30th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

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Monday, 14. Sep 2020


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
14. Sep 20 09:00 10:00

10:00 - 10:30Break

1.1Technology Integration & Testing
Chair(s): Nagel, B.
Track 1
01 - Aircraft Design and Integrated Systems
14. Sep 20 10:30 11:00 1.1.1 TECHNOLOGY INTEGRATION FOR FUTURE AIRCRAFT CONFIGURATIONS
D. Reckzeh, Airbus, Germany
14. Sep 20 11:00 11:30 1.1.2 TECHNOLOGY INTEGRATION AND OVERALL AIRCRAFT PERFORMANCE ASSESSMENT FOR AN ADVANCED MID-RANGE AIRCRAFT
S. Woehler, German Aerospace Center, Germany
14. Sep 20 11:30 12:00 1.1.3 MAXIMIZING THE DEGREE OF SIMILITUDE OF SUB-SCALE MODELS TO SUPPORT SCALED FLIGHT TESTING
A Raju Kulkarni, TU Delft, Netherlands
Reserve Paper 1.1.R MULTI-ROLE TANKER-TRANSPORT CONVERSION
Ilan Berlowitz, IBAero Engineering, Israel
2.1Rotorcraft
Chair(s): Melkert, J.
Track 2
01 - Aircraft Design and Integrated Systems
14. Sep 20 10:30 11:00 2.1.1 VAST – VERSATILE AEROMECHANICS SIMULATION PLATFORM FOR HELICOPTERS
J. Hofmann, German Aerospace Center (DLR), Germany
14. Sep 20 11:00 11:30 2.1.2 HELICOPTER FLIGHT DYNAMICS MODELLING WITH FREE-WAKE METHOD EMBEDDED FOR ROTOR ICING ANALYSES
Guozhi Li¹, Guanglin Zhang¹, Shiyong Chu¹; ¹Aviation Industry Development Research Center of China, China
14. Sep 20 11:30 12:00 2.1.3 DESIGN AND ANALYSIS METHOD OF HELICOPTER ANTI-BALLISTIC VULNERABILITY
P. Hou, School of Aeronautics, Northwestern Polytechnical University, China
3.1Design architecture & integration methodology 1
Chair(s): Vian, J.
Track 3
02 - Systems Engineering and Integration
14. Sep 20 10:30 11:00 3.1.1 SYSTEM-OF-SYSTEMS DESIGN SPACE REFINEMENT USING MATRIX-BASED APPROACHES
L. Knöös Franzén, Linköping University, Sweden
14. Sep 20 11:00 11:30 3.1.2 SYSTEM ARCHITECTING: THE ARCHITECTURE DESIGN PROBLEM AS A GRAPH
J.H. Bussemaker, DLR, Germany
14. Sep 20 11:30 12:00 3.1.3 STRATEGIES TO ENHANCE CONFIGURATIONS FOR HIGH-PRECISION MULTI-DISCIPLINARY OPTIMIZATION
L.-H. LIU, Science and Technology on Electro-optic Control Laboratory, Chin, China
Reserve Paper 3.1.R AIRCRAFT CRUISE PERFORMANCE DESIGN INTEGRATION BASED ON SYSTEM ENGINEERING
HBH BIHAI, COMAC/SADRI, China
4.1Unsteady Aerodynamics 1
Chair(s): Mello, O., Pezzella, G.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
14. Sep 20 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
14. Sep 20 11:00 11:30 4.1.2 NONLINEAR UNSTEADY AERODYNAMIC DESCRIPTIONS BASED ON IMPROVED GOMAN\'S MODEL
J.-Y. YU, China Aerodynamics Research and Development Center, China
14. Sep 20 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
5.1Adaptive Wings
Chair(s): Dakai, L., Gowree, E.
Track 5
03.2 - Experimental Aerodynamics
14. Sep 20 10:30 11:00 5.1.1 EXPERIMENTAL INVESTIGATIONS OF A FULL MODEL WITH ADAPTIVE ELASTO-FLEXIBLE MEMBRANE WINGS
J Pflueger, Technical University Munich, Chair Aerodynamics/Fluidmechanics, Germany
14. Sep 20 11:00 11:30 5.1.2 EXPERIMENTAL ANALYSIS OF A BLOWN-WING CONFIGURATION DURING TRANSITION FLIGHT
Y Leng, ISAE, France
14. Sep 20 11:30 12:00 5.1.3 WIND TUNNEL ASSESSMENT OF A PASSIVE-ADAPTIVE WING FOR DRAG REDUCTION
C. B. York, Singapore Institute of Technology, Singapore
6.1Cavity Flows
Chair(s): Breitsamter, C., Prince, S.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
14. Sep 20 10:30 11:00 6.1.1 COMPUTATIONAL STUDY OF THREE-DIMENSIONAL OPEN CAVITY FLOWS
Y Luo, China
14. Sep 20 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
14. Sep 20 11:30 12:00 6.1.3 DETACHED-EDDY SIMULATIONS OF LEADING EDGE PLATE FLOW CONTROL BEFORE HIGH-SPEED CAVITY
PC.C Cui, China Aerodynamics Research and Development Center, China
Reserve Paper 6.1.R EXPERIMENTAL STUDY ON SUPERSONIC CAVITY ACOUSTICS
M. JIAN, CADI, China
7.1Aero Acoustics
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
14. Sep 20 10:30 11:00 7.1.1 MEDIUM-FIDELITY NOISE ASSESSMENT OF NOVEL MID RANGE TRANSPORT AIRCRAFT
M. Lummer, German Aerospace Center (DLR), Germany
14. Sep 20 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
14. Sep 20 11:30 12:00 7.1.3 NUMERICAL AND EXPERIMENTAL INVESTIGATION OF A DRESSED NOSE LANDING GEAR
L.-B. Botero-Bolívar, University of São Paulo, Brazil
Reserve Paper 7.1.R AERODYNAMIC NOISE SIMULATION OF CIVIL AIRCRAFT LANDING GEARS BASED ON LATTICE BOLTZMANN LES-SMARGORINSKY MODEL
Qing Li, Chinese Aeronautical Establishment, China; Bao Chen¹, Puyuan Wang¹, Yang Han, DEMX Shanghai Suochen Information Technology, China; 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
14. Sep 20 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
14. Sep 20 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
14. Sep 20 11:30 12:00 8.1.3 THEORETICAL AND EXPERIMENTAL INVESTIGATION OF THE AEROELASTIC CHARACTERISTICS OF THE AFLONEXT PROJECT DEMONSTRATOR
G. A. Amiryants, TsAGI, Russia
9.1Compressors & Turbines
Chair(s): Yimer, I.
Track 9
05 - Propulsion
14. Sep 20 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
14. Sep 20 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
14. Sep 20 11:30 12:00 9.1.3 DESIGN EXPERIENCE OF PENETRATION COOLING SYSTEM FOR HIGH-TEMPERATURE TURBINE BLADES
S. Kharkovskiy, CIAM, Russia
Reserve Paper 9.1.R PROBABILISTIC ANALYSIS OF A TURBOFAN SECONDARY AIR SYSTEM BASED ON MEASURED DATA OF LABYRINTH SEALS
C. -X Song, AECC Shenyang Engine Research Institute, China
Reserve Paper 9.1.R INFLUENCE OF THE AXIAL ASSEMBLAGE DEVIATION ON PERFORMANCE OF ONE TRANSONIC CENTRIFUGAL COMPRESSOR
Z.-W. Zhang, AECC HAPRI, China
10.1Computational Aeroelasticity 1
Chair(s): Amiryants, G., Luber, W.
Track 10
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
14. Sep 20 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
14. Sep 20 11:00 11:30 10.1.2 COMPUTATIONAL FLUID-STRUCTURE INTERACTIONS OF A 3D FLEXIBLE FLAPPING WING
Y.-D. Dong, China
14. Sep 20 11:30 12:00 10.1.3 COMPUTATION OD ELASTIC FOR A TRANSPORT AIRPLANE FITTED WITH WINGLETS BY FLUID-STRUCTURE INTERACTION
Mattos, B. S. Mattos, Instituto Tecnologico de Aeronautica (ITA), Brazil
11.1Aircraft & UAV as Sensor Platform
Chair(s): Goes, L., Fu, J.
Track 11
07 - Systems, Subsystems and Equipment
14. Sep 20 10:30 11:00 11.1.1 SYSTEM OF UNMANNED AERIAL VEHICLES FOR WILD BOARS WITH AFRICAN SWINE FEVER SYMPTOMS DETECTION
K.-S. Sibilski, Air Force Institute of Technology, Poland
14. Sep 20 11:00 11:30 11.1.2 VISION-BASED LOCALIZATION OF UAV FOR THE INSPECTION OF WIND TURBINE
T Kato, Graduate School of Tokai University, Japan
14. Sep 20 11:30 12:00 11.1.3 EVALUATION OF AN OBSTACLE TRACKING SYSTEM FOR AIRCRAFT GROUND OPERATIONS
K.T. Theuma, University of Malta, Malta
12.1Condition Based Maintenance 1
Chair(s): Molent, L., Li, D.
Track 12
11 - Operations and Sustainment
14. Sep 20 10:30 11:00 12.1.1 STRUCTURAL HEALTH MONITORING – THE ROUTE TO CONDITION BASED MAINTENANCE
J van Doeselaar, Airbus, France
14. Sep 20 11:00 11:30 12.1.2 COST AND BENEFIT OF STRUCTURAL HEALTH MONITORING FOR COMMERCIAL AIRCRAFT
D. M. Steinweg, Bauhaus-Luftfahrt e.V., Germany
14. Sep 20 11:30 12:00 12.1.3 REAL TIME IMPACT IDENTIFICATION TECHNIQUE USING MODAL SUPERPOSITION / APPLICATION ON AIRCRAFT FUSELAGE
D GENDRE, AIRBUS, France
Reserve Paper 12.1.R COMPOSITE RECYCLING – AN OVERVIEW OF A 21ST CENTURY CHALLENGE IN AEROSPACE INDUSTRY
J. Mašek, Brno University of Technology, Faculty of Mechanical Engineering, Czech Republic
13.1Education and industry processes
Chair(s): ,
Track 13
14 - Education and Training

12:00 - 13:00Lunch

1.2System of Systems
Chair(s): Padulo, M.
Track 1
01 - Aircraft Design and Integrated Systems
14. Sep 20 13:00 13:30 1.2.1 DEVELOPMENT AND INTEGRATION OF MULTIFIDELITY MODELS FOR SYSTEM-OF-SYSTEMS TRADE STUDIES
A. Papageorgiou, Linkoping University, Sweden
14. Sep 20 13:30 14:00 1.2.2 SYSTEM OF SYSTEMS DRIVEN AIRCRAFT DESIGN FOR WILDFIRE SUPPRESSION
P Shiva Prakasha, DLR - German Aerospace Center, Germany
14. Sep 20 14:00 14:30 1.2.3 OPTIMAL AIRLINE FLEET COMPOSED BY A COMBINATION OF JET AND TURBOPROP AIRPLANES
Mattos, B. S. Mattos, Instituto Tecnologico de Aeronautica (ITA), Brazil
Reserve Paper 1.2.R DESIGN SPECIFICATIONS AND PAYLOAD-RANGE EFFICIENCY OF TRANSPORT AIRPLANES
R. Martínez-Val, Univ. Politécnica Madrid, Spain
2.2Unconventional Configuration
Chair(s): Kimmel, B.
Track 2
01 - Aircraft Design and Integrated Systems
14. Sep 20 13:00 13:30 2.2.1 A CONCEPTUAL DESIGN OF LSA CLASS AMPHIBIOUS AIRCRAFT
S. Hanada, Sophia University, Japan
14. Sep 20 13:30 14:00 2.2.2 AEROELASTIC OPTIMIZATION OF A BLENDED WING BODY AIRCRAFT CONSIDERING STABILITY/CONTROL CONSTRAINTS
X.Z. Wang, Beihang University, China
14. Sep 20 14:00 14:30 2.2.3 PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY
Z. L. Chen, Northwestern Polytechnical University, China
Reserve Paper 2.2.R STUDY ON ADJOINT BASED OPTIMIZATION OF BWB CONFIGURATION CONSIDERING THE INTAKE AND EXHAUST EFFECTS
J.-T. Huang, China Aerodynamics Research and Development Center, China
3.2Design architecture & integration methodology 2
Chair(s): Nagel, B.
Track 3
02 - Systems Engineering and Integration
14. Sep 20 13:00 13:30 3.2.1 A COLLABORATIVE, DISTRIBUTED AND MULTILEVEL PROCESS TO SUPPORT THE DESIGN OF A NOVEL MID-RANGE AIRCRAFT CONFIGURATION
B. Gerlinger, DLR, Germany
14. Sep 20 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
14. Sep 20 14:00 14:30 3.2.3 RESEARCH ON AERO-ENGINE COLLABORATIVE DESIGN PROCESS BASED ON SYSTEM ENGINEERING
C.-Y.G. YINGANG, AECC Commercial Aviation Engine .LITD, China
Reserve Paper 3.2.R THE APPLICATION OF DIGITAL TWIN TECHNOLOGY IN INTELLIGENT OPERATION AND MAINTENANCE OF AERO-ENGINE
W-P Wang, Aero-Engine Academy of China, China
4.2Unsteady Aerodynamics 2
Chair(s): Mello, O., Bykerk, T.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
14. Sep 20 13:00 13:30 4.2.1 NUMERICAL SIMULATIONS OF TRANSONIC BUFFET ON A HALF WING-BODY CONFIGURATION
F. Sartor, ONERA, France
14. Sep 20 13:30 14:00 4.2.2 UNSTEADY FLOW SIMULATION AROUND MAIN LANDING GEAR USING HIERARCHICAL CARTESIAN GRID METHOD WITH IMMERSED BOUNDARY METHOD
T. Imamura, The University of Tokyo, Japan; Y. Tamaki, Tohoku University, Japan
14. Sep 20 14:00 14:30 4.2.3 NUMERICAL SIMULATION OF A BIO-INSPIRED FLEXIBLE FLAPPING-WING BASED ON EXPERIMENTAL MEASURED DEFORMATION
X.-Y. Yang, School of Aeronautics, Northwestern Polytechnical University, China
Reserve Paper 4.2.R ATMOSPHERIC TURBULENCE EFFECTS ON SONIC BOOM PROPAGATION
Z-S Qian, AVIC Aerodynamics Research Institute, China
5.2Full Configuration Test 1
Chair(s): Chen, Y., Ivanov, A.
Track 5
03.2 - Experimental Aerodynamics
14. Sep 20 13:00 13:30 5.2.1 EXPERIMENTAL INVESTIGATION OF DAMAGE WING IMPACT ON THE AIRLINER AERODYNAMIC CHARACTERISTICS
Andrzej. A. Krzysiak, ?ukasiewicz Research Network – Institute of Aviation, Poland
14. Sep 20 13:30 14:00 5.2.2 WIND-TUNNEL INVESTIGATION OF AERODYNAMIC CHARACTERISTICS FOR COMMERCIAL TRANSPORT AIRCRAFT AT EXTREME FLIGHT CONDITIONS
L. zhang, China Aerodynamics Research and Development Center , China
14. Sep 20 14:00 14:30 5.2.3 EXPERIMANTAL INVESTIGATION OF THE CHN-T1 MODEL IN FL-13 WIND TUNNEL OF CARDC AND DNW-LLF FACILITY
F.L.T Fan, CARDC, China
6.2Robust Control
Chair(s): Naruoka, M.
Track 6
06.1 - Flight Dynamics and Control (Control & Modelling)
14. Sep 20 13:00 13:30 6.2.1 DECENTRALIZED CONFLICT DETECTION AND RESOLUTION METHOD ACCOUNTING FOR UNCERTAINTIES OF TRAJECTORIES
N. Yokoyama, National Defense Academy, Japan
14. Sep 20 13:30 14:00 6.2.2 AN ALTERNATIVE BUT EQUIVALENT REALIZATION OF FINITE-HORIZON SUBOPTIMAL CONTROL FOR VEHICLE LANDING
S. Zhang, China Aerodynamics Research and Development Center, China
14. Sep 20 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
7.2Low Speed Aero
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
14. Sep 20 13:00 13:30 7.2.1 TRANSPORT AIRCRAFT WING INVESTIGATIONS AIMED ON CROW INSTABILITY EXCITATION AND HIGH LIFT INCREASE BY OSCILLATING FLAPS
J. Ruhland, Chair of Aerodynamics and Fluid Mechanics (TU Munich), Germany
14. Sep 20 13:30 14:00 7.2.2 NUMERICAL INVESTIGATIONS OF HINGED STRAKES AERODYNAMICS AT HIGH ANGLES OF ATTACK
Z. F. Xia, China Academy of Aerospace Aerodynamics, China
14. Sep 20 14:00 14:30 7.2.3 AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATION
Min ZHONG¹, Jun HUA¹, Xiasheng SUN¹, Sui ZHENG¹, Ganglin WANG¹, Guoxin ZHANG¹, Hao WANG¹, Yan LI¹, Xiaofei LI¹, Junqiang BAI, Northwestern Polytechnical University, China; ¹Chinese Aeronautical Establishment, China
Reserve Paper 7.2.R NUMERICAL STUDY ON WING ROCK MECHANISM OF A LOW-ASPECT-RATIO RECTANGULAR WING AT LOW REYNOLDS NUMBER
Y. Huang, Beihang University, China
8.2Aeroelasticity of Morphing Structures
Chair(s): Ritter, M., Kuzmina, S.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
14. Sep 20 13:00 13:30 8.2.1 STATIC AEROELASTIC TAILORING OF A HIGH-ASPECT-RATIO-WING FOR A SAILPLANE WITH A MORPHING FORWARD WING SECTION
F. Sturm, Technical University of Munich, Germany
14. Sep 20 13:30 14:00 8.2.2 AEROSERVOELASTIC OPTIMIZATION OF A HIGH ASPECT TRANSPORT WING WITH MORPHING TRAILING EDGE
Z. Zhang, Beihang University, China
14. Sep 20 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
14. Sep 20 13:00 13:30 9.2.1 THE USE OF SOFTWARE “VIRTUAL ENGINE” FOR TIMELY GAS-TURBINE ENGINE FAULT LOCALIZATIONS
V. Vladimir, CIAM, Russia
14. Sep 20 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
14. Sep 20 14:00 14:30 9.2.3 METHODS OF PROGRAMMED THRUST MANAGEMENT FOR NOISE REDUCTION OF SUPERSONIC CIVIL AIRCRAFT
A. Mirzoyan, CIAM, Russia
Reserve Paper 9.2.R RESEARCH ON CIVIL AIRCRAFT POWERPLANT SYSTEM EICAS MESSAGES DESIGN METHOD
S.-Y. Yang, COMAC, China
10.2Computational Aeroelasticity 2
Chair(s): Ritter, M., Amiryants, G.
Track 10
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
14. Sep 20 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
14. Sep 20 13:30 14:00 10.2.2 STUDY ON THE MULTIPLE EQUILIBRIUM POINTS OF TRANSONIC FLUTTER IN VISCOUS FLOW
G. Wang, Northwestern Polytechnical University, China
14. Sep 20 14:00 14:30 10.2.3 AEROELASTIC STRUCTURAL DESIGN OF A MID-RANGE COMPOSITE WING AIRCRAFT USING CPACS-MONA
K. Sinha, German Aerospace Center, Germany
11.2Avionics
Chair(s): Viola, N., Fu, J.
Track 11
07 - Systems, Subsystems and Equipment
14. Sep 20 13:00 13:30 11.2.1 CASCADE CONTROL OF AVIATION VARIABLE FREQUENCY AC GENERATION SYSTEM BASED ON SLIDING MODE ACTIVE DISTURBANCE REJECTION
R.-Z.-X. RUAN, Nanjing University Of Aeronautics And Astronautics, China
14. Sep 20 13:30 14:00 11.2.2 DYNAMIC PERFORMANCE ANALYSIS AND ADAPTIVE FAULT DIAGNOSIS OF AIRCRAFT POWER SYSTEM
H Li, Chengdu Aircraft Industrial (Group) Corporation, China
14. Sep 20 14:00 14:30 11.2.3 DESIGN AND APPLICATION OF 18-PULSE AUTO-COUPLING TRANSFORMER RECTIFIER FOR AVIATION
WX.-C. CHEN¹, TY.-S. SUN¹, LX.-J. JIANG¹; ¹AVIC, China
Reserve Paper 11.2.R INTEGRATED ON-BOARD NETWORKS FOR NEXT GENERATION AVIONICS
Valentin: V Olenev, St. Petersburg State University of Aerospace Instrumentation, Russia
Reserve Paper 11.2.R AN AGILE PRACTICE OF AVIONICS SYSTEM DEVELOPMENT
Lei: L Dong, China Aeronautical Radio Electronics Research Institute, China
12.2Condition Based Maintenance 2
Chair(s): , , Kecen, H.
Track 12
11 - Operations and Sustainment
14. Sep 20 13:00 13:30 12.2.1 CONDITION BASED MAINTENANCE (CBM) IN THE DIGITAL TRANSFORMATION STREAM
PC ROLLAND, AIRBUS SAS, France
14. Sep 20 13:30 14:00 12.2.2 ANALYSIS OF THE ECONOMIC PERFORMANCE FOR AIRCRAFT MAINTENANCE USING DATA DRIVEN APPROACH
X Zhao, China
14. Sep 20 14:00 14:30 12.2.3 TOTAL LIFE CYCLE COST AND EMISSION OF ELECTRIC, HYBRID – ELECTRIC AIRCRAFT
N. D. Dung, Budapest University of Tech. and econ.;, Hungary
Reserve Paper 12.2.R A METHOD FOR EVALUATING THE APPLICABILITY OF MAINTENANCE TASKS BASED ON HELICOPTER HEALTH AND USAGE MONITORING SYSTEM
DN-D Dong, AVIC China Aero-Polytechnology Establishment, China
13.2Flight Control During Approach
Chair(s): ,
Track 13
10 - Safety and Security
14. Sep 20 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
14. Sep 20 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
14. Sep 20 14:00 14:30 13.2.3 AN OVERVIEW OF FLARE TECHNIQUES AND FLARE TRAINING METHODS
J.O. Entzinger, The University of Tokyo, Japan
Reserve Paper 13.2.R MACHINE LEARNING BASED PREDICTION OF VEER-OFFS DURING LANDING PHASE
S. Lagunas-Caballero, Airbus Defence and Space, Spain

14:30 - 15:00Break

1.3HMI & Cabin Design
Chair(s): Nagel, B.
Track 1
01 - Aircraft Design and Integrated Systems
14. Sep 20 15:00 15:30 1.3.1 ATTENUATION OF NOISE IN THE CABIN OF A REGIONAL AIRCRAFT BY METAMATERIAL TRIM PANELS
M. Cinefra, Politecnico di Torino, Italy
14. Sep 20 15:30 16:00 1.3.2 ACOUSTIC FLIGHT LAB – A UNIQUE INTEGRATION PLATFORM FOR OPTIMIZING OF VIBRO-ACOUSTIC PERFORMANCE OF AIRCRAFT
M. Wandel, Airbus Operations GmbH, Germany
14. Sep 20 16:00 16:30 1.3.3 DEVELOPMENT OF A GESTURE-BASED INTERFACE FOR FLIGHT CONTROLS: RESULTS OF INITIAL EXPERIMENTS WITH THE SYSTEM
M.A. Rodriguez Diaz, Instituto Tecnologico de Aeronáutica, Brazil
2.310 years of IFAR
Chair(s): ,
Track 2
15 - Guest lectures
14. Sep 20 15:00 15:30 2.3.1 IFAR (INTERNATIONAL FORUM FOR AVIATION RESEARCH) INFRASTRUCTURE DATABASE
rd Degenhardt, DLR, Germany
14. Sep 20 15:30 16:00 2.3.2 SOL-GEL BASED ORGANIC-INORGANIC HYBRID COATINGS FOR CORROSION PROTECTION OF AEROSPACE ALUMINIUM ALLOY
R.V. Lakshmi, India
3.3Knowledge based Engineering
Chair(s): Conway, S., Stezycki, P.
Track 3
02 - Systems Engineering and Integration
14. Sep 20 15:00 15:30 3.3.1 FORMALIZED KNOWLEDGE MANAGEMENT FOR THE AIRCRAFT CABIN DESIGN PROCESS
M. Fuchs¹, C. Hesse¹; ¹DLR, Germany
14. Sep 20 15:30 16:00 3.3.2 A MODULAR KNOWLEDGE-BASED-ENGINEERING APPLICATION SUPPORTING THE PREDESIGN OF NOVEL AIRCRAFT CONFIGURATIONS
A. Zamfir, German Aerospace Center (DLR), Germany
14. Sep 20 16:00 16:30 3.3.3 IMPROVING CONCEPTUAL DESIGN SPACE EXPLORATION CAPABILITIES USING AN ADVANCED KNOWLEDGE-BASED-ENGINEERING TOOL
J. Zamboni, German Aerospace Center (DLR), Germany
Reserve Paper 3.3.R APPLICATION OF KNOWLEDGE ENGINEERING IN SPACECRAFT OVERALL DESIGN
Zhao Zhao, Harbin Institute Technology, China
4.3High Speed Flows
Chair(s): Alves, L., Liu, H.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
14. Sep 20 15:00 15:30 4.3.1 LONGITUDINAL VORTEX FORMATION IN HYPERSONIC BOUNDARY LAYER ON BLUNTED DELTA WING AND ITS EFFECT ON FLOW CHARACTERISTICS
V.I. Shalaev, Moscow Institute of Physics and Technology, Russia
14. Sep 20 15:30 16:00 4.3.2 LONGITUDINAL AND LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE HIGH-SPEED VEHICLE
G. Pezzella, University of Campania, Italy
14. Sep 20 16:00 16:30 4.3.3 MULTI-SCALE CFD/MD MODELLING OF HIGH-ENTHALPY FLOW/TPS INTERACTION AND ITS PRELIMINARY AERONAUTICAL APPLICATION
X. Yang, China Aerodynamics Research and Development Center, China
Reserve Paper 4.3.R RESEARCH OF HYPERSONIC BOUNDARY LAYER INSTABILITY AND TRANSITION WITH THERMAL-CHEMICAL NON-EQUILIBRIUM EFFECTS
X.-L. Chen, Tsinghua University, China
5.3Full Configuration Test 2
Chair(s): Ivanov, A., Chen, Y.
Track 5
03.2 - Experimental Aerodynamics
14. Sep 20 15:00 15:30 5.3.1 EXPERIMENTAL AND NUMERICAL AERODYNAMIC LOAD RESULTS ACTIONG ON THE M5/ONERA/IAE AERONAUTICAL STANDARD MODEL
M. S. Souza, IAE, Brazil
14. Sep 20 15:30 16:00 5.3.2 OPTIMIZATION OF AN ACTIVE DAMPING SYSTEM FOR USE WITH A SINGLE STRUT MOUNT
J.L. Pereira, National Research Council Canada, Canada
14. Sep 20 16:00 16:30 5.3.3 STUDY ON AERODYNAMIC CHARACTERISTICS OF LIGHT CONVERTIBLE AIRCRAFT MODEL
E.A. Pigusov, Central Aerohydrodinamic Institute, Russia
6.3Composite Defect and Damage
Chair(s): Herman, M., Ikeda, T.
Track 6
04.1 - Material Issues, Fatigue and Damage Tolerance
14. Sep 20 15:00 15:30 6.3.1 ADJUSTED SHAPES OF ADHESIVELY BONDED REPAIR PATCHES FOR THE EARLY INDICATION OF DEBOND IN FIGHTER AIRCRAFT STRUCTURES
J Jokinen, Tampere University, Finland
14. Sep 20 15:30 16:00 6.3.2 THE INFLUENCE OF THE NUMBER OF ADHESIVE PLIES (FM-300-2K) ON FRACTURE PROPERTIES
J Jokinen, Tampere University, Finland
14. Sep 20 16:00 16:30 6.3.3 STATISTICS AND ANALYSIS OF MANUFACTURE DEFECTS AND DAMAGE OF HELICOPTER COMPOSITE STRUCTURES
Jun Li, China
Reserve Paper 6.3.R DEVELOPMENT OF METHOD FOR DETERMINING THE SHEAR FRACTURE TOUGHNESS ON SPECIMENS WITHOUT A DELAMINATION INITIATOR MADE OF
V. Tokar, TsAGI, Russia
7.3Simulation
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
14. Sep 20 15:00 15:30 7.3.1 NUMERICAL VIRTUAL FLIGHT SIMULATION OF QUASI-COBRA MANEUVER OF A FIGHTER AIRCRAFT
None Wang, China Aerodynamics Research and Development Center, China
14. Sep 20 15:30 16:00 7.3.2 NUMERICAL SIMULATION OF AIRFOIL SPANWISE-RIDGE ICE FORMATION BASED ON HOT AIR ANTI-ICING SYSTEM
J.-T Wang, Northwestern Polytechnical University, China
14. Sep 20 16:00 16:30 7.3.3 VERIFICATION AND VALIDATION OF SONIC BOOM SIMULATION CAPABILITIES
G. CARRIER, ONERA, France
8.3Aeroservoelasticity
Chair(s): Degenhardt, R., Schmidt, H.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
14. Sep 20 15:00 15:30 8.3.1 MULTI-AXIS MANEUVER SIMULATION FOR SYSTEM IDENTIFICATION OF FLEXIBLE TRANSPORT AIRCRAFT BY HIGH-FIDELITY METHODS
M Ritter, German Aerospace Center (DLR), Germany
14. Sep 20 15:30 16:00 8.3.2 STRUCTURAL DESIGN OF MILITARY AIRCRAFT VERTICAL TAIL INCLUDING DYNAMIC LOADS FROM WING AND AIRBRAKE SEPARATED FLOW
W.G. LUBER, wgl-dynamics Consulting, Germany
14. Sep 20 16:00 16:30 8.3.3 RECEPTANCE-BASED UNCERTAINTY QUANTIFICATION AND MINIMIZATION IN AEROSERVOELASTIC SYSTEMS
L. J. Adamson, University of Liverpool, United Kingdom
9.3ISABE 1
Chair(s): ,
Track 9
15 - Guest lectures
14. Sep 20 15:00 15:30 9.3.1 THE POTENTIAL OF CASING TREATMENTS FOR TRANSONIC COMPRESSORS: EVALUATION BASED ON AXIAL-SLOT AND ROTOR BLADE OPTIMISATIO
G. Goinis¹, C. Voß¹, E. Nicke¹; ¹German Aerospace Center (DLR), Germany
14. Sep 20 15:30 16:00 9.3.2 CONJUGATE HEAT TRANSFER MODELLING OF A TURBINE VANE ENDWALL WITH THERMAL BARRIER COATINGS
Z. Fen, China
10.3Vibration and Damping
Chair(s): Zappino, E., Bisagni, C.
Track 10
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
14. Sep 20 15:00 15:30 10.3.1 STRUCTURAL VIBRATION CONTROL BY USING THE ENERGY FROM DIFFERENT MODE
K.L LI, Aircraft strength research institute, China
14. Sep 20 15:30 16:00 10.3.2 PREDICTING THE DYNAMIC BEHAVIOUR OF AERONAUTICAL STRUCTURES IN PRESENCE OF RUBBER-LIKE STRUCTURAL CONNECTIONS
i Isnardi, University of Liverpool, United Kingdom
14. Sep 20 16:00 16:30 10.3.3 MODAL DAMPING IDENTIFICATION METHOD BASED ON VARIATIONAL MODE DECOMPOSITION AND ENVELOPE FITTING AND ITS APPLICATIONS
J. BIAN, AECC Hunan Aviation Powerplant Research Institute, China
Reserve Paper 10.3.R A PERTURBATION ANALYSIS OF NONLINEARITY IN LANDING-GEAR SHIMMY OF A FLEET AIRCRAFT
M.-L Kou, AECC CAE, China
Reserve Paper 10.3.R ANALYSIS OF WHIRL VIBRATION IN AN AIRCRAFT BRAKE SYSTEM DURING BRAKING
D.Y.H Han, China
11.3Military Technology
Chair(s): Fu, Y., Goes, L.
Track 11
07 - Systems, Subsystems and Equipment
14. Sep 20 15:00 15:30 11.3.1 RESEARCH ON OPTIMIZATION TECHNOLOGY FOR CONTROL PARAMETERS OF EJECTION SEAT BASED ON PSO ALGORITHM
J-L Lou, Aerospace Life-support Industries,LTD., China
14. Sep 20 15:30 16:00 11.3.2 MANOEUVRABLE AERIAL TARGET TRACKING IN THE PRESENCE OF STAND-OFF JAMMING
C. Tian, School of Aeronautics, Northwestern Polytechnical University, China
14. Sep 20 16:00 16:30 11.3.3 RESEARCH ON THE PRESSURE COMFORT OF PILOT’S HELMET
X. Wang, AVIC Aerospace Life Support Industries LTD, China
12.3Flight Operations
Chair(s): Vincent, J., Da Cunha, S.
Track 12
11 - Operations and Sustainment
14. Sep 20 15:00 15:30 12.3.1 MODELING THE CLIMATE IMPACT OF FORMATION FLIGHT
T. Marks, German Aerospace Center (DLR), Germany
14. Sep 20 15:30 16:00 12.3.2 A MULTI-CRITERIA SEQUENCING LOGIC FOR THE EXTENDED TERMINAL MANOEUVRING AREA CONSIDERING INTERDEPENDENT UNCERTAINTIES
T. Zeh, Technische Universität Dresden, Germany
14. Sep 20 16:00 16:30 12.3.3 ADVANCED PASSENGER MOVEMENT MODEL DEPENDING ON THE AIRCRAFT CABIN GEOMETRY
M. Engelmann¹, T. Kleinheinz¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
Reserve Paper 12.3.R ON THE AIRCRAFT OPERATIONAL INTEGRITY
Yuting He He, Air Force Engineering University, China
13.3Flight Control and Critical Situations
Chair(s): ,
Track 13
10 - Safety and Security
14. Sep 20 15:00 15:30 13.3.1 ACTIVITY CHARACTERISTICS AND THE MECHANISM OF MESO-MICRO SCALE DISTURBANCES IN THE EAST ASIAN SUBTROPICAL UPPER-LEVEL JE
X. Chen, China Aerodynamics Research and Development Center, China
14. Sep 20 15:30 16:00 13.3.2 A METHODOLOGY FOR CHARACTERISING LOSS OF CONTROL IN FLIGHT ACCIDENTS
J.P. Macedo, Univeristy of Sao Paulo, Brazil
14. Sep 20 16:00 16:30 13.3.3 MAIN OUTCOMES FROM H2020 VISION PROJECT: EU-JAPAN COLLABORATIVE RESEARCH IN INTELLIGENT FLIGHT CONTROL STSTEMS
Y. Watanabe, ONERA, France
Reserve Paper 13.3.R ANALYSIS OF RISK FACTORS AND IDENTIFICATION OF PRECURSORS OF RUNWAY EXCURSIONS AT LANDING
Nail: N. Khairullin, Central Aerohydrodynamic Institute (TsAGI), Russia

0.2General Lecture 1 - CTO
Chair: J. Azevedo ICAS PC Chair
14. Sep 20 16:35 18:35