Session List
Interactive Presentations
Reserve Papers
Monday, 06. September 2021
RaumTrack 1Track 2Track 3Track 4Track 5Track 6Track 7Track 8Track 9Track 10Track 11
07:00
08:00
Registration
08:00
09:00
Opening Ceremony - Chair: Suzuki S. ICAS President JP
09:00
10:00
ICAS Daniel & Florence Guggenheim Memorial Lecture, Digital Engineering Transformation and Innovation, Xinguo Zhang, China - Chair: S. Suzuki, ICAS President 2020, JP
10:00
10:30
Break
10:30
12:00
1.1
China Session 1
2.1
Unconventional Configuration
3.1
Military Technology
4.1
Unsteady Aerodynamics 1
5.1
Composite Characterization and Fabrication
6.1
Cavity Flows
7.1
Aero Acoustics
8.1
Testing and Measurement
9.1
Education and industry processes-Pitch talk
10.1
Decoupling Control
11.1
Flight Operations
12:00
13:00
Lunch
13:00
14:30
1.2
China Session 2
2.2
Rotorcraft & Seaplane
3.2
Avionics
4.2
Unsteady Aerodynamics 2
5.2
Dynamics and Noise
6.2
Transition Physics 1
7.2
Performance
8.2
Aeroelasticity of Morphing Structures
9.2
Combustion & Heat Transfer
10.2
Robust Control
11.2
Operational Training
14:30
15:00
Break
15:00
17:00
1.3
Sino-French Session: MBSE and Digital Transformation
2.3
Digital Pioneering – Where will MBSE, AI, VR and SoSE bring engineering in 20 years?
3.3
System Qualification and Testing
4.3
Turbulence Modeling
5.3
Fatigue and Structural Integrity
6.3
Flow Control Applications
7.3
Propulsion Airframe Integration
8.3
Impact
9.3
Controls & Software
10.3
Design architecture & integration methodology
11.3
Safety and Security Analysis
17:05
18:00
Project Clean Sky - Axel Krein, GER, Ron van Manen, NL, Sebastien Dubois, FR - Chair: D. Müller Wiesner, former ICAS President, DE
Tuesday, 07. September 2021
RaumTrack 1Track 2Track 3Track 4Track 5Track 6Track 7Track 8Track 9Track 10Track 11
08:00
10:00
1.4
Design Optimization under Uncertainty
2.4
Hypersonics
3.4
UAV Dynamics and Control 1
4.4
Aerodynamic Optimization
5.4
Air Traffic Efficiency
6.4
Developments in Modelling
7.4
Configurations
8.4
Computational Aeroelasticity
9.4
Fan / Nacelle & Propeller 1
10.4
System Architecture
11.4
ATC, Pilot & Controller
10:00
10:30
Break
10:30
12:00
1.5
Hybrid/Electric & Unconventional Aircraft 1
2.5
Cost Assessment
3.5
UAV Conflict Avoidance
4.5
Flows with Thermal Effects
5.5
Airport/Aircraft Operation
6.5
Turbulent Flows
7.5
Low Speed Aero
8.5
Composite Materials and Structures
9.5
Helicopter Control
10.5
Condition Based Maintenance 1
11.5
Systems & Components Safety
12:00
13:00
Lunch
13:00
14:30
1.6
HMI & Cabin Design
2.6
Aviation and World Wildfires
3.6
Model Based Systems Engineering 1
4.6
High Speed Flows
5.6
Airspace Management
6.6
Composite Defect and Damage
7.6
Simulation
8.6
Failure Analysis and Fatigue
9.6
Additive Manufacturing
10.6
Condition Based Maintenance 2
11.6
Flight Control and Critical Situations
14:30
16:00
Interactive presentations
16:00
16:10
Break
16:10
17:00
General Lecture 2 - Future needs you-the panel discussion of the skills of aeronautics C.Combs, USA T.Ito, Japan, P.Vialettes, France,L.Jiang, China - Chair: M. Kanerva, ICAS ECSC Chair, FI
17:00
18:00
ICAS Lecture for Innovation in Aeronautics - Electrification - The third revolution in aviation, Cory Combs, USA - Chair: C. Atkin, ICAS PPSC Chair, GB
18:00
19:00
Speed mentoring - for early career proffesionals only, for programme see www.icas2020.com
Wednesday, 08. September 2021
RaumTrack 1Track 2Track 3Track 4Track 5Track 6Track 7Track 8Track 9Track 10Track 11
08:00
10:00
1.7
Hybrid/Electric & Unconventional Aircraft 2
2.7
Global Collaborative Digital Integration in Aviation / IFAR-X challenge
3.7
AFLoNext
4.7
Applied CFD 1
5.7
UTM/On-Demand Mobility
6.7
Laminar Flow
7.7
Failure And Fracture Mechanics
8.7
Compressors & Turbines
9.7
Flight Control During Approach
10.7
Flight Dynamics 2
11.7
empty 1
10:00
10:30
Break
10:30
12:00
1.8
MDO
2.8
Compressor and Fan Aerodynamics 1
3.8
Aspects of Landing Gear Design
4.8
Numerical Methods 1
5.8
UAV Flight Testing
6.8
Transition Physics 2
7.8
Optimization 1
8.8
Aeroelastic Identification and Control
9.8
empty 2
10.8
Flying Quality
11.8
Turbomechanics & Rotating Wings
12:00
13:00
Lunch
13:00
15:30
1.9
System of Systems
2.9
UAS
3.9
Model Based Systems Engineering 2
4.9
Applied CFD 2
5.9
Buckling and Instability
6.9
Unsteady Flow Phenomena
7.9
Advanced Manufacturing Management
8.9
Design of Aircraft Structures 1
9.9
Airworthiness & Certification
10.9
Flight Dynamics 1
11.9
Measurement Techniques & Data Analysis
15:30
16:00
Break
16:00
17:00
General Lecture 3 - Trends in Aircraft Propulsion: Reflections on ISABE, Ric Parker, President ISABE - Chair: J.L. Azevedo, ICAS President, BR
17:00
18:00
General Lecture 4 - Virtual Aircraft Technology Integration Platform - Results of DLR's Project VicToria - S. Görtz - Chair: B. Nagel, ICAS PC Member, DE
Thursday, 09. September 2021
RaumTrack 1Track 2Track 3Track 4Track 5Track 6Track 7Track 8Track 9Track 10Track 11
08:00
09:30
1.10
Hybrid/Electric & Unconventional Aircraft 3
2.10
10 years of IFAR
3.10
Compressor and Fan Aerodynamics 2
4.10
Applied CFD 3
5.10
Transonic/Supersonic
6.10
UAV Dynamics and Control 2
7.10
Stability
8.10
Static Analysis of Aircraft Structures
9.10
Avionics and Aircraft Systems
10.10
Fan / Nacelle & Propeller 2
11.10
Fault Detection
09:30
10:00
Break
10:00
12:30
1.11
Wing Design
2.11
Design Methods
3.11
Transition
4.11
Numerical Methods 2
5.11
Full Configuration Test
6.11
Design of Aircraft Strutcures 2
7.11
Optimization 2
8.11
Vibration and Damping
9.11
Actuator design & Analysis
10.11
MDO & More / Hybrid / Electric Propuslion
11.11
Nonlinear Control
12:30
13:30
Lunch
13:30
15:00
General Lecture 5 “IFAR perspective on sustainable aviation – (how) can we achieve zero emission aviation?” Sergey Chernyshev, Rolf Henke, Sun Xiasheng, Michel Peters, Bob Pearce, Ibrahim Yimer - Chair: D. Mavris, ICAS PC Chair, US
15:00
15:20
Break
15:20
16:20
ICAS von Karman Lecture - Active Flow- Loads- and Noise- Control on next Generation Wing, M.Wahlich - Chair: R. Gerhards, ICAS EC Member, DE
16:20
17:30
Closing ceremony - Chair: Suzuki S. ICAS President 2020 JP
1.1China Session 1
Chair: X.G. Zhang
Track 1
12 - Host nation
  10:30 11:00 1.1.1 SMART CIVIL AVIATION TRANSPORTATION SYSTEM
S. Yin, China
  11:00 11:30 1.1.2 FLIGHT TEST ON THE ICING OF CIVIL AIRCRAFT
Y. Chen, China
  11:30 12:00 1.1.3 CURRENT PROGRESS AND FUTURE PROSPECTS OF CHINESE COMMERCIAL AIRCRAFT ENGINE DEVELOPMENT
C. Shao, China
2.1Unconventional Configuration
Chair: B. Kimmel
Track 2
01 - Aircraft Design and Integrated Systems
  10:30 11:00 2.1.1 PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY
Z.-L. Chen¹, Y.-C. Chen², S. Zhang, Beijing Aeronautical Science & Technology Research Institute, China; L.-X. Wang, Beihang University, China; Z.-G. Tan², B. Chen, AVIC Aerodynamics Research Institute, China; S.-W. Zhao, AVIC The First Aircraft Institute, China; L. Wang, AVIC Huiyang Aviation Propeller Co., LTD., China; J. Li¹, C.-S. Yuan¹, Y.-J. Zhang¹, Y.-Z. Zhang¹, W.-M. Sang¹, Y.-J. Tao¹, D. Li¹, B.-Q. Zhang¹; ¹Northwestern Polytechnical University, China ;²Shanghai Aircraft Design and Research Institute, COMAC, China
  11:00 11:30 2.1.2 STUDY ON ADJOINT OPTIMIZATION OF BWB CONFIGURATION CONSIDERING THE INFLUENCE OF INTAKE AND EXHAUST SYSTEM
J.-T. Huang¹, Z. Zhou¹, Z.-H. Gao, Northwestern Polytechnical University, China; X. Chen¹, S.-D. Zhong¹; ¹China Aerodynamics Research and Development Center, China
  11:30 12:00 2.1.3 THE USE OF REVERSE ENGINEERING AND COMPUTATIONAL FLUID DYNAMICS METHODS IN THE PRELIMINARY DESIGN OF A LOW COST SATELLITE LAUNCH SYSTEM
L. Kiszkowiak¹, A. Olejnik¹, A. Dziubinski, Lukasiewicz Research Network – Institute of Aviation, Poland; P. Zalewski¹; ¹Military University of Technology, Poland
3.1Military Technology
Chair: Y. Fu
Track 3
07 - Systems, Subsystems and Equipment
  10:30 11:00 3.1.1 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
  11:00 11:30 3.1.2 RESEARCH ON THE PRESSURE COMFORT OF PILOT HELMETS
X.J. Wang¹, J. Xu¹, J.H. Wang¹, J.C. Mi, Intel Engineering Simulation Technology Co.,Ltd, China; Y.M. Jiang, Tiangong University, China; ¹Aerospace Life-support Industries LTD, China
4.1Unsteady Aerodynamics 1
Chair: J. Azevedo
Track 4
03.1 - Aerodynamics – CFD Methods and Validation
  10:30 11:00 4.1.1 NONLINEAR UNSTEADY AERODYNAMIC DESCRIPTIONS BASED ON IMPROVED GOMAN’S MODEL
J. Yu¹, X.-J. Wu¹, D. Hao¹, H.-Y. Jia¹, S.-S. Liu¹; ¹CARDC, China
  11:00 11:30 4.1.2 DATA FUSION UNSTEADY AERODYNAMIC MODELING BASED ON EXPERIMENTAL DATA
X. Wang¹, J.Q. Kou¹, W.W. Zhang¹; ¹Northwestern Polytechnical University, China
  11:30 12:00 4.1.3 INVESTIGATION OF AERODYNAMIC INTERACTIONS BETWEEN NACA0012 AIRFOILS IN TANDEM
M. Li, No.2 High School of East China Normal University, China; H. Xu, Fudan University, China
Presenter: Muyao Li, No.2 High School of East China Normal University
Reserve Paper (Interactive) 4.1.R AERODYNAMIC ANALYSIS OF DRAGONFLY WINGS SPACE DISTRIBUTION ON THREE-DIMENSIONAL DURING HOVERING FLIGHT
T. Tang¹, Y. Yang¹, S. Song¹, L. Lang¹; ¹Northwestern Polytechnical University, China
5.1Composite Characterization and Fabrication
Chair: J. Jokinen
Track 5
04.1 - Material Issues, Fatigue and Damage Tolerance
  10:30 11:00 5.1.1 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
  11:00 11:30 5.1.2 IN-SITU LASER ASSISTED DIRECT IMPREGNATION, LAMINATION AND PLACEMENT OF CFRTP
T. Ikeda, Chubu University, Japan; Takeharu Sakai, Tottori University, Japan; A. Yokosu¹, Y. Fujii¹, H. Takenami¹, M. Arai¹, T. Ishikawa¹; ¹Nagoya University, Japan
  11:30 12:00 5.1.3 A TWO PHASES COUPLING FREE AND POROUS FLOW NUMERICAL SIMULATION METHOD OF LCM PROCESS
C. Chen, China; C. Chen, China; L.M. Gao, China; J.F. Xu, China
Presenter: Chen Li, COMAC Beijing Aircraft Technology Research Institut
6.1Cavity Flows
Chair: C. Breitsamter
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  10:30 11:00 6.1.1 COMPUTATIONAL STUDY OF THREE-DIMENSIONAL OPEN CAVITY FLOWS
Yong Luo, China; Conghai Wu, China; Siqi Yuan, China; Hao Tian, China; Hu Li, China; Shuhai Zhang, China
Presenter: Siqi Yuan
  11:00 11:30 6.1.2 EXPERIMENTAL STUDY ON SUPERSONIC CAVITY ACOUSTICS
M. Jiang¹, M. Wang¹, F. He¹; ¹AVIC Chengdu Aircraft Design & Research Institute, China
Presenter: MING WANG
7.1Aero Acoustics
Chair: Y. Zhang
Track 7
03.4 - Applied Aerodynamics
  10:30 11:00 7.1.1 SNGR BASED FAST ANALYSIS OF SLAT TRACK NOISE SOURCES
W.H. Wang, China; Q.C. Wang, China; C. Breard, China; Y.F. Sun, China
  11:00 11:30 7.1.2 AERODYNAMIC NOISE SIMULATION OF CIVIL AIRCRAFT LANDING GEARS BASED ON LES-SMARGORINSKY MODEL
Q. Li, Chinese Aeronautical Establishment, China; P. Wang ¹, B. Chen ¹; ¹AVIC Aerodynamics Research Institute, China
8.1Testing and Measurement
Chair:
Track 8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
  10:30 11:00 8.1.1 RESEARCH ON ATTITUDE CONTROL AND CONSTRAINT SYSTEM DESIGN OF FULL-SCALE AIRCRAFT STATIC TEST BASED ON BARYCENTER
J.-J. Zheng¹, B.-W. Wang¹, L.-G. Zhu, Shanghai Aircraft Design and Research Institute, China; J.-Y. Tang¹; ¹Aircraft Strength Research Institute of China, China
  11:00 11:30 8.1.2 DESIGN OF A VERTICAL DITCHING TEST
G. Nicolosi¹, F. Valpiani¹, G. Grilli¹, A. Saponaro Piacente¹, L. Di Ianni¹, E. Cestino¹, V. Sapienza¹, A. Polla, Aeronautical Consultant, Italy; P. Piana, TescoGo, Italy; ¹Politecnico di Torino, Italy
Presenter: Gabriele Nicolosi, Politecnico di Torino (DIMEAS)
  11:30 12:00 8.1.3 A SUBJECTIVE EVALUATION METHOD OF AIRCRAFT VIBRATION IN FLIGHT TEST
H. Wang, COMAC Flight test Center, China
Reserve Paper (Interactive) 8.1.R IMPROVED STOCHASTIC PERTURBATION ALGORITHM FOR GENERALIZED REPEATED EIGENVALUES PROBLEM BASED ON SURROGATE MODEL
H.-C Qiu¹, W.-C Fan¹, Y.-N Fang¹; ¹COMAC Shanghai Aircraft Manufacturing Co., Ltd., China
9.1Education and industry processes-Pitch talk
Chair: M. Kanerva
Track 9
14 - Education and Training
  10:30 11:00 9.1.1 THIS SESSION IS A PITCH TALK SESSION WITH 4 SPEAKERS
ICAS ECSC, Finland
  11:00 11:30 9.1.2 DEEP LEARNING BASED AUTOMATED AERIAL DOCKING SYSTEM J.CHOI, CAMBER MORPHING INLET MAKES AVIATION GREENER,J.P.EGUEA
ICAS ECSC, Finland
  11:30 12:00 9.1.3 NEW DRONE PARCEL DELIVERY SYSTEM, T.M.B.BASTOS, WAKE-BOUNDARY LAYER INTERACTION, V. VEERASAMY
ICAS ECSC, Finland
10.1Decoupling Control
Chair: Q. Wang
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  10:30 11:00 10.1.1 DECOUPLING CONTROL LAW DESIGN FOR OBLIQUE-WING AIRCRAFT BASED ON EIGENSTRUCTURE ASSIGNMENT AND MODEL FOLLOWING
L. Qiu, Chinese Flight Test Establishment, China; Z.H. Gao¹, Y. Liu¹; ¹Northwestern Polytechnical University, China
  11:00 11:30 10.1.2 A REDUNDANT ADAPTIVE NAVIGATION METHOD BASED ON DYNAMIC PERFORMANCE EVALUATION FOR AEROSPACE VEHICLE
T.-Y. Nie¹, R. Wang¹, J.-Y. Liu¹, Z. Xiong¹; ¹Nanjing University of Aeronautics and Astronautics, China
Presenter: Tingyu Nie, Nanjing University of Aeronautics and Astronautics
11.1Flight Operations
Chair:
Track 11
11 - Operations and Sustainment
  10:30 11:00 11.1.1 ON AIRCRAFT OPERATIONAL INTEGRITY
Yuting He, Air Force Engineering University, China
  11:00 11:30 11.1.2 INTEGRATION OF SPACE VEHICLE OPERATIONS INTO THE UNITED ARAB EMIRATES AIR TRAFFIC MANAGEMENT - AN IMPACT ANALYSIS
O. Lehmann¹, R. El-Jabi¹, K. Webster¹, A. Rachdi¹, Z. Malik¹; ¹Abu Dhabi University, United Arab Emirates
Presenter: Ramy El-Jabi, Abu Dhabi University
1.2China Session 2
Chair: Z.H. Gao
Track 1
12 - Host nation
  13:00 13:30 1.2.1 SHAPE MORPHING SMART STRUCTURES: MECHANICS, MATERIALS AND APPLICATIONS
L. Jinsong, China
  13:30 14:00 1.2.2 AN OVERVIEW OF HELICOPTER DEVELOPMENT IN CHINA AND SOME NEW HELICOPTER TECHNOLOGIES
X. Pinqi, China
  14:00 14:30 1.2.3 IMPLEMENTATION MECHANISM OF UAS INTEROPERABILITY BASED ON ARCHITECTURE META-MODEL
X.H Gao, /, China
2.2Rotorcraft & Seaplane
Chair: J. Melkert
Track 2
01 - Aircraft Design and Integrated Systems
  13:00 13:30 2.2.1 AERODYNAMIC AND STRUCTURAL MODELING IN THE ROTORCRAFT MULTI-PHYSICS SIMULATION VAST
J. Hofmann¹, M. Mindt¹, F. Weiss¹; ¹German Aerospace Center (DLR), Germany
  13:30 14:00 2.2.2 HELICOPTER FLIGHT DYNAMICS MODELLING WITH FREE-WAKE METHOD EMBEDDED FOR ROTOR ICING ANALYSES
G. Li, Chinese Aeronautical Establishment, China; G. Zhang¹, S. Chu¹; ¹Aviation Industry Development Research Center of China, China
Presenter: Guozhi Li, Chinese Aeronautical Establishment
  14:00 14:30 2.2.3 TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55X
L. Di Ianni¹, L. Loiodice¹, D. Celestini¹, D. Tiberti¹, C. Baldon¹, P. Iavecchia¹, A. Saponaro Piacente¹, M. Prodan¹, S. Grendene¹, B. Barberis¹, L. Santoro¹; ¹Politecnico di Torino, Italy
Presenter: Lucia Loiodice, Politecnico di Torino (DIMEAS)
3.2Avionics
Chair: N. Viola
Track 3
07 - Systems, Subsystems and Equipment
  13:00 13:30 3.2.1 DYNAMIC PERFORMANCE ANALYSIS AND WEIGHTED-BASED FAULT DIAGNOSIS SCHEME FOR AIRCRAFT ELECTRIC POWER SYSTEM
H. Li¹, Z. Zhao¹, Y. Zhang¹, S. Zhao¹, L. Xu¹; ¹Chengdu Aircraft Industrial (Group) Company Limited, China
  13:30 14:00 3.2.2 RESEARCH ON 18-PULSE AUTOTRANSFORMER RECTIFIER DEVICE FOR AVIATION
WX.-C. Chen¹, TY.-S. Sun¹, LX.-J. Jiang¹; ¹AVIC, China
  14:00 14:30 3.2.3 INTEGRATED ON-BOARD NETWORKS FOR NEXT GENERATION AVIONICS
E. Suvorova¹, V. Olenev¹; ¹St. Petersburg State University of Aerospace Instrumentation, Russia
Presenter: Elena Suvorova, St. Petersburg State University of Aerospace Instrumentation
Reserve Paper (Interactive) 3.2.R MEMS-BASED DISTRIBUTED NAVIGATION SYSTEM
Z. Liu¹, P. Chen¹, X. Wei¹; ¹Xi'an Flight Automatic Control Research Institute, China
4.2Unsteady Aerodynamics 2
Chair: T. Wan
Track 4
03.1 - Aerodynamics – CFD Methods and Validation
  13:00 13:30 4.2.1 NUMERICAL SIMULATIONS OF TRANSONIC BUFFET ON A HALF WING-BODY CONFIGURATION
F. Sartor¹, M. Martin¹, C. Riveiro Moreno¹, J. Dandois¹; ¹ONERA, France
  13:30 14:00 4.2.2 UNSTEADY FLOW SIMULATION AROUND MAIN LANDING GEAR USING HIERARCHICAL CARTESIAN GRID METHOD WITH IMMERSED BOUNDARY METHOD
T. Imamura, The University of Tokyo, Japan; Y. Tamaki, Tohoku University, Japan
  14:00 14:30 4.2.3 NUMERICAL SIMULATION OF A BIO-INSPIRED FLEXIBLE FLAPPING-WING BASED ON EXPERIMENTAL MEASURED DEFORMATION
X.-W. Yang¹, Y. Pei¹, W.-Q. Yang¹, P. Nian¹, B.-F. Song¹; ¹Northwestern Polytechnical University, China
Reserve Paper (Interactive) 4.2.R NUMERICAL SIMULATION OF SWEEPING MOTION EFFECTS ON THE HOVERING DRAGONFLIES
Z.C. Zhu¹, B.F. Song¹, W.Q. Yang¹, X.Y. Lang¹; ¹Northwestern Polytechnical University, China
Presenter: Zhichao Zhu, Northwestern Polytechnical University
5.2Dynamics and Noise
Chair: J. Bayandor
Track 5
04.1 - Material Issues, Fatigue and Damage Tolerance
  13:00 13:30 5.2.1 THE NOISE REDUCTION STUDY OF COMPOSITE ACOUSTIC LINER ON HIGH BYPASS RATIO TURBOFAN AEROENGINE
P. Hou¹, X.-J. Shang¹, Y. Dong¹; ¹Shenyang Aero Engine Research Institute, China
Presenter: peng hou, Shenyang Aero Engine Research Institute
  13:30 14:00 5.2.2 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
Reserve Paper (Interactive) 5.2.R RESEARCH ON FATIGUE STRENGTH PREDICTION MODEL OF AERO-ENGINE BLADES SUBJECTED TO FOREIGN OBJECT DAMAGE
L.F. Wang¹, L. Liu², C. Liu, Jiangsu Aero-XY Technology Co., Ltd, China; X.L. Pan¹, Z.H. Zhao², L.C. Zhou¹; ¹Air Force Engineering University, China ;²Nanjing University of Aeronautics and Astronautics, China
6.2Transition Physics 1
Chair: C. Atkin
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  13:00 13:30 6.2.1 VIBRATION INDUCED EXCITATION OF INSTABILITY WAVES IN A BLASIUS FLOW
E.R. Gowree, ISAE-SUPAERO, France; C.J. Atkin, University of East Anglia, United Kingdom
  13:30 14:00 6.2.2 STUDY ON THE STATISTICAL CHARACTERISTICS OF SKIN FRICTION OF SHOCK WAVE/ TURBULENT BOUDARY LAYER INTERATION IN A HOLLOW FLARE CONFIGURATION AT MACH 6
P.F. Shen ¹, hengyu Cai, School of Aeronautics, Northwestern Polytechnical University, China; Pengxin Liu¹, Dong Sun¹, Xianxu: Yuan¹; ¹State Key Laboratory of Aerodynamics, China
Presenter: Shen pengfei, State Key Laboratory of Aerodynamics
7.2Performance
Chair: J. Monk
Track 7
03.4 - Applied Aerodynamics
  13:00 13:30 7.2.1 ROBUST DESIGN OF 3D SHOCK CONTROL BUMPS TO TRANSPORT AIRCRAFT UNDER REALISTIC UNCERTAINTIES
C. Sabater¹, S. Goertz¹; ¹German Aerospace Center (DLR), Germany
Presenter: Christian Sabater, German Aerospace Center (DLR)
  13:30 14:00 7.2.2 DRAG REDUCTION ANALYSIS IN CLOSE-FORMATION FLIGHT
X.-X. Meng¹, M. Chang², J.-Q. Bai², M. Li¹; ¹School of Aeronautics, Northwestern Polytechnical University, China ;²Unmanned System Research Institute, Northwestern Polytechnical U, China
  14:00 14:30 7.2.3 INCREASING THE EFFECTIVENESS OF AN AERODYNAMICALLY BALANCED CONTROL SURFACE ON A MODIFIED AIRFOIL WITH REDUCED DRAG
V. Bogatyrev, TsAGI, Russia
8.2Aeroelasticity of Morphing Structures
Chair: M. Ritter
Track 8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
  13:00 13:30 8.2.1 STATIC AEROELASTIC TAILORING OF A HIGH-ASPECT-RATIO-WING FOR A SAILPLANE WITH A FORWARD MORPHING WING SECTION
F. Sturm¹, G. Illenberger¹, D. Techmer¹, M. Hornung¹; ¹Technical University of Munich, Germany
  13:30 14:00 8.2.2 AEROSERVOELASTIC OPTIMIZATION OF A HIGH ASPECT TRANSPORT WING WITH MORPHING TRAILING EDGE
Z.-K. Zhang¹, Y.-J. Yang¹, S. Ricci², A. De Gaspari², C. Song¹, C. Yang¹; ¹Beihang University, China ;²Politecnico di Milano, Italy
  14:00 14:30 8.2.3 A COMPREHENSIVE FRAMEWORK FOR THE COUPLED NONLINEAR AEROELASTIC AND FLIGHT DYNAMIC ANALYSES OF HIGHLY FLEXIBLE AIRCRAFT
C. Zhang¹, X.F. Li¹, J.W. Chen¹, Z. Zhou², L. Qiao²; ¹Xi'an Modern Control Technology Research Institute, China ;²Northwestern Polytechnical University, China
Presenter: Chi Zhang, Xi'an Institute of Modern Control Technology
9.2Combustion & Heat Transfer
Chair: P. Steczycki
Track 9
05 - Propulsion
  13:00 13:30 9.2.1 HYBRID IGNITION PROBABILITY METHOD TO PREDICT THE IGNITION PERFORMANCE OF A GAS TURBINE COMBUSTOR
W. Xiao, AECC Hunan Aviation Powerplant Research Institute, China; Y. Cheng, HUNAN MECHANICAL & ELECTRICAL POLYTECHNIC, China; K. Wang, Aero Engine Academy of China (AECC), China; Z. Ren, Tsinghua University, China
  13:30 14:00 9.2.2 LARGE-EDDY SIMULATION OF A SWIRLING AVIATION KEROSENE SPRAY FLAME USING 3-COMPONENT SURROGATE FUELS
K.D. Wan¹, Y.Z. Huang¹, Z.X. Gao¹, Y. He, Zhejiang University, China; C.W. Jiang¹; ¹Ningbo Institute of Technology, Beihang University, China
Reserve Paper (Interactive) 9.2.R INFLUENCE OF SHOCK TRAIN ON HEAT FLUX DISTRIBUTION OF ACIRCULAR CONSTANT-AREA ISOLATOR
X. Yang¹, Z.-W. Wang¹, Y.-B. Niu¹, H.-Y. Miao¹; ¹college of aerospace science and engineering,national university, China
10.2Robust Control
Chair: M. Naruoka
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  13:00 13:30 10.2.1 DECENTRALIZED CONFLICT DETECTION AND RESOLUTION METHOD ACCOUNTING FOR UNCERTAINTIES OF TRAJECTORIES
N. Yokoyama, National Defense Academy of Japan, Japan
  13:30 14:00 10.2.2 AN ALTERNATIVE BUT EQUIVALENT REALIZATION OF FINITE-HORIZON SUBOPTIMAL CONTROL FOR VEHICLE LANDING
S. Zhang, China; X. Du, China; F. Liao, China; J.T. Huang, China
11.2Operational Training
Chair:
Track 11
11 - Operations and Sustainment
  13:00 13:30 11.2.1 DESIGN OF SIMULATION-BASED PILOT TRAINING SYSTEMS USING MACHINE LEARNING AGENTS
J. Källström¹, R. Granlund, RISE SICS East, Sweden; F. Heintz¹; ¹Linköping University, Sweden
  13:30 14:00 11.2.2 A STUDY ON TRAINING NEEDS ANALYSIS (TNA) METHOD FOR MILITARY AIRCRAFT
Q. Wang¹, C. Sun¹, B. Hao¹; ¹ Chengdu Aircraft Design and Research Institute, AVIC, China
Presenter: CHEN SUN, Chengdu Aircraft Design and Research Institute, AVIC
  14:00 14:30 11.2.3 INFORMATION DISTRIBUTION METHOD FOR MULTI-AIRCRAFT COOPERATION BASED ON COLLABORATIVE FILTERING ALGORITHM
Y.H. WANG, China; Z.J. ZHAN, China; B. XUE, China; P.Y. DENG, China
Reserve Paper (Interactive) 11.2.R THE DATABASE DESIGN OF UNMANNED AERIAL VEHICLE
R.P. Liu, China; Q. Wang, China; G.Y. He, China; M.T. Tang, China; J.X. Ren, China
1.3Sino-French Session: MBSE and Digital Transformation
Chair: L. Li
Track 1
12 - Host nation
  15:00 15:30 1.3.1 TOWARDS AGILE SYSTEMS ENGINEERING: AN ITERATIVE & COLLABORATIVE APPROACH FOR COMPLEX SYSTEMS DEVELOPMENT
D. Krob, France
  15:30 16:00 1.3.2 DEPLOY SYSTEM ENGINEERING METHODS IN AIRBORNE GUIDANCE NAVIGATION CONTROL DOMAIN
F.F. Wu, FACRI, China
  16:00 16:30 1.3.3 MODEL BASED DESIGN AND PRACTICE FOR AVIONICS SYSTEM
L. Gao, /, China
2.3Digital Pioneering – Where will MBSE, AI, VR and SoSE bring engineering in 20 years?
Chair: B. Nagel
Track 2
15 - Guest lectures
  15:00 15:30 2.3.1 ICAS DIGITAL PIONEERING INITIATIVE AND FUTURE PERSPECTIVES ON MDO & MBSE
P.D. Ciampa, German Aerospace Center, Germany
  15:30 16:00 2.3.2 FUTURE PERSPECTIVES ON KBE & AI
G. La Rocca, Delft University of Technology, Netherlands
  16:00 16:30 2.3.3 FUTURE PERSPECTIVES ON VR & AR
S. Bagassi, University of Bologna, Italy
  16:30 17:00 2.3.4 FUTURE PERSPECTIVES ON SOSE
C. Jouannet, Saab, Sweden
3.3System Qualification and Testing
Chair: J. Fu
Track 3
07 - Systems, Subsystems and Equipment
  15:00 15:30 3.3.1 RESEARCH ON THE ENVIRONMENTAL WORTHINESS OF THE CIVIL AIRCRAFT USING THE FUZZY THEORY
H. Zhang¹, J.T. Wu¹, P.Q. Tian¹, Z.P. Ren¹; ¹Aircraft Strength Research Institute of China, China
  15:30 16:00 3.3.2 EXPERIMENTAL STUDY OF THE DYNAMICS CHARACTERISTICS OF AN IMPACT WATER DROPLET ON SUPERHYDROPHOBIC SURFACE
J.X. Wang¹, C.L. Zhu¹, Z. Yang¹, C.X. Zhu, Nanjing University of Aeronautics and Astronautics,, China; ¹Nanjing University of Aeronautics and Astronautics, China
  16:00 16:30 3.3.3 STUDY ON CLOSED-LOOP CROSS COMPENSATION CONTROL TECHNOLOGY IN ACCELERATED FATIGUE TESTING
H. ZHAO, Aircraft Strength Research Institute of China, Xi’an jiaotong Un, China; H. TAO¹, Z. GU, Chongqing Hongyu Precision Industrial Co., Ltd., China; G. SHI, Shenyang Aircraft Design & Research Institute of China, China; S. DUAN¹, J. FENG¹; ¹Aircraft Strength Research Institute of China, China
  16:30 17:00 3.3.4 RESEARCH AND VALIDATION OF SYSTEM MODELING AND SIMULATION OF INTAKE AIR MIXER ALTITUDE TEST BED
F. Wu, Northwestern Polytechnical,AECC Sichuan Gas Turbine Establishmen, China; X.-D. Feng¹, L.-T. Leng¹, T. Liu¹, C.-Q. Yang¹; ¹AECC Sichuan Gas Turbine Establishment, China
Presenter: FENG WU, Northwestern Polytechnical University
Reserve Paper (Interactive) 3.3.R A MANUFACTURING COST ESTIMATION MODEL WITH RELIABILITY FOR CIVIL AERO-ENGINE
X. Li¹, H.F. Wei¹, J.M. Wu¹, F. Liu¹; ¹ADR (Aviation Industry Development Research Center of China), China
4.3Turbulence Modeling
Chair: A. Viviani
Track 4
03.1 - Aerodynamics – CFD Methods and Validation
  15:00 15:30 4.3.1 ON THE ASSESSMENT OF CFD METHODS FOR VORTICAL FLOWS
R.C. Gonzalez, Cranfield Unversity, United Kingdom; S.A. Prince, Cranfield University, United Kingdom
  15:30 16:00 4.3.2 RESEARCH OF TURBULENCE MODELING BASED ON MACHINE LEARNING
Y.-H. Yin¹, Y.-F. Zhang¹; ¹Tsinghua University, China
  16:00 16:30 4.3.3 TURBULENCE MODEL ASSESSMENT OF THE SEPARATED FLOW IN THE STANFORD DIFFUSER
M. Bonnici¹, S. Prince¹, K. Garry¹; ¹Cranfield University, United Kingdom
  16:30 17:00 4.3.4 RESEARCH OF HYPERSONIC BOUNDARY LAYER INSTABILITY AND TRANSITION WITH THERMAL-CHEMICAL NON-EQUILIBRIUM EFFECTS
X.L. Chen¹, F. Song¹; ¹Tsinghua University, China
5.3Fatigue and Structural Integrity
Chair: J. van Doeselaar
Track 5
04.1 - Material Issues, Fatigue and Damage Tolerance
  15:00 15:30 5.3.1 STUDY OF COMPOSITE SKIN-STRINGER FATIGUE BEHAVIOR UNDER BROADBAND RANDOM VIBRATION
S. Dubinskii¹, F. Sevastyanov¹, V. Kostenko¹, S. Denisov¹, I. Zharenov¹; ¹The Central Aerohydrodynamic Institute (TsAGI), Russia
  15:30 16:00 5.3.2 MODEL CURVES: A SIMPLE WAY TO ACCOUNT FOR COMPLEX EFFECTS
A. Bautin¹, Y. Svirsky¹, V. Basov¹, Y. Melnikov¹; ¹1Central Aerohydrodynamic Institute (TsAGI), Russia
Presenter: Bautin Andrey, 1Central Aerohydrodynamic Institute (TsAGI)
  16:00 16:30 5.3.3 A DIGITAL EQUIVALENT DEVELOPMENT FOR FATIGUE AND DAMAGE TOLERANCE IN AIRCRAFT STRUCTURES
L. Zaplana Manzano¹, J. Romero Arana¹, J. Gómez-Escalonilla Martín¹; ¹AIRBUS DS, Spain
  16:30 17:00 5.3.4 FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSURE
S. Olsson, Quintus Technologies AB, Sweden; B. Carlsson¹, M. Bergkvist, Quintus Teachnologies AB, Sweden; R. He¹; ¹Quintus Technologies, China
Presenter: He Lei, Quintus Technologies
Reserve Paper (Interactive) 5.3.R STUDY ON THE FATIGUE SCATTER FACTOR UNDER SEVERE LOAD SPECTRUM
Y.J. Wang¹, Y. Liao¹, H. Dui¹, J. Dong¹; ¹Chengdu Aircraft Design and Research Institute, China
6.3Flow Control Applications
Chair: R. Gowree
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  15:00 15:30 6.3.1 HIGH-LIFT NOISE REDUCTION USING PLASMA ACTUATORS
G.P.G. Silva¹, J.P. Eguea¹, J.A.G. Croce, Federal Institute of Education, Science and Technology of São Pa, Brazil; F.M. Catalano¹; ¹Department of Aeronautical Engineering, University of São Paulo, Brazil
  15:30 16:00 6.3.2 ENERGY HARVESTING FROM PIEZOELECTRIC FRINGES AT THE TRAILING-EDGE OF A FINITE WING WITH LEADING-EDGE TUBERCLES
E.P. Pereira¹, A. Esmaeili, Ferdowsi University of Mashhad, Iran; J.M.M. Sousa¹; ¹Instituto Superior Técnico, Portugal
  16:00 16:30 6.3.3 SUBSONIC WIND TUNNEL SMALL RIBLETS DRAG REDUCTION EXPERIMENT ON C919 FUSELAGE MODEL
H.W. Wang¹, Z. Huang¹, M.L. Yuan¹, X.H. Li¹, M. Zhang, Shanghai Aircraft Design and Research Institute, China; ¹China Academy of Aerospace Aerodynamics, China
  16:30 17:00 6.3.4 HYBRID LAMINAR FLOW CONTROL (HLFC) RESEARCH AT AIRCRAFT RESEARCH ASSOCIATION (ARA), PAST, PRESENT AND FUTURE
P.W.C. Wong, IHS Markit ESDU, United Kingdom; M. Maina¹, S. Lawson¹; ¹ARA, United Kingdom
Presenter: Peter Wong, IHS Markit ESDU
7.3Propulsion Airframe Integration
Chair:
Track 7
03.4 - Applied Aerodynamics
  15:00 15:30 7.3.1 PROPELLER WAKE - OBJECT INTERACTION USING A FREE WAKE MODEL UTILIZING LOCAL MESH SEPARATION
M. Thiele¹, D. Salassidis¹, M. Hornung¹; ¹Institute of Aircraft Design, Technical University of Munich, Germany
  15:30 16:00 7.3.2 NUMERICAL STUDY OF QUAD-ROTOR AIRCRAFT PERFORMANCE UNDER ADVERSE SITUATIONS
T.W. Wan¹, M.-H. Tsai¹; ¹Tamkang Univ., Taiwan, China
  16:00 16:30 7.3.3 AERODYNAMIC ANALYSIS OF A HIGH SPEED TEST RIG FOR USE IN ENGINE TEST FACILITIES
F. Rasimarzabadi¹, M. Neuteboom¹, C. Clark¹, H. Martensson, GKN Aerospace Engine Systems, Sweden; ¹NRC, Canada
8.3Impact
Chair: J. Han
Track 8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
  15:00 15:30 8.3.1 BIRD STRIKE SIMULATIONS IN MSC.SOFTWARE: CORRELATION BETWEEN THE EXPERIMENTS AND SIMULATIONS
V. Symonov¹, J. Juracka¹; ¹Brno University of Technology, Czech Republic
  15:30 16:00 8.3.2 MODELS AND METHODS FOR DRONE STRIKE LOAD PREDICTIONS
F. Franke¹, U. Burger¹, C. Hühne, DLR, Germany; ¹Technische Hochschule Ingolstadt, Germany
  16:00 16:30 8.3.3 EXPERIMENTAL STUDY ON ATTENUATION PERFORMANCE OF SHOCK-ABSORBING INSERT
H.-S. Park¹, D.-H. Hwang¹, J. Yang, University of Washington, United States; J.-H. Han¹; ¹KAIST, South Korea
  16:30 17:00 8.3.4 REVIEW OF PREDICTIVE METHODS FOR CAPTURING ONSET OF DAMAGE AND INITIAL DELAMINATION IN CARBON FIBRE REINFORCED POLYMER LAMINATES SUBJECT TO IMPACT
H. Raza¹, O. Rodera Garcia², K. Carpenter¹, T. Pärnänen², J. Jokinen², M. Kanerva², J. Bayandor¹; ¹CRASH Lab, University at Buffalo, United States ;²Tampere University , Finland
Presenter: Hasan Raza, University at Buffalo - The State University of New York
9.3Controls & Software
Chair: S. Remy
Track 9
05 - Propulsion
  15:00 15:30 9.3.1 THE USE OF SOFTWARE “VIRTUAL ENGINE” FOR TIMELY GAS-TURBINE ENGINE FAULT LOCALIZATIONS
F.D. Golberg¹, M.P. Sokolov¹, V.E. Volkov¹, A.A. Petukhov¹; ¹Central Institute of Aviation Motors, Russia
  15:30 16:00 9.3.2 AN IMPROVED IDENTIFICATION METHOD FOR ACTUATOR LOOPOF AIRCRAFT ENGINE CONTROL SYSTEM
N. Liu, Shanghai Aircraft Design & Research Institute, Commercial Aircra, China
  16:00 16:30 9.3.3 METHODS OF PROGRAMMED THRUST MANAGEMENT FOR NOISE REDUCTION OF SUPERSONIC CIVIL AIRCRAFT
A. Mirzoyan¹, I. Khaletskii¹; ¹CIAM, Russia
  16:30 17:00 9.3.4 RESEARCH ON CIVIL AIRCRAFT POWERPLANT SYSTEM EICAS MESSAGES DESIGN METHOD
SHANG Yang, Shanghai Aircraft Design and Research Institute, China
10.3Design architecture & integration methodology
Chair: J. Vian
Track 10
02 - Systems Engineering and Integration
  15:00 15:30 10.3.1 SYSTEM ARCHITECTING: THE ARCHITECTURE DESIGN PROBLEM AS A GRAPH
J.H. Bussemaker¹, P.D. Ciampa¹, B. Nagel¹; ¹DLR, Germany
  15:30 16:00 10.3.2 AIRCRAFT CRUISE PERFORMANCE DESIGN INTEGRATION BASED ON SYSTEM ENGINEERING
HE BIHAI¹, HUA ZHEN¹; ¹COMAC, China
  16:00 16:30 10.3.3 RESEARCH ON AERO-ENGINE COLLABORATIVE DESIGN PROCESS BASED ON SYSTEM ENGINEERING
Y.-G. Chai¹, J. Tao¹, S.-P. Guo¹; ¹AECC Commercial Aero Engine co. LTD, China
  16:30 17:00 10.3.4 STRATEGIES TO ENHANCE CONFIGURATIONS FOR HIGH-PRECISION MULTI-DISCIPLINARY OPTIMIZATION
H. Liu¹, M. Li¹, R. zhu¹, L. Zhou, Beijing Institute of Technology, China; ¹Science and Technology on Electro-optic Control Laboratory, China
Reserve Paper (Interactive) 10.3.R THE CIVIL AIRCRAFT DEVELOPMENT PROJECT RISK MANAGEMENT RESEARCH
W. Bin¹, Q. Xudong¹; ¹NUAA, COMAC SADRI, China
11.3Safety and Security Analysis
Chair: D. Waller
Track 11
10 - Safety and Security
  15:00 15:30 11.3.1 RESEARCH ON SAFETY ASSESSMENT APPROACH FOR UAS OPERATIONS OVER UNINHABITED AREAS
QIAN ZHANG, Northwestern Polytechnical University, China
  15:30 16:00 11.3.2 EXPERIMENTAL STUDY ON CRITICAL HEAT FLUX CHARACTERISTICS OF R134A FLOW BOILING IN A HORIZONTAL 2.1 MM TUBE UNDER HYPERGRAVITY
J.J. Han, Nanjing engineering Institute of Aircraft System, Jincheng, AVIC, China; G. Li, Nanjing University of Aeronautics and Astronautics, China
  16:00 16:30 11.3.3 ULTRASONIC DE-ICING SYSTEM DESIGN METHODS BASED ON RESONANCE AND IMPEDANCE MATCHING
B. Miao¹, M.-X. Bao¹, C.-L. Zhu¹; ¹Nanjing University of Aeronautics and Astronautics, China
  16:30 17:00 11.3.4 A NUMEIRCAL PREDICTION OF THE AIRCRAFT ICING METEOROLOGICAL ENVIRONMENT
Q.-L. Guo¹, W.-M. Sang¹, J.-J. Niu¹, A.-X. Qiu¹; ¹Northwestern Polytechnical University, China
Reserve Paper (Interactive) 11.3.R AN INTEGRATED METHOD FOR ACCURATE IDENTIFICATION AND DYNAMIC MONITORING OF BUILDINGS IN AERODROME OBSTACLE FREE SPACE
K. Tong¹, Y. Song¹, X.-F. Kong¹, K.-W. Zhang¹, Z.-J. Chen¹; ¹Civil Aviation University of China, China
1.4Design Optimization under Uncertainty
Chair: M. Padulo
Track 1
01 - Aircraft Design and Integrated Systems
  08:00 08:30 1.4.1 APPLICATION OF ARTIFICIAL NEURAL NETWORKS FOR EFFICIENT RELIABILITY-BASED DESIGN OPTIMIZATION
X. Chen¹, A. Riaz¹, S. El Fassi¹; ¹Cranfield University, United Kingdom
  08:30 09:00 1.4.2 VALIDATING SURROGATE MODELS AND ICORPORATING UNCERTAINTY QUANTIFICATION IN MULTI-ELEMENTS AIRFOIL DESIGN OPTIMISATION
D. Di Pasquale¹, C Bolart¹; ¹Cranfield University, United Kingdom
Presenter: Carles Bolart, Cranfield University
  09:00 09:30 1.4.3 EFFICIENT ADAPTIVE SURROGATE-BASED OPTIMIZATION USING FUZZY CLUSTERING FOR COMPLEX SYSTEM OPTIMIZATIONS
C. Li¹, W. Ji¹, C. Gong¹, H. Fang, Shanghai Electro-Mechanical Engineering Institute, China; ¹Northwestern Polytechnical University, China
  09:30 10:00 1.4.4 A NOVEL RBF DATA TRANSFER METHOD BASED ON PCA GEOMETRIC FEATURE EXTRACTION
S.S. Liu¹, Q. You¹, Z. Liu², X. Liu², Y.W. Gui²; ¹State Key Laboratory of Aerodynamics, China ;²China Aerodynamics Research and Development Center, China
Presenter: Qi You
2.4Hypersonics
Chair: B. Kimmel
Track 2
01 - Aircraft Design and Integrated Systems
  08:00 08:30 2.4.1 H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS
N. Viola¹, R. Fusaro¹, D. Ferretto¹, O. Gori¹, B. Saracoglu², A.C. Ispir², C. Schram², V. Grewe³, J.F. Plezer³, J. Martinez³, M. Marini*, L. Cutrone*, G. Saccone*, S. Hernandez, University of La Coruna, Spain; K. Lammers, Netherlands Aerospace Centre, Netherlands; A. Vincent, The French Aerospace Lab ONERA, France; D. Hauglustaine, CNRS, France; B. Liebhardtº, F. Linkeº, D. Bodmerº; ¹Politecnico di Torino, Italy ;²Von Karman Institute for Fluid Dynamics, Belgium ;³Deutsches Zentrum für Luft- und Raumfahrt, Germany ;*Centro Italiano Ricerche Aerospaziali, Italy ;ºTechnical University of Hamburg Harburg, Germany
  08:30 09:00 2.4.2 THERMAL PROTECTION SYSTEM PRELIMINARY DESIGN OF STRATOFLY HIGH-SPEED PROPELLED VEHICLE
R. Scigliano¹, V. De Simone¹, M. Marini¹, R. Fusaro², D. Ferretto², N. Viola²; ¹Italian Aerospace Research Centre (CIRA), Italy ;²Politecnico di Torino (PoliTO), Italy
Presenter: Roberta Fusaro, Politecnico di Torino (PoliTo)
  09:00 09:30 2.4.3 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
  09:30 10:00 2.4.4 INTEGRATION OF AN INCREASING-FIDELITY AERODYNAMIC MODELLING APPROACH IN THE CONCEPTUAL DESIGN OF HYPERSONIC CRUISER
R. Fusaro¹, O. Gori¹, D. Ferretto¹, N. Viola¹, P. Roncioni², M. Marini²; ¹Politecnico di Torino, Italy ;²CIRA, Italy
Presenter: Oscar Gori, Politecnico di Torino
3.4UAV Dynamics and Control 1
Chair: P. Krus
Track 3
06.2 - Flight Dynamics and Control (UAV related)
  08:00 08:30 3.4.1 MUMULTIROTOR VEHICLES DESIGN BASED ON DYNAMIC MANIPULABILITY FOR UNDERACTUATED FLYING SYSTEMS
Y. Matsumura¹, M. Bando¹, S. Hokamoto¹; ¹Kyushu Univ., Japan
  08:30 09:00 3.4.2 LANDING SYSTEM USING EXTENDED DYNAMIC WINDOW APPROACH FOR FIXED-WING UAV
S. Ishioka¹, K. Uchiyama¹, K. Masuda¹; ¹Nihon University, Japan
  09:00 09:30 3.4.3 OPTIMIZATION OF LONGITUDINAL CONTROL OF AN AGRICULTURAL UAV USING LQR-PID CONTROL
A. Gomes Pereira Sarmento¹, A. Giacobini de Souza¹, A. Muniz Neves, CENIC Aeronáutica, Brazil; L.C. Sandoval Góes¹, R. Gil Annes da Silva¹; ¹Instituto Tecnológico de Aeronáutica (ITA), Brazil
4.4Aerodynamic Optimization
Chair: D. Zingg
Track 4
03.1 - Aerodynamics – CFD Methods and Validation
  08:00 08:30 4.4.1 MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF A CIVIL AIRCRAFT FUSELAGE
Seyed Vahidreza Rohani¹, Alireza Jahangirian¹; ¹Amirkabir University of Technology, Iran
  08:30 09:00 4.4.2 OPTIMISATION OF VORTEX GENERATORS FOR STALL SPEED REDUCTION
J. Meyer¹, P.M. Okfen¹, C. Bil¹; ¹RMIT University, Australia
  09:00 09:30 4.4.3 MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF A CIVIL AIRCRAFT WINGLET
M. Heidari Soreshjani, Amirkabir University of Technology, Iran; A. Jahangirian, Amirkabir university of technology, Iran
Presenter: Alireza Jahangirian, Amirkabir University of Technology
  09:30 10:00 4.4.4 OPTIMAL DESIGN OF A NEXT GENERATION HIGH-LIFT REUSABLE RE-ENTRY VEHICLE
A. Aprovitola, University of Campania , Italy; L. Iuspa¹, G. Pezzella¹, A. Viviani¹; ¹University of Campania, Engineering Department., Italy
5.4Air Traffic Efficiency
Chair: D. Nguyen
Track 5
09 - Air Transport System Efficiency
  08:00 08:30 5.4.1 IMPACT OF ENROUTE TIME-BASED METERING ON EQUITY IN DELAY DISTRIBUTION
Adriana Andreeva-Mori¹, Yoshinori Matsuno¹; ¹Japan Aerospace Exploration Agency, Japan
  08:30 09:00 5.4.2 ARTIFICIAL INTELLIGENCE AND HUMAN-MACHINE INTERACTIONS
P. Lertworawanich¹, N. Pongsakornsathien¹, Y Xie¹, A. Gardi¹, R. Sabatini¹; ¹RMIT University, Australia
Presenter: Yibing Xie, RMIT University
  09:00 09:30 5.4.3 RESEARCH ON TRAJECTORY OPTIMIZATION TECHNOLOGY CONSIDERING METEOROLOGICAL INFORMATION PREDICTION
W. Guo¹, R.Y. Zhang¹; ¹China National Aeronautical Radio Electronics Research Institute, China
  09:30 10:00 5.4.4 POINT MERGE SYSTEM AND ARRIVAL METERING SYNERGY EFFECT ESTIMATION OF INBOUND FLIGHT EFFICIENCY AT TOKYO INTERNATIONAL (HANEDA) AIRPORT
T. Mori, Osaka Prefecture University, Japan
6.4Developments in Modelling
Chair: E. Stumpf
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  08:00 08:30 6.4.1 EXPERIMENTAL INVESTIGATION, NUMERICAL AND MATHEMATICAL SIMULATION OF DISPERSE FLOWS IMPINGING ON AIRCRAFT SURFACE
I.A. Amelyushkin¹, M.A. Kudrov¹, A.B. Miller¹, Y.F. Potapov¹, A.L. Stasenko¹, V.A. Zhbanov¹; ¹Central Aerohydrodynamic Institute, Russia
  08:30 09:00 6.4.2 MODIFICATION OF TURBULENCE MODELS FOR PRESSURE-INDUCED SEPARATION ON SMOOTH SURFACES USING THE DLR VICTORIA EXPERIMENT
T. Knopp¹, M. Novara¹, D. Schanz¹, W. Lühder¹, E. Schülein¹, R. Geisler¹, F. Philipp¹, M. Schroll², A. Krumbein¹, C. Willert², A. Schröder¹; ¹DLR AS, Germany ;²DLR AT, Germany
Presenter: Tobias Knopp, DLR AS CAS
  09:00 09:30 6.4.3 SINGULARITIES IN THE NEAR-WALL REGION OF 3D BOUNDARY LAYER AND THE FLOW STRUCTURE IN ITS VICINITY
V.I. Shalaev, Moscow Institute of Physics and Technology, Russia
7.4Configurations
Chair: F. Collier
Track 7
03.4 - Applied Aerodynamics
  08:00 08:30 7.4.1 INTAKE BOUNDARY LAYER PROFILE ESTIMATION FOR BLI PERFORMANCE PREDICTION ON A BLENDED WING BODY
K. Ma¹, S. Prince¹; ¹Cranfield University, United Kingdom
Presenter: Simon Prince, Cranfield University
  08:30 09:00 7.4.2 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
  09:00 09:30 7.4.3 AN OPTIMIZATION OF ANTI-ICING CHAMBER BASED ON POD AND KRIGING
J. Niu¹, W. Sang¹, A. Qiu¹, Q. Guo¹, D. Li¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
  09:30 10:00 7.4.4 NUMERICAL INVESTIGATION OF THE EFFECT OF WALL TEMPERATURE ON THERMAL ENVIRONMENT OF TWO-DIMENSIONAL TRANSVERSE GAP
B. Qiu, State Key Laboratory of Aerodynamics, China Aerodynamic Research, China; R. Li, Computational Aerodynamics Institute China Aerodynamic Research, China; X. Liu¹, J. Yao¹, B. Jiang¹, Y. Zhu, School of Chemical Engineering, China; ¹Computational Aerodynamics Institute, China Aerodynamic Research, China
Presenter: Zhu Yuanhao, Sichuan University
8.4Computational Aeroelasticity
Chair: W. Luber
Track 8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
  08:00 08:30 8.4.1 COMPUTATIONAL FLUID-STRUCTURE INTERACTIONS OF A 3D FLEXIBLE FLAPPING WING
Y. Guo¹, W. Yang¹, Y. Dong¹, X. Lang¹; ¹Northwestern Polytechnical University, China
Presenter: Yueyang Guo, Northwestern Polytechnical University
  08:30 09:00 8.4.2 FLUID-STRUCTURE INTERACTION ANALYSIS OF ELASTIC EFFECTS OF A TRANSPORT AIRCRAFT FITTED WITH WINGLETS
W.M. Alves, Embraer, Brazil; B.S. Mattos¹, J.A. Hernandes¹; ¹ITA, Brazil
Presenter: William Alves, Embraer
  09:00 09:30 8.4.3 EFFECTS OF ELASTICITY, VISCOSITY AND BOUNDARY LAYER TRANSITION ON AEROELASTICITY CHARACTERISTICS OF LAMINAR WINGS
S. Kuzmina¹, F. Ishmuratov¹, O. Karas¹; ¹TsAGI, Russia
  09:30 10:00 8.4.4 AEROELASTIC RESPONSE CALCULATION USING DUHAMEL INTEGRAL AND ITS APPLICATIONS
L. Bortolotto¹, R.G.A. Silva¹, M.H.J. Pedras, Embraer, Brazil; ¹Instituto Tecnológico de Aeronáutica, Brazil
Reserve Paper (Interactive) 8.4.R SUPERSONIC AEROELASTIC ANALYSIS OF AN ALL-MOVABLE WING WITH FREE PLAY
K. Yuan¹, M. Cheng¹; ¹Beijing Electro-Mechanical Engineering Institute, China
Presenter: Meng Cheng
9.4Fan / Nacelle & Propeller 1
Chair: A. Mirzoyan
Track 9
05 - Propulsion
  08:00 08:30 9.4.1 DESIGN AND PERFORMANCE OF A LOW FAN-PRESSURE-RATIO PROPULSION SYSTEM
R. Schnell, German Aerospace Center (DLR), Germany; E. Goldhahn, Airbus Operations GmbH, Germany; M. Julian, Airbus Operations SAS, France
Presenter: Rainer Schnell, German Aerospace Center (DLR)
  08:30 09:00 9.4.2 ANALYSIS OF AERODYNAMIC CHARACTERISTICS OF PROPELLER AT LOW ADVANCE RATIO USING A WHIRING ARM
Y. Itoh¹, A. Satoh¹; ¹Iwate university, Japan
  09:00 09:30 9.4.3 EXPERIMENTAL STUDIES OF SLOT-TYPE CASING TREATMENTS FOR MODEL FANS WITH THE AIM OF AERODYNAMIC AND ACOUSTIC IMPROVEMENTS
V. Mileshin¹, S. Markov¹, V. Korzhnev¹, I. Pochkin¹; ¹CIAM, Russia
  09:30 10:00 9.4.4 ANALYSIS OF THRUST-SCALED ACOUSTIC EMISSIONS OF AIRCRAFT PROPELLERS AND THEIR DEPENDENCE ON PROPULSIVE EFFICIENCY
X. Geng¹, T. Hu¹, P. Liu¹, T. Sinnige², G. Eitelberg²; ¹Beihang University, China ;²Delft University of Technology, Netherlands
Presenter: Xin Geng
Reserve Paper (Interactive) 9.4.R THE RESEARCH ON PROPELLER NOISE PREDICTION METHOD FOR TURBOPROP AIRCRAFT
C. Hu¹, J. Gu¹, F. Gao¹; ¹AVIC The First Aircraft Institute, China
10.4System Architecture
Chair:
Track 10
02 - Systems Engineering and Integration
  08:00 08:30 10.4.1 ARCHITECTURE INTEGRATION OF FUTURE ATM SYSTEM BASED ON META-MODEL
J. Wang¹, J. Mao¹, Q. Zhou¹; ¹Chinese Aeronautical Radio and Electronics Research Institute, China
  08:30 09:00 10.4.2 TECHNOLOGY ROADMAPS FOR THE DEVELOPMENT OF FUTURE HIGH-SPEED TRANSPORTATION SYSTEMS
V. Vercella¹, R. Fusaro¹, N. Viola¹; ¹Politecnico di Torino, Italy
Presenter: Valeria Vercella, Politecnico di Torino
  09:00 09:30 10.4.3 ARCHITECTURE OF PRODUCT RESEARCH AND DEVELOPMENT SYSTEM FOR COMPLICATED PRODUCTS ENGINEERING
L. Su¹, H. Zhou¹, Y. Cheng¹, L. Du¹; ¹AEAC, China
  09:30 10:00 10.4.4 GREENER ATM SYSTEM ARCHITECTURE RESEARCH BASED ON COMPLEX SYSTEM ENGINEERING METHOD
H. Hu¹, J. Mao¹, D. Hu¹; ¹China Aeronautical Radio Electronics Research Institute, China
Reserve Paper (Interactive) 10.4.R CREATING A MULTI-FUNCTIONAL EXPERT ANALYTICAL SYSTEM IN THE AIRCRAFT INDUSTRY AND THE FORMATION OF GENERAL REQUIREMENTS
V.I. Budzko, FRC, Russia; A.V. Kan¹, G.G. Kazarinov¹, I.S. Mikhalyn ¹; ¹NRC Zhukovsky, Russia
11.4ATC, Pilot & Controller
Chair: H. de Jong
Track 11
10 - Safety and Security
  08:00 08:30 11.4.1 ATTENTION: TARGET AND ACTUAL - THE CONTROLLER FOCUS
J. Rataj¹, O. Ohneiser¹, G. Marin², R. Postaru²; ¹DLR, Germany ;²ROMATSA, Romania
  08:30 09:00 11.4.2 ANALYSIS OF PILOT OPERATIONAL STRATEGY DIFFERENCE USING NEURAL NETWORK
R. Mori, Electronic Navigation Research Institute, Japan
  09:00 09:30 11.4.3 OBJECTIVE MEASUREMENT OF HUMAN FACTORS FOR SUPPORTING THE OPERATOR’S LOAD SIMULATION AND MANAGEMENT
U. Kale¹, O. Alharasees¹, F. Kling, Research, Development and Simulation Department, HungaroControl, Hungary; D. Rohacs¹; ¹Budapest University of Technology and Economics, Hungary
Presenter: Utku Kale, Budapest University of Technology and Economics
  09:30 10:00 11.4.4 MACHINE LEARNING ENABLED TURBULENCE PREDICTION USING FLIGHT DATA FOR SAFETY ANALYSIS
M. Emara¹, M. dos Santos¹, N. Chartier¹, J. Ackley¹, T.G. Puranik¹, A. Payan¹, M. Kirby¹, O.J. Pinon¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States
Presenter: Mariam Emara, Georgia Institute of Technology
1.5Hybrid/Electric & Unconventional Aircraft 1
Chair: P. Prakasha
Track 1
01 - Aircraft Design and Integrated Systems
  10:30 11:00 1.5.1 PRELIMINARY DESIGN AND EXPERIMENTAL INVESTIGATION OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT
Y. Ma¹, W. Zhang¹, Y. Zhang¹, Y. Ma¹, Z. Bai¹; ¹Northwestern Polytechnical University, China
Presenter: Yiyuan Ma
  11:00 11:30 1.5.2 UNMANNED FIRE-FIGHTING AMPHIBIOUS AIRCRAFT WITH DISTRIBUTED TURBOELECTRIC PROPULSION SYSTEM
A.N. Varyukhin¹, M.A. Ovdienko¹, A.V. Vlasov, Central Institute of Aviation Motors, Russia; V.S. Zakharchenko¹; ¹CENTRAL INSTITUTE OF AVIATION MOTORS, Russia
  11:30 12:00 1.5.3 VALIDATION OF AN AERODYNAMIC MODEL FOR THE ANALYSIS OF SUBSCALE TEST AIRCRAFT WITH DISTRIBUTED ELECTRICAL PROPULSION
O. Luderer¹, M. Jünemann¹, F. Thielecke¹; ¹Hamburg University of Technology, Germany
2.5Cost Assessment
Chair: S. Bagassi
Track 2
01 - Aircraft Design and Integrated Systems
  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
  11:00 11:30 2.5.2 BASED ON THE CHARACTERISTIC PARAMETERS ESTIMATE MANUFACTURING COST FOR COMPOSITE STRUCTURES
H. Feng¹, F. Liu¹, H.F. W.¹, J.M. Wu¹; ¹Aviation industry Development Research Center of China, China
  11:30 12:00 2.5.3 ASSESSMENT OF NEW TECHNOLOGIES IN A MULTI-DISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION ENVIRONMENT INCLUDING RAMS AND COST DISCIPLINES
C. Cabaleiro¹, M. Fioriti¹, L. Boggero², S. Corpino¹, P.D. Ciampa², B. Nagel²; ¹Politecnico di Torino, Spain ;²German Aerospace Center (DLR), Germany
3.5UAV Conflict Avoidance
Chair: C. Bil
Track 3
06.2 - Flight Dynamics and Control (UAV related)
  10:30 11:00 3.5.1 AUTONOMOUS CONFLICT RESOLUTION ALGORITHM BASED ON ELLIPTIC GEOMETRY
S.S. Rawikara¹, R.A. Sasongko¹, S.A. Munthahar¹; ¹Institut Teknologi Bandung, Indonesia
Presenter: Sayid Munthahar, Institut Teknologi Bandung
  11:00 11:30 3.5.2 A NOVEL DETECT-AND-AVOID APPROACH FOR UAS IN URBAN ENVIRONMENTS
S. Bijjahalli¹, A. Gardi¹, S. Hilton¹, R. Sabatini¹; ¹RMIT University, Australia
  11:30 12:00 3.5.3 MULTI-UAV TRAJECTORY PLANNING BASED ON COORDINATION VARIABLES
X.Z. Zheng¹, S.H. He¹, D.L. Lin¹; ¹Beijing Institute of Technology, China
4.5Flows with Thermal Effects
Chair: Z. Gao
Track 4
03.1 - Aerodynamics – CFD Methods and Validation
  10:30 11:00 4.5.1 EFFECT OF DROPLET MVD ON ICING COLLECTION EFFICIENCY FOR A HELICOPTER BLADE
W.B. Li¹, K.C. Li, Aviation Industry Corporation of China, China; C. Song¹, H.L. Ma¹, Y.Y. Wang¹; ¹China Aerodynamics Research and Development Center, China
  11:00 11:30 4.5.2 NUMERICAL SIMULATION OF RIDGE ICE AND AERODYNAMIC EFFECT UNDER THERMAL ANTI-ICE
L.B. Guo¹, G.Z. Cao, Nanjing University of Aeronautics and Astronautics, China; H.P. Zhang¹; ¹Shanghai Aircraft Design and Research Institute, China
  11:30 12:00 4.5.3 COUPLED HEAT TRANSFER CHARACTERISTICS ON CHEMICALLY REACTING INTERFACE OF HIGH-SPEED AIRCRAFT CONSIDERING WALL INJECTION
Q. You¹, X.-F. Yang¹, L. Zeng¹, Y.-W. Gui¹, Y.-X. Du¹, L. Liu¹, G.-M. Xiao¹; ¹China Aerodynamics Research and Development Center, China
Reserve Paper (Interactive) 4.5.R FLOW AND HEAT TRANSFER MECHANISM OF JET IMPINGEMENT COOLING ONTO MID-CHORD REGION OF TWISTED BLADE
W. Jin¹, S.-E. Peng¹, J.-M. Wu¹, J. Lei¹, W.-T. Ji¹; ¹Xian Jiaotong University, China
Presenter: Wei Jin, Xi'an Jiaotong University
5.5Airport/Aircraft Operation
Chair: E. Itoh
Track 5
09 - Air Transport System Efficiency
  10:30 11:00 5.5.1 ERAS- EVALUATION OF REALISTIC APPROACH SCENARIOS FOR MINIMAL NOISE - PRELIMINARY FINDINGS
B. Moberg, Vernamack AB, Sweden; P. Näsman, KTH Royal Institute of Technology, Sweden; U. Ziverts, Infobahn AB, Sweden
  11:00 11:30 5.5.2 A NOVEL APPROACH FOR TURNAROUND TIME ALLOCATION BASED ON REINFORCEMENT LEARNING
A. Rodriguez-Sanz, Universidad Politecnica de Madrid (UPM), Spain; J. Herrera de la Cruz , Universidad Complutense de Madrid (UCM), Spain
6.5Turbulent Flows
Chair: C. Breitsamter
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  10:30 11:00 6.5.1 EFFECTS OF ADVERSE PRESSURE GRADIENT ON THE BEHAVIOURS OF RESOLVENT MODE
C. Chen, China; J.-T. Huang, China; X. Chen, China
  11:00 11:30 6.5.2 NUMERICAL SIMULATION STUDY ON BOUNDARY LAYER FLOW AND DRAG REDUCTION CHARACTERISTICS OF RIBLETS
S.Y. Du¹, R. Pang, AVIC Xi’an Flight Automatic Control Research Institute, China; W.M. Sang¹, G.J. Yang¹; ¹Northwestern Polytechnical University, China
  11:30 12:00 6.5.3 STUDY ON THE HEAT FLUX OF HYPERSONIC SHOCK WAVE BOUNDARY LAYER INTERACTION CONTROLLED BY A MICRO-RAMP VORTEX GENERATOR
D. Sun¹, C. Li¹, H.-Y. Cai, School of Aeronautics, Northwestern Polytechnical University, China; Q.-L. Guo¹, P.-X. Liu¹, X.-Y. Yuan¹; ¹State Key Laboratory of Aerodynamics, China
7.5Low Speed Aero
Chair: F. Collier
Track 7
03.4 - Applied Aerodynamics
  10:30 11:00 7.5.1 TRANSPORT AIRCRAFT WING INVESTIGATIONS AIMED ON WAKE VORTEX IMPACT BY OSCILLATING FLAPS
J. Ruhland¹, F.M. Heckmeier¹, C. Breitsamter¹; ¹Technical University of Munich, Germany
  11:00 11:30 7.5.2 AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATION
M. Zhong¹, J. Hua¹, X. Sun¹, S. Zheng¹, G. Wang¹, G. Zhang¹, H. Wang¹, Y. Li¹, X. Li¹, J. Bai, Northwestern Polytechnical University, China; ¹Chinese Aeronautical Establishment, China
Presenter: min zhong
Reserve Paper (Interactive) 7.5.R NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING LEADING EDGE COVERTS
J.X. Gao¹, W.Q. Yang¹, R. Zhang¹, Y.B. Li¹; ¹Northwestern Polytechnical University, China
8.5Composite Materials and Structures
Chair: A. Alaimo
Track 8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
  10:30 11:00 8.5.1 ACCURATE MODELS FOR THE PREDICTION OF FREE-EDGE STRESSES OF COMPOSITE STRUCTURES UNDER THERMAL LOADS
E. Zappino¹, E. Carrera¹; ¹Politecnico di Torino, Italy
  11:00 11:30 8.5.2 TEMPERATURE-INDUCED LOAD OF BOLTED HYBRID COMPOSITE/METAL JOINT
K LEI¹, B.-W WANG¹, J.-T WU¹, W.-L DENG¹; ¹Aircraft Strength Research Institute of China, China
Presenter: KAI LEI, AVIC Aircraft Strength Research Institute
  11:30 12:00 8.5.3 DEVELOPMENT OF LIGHTWEIGHT HYBRID AIRFRAMES BASED ON UNIDIRECTIONAL COMPOSITE STRUCTURE CONCEPTS
A. Shanygin, Russia
Reserve Paper (Interactive) 8.5.R DEVELOPMENT OF ADVANCED DESIGNS OF GAS TURBINE ENGINES FROM POWDER COMPOSITIONS
L. Magerramova, Central Institute of Aviation Motors, Russia; E. Kratt, Laboratory of New Technology, Russia
9.5Helicopter Control
Chair: J. Che
Track 9
06.1 - Flight Dynamics and Control (Control & Modelling)
  10:30 11:00 9.5.1 DESIGN TECHNIQUE OF INTEGRAL ALGORITHMS FOR HELICOPTER FBW CONTROL SYSTEM
V.M. Kuvshinov¹, A.Y. Voronin¹; ¹TsAGI, Russia
Presenter: Alexander Voronin, Central Aerohydrodynamic Institute (TsAGI)
  11:00 11:30 9.5.2 TRAJECTORY GENERATION AND CONTROL FOR PERCHING MANEUVERING WITH QUADROTOR
Y. Sun¹, M. Chang¹, J.Q. Bai¹; ¹NWPU, China
10.5Condition Based Maintenance 1
Chair: J. Vincent
Track 10
11 - Operations and Sustainment
  10:30 11:00 10.5.1 STRUCTURAL HEALTH MONITORING - THE ROUTE TO CONDITION BASED MAINTENANCE
J. van Doeselaar¹, D. Daverschot¹; ¹Airbus, France
  11:00 11:30 10.5.2 COST AND BENEFIT OF SCHEDULED STRUCTURAL HEALTH MONITORING FOR COMMERCIAL AIRCRAFT
D.M. Steinweg¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
  11:30 12:00 10.5.3 REAL TIME IMPACT LOCALIZATION USING MODAL SUPERPOSITION - APPLICATION TO A COMPOSITE AIRCRAFT FUSELAGE
D. Goutaudier, CNRS, France; D. Gendre, Airbus, France
Presenter: Dimitri Goutaudier, PIMM Laboratory
11.5Systems & Components Safety
Chair: G. Weber
Track 11
10 - Safety and Security
  10:30 11:00 11.5.1 AIRCRAFT INFLIGHT ICING DETECTION AND DIAGNOSIS METHODS
D. Ding¹, W.-Q. Qian¹, Q. Wang¹; ¹China Aerodynamics Research and Development Center, China
  11:00 11:30 11.5.2 DESIGN AND RESEARCH ON SAFETY ANALYSIS TOOL FOR AVIONICS SYSTEM
Y. Liu, Shanghai Aircraft Design and Research Institute, China
  11:30 12:00 11.5.3 A PROTOTYPE WHIRL TOWER FOR TESTING INSOLATED ROTOR SYSTEMS IN HOVER
M.-M. Wojtas¹, K. Raczko¹, L. Czajkowski¹; ¹Institute of Aviation, Poland
1.6HMI & Cabin Design
Chair: B. Nagel
Track 1
01 - Aircraft Design and Integrated Systems
  13:00 13:30 1.6.1 ATTENUATION OF NOISE IN THE CABIN OF A REGIONAL AIRCRAFT BY METAMATERIAL TRIM PANELS
M.C. Moruzzi, University of Bologna, Italy; M. Cinefra, Italy; S. Bagassi, Italy; E. Carrera, Italy
  13:30 14:00 1.6.2 GAZE-BASED INTERFACE FOR FLIGHT CONTROL: RESULTS OF INITIAL EXPERIMENTS WITH THE SYSTEM
M.A. Rodriguez Diaz¹, E. Villani¹, P. Krus, Linköping University, Sweden; ¹Aeronautics Institute of Technology, Brazil
  14:00 14:30 1.6.3 ESTIMATION OF STATIC AND DYNAMIC FLOATATION CHARACTERISTICS DURING AIRCRAFT DITCHING
Y. Zhao¹, P. Liu¹, Q. Qu¹; ¹Beihang University, China
2.6Aviation and World Wildfires
Chair: A. Mirzoyan
Track 2
15 - Guest lectures
  13:00 13:30 2.6.1 PROPOSAL FOR INTERNATIONAL FIRE AVIATION SERVICE UNDER THE AUSPICES OF ICAO TO IMPROVE WORLD WILDFIRE MANAGEMENT
A. Mirzoyan, CIAM, Russia
  13:30 14:00 2.6.2 ICAO ADDRESSING CLIMATE CHANGE AND WILDFIRES
J. Hupe, ICAO, Canada
  14:00 14:30 2.6.3 EXPERIENCE OF BELARUS IN USING HELICOPTER TECHNOLOGY FOR FOREST FIREFIGHTING
I. Labzin, SAERA “Aviatsiya”, Belarus
3.6Model Based Systems Engineering 1
Chair: S. Conway
Track 3
02 - Systems Engineering and Integration
  13:00 13:30 3.6.1 FORMALIZED KNOWLEDGE MANAGEMENT FOR THE AIRCRAFT CABIN DESIGN PROCESS
M. Fuchs¹, C. Hesse¹, J. Biedermann¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany
  13:30 14:00 3.6.2 SOS BEHAVIOR MODEL TRANSFORMATION FOR AIRCRAFT TOP-LEVEL DEMONSTRATION
J. Zang¹, J.Q. Zhu¹; ¹Chinese Aeronautical Establishment, China
  14:00 14:30 3.6.3 CONNECTING SYSTEM SIMULATION TO AIRCRAFT CONCEPT DEVELOPMENT
A. Oprea¹, R. Hällqvist¹, L. Knöös Franzén², M. Eek¹, I. Staack², H. Gavel¹; ¹Saab Aeronautics, Sweden ;²Linköping University, Sweden
Reserve Paper (Interactive) 3.6.R CO-SIMULATION OF SYSML AND SIMULINK OR MODELICA USING FMI
J. Shen¹, Q. Zhou¹, B.F. Li¹, C. Chen¹; ¹Chinese Aeronautical Radio and Electronics Research Institute, China
4.6High Speed Flows
Chair: A. Viviani
Track 4
03.1 - Aerodynamics – CFD Methods and Validation
  13:00 13:30 4.6.1 LONGITUDINAL VORTEX FORMATION IN HYPERSONIC BOUNDARY LAYER ON BLUNTED DELTA WING AND ITS EFFECT ON FLOW CHARACTERISTICS
V.I. Shalaev¹, S.V. Alexandrov¹, A.V. Vaganov², M.A. Starodubtsev²; ¹Moscow Institute of Physics and Technology, Russia ;²Central aerohydrodynamic Institute, Russia
  13:30 14:00 4.6.2 LONGITUDINAL AND LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE HIGH-SPEED VEHICLE
T. Bykerk, Honorary Associate, the University of Sydney, Australia, Australia; G. Pezzella, University of Campania, Engineering Department. , Italy; D. Verstraete, University of Sydney, School of Aerospace, Australia; A. Viviani, University of Campania, Engineering Department., Italy
  14:00 14:30 4.6.3 MULTI-SCALE CFD/MD MODELLING OF HIGH-ENTHALPY FLOW/TPS INTERACTION AND ITS PRELIMINARY AERONAUTICAL APPLICATION
X.F. Yang¹, Q. Li, Shanghai Jiao Tong University, China; Y.X. Du¹, G.M. Xiao¹, L. Liu¹, D. Wei¹, Y.W. Gui¹; ¹China Aerodynamics Research and Development Center, China
Presenter: Qin Li
Reserve Paper (Interactive) 4.6.R INVESTIGATION ON DIFFERENT NUMERICAL SIMULATIONMETHODS OF ROCKET ENGINE
H. Chen¹, Y.F. Yang¹, P. Xue¹, X.X. Li¹, C. Dong¹, S. Wang¹, M.X. Zhang¹; ¹Beijing Institute of Space Long March Vehicle, China
5.6Airspace Management
Chair: A. Andreeva Mori
Track 5
09 - Air Transport System Efficiency
  13:00 13:30 5.6.1 DESIGNING AIRCRAFT TRAFFIC FLOWS USING DATA-DRIVEN QUEUING MODELS
E. Itoh, The University of Tokyo/ENRI, Japan; F. Kato¹, K. Higasa¹, M. Schultz, Technische Universität Dresden, Germany; ¹The University of Tokyo, Japan
Presenter: Eri Itoh, The University of Tokyo/ENRI
  13:30 14:00 5.6.2 ON THE MINIMUM SEPARATION BETWEEN ANY PAIR OF FLIGHT PATHS
L.M.B.C. Campos, IDMEC/CCTAE/IST, Portugal; J.M.G. Marques, Escola de Ciências e Tecnologias, Universidade de Évora, Portugal
6.6Composite Defect and Damage
Chair: M. Herman
Track 6
04.1 - Material Issues, Fatigue and Damage Tolerance
  13:00 13:30 6.6.1 ADJUSTED SHAPES OF ADHESIVELY BONDED REPAIR PATCHES FOR THE EARLY INDICATION OF DEBOND IN FIGHTER AIRCRAFT STRUCTURES
J Jokinen¹, M Wallin, Patria Aviation, Finland; M Kanerva¹; ¹Tampere University, Finland
  13:30 14:00 6.6.2 THE INFLUENCE OF THE NUMBER OF ADHESIVE PLIES (FM-300-2K) ON FRACTURE PROPERTIES
J Jokinen¹, M Wallin, Patria Aviation, Finland; M Kanerva¹; ¹Tampere University, Finland
  14:00 14:30 6.6.3 STATISTICS AND ANALYSIS OF 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
7.6Simulation
Chair: J. Monk
Track 7
03.4 - Applied Aerodynamics
  13:00 13:30 7.6.1 RESEARCH ON UNSTEADY AERODYNAMIC MODELS AT HIGH ANGLES OF ATTACK BASED ON NONLINEAR REGRESSION
J.A. Cheng¹, H. Zhan¹, B.G. Mi¹; ¹School of Aeronautics,Northwestern Polytechnical University, China
Presenter: Jia Ao Cheng, Northwestern Polytechnical University
  13:30 14:00 7.6.2 RESEARCH ON THE TRIGGERING CONDITIIONS OF EJECTABLE RECORDER FOR CIVIL AIRCRAFT
S.M. Pu¹, H.F. Wang¹, L.K. Cheng¹; ¹Northwestern Polytechnical University, China
Presenter: Liukai Cheng
Reserve Paper (Interactive) 7.6.R NUMERICAL SIMULATION OF VARIABLE WINGSPAN EFFECTS ON A BIONIC FLAPPING WING
R. Zhang¹, W.Q. Yang¹, Y.B. Li¹, J.X. Gao¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
8.6Failure Analysis and Fatigue
Chair: V. Symonov
Track 8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
  13:00 13:30 8.6.1 METHODS FOR CALCULATING THE FATIGUE DAMAGE OF A STRUCTURE FOR VARIOUS SPECTRA OF VIBRO-ACOUSTIC LOADS
P. Bessonov¹, Y. Svirsky¹, I. Sidorov¹, S. Dubinskii¹; ¹TsAGI, Russia
  13:30 14:00 8.6.2 ITERATIVE GLOBAL/LOCAL NON-INTRUSIVE MODEL COUPLING METHOD FOR STRUCTURE FAILURE ANALYSIS
Y.J. LIU¹, S.Q. LIANG¹, R.J. SUN¹, M.Q. LI, China; ¹AVIC THE FIRST AIRCRAFT INSTITUTE, China
  14:00 14:30 8.6.3 A STRUCTURE DESIGN OF CFRP REAR PRESSURE BULKHEAD WITHOUT STIFFENERS
Z.Y. Li¹, Y.Z. Han¹, X.H. Yao¹; ¹AVIC the First Aircraft Institute, China
Presenter: ZHONGYANG LI, FAI AVIC
Reserve Paper (Interactive) 8.6.R PROCESS RESEARCH AND OPTIMINZATION OF PINHOLE HOLEAND NAIL HEAD DAMAGE ON COMPOSITE PARTS
Y. Liu¹, D. Zhou¹, S. Feng¹, C. Yang¹, H. Xie¹; ¹Chengdu Aircraft Industry (Group) Corporation Ltd., China
9.6Additive Manufacturing
Chair: D. Gu
Track 9
08 - Manufacturing and Supply Chain Management
  13:00 13:30 9.6.1 EFFECTS OF COOLANT BUILD DIRECTION ON ADDITIVELY MANUFACTURED FAN-SHAPED COOLING HOLES
Q. Zeng, School of Aeronautics and Astronautics, Zhejiang University, China; C. Li¹, J. Cao¹, B. Wang¹, G. Wang, ZHEJIANG UNIVERSITY, China; ¹AECC HAPRI, China
  13:30 14:00 9.6.2 APPLICATION OF ADDITIVE MANUFACTURING TO THE PRODUCTION OF RPAV COMPONENTS
P. Iavecchia¹, G. Campolo¹, G. Maritano¹, M. Coppola¹, E. Cestino¹, G. Frulla¹, V. Sapienza, 2Aeronautical Consultant, Italy; P. Piana, TescoGO, Italy; ¹Politecnico di Torino, Italy
Presenter: Giuseppe Campolo, Politecnico di Torino (DIMEAS)
  14:00 14:30 9.6.3 AN EFFICIENT FINITE ELEMENT SIMULATION METHOD FOR ADDITIVE MANUFACTURING PROCESS
Q.Y. Liu¹, C.Y. Wang¹, P. Yan¹, H. Ruan¹, H.Z. Xue¹, L.T. Dong¹; ¹Beihang University, China
10.6Condition Based Maintenance 2
Chair:
Track 10
11 - Operations and Sustainment
  13:00 13:30 10.6.1 CONDITION BASED MAINTENANCE (CBM) IN THE DIGITAL TRANSFORMATION STREAM
V. Gros¹, P.-C. Rolland¹, S. Veron¹, B. Ordy¹, F. Dessertenne, AIRBUS OPERATIONS SAS, France; ¹AIRBUS SAS, France
  13:30 14:00 10.6.2 TOTAL LIFE CYCLE COST AND EMISSION OF ELECTRIC, HYBRIDELECTRIC AIRCRAFT
D.D. Nguyen¹, U. Kale¹, A.W. Wangai¹; ¹Budapest University of Technology and Economics, Hungary
Presenter: Agnes Wanjiku Wangai, Budapest University of Technology and Economics
  14:00 14:30 10.6.3 A METHOD FOR EVALUATING THE APPLICABILITY OF MAINTENANCE TASKS BASED ON HELICOPTER HEALTH AND USAGE MONITORING SYSTEM
D.N. Dong¹, Z.Y. Jia¹, Y. Zhou¹; ¹AVIC China Aero-Polytechnology Establishment, China
11.6Flight Control and Critical Situations
Chair: M. Maroni
Track 11
10 - Safety and Security
  13:00 13:30 11.6.1 ACTIVITY CHARACTERISTICS AND THE MECHANISM OF MESO-MICRO SCALE DISTURBANCES IN THE EAST ASIAN SUBTROPICAL UPPER-LEVEL JET STREAM
X. Chen¹, J. Huang¹, M. Meng, Wenzhou Meteorological Burea, China; C. Chen¹, Q. Chen¹; ¹China Aerodynamics Research and Development Center, China
  13:30 14:00 11.6.2 RESEARCH ON FAULT DIAGNOSIS AND FAILURE RECONFIGURATION OF FLUSH AIR DATA SENSING
Q. Jia¹, W. Zhang¹, J. Shi¹, J. Hu¹, E. Safwat, Military Technical College, Egypt; ¹Northwestern Polytechnical University, China
  14:00 14:30 11.6.3 CONCEPT OF A NEW SYSTEM SYNTHESIZING METEOROLOGICAL AND OROGRAPHIC INFLUENCES ON THE AIRPLANE SAFE ENERGY ENVELOPE
X. Liu¹, L. Manfriani, Centre for Aviation, Zurich University of Applied Sciences, Switzerland; Y. Fu¹; ¹Lab. of Aerosp. Servo Actuation and Transmission, Beihang Univ., China
1.7Hybrid/Electric & Unconventional Aircraft 2
Chair: P. Prakasha
Track 1
01 - Aircraft Design and Integrated Systems
  08:00 08:30 1.7.1 CONCEPTUAL DESIGN OF SILENT ELECTRIC COMMUTER AIRCRAFT
P. Wassink¹, G. Atanasov¹, C. Hesse¹, B. Froehler¹; ¹German Aerospace Center (DLR), Germany
Presenter: Philip Wassink, German Aerospace Center (DLR)
  08:30 09:00 1.7.2 DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: CONTROL, ALIMENTATION, AND PROPULSION SYSTEMS
P. Gili¹, M. Civera¹, R. Roy¹, S. Cibrario Bertolotti¹, D. Cosenza¹, A. Gili¹, C. Surace, Department of Structural, Geotechnical and Building Engineering,, Italy; ¹Department of Mechanical and Aerospace Engineering, Politecnico , Italy
  09:00 09:30 1.7.3 EXPERIMENTAL RESEARCH ON PROPULSION AND AERODYNAMIC CHARACTERISTICS OF A DUAL-BODY DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT
X.-Y. Zhang¹, Z.-H. Gao¹, T. Lei¹, X.-B. Zhang¹, W. Zhang¹; ¹Northwestern Polytechnical University, China
  09:30 10:00 1.7.4 ON-BOARD SYSTEM ARCHITECTURES FOR HYBRID/ALL-ELECTRIC REGIONAL AIRCRAFT
M. Fioriti¹, F. Di Fede¹, S. Corpino¹, P. Iodice², G. Cerino²; ¹Politecnico di Torino, Italy ;²LEONARDO Aircraft Division, Italy
2.7Global Collaborative Digital Integration in Aviation / IFAR-X challenge
Chair:
Track 2
02 - Systems Engineering and Integration
  08:00 08:30 2.7.1 COLLABORATIVE AIRCRAFT DESIGN TECHNIQUES IN RESEARCH
B. Nagel¹, E. Moerland¹; ¹German Aerospace Center, Germany
  08:30 09:00 2.7.2 IFAR-X COLLABORATIVE AIRCRAFT DESIGN EXERCISE ON ENVIRONMENTALLY COMPATIBLE TRANSPORT AIRCRAFT
T. Nunes, CEIIA, Portugal
  09:00 09:30 2.7.3 COLLABORATIVE AIRCRAFT DESIGN EXERCISE BEYOND IFAR
P. Novelli, ONERA, France
  09:30 10:00 2.7.4 HARMONIZING SUSTAINABLE AVIATION RESEARCH AMONG IFAR ORGANIZATIONS
E. Campillo-Borras, DLR, Germany
3.7AFLoNext
Chair:
Track 3
15 - Guest lectures
  08:00 08:30 3.7.1 FLIGHT TEST OF AN ADVANCED HYBRID-LAMINAR-FLOW-CONTROL (HLFC) SYSTEM ON AN A320 VERTICAL TAIL PLANE
G. Ernst, German Aerospace Center, Germany; S. Pawellek¹, A. Büscher¹; ¹Airbus Operations GmbH, Germany
Presenter: Heiko von Geyr, German Aerospace Center
  08:30 09:00 3.7.2 NOISE REDUCTION AT FLAP SIDE EDGE AND UNDERCARRIAGE
M Pott-Pollenske, Germany
  09:00 09:30 3.7.3 MAIN LANDING GEAR DOORS VIBRATION REDUCTION BASED ON FLIGHT TEST
C. Aquilini¹, P. Lubrina, ONERA, France; S.-H. Peng, FOI, Sweden; J. Schwochow, DLR, Germany; R. Abarca López¹; ¹Airbus, Germany
  09:30 10:00 3.7.4 TOWARDS THE INDUSTRIAL APPLICATION OF ACTIVE FLOW CONTROL AT THE PYLON/WING JUNCTION OF CIVIL AIRCRAFT
Vitaly Soudakov, TsAGI, Russia; Philipp Schlösser, Airbus, Germany; Perez Weigel, Fraunhofer-Gesellschaft, Germany; Theo ter Meer, NLR, Netherlands; Anna Gebhardt, DLR, Germany
4.7Applied CFD 1
Chair: L. Alves
Track 4
03.1 - Aerodynamics – CFD Methods and Validation
  08:00 08:30 4.7.1 COMPUTATIONAL STUDY ON COANDA BLANKET CURVATURE EFFECTS ON HALF-SPHERICAL COANDA DEVICE PERFORMANCE
H. Djojodihardjo, The Institute for the Advancement of Aerospace Science and Techn, Indonesia; M.A. Andira¹, R. Julistina¹, M.A. Moeljadi, Institute of Technology Bandung, Indonesia; ¹CCIT Group Indonesia, Indonesia
  08:30 09:00 4.7.2 AERODYNAMIC MODELING AND FLIGHT PERFORMANCE RESEARCH OF THE COAXIAL RIGID HELICOPTER IN POP-UP PROCESS
H.-Y. Li¹, X. Zhao¹, K. You¹, S.-Z. Zhao¹, Y.-F. Lin, China Helicopter Research and Development Institute, China; ¹Northwestern Polytechnical University, China
  09:00 09:30 4.7.3 STALL PREDICTION OF AIRCRAFT WITH ADAPTIVE HYBRID MESH
J. Tang¹, J. Zhang¹, N.-C. Zhou¹, B. Li¹, P.-C. Cui¹; ¹China Aerodynamics Research and Development Center, China
  09:30 10:00 4.7.4 NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING WITH SLOTTED-TIP
D. Liu, School of Aeronautics,Northwestern Polytechnical University, China; W.Q. Yang¹, B.F. Song¹; ¹Research & Development Institute of NWPU in Shenzhen, China
Reserve Paper (Interactive) 4.7.R AERODYNAMIC COEFFICIENT RESPONSE OF RECEIVER DURING AERIAL REFUELING PROCESS
G.Y. Li, AVIC Xi'an Aircraft Industry Group Company LTD., China; T. Miao¹, B. Chen¹, F. Liu¹; ¹China Aerodynamics Research and Development Center, China
5.7UTM/On-Demand Mobility
Chair: A. Andreeva-Mori
Track 5
09 - Air Transport System Efficiency
  08:00 08:30 5.7.1 AIRLINE NETWORK-AIRPLANE INTEGRATED OPTIMIZATION CONSIDERING MANUFACTURER\'S PROGRAM COST
J.A. Fregnani, Airbus, Brazil; B.S. Mattos¹, J.A. Hernandes¹; ¹ITA, Brazil
Presenter: José Fregnani, ITA
  08:30 09:00 5.7.2 AIR TRAFFIC MANAGEMENT OF DRONES INTEGRATED INTO THE SMART CITIES
D. Dinh Nguyen¹, D. Rohacs¹; ¹Budapest University of Technology and Economics, Hungary
Presenter: Dinh Dung Nguyen, Budapest University of Technology and Economics
  09:00 09:30 5.7.3 VERTIPORT PLACEMENT METHOD BASED ON MOBILITY SURVEY DATA
K. Lippoldt¹, L. Preis, Bauhaus Luftfahrt e.V., Germany; K. Bogenberger¹; ¹Technical University Munich, Germany
  09:30 10:00 5.7.4 ASSESSING THE ENVIRONMENTAL IMPACT OF AIRCRAFT TAXIING TECHNOLOGIES
R. Camilleri¹, A. Batra¹; ¹Institute of Aerospace Technologies, University of Malta, Malta
6.7Laminar Flow
Chair: S. Fu
Track 6
03.4 - Applied Aerodynamics
  08:00 08:30 6.7.1 BLADE - NATURAL LAMINAR FLOW FLIGHT TESTING
Tom Gibson¹, Bertrand Soucheleau¹, Nick Rogers¹; ¹Airbus, United Kingdom
  08:30 09:00 6.7.2 METHODICAL STUDIES OF THE POSSIBILITY TO APPLY A NUMERICAL METHOD WITH BUILD-IN EMPIRICAL CRITERIA FOR DETERMIMING THE LAMINAR-TO-TURBULENT TRANSITION ON THE CONE SURFACE AT HIGH MACH NUMBERS
N.V. Voevodenko¹, Y.G. Shvalev¹; ¹TsAGI, Russia
  09:00 09:30 6.7.3 NATURAL-LAMINAR-FLOW AIRFOIL DESIGN OPTIMIZATION CONSIDERING CROSSFLOW INSTABILITY WHEN CONFIGURED ON A SWEPT WING
Z.-M. Xu¹, Z.-H. Han¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China
  09:30 10:00 6.7.4 MULTIPOINT OPTIMIZATION OF TRANSONIC NATURAL LAMINAR FLOW NACELLES
C.Y. Yan¹, Y.F. Zhang¹, M.H. Zhang, Shanghai Aircraft Design and Research Institute, China; ¹School of Aerospace, Tsinghua University, China
7.7Failure And Fracture Mechanics
Chair: M. Kanerva
Track 7
04.1 - Material Issues, Fatigue and Damage Tolerance
  08:00 08:30 7.7.1 FAILURE PROCESS IDENTIFICATION IN C/SIC SAMPLES WITH A RANGE OF TENSILE PERFORMANCE USING ACOUSTIC EMISSION
Y.Z. Zhang¹, X.Y. Tong¹, L.J. Yao¹, A.T. Augousti, Kingston University London, United Kingdom; ¹Northwestern Polytechnical University, China
  08:30 09:00 7.7.2 EXPERIMENTAL INVESTIGATION AND LIFE PREDICTION FOR DEFECT INDUCED CRACK OF A P/M NICKEL BASED SUPERALLOY
Y. Shi, China; X. Yang, China; D. Shi, China; D. Yang, China; G. Miao, China; S. Lv, China
Presenter: YI SHI
Reserve Paper (Interactive) 7.7.R STUDY ON THE METHOD OF DETERMINING SKIN WAVINESS REQUIREMENT OF CIVIL AIRCRAFT
D. Jin¹, G.P. Qian¹, K. Feng¹; ¹Shanghai Aircraft Design and Research Institute, China
8.7Compressors & Turbines
Chair: I. Yimer
Track 8
05 - Propulsion
  08:00 08:30 8.7.1 RESEARCH OF LABYRINTH SEALS MEASUREMENT-BASED PROBABILITISTIC ANALYSIS METHOD FOR TURBOFAN INTERNAL AIR SYSTEM
C.-X. Song¹, M.-C. Deng¹, Y. Fan¹, Y.-Q. Liang¹, Y. Shen¹; ¹AECC Shenyang Engine Research Institute, China
  08:30 09:00 8.7.2 AXIAL ASSEMBLAGE DEVIATION ON PERFORMANCE OF ONE TRANSONIC CENTRIFUGAL COMPRESSOR
W. Zhang¹, K. Luo¹, X.-W. LIU², Q. Wen², F.-M. Tang¹; ¹AECC HAPRI, China ;²AECC AEAC, China
  09:00 09:30 8.7.3 THE POTENTIAL OF CASING TREATMENTS FOR TRANSONIC COMPRESSORS: EVALUATION BASED ON AXIAL-SLOT AND ROTOR BLADE OPTIMISATION
G. Goinis¹, C. Voß¹, E. Nicke¹; ¹German Aerospace Center (DLR), Germany
  09:30 10:00 8.7.4 APPLICATION OF REINFORCEMENT LEARNING IN 1-D AERODYNAMIC DESIGN OF AXIAL COMPRESSOR
Y. Liu¹, X. Hang¹, C. Jiang¹; ¹Beihang University, China
Reserve Paper (Interactive) 8.7.R EFFECT OF COMPLEX FLOW PROFILES AT COMBUSTOR EXIT ON TURBINE CHARACTERISTICS
Yongfan Li¹, Zhenzhe Na¹, Yun Chen¹, Yangbing Wang¹; ¹AECC, China
9.7Flight Control During Approach
Chair: A. Boucher
Track 9
10 - Safety and Security
  08:00 08:30 9.7.1 TOWARDS AN ONLINE PREDICTIVE MODEL OF AIRCRAFT ENERGY STATE USING SUPERVISED MACHINE LEARNING
H.K. Lee¹, T.G. Puranik¹, O.J. Pinon Fischer¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States
Presenter: HyunKi Lee, Georgia Institute of Technology
  08:30 09:00 9.7.2 AN OVERVIEW OF FLARE TECHNIQUES AND FLARE TRAINING METHODS
K. Okubo¹, J.O. Entzinger¹; ¹The University of Tokyo, Japan
Presenter: Kosuke Okubo, The University of Tokyo
  09:00 09:30 9.7.3 FLIGHT PERFORMANCE AND TRAJECTORY PREDICTION OF THE COAXIAL HELICOPTER IN AUTOROTATION
S.-Z. Zhao¹, X. Zhao¹, R. Yao¹, Y.-F. Lin, China Helicopter Research and Development Institute, China; ¹Northwestern Polytechnical University, China
  09:30 10:00 9.7.4 NUMERICAL STUDY OF DITCHING CHARACTERISTICS OF BWB AIRCRAFT
S.L. Ding¹, Q.L. Qu¹, P.Q. Liu¹; ¹Beihang University, China
10.7Flight Dynamics 2
Chair:
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  08:00 08:30 10.7.1 ANALYTICAL MODELLING OF A HOVERABLE X-SHAPE FLAPPING WING AIRCRAFT CONSIDERING WING-TAIL INTERACTION
L.F. Zhao, Beihang University, Research Institute for Frontier Science, China; W.S. Wang, Beihang University, School of Automation Science and Electrical , China; Y.X. Chen, Beihang University, School of Aeronautic Science and Engineering, China; Z.X. Jiao, Beihang University, Ningbo Institute of Technology, China
  08:30 09:00 10.7.2 MODELING AND CONTROL OF A HOVERABLE FLAPPING WING AIRCRAFT CONSIDERING FLAPPING WING INDUCED FLOW
L. Wang¹, L.F. Zhao¹, W.Y. Jiang¹, Z.X. Jiao¹; ¹Beihang University, China
  09:00 09:30 10.7.3 SIMULATION ON THE EFFECT OF AIRCRAFT LOCAL STRUCTURE DAMAGES ON THE DYNAMIC DERIVATIVE COUPLING CHARACTERISTICS
B.-G. Mi¹, H. Zhan¹, X. Bai¹, J.-Y. Yu¹; ¹Northwestern Polytechnical University, China
  09:30 10:00 10.7.4 INFLUENCE OF AERODYNAMIC ASYMMETRY ON SPIN PARAMETERS OF THE COMMON RESEARCH MODEL
A.N. Khrabrov¹, M.E. Sidoryuk¹; ¹TsAGI, Russia
11.7empty 1
Chair:
Track 11
1.8MDO
Chair: S. Bagassi
Track 1
01 - Aircraft Design and Integrated Systems
  10:30 11:00 1.8.1 COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN
S. Görtz¹, C. Ilic¹, M. Abu-Zurayk¹, T. Wunderlich¹, M. Schulze¹, T. Klimmek¹, Ö. Süelözgen¹, T. Kier¹, A. Schuster¹, S. Dähne¹, M. Petsch¹, J. Häßy¹, R.-G. Becker¹, M. Siggel¹, J. Kleinert¹, R. Mischke¹, S. Gottfried¹; ¹DLR, Germany
Presenter: Stefan Görtz, DLR
  11:00 11:30 1.8.2 BLENDED WING BODY PLANFORM MULTIDSCIPLIANRY OPTIMISATION
Davide DI Pasquale¹, Divyam Verma¹, Giampaolo Pagliuca¹; ¹Cranfield University, United Kingdom
  11:30 12:00 1.8.3 TOPOLOGY OPTIMIZATION FOR WING STRUCTURE OF HYPERSONIC VEHICLE
S.S. Zhang¹, Z.Q. Wan¹, X.Z. Wang, Institute of Unmanned System, Beihang University, China; Y.Z. Liu, China North Ind Grp Corp, Nav & Control Technol Inst, China; ¹School of Aeronautic Science and Engineering, Beihang University, China
2.8Compressor and Fan Aerodynamics 1
Chair: Z. Gao
Track 2
03.1 - Aerodynamics – CFD Methods and Validation
  10:30 11:00 2.8.1 DESIGN AND TEST OF A HIGH SLOPE ANGLE INTERMEDIATE DUCT BETWEEN LOW PRESSURE COMPRESSOR AND HIGH PRESSURE COMPRESSOR
H.-L. Jin¹, J. Zhang¹, J.-F. Wu¹, D.-B. Qiu¹, Y.-Q. Yin¹; ¹AECC Hunan Aviation Powerplant Research Institute, China
  11:00 11:30 2.8.2 NUMERICAL STUDY ON COOLING CHARACTERISTICS IN CHANNELS WITH PIN FIN ARRAYS UNDER HIGH TEMPERATURE/PRESSURE CONDITIONS
S.-E. Peng¹, W. Jin¹, J.-M. WU¹; ¹Xi’an Jiaotong University, China
  11:30 12:00 2.8.3 THE FLOW AND HEAT TRANSFER OF ANALYSIS TO ANNULAR CAVITY IN ENGINE CASE
G.Y. Pan¹, X. Yu¹, Y. Ii¹, Y.X. Zhao¹; ¹AECC SHENYANG ENGINE RESEACH INSTITUE, China
3.8Aspects of Landing Gear Design
Chair: P. Krus
Track 3
07 - Systems, Subsystems and Equipment
  10:30 11:00 3.8.1 IMPROVED DESIGN OF AIRCRAFT NOSEWHEEL STEERINGSYSTEM
X. Li¹, Z.J. Wang¹, X.B. Ding ¹, Z.B. Wei¹; ¹FAI AVIC, China
  11:00 11:30 3.8.2 INVESTIGATIONS ON LANDING GEAR SHOCK ABSORBER ACTIVE FORCE CONTROL
Z. Skorupka¹, R. Harla¹; ¹Lukasiewicz Research Network - Institute of Aviation, Poland
  11:30 12:00 3.8.3 A STOCHASTIC ROBUSTNESS VERIFICATION OF NLG SIMPLE ADAPTIVE SHIMMY SUPPRESSION SYSTEM
A. Alaimo¹, C. Orlando¹; ¹Università di Enna Kore, Italy
4.8Numerical Methods 1
Chair: T. Wan
Track 4
03.1 - Aerodynamics – CFD Methods and Validation
  10:30 11:00 4.8.1 VALIDATION OF A DISCONTINUOUS GALERKIN BASED DES SOLVER IN FLOW PROBLEMS USING HIGH PERFORMANCE COMPUTING
I. Bosnyakov¹, S. Bosnyakov¹, S. Mikhaylov¹, V. Podaruev¹, A. Troshin¹, A. Wolkov¹; ¹Central Aerohydrodynamic Institute, Russia
  11:00 11:30 4.8.2 ADVANCED WEAK SOLUTIONS IN FLUID DYNAMICS AND THEIR NUMERICAL COMPUTATIONS WITH AERODYNAMIC HEATING
M. Ivanov¹, V. Mamaev¹, J. Li², G. Zheng²; ¹CIAM, Russia ;²NWPU, China
  11:30 12:00 4.8.3 A BENCHMARK METHOD FOR PREDICTING OBLIQUE SHOCK STRUCTURE
A. SHI, NORTHWESTERN POLYTECHNICAL UNIVERSITY, China; E. DOWELL, DUKE UNIVERSITY, United States
Reserve Paper (Interactive) 4.8.R SIMULATION OF HIGH REYNOLDS NUMBER VISCOUS FLOW BASED ON ADAPTIVE CARTESIAN GRID
H. Chen, China; X. Yuan, China; R. Hua, China; Z. Tang, China; L. Bi, China; S. Meng, China
5.8UAV Flight Testing
Chair: J. Monk
Track 5
06.2 - Flight Dynamics and Control (UAV related)
  10:30 11:00 5.8.1 FLIGHT TESTING OF 65KG T-FLEX SUBSCALE DEMONSTRATOR
J. Bartasevicius¹, S.J. Koeberle¹, D. Teubl¹, C. Roessler¹, M. Hornung¹; ¹ Institute of Aircraft Design, Technical University of Munich, Germany
  11:00 11:30 5.8.2 THE STUDY OF UNMANNED AERIAL VEHICLE FLYING QUALITIESFLIGHT TEST METHOD BASED ON TIME-DELAY EVALUATION
S.-J. Qi¹, F. Wang¹, L. Jing¹; ¹Chinese Flight Test Establishment, China
  11:30 12:00 5.8.3 STUDY OF SMALL UAVS DISTURBED MOTION NATURAL FREQUENCIES USING EXTENDED EXPERIMENTAL DATASETS
M. El-Salamony, Peking University, China; S. Serokhvostov, Moscow Institute of Physics and Technology, Russia
6.8Transition Physics 2
Chair: Z. Goraj
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  10:30 11:00 6.8.1 STABILIZATION OF SUPERSONIC BOUNDARY LAYERS IN THE PRESENCE OF FAVORABLE PRESSURE GRADIENT
P.V. Chuvakhov, Central Aerohydrodynamic Institue (TsAGI), Russia
Presenter: Anton Obraz, Central Aerohydrodynamic Institute (TsAGI)
  11:00 11:30 6.8.2 NUMERICAL SIMULATION OF THREE-DIMENSIONAL DISTURBANCES EVOLUTION IN SUPERSONIC FLOW OVER A WAVY SURFACE
A. Novikov, TsAGI, MIPT, Russia; A. Fedorov, MIPT, Russia
  11:30 12:00 6.8.3 MECHANISMS OF NATURAL LAMINAR-TURBULENT TRANSITION ON AN UNSWEPT WING IN SUPERSONIC FLIGHT
P.V. Chuvakhov, Central Aerohydrodynamic Institue (TsAGI), Russia; A.V. Fedorov¹, I.O. Pogorelov¹; ¹Moscow Institute of Physics and Technology (MIPT), Russia
Presenter: Pavel Chuvakhov, Central Aerohydrodynamic Institute (TsAGI)
Reserve Paper (Interactive) 6.8.R NUMERICAL SIMULATION OF LOCAL LONG SHALLOW CAVITY EFFECT ON THE STABILITY OF A HYPERSONIC BOUNDARY LAYER
J.J. Yang¹, Y.D. Zhang¹, P. Lv¹, T. Pagliaroli, Università Niccolò Cusano, Italy; ¹China Academy of Aerospace Aerodynamics, China
Presenter: Jiaji Yang, China Academy of Aerospace Aerodynamics
7.8Optimization 1
Chair: F. Collier
Track 7
03.4 - Applied Aerodynamics
  10:30 11:00 7.8.1 AERODYNAMIC OPTIMIZATION DESIGN OF DOUBLE BLUNT ROTOR AIRFOIL WITH LARGE THICKNESS IN FORWARD AND REVERSE FLOW
Y.M. Yao¹, X.D. Yang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
  11:00 11:30 7.8.2 PARETO FRONT EXPLORATION USING MANIFOLD RECONSTRUCTION APPROACH FOR ROTORCRAFT AIRFOILS DESIGN
C. Song, China; W.-B. Li, China; Z. Zhou, China; H.-Y. Liu, China; X. Luo, China
  11:30 12:00 7.8.3 AERODYNAMIC DESIGN OPTIMIZAITON OF HYPERSONIC WING OVER WIDE MACH-NUMBER RANGE CONSIDERING LIFT MATCHING
Y. Zhang¹, Z.-H. Han¹, F. Liu¹, C.-Z. Xu¹; ¹Northwestern Polytechnical University, China
8.8Aeroelastic Identification and Control
Chair: F. Franke
Track 8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
  10:30 11:00 8.8.1 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
  11:00 11:30 8.8.2 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
  11:30 12:00 8.8.3 ACTUATION MECHANISM USING SHAPE MEMORY ALLOY WIRES IN SPIRAL ARRANGEMENT FOR MORPHING WINGS
R. Tsukamoto¹, A. Senba¹, T. Ikeda, Chubu University, Japan; M. Tamayama², H. Arizono²; ¹Meijo University, Japan ;²JAXA, Japan
9.8empty 2
Chair:
Track 9
10.8Flying Quality
Chair: N. Yokoyama
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  10:30 11:00 10.8.1 THE APPLICATION OF THE PILOT-AIRCRAFT SYSTEM APPROACH FOR OPTIMIZING 3D DISPLAY PARAMETERS
A.V. Efremov¹, M.S. Tiaglik¹, I.K. Irgaleev¹; ¹Moscow Aviation Institute, Russia
  11:00 11:30 10.8.2 ON THE MAXIMIZATION OF CONTROL POWER IN LOW-SPEED FLIGHT FOR A BWB CONFIGURATION
L.M.B.C. Campos, IDMEC/CCTAE/IST, Portugal; J.M.G. Marques, Escola de Ciências e Tecnologias, Universidade de Évora, Portugal
11.8Turbomechanics & Rotating Wings
Chair: D. Hui
Track 11
03.2 - Experimental Aerodynamics
  10:30 11:00 11.8.1 EXPERIMENT AND THEORETICAL ANALYSIS OF A TYPE OF NON-SYNCHRONOUS VIBRATION IN A HIGH PRESSURE COMPRESSOR
F.L. Gao¹, M.S. Yang¹, Z.B. Zhang¹, Y. Chen¹; ¹AECC Shenyang Engine Research Institute, China
  11:00 11:30 11.8.2 MEASUREMENT AND ANALYSIS OF INTER-STAGE FLOW FIELD IN A HIGH-LOAD AXIAL MULTISTAGE COMPRESSOR
Z.-B. Zhang¹, F.-L. Gao¹, H. Wu¹, Y.-H. Chen¹; ¹Shenyang Engine Research Institute, China
  11:30 12:00 11.8.3 ANALYSIS OF A WING-TIP-MOUNTED SMALL-SCALE PROPELLER CONFIGURATION UNDER NON-AXIAL INFLOW CONDITIONS
M. Cerny¹, N. Herzog, Rolls-Royce Deutschland Ltd & Co KG, Germany; C. Breitsamter¹; ¹Technical University of Munich, Germany
Reserve Paper (Interactive) 11.8.R EXPERIMENTAL INVESTIGATION ON FLOW CHARACTERISTICS IN COMPRESSOR ACOUSTIC-CAVITY RESONANCE TEST FACILITY BY PIV
Z.-B. Zhang¹, M.-S. Yang¹, H. Wu¹, M. Wang¹; ¹Shenyang Engine Research Institute, China
1.9System of Systems
Chair: M. Padulo
Track 1
01 - Aircraft Design and Integrated Systems
  13:00 13:30 1.9.1 EXPLORATION OF AERIAL FIREFIGHTING FLEET EFFECTIVENESS AND COST BY SYSTEM OF SYSTEMS SIMULATIONS
P. Shiva Prakasha¹, N. Naeem¹, N. Cigal¹, P. Ratei¹, B. Nagel¹; ¹German Aerospace Center, Germany
Presenter: Prajwal Shiva Prakasha, German Aerospace Center
  13:30 14:00 1.9.2 BENEFIT ANALYSIS OF AIR REFUELING IN ULTRA LONG ROUTEAIRLINER OPERATION
C. Ma¹, J.T. Si¹, Y.C. Chen, Commercial Aircraft Corporation of China, China; ¹Shanghai Aircraft Design and Research Institute, China
  14:00 14:30 1.9.3 CLOUD-BASED ENVIRONMENT FOR AIRCRAFT DESIGN COLLABORATION
X. Chen¹, A. Riaz¹, M.D. Guenov¹; ¹Cranfield University, United Kingdom
  14:30 15:00 1.9.4 QUANTIFICATION OF OPERATIONAL EFFECTIVENESS FOR TECHNOLOGY EVALUATION
A. Hull¹, A. Sudol¹, D. Mavris¹; ¹Georgia Institute of Technology, United States
2.9UAS
Chair: R. Gerhards
Track 2
01 - Aircraft Design and Integrated Systems
  13:00 13:30 2.9.1 METHODOLOGY FOR OBTAINING AN OPTIMIZED BAFFLED AIRFOIL FOR AN INFLATABLE WING
S.R. Mistri¹, R.S. Pant¹, C.S. Yerramalli¹, A. Guha¹; ¹Indian Institute of Technology- Bombay, India
  13:30 14:00 2.9.2 INTEGRATED AERODYNAMIC DESIGN OF PROPELLER POSITION AND WING SHAPE AT A LOW REYNOLDS NUMBER
W. Yang, National University of Defense Technology, China; L. Yu¹, W.H. Wu¹, Z.L. Fan¹; ¹China Aerodynamics Research and Development Center, China
  14:00 14:30 2.9.3 LIGHTWEIGHT UAV FOR EMERGENCY MEDICAL SERVICE
T. Goetzendorf-Grabowski¹, J. Mieloszyk¹, M. Figat¹, A. Tarnowski¹, B. Hernik¹; ¹Warsaw University of Technology, Poland
Presenter: Jacek Mieloszyk, Warsaw University of Technology
  14:30 15:00 2.9.4 DESIGN OF A HYBRID VTOL LOGISTICS UAV SYSTEM INTEGRATEDINTO CIVIL AVIATION AIR TRAFFIC CONTROL SYSTEM
Jiang Hanjie¹, Ma Yi , Xi’an Institute of Space Radio Technology, China; Zhou Ye ¹; ¹School of Aerospace Engineering, Universiti Sains Malaysia, Malaysia
  15:00 15:30 2.9.5 DESIGN OPTIMIZATION OF MULTIROTOR DRONES IN FORWARD FLIGHT
F. Pollet¹, S. Delbecq¹, M. Budinger, INSA Toulouse/ICA, France; J.-M. Moschetta¹; ¹ISAE-SUPAERO, France
Presenter: Félix Pollet, ISAE-SUPAERO
Reserve Paper (Interactive) 2.9.R RESEARCH ON BARYCENTER MEASUREMENT METHOD IN LAUNCH OF ROCKET-BOOSTED UNMANNED AERIAL VEHICLES
H.-L. Liu¹, M.-H. Tang¹, A.-Y. Zhu¹, W. Kong¹, H.-C. Shi, The First Military Representative Office of the Air Force Equipm, China; ¹Chengdu Aircraft Industrial (Group) Co., Ltd, China
3.9Model Based Systems Engineering 2
Chair: P. Vijgen
Track 3
02 - Systems Engineering and Integration
  13:00 13:30 3.9.1 RESEARCH ON AIRCRAFT-LEVEL PHYSICAL INTEGRATION VERIFICATION TEST TECHNOLOGY
Z.C. Yao¹, L.B. Liu¹; ¹Shanghai Aircraft Design and Research Institute, Shanghai, China
  13:30 14:00 3.9.2 THE APPLICATION OF THE AGILE 4.0 MBSE ARCHITECTURAL FRAMEWORK FOR THE MODELING OF SYSTEM STAKEHOLDERS, NEEDS AND REQUIREMENTS
L. Boggero¹, P.D. Ciampa¹, B. Nagel¹; ¹DLR, Germany
  14:00 14:30 3.9.3 HYBRID MODELLING FOR FULL MISSION SIMULATION
P. Krus, Linköping university, Sweden; R. Braun, ICAS2020_0980, Sweden; E. Villani, Instituto Tecnológico de Aeronáutica, Brazil
  14:30 15:00 3.9.4 MODEL-BASED VIRTUAL INTEGRATED TEST METHOD FOR AVIONICS SYSTEM
S.F. Zhu¹, P.P. Xing¹; ¹COMAC Beijing Aircraft Technology Research Institute, China
  15:00 15:30 3.9.5 A DEEP LEARNING AND ONTOLOGY BASED FRAMEWORK FOR TEXTUAL REQUIREMENTS ANALYSIS AND CONCEPTUAL MODEL GENERATION
A. Liu, Avic Digital Corporation LTD., China
4.9Applied CFD 2
Chair: S. Prince
Track 4
03.1 - Aerodynamics – CFD Methods and Validation
  13:00 13:30 4.9.1 EXPERIMENTAL VALIDATION OF NUMERICAL PREDICTION OF WING-PROPELLER AERODYNAMIC INTERACTION
S. De Lucas Bodas¹, J. Narbona Gonzalez¹, V. Ossorio Contreras¹, J.J. Guerra Crespo¹, D.E. Funes Sebastian¹, L.P. Ruiz Calavera¹; ¹Airbus Defence & Space, Spain
Presenter: David Funes Sebastian, Airbus Defence & Space
  13:30 14:00 4.9.2 STATIC AEROELASTIC COMPUTATIONS OF WING CONFIGURATIONS IN TRANSONIC FLOWS AT HIGH REYNOLDS NUMBERS
J.A.A. Lyrio¹, J.L.F. Azevedo², D.A. Rade¹, R.G. da Silva²; ¹Instituto Tecnológico de Aeronáutica, Brazil ;²Instituto de Aeronáutica e Espaço, Brazil
Presenter: Joao Luiz Azevedo, Instituto de Aeronautica e Espaco
  14:00 14:30 4.9.3 NUMERICAL INVESTIGATION OF WING ROCK PHENOMENON ON LOW ASPECT RATIO RECTANGULAR WINGS AT LOW REYNOLDS NUMBER
A. Sultan¹, A. Maqsood¹, T.H. Go, Raytheon Missile Systems, United States; R. Riaz¹; ¹National University of Sciences & Technology, Pakistan
Presenter: Aamir Sultan , National University of Sciences and Technology (NUST)
  14:30 15:00 4.9.4 S55 PROJECT - CFD ANALYSIS OF AN HISTORICAL SEAPLANE
C. Baldon¹, R. Indelicato¹, N. Bottino¹, M. Sinisi¹, F. Carrone¹, G. Cantanna¹, E. Cestino¹, V. Sapienza, Aeronautical Consultant, Italy; ¹Politecnico di Torino, Italy
Presenter: Cesare Baldon, Politecnico di Torino (DIMEAS)
  15:00 15:30 4.9.5 RESEARCH ON FSI DYNAMIC CHARACTERISTICS OF PARAFOIL TRAILING EDGE DEFLECTION
X.L. Gao¹, Q.B. Zhang, National Defense Technology University, China; Z.H. Li, Beijing Pioneering Innovation Center of China Aerodynamics Resea, China; Q. Chen¹, W.K. Wang, AVIC Aerospace Life-Support Industries. Ltd, China; ¹China Aerodynamic R&D Center, China
Reserve Paper (Interactive) 4.9.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
5.9Buckling and Instability
Chair: J. Juracka
Track 5
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
  13:00 13:30 5.9.1 ACHIEVEMENTS IN THE BUCKLING OF THIN-WALLED COMPOSITE LAUNCHER STRUCTURES
R. Degenhardt¹, F. Franzoni¹, S.G.P. Castro, TU-Delft, Netherlands; ¹DLR, Germany
  13:30 14:00 5.9.2 THE VIBRATION CORRELATION TECHNIQUE – A RELIABLE NONDESTRUCTIVE METHOD TO PREDICTBUCKLING LOADS
Haim Abramovich, Technion, I.I.T.,, Israel
  14:00 14:30 5.9.3 KINEMATIC MODEL OF REFINED THEORY AND EXACT ANALYTICAL SOLUTIONS OF STATIC AND BUCKLING PROBLEMS OF STRUCTURALLY-ANISOTR
L M Gavva, Moscow Aviation Institute (NRU) , Russia
  14:30 15:00 5.9.4 STUDY ON THE OUT-OF-PLANE COMPRESSION PROPERTIES OF MULTISTAGE TITANIUM ALLOY LATTICE METAMATERIALS AT 350°C
H.Y. Huang¹, D. Wang¹, X.F. Du¹, Y.X Xu¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
Presenter: Dong Wang, School of Aeronautics, Northwestern Polytechnical University
  15:00 15:30 5.9.5 ACCURATE BUCKLING AND POST-BUCKLING ANALYSIS OF COMPOSITE STIFFENED PANELS
E. Carrera¹, A. Pagani¹, R. Augello¹, D. Scano¹; ¹Politecnico di Torino, Italy
6.9Unsteady Flow Phenomena
Chair: C. Breitsamter
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  13:00 13:30 6.9.1 ANALYSIS AND CONTROL OF DYNAMIC STALL CHARACTERISTICS OF S809 AIRFOIL
L.-S. Hao¹, Y.-W. Gao¹, B.-B. Wei¹, B. Hu¹; ¹Northwestern Polytechnical University, China
Presenter: Li-Shu Hao
  13:30 14:00 6.9.2 PHISICAL AND MATHEMATICAL MODELS OF THE BUFFET ONSET
A.M. Lipanov, Institute of Applied Mathematics RAS, Russia; I.I. Lipatov, TsAGI, Russia; S.A. Karskanov, Instiute of Mechanics, Germany
  14:00 14:30 6.9.3 IMPROVEMENT OF HELICOPTER PERFORMANCE THROUGH PULSE AIR JETS BLOWN FROM THE TRAILING EDGE OF MAIN ROTOR BLADES
W. Stalewski, Lukasiewicz Research Network- Institute of Aviation, Poland
  14:30 15:00 6.9.4 STUDY ON THE EFFECTS OF PROPLET GEOMETRIC PARAMETERS ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLER
B. Wang¹, X.D. Yang¹, B.F. Song¹, J.H. Xu¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
  15:00 15:30 6.9.5 ANALYSIS OF AERODYNAMIC COUPLING EFFECT IN CLOSE FORMATION FOR FLAPPING WINGS
Z.T. Chen ¹, Z.X. Jiao¹, YX. Shang¹, L.F. Zhao¹; ¹Beihang University, China
7.9Advanced Manufacturing Management
Chair: D. Gu
Track 7
08 - Manufacturing and Supply Chain Management
  13:00 13:30 7.9.1 AN EXERCISE IN DEVELOPING A SUPERVISED ANOMALY DETECTION MODEL WITH AUTOMATICALLY ENGINEERED FEATURES
R. Rameshbabu¹, D. Rajaram¹, O.J. Pinon Fischer¹, T.G. Puranik¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States
Presenter: Rahul Rameshbabu, Georgia Institute of Technology
  13:30 14:00 7.9.2 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
  14:00 14:30 7.9.3 DESIGN AND BEST PRACTICES OF SUPPLIER PERFORMANCE EVALUATION IN SUPPLY CHAIN
H. Li¹, Y. Xu¹, Y. Chen¹; ¹AECC SHANGHAI COMMERCIAL AIRCRAFT ENGINE MANUFACTURING CO.,LTD., China
  14:30 15:00 7.9.4 AUTOMATIC DETECTION TECHNOLOGY OF LARGE CIVIL AIRCRAFT BASED ON IMAGE RECOGNITION
T.L. Shen¹, Z.Q. Li¹, Y. Liu¹; ¹Automatic Detection Technology of Large Civil Aircraft Based on, China
Presenter: tianlun shen
  15:00 15:30 7.9.5 ENABLING THE SMART SHOP FLOOR THROUGH THE INTEGRATION OF IOT AND AUTONOMOUS INTELLIGENCE
A. Xu, Chengdu Aircraft Industrial (Group) Co., Ltd., China
8.9Design of Aircraft Structures 1
Chair: E. Cestino
Track 8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
  13:00 13:30 8.9.1 AN INVERSE APPROACH BASED ON EUCLIDEAN SPACE FOR DETERMINING STRUCTURAL LOAD DISTRIBUTION FROM STRAIN MEASUREMENTS
H.N. Dui, China; D.L. Liu, China; Z.X. Zhang, China; S.Z. Pan, China; L.X. Zhang, China
  13:30 14:00 8.9.2 THERMOPLASTIC APPLICATIONS FOR AEROSTRUCTURES: TOWARDS SUSTAINABLE AND WEIGHT EFFICIENT APPLICATIONS
M. Herman¹, E. Dupuy¹, C. Paris¹, E. Petiot¹, J.-P. Cabanac¹, C. Fualdes¹, G. Masse², M.-A. Celli²; ¹Airbus Operations, France ;²Airbus Helicopters, France
  14:00 14:30 8.9.3 RATIONAL DETERMINATION OF WING JIG SHAPE OF A LONG-RANGE AIRCRAFT WITH TRANSONIC CRUISE REGIME
A.V. Bezuevsky¹, A.V. Grigorev¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
  14:30 15:00 8.9.4 AIRCRAFT ENGINE ROTOR DYNAMICS ANALYSIS AFTER FAN BLADE-OUT WITH ACCOUNT OF ROTOR-CASING CONTACT INTERACTIONS
V.Y. Myasnikov¹, I.I. Ivanov¹, B.S. Blinnik¹; ¹CIAM, Russia
  15:00 15:30 8.9.5 STRUCTURAL HEALTH MONITORING OF SANDWICH STRUCTURES WITH LATTICE CORES IN AIRCRAFT DESIGN: CHALLENGES AND POTENTIAL
T. Huang, Nanjing University of Aeronautics and Astronautics, China; M. Nuño ¹, K.-U. Schröder¹; ¹RWTH Aachen University, Germany
Presenter: Miguel Nuño, RWTH Aachen
Reserve Paper (Interactive) 8.9.R DEFORMATION ANALYSIS OF C-SPAR COMPOSITE STRUCTURE DURING THE PREFORMING PROCESSING
F. Chen¹, P. Chen¹, Y.Q. Zhao¹; ¹Shanghai Aircraft Manufacturing Corporation Ltd, China
9.9Airworthiness & Certification
Chair: J.C. Nanche
Track 9
10 - Safety and Security
  13:00 13:30 9.9.1 CERTIFICATION CONSIDERATIONS FOR EVTOL AIRCRAFT
Yingkang MOU¹, Mei JIANG¹, gang ZHU¹; ¹Nanjing Engineering Institute of Aircraft Systems, China
  13:30 14:00 9.9.2 APPLICATION OF DEVELOPMENT ASSURANCE METHODOLOGIES TO ELECTRONIC ENGINE CONTROL SYSTEM (EECS)
QIN ZHU¹, Chunxiao Wang¹; ¹AECC Commercial Aircraft Engine Co. Ltd, China
  14:00 14:30 9.9.3 RESEARCH ON CERTIFICATION MANAGEMENT OF AIRCRAFT ENGINE BASED ON RISK ANALYSIS
C.X. Wang¹, Q. Zhu¹, X.K. Wang¹, X.H. Tang¹; ¹AECC Commercial Aircraft Engine Co. Ltd, China
  14:30 15:00 9.9.4 STUDY ON THE AIRWORTHINESS AND COMFORTABLENESS REQUIREMENTS OF AIRCRAFT CABIN AIR CONTAMINATIONS
H. Tao, CAPEChina Aero-Polytechnology Establishment, China; L. Haixia¹, Y. Ning¹; ¹China Aero-Polytechnology Establishment, China
Presenter: Tao Hu, CAPE
  15:00 15:30 9.9.5 NUMERICAL ANALYSIS METHOD OF CIVIL AIRCRAFT DITCHINGFLOATING PERFORMANCE
H. Wang¹, H. Wang¹; ¹Shanghai Aircraft Design and Research Institute, China
10.9Flight Dynamics 1
Chair: T. Götzendorf Grabowski
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  13:00 13:30 10.9.1 VIRTUAL FLIGHT TEST OF A BWB AIRCRAFT IN LOW SPEED WIND TUNNEL
B. Nie¹, F. Cen¹, Z. Liu¹, T. Guo¹, H. Sun¹; ¹China Aerodynamics Research and Development Center, China
  13:30 14:00 10.9.2 BAYESIAN APPROACH TO SIMULTANEOUS STATIC AND DYNAMIC FLIGHT CHARACTERISTICS MODELING
M. Naruoka, JAXA, Japan
  14:00 14:30 10.9.3 THE ANALYSIS OF TAKEOFF ROTATION OF SUBSCALE FREE-FLIGHT
K. MA¹, L.-B. WANG¹, H. DU¹, W. WANG¹, W.-T. GU¹; ¹AVIC THE FIRST AIRCRAFT INSTITUTE, China
Presenter: KUN MA, AVIC THE FIRST AIRCRAFT INSTITUTE
  14:30 15:00 10.9.4 ESTIMATION OF WIND BY ESTIMATING DERIVATIVES OF A LATERAL-DIRECTIONAL MOTION MODEL
L.H. Son¹, Y. Ochi¹; ¹National Defense Academy, Japan
Presenter: Luu Son, National Defense Academy
11.9Measurement Techniques & Data Analysis
Chair: W. Jujun
Track 11
03.2 - Experimental Aerodynamics
  13:00 13:30 11.9.1 AN OBJECTIVE APPROACH FOR MEASURING INTERMITTENCY IN THE TRANSITIONAL BOUNDARY LAYER
D. Veerasamy, Khalifa University, United Arab Emirates; C. Atkin, University of East Anglia, United Kingdom
Presenter: Chris Atkin, University of East Anglia
  13:30 14:00 11.9.2 DYNAMIC TRAILING-EDGE FLAP MOVEMENT AS A NON-CONVENTIONAL AERODYNAMIC LIFT MECHANISM
M. Bremm¹, R. Stephan¹, R. Hörnschemeyer¹, E. Stumpf¹; ¹RWTH Aachen University, Germany
Presenter: Martin Bremm, RWTH Aachen University
  14:00 14:30 11.9.3 APPLIED RESEARCH ON SUPERVISED LEARNING IN THE JUDGMENT OF AIRFOIL TRANSITION
Binbin Wei¹, Yongwei Gao¹, Dong Li¹; ¹Northwestern Polytechnical University, China
  14:30 15:00 11.9.4 TOTAL TEMPERATURE MEASUREMENTS IN WATER INJECTION AND PRE-COMPRESSOR COOLING TECHNOLOGY
X. Geng¹, X.P. Liu¹, Z.Y. Song¹, L. Zhang¹; ¹AECC Shenyang Engine Research Institute, China
  15:00 15:30 11.9.5 MICROPHONE ARRAY TECHNIQUES FOR TRAILING EDGE NOISE BASED ON CONVOLUTIONAL NEUTRAL NETWORK
Z.C. Song¹, P.Q. Liu¹, H. Guo¹; ¹Beihang Univerisity, China
1.10Hybrid/Electric & Unconventional Aircraft 3
Chair: K. Rinoie
Track 1
01 - Aircraft Design and Integrated Systems
  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
Presenter: David Funes Sebastian, Airbus Defence & Space
  08:30 09:00 1.10.2 LANDING PLATFORM FOR URBAN AIR MOBILITY VEHICLES INTEGRATED INTO PARKING LOT INFRASTRUCTURE IN DENSELY BUILT-UP AREAS
P. Brusberg¹, A.C. Doberts¹, T.M. Jansen¹, T. Witt¹; ¹HAW Hamburg, Germany
  09:00 09:30 1.10.3 CIRCULATION CONTROL AIRCRAFT - RECENT DEVELOPMENTS OF THE CHANNEL WING DESIGN
Mohd Faisal Abdul Hamid¹, Abd. Rahim Abu Talib¹, Azmin Shakrine Mohd Rafie¹, Harijono Djojodihardjo, The Institute for the Advancement of Aerospace Science and Tech, Indonesia; ¹Universiti Putra Malaysia, Malaysia
2.1010 years of IFAR
Chair: B. Nagel
Track 2
15 - Guest lectures
  08:00 08:30 2.10.1 IFAR - INFRASTRUCTURE DATABASE
R. Degenhardt, DLR, Germany; D. Paraschivoiu, NRC, Canada
  08:30 09:00 2.10.2 SOL-GEL BASED ORGANIC-INORGANIC HYBRID COATINGS FOR CORROSION PROTECTION OF AEROSPACE ALUMINIUM ALLOY
R.V. Lakshmi¹, S.T. Aruna¹, S. Sampath, Indian Institute of Science, India; ¹CSIR-National Aerospace Laboratories, India
3.10Compressor and Fan Aerodynamics 2
Chair: D. Zingg
Track 3
03.1 - Aerodynamics – CFD Methods and Validation
  08:00 08:30 3.10.1 APPLICATION OF A SKEWED-SLOT CASING TREATMENT IN A HIGH-LOADING AXIAL-CENTRIFUGAL COMPRESSOR
H.-L. Jin, China; D.-B. Qiu, China; Y.-Q. Yin, China; X.-Q. Zou, China
  08:30 09:00 3.10.2 DISTORTION PLATE DESIGN, SIMULATION VALIDATION AND TEST SCHEME FOR STABILITY ANALYSIS ON A FAN COMPONENT OF AN AEROENGINE
Z.-P. Li, AECC Shenyang Engine Research Institute, China
  09:00 09:30 3.10.3 EFFECT OF INTER-STAGE BLEEDING ON FLOW STABILITY OF A MULTI-STAGE COMPRESSOR
Xiwu LIU, China; Hailiang JIN, China; Daobin QIU, China; Yueqian Yin, China
Reserve Paper (Interactive) 3.10.R CFD OPTIMUM DESIGN OF SUPERSONIC EJECTOR SYSTEM STRUCTURE OF TEST CELL
Jinyou SU, China; Zhili TANG, China; Jinhu TIAN, China; Biao PAN, China; Shaojun LUO, China
Presenter: SU JINYOU
4.10Applied CFD 3
Chair: J. Azevedo
Track 4
03.1 - Aerodynamics – CFD Methods and Validation
  08:00 08:30 4.10.1 GEOMETRICAL PARAMETER STUDY OF A HYPERSONIC VERTICAL GAP FLOW
H.-Y. Zhang, State Key Laboratory of Aerodynamics, China; W.-G. Zong¹, Y.-H. Zhu¹, Y.-W. Gui, Computational Aerodynamics Institute, CARDC, China; B. Qiu, State Key Laboratory of Aerodynamics, China; ¹University of Sichuan, China
Presenter: Yuanhao Zhu, Sichuan University
  08:30 09:00 4.10.2 ATMOSPHERIC TURBULENCE EFFECTS ON SONIC BOOM PROPAGATION
Z. Qian¹, Y. Leng¹; ¹AVIC Aerodynamics Research Institute, China
  09:00 09:30 4.10.3 NUMERICAL SIMULATION OF PITCHING MOTION EFFECTS ON THE AERODYNAMIC PERFORMANCE OF DRAGONFLY-LIKE FLAPPING WING
X.-Y. Lang¹, B.-F. Song¹, W.-Q. Yang¹; ¹Northwestern Polytechnical University, China
Reserve Paper (Interactive) 4.10.R NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING WITH SLOTTED-TIP
D. Liu, School of Aeronautics,Northwestern Polytechnical University, China; W.Q. Yang¹, B.F. Song¹; ¹Research & Development Institute of NWPU in Shenzhen, China
5.10Transonic/Supersonic
Chair: S. Prince
Track 5
03.2 - Experimental Aerodynamics
  08:00 08:30 5.10.1 INFLUENCE OF VARIABLE WALL PERFORATION RATIO ON BOUNDARY LAYER PARAMETERS AT TRANSONIC SPEEDS
S. Osipova, Russia
Reserve Paper (Interactive) 5.10.R A STUDY OF SONIC BOOM TEST WITH NOZZLE PLUME INTERACTIONS
X. Li¹, Z. Liu¹, Z. Qian¹; ¹AVIC Aerodynamics Research Institute, China
6.10UAV Dynamics and Control 2
Chair: T. Götzendorf-Grabowski
Track 6
06.2 - Flight Dynamics and Control (UAV related)
  08:00 08:30 6.10.1 PERCHING PRINCIPLES ANALYSIS OF POST-STALL PERCHING UNMANNED AERIAL VEHICLE
S. Yang, Northwestern Polytechnical University, China; C. Min ¹, B. Junqiang¹; ¹NWPU, China
  08:30 09:00 6.10.2 DEVELOPMENTS TOWARDS A TOOLCHAIN FOR UAV FLIGHT DYNAMIC MODELS IN EARLY DESIGN
S.J. Koeberle¹, M. Hornung¹; ¹Institute of Aircraft Design, TUM, Germany
  09:00 09:30 6.10.3 NEW ROLL-SPIRAL COUPLING MODE CRITERION FOR HIGH-SPEED VEHICLES
G.H. Dou¹, Y.J. Yang¹, A.L. Gong¹, W.J. Zhou¹; ¹China Academy of Aerospace Aerodynamics, China
7.10Stability
Chair: R. Wahls
Track 7
03.4 - Applied Aerodynamics
  08:00 08:30 7.10.1 NUMERICAL EVALUATION OF DYNAMIC STABILITY DERIVATIVES FOR HIGH LIFT DEVICES
H. Ur Rahman¹, A. Maqsood¹, R. Riaz¹, L. Dala, Northumbria University, United Kingdom; ¹National University of Sciences & Technology, Pakistan
Presenter: Hamood Ur Rahman, Research Center for Modelling and Simulation, NUST Islamabad
  08:30 09:00 7.10.2 ADJOINT-BASED STUDY OF THE AERODYNAMIC CENTER SHIFT IN THE TRANSONIC FLOW REGIME
A. Cato¹, M. Hayashi, Federal University of ABC, Brazil; J. Cavalcante¹, J. Qasem, Technical University of Munich, Germany; L. Kavabata¹, U. Costa¹, E. Volpe¹; ¹University of São Paulo, Brazil
Presenter: Arthur Cato, University of São Paulo
  09:00 09:30 7.10.3 NASA-CRM LATERAL-DIRECTIONAL STABILITY DERIVATIVES COMPARISON BETWEEN SEMI-EMPIRICAL, VORTEX LATTICE AND PANEL METHOD
R. Sorbilli Cardoso de Sousa¹, R.G. Annes da Silva¹; ¹Instituto Tecnologico de Aeronautica, Brazil
8.10Static Analysis of Aircraft Structures
Chair: E. Zappino
Track 8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
  08:00 08:30 8.10.1 MATHEMATICAL MODELS FOR ANALYSIS AND OPTIMIZATION OF AIRCRAFT STRUCTURAL COMPONENTS TAKING INTO CONSIDERATION OF LOCAL STRESS DISTRIBUTION
V. Chedrik¹, S. Tuktarov¹, K. Balunov¹, V. Nguyen, Moscow Institute of Physics and Technology, Russia; ¹Central Aerohydrodynamic Institute, Russia
  08:30 09:00 8.10.2 A METHOD FOR CALCULATING TORSION ANGLE OF FLEXIBLE RETICULAR TUBE AT DIFFERENT POSITIONS
Y.C. Deng, SADRI, China; Y. Yang, ASRI, China; Y.Q. He, SIA, China; C. Sun, CAE, China; F.H. Qui, SAU, China
  09:00 09:30 8.10.3 SPECIALIZED SOFTWARE DEVELOPMENT FOR BUILDING BLOCK APPROACH INTEGRATION IN FULL-SCALE STATIC TESTS
E.M. Kolman¹, D.V. Kurulyuk¹, E.A. Levchenko¹, M.V. Limonin¹; ¹Central Aerohydrodynamic Institute named after N.E. Zhukovsky, Russia
Reserve Paper (Interactive) 8.10.R THE FINITE ELEMENT MODELLING OF BOLTED STRUCTURE BETWEEN SELECTIVE LASER MELTING ALUMINIUM AND COMPOSITE PLATES
Shiquan Bi¹, Hao Cui¹, L.Y. Liu¹; ¹Shenyang Aircraft Design and Research Institute of AVIC, China
9.10Avionics and Aircraft Systems
Chair: P. Krus
Track 9
07 - Systems, Subsystems and Equipment
  08:00 08:30 9.10.1 FITT’S LAW WITH EYE TRACKING ON A FLIGHT SIMULATOR COCKPIT
M.A. Rodriguez Diaz¹, E. Villani¹, P. Krus, Linköping University, Sweden; ¹Aeronautics Institute of Technology, Brazil
  08:30 09:00 9.10.2 ANALYSIS AND SOLUTION RESEARCH OF THE AIR DATA LOSSFROM AIRCRAFT FOR ENGINE CONTROL
L. Jing, COMAC Sadri, China
  09:00 09:30 9.10.3 AN AGILE PRACTICE OF AVIONICS SYSTEM DEVELOPMENT
L. Dong¹, W.-M. Song¹; ¹China Aeronautical Radio Electronics Research Institute, China
Presenter: Lei Dong
10.10Fan / Nacelle & Propeller 2
Chair: A. Mirzoyan
Track 10
05 - Propulsion
  08:00 08:30 10.10.1 AERODYNAMICS DESIGN, OPTIMIZATION AND FLOW FIELD INVESTIGATION OF A CONTRA-ROTATING PROPFAN AT HIGH FLIGHT MACH NUMBERS
T. Wu¹, Z. Li¹, W. Dong¹; ¹Shanghai Jiao Tong University, China
Presenter: ZhiDa Li, Shanghai JiaoTong University
  08:30 09:00 10.10.2 STUDY OF NON-ROTATING MICROPHONE ARRAY FOR SPINNING DUCT MODE DETECTION
J.Y. Ying¹, X.B. Wang¹, J. Kang¹, M.H. Lu¹; ¹AECC commercial Aircraft Engine Co.,Ltd., China
  09:00 09:30 10.10.3 MODELING OF COUNTER-ROTATING LIFT FAN/MAIN ENGINE COMBINED PROPULSION SYSTEM AND LIFT FAN AERODYNAMIC DESIGN
H.-L. Jin, China; X. Chen, China; D.-B. Qiu, China; Y.-Q. Yin, China
Reserve Paper (Interactive) 10.10.R A DESIGN METHOD OF AN AXISYMMETRIC HYPERSONIC INLET INTERGRATED WITH A LONG FOREBODY
S.C. Xu¹, Y. Wang¹, Z.G. Wang¹, X.Q. Fan¹, B. Xiong¹; ¹National University of Defense Technology, China
11.10Fault Detection
Chair: Y. Wang
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
  08:00 08:30 11.10.1 LEARNING FLIGHT CONTROL SKILLS BY IMITATING EXPERT DEMONSTRATIONS
R. Takase, The University of Tokyo, Japan
  08:30 09:00 11.10.2 FEEDBACK ERROR LEARNING WITH ENHANCED SAMPLING: NEURAL FAULT TOLERANT CONTROLLER OF AIRCRAFT
N. Yoshikawa, Mitsubishi Electric, Japan; S. Suzuki, The university of Tokyo, Germany
1.11Wing Design
Chair: J. Melkert
Track 1
01 - Aircraft Design and Integrated Systems
  10:00 10:30 1.11.1 VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WING
Gang Song¹, Wenyuan Cheng¹, Yu Yang², Zhansen Qian³, Wenjie Ge*, Yonghong Zhang*, Zhigang Wang², Sheng Zhang², Xintong Shi², Chunpeng Li³; ¹Aviation Industry Development Research Center of China, China ;²Aircraft strength research Institute of China, China ;³AVCI Aerodynamics Research Institute, China ;*Northwestern Polytechnical University, China
Presenter: Gang SONG, Aviation Industry Development Research Center of China (ADR)
  10:30 11:00 1.11.2 EVALUATION AND VALIDATION OF AEROELASTIC ANALYSIS PROGRAM FOR THE “AEROSTRUCT” WING OPTIMIZATION PLATFORM
S.-B. Ling¹, K.-S. Zhang, Northwestern polytechnical university, China; Z.-H. Han¹, Z.-J. Gao, Xiantianjihangtong Technology CO. Ltd., China; ¹Northwestern Polytechnical university, China
  11:00 11:30 1.11.3 ON WINGS WITH NON-ELLIPTIC LIFT DISTRIBUTIONS
E. Bragado-Aldana¹, M. M. Lone¹, A Riaz¹; ¹Cranfield University, United Kingdom
  11:30 12:00 1.11.4 A HIERARCHICAL STRUCTURAL MODEL FOR CONCEPTUAL DESIGN OF TRANSPORT AIRCRAFT WING
Y.K. Yin¹, W.B. Song¹; ¹Shanghai Jiao Tong University, China
  12:00 12:30 1.11.5 MULTIFIDELITY AERODYNAMIC/STEALTH DESIGN OPTIMIZATION METHOD FOR FLYING WING AIRCRAFT
Z.-Q Liu¹, W.-P Song¹, Z.-H Han¹, Y. Wang¹; ¹Northwestern Polytechnical University, China
Reserve Paper (Interactive) 1.11.R THE STUDY ON ANTI-ICING AREAS OF LEADING-EDGE SLATS IN MODERN CIVIL AIRCRAFT
G.P. Qian¹, Y.H. Wang¹, C. Ma¹; ¹COMAC, China
2.11Design Methods
Chair: K. Rinoie
Track 2
01 - Aircraft Design and Integrated Systems
  10:00 10:30 2.11.1 IMPACT OF NEW TECHNOLOGIES ON AIRCRAFT SYSTEMS
A. Berres¹, P. Niemeyer¹; ¹German Aerospace Center (DLR), Germany
  10:30 11:00 2.11.2 FAST METHOD AND AN INTEGRATED CODE FOR SONIC BOOM PREDICTION OF SUPERSONIC COMMERCIAL AIRCRAFT
Y.-L. Ding¹, Z.-H. Han¹, J.-L. Qiao¹, W.-P. Song¹, B.-F. Song¹; ¹Northwestern Polytechnical University, China
  11:00 11:30 2.11.3 INTEGRATION OF FUSELAGE-MOUNTED OVER-WING ENGINES ON A MID-RANGE AIRCRAFT
P. Wegener, DLR - German Aerospace Center, Germany
  11:30 12:00 2.11.4 AERODYNAMIC DESIGN OPTIMIZATION OF WAVERIDER-DERIVED VEHICLE
W. Su ¹, C. Dong¹, X.P. Wang, Shanghai Electro-Mechanical Engineering Institute, Shanghai, China; Y.T. Zuo, National Key Laboratory of Aerodynamic Design and Research, Nort, China; ¹Beijing Institute of Space Long March Vehicle, China
  12:00 12:30 2.11.5 MULTI-MISSION TANKER-TRANSPORT CONVERSION
I. Berlowitz, IBAero Engineering, Israel
Presenter: Ilan Berlowitz, IBAero Engineering
Reserve Paper (Interactive) 2.11.R AN ADJOINT-BASDF AERO-STRUCTURAL DESIGN OPTIMIZATION METHOD USING DYNAMIC MESH TECHNOLOGY
Guo Jingrui¹, Li Yi, School of Aeronautics, Northwestern Polytechnical University, China; Xu Min¹; ¹School of Astronautics, Northwestern Polytechnical University, China
3.11Transition
Chair: L. Alves
Track 3
03.1 - Aerodynamics – CFD Methods and Validation
  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
Presenter: Yiming Du, Shenyang Aerospace University
  10:30 11:00 3.11.2 A CONTRIBUTION TO THE SIMULATION OF TRANSITIONAL FLOWS OVER AEROSPACE CONFIGURATIONS
L.M.M.O. Carvalho, Instituto Tecnologico de Aeronautica, Brazil; R.G. da Silva¹, J.L.F. Azevedo¹; ¹Instituto de Aeronautica e Espaco, Brazil
  11:00 11:30 3.11.3 AERODYNAMICS CHARACTERISTICS STUDY ON A NATURE LAMINAR FLOW AIRFOIL OF NEAR-SPACE VEHICLE AT LOW REYNOLDS NUMBERS
F. Cui, Innovation & Research Institute of HIWING Technology Academy, China; H. Zhang, HIWING Technology Academy, China
  11:30 12:00 3.11.4 HYBRID NUMERICAL SCHEMES IN PREDICTION OF HIGH-SPEED LAMINAR-TURBULENT TRANSITION
I.V. Egorov, Russia; A.V. Novikov, Russia; N.K. Nguen, Vietnam
  12:00 12:30 3.11.5 A LOCAL CORRELATION-BASED ALGEBRAIC TRANSITION MODEL WITH COMPRESSIBILITY AND CROSSFLOW CORRECTION
R.X. Xie¹, W.M. Sang¹; ¹Northwestern Polytechnical University, China
4.11Numerical Methods 2
Chair: T. Wan
Track 4
03.1 - Aerodynamics – CFD Methods and Validation
  10:00 10:30 4.11.1 MODELING AND SIMULATION OF DUSTY GAS FLOW IN AERODYNAMICS
Y.M. Tsirkunov¹, D.A. Romanyuk¹, S.V. Panfilov¹; ¹Baltic State Technical University, Russia
  10:30 11:00 4.11.2 AN INTELLIGENT STRUCTURED CHIMERA GRID APPROACH FOR MOVING OBJECTIVES
L. Li, Northwestern Polytechnical University, China; L. Liang¹, Y. Huai¹; ¹AVIC Aeronautics Computing Technique Research Institute , China
  11:00 11:30 4.11.3 METHODS OF DIRECTIONAL COARSENING FOR UNSTRUCTURED GRIDS AND APPLICATIONS
Z.-Y. Xiao¹, L. Zhang¹, X.-D. Cui¹, B. Mou¹; ¹China aerodynamics research and development center , China
  11:30 12:00 4.11.4 AN ACCELERATION METHODOLOGY BASED ON DISTURBANCE REGION UPDATE METHOD FOR STEADY COMPRESSIBLE FLOWS
S. Hu¹, C. Jiang¹, Z. Gao¹, C. Lee¹; ¹Beihang University, China
5.11Full Configuration Test
Chair: Y. Chen
Track 5
03.2 - Experimental Aerodynamics
  10:00 10:30 5.11.1 EXPERIMENTAL INVESTIGATION OF DAMAGE WING IMPACT ON THE AIRLINER AERODYNAMIC CHARACTERISTICS
A. Krzysiak, Lukasiewicz Research Network – Institute of Aviation, Poland; A. Olejnik¹, L. Kiszkowiak¹; ¹Faculty of Mechatronics, Armament & Aerospace; Military Universi, Poland
  10:30 11:00 5.11.2 WIND-TUNNEL INVESTIGATION OF COMMERCIAL TRANSPORT AIRCRAFT STATIC AND DYNAMIC AERODYNAMIC CHARACTERISTICS AT EXTREME FLIGHT CONDITIONS
L. Zhang, Beihang University, China; Z. Liu¹, F. Cen¹, Y. Jiang¹, H. Sun¹; ¹China Aerodynamic Research and Development Center, China
Presenter: LEI ZHANG, Beihang University
  11:00 11:30 5.11.3 EXPERIMENTAL INVESTIGATION OF THE CHN-T1 MODEL IN FL-13 WIND TUNNEL OF CARDC AND DNW-LLF FACILITY
L. Fan¹, H. Zhang¹; ¹China Aerodynamics Research and Development Center, China
  11:30 12:00 5.11.4 STUDY ON AERODYNAMIC CHARACTERISTICS OF LIGHT CONVERTIBLE AIRCRAFT MODEL
V.I. Chernousov¹, A.A. Krutov¹, E.A. Pigusov¹; ¹Central Aerohydrodinamic Institute (TsAGI), Russia
  12:00 12:30 5.11.5 EXPERIMENTAL INVESTIGATIONS OF A FULL MODEL WITH ADAPTIVE ELASTO-FLEXIBLE MEMBRANE WINGS
Jonathan Pflüger¹, Kevin Hirschmann¹, Christian Breitsamter¹; ¹Chair of Aerodynamics and Fluid Mechanics, TUM, Germany
6.11Design of Aircraft Strutcures 2
Chair: J.H. Han
Track 6
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
  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
Presenter: Chuanguang Yang, China Helicopter Design and Research Institute
  10:30 11:00 6.11.2 ON THE DEVELOPMENT OF FUSELAGE WEIGHT ESTIMATION TOOLINTO AIRCRAFT MULTIDISCIPLINARY DESIGN ENVIRONMENT
H. Wang¹, H. Wang¹; ¹Shanghai Aircraft Design and Research Institute, China
  11:00 11:30 6.11.3 AN INTEGRATED AERODYNAMIC/THERMAL/STRUCTURAL DESIGN FRAMEWORK FOR HYPERSONIC VEHICLES
C. Li¹, Z.Q. Wan¹, X. Wang¹; ¹Beihang University, China
  11:30 12:00 6.11.4 A DYNAMIC SELF-CONTROL ERR STRATEGY FOR BI-DIRECTIONAL EVOLUTIONARY STRUCTURAL OPTIMIZATION
H. Zhang¹, Q. Zhang¹; ¹Sun Yat-sen University, China
  12:00 12:30 6.11.5 DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: STRUCTURAL DESIGN AND OPTIMIZATION
C. Surace¹, R. Roy¹, M. Civera¹, D. Allaio¹, R. Barbieri¹, A. Grava¹, R. Tufilli¹, P. Gilli¹; ¹Politecnico di Torino, Italy
Reserve Paper (Interactive) 6.11.R BIONIC LIGHT-WEIGHT GRID SURFACE WING STRUCTURE DESIGN FOR A SOLAR-POWERED UAV
Y. Ding, China; Z. Zhou, China; H.J. Liu, China
7.11Optimization 2
Chair: R. Wahls
Track 7
03.4 - Applied Aerodynamics
  10:00 10:30 7.11.1 SPARSE POLYNOMIAL CHAOS EXPANSION BASED ON FULLY ADAPTIVE FORWARD-BACKWARD SELECTION METHOD
H. Zhao, Sun Yat-sen University, China; Z.H. Gao¹, L. Xia¹; ¹Northwestern Polytechnical University, China
  10:30 11:00 7.11.2 RAPID THEORETICAL EVALUATION OF FORMATION FLIGHT PERFORMANCE
R. Vilumbrales-Garcia¹, M. Lone¹; ¹Cranfield University, United Kingdom
Presenter: Rodrigo Vilumbrales, Cranfield University
  11:00 11:30 7.11.3 IMPROVED WEIGHTED GRADIENT-ENHANCED KRIGING MODEL FOR HIGH-DIMENSIONAL AERODYNAMIC MODELING PROBLEMS
C.-Z. Xu¹, Z.-H. Han¹, K.-S. Zhang¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China
  11:30 12:00 7.11.4 DESIGN OPTIMIZATION OF AIRFOILS AT ULTRA-LOW REYNOLDS NUMBERS
J.-H. Xu¹, D. Li¹, W.-P. Song¹, Z.-H. Han¹, H.-J. Li¹; ¹Northwestern Polytechnical University, China
  12:00 12:30 7.11.5 THE AERODYNAMIC OPTIMIZATION AND TRIM CHARACTERISTICS RESEARCH ON VARIABLE CAMBER WING OF WIDE-BODY CIVIL TRANSPORT
X. Hao¹, C. Su¹, B. Wang¹, Q.Q. Zhang¹; ¹China Academy of Aerospace Aerodynamics, China
8.11Vibration and Damping
Chair: E. Zappino
Track 8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
  10:00 10:30 8.11.1 STRUCTURAL VIBRATION CONTROL BY USING THE ENERGY FROM DIFFERENT MODES
K. Li¹, C. Bai¹; ¹Aircraft strength research institute, China
  10:30 11:00 8.11.2 MODEL REDUCTION AND STOCHASTIC UPDATING OF A VIBRATING SYSTEM
I. Isnardi¹, E. Menga, Airbus Operations S.L, Spain; J.E. Mottershead¹, S. Fichera¹; ¹University of Liverpool, United Kingdom
  11:00 11:30 8.11.3 MODAL DAMPING PARAMETER IDENTIFICATION METHOD BASED ON IMPROVED VMD AND ENVELOPE FITTING AND ITS APPLICATION
J. Bian¹, Y.-N. Chen¹, Q. Mei¹, Y.-L. Xu¹, Y.-H. Lu¹; ¹AECC Hunan Aviation Powerplant Research Institute, China
  11:30 12:00 8.11.4 A PERTURBATION ANALYSIS OF NONLINEARITY IN LANDING-GEAR SHIMMY OF A FLEET AIRCRAFT
M. Kou, AECC CAE, China; J. Zhang¹, J. Lu¹, S. Tan¹; ¹AVIC The First Aircraft Institute, China
  12:00 12:30 8.11.5 NUMERICAL SIMULATION AND EXPERIMENTAL INVESTIGATION ON FLUTTER AND NON-SYNCHRONOUS VIBRATION
Y.X. Liu¹, D. Mo¹, Q. Du¹, Y.Z. Chen¹, M. Wang¹; ¹AECC Shenyang Engine Research Institute, China
Reserve Paper (Interactive) 8.11.R DESIGN AND PERFORMANCE RESEARCH OF ARTIFICIAL ELECTROMAGNETIC STRUCTURE WITH TRANSMISSION AND ABSORPTION CHARACTERISTICS
Pang Xiaoyu, China
9.11Actuator design & Analysis
Chair: J. Mare
Track 9
07 - Systems, Subsystems and Equipment
  10:00 10:30 9.11.1 CONCEPTUAL STUDY OF THE DIGITAL HYDRAULIC ACTUATOR WITH PROPORTIONAL CONTROL FOR FLIGHT CONTROL ACTUATION SYSTEMS
A. Dell'Amico, Saab AB/Linköping University, Sweden; F. Larsson¹, C. Johansson¹, V. De Negri, Federal University of Santa Catarina, Brazil; P. Krus, Linköping University, Sweden; ¹Saab AB, Sweden
  10:30 11:00 9.11.2 VIRTUAL PROTOTYPING OF ELECTRICAL THSA FOCUSED ON MECHANICAL POWER TRANSMISSION FUNCTIONS
J. Fu¹, C. Zheng¹, J.-C. Mare, Institute Clément Ader (CNRS UMR 5312), INSA-Toulouse, France; W. Zhang¹; ¹School of Mechanical Engineering and Automation, Beihang Univ., China
  11:00 11:30 9.11.3 THE DEVELOPMENT OF ALGORITHMS FOR EMA FAULT EARLY DETECTION SYSTEM
S.G. Bazhenov¹, G.S. Veresnikov, Institute of Control Science of Russian Academy of Science, Russia; A.V. Skryabin¹; ¹Central Aerohydrodynamic Institute of Russia, Russia
  11:30 12:00 9.11.4 AN ONTOLOGICAL APPROACH FOR CLASSIFYING AIRCRAFT ACTUATORS
F. Larsson¹, C. Reichenwallner², A. Dell'Amico¹, P. Krus²; ¹Saab AB, Sweden ;²Linköping University, Sweden
  12:00 12:30 9.11.5 EVALUATION ASPECT MAPPING FOR ACTUATION SYSTEM DESIGN
C. Reichenwallner¹, F. Larsson², A. Dell 'Amico², P. Krus¹; ¹Linköping university, Sweden ;²Saab AB, Sweden
10.11MDO & More / Hybrid / Electric Propuslion
Chair: M. Fioriti
Track 10
05 - Propulsion
  10:00 10:30 10.11.1 RESEARCH OF PROPULSION-SYSTEM-SURROGATE-MODELING METHOD USING INFILL CRITERION SAMPLES
D.-C. Wang¹, B.-F. Song¹, H.-F. Wang¹, J. Jiao, Chinese Academy of Sciences, China; ¹Northwestern Polytehnical University, China
  10:30 11:00 10.11.2 THE CAPABILITIES OF AUTOMATION OF MDAO PROBLEM STATEMENT AT COLLABORATIVE CONCEPTUAL DESIGN OF THE PROPULSION SYSTEM USING OPEN SOURCE SOFTWARE TOOLS
L. Mirzoyan¹, A. Mirzoyan¹, A. Isyanov¹; ¹CIAM, Russia
Presenter: Artur Mirzoyan, CIAM
  11:00 11:30 10.11.3 CONCEPTUAL STUDIES OF DIFFERENT TYPE OF HYBRID ELECTRIC PROPULSION SYSTEMS FOR COMMUTER AIRLINERS
V.S. Zakharchenko¹, A.N. Varyukhin¹, D.Y. Rakhmankulov¹, P.S. Suntsov¹, M.A. Ovdienko¹, M.V. Gordin¹; ¹Central Institute of Aviation Motors (CIAM), Russia
  11:30 12:00 10.11.4 IMPLEMENTATION OF DISTRIBUTED ELECTRIC PROPULSION ON A GENERAL AVIATION AIRCRAFT
M.A. Gallani¹, L.C.S. Góes¹, L.A.R. Nerosky, Embraer, Brazil; ¹Instituto Tecnológico de Aeronáutica, Brazil
Presenter: Murilo Augusto Gallani, Instituto Tecnológico de Aeronáutica
  12:00 12:30 10.11.5 INVESTIGATION OF VARIABLE GEOMETRIES ON THE OPERABILITY AND AIRCRAFT LEVEL PERFORMANCE OF A THREE-SHAFT TURBOFAN ENGINE FOR ENTRY INTO SERVICE 2050
D. Mo¹, Y.X. Liu¹, I. Roumeliotis², D. Nalianda²; ¹AECC Shenyang Engine Research Institute, China ;²Cranfield University, United Kingdom
Reserve Paper (Interactive) 10.11.R A SIMPLIFIED MODEL FOR THE SIMULATION OF SYNERGISTIC AIR-BREATHING ROCKET ENGINE
X. Yang¹, Q. Yang¹, W. Dong¹; ¹Shanghai Jiao Tong University, China
11.11Nonlinear Control
Chair: T. Rogalski
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
  10:00 10:30 11.11.1 AIRCRAFT AUTOPILOT DESIGN USING ASYMMETRIC VARIABLE-SPAN WING MORPHING
J. Lee¹, S. Kim¹, S. Jung¹, H. Lee¹, Y. Kim¹; ¹Seoul National University, South Korea
  10:30 11:00 11.11.2 AUTONOMOUS FLIGHT CONTROL BASED ON NEURAL NETWORKS AND FUZZY DECISION
P.C. Wen, China; C.H. Zou, China; Z. Gao, China; J.G. Sun, China
Presenter: Pengcheng WEN, AVIC Xi’an Aeronautics Computing Technique Research Institute
  11:00 11:30 11.11.3 TWISTOR BASED 6-DOF DISTRIBUTED ADAPTIVE LEADER-FOLLOWING CONTROL FOR MULTIPLE RIGID SPACECRAFT FORMATION
B. Zhang¹, F. Li, China Academy of Launch Vehicle Technology, China; J. Bai¹; ¹Northwestern Polytechnical University, China
  11:30 12:00 11.11.4 DEVELOPMENT OF A HUMAN PILOTED AIR COMBAT ENGAGEMENT DATABASE
T. Xue¹, J. Ma¹, J. Wen¹, X. Yang, Science and Technology on Avionics Integration Laboratory, China; Y. Dong¹, J. Ai¹; ¹Fudan University, China
  12:00 12:30 11.11.5 LEARNING-BASED MIDCOURSE GUIDANCE FOR VELOCITY MAXIMIZATION WITH ANGULAR CONSTRAINT
T. Jin¹, H. Li¹, S. He¹, Y. Li¹; ¹Beijing Institute of Technology, China