30th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

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Thursday, 17. Sep 2020


7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
0.1General Lecture 5 - IFAR - Zero emissions in 2050 (Chernyshev, Yimer, Peters, Henke)
Chair: D. Mavris ICAS PPSC Chair
17. Sep 20 08:00 09:30

09:30 - 10:00Break

1.1MDO
Chair(s): Bagassi, S.
Track 1
01 - Aircraft Design and Integrated Systems
17. Sep 20 10:00 10:30 1.1.1 COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN
S. Görtz, DLR - German Aerospace Center, Germany
17. Sep 20 10:30 11:00 1.1.2 ASSESSMENT OF NEW TECHNOLOGIES IN A MDAO ENVIRONMENT INCLUDING RAMS AND COST DISCIPLINES
M. Fioriti, Politecnico di Torino, Italy
17. Sep 20 11:00 11:30 1.1.3 INTERACTIONS BETWEEN MULTIFUNCTIONAL FLIGHT CONTROL SYSTEMS AND HIGH ASPECT RATIO WINGS IN A MID-RANGE AIRCRAFT
O.B. Bertram, German Aerospace Center DLR, Germany
17. Sep 20 11:30 12:00 1.1.4 MDAX: AGILE GENERATION OF COLLABORATIVE MDO WORKFLOWS
A. Makus, German Aerospace Center (DLR), Germany
17. Sep 20 12:00 12:30 1.1.5 BLENDED WING BODY PLANFORM MULTIDSCIPLIANRY OPTIMISATION
Davide DI Pasquale¹, Divyam Verma¹, Giampaolo Pagliuca¹; ¹Cranfield University, United Kingdom
2.1China Aviation
Chair(s): ,
Track 2
12 - Host nation
3.1Transition
Chair(s): Alves, L., Antunes, A.
Track 3
03.1 - Aerodynamics - CFD Methods and Validation
17. Sep 20 10:00 10:30 3.1.1 TRANSITION PREDICTION FOR TRANSPORT AIRCRAFT CONFIGURATIONS BASED ON OVERSET GRID
Y.-M. Du, Northwestern Polytechnical University, China
17. Sep 20 10:30 11:00 3.1.2 A CONTRIBUTION TO THE SIMULATION OF TRANSITIONAL FLOWS OVER AEROSPACE CONFIGURATIONS
J. L. F. Azevedo, Instituto de Aeronautica e Espaco, Brazil
17. Sep 20 11:00 11:30 3.1.3 AERODYNAMICS CHARACTERISTICS STUDY ON A NATURE LAMINAR FLOW AIRFOIL OF NEAR-SPACE VEHICLE AT LOW REYNOLDS NUMBERS
C.F. FEI, Innovation & Research Institute of HIWING Technology Academy, China
17. Sep 20 11:30 12:00 3.1.4 EFFECT OF THE WALL PROPERTIES ON THE SHOCK WAVE / LAMINAR BOUNDARY LAYER INTERACTION
A. Kutepova, Khristianovich Institute of Theoretical and Applied Mechanics, Russia
17. Sep 20 12:00 12:30 3.1.5 TURBOFAN NACELLE DESIGN WITH TAKING INTO ACCOUNT LAMINAR-TURBULENT TRANSITION
A. A. Savelyev, Central Aerohydrodynamic Institute, Russia
Reserve Paper 3.1.R HYBRID NUMERICAL SCHEMES IN PREDICTION OF HIGH-SPEED LAMINAR-TURBULENT TRANSITION
I. Egorov, TsAGI, Russia
Reserve Paper 3.1.R INFLUENCE OF RAREFACTION FAN ON RECEPTIVITY OF SUPERSONIC BOUNDARY LAYER TO FREE STREAM ACOUSTIC DISTURBANCES
N.V. Palchekovskaya, Moscow Institute of Physics and Technology, Russia
4.1Numerical Methods 1
Chair(s): Viviani, A., Wang, Z.J.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
17. Sep 20 10:00 10:30 4.1.1 MODELING AND SIMULATION OF DUSTY GAS FLOW IN AERODYNAMICS
Yu. Tsirkunov, Baltic State Tech U, Russia
17. Sep 20 10:30 11:00 4.1.2 STUDY ON AN IMPROVED PRECONDITIONING METHOD FOR MIXED COMPRESSIBLE AND INCOMPRESSIBLE FLOW
L-H Huan, China Aerodynamics Research and Development Center, China
17. Sep 20 11:00 11:30 4.1.3 STUDY OF UNSTEADY NUMERICAL SIMULATIONS BASED ON UNSTRUCTURED MESH DEFORMATION TECHNIQUE
H.-Y. Liu, China
17. Sep 20 11:30 12:00 4.1.4 2D INCOMPRESSIBLE FLOW SOLVER IN VELOCITY-VORTICITY FORMULATION USING DC-PSE OPERATOR DISCRETIZATION
L. R. Zuhal, Institut Teknologi Bandung, Indonesia
17. Sep 20 12:00 12:30 4.1.5 A HYBRID CFD METHOD FOR HELICOPTER ROTOR NOISE PREDICTION BASED ON KIRCHHOFF-FFOWCS WILLIAMS/HAWKING FORMULATION
J.-B. Fu, Politecnico di Milano, Italy
Reserve Paper 4.1.R ON THE POSSIBILITY OF APPLYING THE HYPERSONIC SMALL-DISTURBANCE THEORY IN AERODYNAMIC STUDIES OF HIGH-SPEED AIRCRAFT
A.A. Gubanov, Central Aerohydrodynamic Institute n.a. Prof. N.E. Zhukovsky, Russia
5.1Impact
Chair(s): Han, J., Bayandor, J.
Track 5
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
17. Sep 20 10:00 10:30 5.1.1 BIRD STRIKE SIMULATIONS IN MSC.SOFTWARE: CORRELATION BETWEEN THE EXPERIMENTS AND SIMULATIONS
V. Symonov¹, J. Juracka¹; ¹Brno University of Technology, Czech Republic
17. Sep 20 10:30 11:00 5.1.2 MODELS AND METHODS FOR DRONE STRIKE LOAD PREDICTIONS
F. F. Franke, Technische Hochschule Ingolstadt, Germany
17. Sep 20 11:00 11:30 5.1.3 EXPERIMENTAL STUDY ON ATTENUATION PERFORMANCE OF SHOCK ABSORBING INSERT
H.-S Park, South Korea
17. Sep 20 11:30 12:00 5.1.4 MULTISCALE ANALYSIS OF BALLISTIC IMPACT OF WOVEN COMPOSITE MATERIALS
D SONG, China
17. Sep 20 12:00 12:30 5.1.5 DEVELOPMENT OF A PREDICTIVE METHODOLOGY FOR FAST ESTIMATION OF IMPACT BEHAVIOR IN AEROSPACE GRADE COMPOSITES
K Carpenter, United States
6.1Student Final
Chair(s): Rein Weston, K.
Track 6
15 - Guest lectures
7.1Laminar Flow
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
17. Sep 20 10:00 10:30 7.1.1 BLADE - NATURAL LAMINAR FLOW FLIGHT TESTING
T. Gibson, Airbus, United Kingdom
17. Sep 20 10:30 11:00 7.1.2 METODICAL STUDIES OF THE POSSIBILITY TO APPLY A NUMERICAL METHOD WITH BUILT-IN EMPIRICAL CRITERIA FOR DETERMINING THE LA
N.V. Voevodenko, TsAGI, Russia
17. Sep 20 11:00 11:30 7.1.3 NATURAL-LAMINAR-FLOW AIRFOIL DESIGN OPTIMIZATION CONSIDERING CROSSFLOW INSTABILITY
Z.-M Xu, Northwestern Polytechnical University, China
17. Sep 20 11:30 12:00 7.1.4 DESIGN OF TRANSONIC NATURAL LAMINAR FLOW NACELLE
C.Y. Yan, Tsinghua University, China
17. Sep 20 12:00 12:30 7.1.5 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
8.1Failure Analysis and Fatigue
Chair(s): Symonov, V., Shanygin, A.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
17. Sep 20 10:00 10:30 8.1.1 METHODS TO CALCULATE THE STRUCTURE FATIGUE DAMAGE UNDER VARIOUS SPECTRA OF VIBRO-ACOUSTIC LOADS
I.S. Sidorov, TsAGI, Russia
17. Sep 20 10:30 11:00 8.1.2 FAILURE PROPERTIES AND MACROSCOPIC MODELLING OF AERONAUTIC RIVETED CONNECTIONS
ZY Yifan, Civil Aviation University of China, China
17. Sep 20 11:00 11:30 8.1.3 ITERATIVE GLOBAL/LOCAL NON-INTRUSIVE MODEL COUPLING METHOD FOR STRUCTURE FAILURE ANALYSIS
Y.J. LIU, AVIC the first aircraft institute, China
17. Sep 20 11:30 12:00 8.1.4 NUMERICAL ANALYSIS AND COMPARISON WITH RESULTS OF FRACTURE TESTS OF LUG MANUFACTURED IN COMPOSITE MATERIAL
G. C. Fonseca, Embraer - Minas Gerais, Brazil
17. Sep 20 12:00 12:30 8.1.5 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
9.1Combustion & Heat Transfer
Chair(s): Steczycki, P.
Track 9
05 - Propulsion
17. Sep 20 10:00 10:30 9.1.1 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
17. Sep 20 10:30 11:00 9.1.2 INVESTIGATION OF MEASUREMENT CHARACTERISTICS OF PROPAGATING FLAME BY MULTIPLE-ION-PROBE METHOD
T.Y. Yatsufusa, Hiroshima Institute of Technology, Japan
17. Sep 20 11:00 11:30 9.1.3 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
17. Sep 20 11:30 12:00 9.1.4 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
17. Sep 20 12:00 12:30 9.1.5 HYBRID KERNEL FORMATION AND TRACKING METHOD TO PREDICT IGNITION LIMITS ON LOW EMISSION COMBUSTORS
X.Wei Xiao, AECC Hunan Aviation Powerplant Research Institute, China
Reserve Paper 9.1.R NONLINEAR DYNAMICS MEASUREMENT OF SELF-SUSTAINED THERMOACOUSTIC INSTABILITIES IN A PREMIXED SWIRLING COMBUSTOR
D. Zhao, University of Canterbury, New Zealand
Reserve Paper 9.1.R DECISION PROBLEMS IN AN IDENTIFICATION OF FACTORS INFLUENCING ON THE EMISSION OF HARMFUL COMPOUNDS OF TRANSPORT MEANS
M. JACYNA, Warsaw University of Technology, Poland
10.1Nonlinear Control
Chair(s): Rogalski, T.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
17. Sep 20 10:00 10:30 10.1.1 NONLINEAR CONTROL STRATEGY FOR QUAD-TILTROTOR IN TRANSITION MODE
K.W. Jang, KAIST, South Korea
17. Sep 20 10:30 11:00 10.1.2 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
17. Sep 20 11:00 11:30 10.1.3 MACHINE LEARNING TECHNIQUES FOR AIRCRAFT STALL DETECTION AND RECOVERY
J Gauci, University of Malta, Malta
17. Sep 20 11:30 12:00 10.1.4 AIRCRAFT AUTOPILOT DESIGN USING ASYMMETRIC VARIABLE-SPAN WING MORPHING
J. Lee, Seoul National University, South Korea
17. Sep 20 12:00 12:30 10.1.5 AUTONOMOUS FLIGHT CONTROL BASED ON NEURAL NETWORKS AND FUZZY DECISION
P.C. Wen, AVIC Xi’an Aeronautics Computing Technique Research Institute, China
Reserve Paper 10.1.R ANALYSIS OF REENTRY TRAJECTORY OPTIMIZATION OF COMPLEX PATH CONSTRAINTS USING HERMIT SPLINE INTERPOLATION
Y Kwak, Konkuk Univ., South Korea
11.1Aspects of More electric Aircraft
Chair(s): Peters, M., Viola, N.
Track 11
07 - Systems, Subsystems and Equipment
17. Sep 20 10:00 10:30 11.1.1 OPTIMALPOWER DISTRIBUTION ON A MORE ELECTRIC AIRCRAFT
E. D'Amato, Università degli studi della Campania "Luigi Vanvitelli", Italy
17. Sep 20 10:30 11:00 11.1.2 CONCEPTUAL SYSTEM-LEVEL MODELING OF CONVENTIONAL AND MEA SYSTEMS ARCHITECTURES FOR MODERN MIDRANGE TRANSPORT AIRCRAFT
M. Jünemann, Hamburg University of Technology, Germany
17. Sep 20 11:00 11:30 11.1.3 ICE THICKNESS IMPACT AND DETECTION IN RESONANT ELECTROMECHANICAL DEICING SYSTEMS
M. Budinger, INSA Toulouse, France
17. Sep 20 11:30 12:00 11.1.4 ANTI-PUMP-FORCE-FIGHT PRESSURE CONTROLLER FOR A REDUNDANT HYDRAULIC POWER PACKAGE WITH SPEED VARIABLE AC MOTOR PUMPS
N. Trochelmann, TUHH/ Institute of Aircraft Systems Engineering, Germany
17. Sep 20 12:00 12:30 11.1.5 ON-BOARD SYSTEM ARCHITECTURES FOR HYBRID/ALL-ELECTRIC REGIONAL AIRCRAFT
M. Fioriti, Politecnico di Torino, Italy
Reserve Paper 11.1.R SURROGATE MODELS OF PM BRUSHLESS MOTORS FOR THE PRELIMINARY DESIGN OF AIRCRAFT APPLICATION SYSTEMS
F De Giorgi, INSA/ICA Toulouse, France
Reserve Paper 11.1.R NUMERICAL SIMULATION OF DE-ICING PROCESS ON COMPOSITE AIRFOIL WITH ANISOTROPIC CONDUCTIVITY
X.F Guo, Shanghai Jiao Tong University, China
12.1UAV Navigation
Chair(s): Logan, M., Viola, N.
Track 12
06.2 - Flight Dynamics and Control (UAV related)
17. Sep 20 10:00 10:30 12.1.1 MISSION CONTROL WITH REAL-TIME FLIGHT PATH PLANNING FOR TILTWING UAVS TO SUPPORT RESCUE OPERATIONS
I. Barz, Institute of Flight System Dynamics, RWTH Aachen University, Germany
17. Sep 20 10:30 11:00 12.1.2 PATH PLANNING OF UNINHABITED AERIAL VEHICLE BASED A MODIFIED ANT ALGORITHM
Y.-F Feng, China
17. Sep 20 11:00 11:30 12.1.3 CONFLICT RESOLUTION ADVISORIES BY UAS TRAFFIC MANAGEMENT SYSTEMS
P. Hartmann, RWTH Aachen University, Germany
17. Sep 20 11:30 12:00 12.1.4 TEMPLATE MATCHING BASED ON SEGMENTED AERIAL IMAGES FOR VISION-AIDED NAVIGATION
K Hong, South Korea
17. Sep 20 12:00 12:30 12.1.5 TERRAIN INFORMATION MEASURE FOR VISION-BASED MAP-REFERENCED NAVIGATION
S. Kim, Korea Advanced Institute of Science and Technology, South Korea
Reserve Paper 12.1.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 12.1.R 3D TRAJECTORY DESIGN AND TRACKING FOR MULTIROTOR UAVS INDOOR FLIGHT
E. Capello, Italy
13.1Airworthiness & Certification
Chair(s): ,
Track 13
10 - Safety and Security
17. Sep 20 10:00 10:30 13.1.1 CERTIFICATION CONSIDERATIONS FOR EVTOL AIRCRAFT
Yingkang MOU¹, Mei JIANG¹; ¹Nanjing Engineering Institute of Aircraft Systems, China
17. Sep 20 10:30 11:00 13.1.2 APPLICATION OF DEVELOPMENT ASSURANCE METHODOLOGIES TO ELECTRONIC ENGINE CONTROL SYSTEM (EECS)
Q ZHU, AECC COMMERCIAL AIRCRAFT ENGINE CO., LTD., China
17. Sep 20 11:00 11:30 13.1.3 RESEARCH ON AIRWOTHINESS CERTIFICATION OF CIVIL AVIATION PRODCUTS BASED ON RISK ANALYSIS
C.-X Wang, AECC COMMERCIAL AIRCRAFT ENGINE CO., LTD, China
17. Sep 20 11:30 12:00 13.1.4 STUDY ON THE AIRWORTHINESS AND COMFORTABLENESS REQUIREMENTS OF AIRCRAFT CABIN AIR CONTAMINATIONS
Hu Tao Tao, CAPE?CAPE?, China
17. Sep 20 12:00 12:30 13.1.5 CRASHWORTHINESS EVALUATION OF AIRCRAFT FUSELAGE BASED ON BUILDING BLOCK APPROACH
C.-K Kun, Civil Aviation University of China, China
Reserve Paper 13.1.R RESEARCH ON THE TRIGGERING CONDITIIONS OF EJECTABLE RECORDER FOR CIVIL AIRCRAFT
Shumin Pu, Northwestern Polytechnical University, China

12:30 - 14:00Lunch

1.2Hybrid/Electric & Unconventional Aircraft 4
Chair(s): Melkert, J.
Track 1
01 - Aircraft Design and Integrated Systems
17. Sep 20 14:00 14:30 1.2.1 STUDY OF THE BENEFITS OF A SEMI-MORPHING WING CONCEPT
L. P. Ruiz Calavera, Airbus Defence & Space, Spain
17. Sep 20 14:30 15:00 1.2.2 FLIGHT EXPERIMENTS FOR THE ALTAIR SEMI-REUSABLE AIR-LAUNCH SYSTEM WITH THE DEMONSTRATOR EOLE
J. Gauvrit-Ledogar, ONERA, France
17. Sep 20 15:00 15:30 1.2.3 CIRCULATION CONTROL AIRCRAFT: RECENT DEVELOPMENTS OF THE CHANNEL-WING DESIGN
HD Djojodihardjo, Retired Professor, Indonesia
2.2tbd4
Chair(s): ,
Track 2
3.2Compressor and Fan Aerodynamics
Chair(s): Wan, T., Tomita, J.
Track 3
03.1 - Aerodynamics - CFD Methods and Validation
17. Sep 20 14:00 14:30 3.2.1 APPLICATION OF A SKEWED SLOT CASING TREATMENT IN A HIGH-LOADING AXIAL-CENTRIFUGAL COMPRESSOR
H. L. JIN, China
17. Sep 20 14:30 15:00 3.2.2 DISTORTION PLATE DESIGN, SIMULATION VALIDATION AND TEST SCHEME FOR STABILITY ANALYSIS ON A FAN COMPONENT OF AEROENGINE
ZP.-L Li, AECC Shenyang Engine Design Institute, China
17. Sep 20 15:00 15:30 3.2.3 EFFECT OF INTER-STAGE BLEEDING ON FLOW STABILITY OF A MULTI-STAGE COMPRESSOR
X. W. LIU, China
Reserve Paper 3.2.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
4.2Numerical Methods 3
Chair(s): Viviani, A., Obayashi, S.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
17. Sep 20 14:00 14:30 4.2.1 AERODYNAMIC AND AEROACOUSTIC INVESTIGATION OF THE FLOW PAST THE 30P30N HIGH-LIFT MULTI-AIRFOIL
Yao Jin Jin, China
17. Sep 20 14:30 15:00 4.2.2 AN INTELLIGENT STRUCTURED CHIMERA GRID APPROACH FOR MOVING OBJECTIVES
L. L. Li, AVIC Aeronautics Computing Technique Research Institute, China
17. Sep 20 15:00 15:30 4.2.3 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 4.2.R INVESTIGATION OF NUMERICAL METHOD OF INTERNAL FLOW AND OIL CAPTURE EFFICIENCY OF UNDER-RACE LUBRICATION
J.-L. Jiang, Northwestern Polytechnical University, China
5.2UAV Flight Testing
Chair(s): Wong, K.C., Monk, J.
Track 5
06.2 - Flight Dynamics and Control (UAV related)
17. Sep 20 14:00 14:30 5.2.1 VALIDATION OF SCALED FLIGHT TESTING - OVERALL APPROACH AND FIRST RESULTS
P. Schmollgruber, France
17. Sep 20 14:30 15:00 5.2.2 COMPARISON OF ESTIMATED AND ACTUAL AERODYNAMIC PERFORMANCE OF A 65KG UAV
J. Bartasevicius, Technical University of Munich, Germany
17. Sep 20 15:00 15:30 5.2.3 BIO-INSPIRED SWARM CONTROL OF DRONES USING SIMPLE INTERACTION RULES
J Kikuchi, Graduate School of Tokai University, Japan
Reserve Paper 5.2.R THE STUDY OF UNMANNED AERIAL VEHICLE FLYING QUALITIES FLIGHT TEST METHOD BASED ON TIME-DELAY EVALUATION
S.J.-Q. QI, Chinese Flight Test Establishment , China
6.2System Qualification
Chair(s): Fu, J., Peters, M.
Track 6
07 - Systems, Subsystems and Equipment
17. Sep 20 14:00 14:30 6.2.1 RESEARCH ON CIVIL AIRCRAFT EQUIPMENT QUALIFICATION TEST
G.-C Zhang, Shanghai Aircraft Design and Research Institute, China
17. Sep 20 14:30 15:00 6.2.2 KNOWLEDGE-BASED ENGINEERING FOR MODELLING AIRCRAFT THERMAL BEHAVIOUR
A.S.J. van Heerden, Cranfield University, United Kingdom
17. Sep 20 15:00 15:30 6.2.3 EXPERIMENTAL STUDY OF A LOOP HEAT PIPE FOR COOLING AIRCRAFT NACELLE ENGINE EQUIPEMENT
V. Ayel, ISAE-ENSMA, France
Reserve Paper 6.2.R 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
7.2Stability
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
17. Sep 20 14:00 14:30 7.2.1 NUMERICAL EVALUATION OF DYNAMIC STABILITY DERIVATIVES FOR HIGH LIFT DEVICES
N/A Maqsood, Pakistan
17. Sep 20 14:30 15:00 7.2.2 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
17. Sep 20 15:00 15:30 7.2.3 EFFECT OF CANARD DEFLECTION ON MAIN WING FOR A CLOSE-COUPLED-CANARD CONFIGURATION DURING PITCHING OSCILLATIONS
Q. Chen, Beihang University, China
Reserve Paper 7.2.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 7.2.R ADJOINT-BASED STUDY OF THE AERODYNAMIC CENTER SHIFT IN THE TRANSONIC FLOW REGIME
M. Hayashi, Federal University of ABC, Brazil
8.2Static Analysis of Aircraft Structures
Chair(s): Zheng, J., Zappino, E.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
17. Sep 20 14:00 14:30 8.2.1 MULTIDIMENSIONAL FINITE ELEMENT MODELS FOR ADVANCED HELICOPTER BLADES
M. Filippi, Politecnico di Torino, Italy
17. Sep 20 14:30 15:00 8.2.2 MATHEMATICAL MODELS FOR OPTIMIZATION OF AIRCRAFT STRUCTURES TAKING INTO CONSIDERATION OF LOCAL STRESS DISTRIBUTION
S. A. Tuktarov, Central aerohydrodynamic institute, Russia
17. Sep 20 15:00 15:30 8.2.3 THE BEAM MODEL OF A HAWKMOTH WING STRUCTURE
A. T. Nguyen, Le Quy Don Technical University, Vietnam
Reserve Paper 8.2.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 8.2.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
9.2ISABE 2
Chair(s): ,
Track 9
15 - Guest lectures
17. Sep 20 14:00 14:30 9.2.1 KEY TECHNOLOGIES FOR THE NEXT GENERATION OF CIVIL AIRCRAFT ENGINES
F. Haselbach, United Kingdom
17. Sep 20 14:30 15:00 9.2.2 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
17. Sep 20 15:00 15:30 9.2.3 AN EXPERIMENTAL-NUMERICAL METHOD FOR TRANSIENT INFRARED MEASUREMENT OF FILM COOLING EFFECTIVENESS
N.E. Holgate, United Kingdom
10.2Helicopter Control
Chair(s): Che, J.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
17. Sep 20 14:00 14:30 10.2.1 MODELING OF HELICOPTER FLIGHT DYNAMICS AND ROTOR BLADES LOADS DURING EXTREME FLIGHTS
Grzegorz Kowalec Kowaleczko, Air Force Institute of Technology, Poland
17. Sep 20 14:30 15:00 10.2.2 DESIGN TECHNIQUE OF INTEGRAL ALGORITHMS FOR HELICOPTER FBW CONTROL SYSTEM
V.M. Kuvshinov, Central Aero-Hydrodynamics Institute, Russia
17. Sep 20 15:00 15:30 10.2.3 AERODYNAMIC PERFORMANCE CALCULATION OF XH-59A HELICOPTER IN MANEUVERING PROCESS
K. Y. You, Northwestern Polytechnical University, China
11.2Vehicle Mangement Systems
Chair(s): Krus, P., Viola, N.
Track 11
07 - Systems, Subsystems and Equipment
17. Sep 20 14:00 14:30 11.2.1 EVALUATION OF A GESTURE-BASED PILOT-AIRCRAFT INTERFACE IN A SIMULATION ENVIRONMENT
M.A. Rodriguez Diaz, Instituto Tecnologico de Aeronáutica, Brazil
17. Sep 20 14:30 15:00 11.2.2 ANALYSIS AND SOLUTION RESEARCH OF THE AIR DATA LOSS FROM AIRCRAFT FOR ENGINE CONTROL
J LI, COMAC, China
17. Sep 20 15:00 15:30 11.2.3 REAL-TIME GNSS PRECISE POINT POSITIONING AND VISUAL-INERTIAL ODOMETRY COUPLED NAVIGATION SYSTEM FOR UAVS
C.-C. Cheng, SJTU, China
Reserve Paper 11.2.R DESIGN OF UAV NAVIGATION ALGORITHM IN SINGLE SATELLITE ENVIRONMENT BASED ON HIGH PRECISION TIMING
L.KT Li, China National Aeronautical Radio Electronics Research Institute, China
12.2UTM/On-Demand Mobility
Chair(s): ,
Track 12
09 - Air Transport System Efficiency
17. Sep 20 14:00 14:30 12.2.1 AIRLINE NETWORK-AIRPLANE INTEGRATED OPTIMIZATION CONSIDERING MANUFACTURER\'S PROGRAM COST
Mattos, B. S. Mattos, Instituto Tecnologico de Aeronautica (ITA), Brazil
17. Sep 20 14:30 15:00 12.2.2 ANALYSIS AND EVALUATION OF AN URBAN AIR TRAFFIC NETWORK BASED ON OPERATIONAL PERFORMANCE PARAMETERS
M. Husemann, Institute of Aerospace Systems, Germany
17. Sep 20 15:00 15:30 12.2.3 ON-DEMAND AIR MOBILITY FOR BEIJING: PREREQUISITES FOR COMPETITIVENESS
X. Sun, Beihang University, China
Reserve Paper 12.2.R ASSESSMENT OF THREE COMMUTER AIRCRAFT CONCEPTS FROM A TRANSPORT SYSTEM PERSPECTIVE
V. Papantoni, German Aerospace Center (DLR), Germany
Reserve Paper 12.2.R AIR TRAFFIC MANAGEMENT OF DRONES INTEGRATED INTO SMART CITIES
D. Rohacs, B udapest University of Tech. and econ.;, Hungary
13.2Operational Training
Chair(s): Holmes, D., Ren, H.
Track 13
11 - Operations and Sustainment
17. Sep 20 14:00 14:30 13.2.1 DESIGN OF SIMULATION-BASED PILOT TRAINING SYSTEMS USING MACHINE LEARNING AGENTS
J. Källström¹, R. Granlund, RISE SICS East, Sweden; F. Heintz¹; ¹Linköping University, Sweden
17. Sep 20 14:30 15:00 13.2.2 A STUDY ON TRAINING NEEDS ANALYSIS (TNA) METHOD FOR MILITARY AIRCRAFT
Q WANG, Chengdu Aircraft Design and Research Institute, AVIC, China
17. Sep 20 15:00 15:30 13.2.3 COMPARISON OF READINESS TO PERFORM THE TASK OF AIRCRAFT USED FOR CADET TRAINING
J. Tomaszewska, Polish Air Force University, Poland
Reserve Paper 13.2.R INFORMATION DISTRIBUTION METHOD FOR MULTI-AIRCRAFT COOPERATION BASED ON COLLABORATIVE FILTERING ALGORITHM
Y Wang, AVIC, China

15:30 - 16:00Break

0.2von Karman Lecture - Active Flow-, Loads- and Noise Control on Next Generation Wing (AFLoNext) - M.Wahlich
Chair: C. Atkin ICAS MRSC Chair
17. Sep 20 16:00 17:00

17:00 - 17:30Closing Ceremony