSITION MODE
K.W. Jang, KAIST, South Korea
08. Sep 21 13:30 14:00 10.9.2 NONLINEAR FAULT-TOLERANT FLIGHT CONTROL WITH CONTROL ALLOCATION OF NASA GTM T-2 MODEL WITH DIFFERENT DAMAGE SCENARIOS
B. Ergocmen, Middle East Technical University, Turkey
08. Sep 21 14:00 14:30 10.9.3 MACHINE LEARNING TECHNIQUES FOR AIRCRAFT STALL DETECTION AND RECOVERY
J Gauci, University of Malta, Malta
08. Sep 21 14:30 15:00 10.9.4 AIRCRAFT AUTOPILOT DESIGN USING ASYMMETRIC VARIABLE-SPAN WING MORPHING
J. Lee, Seoul National University, South Korea
08. Sep 21 15:00 15:30 10.9.5 AUTONOMOUS FLIGHT CONTROL BASED ON NEURAL NETWORKS AND FUZZY DECISION
P.C. Wen, AVIC Xi’an Aeronautics Computing Technique Research Institute, China
Reserve Paper 10.9.R ANALYSIS OF REENTRY TRAJECTORY OPTIMIZATION OF COMPLEX PATH CONSTRAINTS USING HERMIT SPLINE INTERPOLATION
Y Kwak, Konkuk Univ., South Korea
Reserve Paper 10.9.R 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
Reserve Paper 10.9.R DEVELOPMENT OF A HUMAN PILOTED AIR COMBAT ENGAGEMENT DATABASE
Xue Tao¹, Ma JinYi¹, Wen Jiongran¹, Yang Xizhong, Science and Technology on Avionics Integration Laboratory, China; Dong Yiqun¹, Ai Jianliang¹; ¹Fudan University, China
Reserve Paper 10.9.R LEARNING-BASED MIDCOURSE GUIDANCE FOR VELOCITY MAXIMIZATION WITH ANGULAR CONSTRAINT
T. Jin¹, H. Li¹, S. He¹, Y. Li¹; ¹Beijing Institute of Technology, China
11.9Aspects of Landing Gear Design
Chair(s): Krus, P., Shang, Y.
Track 11
07 - Systems, Subsystems and Equipment
08. Sep 21 13:00 13:30 11.9.1 IMPROVED DESIGN OF AIRCRAFT NOSEWHEEL STEERING SYSTEM
L.-X. Xin, FAI AVIC, China
08. Sep 21 13:30 14:00 11.9.2 NEW SOLUTION OF A DAMPER WITH A MAGNETORHEOLOGICAL ELASTOMER
P. Skalski, Institute of Aviation, Poland
08. Sep 21 14:00 14:30 11.9.3 INVESTIGATIONS ON LANDING GEAR SHOCK ABSORBER ACTIVE FORCE CONTROL
Z. Skorupka¹, R. Harla¹; ¹?ukasiewicz Research Network - Institute of Aviation, Poland
08. Sep 21 14:30 15:00 11.9.4 A STOCHASTIC ROBUSTNESS VERIFICATION OF NLG SIMPLE ADAPTIVE SHIMMY SUPPRESSION SYSTEM
C. Orlando¹, A. Alaimo¹; ¹Università di Enna Kore, Italy
08. Sep 21 15:00 15:30 11.9.5 RESEARCH ON DESIGN OF HYDRAULIC ACCUMULATOR FOR A CIVIL AIRCRAFT BRAKE SYSTEM
G.-C Zhang, Shanghai Aircraft Design and Research Institute, China
Reserve Paper 11.9.R STUDY ON THE DYNAMIC COUPLING CHARACTERISTICS OF AIRCRAFT LOW SPEED BRAKE
ZHAO HAO, Shanghai Aircraft Design And Research Institute , China
Reserve Paper 11.9.R A NOVEL OF CONTROL METHOD BASED ON PWM FOR HIGH_SPEED ON/OFF VALVES ARRAY OF AIRCRAFT BRAKE SYSTEMS
Renjie Li Li, Beihang unversity, China
12.9Air Traffic Efficiency
Chair(s): Nguyen, D.
Track 12
09 - Air Transport System Efficiency
08. Sep 21 13:00 13:30 12.9.1 IMPACT OF ENROUTE TIME-BASED METERING ON EQUITY IN DELAY DISTRIBUTION
Adriana Andreeva-Mori¹, Yoshinori Matsuno¹; ¹Japan Aerospace Exploration Agency, Japan
08. Sep 21 13:30 14:00 12.9.2 COGNITIVE HUMAN-MACHINE INTERFACES FOR ENROUTE AIR TRAFFIC FLOW MANAGEMENT
P Lertworawanich¹, N Pongsakornsathien¹, A Gardi¹, R Sabatini¹; ¹RMIT University, Australia
08. Sep 21 14:00 14:30 12.9.3 RESEARCH ON TRAJECTORY OPTIMIZATION TECHNOLOGY CONSIDERING METEOROLOGICAL INFORMATION PREDICTION
G.-W Guo, China National Aeronautical Radio Electronics Research Institute, China
08. Sep 21 14:30 15:00 12.9.4 QUANTITATIVE ANALYSIS OF PMS AND ARRIVAL METERING SYNERGY EFFECT ON INBOUND FLIGHTS AT TOKYO INTERNATIONAL AIRPORT
Toshinori Mori, Osaka Prefecture University, Japan
13.9Fan / Nacelle & Propeller
Chair(s): Pankov, S.
Track 13
05 - Propulsion
08. Sep 21 13:00 13:30 13.9.1 GEARED FANS AND VARIABLE PITCH FANS - NUMERICAL AND EXPERIMENTAL INVESTIGATIONS OF THEIR AERODYNAMICS
S.V. Pankov, Central Institute of Aviation Motors (CIAM), Russia
08. Sep 21 13:30 14:00 13.9.2 ANALYSIS OF AERODYNAMIC CHARACTERISTICS OF PROPELLERS AT LOW ADVANCE RATIO USING A WHIRLING ARM
Y. Itoh¹, A. Satoh¹; ¹Iwate university, Japan
08. Sep 21 14:00 14:30 13.9.3 EXPERIMENTAL STUDIES OF SLOT-TYPE CASING TREATMENTS FOR MODEL FANS WITH THE AIM OF AERODYNAMIC AND ACOUSTIC IMPROVEMENTS
V.I. Mileshin, Central Institute of Aviation Motors, Russia
08. Sep 21 14:30 15:00 13.9.4 ANALYSIS OF THRUST-SCALED PROPELLER NOISE AND ITS TRADE-OFF WITH PROPELLER EFFICIENCY
X. Geng¹, T. Hu¹, P. Liu¹, T Sinnige², G. Eitelberg²; ¹Beihang University, China ;²Delft University of Technology, Netherlands
08. Sep 21 15:00 15:30 13.9.5 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
Reserve Paper 13.9.R 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
Reserve Paper 13.9.R STUDY OF NON-ROTATING MICROPHONE ARRAY FOR SPINNING DUCT MODE DETECTION
Y. Jiyong, AECC Commercial Aircraft Engine Co., Ltd., China

15:30 - 16:00Break

0.6General Lecture 3 - Trends in Aircraft Propulsion: Reflections on ISABE, Ric Parker, President ISABE
Chair:
08. Sep 21 16:00 17:00

0.7General Lecture 4 - Virtual Aircraft Technology Integration Platform - Results of DLR\'s Project VicToria, Björn Nagel, DLR
Chair:
08. Sep 21 17:00 18:00

Thursday, 09. Sep 2021

7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
1.10Hybrid/Electric & Unconventional Aircraft 4
Chair(s): Melkert, J.
Track 1
01 - Aircraft Design and Integrated Systems
09. Sep 21 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
09. Sep 21 08:30 09:00 1.10.2 CIRCULATION CONTROL AIRCRAFT: RECENT DEVELOPMENTS OF THE CHANNEL-WING DESIGN
Harijono Djojodihardjo, Retired Professor, Indonesia; M.Arif Andira¹, Ratih Julistina¹, M.Agoes Moeljadi, Institut Teknologi Bandung, Indonesia; ¹CCIT Group Indonesia, Indonesia
09. Sep 21 09:00 09:30 1.10.3 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
2.1010 years of IFAR
Chair(s): ,
Track 2
15 - Guest lectures
09. Sep 21 08:00 08:30 2.10.1 IFAR (INTERNATIONAL FORUM FOR AVIATION RESEARCH) INFRASTRUCTURE DATABASE
Dany Paraschivoiu, NRC, Canada
09. Sep 21 08:30 09:00 2.10.2 SOL-GEL BASED ORGANIC-INORGANIC HYBRID COATINGS FOR CORROSION PROTECTION OF AEROSPACE ALUMINIUM ALLOY
R.V. Lakshmi, India
3.10Compressor and Fan Aerodynamics
Chair(s): Wan, T., Tomita, J.
Track 3
03.1 - Aerodynamics - CFD Methods and Validation
09. Sep 21 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
09. Sep 21 08:30 09:00 3.10.2 DISTORTION PLATE DESIGN, SIMULATION VALIDATION AND TEST SCHEME FOR STABILITY ANALYSIS ON A FAN COMPONENT OF AEROENGINE
Zhi-peng:Z.-P Li, AECC Shenyang Engine Research Institute, China
09. Sep 21 09:00 09:30 3.10.3 EFFECT OF INTER-STAGE BLEEDING ON FLOW STABILITY OF A MULTI-STAGE COMPRESSOR
Hailiang JIN, China; Daobin QIU, China; Yueqian YIN, China
Reserve Paper 3.10.R DESIGN AND TEST OF A HIGH SLOPE ANGLE INTERMEDIATE DUCT BETWEEN AN AXIAL-CENTRIFUGAL LOW PRESSURE AND HIGH PRESSURE COMP
H.-L. Jin, China; J. Zhang, China; J.-F. Wu, China; D. -B. Qiu, China; Y.-Q. Yin, China
Reserve Paper 3.10.R 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
4.10Numerical Methods 2
Chair(s): Viviani, A., Obayashi, S.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
09. Sep 21 08:00 08:30 4.10.1 AERODYNAMIC AND AEROACOUSTIC INVESTIGATION OF THE FLOW PAST THE 30P30N HIGH-LIFT MULTI-AIRFOIL
Yao Jin Jin, China
09. Sep 21 08:30 09:00 4.10.2 AN INTELLIGENT STRUCTURED CHIMERA GRID APPROACH FOR MOVING OBJECTIVES
L. L. Li, AVIC Aeronautics Computing Technique Research Institute, China
09. Sep 21 09:00 09:30 4.10.3 SUN CODE: AN AUTOMATIC AND FAST FLOW SIMULATION TOOL FOR AIRCRAFT AERODYNAMIC DESIGN
Mingzhe Sun¹, Rongting Lin¹, Dongrun Wu¹, Jender Lee¹, Xi Du¹, Dakai Lin¹; ¹COMAC BATRI, China
Reserve Paper 4.10.R INVESTIGATION OF NUMERICAL METHOD OF INTERNAL FLOW AND OIL CAPTURE EFFICIENCY OF UNDER-RACE LUBRICATION
J.-L. Jiang, Northwestern Polytechnical University, China
5.10Rotating Wings
Chair(s): Gowree, E., Rasuo, B.
Track 5
03.2 - Experimental Aerodynamics
09. Sep 21 08:00 08:30 5.10.1 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
09. Sep 21 08:30 09:00 5.10.2 INVESTIGATION OF THE CHARACTERISTICS OF THE HELICOPTER MAIN ROTOR WITH ELASTIC MOUNTING BLADES
O.-E. Kirillov, Central Aerohydrodynamic Institute (TsAGI), Russia
09. Sep 21 09:00 09:30 5.10.3 EXPERIMENTAL MEASUREMENTS ON BIOMIMETIC WIND TURBINE BLADES BY P. TOMENTOSA SEED
L.-P Paiva, UFU, Brazil
Reserve Paper 5.10.R EXPERIMENTAL INVESTIGATION OF PULSATION OF THE ROTOR SLIPSTREAM ACTING ON AN ELEVATED HELIPORT
P. Ruchala, Institute of Aviation, Poland
6.10System Qualification
Chair(s): Fu, J., Peters, M.
Track 6
07 - Systems, Subsystems and Equipment
09. Sep 21 08:00 08:30 6.10.1 RESEARCH ON CIVIL AIRCRAFT EQUIPMENT QUALIFICATION TEST
G.-C Zhang, Shanghai Aircraft Design and Research Institute, China
09. Sep 21 08:30 09:00 6.10.2 RESEARCH ON THE ENVIRONMENTAL WORTHINESS OF THE CIVIL AIRCRAFT USING THE FUZZY THEORY WITH THE TEST RESULT
Z-H hui, Aircraft Strength Institute Research, China
09. Sep 21 09:00 09:30 6.10.3 AN EXPERIMENTAL AND NUMERICAL METHODOLOGY TO MODEL THE SHEDDING OF ICE ACCRETED TO ICEPHOBIC COATINGS
MH Huré, IRT Saint Exupery, France
Reserve Paper 6.10.R EXPERIMENTAL STUDY OF THE DYNAMIC CHARACTERISTICS OF AN IMPACT WATER DROPLET ON SUPERHYDROPHOBIC SURFACE
Jingxin Wang¹, Chunling Zhu¹, Zaili Yang¹, Chengxiang Zhu, Nanjing University of Aeronautics and Astronautics,, China; ¹Nanjing University of Aeronautics and Astronautics, China
7.10Stability
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
09. Sep 21 08:00 08:30 7.10.1 NUMERICAL EVALUATION OF DYNAMIC STABILITY DERIVATIVES FOR HIGH LIFT DEVICES
Hamood Ur Rahman¹, Adnan Maqsood¹, Rizwan Riaz¹, Laurent Dala, Northumbria University, United Kingdom; ¹National University of Sciences & Technology, Pakistan
09. Sep 21 08:30 09:00 7.10.2 THE AERODYNAMIC OPTIMIZATION AND TRIM CHARACTERISTICS RESEARCH ON VARIABLE CAMBER WING OF WIDEBODY CIVIL TRANSPORT
Cheng Su¹, Xuan Hao¹, Bin Wang¹, Qingqing Zhang¹; ¹China Academy of Aerospace Aerodynamics, China
09. Sep 21 09:00 09:30 7.10.3 EFFECT OF CANARD DEFLECTION ON MAIN WING FOR A CLOSE-COUPLED-CANARD CONFIGURATION DURING PITCHING OSCILLATIONS
Q. Chen, Beihang University, China
Reserve Paper 7.10.R DESIGN OF VORTEX GENERATORS OF HYBRID SIZES OF AN AIRCRAFT HORIZONTAL TAIL
Y. Liu¹, L. Ping¹, R. Zeng¹; ¹CETC Wuhu Diamond Aircraft Manufacture co., LTD, China
Reserve Paper 7.10.R 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
Reserve Paper 7.10.R NASA-CRM LATERAL-DIRECTIONAL STABILITY DERIVATIVES COMPARISON BETWEEN SEMI-EMPIRICAL, VORTEX LATTICE AND PANEL METHOD
Roberto Gil Annes da Silva, Instituto Tecnologico de Aeronautica, Brazil
8.10Static Analysis of Aircraft Structures
Chair(s): Zheng, J., Zappino, E.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
09. Sep 21 08:00 08:30 8.10.1 MULTIDIMENSIONAL FINITE ELEMENT MODELS FOR ADVANCED HELICOPTER BLADES
M. Filippi, Politecnico di Torino, Italy
09. Sep 21 08:30 09:00 8.10.2 MATHEMATICAL MODELS FOR OPTIMIZATION OF AIRCRAFT STRUCTURES TAKING INTO CONSIDERATION OF LOCAL STRESS DISTRIBUTION
V.V. Chedrik¹, S.A. Tuktarov¹, K.A. Balunov¹, V.N. Nguen, Moscow Institute of Physics and Technology, Russia; ¹Central Aerohydrodynamic Institute, Russia
09. Sep 21 09:00 09:30 8.10.3 THE BEAM MODEL OF A HAWKMOTH WING STRUCTURE
A. T. Nguyen, Le Quy Don Technical University, Vietnam
Reserve Paper 8.10.R INVESTIGATION ON PERFORMANCE OF PCM-BASED ORTHOTROPIC COOLING PLATE FOR THERMAL MANAGEMENT OF AVIONICS MODULE.
B. Wu, Aeronautical Computing Technique Research Institute, China
Reserve Paper 8.10.R A METHOD FOR CALCULATING TORSION ANGLE OF FLEXIBLE RETICULAR TUBE AT DIFFERENT POSITIONS
DENG Yangchen, SADRI, China; YANG Yu, ASRI, China; HE Yuqing, SIA, China; SUN Cong, CAE, China; QIU Fusheng, SAU, China
Reserve Paper 8.10.R SPECIALIZED SOFTWARE DEVELOPMENT FOR BUILDING BLOCK APPROACH INTEGRATION IN FULL-SCALE STATIC TESTS
D. V. Kurulyuk¹, E. M. Kolman¹, E. A. Levchenko¹, M. V. Limonin¹; ¹Central Aerohydrodynamic Institute named after N.E. Zhukovsky, Russia
9.10ISABE 2
Chair(s): ,
Track 9
15 - Guest lectures
09. Sep 21 08:00 08:30 9.10.1 KEY TECHNOLOGIES FOR THE NEXT GENERATION OF CIVIL AIRCRAFT ENGINES
F. Haselbach, United Kingdom
09. Sep 21 08:30 09:00 9.10.2 DESIGN AND PERFORMANCE OF A LOW FAN-PRESSURE-RATIO PROPULSION SYSTEM
R. Schnell, German Aerospace Center (DLR), Germany; E. Goldhahn, Airbus Operations GmbH, Germany; M. Julian, Airbus Operations SAS, France
09. Sep 21 09:00 09:30 9.10.3 AN EXPERIMENTAL-NUMERICAL METHOD FOR TRANSIENT INFRARED MEASUREMENT OF FILM COOLING EFFECTIVENESS
N.E. Holgate, United Kingdom
10.10Helicopter Control
Chair(s): Che, J.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
09. Sep 21 08:00 08:30 10.10.1 MODELING OF HELICOPTER FLIGHT DYNAMICS AND ROTOR BLADES LOADS DURING EXTREME FLIGHTS
Grzegorz Kowalec Kowaleczko, Air Force Institute of Technology, Poland
09. Sep 21 08:30 09:00 10.10.2 DESIGN TECHNIQUE OF INTEGRAL ALGORITHMS FOR HELICOPTER FBW CONTROL SYSTEM
V. M. Kuvshinov¹, A. Yu. Voronin¹; ¹TsAGI, Russia
09. Sep 21 09:00 09:30 10.10.3 AERODYNAMIC PERFORMANCE CALCULATION OF XH-59A HELICOPTER IN MANEUVERING PROCESS
K. Y. You, Northwestern Polytechnical University, China
11.10Vehicle Mangement Systems
Chair(s): Krus, P., Viola, N.
Track 11
07 - Systems, Subsystems and Equipment
09. Sep 21 08:00 08:30 11.10.1 EVALUATION OF A GESTURE-BASED PILOT-AIRCRAFT INTERFACE IN A SIMULATION ENVIRONMENT
M.A. Rodriguez Diaz, Instituto Tecnologico de Aeronáutica, Brazil
09. Sep 21 08:30 09:00 11.10.2 ANALYSIS AND SOLUTION RESEARCH OF THE AIR DATA LOSS FROM AIRCRAFT FOR ENGINE CONTROL
LI JING, COMAC Sadri, China
09. Sep 21 09:00 09:30 11.10.3 REAL-TIME GNSS PRECISE POINT POSITIONING AND VISUAL-INERTIAL ODOMETRY COUPLED NAVIGATION SYSTEM FOR UAVS
C.-C. Cheng, SJTU, China
Reserve Paper 11.10.R DESIGN OF UAV NAVIGATION ALGORITHM IN SINGLE SATELLITE ENVIRONMENT BASED ON HIGH PRECISION TIMING
Li Ketao¹, Ma Hangshuai¹, Wang Dan¹; ¹China National Aeronautical Radio Electronics Research Institute, China
12.10UTM/On-Demand Mobility
Chair(s): ,
Track 12
09 - Air Transport System Efficiency
09. Sep 21 08:00 08:30 12.10.1 ON-DEMAND AIR MOBILITY FOR BEIJING: PREREQUISITES FOR COMPETITIVENESS
X. Sun, Beihang University, China
09. Sep 21 08:30 09:00 12.10.2 AIRLINE NETWORK-AIRPLANE INTEGRATED OPTIMIZATION CONSIDERING MANUFACTURER\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\\'S PROGRAM COST
J. A. Fregnani, Airbus, Brazil; B. S. Mattos¹, J. A. Hernandes¹; ¹ITA, Brazil
09. Sep 21 09:00 09:30 12.10.3 AIR TRAFFIC MANAGEMENT OF DRONES INTEGRATED INTO SMART CITIES
D. Rohacs, B udapest University of Tech. and econ.;, Hungary
Reserve Paper 12.10.R VERTIPORT PLACEMENT METHOD BASED ON MOBILITY SURVEY DATA
K Lippoldt, Technische Universität München, Germany
Reserve Paper 12.10.R ASSESSING THE ENVIRONMENTAL IMPACT OF AIRCRAFT TAXIING TECHNOLOGIES AND STRATEGIES
Robert Camilleri¹, Aman Batra¹; ¹Institute of Aerospace Technologies, University of Malta, Malta
13.10Operational Training
Chair(s): Holmes, D., Ren, H.
Track 13
11 - Operations and Sustainment
09. Sep 21 08:00 08:30 13.10.1 DESIGN OF SIMULATION-BASED PILOT TRAINING SYSTEMS USING MACHINE LEARNING AGENTS
J. Källström¹, R. Granlund, RISE SICS East, Sweden; F. Heintz¹; ¹Linköping University, Sweden
09. Sep 21 08:30 09:00 13.10.2 A STUDY ON TRAINING NEEDS ANALYSIS (TNA) METHOD FOR MILITARY AIRCRAFT
QIN WANG¹, CHEN SUN¹, BING HAO¹; ¹ Chengdu Aircraft Design and Research Institute, AVIC, China
09. Sep 21 09:00 09:30 13.10.3 COMPARISON OF READINESS TO PERFORM THE TASK OF AIRCRAFT USED FOR CADET TRAINING
J. Tomaszewska, Polish Air Force University, Poland
Reserve Paper 13.10.R 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

09:30 - 10:00Break

1.11Wing Design
Chair(s): Rinoie, K.
Track 1
01 - Aircraft Design and Integrated Systems
09. Sep 21 10:00 10:30 1.11.1 A HIERARCHICAL STRUCTURAL MODEL FOR CONCEPTUAL DESIGN OF TRANSPORT AIRCRAFT WING
Y.K. Yin¹, W.B. Song¹; ¹Shanghai Jiao Tong University, China
09. Sep 21 10:30 11:00 1.11.2 VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WING
Gang Song¹, Wenyuan Cheng¹, Yu Yang², Wenjie Ge³, Yonghong Zhang³, Zhigang Wang², Sheng Zhang², Xintong Shi²; ¹Aviation Industry Development Research Center of China, China ;²Aircraft strength research Institute of China, China ;³Northwestern Polytechnical University, China
09. Sep 21 11:00 11:30 1.11.3 EVALUATION AND VALIDATION OF AEROELASTIC ANALYSIS PROGRAM FOR AEROSTRUCT WING OPTIMIZATION PLATFORM
Sheng-bo Ling¹, Ke-shi Zhang, Northwestern polytechnical university, China; Zhong-hua Han¹, Zhong-jian Gao, Xiantianjihangtong Technology CO. Ltd., China; ¹Northwestern Polytechnical university, China
09. Sep 21 11:30 12:00 1.11.4 ON WINGS WITH NON-ELLIPTIC LIFT DISTRIBUTIONS
E. Bragado Aldana¹, M. M. Lone¹, A Riaz¹; ¹Cranfield University, United Kingdom
09. Sep 21 12:00 12:30 1.11.5 ON THE FLIGHT MECHANICS OF A TRANSPORT AIRCRAFT FITTED WITH FLARED-HINGE FOLDING WINGTIPS
R Ajaj, Khalifa University, United Arab Emirates
Reserve Paper 1.11.R UNCERTAINTY ANALYSIS OF HYBRID LAMINAR FLOW CONTROL WINGS FOR WING-GLOVE FLIGHT TESTS
T.Y. Yang, Northwestern Polytechnical University, China
2.11Design Methods
Chair(s): Cestino, E.
Track 2
01 - Aircraft Design and Integrated Systems
09. Sep 21 10:00 10:30 2.11.1 IMPACT OF NEW TECHNOLOGIES ON AIRCRAFT SYSTEMS
Philipp Niemeyer, DLR, Germany
09. Sep 21 10:30 11:00 2.11.2 LAMBDA: A KNOWLEDGE-BASED MODULAR, MULTIFIDELITY AND MULTIDISCIPLINARY AIRCRAFT CONCEPTUAL DESIGN ENVIRONMENT
S. Hosseini, Amirkabir University of Technology, Iran
09. Sep 21 11:00 11:30 2.11.3 FAST METHOD AND 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
09. Sep 21 11:30 12:00 2.11.4 LOW SWEEP LAMINAR FLOW WING AT TRANSONIC SPEED
N. Qin, The University of Sheffield, United Kingdom
09. Sep 21 12:00 12:30 2.11.5 AERODYNAMIC DESIGN OPTIMIZATION OF WAVERIDER-DERIVED VEHICLE
S.W. Wei, Beijing Institute of Space Long March Vehicle, China
Reserve Paper 2.11.R INTEGRATION OF FUSELAGE-MOUNTED OVER-WING ENGINES ON A MID-RANGE AIRCRAFT
P. Wegener, DLR - German Aerospace Center, Germany
3.11Transition
Chair(s): Alves, L., Antunes, A.
Track 3
03.1 - Aerodynamics - CFD Methods and Validation
09. Sep 21 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
09. Sep 21 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
09. Sep 21 11:00 11:30 3.11.3 AERODYNAMICS CHARACTERISTICS STUDY ON A NATURE LAMINAR FLOW AIRFOIL OF NEAR-SPACE VEHICLE AT LOW REYNOLDS NUMBERS
Cui Fei, China; Zhang Hongkun, China
09. Sep 21 11:30 12:00 3.11.4 EFFECT OF THE WALL PROPERTIES ON THE SHOCK WAVE / LAMINAR BOUNDARY LAYER INTERACTION
A. Kutepova, Khristianovich Institute of Theoretical and Applied Mechanics, Russia
09. Sep 21 12:00 12:30 3.11.5 INFLUENCE OF RAREFACTION FAN ON RECEPTIVITY OF SUPERSONIC BOUNDARY LAYER TO FREE STREAM ACOUSTIC DISTURBANCES
N.V. Palchekovskaya, Moscow Institute of Physics and Technology, Russia
Reserve Paper 3.11.R HYBRID NUMERICAL SCHEMES IN PREDICTION OF HIGH-SPEED LAMINAR-TURBULENT TRANSITION
I. Egorov, TsAGI, Russia
Reserve Paper 3.11.R A LOCAL CORRELATION-BASED ALGEBRAIC TRANSITION MODEL WITH COMPRESSIBILITY AND CROSS-FLOW CORRECTION
R. X. Xie¹, W. M. Sang¹; ¹Northwestern Polytechnical University, China
4.11Numerical Methods 3
Chair(s): Viviani, A., Wang, Z.J.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
09. Sep 21 10:00 10:30 4.11.1 MODELING AND SIMULATION OF DUSTY GAS FLOW IN AERODYNAMICS
Yu.M. Tsirkunov¹, D.A. Romanyuk¹, S.V. Panfilov¹; ¹Baltic State Technical University, Russia
09. Sep 21 10:30 11:00 4.11.2 STUDY ON AN IMPROVED PRECONDITIONING METHOD FOR MIXED COMPRESSIBLE AND INCOMPRESSIBLE FLOW
Huan Li, Computational Aerodynamics Institute,CARDC , China; Bin Li ¹, Hongyin Jia¹, Pengcheng Cui¹, Xiaojun Wu¹, Mingsheng Ma¹; ¹Computational Aerodynamics Institute,CARDC, China
09. Sep 21 11:00 11:30 4.11.3 STUDY OF UNSTEADY NUMERICAL SIMULATIONS BASED ON UNSTRUCTURED MESH DEFORMATION TECHNIQUE
H.-Y. Liu, China
09. Sep 21 11:30 12:00 4.11.4 2D INCOMPRESSIBLE FLOW SOLVER IN VELOCITY-VORTICITY FORMULATION USING DC-PSE OPERATOR DISCRETIZATION
L. R. Zuhal¹, T. S. Sugandi¹, A. Pristiansyah¹, A. J. Sepnov¹; ¹Institut Teknologi Bandung, Indonesia
09. Sep 21 12:00 12:30 4.11.5 ON THE POSSIBILITY OF APPLYING THE HYPERSONIC SMALL-DISTURBANCE THEORY IN AERODYNAMIC STUDIES OF HIGH-SPEED AIRCRAFT
A.A. Gubanov, Central Aerohydrodynamic Institute n.a. Prof. N.E. Zhukovsky, Russia
5.11Transonic/Supersonic
Chair(s): Prince, S., Dehua, C.
Track 5
03.2 - Experimental Aerodynamics
09. Sep 21 10:00 10:30 5.11.1 NEW INVESTIGATION METHOD OF THE SHOCK WAVE/BOUNDARY LAYER INTERACTION PATTERN AT TRANSONIC SPEEDS
M.A. Brutyan, TsAGI, Russia
09. Sep 21 10:30 11:00 5.11.2 INFLUENCE OF VARIABLE WALL PERFORATION RATIO ON BOUNDARY LAYER PARAMETERS AT TRANSONIC SPEEDS
S. Osipova, Russia
09. Sep 21 11:00 11:30 5.11.3 RESEARCH OF HYBRID LAMINAR FLOW CONTROL TECHNOLOGY FOR CIVIL AIRCRAFT WING
C. Shao, Shanghai Aircraft Design and Research Institute, COMAC, China
09. Sep 21 11:30 12:00 5.11.4 STUDY OF SHOCK WAVE / LAMINAR BOUNDARY LAYER INTERACTION AREA BY PIV TECHNIQUE
Oleg: O. Vishnyakov, Khristianovich Institute of Theoretical and Applied Mechanics SB, Russia
09. Sep 21 12:00 12:30 5.11.5 DEVELOPMENT OF THE MODEL NEAR-FIELD STUDY TECHNIQUES INTHE SUPERSONIC WIND TUNNELS AIMED AT THE SONIC BOOM PREDICTION
A.I. IVANOV, TSAGI, Russia
Reserve Paper 5.11.R THE EXPERIMENTAL INVESTIGATION OF THE THROTTLING SECOND THROAT INFLUENCE ON TRANSONIC WIND TUNNEL FLOW QUALITY
Z HaiYang, China Aerodynamics Research and Development Center, Facility des, China
6.11Design of Aircraft Strutcures 2
Chair(s): ,
Track 6
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
09. Sep 21 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
09. Sep 21 10:30 11:00 6.11.2 ON THE DEVELOPMENT OF FUSELAGE WEIGHT ESTIMATION TOOL INTO AIRCRAFT MULTIDISCIPLINARY DESIGN ENVIRONMENT
Haiqiang Wang¹, Huaiyuan Wang¹; ¹Shanghai Aircraft Design and Research Institute, China
09. Sep 21 11:00 11:30 6.11.3 AN INTEGRATED AERODYNAMIC/THERMAL/STRUCTURAL DESIGN FRAMEWORK FOR HYPERSONIC VEHICLES
Chang Li¹, Zhiqiang Wan¹, Xiaozhe Wang¹; ¹Beihang University, China
09. Sep 21 11:30 12:00 6.11.4 A DYNAMIC SELF-CONTROL ERR STRATEGY FOR BI-DIRECTIONAL EVOLUTIONARY STRUCTURAL OPTIMIZATION
Hui Zhang¹, Qiliang Zhang¹; ¹Sun Yat-sen University, China
09. Sep 21 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 Gilli¹; ¹Politecnico di Torino, Italy, Italy
7.11Optimization 2
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
09. Sep 21 10:00 10:30 7.11.1 SPARSE POLYNOMIAL CHAOS EXPANSION BASED ON FULLY ADAPTIVE FORWARD-BACKWARD SELECTION METHOD
H. Zhao, Northwestern Polytechnical University, China
09. Sep 21 10:30 11:00 7.11.2 ON IMPROVING GRADIENT-ENHANCED KRIGING MODEL FOR AERODYNAMIC DESIGN OPTIMIZATION
H.-D. Dang¹, Z.-H. Han¹, C.-Z. Xu¹, K.-S. Zhang¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China
09. Sep 21 11:00 11:30 7.11.3 FAR-FIELD WAVEFORM DESIGN OPTIMIZATION BASED ON SONIC BOOM NOISE LEVEL
J.-L. Qiao, Northwestern Polytechnical University, China
09. Sep 21 11:30 12:00 7.11.4 RAPID THEORETICAL EVALUATION OF FORMATION FLIGHT PERFORMANCE
Rodrigo Vilumberales¹, Mudassir Lone¹; ¹Cranfield University, United Kingdom
09. Sep 21 12:00 12:30 7.11.5 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
Reserve Paper 7.11.R AERODYNAMIC EVALUATION OF FORWARD-SWEPT AND SWEPTBACK WING WITH OPTIMIZED PLANEFORMS
Sei-ichiro Morizawa, National Institute of Technology, Okinawa College, Japan
Reserve Paper 7.11.R AERODYNAMIC DESIGN OPTIMIZATION OF WAVERIDER-DERIVED VEHICLE
W. Su, Beijing Institute of Space Long March Vehicle, China
Reserve Paper 7.11.R APPLICATION OF TRANSFER LEARNING AND DEEP REINFORCEMENT LEARNING IN OPTIMIZATION OF HIGH-LIFT DEVICES
Jia-Hua Dai¹, Pei-Qing Liu¹, Qiu-Lin Qu¹, Tong-Zhi Niu, Huazhong University of Technology and Science, China; ¹Beihang University, China
8.11Failure Analysis and Fatigue
Chair(s): Symonov, V., Shanygin, A.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
09. Sep 21 10:00 10:30 8.11.1 METHODS TO CALCULATE THE STRUCTURE FATIGUE DAMAGE UNDER VARIOUS SPECTRA OF VIBRO-ACOUSTIC LOADS
P. Bessonov¹, Y. Svirsky¹, I. Sidorov¹, S. Dubinskii¹; ¹TsAGI, Russia
09. Sep 21 10:30 11:00 8.11.2 FAILURE PROPERTIES AND MACROSCOPIC MODELLING OF AERONAUTIC RIVETED CONNECTIONS
ZY Yifan, Civil Aviation University of China, China
09. Sep 21 11:00 11:30 8.11.3 ITERATIVE GLOBAL/LOCAL NON-INTRUSIVE MODEL COUPLING METHOD FOR STRUCTURE FAILURE ANALYSIS
Y.J. LIU, AVIC THE FIRST AIRCRAFT INSTITUTE, China
09. Sep 21 11:30 12:00 8.11.4 NUMERICAL ANALYSIS AND COMPARISON WITH RESULTS OF FRACTURE TESTS OF LUG MANUFACTURED IN COMPOSITE MATERIAL
G. C. Fonseca, Embraer - Minas Gerais, Brazil
09. Sep 21 12:00 12:30 8.11.5 EFFECT OF CENTER HOLE ON SHEAR STABILITY AND BEARING CAPACITY OF SHEET METAL FORMING PLATE
W.L. LI, AVIC Shengyang Aircraft Design & Research Institute, China
9.11Combustion & Heat Transfer
Chair(s): Steczycki, P.
Track 9
05 - Propulsion
09. Sep 21 10:00 10:30 9.11.1 STUDY ON OPTIMIZATION OF SPRAY CONE ANGLE OF THE COMBINED ATOMIZER BY SIMULATION AND EXPERIMENT
C. Q. Cheng Cheng, Beijing Precision Engineering Institute For Aircraft Industr, China
09. Sep 21 10:30 11:00 9.11.2 INVESTIGATION OF MEASUREMENT CHARACTERISTICS OF PROPAGATING FLAME BY MULTIPLE-ION-PROBE METHOD
T.Y. Yatsufusa, Hiroshima Institute of Technology, Japan
09. Sep 21 11:00 11:30 9.11.3 STUDY ON THE INFLUENCE OF A NEW GLIDING ARC PLASMA ACTUATOR ON THE PERFORMANCE IN AN AERO-ENGINE COMBUSTION CHAMBER
Y CHEN, Air Force Engineering University, China
09. Sep 21 11:30 12:00 9.11.4 METHODS OF CHOOSING THE PARAMETERS AND DESIGN OF THE HEAT EXCHANGERS OF AVIATION GAS TURBINE ENGINES (GTE)
A. Revanth Reddy, Moscow Aviation Institute (National Research University), Russia
09. Sep 21 12:00 12:30 9.11.5 HYBRID KERNEL FORMATION AND TRACKING METHOD TO PREDICT IGNITION LIMITS ON LOW EMISSION COMBUSTORS
Wei Xiao, AECC Hunan Aviation Powerplant Research Institute, China; Yajun Cheng, HUNAN MECHANICAL & ELECTRICAL POLYTECHNIC, China; Ke Wang, Aero Engine Academy of China (AECC), China; Zhuyin Ren, Tsinghua University, China
Reserve Paper 9.11.R NONLINEAR DYNAMICS MEASUREMENT OF SELF-SUSTAINED THERMOACOUSTIC INSTABILITIES IN A PREMIXED SWIRLING COMBUSTOR
D. Zhao, University of Canterbury, New Zealand
Reserve Paper 9.11.R ATOMIZATION OF COAXIAL SWIRLING LIQUID SHEETS USING TRANSFORMING ALGORITHM
Xiaoqiang Sun¹, Fuzhen Chen¹, Hong Yan¹; ¹Northwestern Polytechnical University, China
10.11Flight Dynamics
Chair(s): Götzendorf Grabowski, T.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
09. Sep 21 10:00 10:30 10.11.1 VIRTUAL FLIGHT TEST OF A BWB AIRCRAFT IN LOW SPEED WIND TUNNEL
Bowen NIE¹, Fei CEN¹, Zhitao LIU¹, Tianhao GUO¹, Haisheng SUN¹; ¹China Aerodynamics Research and Development Center, China
09. Sep 21 10:30 11:00 10.11.2 INVESTIGATION INTO FLIGHT DYNAMICS OF A BLENDED-WING-BODY AIRCRAFT
F. CEN, China; Y. JIANG, China; B.-W. NIE, China; Z.-T. LIU, China; L. ZHANG, China
09. Sep 21 11:00 11:30 10.11.3 BAYESIAN APPROACH TO SIMULTANEOUS STATIC AND DYNAMIC FLIGHT CHARACTERISTICS MODELING
M. Naruoka, JAXA, Japan
09. Sep 21 11:30 12:00 10.11.4 THE ANALYSIS OF TAKEOFF ROTATION OF SUBSCALE FREE-FLIGHT TESTS
K.-M. MA, Xi’an Aircraft Design Institute, China
09. Sep 21 12:00 12:30 10.11.5 ESTIMATION OF WIND BY ESTIMATING DERIVATIVES OF A LATERAL-DIRECTIONAL MOTION MODEL
L. H. Son¹, Y. Ochi¹; ¹National Defense Academy, Japan
Reserve Paper 10.11.R SEPARATE IDENTIFICATION OF AIRCRAFT THRUST AND DRAG FORCES THROUGH FLIGHT TEST DATA
O. N. Korsun, Moscow Aviation Institute (National Research University), Russia
Reserve Paper 10.11.R ANALYTICAL MODELLING OF A HOVERABLE X-SHAPE FLAPPING WING AIRCRAFT CONSIDERING WING-TAIL INTERACTION
Longfei Zhao, Beihang University, Research Institute for Frontier Science, China; Wenshuo Wang, Beihang University, School of Automation Science and Electrical , China; Yuxin Chen, Beihang University, School of Aeronautic Science and Engineering, China; Zongxia Jiao, Beihang University, Ningbo Institute of Technology, China
Reserve Paper 10.11.R MODELING AND CONTROL OF A HOVERABLE FLAPPING WING AIRCRAFT CONSIDERING FLAPPING WING INDUCED FLOW
Liang Wang¹, Longfei Zhao¹, Wuyao Jiang¹, Zongxia Jiao¹; ¹Beihang University, China
Reserve Paper 10.11.R DEVELOPMENT OF A DEEP NEURAL NETWORK-BASED FAULT DETECTION SCHEME FOR AIRCRAFT AIR DATA SENSORS
Y.Q.-D. Dong, Department of Aeronautics and Astronautics, Fudan University, China
11.11Actuator design & Analysis
Chair(s): Mare, J., Fu, Y.
Track 11
07 - Systems, Subsystems and Equipment
09. Sep 21 10:00 10:30 11.11.1 LIEBHERR-AEROSPACE EHA TECHNOLOGY FOR FUTURE FLIGHT CONTROL APPLICATION
T. Röben, Liebherr-Aerospace, Germany
09. Sep 21 10:30 11:00 11.11.2 THE DEVELOPMENT OF ALGORITHMS FOR EMA FAULT EARLY DETECTION SYSTEM
S.G. Bazhenov¹, G.S. Veresnikov, Institute of Control Science of Russian Academy of Science, Russia; A.V. Skryabin¹; ¹Central Aerohydrodynamic Institute of Russia, Russia
09. Sep 21 11:00 11:30 11.11.3 CONCEPTUAL STUDY OF THE DIGITAL HYDRAULIC ACTUATOR WITH PROPORTIONAL CONTROL FOR FLIGHT CONTROL ACTUATION SYSTEMS
Alessandro Dell'Amico, Saab AB/Linköping University, Sweden; Felix Larsson¹, Christian Johansson¹, Victor De Negri, Federal University of Santa Catarina, Brazil; Petter Krus, Linköping University, Sweden; ¹Saab AB, Sweden
09. Sep 21 11:30 12:00 11.11.4 VIRTUAL PROTOTYPING OF ELECTRICAL THS ACTUATOR FOCUSED ON MECHANICAL POWER TRANSMISSION FUNCTIONS
J. FU FU, BEIHANG UNIVERSITY, China
09. Sep 21 12:00 12:30 11.11.5 DYNAMIC ANALYSIS AND CONTROL DESIGN OF A FAULT-TOLERANT ELECTRO-MECHANICAL ACTUATOR WITH DIFFERENTIAL BALL SCREWS
G. Di Rito, Università di Pisa - Dipartimento di Ing. Civile ed Industriale, Italy; N. Borgarelli¹, M. Nardeschi¹, B. Luciano, AESIS s.r.l., Italy; ¹Umbra Group S.p.A., Italy
Reserve Paper 11.11.R DESIGN AND CHARACTERIZATION OF A NOVEL DUAL REDUNDANCY ELECTRO-HYDROSTATIC ACTUATOR SYSTEM
H.-Q. QI, Beihang University, China
Reserve Paper 11.11.R A RESEARCH ON POSITION CONTROL ACTUATORS FOR FIXEDWINGED RESEARCH UAVS
D.T. Teubl, Institute of Aircraft Design TUM, Germany
Reserve Paper 11.11.R AN ONTOLOGICAL APPROACH FOR CLASSIFYING AIRCRAFT ACTUATORS
F Larsson¹, C Reichenwallner², A Dell'Amico¹, P Krus²; ¹Saab AB, Sweden ;²Linköping University, Sweden
Reserve Paper 11.11.R EVALUATION ASPECT MAPPING FOR ACTUATION SYSTEM DESIGN
C. Reichenwallner¹, F. Larsson², A. Dell 'Amico², P. Krus¹; ¹Linköping university, Sweden ;²Saab AB, Sweden
12.11UAV Navigation
Chair(s): Logan, M., Viola, N.
Track 12
06.2 - Flight Dynamics and Control (UAV related)
09. Sep 21 10:00 10:30 12.11.1 MISSION CONTROL WITH REAL-TIME FLIGHT PATH PLANNING FOR TILTWING UAVS TO SUPPORT RESCUE OPERATIONS
I. Barz¹, P. Hartmann, flyXdrive GmbH, Germany; N. Voget¹, S. Seitz¹, D. Moormann¹; ¹Institute of Flight System Dynamics, RWTH Aachen University, Germany
09. Sep 21 10:30 11:00 12.11.2 PATH PLANNING OF UNINHABITED AERIAL VEHICLE BASED A MODIFIED ANT ALGORITHM
Y.-F Feng, China
09. Sep 21 11:00 11:30 12.11.3 CONFLICT RESOLUTION ADVISORIES BY UAS TRAFFIC MANAGEMENT SYSTEMS
P. Hartmann, RWTH Aachen University, Germany
09. Sep 21 11:30 12:00 12.11.4 TEMPLATE MATCHING BASED ON SEGMENTED AERIAL IMAGES FOR VISION-AIDED NAVIGATION
K Hong, South Korea
09. Sep 21 12:00 12:30 12.11.5 TERRAIN INFORMATION MEASURE FOR VISION-BASED MAP-REFERENCED NAVIGATION
S. Kim, Korea Advanced Institute of Science and Technology, South Korea
Reserve Paper 12.11.R A COMPARATIVE STUDY OF 3-D GRAPH-SEARCH ALGORITHMS FOR UAVS’ SHORTEST FLIGHT PATHS
A. T. Nguyen, Le Quy Don Technical University, Vietnam
Reserve Paper 12.11.R MULTI-UAV TRAJECTORY PLANNING BASED ON COORDINATION VARIABLES
X.Z. Zheng¹, S.H. He¹, D.L. Lin¹; ¹Beijing Institute of Technology, China
13.11Airworthiness & Certification
Chair(s): ,
Track 13
10 - Safety and Security
09. Sep 21 10:00 10:30 13.11.1 CERTIFICATION CONSIDERATIONS FOR EVTOL AIRCRAFT
Yingkang MOU¹, Mei JIANG¹; ¹Nanjing Engineering Institute of Aircraft Systems, China
09. Sep 21 10:30 11:00 13.11.2 APPLICATION OF DEVELOPMENT ASSURANCE METHODOLOGIES TO ELECTRONIC ENGINE CONTROL SYSTEM (EECS)
QIN ZHU¹, Chunxiao Wang¹; ¹AECC, China
09. Sep 21 11:00 11:30 13.11.3 RESEARCH ON AIRWOTHINESS CERTIFICATION OF CIVIL AVIATION PRODCUTS BASED ON RISK ANALYSIS
C.-X Wang, AECC COMMERCIAL AIRCRAFT ENGINE CO., LTD, China
09. Sep 21 11:30 12:00 13.11.4 STUDY ON THE AIRWORTHINESS AND COMFORTABLENESS REQUIREMENTS OF AIRCRAFT CABIN AIR CONTAMINATIONS
Hu Tao, CAPEChina Aero-Polytechnology Establishment, China; Lv Haixia¹, Yue Ning¹; ¹China Aero-Polytechnology Establishment, China
09. Sep 21 12:00 12:30 13.11.5 CRASHWORTHINESS EVALUATION OF AIRCRAFT FUSELAGE BASED ON BUILDING BLOCK APPROACH
C.-K Kun, Civil Aviation University of China, China
Reserve Paper 13.11.R RESEARCH ON THE TRIGGERING CONDITIIONS OF EJECTABLE RECORDER FOR CIVIL AIRCRAFT
Shumin Pu, Northwestern Polytechnical University, China
Reserve Paper 13.11.R NUMERICAL ANALYSIS METHOD OF CIVIL AIRCRAFT DITCHING FLOATING PERFORMANCE
Haiqiang Wang¹, Huaiyuan Wang¹; ¹Shanghai Aircraft Design and Research Institute, China
Reserve Paper 13.11.R NUMERICAL STUDY OF DITCHING CHARACTERISTICS OF BWB AIRCRAFT
S.L. Ding¹, Q.L. Qu¹, P.Q. Liu¹; ¹Beihang University, China

12:30 - 13:30Lunch

0.8General Lecture 5 - IFAR - Zero emissions in 2050 (Chernyshev, Yimer, Peters, Henke)
Chair: D. Mavris ICAS PC Chair
09. Sep 21 13:30 15:30

15:30 - 16:00Break

0.9ICAS von Karman Lecture - Active Flow-, Loads- and Noise Control on Next Generation Wing (AFLoNext) - M.Wahlich
Chair: C. Atkin ICAS PPSC Chair
09. Sep 21 16:00 17:00

17:00 - 17:30Closing Ceremony