Session List
Interactive Presentations
Reserve Papers
Monday, 14. September 2020
RaumTrack 1Track 2Track 3Track 4Track 5Track 6Track 7Track 8Track 9Track 10Track 11Track 12Track 13
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, Yesterday,Today & Tomorrow of AVIC, Yang Wei, China - Chair: S. Suzuki, ICAS President, JP
10:00
10:30
Break
10:30
12:00
1.1
Technology Integration & Testing
2.1
Rotorcraft
3.1
Design architecture & integration methodology 1
4.1
Unsteady Aerodynamics 1
5.1
Adaptive Wings
6.1
Cavity Flows
7.1
Aero Acoustics
8.1
Aeroelastic Experimental Investigation
9.1
Compressors & Turbines
10.1
Computational Aeroelasticity 1
11.1
Aircraft & UAV as Sensor Platform
12.1
Condition Based Maintenance 1
13.1
Education and industry processes
12:00
13:00
Lunch
13:00
14:30
1.2
System of Systems
2.2
Unconventional Configuration
3.2
Design architecture & integration methodology 2
4.2
Unsteady Aerodynamics 2
5.2
Full Configuration Test 1
6.2
Robust Control
7.2
Low Speed Aero
8.2
Aeroelasticity of Morphing Structures
9.2
Controls & Software
10.2
Computational Aeroelasticity 2
11.2
Avionics
12.2
Condition Based Maintenance 2
13.2
Flight Control During Approach
14:30
15:00
Break
15:00
16:30
1.3
HMI & Cabin Design
2.3
10 years of IFAR
3.3
Knowledge based Engineering
4.3
High Speed Flows
5.3
Full Configuration Test 2
6.3
Composite Defect and Damage
7.3
Simulation
8.3
Aeroservoelasticity
9.3
ISABE 1
10.3
Vibration and Damping
11.3
Military Technology
12.3
Flight Operations
13.3
Flight Control and Critical Situations
16:35
18:35
General Lecture 1 - CTO - Chair: J. Azevedo, ICAS PC Chair, BR
Tuesday, 15. September 2020
RaumTrack 1Track 2Track 3Track 4Track 5Track 6Track 7Track 8Track 9Track 10Track 11Track 12Track 13
08:00
09:00
General Lecture 2 - Future needs you – the panel discussion of the skills for aeronautics - Chair: M. Kanerva, ECSC Chair, FI
09:00
10:00
Interactive Presentations
10:00
12:00
1.4
Wing Design
2.4
Cost Assessment
3.4
Global Collaborative Digital Integration in Aviation / IFAR-X challenge
4.4
Aerodynamic Optimization
5.4
Measurement Techniques & Data Analysis
6.4
Developments in Modelling
7.4
Propulsion Airframe Integration 1
8.4
Composite Materials and Structures
9.4
Multi Disciplinary Optimisation (MDO)
10.4
Virtual Testing
11.4
UAV Dynamics and Control 1
12.4
Composite Characterization and Fabrication
13.4
ATC, Pilot & Controller
12:00
13:00
Lunch
13:00
13:45
ICAS Lecture for Innovation in Aeronautics - Electrification - The third revolution in aviation, Cory Combs, USA
14:00
15:30
1.5
Hybrid/Electric & Unconventional Aircraft 1
2.5
Shape Optimization
3.5
System Architecture
4.5
Ice Accretion
5.5
Aeroacoustics & Noise
6.5
Turbulent Flows
7.5
Propulsion Airframe Integration 2
8.5
Fluid Structure Interaction
9.5
More / Hybrid / Electric Propulsion
10.5
Boundary Control
11.5
UAV Conflict Avoidance 1
12.5
Dynamics and Noise
13.5
Systems & Components Safety
15:30
16:00
Break
16:00
18:00
1.6
Design Optimization under Uncertainty
2.6
Hypersonics
3.6
Digital Pioneering - Where will MDO, MBSE, Digital Twins and AI bring engineering in 20 years?
4.6
Turbulence Modeling
5.6
Turbomechanics
6.6
Flow Control Applications 1
7.6
Flapping Wing/MAV
8.6
Buckling and Instability
9.6
Transition Physics 1
10.6
Decoupling Control
11.6
UAV Dynamics and Control 2
12.6
Fatigue Assessment
13.6
Safety and Security Analysis
Wednesday, 16. September 2020
RaumTrack 1Track 2Track 3Track 4Track 5Track 6Track 7Track 8Track 9Track 10Track 11Track 12Track 13
08:00
09:00
General Lecture 3 - Trends in Aircraft Propulsion: Reflections on ISABE 2019 - Chair: Ric Parker, President ISABE,
09:00
09:30
Break
09:30
12:00
1.7
Design Methods
2.7
UAS 1
3.7
Model Based Systems Engineering
4.7
Applied CFD 1
5.7
Transonic/Supersonic
6.7
Unsteady Flow Phenomena
7.7
Optimization 1
8.7
Design of Aircraft Structures
9.7
Advanced Manufacturing
10.7
Flight Dynamics
11.7
Actuator design & Analysis
12.7
Air Traffic Efficiency
13.7
Fan / Nacelle & Propeller
12:00
13:00
Lunch
13:00
13:55
General Lecture 4 - Virtual Aircraft Technology Integration Platform – Results of DLR’s Project VicToria - Chair: Björn Nagel, DLR,
14:00
15:30
1.8
Hybrid/Electric & Unconventional Aircraft 2
2.8
Education & Knowledge Management
3.8
UAV Conflict Avoidance 2
4.8
Numerical Methods 2
5.8
Rotating Wings
6.8
Flow Control Applications 2
7.8
Optimization 2
8.8
Morphing Structures
9.8
Additive Manufacturing
10.8
Flying Quality
11.8
System Health Monitoring
12.8
Airspace Management
13.8
Structural Integrity and Fatigue
15:30
16:00
Break
16:00
18:00
1.9
Hybrid/Electric & Unconventional Aircraft 3
2.9
UAS 2
3.9
AFLoNext
4.9
Applied CFD 2
5.9
Configurations
6.9
Transition Physics 2
7.9
Performance
8.9
Testing and Measurement
9.9
Advanced Manufacturing Management
10.9
Fault Detection
11.9
Aspects of Landing Gear Design
12.9
Airport/Aircraft Operation
13.9
Failure And Fracture Mechanics
Thursday, 17. September 2020
RaumTrack 1Track 2Track 3Track 4Track 5Track 6Track 7Track 8Track 9Track 10Track 11Track 12Track 13
08:00
09:30
General Lecture 5 - IFAR - Zero emissions in 2050 (Chernyshev, Yimer, Peters, Henke) - Chair: D. Mavris, ICAS PPSC Chair, US
09:30
10:00
Break
10:00
12:30
1.10
MDO
2.10
China Aviation
3.10
Transition
4.10
Numerical Methods 1
5.10
Impact
6.10
Student Final
7.10
Laminar Flow
8.10
Failure Analysis and Fatigue
9.10
Combustion & Heat Transfer
10.10
Nonlinear Control
11.10
Aspects of More electric Aircraft
12.10
UAV Navigation
13.10
Airworthiness & Certification
12:30
14:00
Lunch
14:00
15:30
1.11
Hybrid/Electric & Unconventional Aircraft 4
2.11
tbd4
3.11
Compressor and Fan Aerodynamics
4.11
Numerical Methods 3
5.11
UAV Flight Testing
6.11
System Qualification
7.11
Stability
8.11
Static Analysis of Aircraft Structures
9.11
ISABE 2
10.11
Helicopter Control
11.11
Vehicle Mangement Systems
12.11
UTM/On-Demand Mobility
13.11
Operational Training
15:30
16:00
Break
16:00
17:00
von Karman Lecture - Active Flow-, Loads- and Noise Control on Next Generation Wing (AFLoNext) - M.Wahlich - Chair: C. Atkin, ICAS MRSC Chair, GB
17:00
17:30
Closing Ceremony - Chair: Suzuki S. ICAS President JP
1.1Technology Integration & Testing
Chair: B. Nagel
Track 1
01 - Aircraft Design and Integrated Systems
  10:30 11:00 1.1.1 TECHNOLOGY INTEGRATION FOR FUTURE AIRCRAFT CONFIGURATIONS
D. Reckzeh, Airbus, Germany
  11:00 11:30 1.1.2 TECHNOLOGY INTEGRATION AND OVERALL AIRCRAFT PERFORMANCE ASSESSMENT FOR AN ADVANCED MID-RANGE AIRCRAFT
S. Woehler, German Aerospace Center, Germany
  11:30 12:00 1.1.3 MAXIMIZING THE DEGREE OF SIMILITUDE OF SUB-SCALE MODELS TO SUPPORT SCALED FLIGHT TESTING
A Raju Kulkarni, TU Delft, Netherlands
Reserve Paper 1.1.R MULTI-ROLE TANKER-TRANSPORT CONVERSION
Ilan Berlowitz, IBAero Engineering, Israel
2.1Rotorcraft
Chair: J. Melkert
Track 2
01 - Aircraft Design and Integrated Systems
  10:30 11:00 2.1.1 VAST – VERSATILE AEROMECHANICS SIMULATION PLATFORM FOR HELICOPTERS
J. Hofmann, German Aerospace Center (DLR), Germany
  11:00 11:30 2.1.2 HELICOPTER FLIGHT DYNAMICS MODELLING WITH FREE-WAKE METHOD EMBEDDED FOR ROTOR ICING ANALYSES
Guozhi Li¹, Guanglin Zhang¹, Shiyong Chu¹; ¹Aviation Industry Development Research Center of China, China
  11:30 12:00 2.1.3 DESIGN AND ANALYSIS METHOD OF HELICOPTER ANTI-BALLISTIC VULNERABILITY
P. Hou, School of Aeronautics, Northwestern Polytechnical University, China
3.1Design architecture & integration methodology 1
Chair: J. Vian
Track 3
02 - Systems Engineering and Integration
  10:30 11:00 3.1.1 SYSTEM-OF-SYSTEMS DESIGN SPACE REFINEMENT USING MATRIX-BASED APPROACHES
L. Knöös Franzén, Linköping University, Sweden
  11:00 11:30 3.1.2 SYSTEM ARCHITECTING: THE ARCHITECTURE DESIGN PROBLEM AS A GRAPH
J.H. Bussemaker, DLR, Germany
  11:30 12:00 3.1.3 STRATEGIES TO ENHANCE CONFIGURATIONS FOR HIGH-PRECISION MULTI-DISCIPLINARY OPTIMIZATION
L.-H. LIU, Science and Technology on Electro-optic Control Laboratory, Chin, China
Reserve Paper 3.1.R AIRCRAFT CRUISE PERFORMANCE DESIGN INTEGRATION BASED ON SYSTEM ENGINEERING
HBH BIHAI, COMAC/SADRI, China
4.1Unsteady Aerodynamics 1
Chair: O. Mello
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  10:30 11:00 4.1.1 A COMPARISON OF QUASI-STEADY STATE AND UNSTEADY COMPUTATIONAL METHODS FOR PITCH DAMPING DERIVATIVE ESTIMATES
T Bykerk, Australia
  11:00 11:30 4.1.2 NONLINEAR UNSTEADY AERODYNAMIC DESCRIPTIONS BASED ON IMPROVED GOMAN\'S MODEL
J.-Y. YU, China Aerodynamics Research and Development Center, China
  11:30 12:00 4.1.3 DATA FUSION UNSTEADY AERODYNAMIC MODELING BASED ON EXPERIMENTAL DATA
X W Wang, China
Reserve Paper 4.1.R HIGHER ORDER DERIVATIVES OF UNSTEADY AERODYNAMICS OF AIRFOIL ASSOCIATED WITH FORCED PITCHING/PLUNGING MOTIONS
Q ZHANG, Xi'an Aeronautical University, China
5.1Adaptive Wings
Chair: L. Dakai
Track 5
03.2 - Experimental Aerodynamics
  10:30 11:00 5.1.1 EXPERIMENTAL INVESTIGATIONS OF A FULL MODEL WITH ADAPTIVE ELASTO-FLEXIBLE MEMBRANE WINGS
J Pflueger, Technical University Munich, Chair Aerodynamics/Fluidmechanics, Germany
  11:00 11:30 5.1.2 EXPERIMENTAL ANALYSIS OF A BLOWN-WING CONFIGURATION DURING TRANSITION FLIGHT
Y Leng, ISAE, France
  11:30 12:00 5.1.3 WIND TUNNEL ASSESSMENT OF A PASSIVE-ADAPTIVE WING FOR DRAG REDUCTION
C. B. York, Singapore Institute of Technology, Singapore
6.1Cavity Flows
Chair: 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
Y Luo, China
  11:00 11:30 6.1.2 NUMERICAL STUDY OF THE SIDEWALL EFFECTS ON THE OSCILLATORY SHEAR LAYER IN THE CAVITY FLOW OF HIGH REYNOLDS NUMBER
Q.-L. GUO, China
  11:30 12:00 6.1.3 DETACHED-EDDY SIMULATIONS OF LEADING EDGE PLATE FLOW CONTROL BEFORE HIGH-SPEED CAVITY
PC.C Cui, China Aerodynamics Research and Development Center, China
Reserve Paper 6.1.R EXPERIMENTAL STUDY ON SUPERSONIC CAVITY ACOUSTICS
M. JIAN, CADI, China
7.1Aero Acoustics
Chair:
Track 7
03.4 - Applied Aerodynamics
  10:30 11:00 7.1.1 MEDIUM-FIDELITY NOISE ASSESSMENT OF NOVEL MID RANGE TRANSPORT AIRCRAFT
M. Lummer, German Aerospace Center (DLR), Germany
  11:00 11:30 7.1.2 SNGR BASED FAST ANALYSIS OF SLAT TRACK NOISE SOURCES
W Wang, Shanghai Aircraft Design and Research Institute, China
  11:30 12:00 7.1.3 NUMERICAL AND EXPERIMENTAL INVESTIGATION OF A DRESSED NOSE LANDING GEAR
L.-B. Botero-Bolívar, University of São Paulo, Brazil
Reserve Paper 7.1.R INVESTIGATION OF FLOW ACOUSTIC CHARACTERISTICS OF ROTOR-ROTOR INTERACTION FOR MULTICOPTER
Y. Jo, South Korea
8.1Aeroelastic Experimental Investigation
Chair: S. Kuzmina
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  10:30 11:00 8.1.1 TESTING INVESTIGATION OF FLEXIBLE WING LIMIT CYCLES WITH AILERON FREEPLAY NONLINEARITY
X.-F. He, Shanghai Aircraft Airworthiness Certification Center of CAAC, China
  11:00 11:30 8.1.2 EXPERIMENTAL AND THEORETICAL STUDY ON FLUTTER ANALYSIS OF A VERY FLEXIBLE WING
Z.C FU , China Academy of Aerospace Aerodynamics (CAAA), China
  11:30 12:00 8.1.3 THEORETICAL AND EXPERIMENTAL INVESTIGATION OF THE AEROELASTIC CHARACTERISTICS OF THE AFLONEXT PROJECT DEMONSTRATOR
G. A. Amiryants, TsAGI, Russia
9.1Compressors & Turbines
Chair: I. Yimer
Track 9
05 - Propulsion
  10:30 11:00 9.1.1 AERODYNAMC PERFORMANCE IMPROVEMENT OF A TRANSONIC AXIAL COMPRESSOR BY SWEPT AND LEANED ROTORS
K You, Northwestern Polytechnical University, China
  11:00 11:30 9.1.2 FLOW TURBULENCE INVESTIGATION AT THE LINEAR CASCADE’S OUTLET
A.D. Nepomnyashchiy, Central Institute of Aviation Motors, Russia
  11:30 12:00 9.1.3 DESIGN EXPERIENCE OF PENETRATION COOLING SYSTEM FOR HIGH-TEMPERATURE TURBINE BLADES
S. Kharkovskiy, CIAM, Russia
Reserve Paper 9.1.R INFLUENCE OF THE AXIAL ASSEMBLAGE DEVIATION ON PERFORMANCE OF ONE TRANSONIC CENTRIFUGAL COMPRESSOR
Z.-W. Zhang, AECC HAPRI, China
10.1Computational Aeroelasticity 1
Chair: G. Amiryants
Track 10
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  10:30 11:00 10.1.1 A COMPUTATIONAL MODEL OF 3 D.O.F. AIRFOIL FOR FLUTTER ANALYSIS WITH CFD BASED AERODYNAMIC FORCES
A.-O Alam, Dalian university of technology , China
  11:00 11:30 10.1.2 COMPUTATIONAL FLUID-STRUCTURE INTERACTIONS OF A 3D FLEXIBLE FLAPPING WING
Y.-D. Dong, China
  11:30 12:00 10.1.3 COMPUTATION OD ELASTIC FOR A TRANSPORT AIRPLANE FITTED WITH WINGLETS BY FLUID-STRUCTURE INTERACTION
Mattos, B. S. Mattos, Instituto Tecnologico de Aeronautica (ITA), Brazil
11.1Aircraft & UAV as Sensor Platform
Chair: L. Goes
Track 11
07 - Systems, Subsystems and Equipment
  10:30 11:00 11.1.1 SYSTEM OF UNMANNED AERIAL VEHICLES FOR WILD BOARS WITH AFRICAN SWINE FEVER SYMPTOMS DETECTION
K.-S. Sibilski, Air Force Institute of Technology, Poland
  11:00 11:30 11.1.2 VISION-BASED LOCALIZATION OF UAV FOR THE INSPECTION OF WIND TURBINE
T Kato, Graduate School of Tokai University, Japan
  11:30 12:00 11.1.3 EVALUATION OF AN OBSTACLE TRACKING SYSTEM FOR AIRCRAFT GROUND OPERATIONS
K.T. Theuma, University of Malta, Malta
12.1Condition Based Maintenance 1
Chair: L. Molent
Track 12
11 - Operations and Sustainment
  10:30 11:00 12.1.1 STRUCTURAL HEALTH MONITORING – THE ROUTE TO CONDITION BASED MAINTENANCE
J van Doeselaar, Airbus, France
  11:00 11:30 12.1.2 COST AND BENEFIT OF STRUCTURAL HEALTH MONITORING FOR COMMERCIAL AIRCRAFT
D. M. Steinweg, Bauhaus-Luftfahrt e.V., Germany
  11:30 12:00 12.1.3 REAL TIME IMPACT IDENTIFICATION TECHNIQUE USING MODAL SUPERPOSITION / APPLICATION ON AIRCRAFT FUSELAGE
D GENDRE, AIRBUS, France
Reserve Paper 12.1.R COMPOSITE RECYCLING – AN OVERVIEW OF A 21ST CENTURY CHALLENGE IN AEROSPACE INDUSTRY
J. Mašek, Brno University of Technology, Faculty of Mechanical Engineering, Czech Republic
13.1Education and industry processes
Chair:
Track 13
14 - Education and Training
1.2System of Systems
Chair: M. Padulo
Track 1
01 - Aircraft Design and Integrated Systems
  13:00 13:30 1.2.1 DEVELOPMENT AND INTEGRATION OF MULTIFIDELITY MODELS FOR SYSTEM-OF-SYSTEMS TRADE STUDIES
A. Papageorgiou, Linkoping University, Sweden
  13:30 14:00 1.2.2 SYSTEM OF SYSTEMS DRIVEN AIRCRAFT DESIGN FOR WILDFIRE SUPPRESSION
P Shiva Prakasha, DLR - German Aerospace Center, Germany
  14:00 14:30 1.2.3 OPTIMAL AIRLINE FLEET COMPOSED BY A COMBINATION OF JET AND TURBOPROP AIRPLANES
Mattos, B. S. Mattos, Instituto Tecnologico de Aeronautica (ITA), Brazil
Reserve Paper 1.2.R DESIGN SPECIFICATIONS AND PAYLOAD-RANGE EFFICIENCY OF TRANSPORT AIRPLANES
R. Martínez-Val, Univ. Politécnica Madrid, Spain
2.2Unconventional Configuration
Chair: B. Kimmel
Track 2
01 - Aircraft Design and Integrated Systems
  13:00 13:30 2.2.1 A CONCEPTUAL DESIGN OF LSA CLASS AMPHIBIOUS AIRCRAFT
S. Hanada, Sophia University, Japan
  13:30 14:00 2.2.2 AEROELASTIC OPTIMIZATION OF A BLENDED WING BODY AIRCRAFT CONSIDERING STABILITY/CONTROL CONSTRAINTS
X.Z. Wang, Beihang University, China
  14:00 14:30 2.2.3 PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY
Z. L. Chen, Northwestern Polytechnical University, China
Reserve Paper 2.2.R STUDY ON ADJOINT BASED OPTIMIZATION OF BWB CONFIGURATION CONSIDERING THE INTAKE AND EXHAUST EFFECTS
J.-T. Huang, China Aerodynamics Research and Development Center, China
3.2Design architecture & integration methodology 2
Chair: B. Nagel
Track 3
02 - Systems Engineering and Integration
  13:00 13:30 3.2.1 A COLLABORATIVE, DISTRIBUTED AND MULTILEVEL PROCESS TO SUPPORT THE DESIGN OF A NOVEL MID-RANGE AIRCRAFT CONFIGURATION
B. Gerlinger, DLR, Germany
  13:30 14:00 3.2.2 ASTRID-H: A CONCEPTUAL DESIGN METHODOLOGY AND TOOL TO SUPPORT HIGH-SPEED VEHICLE DESIGN
R. Fusaro, Politecnico di Torino, Italy
  14:00 14:30 3.2.3 RESEARCH ON AERO-ENGINE COLLABORATIVE DESIGN PROCESS BASED ON SYSTEM ENGINEERING
C.-Y.G. YINGANG, AECC Commercial Aviation Engine .LITD, China
Reserve Paper 3.2.R THE APPLICATION OF DIGITAL TWIN TECHNOLOGY IN INTELLIGENT OPERATION AND MAINTENANCE OF AERO-ENGINE
W-P Wang, Aero-Engine Academy of China, China
4.2Unsteady Aerodynamics 2
Chair: O. Mello
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. Sartor, ONERA, 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.-Y. Yang, School of Aeronautics, Northwestern Polytechnical University, China
Reserve Paper 4.2.R ATMOSPHERIC TURBULENCE EFFECTS ON SONIC BOOM PROPAGATION
Z-S Qian, AVIC Aerodynamics Research Institute, China
5.2Full Configuration Test 1
Chair: Y. Chen
Track 5
03.2 - Experimental Aerodynamics
  13:00 13:30 5.2.1 EXPERIMENTAL INVESTIGATION OF DAMAGE WING IMPACT ON THE AIRLINER AERODYNAMIC CHARACTERISTICS
Andrzej. A. Krzysiak, ?ukasiewicz Research Network – Institute of Aviation, Poland
  13:30 14:00 5.2.2 WIND-TUNNEL INVESTIGATION OF AERODYNAMIC CHARACTERISTICS FOR COMMERCIAL TRANSPORT AIRCRAFT AT EXTREME FLIGHT CONDITIONS
L. zhang, China Aerodynamics Research and Development Center , China
  14:00 14:30 5.2.3 EXPERIMANTAL INVESTIGATION OF THE CHN-T1 MODEL IN FL-13 WIND TUNNEL OF CARDC AND DNW-LLF FACILITY
F.L.T Fan, CARDC, China
6.2Robust Control
Chair: M. Naruoka
Track 6
06.1 - Flight Dynamics and Control (Control & Modelling)
  13:00 13:30 6.2.1 DECENTRALIZED CONFLICT DETECTION AND RESOLUTION METHOD ACCOUNTING FOR UNCERTAINTIES OF TRAJECTORIES
N. Yokoyama, National Defense Academy, Japan
  13:30 14:00 6.2.2 AN ALTERNATIVE BUT EQUIVALENT REALIZATION OF FINITE-HORIZON SUBOPTIMAL CONTROL FOR VEHICLE LANDING
S. Zhang, China Aerodynamics Research and Development Center, China
  14:00 14:30 6.2.3 A NEW PITCH STABILITY ENHANCEMENT SCHEME FOR AEROSPACE VEHICLE
Guangming: G. M. XIAO, China Aerodynamics Research & Development Center, China
Reserve Paper 6.2.R SENSITIVITY MINIMIZATION ON A PARAMETER INTERVAL FOR ROBUST DIRECT OPTIMAL CONTROL
T. Akman, Technical University of Munich, Germany
7.2Low Speed Aero
Chair:
Track 7
03.4 - Applied Aerodynamics
  13:00 13:30 7.2.1 TRANSPORT AIRCRAFT WING INVESTIGATIONS AIMED ON CROW INSTABILITY EXCITATION AND HIGH LIFT INCREASE BY OSCILLATING FLAPS
J. Ruhland, Chair of Aerodynamics and Fluid Mechanics (TU Munich), Germany
  13:30 14:00 7.2.2 NUMERICAL INVESTIGATIONS OF HINGED STRAKES AERODYNAMICS AT HIGH ANGLES OF ATTACK
Z. F. Xia, China Academy of Aerospace Aerodynamics, China
  14:00 14:30 7.2.3 AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATION
Min ZHONG¹, Jun HUA¹, Xiasheng SUN¹, Sui ZHENG¹, Ganglin WANG¹, Guoxin ZHANG¹, Hao WANG¹, Yan LI¹, Xiaofei LI¹, Junqiang BAI, Northwestern Polytechnical University, China; ¹Chinese Aeronautical Establishment, China
Reserve Paper 7.2.R NUMERICAL STUDY ON WING ROCK MECHANISM OF A LOW-ASPECT-RATIO RECTANGULAR WING AT LOW REYNOLDS NUMBER
Y. Huang, Beihang University, China
8.2Aeroelasticity of Morphing Structures
Chair: M. Ritter
Track 8
04.2 - Structural Analysis and 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 MORPHING FORWARD WING SECTION
F. Sturm, Technical University of Munich, Germany
  13:30 14:00 8.2.2 AEROSERVOELASTIC OPTIMIZATION OF A HIGH ASPECT TRANSPORT WING WITH MORPHING TRAILING EDGE
Z. Zhang, Beihang University, China
  14:00 14:30 8.2.3 A COMPREHENSIVE FRAMEWORK FOR THE COUPLED NONLINEAR AEROELASTIC AND FLIGHT DYNAMIC ANALYSES OF HIGHLY FLEXIBLE AIRCRAFT
Z.-C. Zhang, Northwestern Ploytechnical University, China
9.2Controls & Software
Chair: S. Remy
Track 9
05 - Propulsion
  13:00 13:30 9.2.1 THE USE OF SOFTWARE “VIRTUAL ENGINE” FOR TIMELY GAS-TURBINE ENGINE FAULT LOCALIZATIONS
V. Vladimir, CIAM, Russia
  13:30 14:00 9.2.2 AN IMPROVED IDENTIFICATION METHOD FOR ACTUATOR LOOP OF AIRCRAFT ENGINE CONTROL SYSTEM
Nan Liu, Shanghai Aircraft Design & Research Institute, Commercial Aircra, China
  14:00 14:30 9.2.3 METHODS OF PROGRAMMED THRUST MANAGEMENT FOR NOISE REDUCTION OF SUPERSONIC CIVIL AIRCRAFT
A. Mirzoyan, CIAM, Russia
Reserve Paper 9.2.R RESEARCH ON CIVIL AIRCRAFT POWERPLANT SYSTEM EICAS MESSAGES DESIGN METHOD
S.-Y. Yang, COMAC, China
10.2Computational Aeroelasticity 2
Chair: M. Ritter
Track 10
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  13:00 13:30 10.2.1 EFFECTS OF ELASTICITY, VISCOSITY AND BOUNDARY LAYER TRANSITION ON AEROELASTICITY CHARACTERISTICS OF LAMINAR WINGS
S.I. Kuzmina, TsAGI, Russia
  13:30 14:00 10.2.2 STUDY ON THE MULTIPLE EQUILIBRIUM POINTS OF TRANSONIC FLUTTER IN VISCOUS FLOW
G. Wang, Northwestern Polytechnical University, China
  14:00 14:30 10.2.3 AEROELASTIC STRUCTURAL DESIGN OF A MID-RANGE COMPOSITE WING AIRCRAFT USING CPACS-MONA
K. Sinha, German Aerospace Center, Germany
11.2Avionics
Chair: N. Viola
Track 11
07 - Systems, Subsystems and Equipment
  13:00 13:30 11.2.1 CASCADE CONTROL OF AVIATION VARIABLE FREQUENCY AC GENERATION SYSTEM BASED ON SLIDING MODE ACTIVE DISTURBANCE REJECTION
R.-Z.-X. RUAN, Nanjing University Of Aeronautics And Astronautics, China
  13:30 14:00 11.2.2 DYNAMIC PERFORMANCE ANALYSIS AND ADAPTIVE FAULT DIAGNOSIS OF AIRCRAFT POWER SYSTEM
H Li, Chengdu Aircraft Industrial (Group) Corporation, China
  14:00 14:30 11.2.3 DESIGN AND APPLICATION OF 18-PULSE AUTO-COUPLING TRANSFORMER RECTIFIER FOR AVIATION
WX.-C. CHEN¹, TY.-S. SUN¹, LX.-J. JIANG¹; ¹AVIC, China
Reserve Paper 11.2.R AN AGILE PRACTICE OF AVIONICS SYSTEM DEVELOPMENT
Lei: L Dong, China Aeronautical Radio Electronics Research Institute, China
12.2Condition Based Maintenance 2
Chair:
Track 12
11 - Operations and Sustainment
  13:00 13:30 12.2.1 CONDITION BASED MAINTENANCE (CBM) IN THE DIGITAL TRANSFORMATION STREAM
PC ROLLAND, AIRBUS SAS, France
  13:30 14:00 12.2.2 ANALYSIS OF THE ECONOMIC PERFORMANCE FOR AIRCRAFT MAINTENANCE USING DATA DRIVEN APPROACH
X Zhao, China
  14:00 14:30 12.2.3 TOTAL LIFE CYCLE COST AND EMISSION OF ELECTRIC, HYBRID – ELECTRIC AIRCRAFT
N. D. Dung, Budapest University of Tech. and econ.;, Hungary
Reserve Paper 12.2.R A METHOD FOR EVALUATING THE APPLICABILITY OF MAINTENANCE TASKS BASED ON HELICOPTER HEALTH AND USAGE MONITORING SYSTEM
DN-D Dong, AVIC China Aero-Polytechnology Establishment, China
13.2Flight Control During Approach
Chair:
Track 13
10 - Safety and Security
  13:00 13:30 13.2.1 DETECTION AND ANALYSIS OF AIRCRAFT’S LOW ENERGY STATE DURING THE FINAL APPROACH PHASE
Xiaolong Wang¹, Florian Holzapfel¹; ¹Technische Universität München, Germany
  13:30 14:00 13.2.2 TOWARDS AN ONLINE PREDICTIVE MODEL OF AIRCRAFT ENERGY STATE USING SUPERVISED MACHINE LEARNING
O Pinon Fischer, Georgia Institute of Technology, United States
  14:00 14:30 13.2.3 AN OVERVIEW OF FLARE TECHNIQUES AND FLARE TRAINING METHODS
J.O. Entzinger, The University of Tokyo, Japan
Reserve Paper 13.2.R MACHINE LEARNING BASED PREDICTION OF VEER-OFFS DURING LANDING PHASE
S. Lagunas-Caballero, Airbus Defence and Space, Spain
1.3HMI & Cabin Design
Chair: B. Nagel
Track 1
01 - Aircraft Design and Integrated Systems
  15:00 15:30 1.3.1 ATTENUATION OF NOISE IN THE CABIN OF A REGIONAL AIRCRAFT BY METAMATERIAL TRIM PANELS
M. Cinefra, Politecnico di Torino, Italy
  15:30 16:00 1.3.2 ACOUSTIC FLIGHT LAB – A UNIQUE INTEGRATION PLATFORM FOR OPTIMIZING OF VIBRO-ACOUSTIC PERFORMANCE OF AIRCRAFT
M. Wandel, Airbus Operations GmbH, Germany
  16:00 16:30 1.3.3 DEVELOPMENT OF A GESTURE-BASED INTERFACE FOR FLIGHT CONTROLS: RESULTS OF INITIAL EXPERIMENTS WITH THE SYSTEM
M.A. Rodriguez Diaz, Instituto Tecnologico de Aeronáutica, Brazil
2.310 years of IFAR
Chair:
Track 2
15 - Guest lectures
  15:00 15:30 2.3.1 IFAR (INTERNATIONAL FORUM FOR AVIATION RESEARCH) INFRASTRUCTURE DATABASE
rd Degenhardt, DLR, Germany
  15:30 16:00 2.3.2 SOL-GEL BASED ORGANIC-INORGANIC HYBRID COATINGS FOR CORROSION PROTECTION OF AEROSPACE ALUMINIUM ALLOY
R.V. Lakshmi, India
3.3Knowledge based Engineering
Chair: S. Conway
Track 3
02 - Systems Engineering and Integration
  15:00 15:30 3.3.1 FORMALIZED KNOWLEDGE MANAGEMENT FOR THE AIRCRAFT CABIN DESIGN PROCESS
M. Fuchs¹, C. Hesse¹; ¹DLR, Germany
  15:30 16:00 3.3.2 A MODULAR KNOWLEDGE-BASED-ENGINEERING APPLICATION SUPPORTING THE PREDESIGN OF NOVEL AIRCRAFT CONFIGURATIONS
A. Zamfir, German Aerospace Center (DLR), Germany
  16:00 16:30 3.3.3 IMPROVING CONCEPTUAL DESIGN SPACE EXPLORATION CAPABILITIES USING AN ADVANCED KNOWLEDGE-BASED-ENGINEERING TOOL
J. Zamboni, German Aerospace Center (DLR), Germany
Reserve Paper 3.3.R APPLICATION OF KNOWLEDGE ENGINEERING IN SPACECRAFT OVERALL DESIGN
Zhao Zhao, Harbin Institute Technology, China
4.3High Speed Flows
Chair: L. Alves
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  15:00 15:30 4.3.1 LONGITUDINAL VORTEX FORMATION IN HYPERSONIC BOUNDARY LAYER ON BLUNTED DELTA WING AND ITS EFFECT ON FLOW CHARACTERISTICS
V.I. Shalaev, Moscow Institute of Physics and Technology, Russia
  15:30 16:00 4.3.2 LONGITUDINAL AND LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE HIGH-SPEED VEHICLE
G. Pezzella, University of Campania, Italy
  16:00 16:30 4.3.3 MULTI-SCALE CFD/MD MODELLING OF HIGH-ENTHALPY FLOW/TPS INTERACTION AND ITS PRELIMINARY AERONAUTICAL APPLICATION
X. Yang, China Aerodynamics Research and Development Center, China
Reserve Paper 4.3.R RESEARCH OF HYPERSONIC BOUNDARY LAYER INSTABILITY AND TRANSITION WITH THERMAL-CHEMICAL NON-EQUILIBRIUM EFFECTS
X.-L. Chen, Tsinghua University, China
5.3Full Configuration Test 2
Chair: A. Ivanov
Track 5
03.2 - Experimental Aerodynamics
  15:00 15:30 5.3.1 EXPERIMENTAL AND NUMERICAL AERODYNAMIC LOAD RESULTS ACTIONG ON THE M5/ONERA/IAE AERONAUTICAL STANDARD MODEL
M. S. Souza, IAE, Brazil
  15:30 16:00 5.3.2 OPTIMIZATION OF AN ACTIVE DAMPING SYSTEM FOR USE WITH A SINGLE STRUT MOUNT
J.L. Pereira, National Research Council Canada, Canada
  16:00 16:30 5.3.3 STUDY ON AERODYNAMIC CHARACTERISTICS OF LIGHT CONVERTIBLE AIRCRAFT MODEL
E.A. Pigusov, Central Aerohydrodinamic Institute, Russia
6.3Composite Defect and Damage
Chair: M. Herman
Track 6
04.1 - Material Issues, Fatigue and Damage Tolerance
  15:00 15:30 6.3.1 ADJUSTED SHAPES OF ADHESIVELY BONDED REPAIR PATCHES FOR THE EARLY INDICATION OF DEBOND IN FIGHTER AIRCRAFT STRUCTURES
J Jokinen, Tampere University, Finland
  15:30 16:00 6.3.2 THE INFLUENCE OF THE NUMBER OF ADHESIVE PLIES (FM-300-2K) ON FRACTURE PROPERTIES
J Jokinen, Tampere University, Finland
  16:00 16:30 6.3.3 STATISTICS AND ANALYSIS OF MANUFACTURE DEFECTS AND DAMAGE OF HELICOPTER COMPOSITE STRUCTURES
Jun Li, China
Reserve Paper 6.3.R DEVELOPMENT OF METHOD FOR DETERMINING THE SHEAR FRACTURE TOUGHNESS ON SPECIMENS WITHOUT A DELAMINATION INITIATOR MADE OF
V. Tokar, TsAGI, Russia
7.3Simulation
Chair:
Track 7
03.4 - Applied Aerodynamics
  15:00 15:30 7.3.1 NUMERICAL VIRTUAL FLIGHT SIMULATION OF QUASI-COBRA MANEUVER OF A FIGHTER AIRCRAFT
None Wang, China Aerodynamics Research and Development Center, China
  15:30 16:00 7.3.2 NUMERICAL SIMULATION OF AIRFOIL SPANWISE-RIDGE ICE FORMATION BASED ON HOT AIR ANTI-ICING SYSTEM
J.-T Wang, Northwestern Polytechnical University, China
  16:00 16:30 7.3.3 VERIFICATION AND VALIDATION OF SONIC BOOM SIMULATION CAPABILITIES
G. CARRIER, ONERA, France
8.3Aeroservoelasticity
Chair: R. Degenhardt
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  15:00 15:30 8.3.1 MULTI-AXIS MANEUVER SIMULATION FOR SYSTEM IDENTIFICATION OF FLEXIBLE TRANSPORT AIRCRAFT BY HIGH-FIDELITY METHODS
M Ritter, German Aerospace Center (DLR), Germany
  15:30 16:00 8.3.2 STRUCTURAL DESIGN OF MILITARY AIRCRAFT VERTICAL TAIL INCLUDING DYNAMIC LOADS FROM WING AND AIRBRAKE SEPARATED FLOW
W.G. LUBER, wgl-dynamics Consulting, Germany
  16:00 16:30 8.3.3 RECEPTANCE-BASED UNCERTAINTY QUANTIFICATION AND MINIMIZATION IN AEROSERVOELASTIC SYSTEMS
L. J. Adamson, University of Liverpool, United Kingdom
9.3ISABE 1
Chair:
Track 9
15 - Guest lectures
  15:00 15:30 9.3.1 THE POTENTIAL OF CASING TREATMENTS FOR TRANSONIC COMPRESSORS: EVALUATION BASED ON AXIAL-SLOT AND ROTOR BLADE OPTIMISATIO
G. Goinis¹, C. Voß¹, E. Nicke¹; ¹German Aerospace Center (DLR), Germany
  15:30 16:00 9.3.2 CONJUGATE HEAT TRANSFER MODELLING OF A TURBINE VANE ENDWALL WITH THERMAL BARRIER COATINGS
Z. Fen, China
10.3Vibration and Damping
Chair: E. Zappino
Track 10
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  15:00 15:30 10.3.1 STRUCTURAL VIBRATION CONTROL BY USING THE ENERGY FROM DIFFERENT MODE
K.L LI, Aircraft strength research institute, China
  15:30 16:00 10.3.2 PREDICTING THE DYNAMIC BEHAVIOUR OF AERONAUTICAL STRUCTURES IN PRESENCE OF RUBBER-LIKE STRUCTURAL CONNECTIONS
i Isnardi, University of Liverpool, United Kingdom
  16:00 16:30 10.3.3 MODAL DAMPING IDENTIFICATION METHOD BASED ON VARIATIONAL MODE DECOMPOSITION AND ENVELOPE FITTING AND ITS APPLICATIONS
J. BIAN, AECC Hunan Aviation Powerplant Research Institute, China
Reserve Paper 10.3.R A PERTURBATION ANALYSIS OF NONLINEARITY IN LANDING-GEAR SHIMMY OF A FLEET AIRCRAFT
M.-L Kou, AECC CAE, China
11.3Military Technology
Chair: Y. Fu
Track 11
07 - Systems, Subsystems and Equipment
  15:00 15:30 11.3.1 RESEARCH ON OPTIMIZATION TECHNOLOGY FOR CONTROL PARAMETERS OF EJECTION SEAT BASED ON PSO ALGORITHM
J-L Lou, Aerospace Life-support Industries,LTD., China
  15:30 16:00 11.3.2 MANOEUVRABLE AERIAL TARGET TRACKING IN THE PRESENCE OF STAND-OFF JAMMING
C. Tian, School of Aeronautics, Northwestern Polytechnical University, China
  16:00 16:30 11.3.3 RESEARCH ON THE PRESSURE COMFORT OF PILOT’S HELMET
X. Wang, AVIC Aerospace Life Support Industries LTD, China
12.3Flight Operations
Chair: J. Vincent
Track 12
11 - Operations and Sustainment
  15:00 15:30 12.3.1 MODELING THE CLIMATE IMPACT OF FORMATION FLIGHT
T. Marks, German Aerospace Center (DLR), Germany
  15:30 16:00 12.3.2 A MULTI-CRITERIA SEQUENCING LOGIC FOR THE EXTENDED TERMINAL MANOEUVRING AREA CONSIDERING INTERDEPENDENT UNCERTAINTIES
T. Zeh, Technische Universität Dresden, Germany
  16:00 16:30 12.3.3 ADVANCED PASSENGER MOVEMENT MODEL DEPENDING ON THE AIRCRAFT CABIN GEOMETRY
M. Engelmann¹, T. Kleinheinz¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
Reserve Paper 12.3.R ON THE AIRCRAFT OPERATIONAL INTEGRITY
Yuting He He, Air Force Engineering University, China
13.3Flight Control and Critical Situations
Chair:
Track 13
10 - Safety and Security
  15:00 15:30 13.3.1 ACTIVITY CHARACTERISTICS AND THE MECHANISM OF MESO-MICRO SCALE DISTURBANCES IN THE EAST ASIAN SUBTROPICAL UPPER-LEVEL JE
X. Chen, China Aerodynamics Research and Development Center, China
  15:30 16:00 13.3.2 A METHODOLOGY FOR CHARACTERISING LOSS OF CONTROL IN FLIGHT ACCIDENTS
J.P. Macedo, Univeristy of Sao Paulo, Brazil
  16:00 16:30 13.3.3 MAIN OUTCOMES FROM H2020 VISION PROJECT: EU-JAPAN COLLABORATIVE RESEARCH IN INTELLIGENT FLIGHT CONTROL STSTEMS
Y. Watanabe, ONERA, France
Reserve Paper 13.3.R ANALYSIS OF RISK FACTORS AND IDENTIFICATION OF PRECURSORS OF RUNWAY EXCURSIONS AT LANDING
Nail: N. Khairullin, Central Aerohydrodynamic Institute (TsAGI), Russia
1.4Wing Design
Chair: K. Rinoie
Track 1
01 - Aircraft Design and Integrated Systems
  10:00 10:30 1.4.1 A HIERARCHICAL STRUCTURAL MODEL FOR CONCEPTUAL DESIGN OF TRANSPORT AIRCRAFT WING
Y.K. Yin, Shanghai Jiao Tong University, China
  10:30 11:00 1.4.2 VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WING
W.Y.CHENG CHENG, Aviation Industry Development Research Center of China (ADR), China
  11:00 11:30 1.4.3 EVALUATION AND VALIDATION OF AEROELASTIC ANALYSIS PROGRAM FOR AEROSTRUCT WING OPTIMIZATION PLATFORM
S.B. Ling, Northwestern Polytechnical University, China
  11:30 12:00 1.4.4 ON WINGS WITH NON-ELLIPTIC LIFT DISTRIBUTIONS
E. Bragado Aldana¹, M. M. Lone¹; ¹Cranfield University, United Kingdom
Reserve Paper 1.4.R ON THE FLIGHT MECHANICS OF A TRANSPORT AIRCRAFT FITTED WITH FLARED-HINGE FOLDING WINGTIPS
R Ajaj, Khalifa University, United Arab Emirates
2.4Cost Assessment
Chair: S. Bagassi
Track 2
01 - Aircraft Design and Integrated Systems
  10:00 10:30 2.4.1 FLEET LEVEL DIRECT OPERATING COST ASSESSMENT OF ADVANCED ALL NEW MID-RANGE TRANSPORT AIRCRAFT
J. Hartmann, DLR, Germany
  10:30 11:00 2.4.2 STATISTICAL APPROACH TO INDIRECT COST ASSESSMENT FOR AN AIRCRAFT FLEET
G.-F. Ferrari, Politecnico di Torino, Italy
  11:00 11:30 2.4.3 DEVELOPMENT OF A PARAMETRIC COST MODEL ASSESSING THE IMPACT OF NEW TECHNOLOGIES ON A REGIONAL AIRCRAFT
M. Fioriti, Politecnico di Torino, Italy
  11:30 12:00 2.4.4 LIFECYCLE COST-BENEFIT ASSESSMENT OF SELECTED TECHNOLOGIES CONSIDERING UNCERTAINTIES
A.A. Pohya, DLR, Germany
Reserve Paper 2.4.R BASED ON THE CHARACTERISTIC PARAMETERS ESTIMATE MANUFACTURING COST FOR COMPOSITE STRUCTURES
H.-F. Feng, China
3.4Global Collaborative Digital Integration in Aviation / IFAR-X challenge
Chair:
Track 3
02 - Systems Engineering and Integration
4.4Aerodynamic Optimization
Chair: T. Wan
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  10:00 10:30 4.4.1 FLOW CONTROL AT HIGH LIFT MISSION OF A CIVIL AIRCRAFTBY AN OPTIMUM MORPHING LEADING-EDGE DESIGN
alireza jahangirian, aerospace engineering departmen, Iran
  10:30 11:00 4.4.2 OPTIMISATION OF VORTEX GENERATORS FOR STALL SPEED REDUCTION
C Bil, RMIT University, Australia
  11:00 11:30 4.4.3 AERODYNAMIC DESIGN OOPTIMIZATION OF A CIVIL AIRCRAFT WINGLET USING MULTI-OBJECTIVE EVOLUTIONARY ALGORITHM AND CFD SOLVER
alireza jahangirian, aerospace engineering departmen, Iran
  11:30 12:00 4.4.4 DESIGN AND OPTIMIZATION OF A HIGH-ALTITUDE LONG ENDURANCE UAV PROPELLER
K. Y. You, Northwestern Polytechnical University, China
Reserve Paper 4.4.R OPTIMAL DESIGN OF A NEXT GENERATION HIGH-LIFT REUSABLE RE-ENTRY VEHICLE
G. Pezzella, University of Campania, Italy
5.4Measurement Techniques & Data Analysis
Chair: W. Jujun
Track 5
03.2 - Experimental Aerodynamics
  10:00 10:30 5.4.1 AN OBJECTIVE APPROACH FOR MEASURING INTERMITTENCY IN THE TRANSITIONAL BOUNDARY LAYERS
D Veerasamy, City, University of London, United Kingdom
  10:30 11:00 5.4.2 DYNAMIC TRAILING-EDGE FLAP MOVEMENT AS A NON-CONVENTIONAL LIFTING MECHANISM
M. Bremm, RWTH Aachen University, Germany
  11:00 11:30 5.4.3 COMPUTATIONAL FLUID DYNAMIC STUDY ON LOW SPEED WIND TUNNEL DATA CORRECTIONS
W. S. Stryczniewicz, Lukasiewicz Research Network - Institute of Aviation, Poland
  11:30 12:00 5.4.4 SKIN-FRICTION TOPOLOGY ON AXISYMMETRIC BOATTAIL MODELS BY AN OPTICAL-FLOW ALGORITHM WITH SUBGRID FUNCTION
T. H. Tran, Le Quy Don Technical University, Vietnam
Reserve Paper 5.4.R APPLIED RESEARCH ON SUPERVISED LEARNING IN THE JUDGMENT OF AIRFOIL TRANSITION
W.-B.B. Wei, China
6.4Developments in Modelling
Chair: C. Atkin
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  10:00 10:30 6.4.1 EXPERIMENTAL INVESTIGATION, NUMERICAL AND MATHEMATICAL SIMULATION OF DISPERSE FLOWS IMPINGING ON AIRCRAFT SURFACE
Ivan Alexeevich: Amelyushkin, TsAGI, Russia
  10:30 11:00 6.4.2 MODIFICATION OF TURBULENCE MODELS FOR PRESSURE-INDUCED SEPARATION ON SMOOTH SURFACES USING THE DLR VICTORIA EXPERIMENT
A. M. Krumbein, DLR - German Aerospace Center, Germany
  11:00 11:30 6.4.3 A NETWORK-CENTROID BASED REDUCED-ORDER MODEL FOR A MIXING LAYER
H. Li, National University of Defense Technology, China
  11:30 12:00 6.4.4 SINGULARITIES IN THE NEAR-WALL REGION OF 3D BOUNDARY LAYER AND ASYMPTOTIC FLOW STRUCTURE IN ITS VICINITY
V.I. Shalaev, Moscow Institute of Physics and Technology, Russia
Reserve Paper 6.4.R LOW ORDER MODELLING OF UNSTEADY AERODYNAMIC LIFT FORCES ON 2D FLAT-PLATE DURING SINUSOIDAL PITCHING
R. Zeng, Beihang University, China
7.4Propulsion Airframe Integration 1
Chair:
Track 7
03.4 - Applied Aerodynamics
  10:00 10:30 7.4.1 PROPELLER WAKE - OBJECT INTERACTION USING A FREE WAKE MODEL UTILIZING LOCAL MESH REFINEMENT
M. Thiele, Technical University of Munich - Institute of Aircraft Design, Germany
  10:30 11:00 7.4.2 AERODYNAMIC INVESTIGATION OF ROTOR-ROTOR INTERACTION FOR DISTRIBUTED-PROPELLER SYSTEMS
R. de Vries, Delft University of Technology, Netherlands
  11:00 11:30 7.4.3 NUMERICAL STUDY OF QUAD-ROTOR AIRCRAFT PERFORMANCE UNDER SEVERE WEATHER
T. Wan, Tamkang University, Taiwan, China
  11:30 12:00 7.4.4 MULTI-DISCIPLINARY FRAMEWORK FOR PROPELLER BLADE DESIGN
A. Kümmel, Germany
8.4Composite Materials and Structures
Chair: S. Fichera
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  10:00 10:30 8.4.1 LIGHTWEIGHT DESIGN OF THERMAL PROTECTION STRUCTURES WITH EFFECTS OF MESO-PROPERTIES OF MATERIALS
S.-H.-A. You An, Computational Aerodynamic Institute(CAI), CARDC, China
  10:30 11:00 8.4.2 ACCURATE MODELS FOR THE PREDICTION OF FREE-EDGE STRESSES OF COMPOSITE STRUCTURES UNDER THERMAL LOADS
E. Zappino, Italy
  11:00 11:30 8.4.3 TEMPERATURE-INDUCED LOAD OF BOLTED HYBRID COMPOSITE/METAL JOINT
L.-K KAI, AVIC Aircraft Strength Research Institute, China
  11:30 12:00 8.4.4 DEVELOPMENT OF LIGHTWEIGHT HYBRID AIRFRAMES BASED ON UNIDIRECTIONAL COMPOSITE STRUCTURE CONCEPTS
A. Shanygin, Central Aerohydrodynamic Institute (TsAGI), Russia
Reserve Paper 8.4.R STRUCTURAL INDICES-BASED OPTIMIZATION METHODOLOGY FOR LIGHT AIRCRAFT COMPOSITE WINGS
M Nuño, RWTH Aachen University, Germany
9.4Multi Disciplinary Optimisation (MDO)
Chair: A. Mirzoyan
Track 9
05 - Propulsion
  10:00 10:30 9.4.1 KNOWLEDGE-BASED CONCEPTUAL DESIGN METHODS FOR GEOMETRY AND WEIGHT ESTIMATION OF RUBBER AERO ENGINES
J. Häßy, German Aerospace Center (DLR), Germany
  10:30 11:00 9.4.2 RESEARCH OF PROPULSION-SYSTEM-SURROGATE-MODELING METHOD USING INFILL CRITERION SAMPLES
DC.W Wang, School of Aeronautics, Northwestern Polytechnical University, China
  11:00 11:30 9.4.3 ELABORATION OF DISTRIBUTED MDAO SYSTEM FOR CONCEPTUAL DESIGN OF SCA PROPULSION SYSTEM IN INTEGRATED DEVELOPMENT ENVIRONM
L.A. Mirzoyan, CIAM, Russia
  11:30 12:00 9.4.4 AERODYNAMIC PROPULSION SYSTEM OPTIMIZATION: TOWARDS TO AGILE 4.0
K.S. Anisimov, Federal State Unitary Enterprise Central Aerohydrodynamic Instit, Russia
10.4Virtual Testing
Chair: E. Stumpf
Track 10
07 - Systems, Subsystems and Equipment
  10:00 10:30 10.4.1 VIRTUAL TESTING IN LANDING GEAR SHOCK ABSORBER DESIGN USING AN EQUIVALENT CFD-MODEL
R. Springmann, Hamburg University of Technology, Germany
  10:30 11:00 10.4.2 VIRTUAL TESTING OF A MULTIFUNCTIONAL POWER CONTROL UNIT FOR HYDRAULIC SUPPLY AND HIGH LIFT ACTUATION
L. Nordmann, Germany
  11:00 11:30 10.4.3 RESEARCH AND VALIDATION OF SYSTEM MODELING AND SIMULATION OF INTAKE AIR MIXER ALTITUDE TEST BED
Feng-Wu: F. -W. Wu, AECC Sichuan Gas Turbine Establishment, China
  11:30 12:00 10.4.4 DESIGN AND DEVELOPMENT OF A MODULAR IRON BIRD TO TEST MOVABLE SURFACE ACTUATORS OF GENERAL AVIATION AIRCRAFT AND UAVS
M. Mattei, Università della Campania "Luigi Vanvitelli", Italy
11.4UAV Dynamics and Control 1
Chair: W. Rui
Track 11
06.2 - Flight Dynamics and Control (UAV related)
  10:00 10:30 11.4.1 RESEARCH ON DYNAMIC MODELING AND TRANSITION FLIGHT STRATEGY OF INDUCED-LIFT VTOL UAV
C.W Wang, Northwestern Polytechniacl University, China
  10:30 11:00 11.4.2 COMPARATIVE ANALYSIS OF METHODS USED TO ACTIVE CONTROL OF MICRO AERIAL VEHICLE
K.-S. Sibilski, Warsaw University of Technology, Poland
  11:00 11:30 11.4.3 PERCHING PRINCIPLES ANALYSIS OF POST-STALL PERCHING UNMANNED AERIAL VEHICLE
S.-Y Yang, NWPU, China
  11:30 12:00 11.4.4 DEVELOPMENT TOWARDS A TOOLCHAIN FOR ESTIMATING UAV FLIGHT DYNAMIC MODELS IN EARLY DESIGN
S. Koeberle, Institute of Aircraft Design/Technical University of Munich, Germany
Reserve Paper 11.4.R STUDY OF SMALL UAVS DISTURBED MOTION NATURAL FREQUENCIES USING EXTENDED EXPERIMENTAL DATASETS
M. E. El-Salamony, Peking University, China
12.4Composite Characterization and Fabrication
Chair: L. Pinto
Track 12
04.1 - Material Issues, Fatigue and Damage Tolerance
  10:00 10:30 12.4.1 A DEEP-LEARNING-BASED METHOD FOR DAMAGE IDENTIFICATION OF COMPOSITE LAMINATES
Y Yu¹, W Binwen¹, L Shuaishuai¹, Z Yuxi, Peking University, China; W Li¹, L Guoqiang¹; ¹Aircraft Strength Research Institute of ChinaAffiliation, China
  10:30 11:00 12.4.2 IN-SITU LASER ASSISTED DIRECT IMPREGNATION, LAMINATION AND PLACEMENT OF CFRTP
T. Ikeda, Chubu University, Japan
  11:00 11:30 12.4.3 MOISTURE ABSORPTION BEHAVIOR OF COMPOSITE STIFFENED PANELS IN HYGROTHERMAL ENVIRONMENT
B-L Ma, China
  11:30 12:00 12.4.4 A TWO PHASES COUPLING FREE AND POROUS FLOW NUMERICAL SIMULATION METHOD OF LCM PROCESS
C. Li, BASTRI of COMAC, China
Reserve Paper 12.4.R DESIGN FOR MANUFACTURING APPROACH AND LOW COST METAL STRUCTURE
LP PINTO, AIRBUS, France
13.4ATC, Pilot & Controller
Chair:
Track 13
10 - Safety and Security
  10:00 10:30 13.4.1 ATTENTION: TARGET AND ACTUAL – THE CONTROLLER FOCUS
J. Rataj, DLR, Germany
  10:30 11:00 13.4.2 ANALYSIS OF PILOT OPERATIONAL STRATEGY DIFFERENCE USING NEURAL NETWORK
R. Mori, Electronic Navigation Research Institute, Japan
  11:00 11:30 13.4.3 WORKLOAD EVALUATION USING OBJECTIVE AND SUBJECTIVE DATA MEASURED DURING SIMULATED FLIGHT
C. Orlando, Kore University of Enna, Italy
  11:30 12:00 13.4.4 ENSURING HIGH NAVIGATION INTEGRITY FOR URBAN AIR MOBILITY USING TIGHTLY COUPLED GNSS/INS SYSTEM
S.-Z Wang, Shanghai Jiao Tong University, China
Reserve Paper 13.4.R OBJECTIVE MEASUREMENT OF HUMAN FACTORS FOR SUPPORTING THE OPERATOR’S LOAD SIMULATION AND MANAGEMENT
U. Kale, Budapest University of Tech. and econ.;, Hungary
1.5Hybrid/Electric & Unconventional Aircraft 1
Chair: P. Prakasha
Track 1
01 - Aircraft Design and Integrated Systems
  14:00 14:30 1.5.1 CONCURRENT OPTIMIZATION OF AIRFRAME AND ENERGY STORAGE AND CONVERSION SYSTEMS FOR HYBRID ELECTRIC PROPULSION AIRCRAFT
A. Elham, TU Braunschweig, Germany
  14:30 15:00 1.5.2 PRELIMINARY DESIGN AND EXPERIMENTAL INVESTIGATION OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT
Y.-M. Ma, Northwestern Polytechnical University, China
  15:00 15:30 1.5.3 UNMANNED FIRE-FIGHTING AMPHIBIOUS AIRCRAFT WITH DISTRIBUTED TURBOELECTRIC PROPULSION SYSTEM
A.N. Varyukhin, CENTRAL INSTITUTE OF AVIATION MOTORS (CIAM), Russia
Reserve Paper 1.5.R MULTIFIDELITY OPTIMISATION OF A BLENDED WING BODY MARTIAN GLIDER
D. Verstraete, The University of Sydney, Australia
2.5Shape Optimization
Chair: K. Rinoie
Track 2
01 - Aircraft Design and Integrated Systems
  14:00 14:30 2.5.1 MULTI-FIDELITY AND MULTI-POINT SIMULTANEOUS SHAPE AND SIZING OPTIMISATION FOR MAXIMUM AIRCRAFT PERFORMANCE
A. Gastaldi, Airbus Defence and Space, Germany
  14:30 15:00 2.5.2 BWB CONFIGURATION’S AERODYNAMIC OPTIMIZATION DESIGN AND SHAPE PARAMETERIZATION BASED ON GRADIENT METHOD
W.zy Wang, The First Aircraft Institute, China
  15:00 15:30 2.5.3 MULTIFIDELITY AERODYNAMIC/STEALTH SHAPE DESIGN OPTIMIZATION METHOD FOR FLYING WING AIRCRAFT
Z.-Q. Liu, School of Aeronautics, Northwestern Polytechnical University, China
Reserve Paper 2.5.R A GRADIENT-BASED AERO-STEALTH OPTIMIZATION DESIGN METHOD FOR THE LONG-ENDURANCE UAV SHAPE DESIGN
L.-M. Ming, Northwestern Polytechnical University, China
3.5System Architecture
Chair: J.C. Limouzy
Track 3
02 - Systems Engineering and Integration
  14:00 14:30 3.5.1 ARCHITECTURE INTEGRATION OF FUTURE ATM SYSTEM BASED ON META MODEL
JY Wang, China Aeronautical Radio Electronics Research Institute, China
  14:30 15:00 3.5.2 TECHNOLOGY ROADMAPS FOR THE DEVELOPMENT OF FUTURE HIGH-SPEED TRANSPORTATION SYSTEMS
N. Viola, Politecnico di Torino, Italy
  15:00 15:30 3.5.3 ARCHITECTURE OF PRODUCT RESEARCH AND DEVELOPMENT SYSTEM
L. Su, Aero-Engine Academy of China, China
Reserve Paper 3.5.R GREENER ATM SYSTEM ARCHITECTURE RESEARCH BASED ON COMPLEX SYSTEM ENGINEERING METHOD
H. Hu, China Aeronautical Radio Electronics Research Institute, China
4.5Ice Accretion
Chair: Z. Gao
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  14:00 14:30 4.5.1 DEVELOPMENT OF ANTI-ICING SIMULATION CODE USING THE CONJUGATE HEAT TRANSFER BASED ON ICEPAC
YH KIM, SNU, South Korea
  14:30 15:00 4.5.2 NUMERICAL STUDY ON THE STALL CHARACTERISTICS AND SEPARATED FLOW AROUND ICED AIRFOILS USING LATTICE BOLTZMANN METHOD
H.Y.G Gu, Northwestern Polytechnical University, China
  15:00 15:30 4.5.3 EFFECT OF DROPLET SIZE ON ICING RANGE FOR HELICOPTER BLADE
Li Weibin, China
Reserve Paper 4.5.R THREE-EQUATION TTURBULENCE MODEL FOR SEPARATION PREDICTION OF ICE-ACCRETION AIRFOIL
H.-L Li, Tsinghua University, China
5.5Aeroacoustics & Noise
Chair: C. Bao
Track 5
03.2 - Experimental Aerodynamics
  14:00 14:30 5.5.1 WAVE AND SOUND ATTENUATION EFFECT OF BIO-INSPIRED SMALL TUBERCLES
Y Inada, Tokai University, Japan
  14:30 15:00 5.5.2 FEASIBILITY OF DETERMINING AIRCRAFT CERTIFICATION NOISE LEVELS USING GROUND PLANE MICROPHONE MEASUREMENTS
V.-P. Blandeau, Airbus, France
  15:00 15:30 5.5.3 INVESTIGATION OF A NOISE REDUCTION PROPELLER GEOMETRY BASED ON AERODYNAMIC AND AEROACOUSTIC OPTIMIZATION
X GENG, BEIHANG UNIVERSITY, China
Reserve Paper 5.5.R MICROPHONE ARRAY TECHNIQUES FOR TRAILING EDGE NOISE BASED ON CONVOLUTIONAL NEUTRAL NETWORK
ZC Song, BeiHang Univerisity, China
6.5Turbulent Flows
Chair: C. Breitsamter
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  14:00 14:30 6.5.1 NUMERICAL SIMULATION OF BOUNDARY LAYER FLOW ON MICROSTRUCTURE SURFACE
R.P. Pang, Northwestern Polytechnical University , China
  14:30 15:00 6.5.2 SUBSONIC WIND TUNNEL SMALL RIBLETS DRAG REDUCTION TEST ON C919 FUSELAGE MODEL
H.W. Wang, China Academy of Aerospace Aerodynamics, China
  15:00 15:30 6.5.3 THE EFFECTS OF ADVERSE PRESSURE GRADIENT ON THE BEHAVIORS OF RESOLVENT MODE IN TURBULENT CHANNEL FLOWS
Cheng Chen, CARDC, China
Reserve Paper 6.5.R DIRECT SIMULATION OF THE HYPERSONIC SHOCK WAVE/BOUNDARY LAYER INTERACTION AND ITS HEATING LOAD CONTROL BY MICRO-RAMP VOR
D. Sun, State Key Laboratory of Aerodynamics, China
7.5Propulsion Airframe Integration 2
Chair:
Track 7
03.4 - Applied Aerodynamics
  14:00 14:30 7.5.1 AERODYNAMIC ANALYSIS OF AN AIR DRIVE EJECTOR FOR USE IN ENGINE TEST FACILITIES
F. R. Rasi, NRC, Canada
  14:30 15:00 7.5.2 LOW PARAMETRIZED MODELLING METHODOLOGY TO OPTIMIZE THE WING SURFACE OF AN AIRCRAFT WITH OVER_WING MOUNTED ENGINES
PW WEGENER, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany
  15:00 15:30 7.5.3 AERODYNAMIC INTERFERENCE OPTIMIZATION OF THE FUSELAGE-PUSHING PROPELLER CONFIGURATION
V. Gubskiy, TsAGI, Russia
8.5Fluid Structure Interaction
Chair: H. Schmidt
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  14:00 14:30 8.5.1 OPTIMAL DESIGN OF FLUID-CONVEYING PIPE SUPPORT FOR CONTROLLING REACTION FORCE DURING VIBRATION
R.T. tian, Aviation Industry Aircraft Strength Research Institute, China
  14:30 15:00 8.5.2 OPERATIONAL MODAL ANALYSIS AND ESTIMATION OF AERODYNAMIC PARAMETERS OF A FLEXIBLE AIRCRAFT
L. Goes, ITA, Brazil
  15:00 15:30 8.5.3 PRELIMINARY DESIGN AND OPTIMIZATION OF A REFERENCE AIRCRAFT UNDER DYNAMIC LOADS
H. Schmidt, RWTH University, Germany
9.5More / Hybrid / Electric Propulsion
Chair: M. Fioriti
Track 9
05 - Propulsion
  14:00 14:30 9.5.1 CONCEPTUAL STUDIES OF DIFFERENT TYPE OF HYBRID ELECTRIC PROPULSION SYSTEMS FOR COMMUTER AIRLINERS
V.S. Zakharchenko, CENTRAL INSTITUTE OF AVIATION MOTORS, Russia
  14:30 15:00 9.5.2 THERMAL MANAGEMENT FOR GASOLINE ENGINE-BATTERY HYBRID PROPULSION SYSTEM OF SMALL UAV PLATFORM
H.R. Gwon, Korean Air R&D Center, South Korea
  15:00 15:30 9.5.3 COMPARATIVE ANALYSIS OF THE HWB WITH MECHANICAL AND ELECTRICAL DRIVEN
M. Fioriti, Politecnico di Torino, Italy
Reserve Paper 9.5.R DIGITAL SIMULATION OF STARTER/GENERATOR CONTROL FOR MORE ELECTRIC ENGINE
J XU, AECC COMMERCIAL AIRCRAFT ENGINE CO., LTD., China
10.5Boundary Control
Chair: E. Itoh
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  14:00 14:30 10.5.1 INFLUENCE OF STABILITY AND CONTROL DERIVATIVES IN PIO PHENOMENON
G.D.A.N. Daher de Alencar Neves, Escola de Engenharia de São Carlos, Brazil
  14:30 15:00 10.5.2 AIRCRAFT GROUND MOTION SIMULATION ORIENTED 6 DEGREE OF FREEDOM MODEL
N. Bai Bai, Beihang University, China
  15:00 15:30 10.5.3 RE-ENTRY TRAJECTORY TRACKING CONTROL OF A MICRO-SATELLITE SYSTEM WITH A DEPLOYABLE FRONT STRUCTURE
M. Mattei, Università della Campania "Luigi Vanvitelli", Italy
Reserve Paper 10.5.R INFLUENCE OF AERODYNAMIC ASYMMETRY ON SPIN PARAMETERS OF THE COMMON RESEARCH MODEL
M. Sidoryuk, Central Aerohydrodynamic Institute (TsAGI) , Russia
11.5UAV Conflict Avoidance 1
Chair: R. Sabatini
Track 11
06.2 - Flight Dynamics and Control (UAV related)
  14:00 14:30 11.5.1 IMPLEMENTATION OF VELOCITY OBSTACLE METHOD ON A QUADROTOR UNMANNED AERIAL VEHICLE FOR DYNAMIC CONFLICT AVOIDANCE
Y.I. Jenie, FTMD - Institut Teknologi Bandung, Indonesia
  14:30 15:00 11.5.2 MPC BASED PARTIAL TRAJECTORY PLANNING FOR MULTIROTOR WITH POINT CLOUD OBSTACLES
H. Ahn, KAIST, South Korea
  15:00 15:30 11.5.3 VELOCITY OBSTACLE METHOD IN OPTICAL FLOW FRAMEWORK FOR AUTOMATIC CONFLICT DETECTION AND RESOLUTION IN UAVS
Y.I. Jenie, Faculty of Mechanical and Aerospace Engineering, ITB, Indonesia
Reserve Paper 11.5.R MOTHERSHIP PLANE WITH SENSING DRONES SYSTEM FOR 3D MAPPING APPLICATIONS
M.J. Modzelewski, Warsaw University of Technology, Poland
12.5Dynamics and Noise
Chair: J. Jokinen
Track 12
04.1 - Material Issues, Fatigue and Damage Tolerance
  14:00 14:30 12.5.1 THE NOISE REDUCTION STUDY OF COMPOSITE ACOUSTIC LINER ON HIGH BYPASS RATIO TURBOFAN AEROENGINE
P-H Hou, Shenyang Aeroengine Research Institute, China
  14:30 15:00 12.5.2 DYNAMIC RESPONSE AND DAMAGE OF THE FAN BLADES DURING UAV INGESTION INTO AN AERO-ENGINE
N.D Hou, China
  15:00 15:30 12.5.3 EXPERIMENTAL AND NUMERICAL STUDY ON BALLISTIC IMPACT OF ARAMID FABRIC
H. Pei, China
Reserve Paper 12.5.R ANALYSIS OF THE DYNAMIC RESPONSE AND FAILURE OF FABRIC SUBJECTED TO BLAST LOADING
J.C Jiang, Civil Aviation University of China, China
13.5Systems & Components Safety
Chair:
Track 13
10 - Safety and Security
  14:00 14:30 13.5.1 AIRCRAFT INFLIGHT ICING DETECTION AND DIAGNOSIS METHODS
D. D. Ding, China Aerodynamics Research and Development Center, China
  14:30 15:00 13.5.2 DESIGN AND RESEARCH ON SAFETY ANALYSIS TOOL FOR AVIONICS SYSTEM
Yu Liu, Shanghai Aircraft Design and Research Institute, China
  15:00 15:30 13.5.3 A PROTOTYPE WHIRL TOWER FOR TESTING INSOLATED ROTOR SYSTEMS IN HOVER
M. Wojtas, ?ukasiewicz Research Network - Institute of Aviation, Poland
Reserve Paper 13.5.R EXPERIMENTAL STUDY ON CRITICAL HEAT FLUX CHARACTERISTICS OF R134A FOLW BOILING IN HORIZONTAL 2.1MM TUBE UNDER HYPERGRAVI
H.JJ Jianjun, Nanjing engineering Institute of Aircraft System, Jincheng, AVIC, China
1.6Design Optimization under Uncertainty
Chair: M. Padulo
Track 1
01 - Aircraft Design and Integrated Systems
  16:00 16:30 1.6.1 ON ROBUST MULTI DISCIPLINARY ANALYSIS AND OPTIMISATION FOR NEW GENERATION FLEXIBLE AIRCRAFT
M. Saporito, University of Southampton, United Kingdom
  16:30 17:00 1.6.2 APPLICATION OF ARTIFICIAL NEURAL NETWORKS FOR EFFICIENT RELIABILITY-BASED DESIGN OPTIMIZATION
X. Chen, Cranfield University, United Kingdom
  17:00 17:30 1.6.3 VALIDATING SURROGATE MODELS AND ICORPORATING UNCERTAINTY QUANTIFICATION IN MULTI-ELEMENTS AIRFOIL DESIGN OPTIMISATION
C. Bolart, Cranfield University, United Kingdom
  17:30 18:00 1.6.4 A SET-BASED DESIGN APPROACH FOR EVOLVABILITY EXPLORATION
A.S.J. van Heerden, Cranfield University, United Kingdom
Reserve Paper 1.6.R EFFICIENT ADAPTIVE SURROGATE-BASED OPTIMIZATION USING FUZZY CLUSTERING FOR COMPLEX SYSTEM OPTIMIZATIONS
C.-N. Li, Northwestern Polytechnical University, China
2.6Hypersonics
Chair: B. Kimmel
Track 2
01 - Aircraft Design and Integrated Systems
  16:00 16:30 2.6.1 H2020 STRATOFLY PROJECT FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS
N. Viola, Politecnico di Torino, Italy
  16:30 17:00 2.6.2 THERMAL PROTECTION SYSTEM PRELIMINARY DESIGN OF STRATOFLY HIGH-SPEED PROPELLED VEHICLE
R. SCIGLIANO, Italian Aerospace Research Centre (CIRA), Italy
  17:00 17:30 2.6.3 HEXAFLY-INT HYPERSONIC VEHICLE THERMAL PROTECTION SYSTEM DESIGN
R. SCIGLIANO, Italian Aerospace Research Centre (CIRA), Italy
  17:30 18:00 2.6.4 AERODYNAMIC DESIGN THEORY AND METHODOLOGY FOR AN AIRFRAME-INLET INTEGRATED FULL-WAVERIDER VEHICLE
F. D. Ding, National University of Defense Technology, China
Reserve Paper 2.6.R NOVEL OSCULATING AXISYMMETRIC DESIGN METHOD FOR A HYPERSONIC WAVERIDER VEHICLE DERIVED FROM A POINTED VON KARMAN OGIVE
F. D. Ding, National University of Defense Technology, China
3.6Digital Pioneering - Where will MDO, MBSE, Digital Twins and AI bring engineering in 20 years?
Chair:
Track 3
4.6Turbulence Modeling
Chair: E. Bigarella
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  16:00 16:30 4.6.1 ON THE ASSESSMENT OF TURBULENCE MODELS FOR THE SIMULATION OF VORTICAL FLOWS
R. C. Gonzalez, Cranfield Unversity, United Kingdom; S. A. Prince, Cranfield University, United Kingdom
  16:30 17:00 4.6.2 COMPARISON OF DIFFERENT TURBULENCE MODELS FOR PREDICTING IMPINGING JET FLOWS
X.C Cai¹, W Dong¹; ¹Shanghai Jiao Tong University, China
  17:00 17:30 4.6.3 RESEARCH OF TURBULENCE MODELING BASED ON MACHINE LEARNING
Y. Y. Yin, Tsinghua University, China
  17:30 18:00 4.6.4 RESEARCH ON MACHINE LEARNING RECONSTRUCTION OF TURBULENCE MODEL DRIVEN BY EXPERIMENTAL DATA
Y.-F. Wang, BUAA, China
Reserve Paper 4.6.R TURBULENCE MODEL ASSESSMENT OF THE SEPARATED FLOW IN THE STANFORD DIFFUSER
M. Bonnici¹, S. A. Prince¹, K. P. Garry¹; ¹Cranfield University, United Kingdom
5.6Turbomechanics
Chair: D. Hui
Track 5
03.2 - Experimental Aerodynamics
  16:00 16:30 5.6.1 EXPERIMENT AND THEORETICAL ANALYSIS OF A TYPE OF NON-SYNCHRONOUS VIBRATION IN A HIGH PRESSURE COMPRESSOR
GAO Fei-Long, Shenyang Engine Research Institute, China
  16:30 17:00 5.6.2 COMMISSIONING A NEW VIGV WIND TUNNEL
R.G. Frank, Institute of Jet Propulsion, Bundeswehr University Munich, Germany
  17:00 17:30 5.6.3 TSAGI’S EXPERIENCE IN THE DEVELOPMENT OF SIX-COMPONENT ROTATING SHAFT BALANCES
V.S. Manvelyan, Central Aerohydrodynamic Institute (TsAGI), Russia
  17:30 18:00 5.6.4 JET FLAME RESEARCH BASED ON PHOSPHORESCENT IMAGING TECHNIQUE AND HILBERT-HUANG TRANSFORM METHOD
P Tian, Shanghai Jiao Tong University, China
Reserve Paper 5.6.R MEASUREMENT AND ANALYSIS OF INTER-STAGE FLOW FIELD IN A HIGH-LOAD AXIAL MULTISTAGE COMPRESSOR
Z.-Z. Zhang, AECC Shenyang Engine Research Institute, China
6.6Flow Control Applications 1
Chair: E. Gowree
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  16:00 16:30 6.6.1 HYBRID LAMINAR FLOW CONTROL (HLFC) RESEARCH AT AIRCRAFT RESEARCH ASSOCIATION (ARA), PAST, PRESENT AND FUTURE
P.W.C. Wong, Aircraft Research Association, United Kingdom
  16:30 17:00 6.6.2 INVESTIGATION OF LAMINARIZATION EFFICIENCY OF THE SECTIONED SUCTION SYSTEM ON THE SWEPT WING IN FAILURE CASE
S.N. Tolkachev, Central Aerohydrodynamic Institute (TsAGI), Russia
  17:00 17:30 6.6.3 ENERGY HARVESTING FROM PIEZOELECTRIC FRINGES AT THE TRAILING EDGE OF A FINITE WING WITH LEADING-EDGE TUBERCLES
M. Melo de Sousa, Instituto Superior Tecnico, Portugal
  17:30 18:00 6.6.4 HIGH-LIFT NOISE REDUCTION USING PLASMA ACTUATORS
G. P. G. Silva, University of Sao Paulo, Brazil
Reserve Paper 6.6.R INVESTIGATION OF ROLL ATTENUATION MECHANISM OF LOW-ASPECT-RATIO WINGS USING BIONIC FLOW CONTROL APPROACHES
T. Hu, Beihang University, China
7.6Flapping Wing/MAV
Chair:
Track 7
03.4 - Applied Aerodynamics
  16:00 16:30 7.6.1 INVESTIGATION AERODYNAMICS FLAPPING FLIGHT ROBOTIC BIRD
H.W.M. Hoeijmakers, University of Twente, Netherlands
  16:30 17:00 7.6.2 DEFORMATION AND FLOWFIELD INVESTIGATION OF A FLAPING-WING MAV IN GROUND EFFECT
J WANG, Northwestern Polytechnical University, China
  17:00 17:30 7.6.3 EFFECTS OF SPANWISE AREA DISTRIBUTION ON AERODYNAMIC PERFORMANCE OF FLAPPING WINGS IN HOVER
Z CAO, Northwestern Polytechnical University, China
  17:30 18:00 7.6.4 THE INFLUENCE OF SWEEPING MOTION ON THREE-DIMENSIONAL FLOW PATTERNS AND AERODYNAMIC PERFORMANCE OF FLAPPING WINGS
T.-W. Wu, Northwestern Polytechnical University, China
Reserve Paper 7.6.R BIO-INSPIRED AERODYNAMIC OPTIMISATION OF BLUFF-BODIES
E.R.G Gowree, ISAE-SUPAERO, France
8.6Buckling and Instability
Chair: J. Juracka
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  16:00 16:30 8.6.1 ACHIEVEMENTS IN THE BUCKLING OF THIN-WALLED COMPOSITE LAUNCHER STRUCTURES
RD Degenhardt, DLR, Germany
  16:30 17:00 8.6.2 THE VIBRATION CORRELATION TECHNIQUE – A RELIABLE NONDESTRUCTIVE METHOD TO PREDICTBUCKLING LOADS
- Abramovich, Technion, I.I.T.,, Israel
  17:00 17:30 8.6.3 INVESTIGATION OF BUCKLING RESPONSE OF CYLINDRICAL SHELLS USING 3D-PRINTING TECHNOLOGY
C. Bisagni, Delft University of Technology, Netherlands
  17:30 18:00 8.6.4 KINEMATIC MODEL OF REFINED THEORY AND EXACT ANALYTICAL SOLUTIONS OF STATIC AND BUCKLING PROBLEMS OF STRUCTURALLY-ANISOTR
L M Liubov, Moscow Aviation Institute (NRU), Russia
Reserve Paper 8.6.R OPTIMIZATION AND STRENGTH TESTS OF COMPRESSED COMPOSITE TUBE AS A MAIN ELEMENT OF MECHANICAL FLIGHT CONTROL SYSTEM.
W. Grendysa, Warsaw University of Technology, Poland
9.6Transition Physics 1
Chair: C. Atkin
Track 9
03.3 - Basic Fluid Dynamics and Flow Control
  16:00 16:30 9.6.1 EVOLUTION OF TOLLMIEN-SCHLICHTING DISTURBANCES OVER NATURALLY DISTRIBUTED ROUGH SURFACES
S. Mughal, Imperial College London, United Kingdom
  16:30 17:00 9.6.2 VIBRATION INDUCED EXCITATION AND CONTROL OF TOLLMIEN-SCHLICHTING WAVES
E.R.G Gowree, ISAE-SUPAERO, France
  17:00 17:30 9.6.3 NON-LINEAR BOUNDARY LAYER RECEPTIVITY TO FREE-STREAM TURBULENCE
D. Sboev, Central Aerohydrodynamic Institute (TsAGI), Russia
  17:30 18:00 9.6.4 STABILITY ANALYSIS OF STREAMWISE CORNER FLOW
D Xu, Tsinghua University, China
10.6Decoupling Control
Chair: Q. Wang
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  16:00 16:30 10.6.1 LANDING PERFORMANCE OF BOX-WING AIRCRAFT USING DIRECT LIFT CONTROL IN TURBULENT ATMOSPHERE
C. Varriale, Delft University of Technology, Netherlands
  16:30 17:00 10.6.2 DECISION-MAKING MODELLING: APPLICATION TO APPROACH PHASE IN AUTONOMOUS AIR TO AIR REFUELLING
I Romo, Airbus, Spain
  17:00 17:30 10.6.3 ADVANCED REFUELING BOOM SYSTEM (ARBS) AUTOMATIC AIR TO AIR REFUELING FLIGHT CONTROL LAWS
A. Sanz de Blas, Airbus Defence & Space, Spain
  17:30 18:00 10.6.4 DECOUPLING CONTROL LAW DESIGN FOR AN OBLIQUE-WING AIRCRAFT BASED ON EIGENSTRUCTURE ASSIGNMENT AND MODEL FOLLOWING
L Qiu, Chinese Flight Test Establishment, China
Reserve Paper 10.6.R GAIN SCHEDULING BY FREQUENCY SHAPED LINEAR QUADRATIC CONTROL OF FIXED-WING AIRCRAFT LONGITUDINAL MOTION.
L.S. Kim, Korea Advanced Institute of Science and Technology, South Korea
11.6UAV Dynamics and Control 2
Chair: J. Bai
Track 11
06.2 - Flight Dynamics and Control (UAV related)
  16:00 16:30 11.6.1 A VARIABLE-FIDELITY METHOD FOR UNMANNED AIRCRAFT WAKE VORTEX SAFETY AND CONTROL ANALYSIS
V. Golubev, ERAU, United States
  16:30 17:00 11.6.2 MULTIROTOR VEHICLES DESIGN BASED ON DYNAMIC MANIPULABILITY FOR UNDERACTUATED FLYING SYSTEMS
S. Hokamoto, Kyushu Univ., Japan
  17:00 17:30 11.6.3 LANDING SYSTEM USING EXTENDED DYNAMIC WINDOW APPROACH FOR FIXED-WING UAV
S Ishioka, Nihon university, Japan
  17:30 18:00 11.6.4 MPPC OF MULTICOPTER WITH FAULT ROTOR IN COLLISION SITUATION
Y Shimizu, Univerisity of Tokyo, Japan
Reserve Paper 11.6.R AUTONOMOUS CONTROL OF FIXED-WING UNMANNED AERIAL SYSTEMS(UASS) BY REINFORCEMENT LEARNING
H. Wang, AVIC Xi'an Flight Automatic Control Research Institute, China
12.6Fatigue Assessment
Chair: J. van Doeselaar
Track 12
04.1 - Material Issues, Fatigue and Damage Tolerance
  16:00 16:30 12.6.1 TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES AEROSTRUCTURES
I. Rivero Arevalo, Airbus, Spain
  16:30 17:00 12.6.2 STUDY OF COMPOSITE SKIN-STRINGER FATIGUE BEHAVIOR UNDER BROADBAND RANDOM VIBRATION
F. Sevastyanov, The Central Aerohydrodynamic Institute named after N.E.Zhukovsky, Russia
  17:00 17:30 12.6.3 APPROACH OF THE STATIC AND FATIGUE STRENGTH ESTIMATION OF THE COMPOSITE JOINTS
A.A. Sviridov, The Central Aerohydrodynamic Institute, Russia
  17:30 18:00 12.6.4 FAILURE CRITERION OF CFRP FOR OPEN-HOLE FATIGUE TESTING
A.G. Kalinin, TsAGI, Russia
Reserve Paper 12.6.R MODEL CURVES: A SIMPLE WAY TO ACCOUNT FOR COMPLEX EFFECTS
A.A. Bautin, TsAGI, Russia
13.6Safety and Security Analysis
Chair:
Track 13
10 - Safety and Security
  16:00 16:30 13.6.1 RESEARCH ON SAFETY ASSESSMENT APPROACH FOR UAS OPERATIONS OVER UNINHABITED AREAS
ZQ Zhang, Northwestern Polytechnical University, China
  16:30 17:00 13.6.2 END TO END CYBERSECURITY IN CIVIL AVIATION ECO SYSTEM
JC Jean-Claude, Airbus, France
  17:00 17:30 13.6.3 STUDY ON DYNAMIC RESPONSE AND INJURY OF FRONT ROW OCCUPANT UNDER HORIZONTAL IMPACT
M.S.C. MA, Civil Aviation University of China, China
  17:30 18:00 13.6.4 STATISTICAL ANALYSIS OF AIRCRAFT INCIDENTS M-28 BRYZA
J. Tomaszewska, Polish Air Force University, Poland
Reserve Paper 13.6.R FIRE AND EXPLOSION ANALYSIS OF AIRCRAFT FUEL TANK BASED ON TNT EQUIVALENT METHOD AND FIREBALL EXPLOSION MODEL
W K KAI, AVIC XI'AN AIRCRAFT INDUSTRY (GROUP) COMPANY LTD, China
1.7Design Methods
Chair: E. Cestino
Track 1
01 - Aircraft Design and Integrated Systems
  09:30 10:00 1.7.1 IMPACT OF NEW TECHNOLOGIES ON AIRCRAFT SYSTEMS
A. Berres, German Aerospace Center, Germany
  10:00 10:30 1.7.2 APPLICATIONS OF FAST: AN OPEN SOURCE TOOL FOR AIRCRAFT CONCEPTUAL AND PRELIMINARY DESIGN
S. M. Delbecq, ISAE-SUPAERO, France
  10:30 11:00 1.7.3 MICLADO – LAMINAR AIRCRAFT DESIGN WITH MICADO
F. Schueltke, RWTH Aachen University, Institute of Aerospace Systems, Germany
  11:00 11:30 1.7.4 LAMBDA: A KNOWLEDGE-BASED MODULAR, MULTIFIDELITY AND MULTIDISCIPLINARY AIRCRAFT CONCEPTUAL DESIGN ENVIRONMENT
S. Hosseini, Amirkabir University of Technology, Iran
  11:30 12:00 1.7.5 IMPROVED LINEAR METHOD FOR SONIC BOOM PREDICTION OF SUPERSONIC TRANSPORTS
Y.-L. Ding, Northwestern Polytechnical University, China
Reserve Paper 1.7.R AERODYNAMIC SHAPE OPTIMIZATION PLATFORM ASSISTED WITH SURROOPT AND CPACS TECHNIQUE
C.-Y. Ma, Northwestern Polytechnical University, China
2.7UAS 1
Chair: R. Gerhards
Track 2
01 - Aircraft Design and Integrated Systems
  09:30 10:00 2.7.1 MULTIDISCIPLINARY OPTIMISATION OF A FUEL-CELL-POWERED EVTOL FIXED-WING CARGO UAV
D. Verstraete, The University of Sydney, Australia
  10:00 10:30 2.7.2 CONCEPTUAL DESIGN FOR LONG-ENDURANCE CONVERTIBLE UNMANNED AERIAL SYSTEM
Y Leng, ISAE, France
  10:30 11:00 2.7.3 DESIGN OF A HYBRID-POWER VTOL LOGISTICS UAV SYSTEM INTEGRATED INTO THE CIVIL AVIATION AIR TRAFFIC MANAGEMENT SYSTEM
H.-J. Jiang, Xi'an Tangyan Aviation Technology CO. LTD, China
  11:00 11:30 2.7.4 SURROGATE-BASED MULTIDISCIPLINARY DESIGN OPTIMIZATION OF MULTIROTOR DRONES
S. M. Delbecq, ISAE-SUPAERO, France
  11:30 12:00 2.7.5 AERODYNAMIC ANALYSIS ON TAIL-SITTER UAV HOVERING UNDER CROSSWIND
Chen Jiaojiao Jiaojiao, Northwestern Polytechnical University, China
Reserve Paper 2.7.R CONCEPTUAL DESIGN AND IMPLEMENTATION OF A NOVEL TRICOPTER FIXED-WING VTOL UAV CONFIGURATION
P. Stahl, Technical University of Munich, Germany
3.7Model Based Systems Engineering
Chair: P. Vijgen
Track 3
02 - Systems Engineering and Integration
  09:30 10:00 3.7.1 MODEL-BASED ENGINEERING OF A SYSTEM DIAGNOSTIC ENGINE FOR AN AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM
F. Mardt, Hamburg University of Technology, Germany
  10:00 10:30 3.7.2 A MBSE DESIGN ARCHITECTURE FOR CONTROL SYSTEM BASED ON DEMAND ELEMENT TRANSFER
P.J. Wang, Tsinghua University, China
  10:30 11:00 3.7.3 A DOCUMENT-BASED VS. MODEL-BASED APPLICATION OF THE NASA SYSTEMS ENGINEERING PROCESS
L. Boggero, German Aerospace Center (DLR), Germany
  11:00 11:30 3.7.4 TOWARDS THE NEXT GENERATION OF COMPLEX SYSTEMS ARCHITECTING: A MBSE FRAMEWORK TO AIRCRAFT DEVELOPMENT
P. D. Ciampa, DLR, Germany
  11:30 12:00 3.7.5 HYBRID MODELLING FOR FULL MISSION SIMULATION
P Krus, Linköping university, Sweden
Reserve Paper 3.7.R SOS BEHAVIOR MODEL TRANSFORMATION FOR AIRCRAFT TOP-LEVEL DEMONSTRATION
J Zang, Aviation Industry Development Research Center of China, China
4.7Applied CFD 1
Chair: S. Wei
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  09:30 10:00 4.7.1 EXPERIMENTAL VALIDATION OF NUMERICAL PREDICTION OF WING-PROPELLER AERODYNAMIC INTERACTION
L. P. Ruiz Calavera, Airbus Defence & Space, Spain
  10:00 10:30 4.7.2 FLOW STRUCTURE INVESTIGATION OF CONTRA-ROTATING WIND TURBINES BY CFD AND EXPERIMENTAL METHODS
K You, Northwestern Polytechnical University, China
  10:30 11:00 4.7.3 STATIC AEROELASTIC COMPUTATIONS OF WING CONFIGURATIONS IN TRANSONIC FLOWS AT HIGH REYNOLDS NUMBERS
J. A. A. Lyrio, Instituto Tecnológico de Aeronáutica, Brazil
  11:00 11:30 4.7.4 NUMERICAL INVESTIGATION OF WING ROCK PHENOMENON ON LOW ASPECT RATIO RECTANGULAR WINGS AT LOW REYNOLDS NUMBER
N/A Maqsood, Pakistan
  11:30 12:00 4.7.5 A COMPUTATIONAL FLUID DYNAMICS ANALYSIS OF A HISTORICAL SEAPLANE CRUISE AND TAKE OFF PERFORMANCE
E. Cestino, Politecnico di Torino, Italy
Reserve Paper 4.7.R FLUID STRUCTURE INTERACTION OF RAM-AIR PARACHUTE TRAILING EDGE DEFLECTION
Gao XL Gao, China Aerodynamics Research and Development Center, China
5.7Transonic/Supersonic
Chair: S. Prince
Track 5
03.2 - Experimental Aerodynamics
  09:30 10:00 5.7.1 NEW INVESTIGATION METHOD OF THE SHOCK WAVE/BOUNDARY LAYER INTERACTION PATTERN AT TRANSONIC SPEEDS
M.A. Brutyan, TsAGI, Russia
  10:00 10:30 5.7.2 INFLUENCE OF VARIABLE WALL PERFORATION RATIO ON BOUNDARY LAYER PARAMETERS AT TRANSONIC SPEEDS
S.L. Osipova, Central Aerohydrodynamic Institute named after N.E. Zhukovsky, Russia
  10:30 11:00 5.7.3 RESEARCH OF HYBRID LAMINAR FLOW CONTROL TECHNOLOGY FOR CIVIL AIRCRAFT WING
C. Shao, Shanghai Aircraft Design and Research Institute, COMAC, China
  11:00 11:30 5.7.4 STUDY OF SHOCK WAVE / LAMINAR BOUNDARY LAYER INTERACTION AREA BY PIV TECHNIQUE
Oleg: O. Vishnyakov, Khristianovich Institute of Theoretical and Applied Mechanics SB, Russia
  11:30 12:00 5.7.5 DEVELOPMENT OF THE MODEL NEAR-FIELD STUDY TECHNIQUES INTHE SUPERSONIC WIND TUNNELS AIMED AT THE SONIC BOOM PREDICTION
A.I. IVANOV, TSAGI, Russia
Reserve Paper 5.7.R THE EXPERIMENTAL INVESTIGATION OF THE THROTTLING SECOND THROAT INFLUENCE ON TRANSONIC WIND TUNNEL FLOW QUALITY
Z HaiYang, China Aerodynamics Research and Development Center, Facility des, China
6.7Unsteady Flow Phenomena
Chair: C. Breitsamter
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  09:30 10:00 6.7.1 INVESTIGATIONS OF AERODYNAMIC CHARACTERISTICS AND LAMINAR-TURBULENT TRANSITION ON LARGE-SCALE TRANSONIC AIRFOIL
V.G. Soudakov, TsAGI, Russia
  10:00 10:30 6.7.2 TYPES OF TRANSONIC BUFFET FOR A LAMINAR AIRFOILS
P.A. Polivanov, Khristianovich Institute of Theoretical and Applied Mechanics SB, Russia
  10:30 11:00 6.7.3 BUFFET CONTROL ON STRUCT-BRACED WING AIRCRAFT USING TANGENTIAL BLOWING
S Li, School of Aerospace Engineering, Tsinghua University, China
  11:00 11:30 6.7.4 HIGH-FIDELITY ANALYSIS OF ROBUST NONLINEAR 2-DOF AIRFOIL LCO CONTROL
V. Golubev, ERAU, United States
  11:30 12:00 6.7.5 ANALYSIS AND CONTROL OF DYNAMIC STALL CHARACTERISTICS OF S809 AIRFOIL
L-S Hao, Northwestern Polytechnical University, China
Reserve Paper 6.7.R PHISICAL AND MATHEMATICAL MODELS OF THE BUFFET ONSET
A.M. Lipanov, Institute of Applied Mathematics, Russia
7.7Optimization 1
Chair:
Track 7
03.4 - Applied Aerodynamics
  09:30 10:00 7.7.1 SPARSE POLYNOMIAL CHAOS EXPANSION BASED ON FULLY ADAPTIVE FORWARD-BACKWARD SELECTION METHOD
Huan Zhao, China
  10:00 10:30 7.7.2 ON IMPROVING GRADIENT-ENHANCED KRIGING MODEL FOR AERODYNAMIC DESIGN OPTIMIZATION
D.H.D. Dang, Northwestern Polytechnical University, China
  10:30 11:00 7.7.3 FAR-FIELD WAVEFORM DESIGN OPTIMIZATION BASED ON SONIC BOOM NOISE LEVEL
J.-L. Qiao, Northwestern Polytechnical University, China
  11:00 11:30 7.7.4 PREDICTION OF FLIGHT DYNAMICS IN WAKE SURFING SCENARIOS
MML Lone, Cranfield University, United Kingdom
  11:30 12:00 7.7.5 IMPROVED WEIGHTED GRADIENT-ENHANCED KRIGING MODEL FOR HIGH-DIMENSIONAL AERODYNAMIC DESIGN OPTIMIZATION PROBLEMS
C.-Z. Xu, China
Reserve Paper 7.7.R AERODYNAMIC DESIGN OPTIMIZATION OF WAVERIDER-DERIVED VEHICLE
W. Su, Beijing Institute of Space Long March Vehicle, China
8.7Design of Aircraft Structures
Chair: E. Cestino
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  09:30 10:00 8.7.1 AN INVERSE APPROACH BASED ON EUCLIDEAN SPACE FOR DETERMINING STRUCTURAL LOAD DISTRIBUTION FROM STRAIN MEASUREMENTS
H.N. Dui, AVIC, Chengdu Aircraft Design & Research Institute, China
  10:00 10:30 8.7.2 DESIGN OF EXPERIMENTS TECHNIQUES TO INVESTIGATE LOAD SHARE STRATEGIES BETWEEN AERO ENGINE, NACELLE AND POWERPLANT COMPONENTS
C.-M MARTIN , Queens University Belfast, United Kingdom
  10:30 11:00 8.7.3 THERMOPLASTIC APPLICATIONS FOR AEROSTRUCTURES: TOWARDS SUSTAINABLE AND WEIGHT EFFICIENT APPLICATIONS
M HERMAN, Airbus, France
  11:00 11:30 8.7.4 RATIONAL DETERMINATION OF WING JIG SHAPE OF A LONG-RANGE AIRCRAFT WITH TRANSONIC CRUISE REGIME
A.V. Bezuevsky, TsAGI, Russia
  11:30 12:00 8.7.5 AIRCRAFT ENGINE ROTOR DYNAMICS ANALYSIS AFTER FAN BLADE-OUT WITH ACCOUNT OF ROTOR-CASING CONTACT INTERACTIONS
V. Myasnikov, Central Institute of Aviation Motors, Russia
Reserve Paper 8.7.R THE METHOD OF AIRCRAFT MATHEMATICAL MODEL STIFFNESS PROPERTIES CORRECTION BASED ON EXPERIMENTAL RESEARCH RESULTS
M.A. Pronin, Central Aerohydrodynamic Institute n.a. prof. N.E.Zhukovsky, Russia
9.7Advanced Manufacturing
Chair: L. Rupeng
Track 9
08 - Manufacturing and Supply Chain Management
  09:30 10:00 9.7.1 NUMERICAL AND EXPERIMENTAL INVESTIGATION OF POST-MACHINING DISTORTION FOR LARGE AEROSPACE MONOLITHIC COMPONENTS
BS SHI, National Research Council Canada, Canada
  10:00 10:30 9.7.2 RESEARCH ON THE DEVELOPMENT AND PERFORMANCE OF THE OBSTACLE-PASSING STRUCTURE OF THE CRAWLER INSPECTION ROBOT
Pu Zhang¹, Jin Sun¹; ¹Beihang University, China
  10:30 11:00 9.7.3 SOFTWARE-BASED IMPROVING THE QUALITY OF HIGH-SPEED MACHINING
S. Zietarski, Military University of Technology, Poland
  11:00 11:30 9.7.4 RESEARCH ON MANUFACTURING PROCESS AND MICROSTRUCTURE OF SIC/ALSI7MG COMPOSITE FABRICATED BY SELECTIVE LASER MELTING
H Zhu, China
  11:30 12:00 9.7.5 EXPERIMENTAL STUDY ON PATH PLANNING OF BELT GRINDING FOR BIOMIMETIC SURFACE ON AERO-ENGINE BLADE
Chongqing Univer Xiao, China
Reserve Paper 9.7.R RESEARCH ON SOLVING PROBLEM OF AIRCRAFT ASSEMBLY COORDINATION BASED ON 3D LASER SCANNING MEASUREMENT TECHNOLOGY
W J JIAN, China
10.7Flight Dynamics
Chair: T. Götzendorf Grabowski
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  09:30 10:00 10.7.1 VIRTUAL FLIGHT TEST OF A BWB AIRCRAFT IN LOW SPEED WIND TUNNEL
B.W. NIE, National University of Defense Technology, China
  10:00 10:30 10.7.2 INVESTIGATION INTO FLIGHT DYNAMICS OF A BLENDED-WING-BODY AIRCRAFT
F. CEN, China
  10:30 11:00 10.7.3 BAYESIAN APPROACH TO SIMULTANEOUS STATIC AND DYNAMIC FLIGHT CHARACTERISTICS MODELING
M. Naruoka, Japan Aerospace Exploration Agency, Japan
  11:00 11:30 10.7.4 THE ANALYSIS OF TAKEOFF ROTATION OF SUBSCALE FREE-FLIGHT TESTS
K.-M. MA, Xi’an Aircraft Design Institute, China
  11:30 12:00 10.7.5 SIMULTANEOUS ESTIMATION OF DERIVATIVES, TRIM STATES, AND WIND
Yoshimasa: Y. Ochi, National Defense Academy, Japan
Reserve Paper 10.7.R SEPARATE IDENTIFICATION OF AIRCRAFT THRUST AND DRAG FORCES THROUGH FLIGHT TEST DATA
O. N. Korsun, Moscow Aviation Institute (National Research University), Russia
11.7Actuator design & Analysis
Chair: J. Mare
Track 11
07 - Systems, Subsystems and Equipment
  09:30 10:00 11.7.1 LIEBHERR-AEROSPACE EHA TECHNOLOGY FOR FUTURE FLIGHT CONTROL APPLICATION
T. Röben, Liebherr-Aerospace, Germany
  10:00 10:30 11.7.2 THE DEVELOPMENT OF ALGORITHMS FOR EMA FAULT EARLY DETECTION SYSTEM
A.V. Skryabin, 1. Central Aerohydrodynamic Institute of Russia, Russia
  10:30 11:00 11.7.3 CONCEPTUAL STUDY OF THE DIGITAL HYDRAULIC ACTUATOR WITH PROPORTIONAL CONTROL FOR FLIGHT CONTROL ACTUATION SYSTEMS
A. Dell'Amico, Saab AB, Sweden
  11:00 11:30 11.7.4 VIRTUAL PROTOTYPING OF ELECTRICAL THS ACTUATOR FOCUSED ON MECHANICAL POWER TRANSMISSION FUNCTIONS
J. FU FU, BEIHANG UNIVERSITY, China
  11:30 12:00 11.7.5 DYNAMIC ANALYSIS AND CONTROL DESIGN OF A FAULT-TOLERANT ELECTRO-MECHANICAL ACTUATOR WITH DIFFERENTIAL BALL SCREWS
G. Di Rito, Università di Pisa - Dipartimento di Ing. Civile ed Industriale, Italy; N. Borgarelli¹, M. Nardeschi¹, B. Luciano, AESIS s.r.l., Italy; ¹Umbra Group S.p.A., Italy
Reserve Paper 11.7.R A RESEARCH ON POSITION CONTROL ACTUATORS FOR FIXEDWINGED RESEARCH UAVS
D.T. Teubl, Institute of Aircraft Design TUM, Germany
12.7Air Traffic Efficiency
Chair: D. Nguyen
Track 12
09 - Air Transport System Efficiency
  09:30 10:00 12.7.1 IMPACT OF ENROUTE TIME-BASED METERING ON EQUITY IN DELAY DISTRIBUTION
A. Andreeva-Mori, JAXA, Japan
  10:00 10:30 12.7.2 SPATIO-TEMPORALLY CORRELATED WIND MODELING AND PROBABILISTIC TRAJECTORY PREDICTION USING ENSEMBLE WEATHER FORECASTS
Y Matsuno, Japan Aerospace Exploration Agency, Japan
  10:30 11:00 12.7.3 IMPACT ASSESSMENT OF ENHANCED AIR TRANSPORT CONCEPTS ON AIRLINE OPERATIONAL SCHEDULES
J. Michelmann, Institute of Aircraft Design, Technical University of Munich, Germany
  11:00 11:30 12.7.4 COGNITIVE HUMAN-MACHINE INTERFACES FOR ENROUTE AIR TRAFFIC FLOW MANAGEMENT
A. Gardi, RMIT University, Australia
  11:30 12:00 12.7.5 RESEARCH ON TRAJECTORY OPTIMIZATION TECHNOLOGY CONSIDERING METEOROLOGICAL INFORMATION PREDICTION
G.-W Guo, China National Aeronautical Radio Electronics Research Institute, China
Reserve Paper 12.7.R STANDARD TERMINAL AUTOMATION REPLACEMENT SYSTEM ENHANCEMENT 2 - BENEFITS ANALYSIS THROUGH FAST-TIME MODELING
R. Dean, Regulus Group, United States
13.7Fan / Nacelle & Propeller
Chair: S. Pankov
Track 13
05 - Propulsion
  09:30 10:00 13.7.1 GEARED FANS AND VARIABLE PITCH FANS - NUMERICAL AND EXPERIMENTAL INVESTIGATIONS OF THEIR AERODYNAMICS
S.V. Pankov, Central Institute of Aviation Motors (CIAM), Russia
  10:00 10:30 13.7.2 ANALYSIS OF AERODYNAMIC CHARACTERISTICS OF PROPELLERS AT LOW ADVANCE RATIO USING A WHIRLING ARM
Y.I. Itoh, Iwate university, Japan
  10:30 11:00 13.7.3 EXPERIMENTAL STUDIES OF SLOT-TYPE CASING TREATMENTS FOR MODEL FANS WITH THE AIM OF AERODYNAMIC AND ACOUSTIC IMPROVEMENTS
V.I. Mileshin, Central Institute of Aviation Motors, Russia
  11:00 11:30 13.7.4 ANALYSIS OF THRUST-SCALED PROPELLER NOISE AND ITS TRADE-OFF WITH PROPELLER EFFICIENCY
T. Sinnige, Netherlands
  11:30 12:00 13.7.5 MODELING OF COUNTER-ROTATING LIFT FAN/MAIN ENGINE COMBINED PROPULSION SYSTEM AND LIFT FAN AERODYNAMIC DESIGN
H.-L JIN, AECC Hunan Aviation Powerplant Research Institute, China
Reserve Paper 13.7.R AERODYNAMICS DESIGN, OPTIMIZATION AND FLOW FIELD INVESTIGATION OF A CONTRA-ROTATING PROPFAN AT HIGH FLIGHT MACH NUMBERS
T Wu¹, W Dong¹; ¹Shanghai Jiao Tong University, China
1.8Hybrid/Electric & Unconventional Aircraft 2
Chair: J. Melkert
Track 1
01 - Aircraft Design and Integrated Systems
  14:00 14:30 1.8.1 PRELIMINARY FEASIBILITY STUDY OF A HYBRID TURBOPROP
R. Martínez-Val, Univ. Politécnica Madrid, Spain
  14:30 15:00 1.8.2 EXPERIMENTAL RESEARCH ON PROPULSION AND AERODYNAMIC CHARACTERISTICS OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT
X.-Y. ZHANG, Northwestern Polytechnical University, China
  15:00 15:30 1.8.3 PROPULSIVE FUSELAGE AIRCRAFT CONCEPT – A SUMMARY OF STRUCTURE ANALYSIS BASED ON CENTRELINE H2020
Z. Goraj, Warsaw University of Technology, Poland
2.8Education & Knowledge Management
Chair: R. Fusaro
Track 2
01 - Aircraft Design and Integrated Systems
  14:00 14:30 2.8.1 TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55X
L. Di Ianni, Politecnico di Torino, Italy
  14:30 15:00 2.8.2 INTERNATIONAL VIRTUAL COLLABORATION IN UNDERGRADUATE AERONAUTICAL ENGINEERING EDUCATION – CHALLENGES AND EXPERIENCES
J. Abulawi, HAW Hamburg, Germany
  15:00 15:30 2.8.3 OPEN SCIENCE IN AVIATION RESEARCH: THE INDIVIDUAL ADVANTAGE OF SHARING KNOWLEDGE
M. Spieck, Thelsys GmbH, Germany
3.8UAV Conflict Avoidance 2
Chair: H. Bang
Track 3
06.2 - Flight Dynamics and Control (UAV related)
  14:00 14:30 3.8.1 A RECURRENT PLANNING STRATEGY FOR UAV PATH IDENTIFICATION IN A DYNAMIC ENVIRONMENT BASED ON BIT-CODED FLIGHT MANOEUVRES
L. BLASI, UNIVERSITA' DELLA CAMPANIA "LUIGI VANVITELLI", Italy
  14:30 15:00 3.8.2 A NOVEL DETECT-AND-AVOID SYSTEM OF UAS IN URBAN ENVIRONMENT
L.N. Nurhakim, RMIT University, Australia
  15:00 15:30 3.8.3 AUTONOMOUS CONFLICT RESOLUTION ALGORITHM BASED ON ELLIPTIC GEOMETRY
R.A. Sasongko, Institut Teknologi Bandung, Indonesia
Reserve Paper 3.8.R HYDRO ENVIRONMENTAL MAPPING TOOL USING SWARMS AND MACHINE LEARNING, UAV & USV
R.K.R. Kuntz, Brazil
4.8Numerical Methods 2
Chair: A. Viviani
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  14:00 14:30 4.8.1 VALIDATION OF A DISCONTINUOUS GALERKIN BASED DES SOLVER IN FLOW PROBLEMS USING HIGH PERFORMANCE COMPUTING
A.V. Wolkov, TsAGI, Russia
  14:30 15:00 4.8.2 ADVANCED WEEK SOLUTIONS IN FLUID DYNAMICS AND THEIR NUMERICAL COMPUTATIONS WITH AERODYNAMIC HEATING
M.Ja. Ivanov, Central Institute of Aviation Motors, Russia
  15:00 15:30 4.8.3 A BENCHMARK METHOD FOR PREDICTING OBLIQUE SHOCK STRUCTURE
A. Shi, Northwestern Polytechnical University, China
Reserve Paper 4.8.R ACCURATE SIMULATIONS OF AIRCRAFT WAKE VORTICES WITH HIGH-ORDER NUMERICAL METHOD
S. Bosnyakov, TsAGI, Russia
5.8Rotating Wings
Chair: E. Gowree
Track 5
03.2 - Experimental Aerodynamics
  14:00 14:30 5.8.1 COMPARISON OF ISOLATED AND DUCTED FIXED-PITCH PROPELLERS UNDER NON-AXIAL INFLOW CONDITIONS
M. Cerny, Germany
  14:30 15:00 5.8.2 INVESTIGATION OF THE CHARACTERISTICS OF THE HELICOPTER MAIN ROTOR WITH ELASTIC MOUNTING BLADES
O.-E. Kirillov, Central Aerohydrodynamic Institute (TsAGI), Russia
  15:00 15:30 5.8.3 EXPERIMENTAL MEASUREMENTS ON BIOMIMETIC WIND TURBINE BLADES BY P. TOMENTOSA SEED
L.-P Paiva, UFU, Brazil
Reserve Paper 5.8.R EXPERIMENTAL INVESTIGATION OF PULSATION OF THE ROTOR SLIPSTREAM ACTING ON AN ELEVATED HELIPORT
P. Ruchala, Institute of Aviation, Poland
6.8Flow Control Applications 2
Chair: Z. Goraj
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  14:00 14:30 6.8.1 IMPROVEMENT OF HELICOPTER PERFORMANCE THROUGH PULSE AIR-JETS BLOWN FROM THE TRAILING EDGE OF MAIN ROTOR BLADES
W.S. STALEWSKI, LUKASIEWICZ RESEARCH NETWORK - INSTITUTE OF AVIATION, Poland
  14:30 15:00 6.8.2 ENHANED STRAIGHT BLADED VAWT BY RETRACTABLE GURNEY FLAPS
K. Song, Northwestern Polytechnical University, China
  15:00 15:30 6.8.3 STUDY ON THE EFFECTS OF PROPLET GEOMETRIC PARAMETERS ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLER
B.W Wang, China
Reserve Paper 6.8.R APPLICATION OF A LEADING-EDGE TIP EXTENSION ON DELTA WING WITH WINGLET FOR HIGH LIFT
X.Y. Feng, Northwestern Polytechnical University, China
7.8Optimization 2
Chair:
Track 7
03.4 - Applied Aerodynamics
  14:00 14:30 7.8.1 AERODYNAMIC OPTIMIZATION DESIGN OF DOUBLE BLUNT ROTOR AIRFOIL WITH LARGE THICKNESS IN FORWARD AND REVERSE FLOW
Y.-M. YAO, China
  14:30 15:00 7.8.2 PARETO FRONT EXPLORATION USING MANIFOLD LEARNING APPROACH FOR ROTORCRAFT AIRFOILS DESIGN
C.-S. Song, Computational Aerodynamics Institute, China Aerodynamics Researc, China
  15:00 15:30 7.8.3 MULTI-OBJECTIVE AERODYNAMIC SHAPE OPTIMIZATION OF WIDE-MACH-NUMBER-RANGE WING CONSIDERING LIFT MATCHING
Y Zhang, NORTHWESTERN POLYTECHNICAL UNIVERSITY, China
Reserve Paper 7.8.R DESIGN OPTIMIZATION OF AIRFOILS AT ULTRA-LOW REYNOLDS NUMBERS
J.-H. Xu, Northwestern Polytechnical University, China
8.8Morphing Structures
Chair: F. Franke
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  14:00 14:30 8.8.1 RESEARCH PROGRESS OF DISTRIBUTED OPTICAL FIBER SENSING DEFORMATION MEASUREMENT FOR MORPHING WING
X-Jf Xue, Chinese Aeronautical Establishment, China
  14:30 15:00 8.8.2 ACTUATION MECHANISM USING SHAPE MEMORY ALLOY WIRES IN SPIRAL ARRANGEMENT
R Tsukamoto, Meijo University, Japan
  15:00 15:30 8.8.3 MORPHING AIRCRAFT BASED ON SMART MATERIALS AND STRUCTURES
J. Sun, Harbin Institute of Technology, China
9.8Additive Manufacturing
Chair: J. Zhang
Track 9
08 - Manufacturing and Supply Chain Management
  14:00 14:30 9.8.1 EFFECTS OF COOLANT BUILD DIRECTION ON ADDITIVELY MANUFACTURED FAN-SHAPED COOLING HOLES
Z.-Q QI, AECC HUNAN AVIATION POWERPLANT RESEARCH INSTITUTE, China
  14:30 15:00 9.8.2 APPLICATION OF ADDITIVE MANUFACTURING TO THE PRODUCTION OF RPAV COMPONENTS
E. Cestino, Politecnico di Torino, Italy
  15:00 15:30 9.8.3 DESIGNING AERONAUTICAL PARTS FOR ADDITIVE MANUFACTURING – SUPPORTED BY A VIRTUAL DESIGN ADVISOR
J. Abulawi, HAW Hamburg, Germany
Reserve Paper 9.8.R AN EFFICIENT FINITE ELEMENT SIMULATION METHOD FOR ADDITIVE MANUFACTURING PROCESSES
Q.-Y. Liu, Beihang University, China
10.8Flying Quality
Chair: N. Yokoyama
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  14:00 14:30 10.8.1 GUARANTEED FLYING QUALITIES UNDER REAL AND COMPLEX UNCERTAINTIES
D. Seiferth, Technical University of Munich, Germany
  14:30 15:00 10.8.2 CONTROL ALLOCATION FOR ONERA\'S SMALL BUSINESS CONCEPT PLANE AMPERE WITH DISTRIBUTED ELECTRIC PROPULSION
C. DÖLL, ONERA, France
  15:00 15:30 10.8.3 ON THE MAXIMIZATION OF CONTROL POWER IN LOW-SPEED FLIGHT FOR A BWB CONFIGURATION
L.M.B.C. Campos, IDMEC/CCTAE/IST, Portugal
Reserve Paper 10.8.R THE APPLICATION OF THE PILOT-AIRCRAFT SYSTEM APPROACH FOR OPTIMIZING 3D DISPLAY PARAMETERS
A. V. Efremov¹, M. S. Tiaglik¹, I. Kh. Irgaleev¹; ¹Moscow Aviation Institute, Russia
11.8System Health Monitoring
Chair: J. Mare
Track 11
07 - Systems, Subsystems and Equipment
  14:00 14:30 11.8.1 DAMAGE DETECTION OF AERONAUTICAL PANELS BY USING CROSS-CORRELATION OF SPATIALLY SHIFTED DISTRIBUTED STRAIN SENSORS
M. Ciminello, C.I.R.A. Italian Aerospace Research Center, Italy
  14:30 15:00 11.8.2 THEORETICAL AND EXPERIMENTAL STUDY FOR THE DEVELOPMENT OF SELF-POWERED MONITORING SYSTEMS WITH MFC PIEZOELECTRIC PATCHES
G. Di Rito¹, M.-R. Chiarelli¹, V. Franchi¹, L. Bancallari, MBDA Italia S.p.A., Italy; B. Luciano, AESIS s.r.l., Italy; ¹Università di Pisa - Dipartimento di Ing. Civile ed Industriale, Italy
  15:00 15:30 11.8.3 STUDY ON CLOSED-LOOP CROSS COMPENSATION CONTROL TECHNOLOGY IN ACCELERATED FATIGUE TEST
HONGWEI ZHAO¹, TAO HAN¹, ZHENZHONG GU, Chongqing Hongyu Precision Industrial Co., Ltd., China; GUANGSHENG SHI, Shenyang Aircraft Design & Research Institute of China, China; SHIHUI DUAN¹, JIANMIN FENG¹; ¹Aircraft Strength Research Institute of China, China
Reserve Paper 11.8.R RELIABILITY ANALYSIS AND EVALUATION METHOD FOR DESIGN APPRAISAL OF AIRBORNE EQUIPMENTS
Z-J-L Zhang, AVIC XI’AN AIRCRAFT INDUSTRY (GROUP) COMPANY LTD., China
12.8Airspace Management
Chair: A. Andreeva Mori
Track 12
09 - Air Transport System Efficiency
  14:00 14:30 12.8.1 ANGULAR 3D INSTRUMENT APPROACHES FOR GLS EQUIPPED AIRCRAFT USING A LIGHT AND MOBILE SBAS TO GBAS CONVERTER
T. Dautermann, DLR , Germany
  14:30 15:00 12.8.2 ON THE MINIMUM SEPARATION BETWEEN ANY PAIR OF FLIGHT PATHS
L.M.B.C. Campos, IDMEC/CCTAE/IST, Portugal
  15:00 15:30 12.8.3 AIRSPACE CAPACITY MANAGEMENT OPTIMISATION FOR TRAJECTORY BASED OPERATIONS
D. Zheng Zhang¹, E. Puntero Parla¹, M. Sánchez Cidoncha¹, F. Gómez Comendador², R. Arnaldo Valdés²; ¹CRIDA A.I.E., Spain ;²Technical University of Madrid, Spain
Reserve Paper 12.8.R DESIGNING AIRCRAFT TRAFFIC FLOWS USING DATA-DRIVEN QUEUING MODELS
E. Itoh, ENRI, Japan
13.8Structural Integrity and Fatigue
Chair: M. Liao
Track 13
04.1 - Material Issues, Fatigue and Damage Tolerance
  14:00 14:30 13.8.1 DEVELOPMENT OF AIRFRAME DIGITAL TWIN TECHNOLOGY FOR AIRCRAFT STRUCTURAL INTEGRITY MANAGEMENT PROGRAM
Min Liao, National Research Council Canada, Canada
  14:30 15:00 13.8.2 A DIGITAL EQUIVALENT DEVELOPMENT FOR FATIGUE AND DAMAGE TOLERANCE IN AIRCRAFT STRUCTURES
L. ZAPLANA MANZANO, AIRBUS , Spain
  15:00 15:30 13.8.3 EXPERIMENTAL STUDY OF THE EFFECT OF BIAXIAL STRESS STATE ON THE GROWTH RATE OF FATIGUE CRACKS
A.V. Kulemin, Central Aerohydrodynamic Institute n. a. N.E. Zhukovsky (TsAGI), Russia
Reserve Paper 13.8.R INVESTIGATION OF THE INFLUENCE OF LOW AMPLITUDE LOADS ON THE FATIGUE LIFE OF CFRP SAMPLES WITH IMPACT DAMAGE UNDER IRRE
V.G. Lukyanchuk, Central Aerohydrodynamic Institute, TsAGI, Russia, Russia
1.9Hybrid/Electric & Unconventional Aircraft 3
Chair: P. Prakasha
Track 1
01 - Aircraft Design and Integrated Systems
  16:00 16:30 1.9.1 DESIGN, OPERATIONAL AND ENVIRONMENTAL ASSESSMENT OF A HYBRID-ELECTRIC AIRCRAFT
A. E. Scholz, Technical University of Munich, Germany
  16:30 17:00 1.9.2 DESIGN FOR DIRECTIONAL CONTROL AND STABILITY OF AIRCRAFT WITH DISTRIBUTED PROPULSION
J.S.E. Soikkeli¹, M.F.M. Hoogreef¹; ¹Delft University of Technology, Netherlands
  17:00 17:30 1.9.3 VALIDATION OF AN AERODYNAMIC MODEL FOR THE DESIGN OF SUBSCALE TEST AIRCRAFT WITH DISTRIBUTED ELECTRICAL PROPULSION
O. Luderer, Hamburg University of Technology, Germany
  17:30 18:00 1.9.4 CONCEPTUAL DESIGN OF SILENT ELECTRIC COMMUTER AIRCRAFT
G. Atanasov, Germany
Reserve Paper 1.9.R REQUIREMENTS AND LIMITATIONS FOR GENERAL AVIATION ELECTRIC AIRPLANES
Z. Lei, Suwa University of Science, Japan
2.9UAS 2
Chair: R. Gerhards
Track 2
01 - Aircraft Design and Integrated Systems
  16:00 16:30 2.9.1 HYBRID POWER SYSTEM FOR NEW GENERATION OF VTOL UNMANNED AERIAL VEHICLES WITH A TAKE-OFF WEIGHT OF UP TO 300 KG
L. Czajkowski, ?ukasiewicz Research Network - Institute of Aviation, Poland
  16:30 17:00 2.9.2 DEVELOPMENT OF A TURN-KEY, INTEGRATED RAPID DESIGN AND MANUFACTURING ENVIRONMENT FOR SUAS
D. Verstraete, The University of Sydney, Australia
  17:00 17:30 2.9.3 DATABASE BASED MULTI-MISSION DESIGN FOR E-VTOL UAVS
T. Seren, Institute of Aircraft Design - Technical University of Munich, Germany
  17:30 18:00 2.9.4 METHODOLOGY FOR OBTAINING AN OPTIMIZED BAFFLED AIRFOIL FOR AN INFLATABLE WING
S.R.M. Mistri, Indian Institute of Technology- Bombay, India
3.9AFLoNext
Chair:
Track 3
15 - Guest lectures
  16:00 16:30 3.9.1 FLIGHT TEST OF AN ADVANCED HYBRID-LAMINAR-FLOW-CONTROL (HLFC) SYSTEM ON AN A320 VERTICAL TAIL PLANE
H. von Geyr, German Aerospace >Centre, DLR, Germany
  16:30 17:00 3.9.2 ACTIVE FLOW CONTROL (AFC) AT PYLON / WING JUNCTION OF CIVIL AIRCRAFT – A FULL-SCALE DEMONSTRATION
T. M. Gibson, Airbus Operations Limited, United Kingdom
  17:00 17:30 3.9.3 NOISE REDUCTION AT FLAP SIDE EDGE AND UNDERCARRIAGE
S Pott-Pollenske, DLR, Germany
  17:30 18:00 3.9.4 MAIN LANDING GEAR DOORS VIBRATION REDUCTION BASED ON FLIGHT TEST
R Abarca Lopez, Airbus, Spain
4.9Applied CFD 2
Chair: T. Wan
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  16:00 16:30 4.9.1 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
  16:30 17:00 4.9.2 LATTICE BOLTZMANN SIMULATIONS OF STORE SEPARATION TRAJECTORIES
G. Trapani, Dassault Systemes Spain, Spain
  17:00 17:30 4.9.3 TRAJECTORY PREDICTIONS FOR THE MK-82 STORE FROM A GENERIC CAVITY
Alex CENKO, AIWS, United States
  17:30 18:00 4.9.4 COMPUTATIONAL STUDY ON COAND? BLANKET CURVATURE EFFECTS ON HALF-SPHERICAL COAND? DEVICE PERFORMANCE
HD Djojodihardjo, Retired Professor, Indonesia
Reserve Paper 4.9.R A VALIDATION STUDY FOR EFFECT OF CAMBER IN A MULTI ELEMENT AIRFOIL IN SUBSONIC FLOW CONDITIONS
E. GULRAIZ, RCMS, NUST, Pakistan
5.9Configurations
Chair:
Track 5
03.4 - Applied Aerodynamics
  16:00 16:30 5.9.1 INTAKE BOUNDARY LAYER PROFILE ESTIMATION FOR BLI PERFORMANCE PREDICTION ON A BLENDED WING BODY
K. Ma¹, S. Prince¹; ¹Cranfield University, United Kingdom
  16:30 17:00 5.9.2 NUMERICAL STUDY OF HEAT TRANSFER ENHANCEMENT OF CONFINED JET IN AIRCRAFT ANTI-ICING CHAMBER
J.-J Niu, Northwestern Polytechnical University, China
  17:00 17:30 5.9.3 NUMERICAL INVESTIGATION ON FLOW INTERFERENCE BETWEEN BLENDED-WING-BODY AIRCRAFT AND OVERHANGING NACELLE
A.X.Q Qiu, China
  17:30 18:00 5.9.4 PRELIMINARY AERODYNAMIC DESIGN AND ANALYSIS OF TRUSS-BRACED WING REGIONAL AIRCRAFT USING HIGH-FIDELITY METHODS
S. Hosseini, Amirkabir University of Technology, Iran
Reserve Paper 5.9.R AN INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS FOR SAAB J-29 AIRCRAFT DESIGN USING HIGH FIDELITY CFD
M. Zhang, Airinnova AB, Sweden
6.9Transition Physics 2
Chair: C. Atkin
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  16:00 16:30 6.9.1 STABILIZATION OF SUPERSONIC BOUNDARY LAYERS IN THE PRESENCE OF FAVORABLE PRESSURE GRADIENT
P.V. Chuvakhov¹, A.V. Fedorov, Moscow Institute of Physics and Technology (MIPT), Russia; A.O. Obraz¹; ¹Central Aerohydrodynamic Institue (TsAGI), Russia
  16:30 17:00 6.9.2 NUMERICAL SIMULATION OF THREE-DIMENSIONAL DISTURBANCES EVOLUTION IN SUPERSONIC FLOW OVER A WAVY SURFACE
A.V. Novikov, Central Aerohydrodynamic Institute, Russia
  17:00 17:30 6.9.3 MECHANISMS OF NATURAL LAMINAR-TURBULENT TRANSITION ON AN UNSWEPT WING IN SUPERSONIC FLIGHT
P.V. Chuvakhov¹, A.V. Fedorov², A.O. Obraz¹, I.O. Pogorelov²; ¹Central Aerohydrodynamic Institue (TsAGI), Russia ;²Moscow Institute of Physics and Technology (MIPT), Russia
  17:30 18:00 6.9.4 TRIGGERING SUPERSONIC BOUNDARY-LAYER INSTABILITY BY SMALL-SCALE VORTEX SHEDDING
G. Tu, State Key Laboratory of Aerodynamics, China
7.9Performance
Chair:
Track 7
03.4 - Applied Aerodynamics
  16:00 16:30 7.9.1 GRADIENT-BASED ROBUST DESIGN OF A WING WITH 3D SHOCK CONTROL BUMPS
C. Sabater, German Aerospace Center (DLR), Germany
  16:30 17:00 7.9.2 AERODYNAMIC PERFORMANCE ANALYSIS USING AN EXERGY BALANCE METHOD
I. Petropoulos, ONERA, France
  17:00 17:30 7.9.3 DRAG REDUCTION ANALYSIS IN CLOSE-FORMATION FLIGHT
X.X. Meng, Northwestern Polytechnical University, China
  17:30 18:00 7.9.4 INCREASING THE EFFECTIVENESS OF AN AERODYNAMICALLY BALANCED CONTROL SURFACE ON A MODIFIED AIRFOIL WITH REDUCED DRAG
V.V. Bogatyrev, TsAGI, Russia
Reserve Paper 7.9.R AERODYNAMIC DESIGN AND ANALYSIS ON A NEW STEPPED WINGLET BASED ON THE DYNAMIC CHARACTERISTICS OF THE WINGTIP VORTEX
J.Jin Jin, Shanghai Aircraft Design and Research Institute,COMAC, China
8.9Testing and Measurement
Chair: C. Bisagni
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  16:00 16:30 8.9.1 RESEARCH ON ATTITUDE CONTROL AND CONSTRAINT SYSTEM DESIGN OF FULL-SCALE AIRCRAFT STATIC TEST BASED ON BARYCENTRE
JJ ZHENG, AVICASRI, China
  16:30 17:00 8.9.2 NON-CONTACT MEASUREMENT OF SURFACE DEFORMATION FIELDS BY VIDEOGRAMMETRY METHOD
K.A. Kuruliuk, Central Aerohydrodynamic Institute n. a. prof. N.E. Zhukovsky, Russia
  17:00 17:30 8.9.3 OPTIMIZATION FOR PROCESS AND MANAGEMENT IN MASSIVE STRAIN MEASUREMENT IN THE FULL SCALE AIRCRAFT STRUCTURE STRENGTH TEST
J. Zuo, Aircraft Strength Research Institute of China, China
  17:30 18:00 8.9.4 DESIGN OF A VERTICAL DITCHING TEST
E. Cestino, Politecnico di Torino, Italy
Reserve Paper 8.9.R A SUBJECTIVE EVALUATION METHOD OF AIRCRAFT VIBRATION IN FLIGHT TEST
H.G WANG, COMAC, China
9.9Advanced Manufacturing Management
Chair: S. Wang
Track 9
08 - Manufacturing and Supply Chain Management
  16:00 16:30 9.9.1 ASSESSING THE IMPACT OF PRODUCTION MODELING IN CONCEPTUAL AIRCRAFT DESIGN
J. Page Risueno, German Aerospace Center (DLR), Germany
  16:30 17:00 9.9.2 A STRUCTURED AND SCALABLE APPROACH FOR THE DEFINITION OF DEEP LEARNING ARCHITECTURES FOR BEARING ANOMALY DETECTION
O Pinon Fischer, Georgia Institute of Technology, United States
  17:00 17:30 9.9.3 INCORPORTING KNOWLEDGE COVERAGE MEASUREMENT INTO KNOWLEDGE TRANSFORMATION FROM DATA FOR KNOWLEDGE ACCUMULATION
Y.-B. Fan, NanChang HangKong University, China
  17:30 18:00 9.9.4 DESIGN AND BEST PRACTICES OF SUPPLIER PERFORMANCE EVALUATION IN SUPPLY CHAIN
HZ-L Li, AECC SHANGHAI COMMERCIAL AIRCRAFT ENGINE MANUFACTURING CO.,LTD., China
10.9Fault Detection
Chair: Y. Wang
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  16:00 16:30 10.9.1 AIRCRAFT BRAKING DYNAMICS AND BRAKE SYSTEM MODELING FOR FAULT DETECTION AND ISOLATION
L.C.N. Cardoso Navarro, ITA, Brazil
  16:30 17:00 10.9.2 FLIGHT SIMULATOR EVALUATION OF SIMPLE ADAPTIVE CONTROL FOR LOSS-OF-CONTROL RECOVERY
R. T. Takase, The University of Tokyo, Japan
  17:00 17:30 10.9.3 TWO-LAYER ADAPTIVE AUGMENTATION FOR INCREMENTAL BACKSTEPPING FLIGHT CONTROL OF AIRCRAFT IN FAILURE CONDITIONS
D. Ignatyev, Cranfield University, United Kingdom
  17:30 18:00 10.9.4 FEEDBACK ERROR LEARNING WITH ENHANCED SAMPLING: NEURAL FAULT TOLERANT CONTROL OF AIRCRAFT
N. Yoshikawa, University of Tokyo, Japan
11.9Aspects of Landing Gear Design
Chair: P. Krus
Track 11
07 - Systems, Subsystems and Equipment
  16:00 16:30 11.9.1 IMPROVED DESIGN OF AIRCRAFT NOSEWHEEL STEERING SYSTEM
L.-X. Xin, FAI AVIC, China
  16:30 17:00 11.9.2 NEW SOLUTION OF A DAMPER WITH A MAGNETORHEOLOGICAL ELASTOMER
P. Skalski, Institute of Aviation, Poland
  17:00 17:30 11.9.3 INVESTIGATIONS ON LANDING GEAR SHOCK ABSORBER ACTIVE FORCE CONTROL
Z. Skorupka, ?ukasiewicz Research Network - Institute of Aviation, Poland
  17:30 18:00 11.9.4 A STOCHASTIC ROBUSTNESS VERIFICATION OF NLG SIMPLE ADAPTIVE SHIMMY SUPPRESSION SYSTEM
C. Orlando, Italy
Reserve Paper 11.9.R A NOVEL OF CONTROL METHOD BASED ON PWM FOR HIGH_SPEED ON/OFF VALVES ARRAY OF AIRCRAFT BRAKE SYSTEMS
Renjie Li Li, Beihang unversity, China
12.9Airport/Aircraft Operation
Chair: E. Itoh
Track 12
09 - Air Transport System Efficiency
  16:00 16:30 12.9.1 INTEGRATION AND EVALUATION OF AN AIRCRAFT TAXIING SOLUTION USING AUTONOMOUS TOW TRUCKS
J Gauci, University of Malta, Malta
  16:30 17:00 12.9.2 ERAS - EVALUATION OF REALISTIC APPROACH SCENARIOS FOR MINIMAL NOISE - PRELIMINARY FINDINGS
B Moberg, Vernamack AB, Sweden
  17:00 17:30 12.9.3 DESIGN AND TRIALING OF A CONCEPT OF OPERATIONS (CONOPS) FOR OPTIMAL CLIMBS AND DESCENTS INTO MEDIUM DENSITY AIRFIELDS
D. Zammit-Mangion, University of Malta, Malta
  17:30 18:00 12.9.4 A NOVEL APPROACH FOR TURNAROUND TIME ALLOCATION BASED ON REINFORCEMENT LEARNING
A. Rodriguez-Sanz, Universidad Politecnica de Madrid (UPM), Spain
Reserve Paper 12.9.R OPERATION PLANNING AIDED METHOD OF GENERAL AIRCRAFT BASED ON MULTI-CBR AND COMBINATION EVALUATION METHOD
R.-X. Xie, Beihang University, China
13.9Failure And Fracture Mechanics
Chair: M. Liao
Track 13
04.1 - Material Issues, Fatigue and Damage Tolerance
  16:00 16:30 13.9.1 FAILURE PROCESS IDENTIFICATION OF C-SIC WITH DIFFERENT TENSILE PERFORMANCE
Y.Z. Zhang, Northwestern Polytechnical University, China
  16:30 17:00 13.9.2 INVESTIGATION OF STOPPER STRAPS EFFECTS ON LONGITUDINAL CRACK GROWTH RATES IN A SKIN OF PRESSURIZED AIRCRAFT FUSELAGE
A.S. Kim, TsAGI, Russia
  17:00 17:30 13.9.3 INFLUENCE OF NOTCH EFFECTS ON STATIC CHARACTERISTICS OF STEEL BASED ON THERMOGRAPHIC METHOD
Junling Fan¹, Pengfei Yang¹, Shaozheng Zhan¹; ¹Aircraft Strength Research Institute, China
  17:30 18:00 13.9.4 EXPERIMENTAL INVESTIGATION AND NUMERICAL SIMULATION OF SINGLE LAP JOINTS OF ALLOY-ARAMID FIBER COMPOSITE BASED ON COHESI
ZTC Zou, Civil Aviation University of China, China
Reserve Paper 13.9.R EXPERIMENTAL INVESTIGATION AND LIFE PREDICTION FOR DEFECT INDUCED CRACK OF A P/M NICKEL BASED SUPERALLOY
SHI Y. SHI, Beihang University, China
1.10MDO
Chair: S. Bagassi
Track 1
01 - Aircraft Design and Integrated Systems
  10:00 10:30 1.10.1 COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN
S. Görtz, DLR - German Aerospace Center, Germany
  10:30 11:00 1.10.2 ASSESSMENT OF NEW TECHNOLOGIES IN A MDAO ENVIRONMENT INCLUDING RAMS AND COST DISCIPLINES
M. Fioriti, Politecnico di Torino, Italy
  11:00 11:30 1.10.3 INTERACTIONS BETWEEN MULTIFUNCTIONAL FLIGHT CONTROL SYSTEMS AND HIGH ASPECT RATIO WINGS IN A MID-RANGE AIRCRAFT
O.B. Bertram, German Aerospace Center DLR, Germany
  11:30 12:00 1.10.4 MDAX: AGILE GENERATION OF COLLABORATIVE MDO WORKFLOWS
A. Makus, German Aerospace Center (DLR), Germany
  12:00 12:30 1.10.5 BLENDED WING BODY PLANFORM MULTIDSCIPLIANRY OPTIMISATION
Davide DI Pasquale¹, Divyam Verma¹, Giampaolo Pagliuca¹; ¹Cranfield University, United Kingdom
2.10China Aviation
Chair:
Track 2
12 - Host nation
3.10Transition
Chair: L. Alves
Track 3
03.1 - Aerodynamics - CFD Methods and Validation
  10:00 10:30 3.10.1 TRANSITION PREDICTION FOR TRANSPORT AIRCRAFT CONFIGURATIONS BASED ON OVERSET GRID
Y.-M. Du, Northwestern Polytechnical University, China
  10:30 11:00 3.10.2 A CONTRIBUTION TO THE SIMULATION OF TRANSITIONAL FLOWS OVER AEROSPACE CONFIGURATIONS
J. L. F. Azevedo, Instituto de Aeronautica e Espaco, Brazil
  11:00 11:30 3.10.3 AERODYNAMICS CHARACTERISTICS STUDY ON A NATURE LAMINAR FLOW AIRFOIL OF NEAR-SPACE VEHICLE AT LOW REYNOLDS NUMBERS
C.F. FEI, Innovation & Research Institute of HIWING Technology Academy, China
  11:30 12:00 3.10.4 EFFECT OF THE WALL PROPERTIES ON THE SHOCK WAVE / LAMINAR BOUNDARY LAYER INTERACTION
A. Kutepova, Khristianovich Institute of Theoretical and Applied Mechanics, Russia
  12:00 12:30 3.10.5 TURBOFAN NACELLE DESIGN WITH TAKING INTO ACCOUNT LAMINAR-TURBULENT TRANSITION
A. A. Savelyev, Central Aerohydrodynamic Institute, Russia
Reserve Paper 3.10.R HYBRID NUMERICAL SCHEMES IN PREDICTION OF HIGH-SPEED LAMINAR-TURBULENT TRANSITION
I. Egorov, TsAGI, Russia
4.10Numerical Methods 1
Chair: A. Viviani
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  10:00 10:30 4.10.1 MODELING AND SIMULATION OF DUSTY GAS FLOW IN AERODYNAMICS
Yu. Tsirkunov, Baltic State Tech U, Russia
  10:30 11:00 4.10.2 STUDY ON AN IMPROVED PRECONDITIONING METHOD FOR MIXED COMPRESSIBLE AND INCOMPRESSIBLE FLOW
L-H Huan, China Aerodynamics Research and Development Center, China
  11:00 11:30 4.10.3 STUDY OF UNSTEADY NUMERICAL SIMULATIONS BASED ON UNSTRUCTURED MESH DEFORMATION TECHNIQUE
H.-Y. Liu, China
  11:30 12:00 4.10.4 2D INCOMPRESSIBLE FLOW SOLVER IN VELOCITY-VORTICITY FORMULATION USING DC-PSE OPERATOR DISCRETIZATION
L. R. Zuhal, Institut Teknologi Bandung, Indonesia
  12:00 12:30 4.10.5 A HYBRID CFD METHOD FOR HELICOPTER ROTOR NOISE PREDICTION BASED ON KIRCHHOFF-FFOWCS WILLIAMS/HAWKING FORMULATION
J.-B. Fu, Politecnico di Milano, Italy
Reserve Paper 4.10.R ON THE POSSIBILITY OF APPLYING THE HYPERSONIC SMALL-DISTURBANCE THEORY IN AERODYNAMIC STUDIES OF HIGH-SPEED AIRCRAFT
A.A. Gubanov, Central Aerohydrodynamic Institute n.a. Prof. N.E. Zhukovsky, Russia
5.10Impact
Chair: J. Han
Track 5
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  10:00 10:30 5.10.1 BIRD STRIKE SIMULATIONS IN MSC.SOFTWARE: CORRELATION BETWEEN THE EXPERIMENTS AND SIMULATIONS
V. Symonov¹, J. Juracka¹; ¹Brno University of Technology, Czech Republic
  10:30 11:00 5.10.2 MODELS AND METHODS FOR DRONE STRIKE LOAD PREDICTIONS
F. F. Franke, Technische Hochschule Ingolstadt, Germany
  11:00 11:30 5.10.3 EXPERIMENTAL STUDY ON ATTENUATION PERFORMANCE OF SHOCK ABSORBING INSERT
H.-S Park, South Korea
  11:30 12:00 5.10.4 MULTISCALE ANALYSIS OF BALLISTIC IMPACT OF WOVEN COMPOSITE MATERIALS
D SONG, China
  12:00 12:30 5.10.5 DEVELOPMENT OF A PREDICTIVE METHODOLOGY FOR FAST ESTIMATION OF IMPACT BEHAVIOR IN AEROSPACE GRADE COMPOSITES
K Carpenter, United States
6.10Student Final
Chair: K. Rein Weston
Track 6
15 - Guest lectures
7.10Laminar Flow
Chair:
Track 7
03.4 - Applied Aerodynamics
  10:00 10:30 7.10.1 BLADE - NATURAL LAMINAR FLOW FLIGHT TESTING
T. Gibson, Airbus, United Kingdom
  10:30 11:00 7.10.2 METODICAL STUDIES OF THE POSSIBILITY TO APPLY A NUMERICAL METHOD WITH BUILT-IN EMPIRICAL CRITERIA FOR DETERMINING THE LA
N.V. Voevodenko, TsAGI, Russia
  11:00 11:30 7.10.3 NATURAL-LAMINAR-FLOW AIRFOIL DESIGN OPTIMIZATION CONSIDERING CROSSFLOW INSTABILITY
Z.-M Xu, Northwestern Polytechnical University, China
  11:30 12:00 7.10.4 DESIGN OF TRANSONIC NATURAL LAMINAR FLOW NACELLE
C.Y. Yan, Tsinghua University, China
  12:00 12:30 7.10.5 THE NUMERICAL AND EXPERIMENTAL STUDIES ON LAMINAR WING SHORT RANGE AIRCRAFT WITH REDUCED COMMUNITY NOISE
A.L. Bolsunovsky, Central Aerohydrodynamic Institute n.a. prof. N.E.Zhukovsky (TsA, Russia
8.10Failure Analysis and Fatigue
Chair: V. Symonov
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  10:00 10:30 8.10.1 METHODS TO CALCULATE THE STRUCTURE FATIGUE DAMAGE UNDER VARIOUS SPECTRA OF VIBRO-ACOUSTIC LOADS
I.S. Sidorov, TsAGI, Russia
  10:30 11:00 8.10.2 FAILURE PROPERTIES AND MACROSCOPIC MODELLING OF AERONAUTIC RIVETED CONNECTIONS
ZY Yifan, Civil Aviation University of China, China
  11:00 11:30 8.10.3 ITERATIVE GLOBAL/LOCAL NON-INTRUSIVE MODEL COUPLING METHOD FOR STRUCTURE FAILURE ANALYSIS
Y.J. LIU, AVIC the first aircraft institute, China
  11:30 12:00 8.10.4 NUMERICAL ANALYSIS AND COMPARISON WITH RESULTS OF FRACTURE TESTS OF LUG MANUFACTURED IN COMPOSITE MATERIAL
G. C. Fonseca, Embraer - Minas Gerais, Brazil
  12:00 12:30 8.10.5 EFFECT OF CENTER HOLE ON SHEAR STABILITY AND BEARING CAPACITY OF SHEET METAL FORMING PLATE
W.L. LI, AVIC Shengyang Aircraft Design & Research Institute, China
9.10Combustion & Heat Transfer
Chair: P. Steczycki
Track 9
05 - Propulsion
  10:00 10:30 9.10.1 STUDY ON OPTIMIZATION OF SPRAY CONE ANGLE OF THE COMBINED ATOMIZER BY SIMULATION AND EXPERIMENT
C. Q. Cheng Cheng, Beijing Precision Engineering Institute For Aircraft Industr, China
  10:30 11:00 9.10.2 INVESTIGATION OF MEASUREMENT CHARACTERISTICS OF PROPAGATING FLAME BY MULTIPLE-ION-PROBE METHOD
T.Y. Yatsufusa, Hiroshima Institute of Technology, Japan
  11:00 11:30 9.10.3 STUDY ON THE INFLUENCE OF A NEW GLIDING ARC PLASMA ACTUATOR ON THE PERFORMANCE IN AN AERO-ENGINE COMBUSTION CHAMBER
Y CHEN, Air Force Engineering University, China
  11:30 12:00 9.10.4 METHODS OF CHOOSING THE PARAMETERS AND DESIGN OF THE HEAT EXCHANGERS OF AVIATION GAS TURBINE ENGINES (GTE)
A. Revanth Reddy, Moscow Aviation Institute (National Research University), Russia
  12:00 12:30 9.10.5 HYBRID KERNEL FORMATION AND TRACKING METHOD TO PREDICT IGNITION LIMITS ON LOW EMISSION COMBUSTORS
X.Wei Xiao, AECC Hunan Aviation Powerplant Research Institute, China
Reserve Paper 9.10.R DECISION PROBLEMS IN AN IDENTIFICATION OF FACTORS INFLUENCING ON THE EMISSION OF HARMFUL COMPOUNDS OF TRANSPORT MEANS
M. JACYNA, Warsaw University of Technology, Poland
10.10Nonlinear Control
Chair: T. Rogalski
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  10:00 10:30 10.10.1 NONLINEAR CONTROL STRATEGY FOR QUAD-TILTROTOR IN TRANSITION MODE
K.W. Jang, KAIST, South Korea
  10:30 11:00 10.10.2 NONLINEAR FAULT-TOLERANT FLIGHT CONTROL WITH CONTROL ALLOCATION OF NASA GTM T-2 MODEL WITH DIFFERENT DAMAGE SCENARIOS
B. Ergocmen, Middle East Technical University, Turkey
  11:00 11:30 10.10.3 MACHINE LEARNING TECHNIQUES FOR AIRCRAFT STALL DETECTION AND RECOVERY
J Gauci, University of Malta, Malta
  11:30 12:00 10.10.4 AIRCRAFT AUTOPILOT DESIGN USING ASYMMETRIC VARIABLE-SPAN WING MORPHING
J. Lee, Seoul National University, South Korea
  12:00 12:30 10.10.5 AUTONOMOUS FLIGHT CONTROL BASED ON NEURAL NETWORKS AND FUZZY DECISION
P.C. Wen, AVIC Xi’an Aeronautics Computing Technique Research Institute, China
Reserve Paper 10.10.R ANALYSIS OF REENTRY TRAJECTORY OPTIMIZATION OF COMPLEX PATH CONSTRAINTS USING HERMIT SPLINE INTERPOLATION
Y Kwak, Konkuk Univ., South Korea
11.10Aspects of More electric Aircraft
Chair: M. Peters
Track 11
07 - Systems, Subsystems and Equipment
  10:00 10:30 11.10.1 OPTIMALPOWER DISTRIBUTION ON A MORE ELECTRIC AIRCRAFT
E. D'Amato, Università degli studi della Campania "Luigi Vanvitelli", Italy
  10:30 11:00 11.10.2 CONCEPTUAL SYSTEM-LEVEL MODELING OF CONVENTIONAL AND MEA SYSTEMS ARCHITECTURES FOR MODERN MIDRANGE TRANSPORT AIRCRAFT
M. Jünemann, Hamburg University of Technology, Germany
  11:00 11:30 11.10.3 ICE THICKNESS IMPACT AND DETECTION IN RESONANT ELECTROMECHANICAL DEICING SYSTEMS
M. Budinger, INSA Toulouse, France
  11:30 12:00 11.10.4 ANTI-PUMP-FORCE-FIGHT PRESSURE CONTROLLER FOR A REDUNDANT HYDRAULIC POWER PACKAGE WITH SPEED VARIABLE AC MOTOR PUMPS
N. Trochelmann, TUHH/ Institute of Aircraft Systems Engineering, Germany
  12:00 12:30 11.10.5 ON-BOARD SYSTEM ARCHITECTURES FOR HYBRID/ALL-ELECTRIC REGIONAL AIRCRAFT
M. Fioriti, Politecnico di Torino, Italy
Reserve Paper 11.10.R SURROGATE MODELS OF PM BRUSHLESS MOTORS FOR THE PRELIMINARY DESIGN OF AIRCRAFT APPLICATION SYSTEMS
F De Giorgi, INSA/ICA Toulouse, France
12.10UAV Navigation
Chair: M. Logan
Track 12
06.2 - Flight Dynamics and Control (UAV related)
  10:00 10:30 12.10.1 MISSION CONTROL WITH REAL-TIME FLIGHT PATH PLANNING FOR TILTWING UAVS TO SUPPORT RESCUE OPERATIONS
I. Barz, Institute of Flight System Dynamics, RWTH Aachen University, Germany
  10:30 11:00 12.10.2 PATH PLANNING OF UNINHABITED AERIAL VEHICLE BASED A MODIFIED ANT ALGORITHM
Y.-F Feng, China
  11:00 11:30 12.10.3 CONFLICT RESOLUTION ADVISORIES BY UAS TRAFFIC MANAGEMENT SYSTEMS
P. Hartmann, RWTH Aachen University, Germany
  11:30 12:00 12.10.4 TEMPLATE MATCHING BASED ON SEGMENTED AERIAL IMAGES FOR VISION-AIDED NAVIGATION
K Hong, South Korea
  12:00 12:30 12.10.5 TERRAIN INFORMATION MEASURE FOR VISION-BASED MAP-REFERENCED NAVIGATION
S. Kim, Korea Advanced Institute of Science and Technology, South Korea
Reserve Paper 12.10.R 3D TRAJECTORY DESIGN AND TRACKING FOR MULTIROTOR UAVS INDOOR FLIGHT
E. Capello, Italy
13.10Airworthiness & Certification
Chair:
Track 13
10 - Safety and Security
  10:00 10:30 13.10.1 CERTIFICATION CONSIDERATIONS FOR EVTOL AIRCRAFT
Yingkang MOU¹, Mei JIANG¹; ¹Nanjing Engineering Institute of Aircraft Systems, China
  10:30 11:00 13.10.2 APPLICATION OF DEVELOPMENT ASSURANCE METHODOLOGIES TO ELECTRONIC ENGINE CONTROL SYSTEM (EECS)
Q ZHU, AECC COMMERCIAL AIRCRAFT ENGINE CO., LTD., China
  11:00 11:30 13.10.3 RESEARCH ON AIRWOTHINESS CERTIFICATION OF CIVIL AVIATION PRODCUTS BASED ON RISK ANALYSIS
C.-X Wang, AECC COMMERCIAL AIRCRAFT ENGINE CO., LTD, China
  11:30 12:00 13.10.4 STUDY ON THE AIRWORTHINESS AND COMFORTABLENESS REQUIREMENTS OF AIRCRAFT CABIN AIR CONTAMINATIONS
Hu Tao Tao, CAPE?CAPE?, China
  12:00 12:30 13.10.5 CRASHWORTHINESS EVALUATION OF AIRCRAFT FUSELAGE BASED ON BUILDING BLOCK APPROACH
C.-K Kun, Civil Aviation University of China, China
Reserve Paper 13.10.R RESEARCH ON THE TRIGGERING CONDITIIONS OF EJECTABLE RECORDER FOR CIVIL AIRCRAFT
Shumin Pu, Northwestern Polytechnical University, China
1.11Hybrid/Electric & Unconventional Aircraft 4
Chair: J. Melkert
Track 1
01 - Aircraft Design and Integrated Systems
  14:00 14:30 1.11.1 STUDY OF THE BENEFITS OF A SEMI-MORPHING WING CONCEPT
L. P. Ruiz Calavera, Airbus Defence & Space, Spain
  14:30 15:00 1.11.2 FLIGHT EXPERIMENTS FOR THE ALTAIR SEMI-REUSABLE AIR-LAUNCH SYSTEM WITH THE DEMONSTRATOR EOLE
J. Gauvrit-Ledogar, ONERA, France
  15:00 15:30 1.11.3 CIRCULATION CONTROL AIRCRAFT: RECENT DEVELOPMENTS OF THE CHANNEL-WING DESIGN
HD Djojodihardjo, Retired Professor, Indonesia
2.11tbd4
Chair:
Track 2
3.11Compressor and Fan Aerodynamics
Chair: T. Wan
Track 3
03.1 - Aerodynamics - CFD Methods and Validation
  14:00 14:30 3.11.1 APPLICATION OF A SKEWED SLOT CASING TREATMENT IN A HIGH-LOADING AXIAL-CENTRIFUGAL COMPRESSOR
H. L. JIN, China
  14:30 15:00 3.11.2 DISTORTION PLATE DESIGN, SIMULATION VALIDATION AND TEST SCHEME FOR STABILITY ANALYSIS ON A FAN COMPONENT OF AEROENGINE
ZP.-L Li, AECC Shenyang Engine Design Institute, China
  15:00 15:30 3.11.3 EFFECT OF INTER-STAGE BLEEDING ON FLOW STABILITY OF A MULTI-STAGE COMPRESSOR
X. W. LIU, China
Reserve Paper 3.11.R DESIGN AND TEST OF A HIGH SLOPE ANGLE INTERMEDIATE DUCT BETWEEN AN AXIAL-CENTRIFUGAL LOW PRESSURE AND HIGH PRESSURE COMP
H. L. JIN, China
4.11Numerical Methods 3
Chair: A. Viviani
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  14:00 14:30 4.11.1 AERODYNAMIC AND AEROACOUSTIC INVESTIGATION OF THE FLOW PAST THE 30P30N HIGH-LIFT MULTI-AIRFOIL
Yao Jin Jin, China
  14:30 15:00 4.11.2 AN INTELLIGENT STRUCTURED CHIMERA GRID APPROACH FOR MOVING OBJECTIVES
L. L. Li, AVIC Aeronautics Computing Technique Research Institute, China
  15:00 15:30 4.11.3 SUN CODE: AN AUTOMATIC AND FAST FLOW SIMULATION TOOL FOR AIRCRAFT AERODYNAMIC DESIGN
Mingzhe Sun¹, Rongting Lin¹, Dongrun Wu¹, Jender Lee¹, Xi Du¹, Dakai Lin¹; ¹COMAC BATRI, China
Reserve Paper 4.11.R INVESTIGATION OF NUMERICAL METHOD OF INTERNAL FLOW AND OIL CAPTURE EFFICIENCY OF UNDER-RACE LUBRICATION
J.-L. Jiang, Northwestern Polytechnical University, China
5.11UAV Flight Testing
Chair: K.C. Wong
Track 5
06.2 - Flight Dynamics and Control (UAV related)
  14:00 14:30 5.11.1 VALIDATION OF SCALED FLIGHT TESTING - OVERALL APPROACH AND FIRST RESULTS
P. Schmollgruber, France
  14:30 15:00 5.11.2 COMPARISON OF ESTIMATED AND ACTUAL AERODYNAMIC PERFORMANCE OF A 65KG UAV
J. Bartasevicius, Technical University of Munich, Germany
  15:00 15:30 5.11.3 BIO-INSPIRED SWARM CONTROL OF DRONES USING SIMPLE INTERACTION RULES
J Kikuchi, Graduate School of Tokai University, Japan
Reserve Paper 5.11.R THE STUDY OF UNMANNED AERIAL VEHICLE FLYING QUALITIES FLIGHT TEST METHOD BASED ON TIME-DELAY EVALUATION
S.J.-Q. QI, Chinese Flight Test Establishment , China
6.11System Qualification
Chair: J. Fu
Track 6
07 - Systems, Subsystems and Equipment
  14:00 14:30 6.11.1 RESEARCH ON CIVIL AIRCRAFT EQUIPMENT QUALIFICATION TEST
G.-C Zhang, Shanghai Aircraft Design and Research Institute, China
  14:30 15:00 6.11.2 KNOWLEDGE-BASED ENGINEERING FOR MODELLING AIRCRAFT THERMAL BEHAVIOUR
A.S.J. van Heerden, Cranfield University, United Kingdom
  15:00 15:30 6.11.3 EXPERIMENTAL STUDY OF A LOOP HEAT PIPE FOR COOLING AIRCRAFT NACELLE ENGINE EQUIPEMENT
V. Ayel, ISAE-ENSMA, France
Reserve Paper 6.11.R RESEARCH ON THE ENVIRONMENTAL WORTHINESS OF THE CIVIL AIRCRAFT USING THE FUZZY THEORY WITH THE TEST RESULT
Z-H hui, Aircraft Strength Institute Research, China
7.11Stability
Chair:
Track 7
03.4 - Applied Aerodynamics
  14:00 14:30 7.11.1 NUMERICAL EVALUATION OF DYNAMIC STABILITY DERIVATIVES FOR HIGH LIFT DEVICES
N/A Maqsood, Pakistan
  14:30 15:00 7.11.2 THE AERODYNAMIC OPTIMIZATION AND TRIM CHARACTERISTICS RESEARCH ON VARIABLE CAMBER WING OF WIDEBODY CIVIL TRANSPORT
Cheng Su¹, Xuan Hao¹, Bin Wang¹, Qingqing Zhang¹; ¹China Academy of Aerospace Aerodynamics, China
  15:00 15:30 7.11.3 EFFECT OF CANARD DEFLECTION ON MAIN WING FOR A CLOSE-COUPLED-CANARD CONFIGURATION DURING PITCHING OSCILLATIONS
Q. Chen, Beihang University, China
Reserve Paper 7.11.R DESIGN OF VORTEX GENERATORS OF HYBRID SIZES OF AN AIRCRAFT HORIZONTAL TAIL
Y. Liu¹, L. Ping¹, R. Zeng¹; ¹CETC Wuhu Diamond Aircraft Manufacture co., LTD, China
8.11Static Analysis of Aircraft Structures
Chair: J. Zheng
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  14:00 14:30 8.11.1 MULTIDIMENSIONAL FINITE ELEMENT MODELS FOR ADVANCED HELICOPTER BLADES
M. Filippi, Politecnico di Torino, Italy
  14:30 15:00 8.11.2 MATHEMATICAL MODELS FOR OPTIMIZATION OF AIRCRAFT STRUCTURES TAKING INTO CONSIDERATION OF LOCAL STRESS DISTRIBUTION
S. A. Tuktarov, Central aerohydrodynamic institute, Russia
  15:00 15:30 8.11.3 THE BEAM MODEL OF A HAWKMOTH WING STRUCTURE
A. T. Nguyen, Le Quy Don Technical University, Vietnam
Reserve Paper 8.11.R INVESTIGATION ON PERFORMANCE OF PCM-BASED ORTHOTROPIC COOLING PLATE FOR THERMAL MANAGEMENT OF AVIONICS MODULE.
B. Wu, Aeronautical Computing Technique Research Institute, China
9.11ISABE 2
Chair:
Track 9
15 - Guest lectures
  14:00 14:30 9.11.1 KEY TECHNOLOGIES FOR THE NEXT GENERATION OF CIVIL AIRCRAFT ENGINES
F. Haselbach, United Kingdom
  14:30 15:00 9.11.2 DESIGN AND PERFORMANCE OF A LOW FAN-PRESSURE-RATIO PROPULSION SYSTEM
R. Schnell, German Aerospace Center (DLR), Germany; E. Goldhahn, Airbus Operations GmbH, Germany; M. Julian, Airbus Operations SAS, France
  15:00 15:30 9.11.3 AN EXPERIMENTAL-NUMERICAL METHOD FOR TRANSIENT INFRARED MEASUREMENT OF FILM COOLING EFFECTIVENESS
N.E. Holgate, United Kingdom
10.11Helicopter Control
Chair: J. Che
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  14:00 14:30 10.11.1 MODELING OF HELICOPTER FLIGHT DYNAMICS AND ROTOR BLADES LOADS DURING EXTREME FLIGHTS
Grzegorz Kowalec Kowaleczko, Air Force Institute of Technology, Poland
  14:30 15:00 10.11.2 DESIGN TECHNIQUE OF INTEGRAL ALGORITHMS FOR HELICOPTER FBW CONTROL SYSTEM
V.M. Kuvshinov, Central Aero-Hydrodynamics Institute, Russia
  15:00 15:30 10.11.3 AERODYNAMIC PERFORMANCE CALCULATION OF XH-59A HELICOPTER IN MANEUVERING PROCESS
K. Y. You, Northwestern Polytechnical University, China
11.11Vehicle Mangement Systems
Chair: P. Krus
Track 11
07 - Systems, Subsystems and Equipment
  14:00 14:30 11.11.1 EVALUATION OF A GESTURE-BASED PILOT-AIRCRAFT INTERFACE IN A SIMULATION ENVIRONMENT
M.A. Rodriguez Diaz, Instituto Tecnologico de Aeronáutica, Brazil
  14:30 15:00 11.11.2 ANALYSIS AND SOLUTION RESEARCH OF THE AIR DATA LOSS FROM AIRCRAFT FOR ENGINE CONTROL
J LI, COMAC, China
  15:00 15:30 11.11.3 REAL-TIME GNSS PRECISE POINT POSITIONING AND VISUAL-INERTIAL ODOMETRY COUPLED NAVIGATION SYSTEM FOR UAVS
C.-C. Cheng, SJTU, China
Reserve Paper 11.11.R DESIGN OF UAV NAVIGATION ALGORITHM IN SINGLE SATELLITE ENVIRONMENT BASED ON HIGH PRECISION TIMING
L.KT Li, China National Aeronautical Radio Electronics Research Institute, China
12.11UTM/On-Demand Mobility
Chair:
Track 12
09 - Air Transport System Efficiency
  14:00 14:30 12.11.1 AIRLINE NETWORK-AIRPLANE INTEGRATED OPTIMIZATION CONSIDERING MANUFACTURER\'S PROGRAM COST
Mattos, B. S. Mattos, Instituto Tecnologico de Aeronautica (ITA), Brazil
  14:30 15:00 12.11.2 ANALYSIS AND EVALUATION OF AN URBAN AIR TRAFFIC NETWORK BASED ON OPERATIONAL PERFORMANCE PARAMETERS
M. Husemann, Institute of Aerospace Systems, Germany
  15:00 15:30 12.11.3 ON-DEMAND AIR MOBILITY FOR BEIJING: PREREQUISITES FOR COMPETITIVENESS
X. Sun, Beihang University, China
Reserve Paper 12.11.R AIR TRAFFIC MANAGEMENT OF DRONES INTEGRATED INTO SMART CITIES
D. Rohacs, B udapest University of Tech. and econ.;, Hungary
13.11Operational Training
Chair: D. Holmes
Track 13
11 - Operations and Sustainment
  14:00 14:30 13.11.1 DESIGN OF SIMULATION-BASED PILOT TRAINING SYSTEMS USING MACHINE LEARNING AGENTS
J. Källström¹, R. Granlund, RISE SICS East, Sweden; F. Heintz¹; ¹Linköping University, Sweden
  14:30 15:00 13.11.2 A STUDY ON TRAINING NEEDS ANALYSIS (TNA) METHOD FOR MILITARY AIRCRAFT
Q WANG, Chengdu Aircraft Design and Research Institute, AVIC, China
  15:00 15:30 13.11.3 COMPARISON OF READINESS TO PERFORM THE TASK OF AIRCRAFT USED FOR CADET TRAINING
J. Tomaszewska, Polish Air Force University, Poland
Reserve Paper 13.11.R INFORMATION DISTRIBUTION METHOD FOR MULTI-AIRCRAFT COOPERATION BASED ON COLLABORATIVE FILTERING ALGORITHM
Y Wang, AVIC, China