Outline Technical Programme - 29th ICAS Congress 2014 - St. Petersburg, Russia

Monday, 08. September 2014
08:00
09:00
Registration
09:00
09:45
Opening Session
09:45
10:30
ICAS Daniel & Florence Guggenheim Memorial Lecture
Prof. Sergey Chernyshev, TsAGI, Russia, Aeronautics Challenges and New Opportunities for International Cooperation
10:30
10:50
Break
10:50
12:20
1.1
Design for flow control
2.1
Aerodynamic optimization 1
3.1
Wind tunnel techniques
4.1
Unsteady aerodynamics
5.1
Metal composite
6.1
Experimental method
7.1
Compressor
8.1
Handling quality
9.1
UAV design and testing 1
10.1
Optimization of trajectories
11.1
Air transport system
12.1
Advanced engines
12:20
13:10
Lunch
13:10
14:40
1.2
Design for uncertainty
2.2
Aerodynamic optimization 2
3.2
New analysis / phenomena 1
4.2
Propulsion
5.2
Deformation and damage of composites
6.2
Impact
7.2
RAM / SCRAMjet 1 and supersonic engines
8.2
Operations in turbulence
9.2
UAV design and testing 2
10.2
Innovative concepts (systems)
11.2
Airport
12.2
Innovative engines 1
14:40
15:00
Break
15:00
17:00
1.3
Design methods 1
2.3
CFD applied to design
3.3
High speed flow studies
4.3
Flapping wing
5.3
Separation / lift control
6.3
Dynamic load 1
7.3
RAM / SCRAMjet 2
8.3
Flight dynamic system identification 1
9.3
Flapping wing UAV
10.3
Avionics
11.3
Arrival management
12.3
Innovative engines 2
Tuesday, 09. September 2014
08:00
09:00
General Lecture 1
Ric Parker, Rolls Royce, UK, Vladimir Babkin, CIAM, Russia, Challenges of Advanced Propulsion Systems Development for Future Civil Air Transport
09:00
10:00
Poster presentation
10:00
12:00
1.4
Design methods 2
2.4
UAV applications
3.4
Flow control studies
4.4
Transsonic aerodynamics
5.4
Turbine materials
6.4
Structural design 1
7.4
Turbines 1
8.4
Flight modelling and simulation 1
9.4
Novel fuel / usage and operation
10.4
Navigation and radar 1
11.4
Weather / Wake Vortex
12.4
Engine materials
12:00
13:00
Lunch
13:00
13:45
ICAS Nikolai Zhukovsky Lecture for innovations in aeronautics
Michimasa Fujino, Honda Aircraft Company, Inc. USA, Innovation in Aircraft Design for the HondaJet: Development of Advanced Technologies Including the Unique Over-the-Wing Engine Mount Configuration
14:00
15:30
1.5
Hypersonic vehicles
2.5
Flows with strong Vortex effects
3.5
Low Reynolds number flow studies
4.5
Icing
5.5
CFRP
6.5
Structural design 2
7.5
Nacelles
8.5
Flight modelling and simulation 2
9.5
Aircraft emission and contrails
10.5
Navigation and radar 2
11.5
Hypersonic flow applications
12.5
Engine performance
15:30
16:00
Break
16:00
18:00
1.6
Supersonic vehicles
2.6
Comparison of CFD with experiments
3.6
Supersonic flow control
4.6
Flight vehicle aerodynamics 1
5.6
Fatigue and failure
6.6
Structural analysis 1
7.6
Turbines 2
8.6
Flight control 1
9.6
Novel fuels - emissions
10.6
Requirements and specifications
11.6
Human factors
12.6
Combustor
18:00
19:30
Airbus Fly Your Ideas Student Event
Wednesday, 10. September 2014
08:00
09:00
General Lecture 2
Michael K. Sinnett, Boeing, USA, Eric Bachelet, SAFRAN, France, Pushing the boundaries – The Challenges of New Airplane Design New Future Systems for Aircraft
09:00
09:30
Break
09:30
12:00
1.7
Innovative concepts 1
2.7
Algorithm development
3.7
Boundary layer transition studies
4.7
Hypersonics
5.7
Materials
6.7
Aeroelasticity 1
7.7
Open rotor 1
8.7
Flight control 2
9.7
Multi UAV operations
10.7
Actuations and landing gear
11.7
ATM
12.7
History of aeronautics
12:00
13:00
Lunch
13:00
13:45
General Lecture 3
Fayette Collier,NASA, USA, Jean Botti, Airbus Group,, NASA‘s New Ideas for Greener Aircraft Airbus Group Future aircraft technologies
14:00
15:30
1.8
Innovative concepts 2
2.8
High speed jet flows
3.8
Flow structures
4.8
Aeroacoustics
5.8
Health monitoring
6.8
Structural analysis 2
7.8
Open rotor 2
8.8
Flight dynamic system identification 2
9.8
UAV control
10.8
Fuel systems and fire protection
11.8
Future concepts
12.8
ISABE lectures
15:30
16:00
Break
16:00
18:00
1.9
Aircraft design
2.9
High lift
3.9
Hypersonic boundary layer control
4.9
Flight vehicle aerodynamics 2
5.9
Operational simulation 1
6.9
Aeroelasticity 2
7.9
Fans
8.9
Flight control 3
9.9
Noise abating trajectory optimization
10.9
Design applications and manufacturing
11.9
Ice and water impact on safety
12.9
Education and training
Thursday, 11. September 2014
08:00
09:00
General Lecture 4
Jaiwon Shin, NASA, USA , Rolf Henke, DLR, Germany, Kazuhiro Nakahashi, JAXA, Japan, Shyam Chetty, NAL, India, Sergey Chernyshev, TsAGI, Russia, The Future of Aviation by IFAR
09:00
10:00
Break
10:00
12:30
1.10
UAS 1
2.10
Turbulence modelling
3.10
Boundary layer instability and transition
4.10
Student final
5.10
Structural assessment techniques
6.10
Aeroelasticity 3
7.10
Nozzles and ducts 1
8.10
Flight optimization 1
9.10
Ecodesign
10.10
Simulation of systems and sub-systems
11.10
Safety and security enhancement
12.10
Fundamental Problems of Aeronautics
12:30
14:00
Lunch
14:00
15:30
1.11
UAS 2
2.11
Computational aeroacoustics
3.11
New analysis / phenomena 2
4.11
Optimization
5.11
Operational simulation 2
6.11
Dynamic load 2
7.11
Nozzles and ducts 2
8.11
Flight control 4
9.11
UAV navigation
10.11
Future scenarios
11.11
Safety and synthetic vision systems
12.11
International Cooperation in Aeronautics Research
15:30
16:00
Break
16:00
17:00
von Karman Lecture
Jaques Louis, France, Antonio Marchetto, Italy, Michail Maretsis, Greece, Fernando Mijares, Spain, nEUROn : an international cooperation to enhance innovation
17:00
17:30
Closing Ceremony
1.1Design for flow control
Chair: Bill Kimmel
Track 1
01 - Aircraft and Systems Integration
  10:50 11:20 1.1.1 INDUSTRIAL ASSESSMENT OF OVERALL AIRCRAFT DRIVEN LOCAL ACTIVE FLOW CONTROL
M. Lengers, Airbus Operations GmbH, Germany
  11:20 11:50 1.1.2 IMPACT OF INSECT CONTAMINATION ON OPERATIONAL AND ECONOMIC EFFECTIVENESS OF AIRCRAFT WITH NATURAL LAMINAR FLOW TECHNOLOGY
K. Wicke¹, M. Kruse¹, F. Linke¹, V. Gollnick¹; ¹German Aerospace Center (DLR), Germany
  11:50 12:20 1.1.3 NATURAL LAMINAR FLOW WING DESIGN OF SUPERSONIC TRANSPORT AT HIGH REYNOLDS NUMBER CONDITION
H. Ishikawa, TOUA Co. Ltd., Japan; N. Tokugawa¹, Y. Ueda, Tokyo Business Service Co. Ltd., Japan; K. Yoshida¹; ¹JAXA, Japan
2.1Aerodynamic optimization 1
Chair: Ernani V. Volpe
Track 2
02.1 - Aerodynamics - CFD Methods and Validation
  10:50 11:20 2.1.1 ON THE OPTIMIZATION OF BLENDED WING BODY AIRCRAFT CONFIGURATION VIA THE SURROGATE MODELING METHOD
T. Wan¹, Y.S. Chen¹; ¹Tamkang University, Taiwan
  11:20 11:50 2.1.2 CFD BASED OPTIMIZATION OF HIGH-LIFT DEVICES USING A MESH MORPHING TECHNIQUE
R.G. Silva, Universidade de São Paulo, Brazil; A.P. Antunes¹, R.B. Flatschart¹, J.L.F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil; ¹Embraer, Brazil
  11:50 12:20 2.1.3 AERODYNAMIC OPTIMIZATION OF A GREEN ATF REGIONAL AIRCRAFT IN CRUISE CONDITION
D.G. Romano¹, M. Mancini¹; ¹Piaggio Aero Industries S.p.A., Italy
3.1Wind tunnel techniques
Chair: Michel Guillome
Track 3
02.2 - Experimental Aerodynamics
  10:50 11:20 3.1.1 DESIGN AND VALIDATION OF A FORCED MOTION VARIABLE STIFFNESS AEROELASTIC WIND TUNNEL APPARATUS (AATB)
J. Ertveldt¹, J. Schoukens¹, R. Pintelon¹, S. Vanlanduit¹; ¹Vrije Universiteit Brussel, Belgium
  11:20 11:50 3.1.2 COMPRESSIBLE BOUNDARY LAYER HEAT FLUX MEASUREMENT USING EMBEDDED THERMOCOUPLES
X.J. Zhao¹, Y.H. Ma¹, W.Z. Xiao¹; ¹China Academy of Aerospace Aerodynamics, China
  11:50 12:20 3.1.3 CONTROLLED BOUNDARY LAYER ON THE SOLID WALLS OF WIND TUNNELS: NEW APPROACH TO THE BOUNDARY INTERFERENCE PROBLEM
A.I. Ivanov¹, E.V. Streltsov¹; ¹TsAGI, Russia
4.1Unsteady aerodynamics
Chair: Anatoly Gubanov
Track 4
02.4 - Applied Aerodynamics
  10:50 11:20 4.1.1 EXPERIMENTAL INVESTIGATIONS ON VORTEX FLOW PHENOMENA OF A DIAMOND WING CONFIGURATION
A. Hövelmann¹, C. Breitsamter¹; ¹Technische Universität München, Germany
  11:20 11:50 4.1.2 MODEL OF THE UNSTEADY AERODYNAMIC CHARACTERISTICS AT HIGH AOA WITH NONLINEAR DEPENDENCY IN ANGULAR RATE
D.I. Ignatyev¹, A.N. Khrabrov¹; ¹TsAGI, Russia
  11:50 12:20 4.1.3 SUBSONIC AND TRANSONIC FLOW SIMULATION FOR A WING OSCILLATING IN YAW AND SIDESLIP
K. Isogai, Japan Aerospace Exploration Agency, Japan
5.1Metal composite
Chair:
Track 5
03.1 - Materials issues, Fatigue and Damage Tolerance
  10:50 11:20 5.1.1 NOVEL METAL MATRIX/CARBON COMPOSITES FOR AIRSPACE APPLICATIONS
A.I. Rudskoy¹, A.G. Nasibulin, Skolkovo Institute of Science and Technology, Russia; T.S. Koltsova¹, O.V. Tolochko¹; ¹Saint Petersburg State Polytechnical University, Russia
  11:20 11:50 5.1.2 APPROXIMATE FUNCTION FOR FATIGUE CRACK PROPAGATION IN A DESIGN OPTIMISATION PROCEDURE FOR FIBRE METAL LAMINATES
I. Sen¹, R.C. Alderliesten¹, R. Bendictus¹; ¹Delft University of Technology, Netherlands
  11:50 12:20 5.1.3 AN ANALYTICAL SOLUTION TO THE ELASTIC-PLASTIC BEHAVIOR OF METAL MATRIX COMPOSITES UNDER TENSILE LOADING
S. Khosoussi¹, M. Mondali, , Islamic Azad University, Science and Research Branch, Iran; A. Abedian¹; ¹Sharif University of Technology, Iran
6.1Experimental method
Chair: A. Chizov
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  10:50 11:20 6.1.1 LOADS MODEL FLIGHT TEST VALIDATION BY MEANS OF INNOVATIVE, PHOTOGRAMMETRY BASED, DEFORMATION MEASUREMENT TECHNIQUE.
I. Ruiz Juretschke¹, B. Villalta Oliveira¹, R. Bancalero Santolaya¹; ¹Airbus Defense and Space, Spain
  11:20 11:50 6.1.2 UPDATING OF AIRCRAFT STRUCTURE DYNAMIC MODEL TO GROUND VIBRATION TEST RESULTS
J. Cecrdle, Aeronautical Research and Test Institute (VZLU), Czech Republic
  11:50 12:20 6.1.3 NUMERICAL SIMULATION AND WIND TUNNEL TESTING OF FLUTTER ABOUT AN ALL- MOVABLE HORIZONTAL TAIL AT TRANSONIC SPEEDS
W. Qian¹, G. Yang², G. Zheng², G. Zhang¹; ¹Shenyang Aircraft Design & Research Institute, China ;²Institute of Mechanics, Chinese Academy of Science, China
7.1Compressor
Chair: Song Fu
Track 7
04 - Propulsion
  10:50 11:20 7.1.1 CFD DESIGN AND ANALYSIS OF A COMPACT SINGLE-SPOOL COMPRESSOR FOR A HEAVY TRANSPORT HELICOPTER'S POWERPLANT
A. Startsev¹, Y. Fokin¹, E. Steshakov¹; ¹Central Inst of Aviation Motors, Russia
  11:20 11:50 7.1.2 VARIATION OF UNSTEADY FLOW PATTERN IN COMPRESSORS PRECEDING THE LOSS OF GASDYNAMIC STABILITY. EXPERIMENT.
N.N. Ledovskaya, Central Institute of Aviation Motors, Russia
  11:50 12:20 7.1.3 AERODYNAMIC DESIGN AND OPTIMIZATION OF BLADE CONFIGURATION IN AN INLET STAGE OF AN AIRCRAFT ENGINE COMPRESSOR
O. Marakueva, Baltic State Technical University, Russia
8.1Handling quality
Chair: Masaaki Yanagihara
Track 8
05.1 - Flight Dynamics and Control (Control & Modelling)
  10:50 11:20 8.1.1 THE WAYS FOR IMPROVEMENT OF AGREEMENT BETWEEN IN-FLIGHT AND GROUND-BASED SIMULATION FOR EVALUATION OF HANDLING QUALITIES AND PILOT TRAINING
A.V. Efremov¹, A.V. Koshelenko¹, M.S. Tjaglik¹, A.S. Tjaglik¹; ¹Moscow aviation institute, Russia
  11:20 11:50 8.1.2 REFINEMENT OF THE MODEL OF PILOT PERCEPTION OF AIRCRAFT MOTION IN UPSET CONDITIONS UTILIZING FLIGHT TESTS RESULTS
V.V. Rogozin¹, S.A. Zuev¹, M.A. Grigoryev¹, L.E. Zaichik², Y.P. Yashin²; ¹GFRI, Russia ;²TsAGI, Russia
  11:50 12:20 8.1.3 EVALUATIONS OF FLYING QUALITIES FOR A NEW AND AN AGING TRANSPORT AIRCRAFT IN SEVERE ATMOSPHERIC TURBULENCE
R.C. Chang, China University of Science and Technology, Taiwan; C.E. Lan, University of Kansas, United States; W.-L. Guan, Aviation Safety Council, Taiwan
9.1UAV design and testing 1
Chair: Tomasz Goetzendorf-Grabowski
Track 9
05.2 - Flight Dynamics and Control (UAV related)
  10:50 11:20 9.1.1 DESIGN AND FLIGHT TEST OF A SOLAR-POWERED UNMANNED AIR VEHICLE FOR LONG ENDURANCE
Z. Lei¹, H. Kawamura¹; ¹Tokyo University of Science, Suwa, Japan
  11:20 11:50 9.1.2 OPTIMAL CONTROL SURFACE MIXING OF A RHOMBOID WING UAV
E. Miles, University of Pretoria, South Africa; B.A. Broughton, Incomar Aeronautic, South Africa
  11:50 12:20 9.1.3 PREDICTED FLIGHT CHARACTERISTICS OF THE INVERTED JOINED WING SCALED DEMONSTRATOR
M. Lis¹, A. Dziubinski¹, C. Galinski¹, G. Krysztofiak¹, P. Ruchala¹, K. Surmacz¹; ¹Instytut Lotnictwa, Poland
10.1Optimization of trajectories
Chair: Ron van Manen
Track 10
06 - Systems, Subsystems and Equipment
  10:50 11:20 10.1.1 POLARIMETRIC AVIONIC WEATHER RADAR FOR INCREASING FLIGHT SAFETY AND EFFICIENCY
A. Lupidi¹, S. Lischi¹, F. Berizzi¹, M. Martorella¹, F. Cuccoli¹; ¹CNIT - RaSS, Italy
  11:20 11:50 10.1.2 AN INTELLIGENT ICE PROTECTION SYSTEM FOR NEXT GENERATION AIRCRAFT TRAJECTORY OPTIMISATION
A. Shinkafi¹, C. Lawson¹, R. Seresinhe¹, D. Quaglia¹, I. Madani¹; ¹Cranfield University, United Kingdom
  11:50 12:20 10.1.3 AIRFRAME SYSTEMS POWER OFF-TAKE MODELLING IN MORE-ELECTRIC LARGE AIRCRAFT FOR USE IN TRAJECTORY OPTIMISATION
R. Seresinhe¹, C. Lawson¹, A. Shinkafi¹, D. Quaglia¹, I. Madani¹; ¹Cranfield University, United Kingdom
11.1Air transport system
Chair: Marija Eijkman
Track 11
08 - Air Transport System Efficiency
  10:50 11:20 11.1.1 A SELF-SEPARATION ALGORITHM USING SPEED CONTROL FOR WIDTH-LIMITED HIGH DENSITY AIR CORRIDOR
Y. Nakamura, Electronic Navigation Research Institute, Japan; N. Takeichi¹, K. Fukuoka¹; ¹Nagoya University, Japan
  11:20 11:50 11.1.2 EVALUATING TEMPORAL INTEGRATION OF EUROPEAN AIR TRANSPORT
S. Lehner¹, K. Kölker¹, K. Lütjens¹; ¹German Aerospace Center (DLR), Germany
  11:50 12:20 11.1.3 COLLISION RISK STUDIES WITH 6DOF FLIGHT SIMULATIONS WHEN AERODROME OBSTACLE STANDARDS CANNOT BE MET
A. De Marco¹, J. D\'Auria¹; ¹University of Naples Federico II, Italy
12.1Advanced engines
Chair:
Track 12
04 - Propulsion
  10:50 11:20 12.1.1 IMPROVING CONTROL RELIABILITY AND QUALITY OF AIRCRAFT ENGINES BY MEANS THE SOFTWARE «VIRTUAL ENGINE»
F.D. Golberg¹, O.S. Gurevich¹, A.A. Petukhov¹; ¹CIAM, Russia
  11:20 11:50 12.1.2 CONCEPTS AND TECHNOLOGIES FOR THE NEXT GENERATION OF LARGE CIVIL AIRCRAFT ENGINES
F. Haselbach¹, A. Newby¹, R. Parker¹; ¹Rolls-Royce, United Kingdom
1.2Design for uncertainty
Chair: Martin Spieck
Track 1
01 - Aircraft and Systems Integration
  13:10 13:40 1.2.1 BLACK-BOX MODEL EPISTEMIC UNCERTAINTY AT EARLY DESIGN STAGE. AN AIRCRAFT POWER-PLANT INTEGRATION CASE STUDY
A. Molina-Cristobal¹, M. Nunez¹, M.D. Guenov¹, T. Laudan², T. Druot²; ¹Cranfield University, United Kingdom ;²Airbus Operations S.A.S, France
  13:40 14:10 1.2.2 AIRCRAFT CONFIGURATION ANALYSIS USING A LOW-FIDELITY, PHYSICS BASED AEROSPACE FRAMEWORK UNDER UNCERTAINTY CONSIDERATIONS
T. Pfeiffer¹, E. Moerland¹, D. Böhnke¹, B. Nagel¹, V. Gollnick¹; ¹German Aerospace Center, Germany
  14:10 14:40 1.2.3 FORMULATION OF AN EXPERIMENT SELECTION METHODOLOGY FOR UNCERTAINTY REDUCTION AND APPLICATION TO ACTIVE FLOW CONTROL
R.B. Jacobs¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States
2.2Aerodynamic optimization 2
Chair: Marco Ceze
Track 2
02.1 - Aerodynamics - CFD Methods and Validation
  13:10 13:40 2.2.1 ON THE USE OF THE ADJOINT METHOD TO COMPUTE NON--GEOMETRIC SENSITIVITIES
M. Hayashi, University of São Paulo, Brazil
  13:40 14:10 2.2.2 CFD-BASED COLLABORATIVE DESIGN OPTIMIZATION USING ECFD
B.I. Soemarwoto¹, A. Nugroho, Regio Aviasi Industri, Indonesia; E.H. Baalbergen¹, A. Aribowo, National Institute of Aeronautics and Space LAPAN, Indonesia; ¹National Aerospace Laboratory NLR, Netherlands
  14:10 14:40 2.2.3 AERODYNAMIC DESIGN METHOD FOR SUPERSONIC SLENDER BODY USING AN INVERSE PROBLEM
K. Matsushima¹, I. Yamamichi¹, N. Tokugawa, JAXA, Japan; ¹University of Toyama, Japan
3.2New analysis / phenomena 1
Chair: Kevin Knowles
Track 3
02.3 - Basic Fluid Dynamics and Flow Control
  13:10 13:40 3.2.1 AERODYNAMICS VIA AEROACOUSTICS – THE CASE FOR CIRCULATION CAPTURE
M.P. Brandão, ITA, Brazil
  13:40 14:10 3.2.2 ON THE INTERAL STRUCTURAL OF SHOCK WAVE IN RELAXING GAS
L.M.B.C Campos¹, F.S. Cunha¹; ¹Instituto Superior Técnico, Universidade de Lisboa, Portugal
  14:10 14:40 3.2.3 RANS MODELING FOR FLOWS ON RIBLETS BASED ON EXPERIMENTAL DATA
K. Okabayashi¹, T. Matsue², M. Asai², H. Naito¹; ¹Japan aerospace exploration agency, Japan ;²Tokyo metropolitan university, Japan
4.2Propulsion
Chair: Murd Brutian
Track 4
02.4 - Applied Aerodynamics
  13:10 13:40 4.2.1 STUDY ON PERFORMANCE AND FLOW CHARACTERISTICS FOR EMBEDDED DISTRIBUTED PROPULSION SYSTEM
S. Lee, Hanyang University, South Korea
  13:40 14:10 4.2.2 THE EFFECT OF PYLON TRAILING EDGE BLOWING ON THE PERFORMANCE AND NOISE PRODUCTION OF A PROPELLER
L.L.M. Veldhuis¹, T. Sinnige¹; ¹Delft University of Technology, Netherlands
  14:10 14:40 4.2.3 QUASI-ANALYTICAL AERODYNAMIC METHODS FOR PROPULSIVE FUSELAGE CONCEPTS
S. Kaiser¹, R. Grenon², J. Bijewitz¹, A. Prendinger¹, O. Atinault², A.T. Isikveren¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany ;²ONERA, The French Aerospace Lab, France
5.2Deformation and damage of composites
Chair: Matthias Meyer
Track 5
03.1 - Materials issues, Fatigue and Damage Tolerance
  13:10 13:40 5.2.1 INVESTIGATION OF MULTI-MATERIAL LAMINATES FOR SMART DROOP NOSE DEVICES
M. Kintscher¹, S. Geier¹, H.P. Monner¹, M. Wiedemann¹; ¹DLR, Germany
  13:40 14:10 5.2.2 DEFINITION OF THE BOLT SHEARING LOAD IN MULTIPLE-ROWMETAL COMPOSITE JOINTS
Y.S. Borovskaya¹, M.A. Glebova¹, V.I. Grishin¹; ¹TsAGI, Russia
  14:10 14:40 5.2.3 LOW-COST TITANIUM ALLOYS FOR TITANIUM-POLYMER LAYERED COMPOSITES
P. Panin¹, N. Nochovnaya¹, D. Kablov¹, E. Alexeev¹; ¹FSUE VIAM, Russia
6.2Impact
Chair: E. Dubovikov
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  13:10 13:40 6.2.1 MULTI-TERRAIN IMPACT SIMULATIONS OF A CRASHWORTHY COMPOSITE HELICOPTER SUBFLOOR
T. Billac¹, M. David², M. Battley, Center for Advanced Composite Materials, New Zealand; R. Thomson, Advanced Composite Structures Australia, CRC-ACS, Australia; C. Kindervater², R. Das¹; ¹The University of Auckland, New Zealand ;²German Aerospace Center, Germany
  13:40 14:10 6.2.2 FOD CHARACTERISTICS OF TITANIUM METAL MATRIX COMPOSITE (TMC) TO APPLY AIRCRAFT LANDING GEAR STRUCTURE
N. Takahashi¹, T. Sato¹, K. Fujiwara¹, T. Yokozeki, The University of Tokyo, Japan; A. Yoshimura², H. Shouji²; ¹Sumitomo Precision Products Co., Ltd., Japan ;²Japan Aerospace Exploration Agency, Japan
  14:10 14:40 6.2.3 NUMERICAL SIMULATION OF BIRD STRIKE IN AIRCRAFT LEADING EDGE STRUCTURE USING A NEW DYNAMIC FAILURE MODEL
Q. Sun¹, Y.J. Liu¹, R.H. Jin¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
7.2RAM / SCRAMjet 1 and supersonic engines
Chair: Hong Yan
Track 7
04 - Propulsion
  13:10 13:40 7.2.1 ANALYSIS OF THE PREDICTION ABILITY OF REACTION MECHANISMS FOR CFD MODELING OF THE COMBUSTION IN HIGH VELOCITY ENGINES
V. Kopchenov¹, S. Batura¹, L. Bezgin¹, N. Titova¹, A. Starik¹; ¹CIAM, Russia
  13:40 14:10 7.2.2 PHYSICAL INSIGHT INTO FUEL MIXING ENHANCEMENT WITH BACKWARD-FACING STEP FOR SCRAMJET ENGINES VIA MULTI-OBJECTIVE DESIGN OPTIMIZATION
H. Ogawa, RMIT University, Australia; C.Y. Wen, The Hong Kong Polytechnic University, Hong Kong SAR of China; Y.C. Chang, National Cheng Kung University, Taiwan
  14:10 14:40 7.2.3 STUDIES ON POSSIBLE UNIFICATION OF ENGINES FOR ADVANCED SMALL AND MEDIUM SUPERSONIC CIVIL AEROPLANES
A. Mirzoyan¹, A. Evstigneev¹; ¹Central Institute of Aviation Motors (CIAM), Russia
8.2Operations in turbulence
Chair: Dale King
Track 8
11 - Operations and Sustainment
  13:10 13:40 8.2.1 DEVELOPMENT OF LOW-LEVEL TURBULENCE ADVISORY SYSTEM FOR AIRCRAFT OPERATION
N. Matayoshi¹, T. Iijima¹, E. Yoshikawa¹, T. Ushio, Osaka University, Japan; ¹JAXA, Japan
  13:40 14:10 8.2.2 DYNAMIC WAKE VORTEX SEPARATION COMBINING WITH TRAFFIC OPTIMIZATION
N. Matayoshi, JAXA, Japan
  14:10 14:40 8.2.3 WAKE VORTEX OBSERVATION CAMPAIGN BY ULTRA FAST-SCANNING LIDAR IN NARITA AIRPORT, JAPAN
E. Yoshikawa¹, N. Matayoshi¹; ¹JAXA, Japan
9.2UAV design and testing 2
Chair: Cezary Galinski
Track 9
05.2 - Flight Dynamics and Control (UAV related)
  13:10 13:40 9.2.1 AERODYNAMIC MODEL IDENTIFICATION FROM FLIGHT DATA FOR A NOVEL CONCEPT SCALED UAV
Z.-X. Yao, SADRI, China
  13:40 14:10 9.2.2 CONCEPTUAL DESIGN OF AIRCRAFT FOR OPTIMAL MANEUVERS
N. K. SINHA, IIT-Madras, India
  14:10 14:40 9.2.3 FLIGHT DYNAMICS OF HIGHLY FLEXIBLE SOLAR-POWERED UAV BASED ON GEOMETRICALLY NONLINEAR INTRINSIC BEAM
R. Wang¹, Z. Zhou¹, X. Zhu, Institute of UAV, Northwestern Polytechnical University, China; X. Xu¹; ¹Science and Technology on UAV Laboratory, Northwestern Polytechn, China
10.2Innovative concepts (systems)
Chair: Phillipe Tatry
Track 10
06 - Systems, Subsystems and Equipment
  13:10 13:40 10.2.1 UAV REMOTE POWER SUPPLY SYSTEM BY LASER RADIATION
O.V. Zayats¹, V.Y. Tugaenko¹, V.P. Khvostikov, Ioffe Physico-Technical Institute, Russia; ¹S.P. Korolev Rocket And Space Corporation \\\\\\\\, Russia
  13:40 14:10 10.2.2 EXPERIMENTAL VALIDATION OF A SENSORIZED RING BASED ON OPTICAL FIBER FOR STRAIN MONITORING OF MORPHING STRUCTURE
M. Ciminello¹, P. Bettini², S. Ameduri¹, E. Guerreschi², G. Cuneo²; ¹CIRA, Italy ;²Politecnico di Milano, Italy
  14:10 14:40 10.2.3 DEVELOPMENT OF A HYBRID ICE PROTECTION SYSTEM BASED ON NANOSTRUCTURED HYDROPHOBIC SURFACES
T. Strobl¹, S. Storm¹, M. Kolb¹, J. Haag¹, M. Hornung, Technical University of Munich, Germany; ¹Airbus Group Innovations, Germany
11.2Airport
Chair: Johannes Reichmuth
Track 11
08 - Air Transport System Efficiency
  13:10 13:40 11.2.1 OPTIMAL PUSHBACK TIME WITH EXISTING UNCERTAINTIES AT BUSY AIRPORT
R. Mori, Electronic Navigation Research Institute, Japan
  13:40 14:10 11.2.2 TERMINAL HOLDING TIME OPTIMIZATION BY DYNAMIC CDA ROUTING ALGORITHM
S.M. Malaek¹, F. Enayatollahi¹, J. Parastari, Civil Aviation Technology College, Iran; ¹Sharif University of Technology, Iran
12.2Innovative engines 1
Chair: Ric Parker
Track 12
04 - Propulsion
  13:10 13:40 12.2.1 NUMERICAL MODELING OF FLOW IN GASDYNAMIC RESONATOR AND MODEL VALIDATION BY RESULTS OF PULSE ENGINE TESTS
F.A. Slobodkina¹, V.V. Malinin¹, A.I. Tarasov, Lulka RDC, Russia; ¹Gubkin Russian State University of Oil and Gas, Russia
  13:40 14:10 12.2.2 SENSITIVITY ANALYSIS OF TURBINE ENGINE SUSTAINMENT
E.E. Iglesias¹, H. Millwater¹; ¹University of Texas at San Antonio, United States
1.3Design methods 1
Chair: Spiros Pantelakis
Track 1
01 - Aircraft and Systems Integration
  15:00 15:30 1.3.1 THEORETICAL FRAMEWORK OF SYSTEMS DESIGN FOR THE AIR TRANSPORTATION SYSTEM INCLUDING AN INHERENTLY QUANTITATIVE PHILOSOPHY OF SCENARIO DEVELOPMENT
R. Ghosh¹, T. Schilling¹, K. Wicke¹; ¹German Aerospace Center, Germany
  15:30 16:00 1.3.2 EXPLICIT MODELING OF TECHNOLOGY IMPROVEMENT OVER TIME IN CONCEPTUAL AIRCRAFT DESIGN
D. Böhnke¹, B. Nagel¹, V. Gollnick¹; ¹DLR e.V., Germany
  16:00 16:30 1.3.3 KNOWLEDGE DISCOVERY IN CONCEPTUAL DESIGN OF SPACE PLANES USING MULTI-OBJECTIVE OPTIMIZATION AND DATA MINING
T. Fujikawa, The University of Tokyo, Japan
  16:30 17:00 1.3.4 MULTIDISCIPLINARY OPTIMIZATION OF TRUSS-BRACED WING LAYOUT
K.-S. Zhang¹, A. Bakar¹, P.-B. Ji¹, Z.-H. Han¹, X.-P. Li¹; ¹Northwestern Polytechnical University, China
2.3CFD applied to design
Chair: Mario Lott
Track 2
02.1 - Aerodynamics - CFD Methods and Validation
  15:00 15:30 2.3.1 EFFICIENT STATIONARY AND NONSTATIONARY AERODYNAMIC CALCULATION ALGORITHMS FOR THE APPLIED AERODYNAMICS PROBLEMS
O.V. Karas, TsAGI, Russia
  15:30 16:00 2.3.2 COMMUTER AIRCRAFT AERODYNAMIC DESIGN: WIND-TUNNEL TESTS AND CFD ANALYSIS
F. Nicolosi¹, S. Corcione¹, P. Della Vecchia¹; ¹UNIVERSITY OF NAPLES FEDERICO II, Italy
  16:00 16:30 2.3.3 AERODYNAMIC INTERFERENCE OF WINGTIP AND WING DEVICES ON BWB MODEL
H.D. Ceron-Munoz¹, D.O. Diaz-Izquierdo, São Carlos Engineering School-University of São Paulo-Brazil, Brazil; J. Solarte-Pineda¹, F.M. Catalano¹; ¹São Carlos Engineering School-University of São Paulo, Brazil
  16:30 17:00 2.3.4 COMPUTATIONAL INVESTIGATION OF SIMULATION ON THE DYNAMIC DERIVATIVES OF FLIGHT VEHICLE
B.-G. Mi¹, H. Zhan¹, B. Wang¹; ¹Northwestern Polytechnical University, China
3.3High speed flow studies
Chair: Oliver Chasot
Track 3
02.2 - Experimental Aerodynamics
  15:00 15:30 3.3.1 PIV INTRODUCED EXPERIMENTAL INVESTIGATION OF COUNTERFLOW EJECTION ON BLUNT BODY MOVING WITH SUPERSONIC SPEED
Y.Y. Zheng, University of New South Wales, Australia
  15:30 16:00 3.3.2 HYPERSONIC FLOWFIELD AND HEAT FLUX PECULIARITIES ON THE NEW SPACE LAUNCHER WITH WINGED REUSABLE FIRST STAGE.
S.M. Drozdov¹, V.N. Brazhko¹, V.E. Mosharov¹, A.S. Skuratov¹, D.S. Fedorov², V.V. Gorbatenko², P.A. Lehov², J.N. Chibisov²; ¹TsAGI, Russia ;²KSRPSC, Russia
  16:00 16:30 3.3.3 THE FLOW IN THE PLANE OF SYMMETRY OF THE DELTA WING IN THE REGIME OF STRONG VISCOUS-INVISCID INTERACTION.
G.N. Dudin, Central Aerohydrodynamic Institute (TsAGI), Russia
4.3Flapping wing
Chair: Anatoly Bolsunovsky
Track 4
02.4 - Applied Aerodynamics
  15:00 15:30 4.3.1 EFFECT OF ANGLE OF ATTACK KINEMATICS ON PASSIVE FLAPPING FOIL POWER GENERATION
J. Young¹, J.C.S. Lai¹; ¹University of New South Wales, Australia
  15:30 16:00 4.3.2 COMPUTATIONAL ANALYSIS FOR FLAPPING WING BY COUPLED CFD AND CSD SOLUTIONS
N. Lee¹, S. Lee¹, H. Cho², J.-Y. Kwak, Korea Aerospace Research Institute, South Korea; S.J. Shin²; ¹Inha University, South Korea ;²Seoul National University, South Korea
  16:00 16:30 4.3.3 INVESTIGATION OF AIRFOIL FOR AN INSECT-SIZED FLAPPING WING
H. Nagai¹, K. Isogai¹, N. Uda¹, K. Ono¹; ¹Kyushu University, Japan
  16:30 17:00 4.3.4 AERODYNAMIC RESEARCH OF FLEXIBLE FLAPPING WING BY COMBINING DIC AND CFD APPROACHES
W. Yang¹, B. Song¹, W. Song¹, L. Wang¹, P. Fu¹, J. Xu¹; ¹Northwestern Polytechnical University, China
5.3Separation / lift control
Chair: S. H. Peng
Track 5
02.3 - Basic Fluid Dynamics and Flow Control
  15:00 15:30 5.3.1 INFLUENCE OF WING ASPECT RATIO ON PASSIVE STALL CONTROL AT LOW REYNOLDS NUMBER USING SINUSOIDAL LEADING EDGES
A. Esmaeili¹, J.M.M. Sousa¹; ¹IDMEC - Instituto Superior Tecnico, Portugal
  15:30 16:00 5.3.2 A NOVEL CONCEPTIONS OF PLASMA GURNEY FLAP
L.-H. Feng¹, J.-J. Wang¹, K.-S. Choi, University of Nottingham, United Kingdom; ¹Beijing University of Aeronautics and Astronautics, China
  16:00 16:30 5.3.3 THE EFFICIENCY ANALYSIS OF GUST ALLEVIATION BASED ON ACTIVE FLOW CONTROL
X. XU¹, Z. ZHOU¹, R. WANG¹; ¹Northwestern Polytechnical University, China
  16:30 17:00 5.3.4 COMPUTATIONAL EVALUATION OF FLOW CONTROL FOR ENHANCED CONTROL AUTHORITY OF A VERTICAL TAIL
A. Shmilovich¹, Y. Yadlin¹, E. Whalen¹; ¹The Boeing Company, United States
6.3Dynamic load 1
Chair:
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  15:00 15:30 6.3.1 DYNAMIC RESPONSE OF AN AIRPLANE ELASTIC STRUCTURE IN TRANSONIC FLOW
S. Kuzmina¹, F. Ishmuratov¹, O. Karas¹, A. Chizhov¹; ¹TsAGI, Russia
  15:30 16:00 6.3.2 FE-MODELLING GUIDELINES FOR THE DIMENSIONING OF AIRCRAFT CABIN INTERIOR UNDER STATIONARY DYNAMIC LOADS
R. Seemann¹, B. Plaumann¹, J. Oltmann¹, D. Krause¹; ¹TUHH, Institute PKT, Germany
  16:00 16:30 6.3.3 FLIGHT LOADS ESTIMATION USING LOCAL MODEL NETWORKS
M. Halle¹, F. Thielecke¹; ¹TUHH/FST, Germany
  16:30 17:00 6.3.4 THE DIRECT PREDICTION OF BUCKLING LOADS OF SHELLS UNDER AXIAL COMPRESSION USING VCT - TOWARDS AN UPGRADED APPROACH
E.L. Jansen¹, H. Abramovich, Technion, I.I.T., Israel; R. Rolfes¹; ¹Leibniz Universitaet Hannover, Germany
7.3RAM / SCRAMjet 2
Chair: Valeriy Kopchenov
Track 7
04 - Propulsion
  15:00 15:30 7.3.1 MECHANISMS OF POLLUTANT FORMATION IN THE H2 - FUELLED COMBUSTOR OF HIGH VELOCITY AIR-BREATHING ENGINE: MODELING STUDY
L. Bezgin¹, V. Kopchenov¹, N. Titova¹, A. Starik¹; ¹CIAM, Russia
  15:30 16:00 7.3.2 DESIGN OF SUPERSONIC EJECTION SYSTEM FOR HIGH SPEED COMBUSTION INVESTIGATION AND RESULTS OF WIDE RANGE COMBUSTION CHAMBER TESTS
V. Avrashkov, MAI, Russia; M. Boucheze¹, S. Balland¹; ¹MBDA-France, France
  16:00 16:30 7.3.3 MODERN RESEARCH AREAS OF SOLID HYPERSONIC RAMJET ENGINES
V.M. Abashev¹, A.G. Prudnikov¹, E.E. Son¹; ¹Moscow Aviation Institute, Russia
  16:30 17:00 7.3.4 HEAT FLUX LEVEL DETERMINATION IN MODEL COMBUSTION CHAMBER OF HIGH-SPEED RAMJET ENGINE
M. Danilov¹, M. Frantsuzov¹, N. Kukshinov¹; ¹Central Institute of Aviation Motors, Russia
8.3Flight dynamic system identification 1
Chair: Sato Masayuki
Track 8
05.1 - Flight Dynamics and Control (Control & Modelling)
  15:00 15:30 8.3.1 NEURAL NETWORK ADAPTIVE SEMI-EMPIRICAL MODELS FOR AIRCRAFT CONTROLLED MOTION
M.V. Egorchev¹, D.S. Kozlov¹, Y.V. Tiumentsev¹; ¹Moscow Aviation Institute (MAI), Russia
  15:30 16:00 8.3.2 A COMPARISON OF TECHNIQUES TO GET SPARSE RATIONAL APPROXIMATIONS FOR LINEAR FRACTIONAL REPRESENTATIONS
C. Roos¹, G. Hardier¹, C. Döll¹; ¹ONERA/DCSD, France
  16:00 16:30 8.3.3 AIRCRAFT PARAMETER IDENTIFICATION USING GENTIC ALGORITHMS
M. Ulinowicz¹, J. Narkiewicz¹; ¹Warsaw University of Tchnology, Poland
  16:30 17:00 8.3.4 APPROACHES FOR FLIGHT TESTS AIRCRAFT PARAMETER IDENTIFICATION
O.N. Korsun, State Institute of Aviation Systems, Russia; B.K. Poplavsky, Gromov Flight Research Institute, Russia
9.3Flapping wing UAV
Chair: Petter Krus
Track 9
05.2 - Flight Dynamics and Control (UAV related)
  15:00 15:30 9.3.1 KINEMATIC AND UNSTEADY AERODYNAMIC MODELLING OF FLAPPING BI- AND QUAD-WING ORNITHOPTER
H. Djojodihardjo¹, M. Anas Bin Abd Bari¹; ¹Universiti Putra Malaysia, Malaysia
  15:30 16:00 9.3.2 APPLICATION OF ARTIFICIAL NEURAL NETWORK IN MODELING OF ENTOMOPTER DYNAMICS
P. Czekalowski, Institute of Aviation, Poland; K.-S. Sibilski¹, A. Zyluk¹; ¹Air Force Institute of Technology, Poland
  16:00 16:30 9.3.3 IDENTIFICATION AND TRACKING CONTROL OF FLAPPING MOTIONS IN ROBOTIC BATS
J. Dadashi, Virginia Polytechnic Institute and State University, United States
  16:30 17:00 9.3.4 DEVELOPMENT OF A MULTI-PURPOSE UAV WITH BIO-INSPIRED FEATURES
R.K. Rangel, BRVANT / BRV UAV& Flight Systems , Brazil; K.H. Kienitz¹, M.P. Brandão¹; ¹Technological Institute of Aeronautics - ITA, Brazil
10.3Avionics
Chair: Joseph Huysseune
Track 10
06 - Systems, Subsystems and Equipment
  15:00 15:30 10.3.1 ADVANCED AVIONICS EQUIPMENT ON THE BASIS OF SECOND GENERATION INTEGRATED MODULAR AVIONICS
G.A. Chuyanov¹, V.V. Kosyanchuk¹, N.I. Selvesyuk¹, E.Y. Zybin¹; ¹State Research Institute of Aviation Systems, Russia
  15:30 16:00 10.3.2 INTEGRATED ONBOARD NETWORKING FOR IMA2G
Y. Sheynin¹, E. Suvorova¹, V. Bukov², V. Shurman²; ¹Saint-Petersburg State University of Aerospace Instrumentation, Russia ;²PLC Scientific and Research Institute of Avionic Equipment, Russia
  16:00 16:30 10.3.3 METHOD OF SEARCHING FOR ROUTES WITH DELAY AND JITTER LIMITATION
N. Matveeva, Saint-Petersburg State University of Aerospace Instrumentation, Russia
  16:30 17:00 10.3.4 TOOLSET FOR ONBOARD NETWORKS DESIGN AND CONFIGURATION
Y. Sheynin¹, E. Suvorova¹, A. Syschikov¹, B. Sedov¹, N. Matveeva¹, D. Raszhivin¹; ¹SUAI, Russia
11.3Arrival management
Chair: Kurt Klein
Track 11
08 - Air Transport System Efficiency
  15:00 15:30 11.3.1 A COMPARISON OF THE TWO ARRIVAL TRAFFIC SYNCHRONIZATION CONCEPTS ENVISIONED FOR NEXTGEN AND SESAR.
J. Crespo¹, C. Cuerno¹, R.M. Arnaldo¹, J. Saez Nieto¹, M. Sadornil¹, J. Pérez¹, R. Barragan, CRIDA, Spain; ¹Technical University of Madrid (UPM), Spain
  15:30 16:00 11.3.2 VALIDATION AND SIMULATION STUDY OF THE ARRIVAL MERGING PROCEDURE MODEL
K. Kageyama, ENRI, Japan; B. Park, KOTI, South Korea
  16:00 16:30 11.3.3 OPTIMISED ALGORITHMS FOR EXTENDED ARRIVAL MANAGERS
R. Barragan, CRIDA, Spain; J.A. Perez Castan¹, M. Sadornil¹, F. Saez Nieto¹, J. Crespo¹, R. Arnaldo¹, C. Cuerno¹; ¹UPM, Spain
  16:30 17:00 11.3.4 TRAJECTORY PREDICTION PERFORMANCE COMPARISON TOWARDS EFFICIENT TIME-BASED METERING OPERATIONS
G. Enea, Engility Corporation, United States; G. McDonald¹, J. Bronsvoort¹; ¹AirServices Australia, Australia
12.3Innovative engines 2
Chair: Askin Isikveren
Track 12
04 - Propulsion
  15:00 15:30 12.3.1 RESEARCH OF EFFICIENCY OF THE MID-FLIGHT POWER PLANT BASED ON THE HYBRID ENGINES FOR ADVANCED AIRLINERS
P. Ryabov, CIAM, Russia
  15:30 16:00 12.3.2 THE HYBRID PROPULSION SYSTEMS FOR THE ADVANCED AIRCRAFT
A.V. Lukovnikov¹, O.D. Selivanov¹, P.A. Ryabov¹, Y.A. Ezrokhi¹, S.M. Kalensky¹; ¹CIAM, Russia
  16:00 16:30 12.3.3 INVESTIGATION OF UNIVERSALLY ELECTRIC PROPULSION SYSTEMS FOR TRANSPORT AIRCRAFT
P.C. Vratny¹, P. Forsbach¹, A. Seitz¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
  16:30 17:00 12.3.4 ANALYSIS OF POSSIBILITIES TO APPLY ELECTRIC TECHNOLOGIES FOR HELICOPTER PROPULSION SYSTEM
O. Gurevich¹, A. Lukovnikov¹, A. Gulienko¹, V. Zakharchenko¹, I. Kovalenko¹, P. Suntsov¹; ¹CIAM, Russia
1.4Design methods 2
Chair: Andrey Volkov
Track 1
01 - Aircraft and Systems Integration
  10:00 10:30 1.4.1 A CONCEPTUAL DESIGN AND ANALYSIS METHOD FOR CONVENTIONAL AND UNCONVENTIONAL AIRPLANES
R. Elmendorp¹, R. Vos¹, G. La Rocca¹; ¹TU Delft, Netherlands
  10:30 11:00 1.4.2 SET-BASED DESIGN SPACE EXPLORATION ENABLED BY DYNAMIC CONSTRAINT ANALYSIS
J.R. Kizer¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States
  11:00 11:30 1.4.3 DESIGN AND OPTIMIZATION OF AIRCRAFT ASSEMBLING BASED ON COMPREHENSIVE SIMULATION OF MANUFACTURING PROCESSES
A.V. Rozhdestvensky¹, O.S. Samsonov¹; ¹“MATI” – Russian State University of Aviation Technology, Russia
  11:30 12:00 1.4.4 MULTI-CRITERIAL AERODYNAMIC SYNTHESIS METHOD OF MISSION-ORIENTED AIRCRAFT DESIGN
S. Kachel, Faculty of Mechatronics and Av/Military University of Technology, Poland
2.4UAV applications
Chair: Fernando M. Catalano
Track 2
02.1 - Aerodynamics - CFD Methods and Validation
  10:00 10:30 2.4.1 URBAN WIND FIELD GENERATION USING LES FOR APPLICATION TO QUADROTOR FLIGHT
M. Sutherland¹, J. Etele¹; ¹Carleton University, Canada
  10:30 11:00 2.4.2 NUMERICAL SIMULATION OF SELF-PROPELLED FLYING OF A THREE-DIMENSIONAL BIRD WITH FLAPPING WINGS
C.-J. WU¹, L.-L. ZHU¹; ¹School of Aeronautics and Astronautics, DUT, China
  11:00 11:30 2.4.3 FLUID DYNAMICS ANALYSIS OF A COUNTER ROTATING DUCTED PROPELLER
C. Xu¹, C. Bil¹, C.P. Cheung¹; ¹RMIT University, Australia
  11:30 12:00 2.4.4 COMPUTATIONAL COMPARATIVE STUDY FOR DESIGN OF LOW REYNOLDS NUMBER AIRFOIL
K. Kondo, Tokyo University of Science, Japan
3.4Flow control studies
Chair: Ian Poll
Track 3
02.2 - Experimental Aerodynamics
  10:00 10:30 3.4.1 FLOW FIELD AROUND DIMPLED SHORT PIN-FINS IN A STAGGERED ARRAY
S.M. Roux¹, G.I. Mahmood¹, J.P. Meyer¹; ¹University of Pretoria, South Africa
  10:30 11:00 3.4.2 AN OVERVIEW OF RECENT EXPERIMENTAL STUDIES CONDUCTED IN ONERA S3CH TRANSONIC WIND TUNNEL
R. Bur¹, V. Brion¹, P. Molton¹; ¹ONERA, France
  11:00 11:30 3.4.3 THE EFFECT OF A SYNTHETIC JET ON THE PRESSURE DISTRIBUTION OF A FLAT PLATE
Y.-H. Kim, Emirates Aviation University, United Arab Emirates; K.P. Garry, Cranfield University, Germany
  11:30 12:00 3.4.4 EXPERIMENTAL RESEARCH ON FLOW SEPARATION CONTROL USING SYNTHETIC JET ACTUATORS
E. Koopmans¹, H.W.M. Hoeijmakers¹; ¹University of Twente, Netherlands
4.4Transsonic aerodynamics
Chair: Alexander Pavlenko
Track 4
02.4 - Applied Aerodynamics
  10:00 10:30 4.4.1 AERODYNAMIC MODELLING OF A REFUELLING BOOM
L. Manfriani¹, M. Righi¹; ¹ZHAW, Switzerland
  10:30 11:00 4.4.2 TRANSONIC AIRFOILS, WINGS, AND PROJECTILES ADMITTING ANOMALOUS BEHAVIOR OF AERODYNAMIC COEFFICIENTS
A. Kuzmin¹, A. Ryabinin¹; ¹St. Petersburg State University, Russia
  11:00 11:30 4.4.3 TRANSONIC STORE SEPARATION ANALYSES USING MODERN DESIGN OF EXPERIMENTS AND QUANTITATIVE GRADING OF RESULTS
K.A. Jamison, Council of Scientific and Industrial Research, South Africa
5.4Turbine materials
Chair: Miroslaw Rodjewcj
Track 5
03.1 - Materials issues, Fatigue and Damage Tolerance
  10:00 10:30 5.4.1 EXPERIMENTAL EVALUATION OF THE EFFICIENCY OF GAS TURBINE ENGINE PARTS DAMPING WITH DRY FRICTION DAMPERS USING LASER VIBROMETER
A. Balakirev¹, B. Bolotov¹, A. Golovkin¹, M. Nikhamkin¹, N. Sazhenkov¹, L. Voronov¹, I. Konev¹; ¹Perm National Research Polytechnic University, Russia
  10:30 11:00 5.4.2 PROBLEM OF LOW CYCLE FATIGUE OF TURBOMACHINES
J. Temis¹, K. Azmetov¹, A. Fakeev¹; ¹Central Institute of Aviation Motors, Russia
  11:00 11:30 5.4.3 ANALYSIS AND COUNTERMEASURE ON AERO-ENGINE BLADE DEFECT
Z. Sun¹, Z. Guo¹, G. Liu¹; ¹AVIC Xi’an Aero-engine (Group) LTD., China
  11:30 12:00 5.4.4 HIGH TEMPERATURES TURBINE BLADES DAMAGE PREDICTION TAKING INTO ACCOUNT LOADING HISTORY DURING A FLIGHT CYCLE
B.E. Vasilyev¹, L.A. Magerramova¹; ¹CIAM, Russia
6.4Structural design 1
Chair: Richard Forster
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  10:00 10:30 6.4.1 STRUCTURE DESIGN AND MECHANICAL SIMULATION ON THE SC-MR SUPPORT FOR ROTOR SYSTEM
Y.H. Ma¹, H.X. Zhu¹, J. Hong¹; ¹Beihang University, China
  10:30 11:00 6.4.2 A RAPID ANALYSIS METHODOLOGY FOR EARTH ENTRY VEHICLE DEVELOPMENT
S. Perino¹, J. Bayandor¹; ¹Virginia Tech, United States
  11:00 11:30 6.4.3 DESIGN AND PERFORMANCE TEST OF A TWIN-FUSELAGE CONFIGURATION SOLAR-POWERED UAV
X.-Z. Gao¹, Z.-X. Hou¹, Z. Guo¹, X.-Q. Chen¹; ¹National University of Defense Technology, China
  11:30 12:00 6.4.4 AN ENGINEERING ANALYSIS METHOD OF POST-BUCKLING FOR COMPOSITE STIFFENED PANELS
F.-F. Wang, AMECO, China; D.-G. Cui, AVIC, China
7.4Turbines 1
Chair: Ric Parker
Track 7
04 - Propulsion
  10:00 10:30 7.4.1 EXPERIMENTAL AND NUMERICAL INVESTIGATION OF LOADING LEVELS AND DISTRIBUTIONS ON LOW PRESSURE TURBINE PERFORMANCE
A.R. Wadia, GE Aviation, United States
  10:30 11:00 7.4.2 ABOUT APPROACHES TO RESEARCH OF FLAT LPT CASCADES AT LOW RE NUMBERS
V.D. Venediktov, Central Institute of Aviation Motors, Russia
  11:00 11:30 7.4.3 TURBULENCE MEASUREMENTS IN A FLOW PART OF TURBOMACHINES USING A HIGH-FREQUENCY PRESSURE PROBE
A.D. Nepomnyashchiy, Central Institute of Aviation Motors, Russia
  11:30 12:00 7.4.4 MULTIDISCIPLINARY ANALYSIS OF HIGH AND LOW PRESSURE TURBINES ON TRANSITIVE MODES IN THE FLIGHT CYCLE
S.V. Kharkovskiy ¹, R.Z. Nigmatullin¹, V.S. Kinzburskiy¹, V.V. Starodubtsev¹; ¹CIAM, Russia
8.4Flight modelling and simulation 1
Chair: Abbasi Humayoon
Track 8
05.1 - Flight Dynamics and Control (Control & Modelling)
  10:00 10:30 8.4.1 UPSET RECOVERING SIMULATION TO ENHANCE FLIGHT SAFETY BY ON-GROUND PILOT TRAINING
A.G. Bushgens¹, L.E. Zaychik¹, A.N. Khrabrov¹, I.I. Grishin¹, P.A. Desyatnik¹, V.V. Biryukov, FRI, Russia; ¹TsAGI, Russia
  10:30 11:00 8.4.2 EVALUATION OF LANDING CHARACTERISTICS ACHIEVED BY SIMULATIONS AND FLIGHT TESTS ON A SMALL-SCALED MODEL RELATED TO MAGNETICALLY LEVITATED ADVANCED TAKE-OFF AND LANDING OPERATIONS.
D. Rohacs, REA-TECH, Hungary; M. Voskuijl, Delft University of Technology, Netherlands; N. Siepenkötter, RWTH Aachen, Germany
  11:00 11:30 8.4.3 NEW FEATURES OF UNGUIDED BODY REENTRY WITH SUBCIRCULAR VELOCITY AND PECULIARITIES OF ITS SIMULATION
A.S. Filatyev¹, A.A. Golikov¹; ¹Central Aerohydrodynamic Institute, Russia
  11:30 12:00 8.4.4 COMPUTATIONAL INVESTIGATION OF UNSTEADY AERODYNAMIC CHARACTERISTICS OF A MODERN AIRLINER
A.N. Khrabrov¹, D.A. Kravchenko¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
9.4Novel fuel / usage and operation
Chair: Ruben del Rosarion
Track 9
10 - Challenge of the Environment
  10:00 10:30 9.4.1 COMPARATIVE ANALYSIS OF RUSSIAN AND WESTERN APPROACHES TO THE PROBLEM OF ALTERNATIVE FUEL USAGE IN AVIATION
V.N. Zhuravlev, Moscow Aviation Institute, Russia
  10:30 11:00 9.4.2 CONTROLLED HYDROGEN GENERATOR AND ADDITIONAL SOURCE OF ELECTRICAL CURRENT FOR INDEPENDENT OXYGEN-HYDROGEN POWER PLANTS
K.V. Pushkin, Moscow Aviation Institute (National Research University), MAI, Russia
  11:00 11:30 9.4.3 EVALUATION OF EMISSION CHARACTERISTICS OF GAS TURBINE ENGINES USING ALTERNATIVE FUELS
A.M. Savel’ev¹, V.A. Skibin¹, A.M. Starik¹; ¹Central Institute of Aviation Motors, Russia
10.4Navigation and radar 1
Chair: V. Vitkorovich
Track 10
06 - Systems, Subsystems and Equipment
  10:00 10:30 10.4.1 DADF ( DIGITAL AUTOMATIC DIRECTION FINDER )
M. Mirzaee¹, M. Sam kan, Sattari University, Iran; S. Behroozifar¹; ¹University of Science and Applied of SAMAPARAN, Iran
  10:30 11:00 10.4.2 HIGH ALTITUDE TURBULENCE DETECTION USING AN AIRBORNE DOPPLER LIDAR
H. Inokuchi¹, M. Furuta¹, T. Inagaki¹; ¹JAXA, Japan
  11:00 11:30 10.4.3 ABOUT THE CONCEPT OF STRAPDOWN VECTOR AEROGRAVIMETRIC MEASUREMENTS
A.A. Afonin¹, A.S. Sulakov¹, G.G. Yamashev¹; ¹MAI, Russia
  11:30 12:00 10.4.4 ON A CONCEPT OF CREATION OF AN AIRPORT ADVANCED SURFACE MOVEMENT AND GROUND CONTROL SYSTEM
Konstantin K. Veremeenko, Moscow Aviation Institute (National Research University), Russia
11.4Weather / Wake Vortex
Chair: Bruno Lamiscarre
Track 11
08 - Air Transport System Efficiency
  10:00 10:30 11.4.1 4D TRAJECTORY BASED OPERATION IN HIGH DENSITY TERMINAL CONTROL AREA CONSIDERING THE UNCERTAINTY OF WEATHER FORECAST DATA
A. Tezuka, Waseda University, Japan
  10:30 11:00 11.4.2 THE NETWORK FLOW ENVIRONMENT: SLOT ALLOCATION MODEL EVALUATION WITH CONVECTIVE NOWCASTING
A. Lau¹, R. Budde, Advanced Traffic Solutions (ATRiCS), Germany; J. Berling, Technical University of Hamburg (TUHH), Germany; V. Gollnick¹; ¹German Aerospace Center (Air Transportation Systems) , Germany
  11:00 11:30 11.4.3 DEVELOPMENT AND EVALUATION OF LOW-LEVEL TURBULENCE ADVISORY DISPLAY FOR AIRCRAFT OPERATION
T. Iijima¹, N. Matayoshi¹, E. Yoshikawa¹; ¹JAXA, Japan
  11:30 12:00 11.4.4 APPLICATION OF SUBOPTIMAL 4-D NAVIGATION ALGORITHMS FOR FLIGHT PLANNING AND CONTROL CONSIDERING WEATHER CONDITIONS
N. Grevtsov¹, A. Dymchenko¹; ¹TsAGI, Russia
12.4Engine materials
Chair: Eric Bachelet
Track 12
04 - Propulsion
  10:00 10:30 12.4.1 AEROELASTIC DAMPING PREDICTIONS FOR MULTISTAGE TURBOMACHINERY APPLICATIONS
A. Placzek, Onera, France
  10:30 11:00 12.4.2 STRENGTH RELIABILITY OF TURBINE ROTOR ENSURING BASED ON MULTIDISCIPLINARY OPTIMIZATION
A. Salnikov, CIAM, Russia
  11:00 11:30 12.4.3 BIMETALLIC BLISK DESIGN FOR HIGH TEMPERATURE TURBINES OF GAS TURBINE ENGINE OF DIFFERENT APPLICATION
L. Magerramova, Central Institute of Aviation Motors, Russia
  11:30 12:00 12.4.4 LIFE VALIDATION STRATEGY
A.A. Inozemtsev¹, L.B. Polatidi¹, I.L. Andreychenko¹; ¹Aviadvigatel OJSC, Russia
1.5Hypersonic vehicles
Chair: Igor Lipatov
Track 1
01 - Aircraft and Systems Integration
  14:00 14:30 1.5.1 A HOLISTIC APPROACH TO HYPERSONIC AIRCRAFT DESIGN: ZEHST (ZERO EMISSION HIGH SPEED TECHNOLOGIES)
E. Blanvillain, Airbus Group Innovations, France
  14:30 15:00 1.5.2 THE LAPCAT-MR2 HYPERSONIC CRUISER CONCEPT
J. Steelant¹, T. Langener¹; ¹ESA-ESTEC, Netherlands
  15:00 15:30 1.5.3 LAPCAT-II: DESIGN OF A COMBINED PROPULSION SYSTEM FOR A HYPERSONIC CRUISER
S. Defoort, Onera, France
2.5Flows with strong Vortex effects
Chair: Mauricio Pazini Brandao
Track 2
02.1 - Aerodynamics - CFD Methods and Validation
  14:00 14:30 2.5.1 SIMULATION OF AIRCRAFT WAKE VORTICES DURING LANDING WITH DECAY ENHANCING OBSTACLES
A. Stephan¹, F. Holzäpfel¹, T. Misaka, Tohoku University, Institute of Fluid Science, Japan; ¹Deutsches Zentrum für Luft- und Raumfahrt (DLR), Germany
  14:30 15:00 2.5.2 DYNAMICS OF A VORTEX RING AROUND A MAIN ROTOR HELICOPTER
K. Surmacz, Institute of Aviation, Poland
  15:00 15:30 2.5.3 NUMERICAL INVESTIGATION ON ENGINE INLET DISTORTION UNDER CROSSWIND FOR A COMMERCIAL TRANSPORT AIRCRAFT
K. Liu¹, Y. Sun¹, Y. Zhong¹, H. Zhang¹, K. Zhang, Nanjing University of Aeronautics and Astronautics, China; H. Yang¹; ¹Shanghai Aircraft Design and Research Institute, China
3.5Low Reynolds number flow studies
Chair: Rolf Radespiel
Track 3
02.2 - Experimental Aerodynamics
  14:00 14:30 3.5.1 EFFECT OF ELASTICITY IN THE BIRD-LIKE PRIMARY FEATHER WING ON THE FLIGHT STABILITY
M. Motomatsu, Graduate school of Tokai University, Japan; Y. Inada, Tokai University, Japan
  14:30 15:00 3.5.2 EXPERIMENTAL CHARACTERIZATION OF A FLEXIBLE MEMBRANE FLAPPING-WING IN FORWARD FLIGHT
L.G. Wang¹, B.F. Song¹, W.Q. Yang¹, P. Fu¹; ¹Northwestern Polytechnical University, China
  15:00 15:30 3.5.3 AN EXPERIMENTAL STUDY ON THE INFLUENCE OF PASSIVE DEFORMATION TO LIFT AND THRUST GENERATION IN FLEXIBLE FLAPPING WING
F. Peng¹, S. Bifeng¹, W. Liguang¹; ¹Northwestern Polytechnical University, China
4.5Icing
Chair: Zdobislaw Goraj
Track 4
02.4 - Applied Aerodynamics
  14:00 14:30 4.5.1 THREE-DIMENSIONAL NUMERICAL SIMULATION OF ICE ACCRETION USING A MORPHOGENETIC APPROACH
K. Szilder, Aerospace, National Research Council, Canada
  14:30 15:00 4.5.2 THE INFLUENCE OF ICE ACCRETION ON THE AERODYNAMIC PERFORMENCE OF A UAS AIRFOIL
K. Szilder, National Research Council, Canada
  15:00 15:30 4.5.3 EXPERIMENTAL AND THEORETICAL INVESTIGATIONS OF AIRCRAFT ICING IN THE CASE OF CRYSTAL AND MIXED-PHASE FLOWS
A.B. Miller¹, Y.F. Potapov¹, A.L. Stasenko¹; ¹TsAGI, Russia
5.5CFRP
Chair: Tadashige Ikeda
Track 5
03.1 - Materials issues, Fatigue and Damage Tolerance
  14:00 14:30 5.5.1 SOME LAMINATE DEFORMATIONS FEATURES
Y.I. Dudarkov¹, E.A. Levchenko¹, M.V. Limonin¹; ¹TsAGI, Russia
  14:30 15:00 5.5.2 DESIGN OF A LAMINATED COMPOSITE MULTI-CELL STRUCTURE SUBJECTED TO TORSION
I.C.J. Barbosa¹, M.A.R. Loja¹; ¹GI-MOSM/ISEL, IDMEC/LAETA , Portugal
  15:00 15:30 5.5.3 IMPROVED METHODS FOR MODELLING IMPERFECTIONS FOR BUCKLING ANALYSIS OF COMPOSITE CYLINDRICAL SHELLS
J. Kepple¹, G. Prusty¹, G. Pearce¹, D. Kelly¹, R. Thomson, Cooperative Research Centre for Advanced Composite Structures, Australia; ¹The University of New South Wales, Australia
6.5Structural design 2
Chair: Johannes Schweiger
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  14:00 14:30 6.5.1 EFFICIENT AERO-STRUCTURAL DESIGN OPTIMIZATION BASED ON HIGH-FIDELITY METHODS
Y.T. Zuo¹, Z.H. Gao¹, G. Chen, Xi’ an Jiaotong University, China; ¹Northwestern Polytechnical University, China
  14:30 15:00 6.5.2 STEPS TO FEASIBILITY FOR LAMINAR WING DESIGN IN A MULTIDISCIPLINARY ENVIRONMENT
S. Dähne¹, T. Bach¹, C. Hühne¹; ¹Germen Aerospace Center (DLR), Germany
  15:00 15:30 6.5.3 MAIN BENEFITS OF PRO-COMPOSITE LAYOUTS FOR WING AND FUSELAGE PRIMARY STRUCTURE UNITS
A. Shanygin¹, M. Zichenkov¹, I. Kondakov¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
7.5Nacelles
Chair: Frank Haselbach
Track 7
04 - Propulsion
  14:00 14:30 7.5.1 AERODYNAMIC INLET DESIGN FOR CIVIL AIRCRAFT NACELLE
A.A. Savelyev¹, S.V. Mikhaylov¹, N.A. Zlenko¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
  14:30 15:00 7.5.2 PROGRESS TOWARDS ADAPTIVE AIRCRAFT ENGINE NACELLES
L. da Rocha-Schmidt¹, A. Hermanutz¹, H. Baier¹, A. Seitz², J. Bijewitz², A.T. Isikveren², F. Scarpa³, G. Allegri³, C. Remillat³, E. Feuilloley³, F. Majic*, C. O\'Reilly*, G. Efraimsson*; ¹Technische Universität München, Germany ;²Bauhaus Luftfahrt e.V., Germany ;³University of Bristol, United Kingdom ;*Kungliga Tekniska Högskolan, Sweden
  15:00 15:30 7.5.3 NEW CHALLENGES FOR ENGINE NACELLE COMPARTMENTS PRESSURE AND THERMAL LOADS MANAGEMENT WITH AIRCRAFT ENGINE EVOLUTION
O. Verseux¹, Y. Sommerer¹; ¹Airbus Operation SAS, France
8.5Flight modelling and simulation 2
Chair: John Vian
Track 8
05.1 - Flight Dynamics and Control (Control & Modelling)
  14:00 14:30 8.5.1 SLOSHING MECHANICAL MODEL FOR STABILITY AND HANDLING QUALITIES EVALUATION OF THE C295 AIRCRAFT WITH THE OSD SYSTEM
R. Rodríguez Robles¹, J. Pérez Serrano¹; ¹Airbus Military, Spain
  14:30 15:00 8.5.2 NON-INTRUSIVE FLIGHT TEST INSTRUMENTATION TECHNOLOGIES
H. Abbasi, National Research Council Canada, Canada
  15:00 15:30 8.5.3 WIND TUNNEL INVESTIGATION OF CRITICAL FLIGHT REGIMES USING DYNAMICALLY SCALED ACTIVELY CONTROLLED MODEL IN 3 DOF GIMBAL
I. Grishin¹, A. Khrabrov¹, A. Kolinko¹, M. Sidoryuk¹, A. Vyalkov¹; ¹TsAGI, Russia
9.5Aircraft emission and contrails
Chair: Sigrun Matthes
Track 9
10 - Challenge of the Environment
  14:00 14:30 9.5.1 ECOLOGICAL OPTIMIZATION OF JET AIRCRAFT FLIGHTS IN VIEW OF CONTRAILS AND CONTRAIL CIRRUS FORMATION
V.I. Vid¹, V.T. Dedesh¹, S.N. Kiose¹, R.H. Tenishev¹, E.G. Pavlova¹, R.L. Kagarmanov¹, V.V. Popov¹, G.P. Rumyantseva¹, M.A. Lavrov¹, R.V. Enchilik¹, M.A. Grigoryev¹, A.N. Zamyatin¹, I.V. Voronich, Moscow Institute of Physics and Technology, Russia; A.I. Lanshin², A.A. Evstigneev²; ¹GFRI, Russia ;²Central Institute of Aviation, Russia
  14:30 15:00 9.5.2 A STUDY OF FLOW AND INITIAL STAGE OF WATER CONDENSATION IN THE TWO-PHASE JET-VORTEX WAKE BEHIND A CRUISE AIRCRAFT
M.A. Lobanova, Baltic State Technical University, Russia
10.5Navigation and radar 2
Chair: Tjierry Michal
Track 10
06 - Systems, Subsystems and Equipment
  14:00 14:30 10.5.1 MULTI-FUNCTIONAL AERODROME CONTROL RADAR BY USPR TECHNOLOGY
A.E. Ananenkov¹, A.V. Konovaltsev¹, V.M. Nuzhdin¹, V.V. Rastorguev¹, V.N. Skosyrev, Moscow State Technical University, Russia; ¹Moscow Aviation Institute, Russia
  14:30 15:00 10.5.2 ARTIFICIAL NEURAL NETWORK BASED SIGNAL PROCESSING FOR PERSPECTIVE ONBOARD SYSTEMS
E. Efimov¹, T. Shevgunov¹, A. Valaytite¹, E. Sadovskaya¹; ¹Moscow Aviation Institute (National Research University), Russia
  15:00 15:30 10.5.3 GAN POWER AMPLIFIER FOR ON-BOARD DIGITAL ANTENNA ARRAY
R. Malakhov, The Moscow Aviation Institute (National Research University), Russia
11.5Hypersonic flow applications
Chair: Alexander Kuranov
Track 11
02.1 - Aerodynamics - CFD Methods and Validation
  14:00 14:30 11.5.1 NUMERICAL INVESTIGATION OF FUSELAGE-STABILIZER-CONTROL SURFACE INTERFERENCE FOR A HYPERSONIC WAVERIDER VEHICLE
X.-P. Li¹, W.-P. Song¹, Z.-H. Han¹; ¹Northwestern Polytechnical Universtity, China
  14:30 15:00 11.5.2 MACH NUMBER EFFECT ON THE FLOWFIELD STRUCTURE OF HYPERSONIC GAP FLOWS
L.T.L.C. Paolicchi¹, W.F.N. Santos¹; ¹National Institute for Space Research (INPE), Brazil
  15:00 15:30 11.5.3 THE STUDY OF NONQUILIBRIUM GAS-DYNAMIC PROCESSES IN THE FLOW AROUND BODIES IN THE WIND TUNNEL IT-2M TSAGI
V.A. Levin, Institute of mechanics MSU, Russia
12.5Engine performance
Chair: Sebastien Remy
Track 12
04 - Propulsion
  14:00 14:30 12.5.1 RECOVERY OF HIGH-SPEED AND THROTTLE CHARACTERISTICS TURBOJET ENGINE BASED ON THE EMPIRICAL DATA
G. Veresnikov, IPU, Russia
  14:30 15:00 12.5.2 EVALUATIONS OF PROBLEM AREAS ON CAUSES OF EXCESSIVE FUEL CONSUMPTION FOR TURBOFAN ENGINES
R.C. Chang¹, S. Tan¹; ¹China University of Science and Technology, Taiwan
  15:00 15:30 12.5.3 ANALYSIS OF PROPULSION AND ENERGY SYSTEM’S INFLUENCE ON THE PERFORMANCE OF HIGH ALTITUDE AIRSHIP
S. ChenB. SongH. Wa
1.6Supersonic vehicles
Chair: Kazuhiro Nakahashi
Track 1
01 - Aircraft and Systems Integration
  16:00 16:30 1.6.1 PROPULSION/AIRFRAME INTEGRATION CONSIDERING LOW DRAG AND LOW SONIC BOOM
A. Ueno¹, Y. Watanabe¹; ¹JAXA, Japan
  16:30 17:00 1.6.2 CONCEPTUAL DESIGN STUDY ON LH2 FUELED SST - ENVIRONMENTAL IMPACTS REDUCED BY AIRFRAME/PROPULSION SYSTEM INTEGRATION -
T. Yuhara¹, K. Rinoie, University of Tokyo, Japan; Y. Makino¹; ¹JAXA, Japan
  17:00 17:30 1.6.3 D-SEND#2 FLIGHT DEMONSTRATION FOR LOW SONIC BOOM DESIGN TECHNOLOGY
M. Honda¹, K. Yoshida¹; ¹JAXA, Japan
  17:30 18:00 1.6.4 DEVELOPMENT OF A SMALL-SCALE SUPERSONIC FLIGHT EXPERIMENT VEHICLE AS A FLYING TEST BED
K. Mizobata¹, R. Minato¹, K. Higuchi¹, M. Ueba¹, S. Takagi¹, D. Nakata¹, N. Katsumata¹, K. Higashino¹, N. Tanatsugu¹; ¹Muroran Institute of Technology, Japan
2.6Comparison of CFD with experiments
Chair: Doug Hunter
Track 2
02.1 - Aerodynamics - CFD Methods and Validation
  16:00 16:30 2.6.1 COMPUTER MODELLING TECHNIQUE AERODYNAMIC CHARACTERISTICS MODELLING OF THE STAND WITH LONG-RANGE LARGE DIAMETER AIR JET
N.-A Sidenko, Research-and-development center “CENTRE COMPOSITE” Joint Venture, Latvia
  16:30 17:00 2.6.2 DAHWIN - DIGITAL/ANALOG-HYBRID WIND TUNNEL - FOR INNOVATIVE EFD/CFD INTEGRATION
S. Watanabe¹, S. Kuchi-ishi¹, K. Murakami¹, A. Hashimoto¹, H. Kato¹, K. Yasue¹, H. Saiki², J. Ogino²; ¹JAXA, Japan ;²Ryoyu Systems Co., Ltd., Japan
  17:00 17:30 2.6.3 VERIFICATION OF MODELLING OF FLUID-STRUCTURE INTERACTION (FSI) PROBLEMS BASED ON EXPERIMENTAL RESEARCH OF BLUFF BODY OSCILLATIONS IN FLUIDS
O. Kotsur¹, G. Scheglov, BMSTU, Russia; P. Leyland¹; ¹EPFL, Switzerland
3.6Supersonic flow control
Chair: Chris Atkin
Track 3
02.3 - Basic Fluid Dynamics and Flow Control
  16:00 16:30 3.6.1 DYNAMIC CHARACTERISTICS OF THE THRUST VECTORING CONTROL BY HIGHLY COMPRESSIBLE COANDA EFFECTS
Y. Lee¹, S.H. Park¹, H.B. Chang¹, Y.H. Cho, Seyon Engineering & System Co., South Korea; ¹Korea Aerospace University, South Korea
  16:30 17:00 3.6.2 ARTIFICIAL TURBULIZATION OF THE SUPERSONIC BOUNDARY LAYER BY DIELECTRIC BARRIER DISCHARGE
P.A. Polivanov¹, A.A. Sidorenko¹, A.A. Maslov¹; ¹ITAM SB RAS, Russia
  17:00 17:30 3.6.3 CONTROL OF SONIC BOOM LEVEL BY CRYOGENIC ACTION ON THE PROCESS OF FLOW AROUND THE AIRCRAFT
V.F. Chirkashenko¹, V.M. Fomin¹, A.M. Kharitonov ¹, V.F. Volkov¹; ¹ITAM SB RAS, Russia
  17:30 18:00 3.6.4 INVESTIGATION OF THE OPTICAL PULSING DISCHARGE IN THE SUPERSONIC AIR FLOW
T. Bobarykina, ITAM SB RAS, Russia
4.6Flight vehicle aerodynamics 1
Chair: Fernando Catalono
Track 4
02.4 - Applied Aerodynamics
  16:00 16:30 4.6.1 INNOVATIVE SUPERSONIC TRANSPORT CONFIGURATION BY BIPLANE WING / TWIN-BODY FUSELAGE
W. Yamazaki, Nagaoka University of Technology, Japan; K. Kusunose, Japan Aerospace Exploration Agency, Japan
  16:30 17:00 4.6.2 LEE-SIDE FLOW SIMULATIONS OF CRUCIFORM WING-BODY CONFIGURATIONS AT INCOMPRESSIBLE MACH NUMBERS
J. Versteegh, University of the Witwatersrand, South Africa
  17:00 17:30 4.6.3 THE AERODYNAMIC DESIGN OF THE A350 XWB-900 HIGH LIFT SYSTEM
H. Strüber, Airbus Operations GmbH, Germany
  17:30 18:00 4.6.4 OPTIMISATION OF A NOVEL TRAILING EDGE CONCEPT FOR A HIGH LIFT DEVICE
J.D.M. Botha,, University of the Witwatersrand, South Africa; L. Dala, CSIR, South Africa; S. Schaber, Airbus, Germany
5.6Fatigue and failure
Chair: Frank Abdi
Track 5
03.1 - Materials issues, Fatigue and Damage Tolerance
  16:00 16:30 5.6.1 SMALL CRACKS IN ALUMINUM STRUCTURES UNDER STATIC AND CYCLIC LOADING
V.V. Konovalov¹, A.A. Sviridov¹; ¹TsAGI, Russia
  16:30 17:00 5.6.2 CONSIDERATION OF THE SERVICE LIFE TAKING INTO ACCOUNT A LOT OF ONE-TYPE STRESSED UNIT ELEMENTS
A.V. Pankov¹, I.G. Khlebnikova¹; ¹TsAGI, Russia
  17:00 17:30 5.6.3 THE PRINCIPLES OF FATIGUE APPROVAL FOR TRANSPORT AIRCRAFT AFTER ITS PRINCIPAL STRUCTURE ELEMENTS MODIFICATION
V.I. Kleptsov, Beriev Aircraft Company, Russia
  17:30 18:00 5.6.4 CONTROL OF COMPOSITE MATERIAL CRACK BRANCHING FOR IMPROVED FRACTURE TOUGHNESS
A.C. Orifici, RMIT University, Australia
6.6Structural analysis 1
Chair: Oleg Tolochko
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  16:00 16:30 6.6.1 A METHODICAL APPROACH FOR DYNAMIC SYSTEM ANALYSIS & SYNTHESIS IN THE DIMENSIONING OF VARIANT LIGHTWEIGHT CABIN INTERIOR
B. Plaumann¹, D. Krause¹; ¹TUHH, Institute PKT, Germany
  16:30 17:00 6.6.2 AEROELASTIC OPTIMIZATION OF COMPOSITE WING BASED ON IMPROVED ADAPTIVE GENETIC ALGORITHM
Q. Xiong, CASIC, China; D.-G. Cui, AVIC, China
  17:00 17:30 6.6.3 ASSESSING STRUCTURAL TECHNOLOGY PERFORMANCE FOR THE HYBRID WING BODY THROUGH PROBABILISTIC WEIGHT ESTIMATION
J.A. Corman¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States
  17:30 18:00 6.6.4 ANALYTICAL METHOD FOR LIMIT LOAD CAPACITY CALCULATION OF THIN WALLED AIRCRAFT STRUCTURES
A. Pistek, Brno Univerzity of Technology, Czech Republic
7.6Turbines 2
Chair: Christian Mari
Track 7
04 - Propulsion
  16:00 16:30 7.6.1 ON THE OPTIMAL LOCATION OF BLEED PORTS FOR GAS TURBINE COOLING
A.C. Marta, LAETA, CCTAE, Instituto Superior Técnico, Universidade de Lisboa, Portugal; S. Shankaran, Fluid Mechanics Lab, Global Research Center, General Electric, United States
  16:30 17:00 7.6.2 IMPROVEMENT OF THE DESIGN AND METHODS OF DESIGNING CRITICAL COMPONENTS OF GAS FLOW PATH OF MODULAR AIRCRAFT GAS TURBINE
V.G. Nesterenko¹, A.A. Matushkin¹, V.V. Nesterenko¹; ¹MAI, Russia
  17:00 17:30 7.6.3 AERODYNAMIC DESIGN OF HIGH PERFORMANCES INTER-TURBINE TRANSITION DUCTS
A. Mahallati, National Research Council of Canada, Canada
8.6Flight control 1
Chair: S Ueno
Track 8
05.1 - Flight Dynamics and Control (Control & Modelling)
  16:00 16:30 8.6.1 BOOST-PHASE MISSILE ATTITUDE CONTROLLER DESIGN USING HIGHER-ORDER SLIDING MODES
Y. Lee¹, Y. Kim¹, G. Moon², B.-E. Jun²; ¹Seoul National University, South Korea ;²Agency for Defense Development, South Korea
  16:30 17:00 8.6.2 CONTROL INPUT BLENDING LOGIC WITH AERODYNAMIC CONTROL AND REACTION JET CONTROL
M.-G. Seo¹, C.-H. Lee², M.-J. Tahk¹, J.-I. Lee², B.-E. Jun²; ¹KAIST, South Korea ;²Agency for Defense Development, South Korea
  17:00 17:30 8.6.3 EXTENDED KALMAN FILTER DESIGN USING BEARING AND TIME-TO-GO MEASUREMENT FOR A HOMING MISSILE GUIDANCE
S.W. Shim¹, B.-G. Park², B.-J. Jeon¹, M.-J. Tahk¹, H.H. Kwon²; ¹KAIST, South Korea ;²LIG Nex1, South Korea
  17:30 18:00 8.6.4 SUM-OF-SQUARES BASED STABILITY ANALYSIS FOR SKID-TO-TURN MISSILES WITH THREE-LOOP AUTOPILOT
H.-H. Kwon¹, M.-W. Seo¹, D.-S. Jang¹, H.-L. Choi¹; ¹KAIST, South Korea
9.6Novel fuels - emissions
Chair: Michael Sicard
Track 9
10 - Challenge of the Environment
  16:00 16:30 9.6.1 PERFORMANCE ASSESSMENT OF ALTERNATIVE FUELS AT THE AIR TRANSPORTATION SYSTEM LEVEL
A.A. Okhapkin, Central Aerohydrodynamic Institute, Russia
  16:30 17:00 9.6.2 MODELING STUDY OF POLLUTANT FORMATION IN HOMOGENEOUS METHANE AND SYNGAS FUELED COMBUSTOR
V.E. Kozlov¹, A.M. Starik¹, N.S. Titova¹; ¹Central Institute of Aviation Motors, Russia
  17:00 17:30 9.6.3 PERFORMANCE AND EMISSIONS CHARACTERISTICS OF ALTERNATIVE AVIATION FUELS
W.A. Chishty, National Research Council Canada, Canada
10.6Requirements and specifications
Chair: Dimitri Mavris
Track 10
07 - Systems Engineering and Supply Chain
  16:00 16:30 10.6.1 MISSION PROFILES ANALYSIS: GUIDELINES TO AIRCRAFT ACTUATORS NEW TECHNOLOGY SPECIFICATION
A. Reysset¹, M. Budinger¹, J.-C. Maré¹; ¹Institut Clément Ader, France
  16:30 17:00 10.6.2 QUANTITATIVE FIDELITY MANAGEMENT AND SELECTION OF PHYSICS-BASED MULTIDISCIPLINARY DESIGN ENVIRONMENTS
K.N. Gatian¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States
  17:00 17:30 10.6.3 SELECTION OF AGRICULTURAL AIRCRAFT USING AHP AND TOPSIS METHODS IN FUZZY ENVIRONMENT
G.S. Schwening¹, A.M. Abdalla¹; ¹Escola de Engenharia de São Carlos - Universidade de São Paulo, Brazil
  17:30 18:00 10.6.4 RESEARCH ON TECHNOLOGY READINESS ASSESSMENT MODEL FOR SYSTEM OF SYSTEMS
W. CHENG¹, C. XING¹, H. ZHANG¹, Y. WU¹; ¹Aviation Industry Development Research Center of China (ADR), China
11.6Human factors
Chair: Sidney Dekker
Track 11
09 - Safety and Security
  16:00 16:30 11.6.1 HUMAN FACTORS STUDIES OF AN ADS-B BASED TRAFFIC ALERTING SYSTEM FOR GENERAL AVIATION
S.S. Silva¹, H. Cho¹, R.J. Hansman¹; ¹MIT, United States
  16:30 17:00 11.6.2 MENTAL EFFORT AND SAFETY IN CURVED APPROACHES
J.O. Entzinger¹, T. Uemura¹, S. Suzuki¹; ¹The University of Tokyo, Japan
  17:00 17:30 11.6.3 DEVELOPMENT AND FLIGHT RESEARCH OF NON-INTRUSIVE AIRBORNE SYSTEM OF PILOT PSYCHOPHYSIOLOGICAL STATUS MONITORING
A.D. Mironov¹, A.Y. Nakvasin¹; ¹GROMOV FLIGHT RESEARCH INSTITUTE (LII GROMOV), Russia
  17:30 18:00 11.6.4 SUBJECTIVE FACTORS IN CONTROLLERS' DECISIONS
I. Jankovics, Budapest University of Technology and Economics, Hungary
12.6Combustor
Chair: Michel Desaulty
Track 12
04 - Propulsion
  16:00 16:30 12.6.1 DETAILED RESEARCH ON RICH-LEAN TYPE SINGLE SECTOR AND FULL ANNULAR COMBUSTOR FOR SMALL AIRCRAFT ENGINE
M. MAKIDA¹, H. YAMADA¹, K. SHIMODAIRA¹; ¹Japan Aerospace Exploration Agency, Japan
  16:30 17:00 12.6.2 NUMERICAL AND EXPERIMENTAL INVESTIGATIONS OF LASER IGNITION IN COMBUSTION CHAMBERS
S.G. Rebrov, FSUE Keldysh Research Centre, France; P.V. Kholodov, Moscow Aviation Institute, Russia; G.R. Yakhina, Ecole Centrale de Lyon, France
  17:00 17:30 12.6.3 MECHANISM OF FLAMEHOLDING IN PLASMA-ASSISTED SUPERSONIC COMBUSTOR
S. Leonov, Ohio State University, MAE, Columbus, United States; V. Sabelnikov¹, A. Vincent-Randonnier¹, A. Firsov², D. Yarantsev²; ¹ONERA, the French Aerospace Lab, France ;²Joint Institute for High Temperature RAS, Russia
  17:30 18:00 12.6.4 TECHNOLOGY AND CODE FOR NUMERICAL SIMULATION OF DIFFERENT COMBUSTION TYPES IN HIGH-SPEED VISCOUS GAS TURBULENT FLOWS
A. Shiryaeva, TsAGI, Russia
1.7Innovative concepts 1
Chair: Georges Bridel
Track 1
01 - Aircraft and Systems Integration
  09:30 10:00 1.7.1 MULTIFUNCTIONAL WING MOVEABLES: DESIGN OF THE A350XWB AND THE WAY TO FUTURE CONCEPTS
D. Reckzeh, Airbus, Germany
  10:00 10:30 1.7.2 OPTIMIZATION OF REVENUE SPACE OF A BLENDED WING BODY
J. Fuchte¹, T. Pfeiffer¹, P.D. Ciampa¹, B. Nagel¹, V. Gollnick¹; ¹German Aerospace Center, Germany
  10:30 11:00 1.7.3 RECENT ADVANCES IN AIRFRAME-PROPULSION CONCEPTS WITH DISTRIBUTED PROPULSION
A.T. Isikveren¹, A. Seitz¹, J. Bijewitz¹, M. Hornung¹, A. Mirzoyan², A. Isyanov², J.-L. Godard, ONERA, France; S. Stueckl³, J. van Toor³; ¹Bauhaus Luftfahrt e.V., Germany ;²Central Institute of Aviation Motors, Russia ;³Airbus Group, Germany
  11:00 11:30 1.7.4 AERODYNAMIC ANALYSIS OF THE BWB BUSINESS JET USING DSTRIDUTED PROPULSION SYSTEM
H. Choi, Hanyang Univetsity, South Korea
  11:30 12:00 1.7.5 CONCEPTUAL DESIGN STUDY OF QUAD-BUBBLE-BUSINESS JET
H. Djojodihardjo, Universiti Putra Malysia, Malaysia; M. Anas Bin Abd Bari, Universiti Putra Malaysia, Malaysia
2.7Algorithm development
Chair: Koen de Cock
Track 2
02.1 - Aerodynamics - CFD Methods and Validation
  09:30 10:00 2.7.1 RAPID LARGE-SCALE CARTESIAN MESHING FOR AERODYNAMIC COMPUTATIONS
D. Sasaki, Kanazawa Institute of Technology, Japan; K. Nakahashi, JAXA, Japan
  10:00 10:30 2.7.2 A DEVELOPMENT AND VERIFICATION OF DENSITY BASED SOLVER USING LU-SGS ALGORITHM IN OPENFOAM
J. Kim, Korea Aerospace Research Institute(KARI), South Korea; K. Kim, Seoul National University, South Korea
  10:30 11:00 2.7.3 A MESH ADAPTATION METHOD FOR SIMULATION OF UNSTEADY FLOWS
C.H. Zhou, Nanjing University of Aeronautics and Astronautics, China
  11:00 11:30 2.7.4 MESHLESS METHOD FOR SIMULATION OF COMPRESSIBLE REACTING FLOW
J.Y. Huh¹, K.H. Kim¹, S.Y. Jung, Agency for Defense Development, South Korea; ¹Seoul National University, South Korea
  11:30 12:00 2.7.5 COMPUTATIONAL METHOD FOR STEADY FLOW (RANS) USING ZONAL APPROACH AND ITS IMPLEMENTATION EXPERIENCE FOR SOLUTION OF TASK OF INTERFERENCE ENGINE AND AIRFRAME
K. Anisimov¹, E. Kazhan¹, A. Lysenkov¹; ¹TsAGI, Russia
3.7Boundary layer transition studies
Chair: Herve Consigny
Track 3
02.2 - Experimental Aerodynamics
  09:30 10:00 3.7.1 THE LAMINAR-TURBULENT TRANSITION ZONE IN 2D AND 3D BOUNDARY LAYERS WITH EMPHASIS ON EFFECT OF FREE STREAM TURBULENCE
A.P. Kiselev¹, V.A. Kuzminsky¹, D.S. Sboev¹; ¹TsAGI, Russia
  10:00 10:30 3.7.2 ROUGHNESS EFFECTS ON SWEPT-WING CROSSFLOW TRANSITION IN MODERATE FREE-STREAM TURBULENCE
T.I. Saeed¹, J.F. Morrison¹, M.S. Mughal¹; ¹Imperial College London, United Kingdom
  10:30 11:00 3.7.3 THE ROLE OF LOCALIZED ROUGHNESS ON THE LAMINAR-TURBULENT TRANSITION ON THE OBLIQUE WING
S.N. Tolkachev¹, V.N. Gorev¹, V.V. Kozlov¹; ¹ITAM SB RAS, Russia
  11:00 11:30 3.7.4 LAMINAR-TURBULENT TRANSITION CONTROL BY DIELECTRIC BARRIER DISCHARGE. THEORY AND EXPERIMENT
M.V. Ustinov¹, A.A. Uspensky¹, A.Y. Urusov¹, D.A. Rusianov¹; ¹TsAGI, Russia
  11:30 12:00 3.7.5 APPLICATION OF LIGHT SCATTERING EFFECT IN AERODYNAMIC EXPERIMENT
M.A. Brutyan¹, A.V. Petrov¹, A.V. Potapchik¹; ¹TsAGI, Russia
4.7Hypersonics
Chair: Ivan Egorov
Track 4
02.4 - Applied Aerodynamics
  09:30 10:00 4.7.1 NUMERICAL INVESTIGATIONS ON THE SLENDER AXISYMMETRIC BODIES AERODYNAMICS IN WIDE RANGE OF MACH NUMBERS AND ANGLES OF ATTACK FROM 0° TO 180°
N.V. Voevodenko¹, L.G. Ivanteeva¹, V.J. Lunin¹; ¹TsAGI, Russia
  10:00 10:30 4.7.2 HYPERSONIC AEROTHERMODYNAMICS INVESTIGATION FOR AEROSPACE SYSTEM
Y.I. Khlopkov¹, S.L. Chernyshev¹, Z.Y. Myo Myint², A.Y. Khlopkov²; ¹Central Aerohydrodynamic Institute, Russia ;²Moscow Institute of Physics and Technology, Russia
  10:30 11:00 4.7.3 POTENTIAL USE OF WAVERIDER AND BUSEMANN BIPLANE IN AERODYNAMIC DESIGN OF HIGH-SPEED VEHICLES WITH AIR-BREATHING ENGINES
A.A. Gubanov¹, D.Y. Gusev¹; ¹Central Aerohydrodynamic Institute n.a. Prof. N.E. Zhukovsky, Russia
  11:00 11:30 4.7.4 NUMERICAL INVESTIGATION OF LAMINAR NEAR WAKE SEPARATION ON CIRCULAR CYLINDERS AT SUPERSONIC VELOCITIES
W.S. Hinman¹, C.T. Johansen¹, C.J. Arisman¹, W.C. Galuppo¹; ¹University of Calgary, Canada
  11:30 12:00 4.7.5 HYPERSONIC AERODYNAMIC APPRAISAL OF WINGED BLUNT, RATHER SHARP AND SPATULED BODY RE-ENTRY VEHICLES
A. Viviani, Second University of Naples, Italy; G. Pezzella, Italian Aerospace Research Center, Italy
5.7Materials
Chair: Steven Nutt
Track 5
03.1 - Materials issues, Fatigue and Damage Tolerance
  09:30 10:00 5.7.1 SYNTHESYS OF RADAR ABSORBING MATERIALS FOR STEALTH AIRCRAFT BY USING NANOMATERIALS AND EVOLUTIONARY COMPUTATION
D. Micheli¹, R. Pastore¹, A. Vricella¹, R.-B. Morles¹, M. Marchetti¹; ¹Sapienza University, Italy
  10:00 10:30 5.7.2 CHARACTERISING INTERNAL HEAT TRANSFER IN THERMAL PROTECTION SYSTEMS
N. Banerji¹, P. Leyland¹, S. Haussener¹; ¹Ecole Polytechnique Fédérale de Lausanne, Switzerland
  10:30 11:00 5.7.3 PREPARATION, CHARACTERIZATION AND APPLICATION OF ABRASION-RESISTANT HYBRID COATINGS ON POLYCARBONATE TRANSPARENCIES
Y.-H. CHEN¹, Y. YUAN¹; ¹Beijing Institute of Aeronautical Materials, China
  11:00 11:30 5.7.4 MICROSTRUCTURE AND EVOLUTION OF PORES DURING THE DENSIFICATION CYCLES OF ZRC DOPED CARBON/CARNON COMPOSITES
Z. Chen, Nanjing University of Aeronautics and Astronautics, China
  11:30 12:00 5.7.5 A NEW 3D PROGRESSIVE DAMAGE MODEL FOR COMPOSITE LAMINATES
Z. Ni, Shanghai Aircraft Design and Research Institute, China
6.7Aeroelasticity 1
Chair: Michail Zichenkov
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  09:30 10:00 6.7.1 ON-LINE MONITORING AND FLUTTER SPEED PREDICTION BASED ON IDENTIFICATION OF A TIME-VARYING SYSTEM
J. Ertveldt, Vrije Universiteit Brussel - Dept. MECH, Belgium
  10:00 10:30 6.7.2 AEROELASTIC PREDICTION FOR MISSILE FINS IN SUPERSONIC FLOWS
M.-C. Meijer, University of the Witwatersrand, South Africa
  10:30 11:00 6.7.3 PROXIMITY EFFECTS OF PIEZOELECTRIC ENERGY HARVESTERS IN FLUID FLOW
A Deivasigamani¹, J.M. McCarthy¹, S.J. John¹, S. Watkins¹, F. Coman, FCST Pty. Ltd., Australia; ¹RMIT University, Australia
  11:00 11:30 6.7.4 A SIMPLE APPROACH TO COMPUTATIONAL AEROELASTICITY OF NASA ROTOR 67
R. Wiranegara¹, A. Turan¹; ¹University of Manchester, United Kingdom
  11:30 12:00 6.7.5 NUMERICAL ANALYSIS OF TRANSONIC FLUTTER OF SUPERCRITICAL AIRFOIL OF A BUSINESS JET
Q.Y. Chen, COMAC, China
7.7Open rotor 1
Chair: Aspi Wadia
Track 7
04 - Propulsion
  09:30 10:00 7.7.1 GEOMETRIC VARIABILITY AND ITS INFLUENCE ON STEADY AND UNSTEADY FAN AERODYNAMIC PERFORMANCE
R. Schnell¹, G. Ashcroft¹; ¹DLR, Germany
  10:00 10:30 7.7.2 A STUDY ON AERODYNAMIC DESIGN OF HIGH-EFFICIENCY PROPELLERS AT HIGH-ALTITUDE
J.-H. Xu¹, W.-P. Song¹, W.-Q. Yang¹; ¹Northwestern Polytechnical University, China
  10:30 11:00 7.7.3 RELIABILITY IMPROVEMENT OF ACCESSORY GEARBOX BEVEL DRIVES
E. Kozharinov, Central Institute of Aviation Motors, Russia
  11:00 11:30 7.7.4 MODEL FORM UNCERTAINTY REPRESENTATION TO ENABLE MULTIFIDELITY DESIGN OF ADVANCED CONCEPTS
H.D. Schwartz¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States
  11:30 12:00 7.7.5 A LOW ORDER METHOD FOR CO-AXIAL PROPELLER AND ROTOR PERFORMANCE PREDICTION
P. Beaumier, Onera, France
8.7Flight control 2
Chair: Fulvia Quagliotti
Track 8
05.1 - Flight Dynamics and Control (Control & Modelling)
  09:30 10:00 8.7.1 FLIGHT CONTROL SYSTEMS FOR WIG-CRAFT
A.V. Nebylov, State University of Aerospace Instrumentation, Russia
  10:00 10:30 8.7.2 AERODYNAMICS AND FLIGHT DYNAMICS PROBLEMS OF HIGH SPEED VEHICLES AND WAYS FOR THEIR SOLUTION
A.V. Efremov¹, S.A. Popov¹, I.A. Nikitchenko¹, A.V. Koshelenko¹, Y.V. Tiumentzev¹; ¹Moscow aviation institute, Russia
  10:30 11:00 8.7.3 ENERGY APPROACH FOR AIRCRAFT VELOCITY OPTIMAL CONTROL DESIGN
O.N. Korsun, State Institute of Aviation Systems, Russia; V.P. Harkov, Experimental Enterprise Nauka-Soft, Russia
  11:00 11:30 8.7.4 FLIGHT ENVELOPE EXPANSION VIA ACTIVE CONTROL SOLUTIONS FOR A GENERIC TAILLESS AIRCRAFT
N. Abramov¹, M. Bommanahal², S. Chetty², M. Goman¹, E. Kolesnikov¹, P.V.S. Murthy²; ¹De Montfort University, United Kingdom ;²CSIR-National Aerospace Laboratories, India
  11:30 12:00 8.7.5 PERFORMANCE OF SWITCHING TYPE DATABASE REFERENCED NAVIGATION ALGORITHM USING TERRAIN HEIGHT AND GRAVITY ANOMALY
W. Lee, Seoul Nat'l Univ., South Korea
9.7Multi UAV operations
Chair: Karl Rhein Weston
Track 9
05.2 - Flight Dynamics and Control (UAV related)
  09:30 10:00 9.7.1 REAL-TIME LEADER-FOLLOWER UAV FORMATION FLIGHT BASED ON MODIFIED NONLINEAR GUIDANCE
C. Park¹, H.J. Kim¹, Y. Kim¹; ¹Seoul National University, South Korea
  10:00 10:30 9.7.2 FLEXIBLE FORMATION SHAPE CONTROL BASED ON THE LOCAL INTERACTION AMONG AIR VEHICLES
Y. Inada, Tokai University, Japan
  10:30 11:00 9.7.3 DYNAMICS MODELING AND ROBUST CONTROLLER DESIGN OF THE MULTI-UAV TRANSPORTATION SYSTEM
H.-I. Lee¹, B.-Y. Lee¹, D.-W. Yoo¹, G.-H. Moon¹, M.-J. Tahk¹; ¹KAIST, South Korea
  11:00 11:30 9.7.4 FORMATION FLIGHT OF FIXED-WING UAVS USING ARTIFICIAL POTENTIAL FIELD
Y. Nagao¹, K. Uchiyama¹; ¹Nihon University, Japan
  11:30 12:00 9.7.5 HARDWARE IMPLEMENTATION OF COOPERATIVE AUTONOMOUS COLLISION AVOIDANCE STRATEGY FOR UNMANNED AERIAL VEHICLES
Y.I. Jenie, Delft University of Technology, Faculty of Aerospace Engineering, Netherlands
10.7Actuations and landing gear
Chair: Fu Yongling
Track 10
06 - Systems, Subsystems and Equipment
  09:30 10:00 10.7.1 DYNAMIC NOTCH FILTERING CONTROL FOR FAULT-TOLERANT ACTUATORS OF FLY-BY-WIRE HELICOPTERS
G. Di Rito¹, R. Galatolo¹, E. Denti¹, F. Schettini¹; ¹Università di Pisa - Dip. di Ingegneria Civile ed Industriale, Italy
  10:00 10:30 10.7.2 AN UAV LANDING GEAR SYSTEM ACTUATED THROUGH SMA ACTIVE ELEMENTS
S. Ameduri¹, L. Pellone¹, N. Favaloro¹, M. Ciminello¹; ¹Centro Italiano Ricerche Aerospaziali, Italy
  10:30 11:00 10.7.3 NEW DEVELOPMENTS OF ELECTRICALLY POWERED ELECTROHYDRAULIC AND ELECTROMECHANICAL ACTUATORS FOR THE MORE ELECTRIC AIRCRAFT
I. Ogoltsov¹, S. Samsonovich¹, A. Selivanov¹, A. Alekseenkov¹; ¹Moscow Aviation Institute (National Research University), Russia
  11:00 11:30 10.7.4 RECENT ADVANCES IN ELECTRICAL LANDING GEAR SYSTEMS
P Nevoret, Safran / Messier-Bugatti-Dowty, France
  11:30 12:00 10.7.5 COMBINED SYNTHESIS OF CONTROL LAWS OF THE AIRCRAFT BRAKING ON THE RUNWAY DURING LANDING
O. Kreerenko, Beriev Aircraft Company, Russia; E. Kreerenko, Southern Federal University , Russia
11.7ATM
Chair: Dirk Kuegler
Track 11
08 - Air Transport System Efficiency
  09:30 10:00 11.7.1 4D TRAJECTORY MANAGEMENT SUPPORT IN THE C-SHARE PROJECT
D. Nieuwenhuisen, National Aerospace Laboratory, Netherlands
  10:00 10:30 11.7.2 STOCHASTIC CONFLICT-FREE 4D TRAJECTORY OPTIMIZATION IN THE PRESENCE OF UNCERTAINTY
Y. Matsuno, The University of Tokyo, Japan
  10:30 11:00 11.7.3 ANALYSIS OF AIR TRAFFIC EFFICIENCY USING DYNAMIC PROGRAMMING TRAJECTORY OPTIMIZATION
A. Harada¹, T. Kozuka¹, Y. Miyazawa¹, N.K. Wickramasinghe², M. Brown², Y. Fukuda²; ¹Kyushu University, Japan ;²ENRI Japan, Japan
  11:00 11:30 11.7.4 EUROPEAN AIR NAVIGATION SERVICE PROVIDERS’ EFFICIENCY EVALUATION THROUGH DATA ENVELOPMENT ANALYSIS (DEA)
R.M. Arnaldo Valdés¹, V.F. Gomez Comendador¹, R. Barragán, CRIDA, Spain; L. Perez¹; ¹UPM, Spain
  11:30 12:00 11.7.5 DIFFEREING AIR TRAFFIC CONTROLLER RESPONSES TO SIMILAR TRAJECTORY PREDICTION ERRORS
J. Mercer, San Jose State University / NASA Ames Research Center, United States
12.7History of aeronautics
Chair: Sergey Chernyshev
Track 12
  09:30 10:00 12.7.1 THE CONTRIBUTION OF DIFFERENT COUNTRIES TO AIRPLANE DEVELOPMENT AND MANUFACTURE- PART I. INVENTION OF AIRPLANE
D.A. Sobolev, Institute for the History of Science and Technology, Russia
  10:00 10:30 12.7.2 THE CONTRIBUTION OF DIFFERENT COUNTRIES TO AIRPLANE DEVELOPMENT AND MANUFACTURE - PART II. HOW MANY AIRPLANES WERE THERE?
Y.V. Kuzmin, Institute for the History of Science and Technology, Russia
  10:30 11:00 12.7.3 FROM ST. PETERSBURG TO ZURICH: AERONAUTICAL AND SCIENTIFIC MILESTONES FROM SWISS PERSPECTIVES AROUND THE NAMES BERNOULLI
G. Bridel, Switzerland
  11:00 11:30 12.7.4 CREATING THE MODERN AIRLINER: U.S. GOVERNMENT AND BUSINESS, 1918-2014
F.R. van der Linden, Smithsonian National Air and Space Museum, United States
  11:30 12:00 12.7.5 FIRST AIRFIELDS OF SAINT PETERSBURG - FIRST AIRFIELDS OF RUSSIA
V.V. Lebedev, Institute for History for Science and Technology, Russia
1.8Innovative concepts 2
Chair: Anatoly Bolsunovsky
Track 1
01 - Aircraft and Systems Integration
  14:00 14:30 1.8.1 WING-LOAD CONTROL BASED ON THE \"LEAKY WING\" CONCEPT
W. Stalewski, INSTITUTE of AVIATION, Poland
  14:30 15:00 1.8.2 OPTIMUM AND DESIGN TRENDS OF COMPOUND HELICOPTERS
O. Rand¹, V. Khromov¹; ¹Technion - Israel Institute of Technology, Israel
  15:00 15:30 1.8.3 CONCEPTUAL DESIGN OF A PASSENGER AIRCRAFT FOR AERIAL REFUELING OPERATIONS
G. La Rocca¹, M. Li¹, P.P.M. van der Linden¹, R.J.M. Elmendorp¹; ¹Delft University of Technology, Netherlands
2.8High speed jet flows
Chair: Tatiana A. Lapushkina
Track 2
02.1 - Aerodynamics - CFD Methods and Validation
  14:00 14:30 2.8.1 THE ANALYSIS OF UNDEREXPANDED JET FLOWS FOR HYPERSONIC AEROTHERMODYNAMIC APPLICATIONS
V.V. Riabov, Rivier University, United States
  14:30 15:00 2.8.2 NUMERICAL INVESTIGATION OF LIQUID JET INJECTION INTO A SUPERSONIC CROSSFLOW
L. Haixu¹, G. Yincheng¹, L. Wenyi¹; ¹Tsinghua University, China
  15:00 15:30 2.8.3 NUMERICAL SIMULATIONT OF GAS AND MULTIPHASE SUPERSONIC JETS WITH NON-EQUILIBRIUM PROCESSES
A.M. Molchanov, Moscow Aviation Institute, Russia
3.8Flow structures
Chair: David Philpott
Track 3
02.2 - Experimental Aerodynamics
  14:00 14:30 3.8.1 EXPERIMENTAL INVESTIGATION OF ENDWALL FLOW FIELD, HEAT TRANSFER IN A LINEAR TURBINE BLADE CASCADE WITH CONTOURED ENDWALL
B. Barbieri, University of Pretoria, South Africa
  14:30 15:00 3.8.2 INCOMPRESSIBLE TURBULENT FLOW AT THE LEADING EDGE OF SWEPT WINGS
E.R. Gowree¹, C.J. Atkin¹; ¹City University London, United Kingdom
  15:00 15:30 3.8.3 FLOW STRUCTURE IN THE BASE REGION OF RE-ENTRY VEHICLE WITH SUPERSONIC BRAKING PLUMES IMPINGING WITH LANDING SURFACE
A.A. Dyadkin¹, V.P. Sukhorukov¹, G.A. Trashkov¹, V.F. Volkov², V.I. Zapryagaev², N.P. Kiselev²; ¹Korolev Energiya Rocket and Space Corporation, Russia ;²Khristianovich Institute of Theoretical and Applied Mechanics SB, Russia
4.8Aeroacoustics
Chair: Victor Kopiev
Track 4
02.4 - Applied Aerodynamics
  14:00 14:30 4.8.1 NUMERICAL STUDY OF WIND-TUNNEL ACOUSTIC RESONANCE INDUCED BY TWO-DIMENSIONAL AIRFOIL FLOW AT LOW REYNOLDS NUMBER
T. Ikeda¹, T. Atobe¹, Y. Konishi², H. Nagai², K. Asai²; ¹Japan Aerospace Exploration Agency, Japan ;²Tohoku University, Japan
  14:30 15:00 4.8.2 AERODYNAMIC STUDIES ON LOW-NOISE AIRCRAFT WITH UPPER ENGINE INSTALLATION
A.L. Bolsunovsky¹, N.N. Bragin¹, N.P. Buzoverya¹, I.L. Chernyshev¹, A.K. Ivanyushkin¹, S.I. Skomorohov¹; ¹TsAGI, Russia
  15:00 15:30 4.8.3 AERODYNAMIC NOISE REDUCTION FOR HIGH LIFT DEVICES USING MORPHING FLAP CONCEPT
Y. Tani¹, K. Miyazaki¹, S. Aso¹, H. Ura², T. Ito²; ¹Kyushu University, Japan ;²JAXA, Japan
5.8Health monitoring
Chair:
Track 5
03.1 - Materials issues, Fatigue and Damage Tolerance
  14:00 14:30 5.8.1 NONLINEAR ACOUSTICS FOR HEALTH MONITORING OF COMPOSITE SCARF REPAIRS
L. Pieczonka¹, A. Klepka¹, S. Pavlopoulou², W.J. Staszewski¹, C. Soutis²; ¹AGH University, Poland ;²Manchester University, United Kingdom
  14:30 15:00 5.8.2 DAMAGE IDENTIFICATION USING FIBRE BRAGG GRATING SENSORS EMBEDDED WITHIN A COMPOSITE PLATE
M.H. Safaei, Iran
  15:00 15:30 5.8.3 FATIGUE DAMAGE DETECTION IN LARGE THIN WALL PLATE BASED ON ULTRASONIC GUIDED WAVE BY USING A PIEZOELECTRIC SENSOR NETWORK
B. Alem¹, A. Abedian¹; ¹Sharif university of technology, Iran
6.8Structural analysis 2
Chair: A. Pistek
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  14:00 14:30 6.8.1 POSTBUCKLING ANALYSIS AND OPTIMIZATION OF STIFFENED FUSELAGE PANELS UTILIZING VARIABLE-STIFFNESS LAMINATES
T. Ungwattanapanit¹, H. Baier¹; ¹TU München, Germany
  14:30 15:00 6.8.2 STRENGTH ANALYSIS TECHNIQUE FOR HIGH LOADED ELEMENTS OF COMPOSITE AIRFRAMES
E. Dubovikov¹, V. Fomin¹; ¹TsAGI, Russia
  15:00 15:30 6.8.3 MULTI-OBJECTIVE OPTIMIZATION OF THE COMPOSITE WING BOX OF SOLAR POWERED HALE UAV
G. Romeo¹, F. Danzi¹, E. Cestino¹; ¹Politecnico di Torino, Italy
7.8Open rotor 2
Chair: Phillipe Beaumier
Track 7
04 - Propulsion
  14:00 14:30 7.8.1 ASSESSMENT OF AERODYNAMIC AND ACOUSTIC CHARACTERISTICS OF COUNTER-ROTATING OPEN ROTORS
I. Brailko¹, V. Mileshin¹, A. Rossikhin¹; ¹Central Institute of Aviation Motors, Russia
  14:30 15:00 7.8.2 COMPARISON OF DUCTED AND UNDUCTED COUNTER ROTATING FAN MODEL NOISE
Y. Khaletskiy¹, V. Mileshin¹; ¹Central Institute of Aviation Motors, Russia
8.8Flight dynamic system identification 2
Chair: Min-Jea Tahk
Track 8
05.1 - Flight Dynamics and Control (Control & Modelling)
  14:00 14:30 8.8.1 ITERATIVE LEARNING IDENTIFICATION AGAINST NON-ZERO INITIAL STATES AND ESTIMATION OF AERODYNAMIC DERIVATIVES
A. Fujimori¹, S. Oh-hara¹; ¹University of Yamanashi, Japan
  14:30 15:00 8.8.2 A TIME SERIES MODEL OF ANGLE OF ATTACK AND PITCH RATE FOR A WIDE RANGE OF ALTITUDE AND VELOCITY
N. Yoshitani, TEIKYO UNIVERSITY, Japan
  15:00 15:30 8.8.3 FLIGHT DATA CLASSIFIER FOR EFFECTIVE AIRCRAFT PERFORMANCE ANALYSIS
M. Naruoka, Japan Aerospace Exploration Agency, Japan
9.8UAV control
Chair: Tomasz Goetzendorf-Grabowski
Track 9
05.2 - Flight Dynamics and Control (UAV related)
  14:00 14:30 9.8.1 ON UAV ROBUST NONLINEAR CONTROL IN PRESENCE OF PARAMETRIC UNCERTAINTIES
V.V. Golubev¹, W. MacKunis¹; ¹ERAU, United States
  14:30 15:00 9.8.2 GENERATION OF INITIAL GUESSES FOR OPTIMAL CONTROL PROBLEMS WITH MIXED INTEGER DEPENDENT CONSTRAINTS
M. Rieck¹, M. Richter¹, M. Bittner¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, Germany
  15:00 15:30 9.8.3 L1 ADAPTIVE ATTITUDE CONTROLLER FOR A TAIL-SITTER MAV IN HOVER FLIGHT
J. Wang¹, B. Song¹, L. Wang¹; ¹School of Aeronautics,Northwestern Polytechnical Unversity, China
10.8Fuel systems and fire protection
Chair: Sebastian Remy
Track 10
06 - Systems, Subsystems and Equipment
  14:00 14:30 10.8.1 REDUCTION OF VIBROACOUSTIC LOAD IN AVIATION COMBINED PUMPS
S.A. Gafurov¹, A.B. Prokofiev¹, E.V. Shakhmatov ¹; ¹Samara State Aerospace University (National Research University), Russia
  14:30 15:00 10.8.2 AIR EVOLUTION IN FUEL FLOW UNDER DECREASED PRESSURE CONDITIONS: EXPERIMENTAL STUDIES AND ENGINEERING CODE DEVELOPMENT
E.E. Kitanina, Saint-Petersburg State Technical University, Russia; D.A. Bondarenko, EADS RTO SK LLC, Russia; D. Morrison, Airbus Operations Ltd, United Kingdom
  15:00 15:30 10.8.3 DEVELOPMENT OF A SOLID PROPELLANT GAS GENERATOR (SPGG) SYSTEM FOR FIRE SUPPRESSION IN AVIATION - DESIGN OF AN INJECTOR
E. Richter, EADS Deutschland GmbH, Germany; D. Krause, Otto-Von-Guericke University, Germany
11.8Future concepts
Chair: Colin Meckiff
Track 11
08 - Air Transport System Efficiency
  14:00 14:30 11.8.1 EVALUATION OF OPERATIONS ON AN AIRPORT WITH A CIRCULAR RUNWAY
M. Dupeyrat¹, S. Aubry¹, H. Hesselink², S. Loth, DLR, Germany; A. Remiro, ISDEFE, Spain; P. Schmollgruber¹, R. Verbeek², C. Welman²; ¹ONERA, France ;²NLR, Netherlands
  14:30 15:00 11.8.2 ANALYSES ON A CIVIL AIR TO AIR REFUELING NETWORK IN A TRAFFIC SIMULATION
F. Morscheck, DLR, Germany
  15:00 15:30 11.8.3 MODELING AN OPERATIONS CONCEPT FOR COMMERCIAL AIR-TO-AIR REFUELING BASED ON A VEHICLE ROUTING PROBLEM FORMULATION
M.M. van Lith , TU Delft , Netherlands; H.G. Visser¹, H.S. Hosseini¹; ¹TU Delft, Netherlands
12.8ISABE lectures
Chair:
Track 12
  14:00 14:30 12.8.1 TECHNOLOGIES FOR THE NEXT ENGINE GENERATION
A.R. Wadia, GE Aviation, United States
  14:30 15:00 12.8.2 GEARING UP FOR HIGH VOLUME GTFTM PRODUCTION
J. Henne, MTU, Germany
  15:00 15:30 12.8.3 CHALLENGES IN FAN AND HIGH PRESSURE COMPRESSOR DEVELOPMENT
V. Mileshin, CIAM, Russia
1.9Aircraft design
Chair: Frank Ogilvie
Track 1
01 - Aircraft and Systems Integration
  16:00 16:30 1.9.1 KNOWLEDGE-BASED DESIGN FOR FUTURE COMBAT AIRCRAFT CONCEPTS
R.C Munjulury¹, I. Staack¹, A. Abdalla, USP, Brazil; T. Melin¹, C. Jouannet¹, P. Krus¹; ¹Linköping University, Sweden
  16:30 17:00 1.9.2 CONCEPTUAL AIRCRAFT DESIGN MODEL MANAGEMENT DEMONSTRATED ON A 4TH GENERATION FIGHTER
I. Staack¹, R.C. Munjulury ¹, T. Melin¹, A. Abdalla, University of São Carlos, Brazil; P. Krus¹; ¹Linköping University, Sweden
  17:00 17:30 1.9.3 PASSENGER AIRPLANE CONVERSION TO FREIGHTER
I. Berlowitz, Israel Aerospace Industries, Israel
  17:30 18:00 1.9.4 CONCEPTUAL DESIGN OF THREE ALTERNATIVE CONFIGURATIONS OF NEW-GENERATION 19-SEAT BUSH AIRCRAFT
J.P. Fielding¹, A.J. Stewart¹, G.S. Ji¹, G. Rojas¹; ¹Cranfield University, United Kingdom
2.9High lift
Chair: Mori Mari
Track 2
02.1 - Aerodynamics - CFD Methods and Validation
  16:00 16:30 2.9.1 STUDY OF INSTALLATION EFFECTS ON A HIGH-LIFT WING SECTION IN AN OPEN WIND TUNNEL
L. Tysell, FOI, Sweden
  16:30 17:00 2.9.2 AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM COMPATIBLE WITH A NATURAL LAMINAR FLOW WING WITHIN THE DESIREH PROJECT
H. Strüber, Airbus Operations GmbH, Germany; J. Wild, Deutsches Zentrum für Luft- und Raumfahrt, Germany
  17:00 17:30 2.9.3 NUMERICAL SIMULATION OF UNSTEADY FLOWS AROUND HIGH-LIFT CONFIGURATIONS
S. Bosnyakov¹, I. Kursakov¹, A. Lysenkov¹, S. Mikhaylov¹; ¹TsAGI, Russia
  17:30 18:00 2.9.4 NUMERICAL INVESTIGATION OF AN AILERON HINGE MOMENTS AND EFFECTIVENESS ON A HIGH LIFT WING AIRFOIL
K.A. Makarov¹, A.A. Pavlenko¹; ¹TsAGI, Russia
3.9Hypersonic boundary layer control
Chair: N. Uchiyama
Track 3
02.3 - Basic Fluid Dynamics and Flow Control
  16:00 16:30 3.9.1 LAMINAR FLOW CONTROL OF A HIGH-SPEED BOUNDARY LAYER BY LOCALIZED WALL HEATING OR COOLING
A.V. Fedorov¹, V.G. Soudakov¹, I.V. Egorov¹, A.A. Sidorenko², Y. Gromyko², D. Bountin²; ¹TsAGI, Russia ;²ITAM SB RAS and NSU, Russia
  16:30 17:00 3.9.2 INVESTIGATION OF HEAT FLUX AND EFFUSION/FILM COOLING EFFICIENCY OVER A SHARP CONE SURFACE AT HIGH SUPERSONIC SPEEDS
P.V. Chuvakhov, Central Aerohydrodynamic Institute (TsAGI), Russia
  17:00 17:30 3.9.3 A BLUNTED CONE IN A SUPERSONIC HIGH-ENTHALPY NONEQUILIBRIUM UNDEREXPANDED AIR JET
V.I. Sakharov¹, V.V. Shtapov¹, E.B. Vasilevskiy¹, B.E. Zhestkov¹; ¹TsAGI, Russia
  17:30 18:00 3.9.4 TO THE NON-UNIQUENESS PROBLEM OF HYPERSONIC STEADY-STATE FLOW ON THE BLUNTED BODIES LEADING AGE.
S.M. Drozdov, TsAGI, Russia
4.9Flight vehicle aerodynamics 2
Chair: Henning Strüberg
Track 4
02.4 - Applied Aerodynamics
  16:00 16:30 4.9.1 ARRANGEMENT AND AERODYNAMIC STUDIES FOR LONG-RANGE AIRCRAFT IN “FLYING WING” LAYOUT
A.L. Bolsunovsky¹, N.P. Buzoverya¹, I.L. Chernyshev¹, B.I. Gurevich¹, A.P. Tsyganov¹; ¹TsAGI, Russia
  16:30 17:00 4.9.2 TOWARDS COMPUTATIONAL FLIGHT DYNAMICS OF A PASSENGER JET AIRCRAFT
M. Cristofaro¹, Y. Wang, China Academy of Aerospace Aerodynamics, China; A. Da Ronch¹; ¹University of Southampton, United Kingdom
  17:00 17:30 4.9.3 MISSION ADAPTIVE WING-LET OPTIMIZATION FOR REDUCTING VORTEX DRAG
F.M. Catalano, University of Sao Paulo, Brazil
  17:30 18:00 4.9.4 DEVELOPMENT OF AERODYNAMIC DESIGN PROCESS FOR REUSABLE WINGED SPACE VEHICLE USING OPENVSP
S. Taishi, Tokyo Metropolitan University, Japan
5.9Operational simulation 1
Chair: Stefan Poprawa
Track 5
11 - Operations and Sustainment
  16:00 16:30 5.9.1 PROFIT-BASED NETWORK LEVEL EVALUATION OF AIRCRAFT BLOCK TIMES
M. Schmidt¹, K.O. Plötner¹, A. Seitz¹, A.T. Isikveren¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
  16:30 17:00 5.9.2 SECURING THE SUPPLY CHAIN OF INDUSTRIAL PRODUCTS ON THE BASIS OF THE USE OF MODERN INFORMATION TECHNOLOGIES
Y. Buryak¹, S. Zheltov¹; ¹State Institute of Aviation Systems, Russia
  17:00 17:30 5.9.3 DEVELOPMENT OF INSTRUCTIONS FOR CONTINUING AIRWORTHINESS AND AIRCRAFT LOGISTIC SUPPORT ANALYSIS
A.N. Petrov, Gromov Flight Research Institute, Russia
  17:30 18:00 5.9.4 THE INFLUENCE OF SHM TECHNIQUES ON SCHEDULED MAINTENANCE OF AIRCRAFT COMPOSITE STRUCTURES
X. Chen¹, H. Ren¹, C. Bil¹; ¹RMIT, Australia
6.9Aeroelasticity 2
Chair: S. Kuzmina
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  16:00 16:30 6.9.1 STRUCTURAL NONLINEARITIES SIMULATION ON THE FLUTTER ELECTROMECHANICAL MODELING TEST BENCH
G. Liseykin¹, M. Bogatyrev¹, M. Pronin¹, V. Smyslov¹; ¹TsAGI, Russia
  16:30 17:00 6.9.2 A STUDY ON THE EFFECT OF WEAPON INSTALLATION TO AEROELASTIC CHARACTERISTIC OF FIGHTER AIRCRAFT WING
R. Adhy Sasongko, Institut Teknologi Bandung, Indonesia
  17:00 17:30 6.9.3 FLUTTER CALCULATIONS AND TRANSONIC WIND TUNNEL TESTING OF DYNAMICALLY SCALED MODEL OF THE HIGH-ASPECT-RATIO WING
Y.A. Azarov¹, G.V. Liseykin¹, M.A. Pronin¹, O.A. Orlova¹; ¹TsAGI, Russia
  17:30 18:00 6.9.4 AIRLINERS CONTROL SYSTEMS AUTOMATION FUNCTIONS ENCHANCEMENT IN BEHALF OF AIRPLANE STRUCTURAL STRENGTH
V.K. Svyatodukh¹, D.E. Lopanitsyn¹, A.S. Ustinov¹; ¹TsAGI, Russia
7.9Fans
Chair: Sergey Pankov
Track 7
04 - Propulsion
  16:00 16:30 7.9.1 FAR-FIELD FAN NOISE ESTIMATION WITH THE APPLICATION OF 3D AEROACOUSTIC CALCULATION
A.A. Rossikhin¹, Y.D. Khaletskiy, Central Institute of Aviation Motors , Russia; V.I. Mileshin¹; ¹Central Institute of Aviation Motors, Russia
  16:30 17:00 7.9.2 USING WAVES TO SIMULATE DISTORTION IN INTERNAL FLOWS IN AN AXIAL FLOW FAN
K. Prashant¹, R. Bhaskar¹; ¹Indian Institute of Technology Bombay, India
  17:00 17:30 7.9.3 DYNAMIC LOADS ACTING ON ENGINE FRAME ELEMENTS AFTER FAN BLADE OUT EVENT STUDY
I.I. Ivanov¹, B.S. Blinnik¹; ¹Central Institute of Aviation Motors, Russia
  17:30 18:00 7.9.4 NUMERICAL AND EXPERIMENTAL INVESTIGATIONS BYPASS-FLOW FANS FOR AN ADVANCED CIVIL AIRCRAFT ENGINE
S.V. Pankov¹, V.I. Mileshin¹, V.N. Korzhnev¹; ¹Central Institute of Aviation Motors, Russia
8.9Flight control 3
Chair: Sergey Bazhenov
Track 8
05.1 - Flight Dynamics and Control (Control & Modelling)
  16:00 16:30 8.9.1 SIMULATION OF ON-BOARD MODEL OF AIRLINER TO EVALUATE CAPABILITY OF TRAJECTORIES AND FLIGHT SAFETY
S.G. Bazhen
  16:30 17:00 8.9.2 ON THE COMPENSATION AND DAMPING OF ROLL INDUCED BY WAKE VORTICES
L.M.B.C. Campos, Instituto Superior Técnico, Portugal; J.M.G. Marques, Universidade Lusófona de Humanidades e Tecnologias, Portugal
  17:00 17:30 8.9.3 ATTITUDE PROTECTION FOR SIDE STICK-OPERATED AIRCRAFT - THE CLASSIC APPROACH
Y.Q. Dong¹, L.D. Zhang¹, J.L. Ai¹; ¹Fudan University, China
  17:30 18:00 8.9.4 SYNTHESIS OF AIRCRAFT MOTION CONTROL LAWS USING AGGREGATIVE CONTROLLER ANALYTICAL DESIGN PROCEDURE DURING AUTOMATIC IN-FLIGHT REFUELING
S.P. Kostukov, Beriev Aircraft Company, Russia
9.9Noise abating trajectory optimization
Chair: Dirk Kuegler
Track 9
10 - Challenge of the Environment
  16:00 16:30 9.9.1 NOISE ABATEMENT PATH PLANNING USING VIRTUAL FORCES
H.M.J Kuijpers, TU Delft , Netherlands; H.G. Visser, TU Delft, Netherlands
  16:30 17:00 9.9.2 A NON-COOPERATIVE BI-LEVEL OPTIMAL CONTROL PROBLEM FORMULATION FOR NOISE MINIMAL DEPARTURE TRAJECTORIES
M. Richter¹, M. Bittner¹, M. Rieck¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, TUM, Germany
  17:00 17:30 9.9.3 MULTI-OBJECTIVE TRAJECTORY OPTIMIZATION TO REDUCE AIRCRAFT EMISSIONS IN CASE OF UNFORESEEN WEATHER EVENTS
G. Serafino, Università degli studi di trieste; Selex ES, Italy
  17:30 18:00 9.9.4 A QUASI-REAL-TIME GROUND-BASED TRAJECTORY OPTIMIZATION TOOL FOR GREENER OPERATIONS
M. Micallef¹, K. Chircop¹, D. Zammit-Mangion¹, A. Sammut¹, M. Xuereb¹, A. Muscat, Qu Aero Ltd., Malta; ¹University of Malta, Malta
10.9Design applications and manufacturing
Chair: Ces Bil
Track 10
07 - Systems Engineering and Supply Chain
  16:00 16:30 10.9.1 USING BCIS (BRAIN COMPUTER INTERFACES) TO EVALUATE EMOTIONAL PERCEPTION OF PASSENGER CABIN DESIGN IN VIRTUAL ENVIRONMENTS
F. De Crescenzio¹, F. Lucchi¹, N. Mezannar¹, F. Persiani¹; ¹University of Bologna, Italy
  16:30 17:00 10.9.2 NUMERICAL SIMULATIONS AND EXPERIMENTS ON THE INJECTION MOLDING OF AIRCRAFT TRANSPARENCIES
T. WangY. YanL.
  17:00 17:30 10.9.3 UNIFIED TOOLS OF DEVELOPMENT OF THE ONBOARD EQUIPMENT BASED ON THE INTEGRATED MODULAR AVIONICS
I.V. Koverninskiy¹, A.V. Kan¹; ¹FSUE GosNIIAS, Russia
11.9Ice and water impact on safety
Chair: John Hansmann
Track 11
09 - Safety and Security
  16:00 16:30 11.9.1 SPINNER SHED ICE ENGINE INGESTION ASSESSMENT METHODOLOGY
L.P. Ruiz-Calavera¹, S. Cid-Arroyo¹, L. Benitez-Montañes¹; ¹Airbus Defense and Space, Spain
  16:30 17:00 11.9.2 INVESTIGATION OF ICING EFFECTS ON AERODYNAMIC CHARACTERISTICS OF AIRCRAFT AT TSAGI
G.T. Andreev¹, V.V. Bogatyrev¹; ¹TsAGI, Russia
  17:00 17:30 11.9.3 AIRCRAFT ICING IN FLIGHT: EFFECTS OF IMPACT OF SUPERCOOLED LARGE DROPLETS
E. Norde¹, J.M. Hospers¹, E. van der Weide¹, H.W.M. Hoeijmakers¹; ¹University of Twente, Netherlands
  17:30 18:00 11.9.4 EXTREME INFLUENCE OF ENVIRONMENT AND RISKS OF THE FLIGHT SAFETY DEGRADATION DUE TO THE CHANGE OF THE A/C T/O-AND-L PERF
L. Malysheva, Moscow State Technical University of Civil Aviation, Russia
12.9Education and training
Chair: Vladimir Zhuralev
Track 12
01 - Aircraft and Systems Integration
  16:00 16:30 12.9.1 LEARNING FROM THE DESIGN METHODOLOGY OF FAMOUS AEROSPACE INNOVATORS
E. Kroll¹, I. Farbman¹; ¹Technion, Israel
  16:30 17:00 12.9.2 AIRCADIA - AN INTERACTIVE TOOL FOR THE COMPOSITION AND EXPLORATION OF AIRCRAFT COMPUTATIONAL STUDIES AT EARLY DESIGN STAGE
M.D. Guenov¹, M. Nunez¹, A. Molina-Cristobal¹, V.C. Datta¹, A. Riaz¹; ¹Cranfield University, United Kingdom
  17:00 17:30 12.9.3 DOCTORAL PROGRAMS AND TRAINING: EUROPEAN PERSPECTIVES
F. Quagliotti, Politecnico di Torino, Italy
1.10UAS 1
Chair: Anders Blom
Track 1
01 - Aircraft and Systems Integration
  10:00 10:30 1.10.1 A PARAMETRIC STUDY OF THE DEPLOYABLE WING AIRPLANE FOR MARS EXPLORATION
K. Fujita, Tohoku University, Japan
  10:30 11:00 1.10.2 LONG ENDURANCE ELECTRIC UAV FOR CIVILIAN SURVEILLANCE MISSIONS
A.C. Marta, LAETA, CCTAE, Instituto Superior Técnico, Universidade de Lisboa, Portugal; P.V. Gamboa, Aerospace Sciences Department, Universidade da Beira Interior, Portugal
  11:00 11:30 1.10.3 A GENERAL DESIGN METHODOLOGY FOR YEAR-ROUND SOLAR-POWERED STRATOSPHERIC UAVS FROM LOW TO MIDDLE LATITUDES
M. Chang¹, Z. Zhou¹, R. Wang¹, X.-P. Xu¹; ¹NWPU, China
  11:30 12:00 1.10.4 CONCEPTUAL DESIGN OF SOLAR UAV FOR LONG ENDURANCE
N. Arai¹, W. Harasani, King Abdulaziz University, Saudi Arabia; K. Hiraoka¹; ¹Tokai University, Japan
  12:00 12:30 1.10.5 THE JOINED WING SCALED DEMONSTRATOR RESULTS OF CFD
A. Dziubinski¹, S. Kuprianowicz¹, K. Surmacz¹, C. Galinski¹, J. Zóltak¹; ¹Instytut Lotnictwa, Poland
2.10Turbulence modelling
Chair: Francisco J. Souza
Track 2
02.1 - Aerodynamics - CFD Methods and Validation
  10:00 10:30 2.10.1 IMPLEMENTATION OF EARSM TURBULENCE MODEL WITHIN DISCONTINUOUS GALERKIN METHOD
A.I. Troshin¹, V.V. Vlasenko¹, A.V. Wolkov¹; ¹TsAGI, Russia
  10:30 11:00 2.10.2 CONVERGENCE OF CALCULATED TRANSITION LOCI DURING COMPUTATIONAL ANALYSIS OF TRANSONIC AEROFOILS AND INFINITE SWEPT WINGS
C.J. Atkin, City University, United Kingdom
  11:00 11:30 2.10.3 APPLICATION OF SCALE ADAPTIVE SIMULATION BASED ON K-(OMEGA) SST TURBULENCE MODEL
X.Y. Wang¹, D. Li¹; ¹Northwestern Polytechnical University, China
  11:30 12:00 2.10.4 UNSTEADY FLOW OVER A SD7003 AIRFOIL AT LOW REYNOLDS NUMBERS USING A HIGH-ORDER ACCURATE FLUX RECONSTRUCTION SCHEME
V. Skarolek¹, K. Miyaji¹; ¹Yokohama National University, Japan
  12:00 12:30 2.10.5 LARGE EDDY SIMULATIONS OF TURBULENT FLOWS WITH ADVERSE PRESSURE GRADIENTS
A.B. Jesus¹, L.A.C.A. Schiavo¹, J.L.F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil; W.R. Wolf, Universidade Estadual de Campinas, Brazil; ¹Instituto Tecnológico de Aeronáutica, Brazil
3.10Boundary layer instability and transition
Chair: Stephen Rolston
Track 3
02.3 - Basic Fluid Dynamics and Flow Control
  10:00 10:30 3.10.1 THE EFFECTS OF NONLINEARITY ON CROSSFLOW RECEPTIVITY
C. Thomas¹, P. Hall¹, C. Davies, Cardiff University, United Kingdom; ¹Imperial College, United Kingdom
  10:30 11:00 3.10.2 TRANSMISSION COEFFICIENT OF TOLLMIEN-SCHLICHTING WAVES UNDERGOING SMALL INDENTATION/HUMP DISTORTION
H. Xu¹, S. Sherwin¹, P. Hall, Department of Mathematics, Imperial College London, United Kingdom; ¹Department of Aeronautics, Imperial College London, United Kingdom
  11:00 11:30 3.10.3 THEORETICAL MODELING OF THE ELECTROGASDYNAMIC METHOD OF LAMINAR FLOW CONTROL ON A SWEPT WING
S.L. Chernyshev¹, A.P. Kuryachii¹, S.V. Manuilovich ¹, D.A. Rusyanov¹, M.D. Gamirullin¹; ¹Central Aerohydrodynamic Institute, Russia
  11:30 12:00 3.10.4 INFLUENCE OF SMALL SPATIAL PERTURBATIONS OF SUPERSONIC FLOW VELOCITY ON THE HEAT FLUX TO THE CYLINDER SURFACE
I.V. Egorov, TsAGI, Russia
  12:00 12:30 3.10.5 SEPARATED LAMINAR SHEAR LAYER TRANSITION OVER A TWO-DIMENSIONAL BUMP
Y.-L. Ba¹, C. Pan¹, J.-J. Wang¹; ¹Beijing University of Aeronautics and Astronautics, China
4.10Student final
Chair:
Track 4
5.10Structural assessment techniques
Chair: Dieter Hachenberg
Track 5
03.1 - Materials issues, Fatigue and Damage Tolerance
  10:00 10:30 5.10.1 INTRODUCING RESIDUAL STRESSES IN THIN ALUMINIUM STRUCTURES BY LASER GENERATED TEMPERATURE FIELDS
A. Groth¹, N. Kashaev¹, N. Huber¹; ¹Helmholtz-Zentrum Geesthacht, Germany
  10:30 11:00 5.10.2 THE COOLING GRADIENT AND MICROSTRUCTURE CONTROL IN LASER BEAM WELDED TIAL ALLOY ASSISTED BY TEMPERATURE FIELD SIMULATION
J. Liu¹, P. Staron¹, D. Schnubel¹, N. Schell¹, N. Huber¹, N. Kashaev¹; ¹Helmholtz-Zentrum Geesthacht, Germany
  11:00 11:30 5.10.3 X-RAY COMPUTER TOMOGRAPHY INVESTIGATION FOR POLYMER COMPOSITE MATERIAL UNDER THE STATIC LOAD
S. Vasiliev¹, A. Artemiev¹, S. Jurgenson¹; ¹MAI, Russia
  11:30 12:00 5.10.4 RELATIONSHIP BETWEEN POROSITY INSIDE CFRP SPECIMEN AND RESOLUTION OF MICRO X-RAY CT
Y. Morimoto¹, N. Kishimoto¹; ¹Setsunan Univ., Japan
  12:00 12:30 5.10.5 OWN SPECTRUM BANDS OF MECHANICAL SYSTEMS
I. Ovchinnikov, Bauman Moscow State Technical University, Russia
6.10Aeroelasticity 3
Chair:
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  10:00 10:30 6.10.1 AIRWORTHINESS INVESTIGATION OF A HIGHLY NONPLANAR FLEXIBLE WING CONCEPT
K. Seywald¹, F. Hellmundt¹, A. Wildschek¹, F. Holzapfel, TUM, Germany; ¹Airbus Group Innovations, Germany
  10:30 11:00 6.10.2 NONLINEARITIES AND UNCERTAINTIES OF AEROELASTICITY CHARACTERISTICS IN AIRCRAFT DESIGN AND CERTIFICATION
M. Zichenkov¹, F. Ishmuratov¹; ¹TsAGI, Russia
  11:00 11:30 6.10.3 AEROELASTIC BEHAVIOR OF COMPOSITE WINGS IN POSTBUCKLING REGIME
L.C. de Oliveira¹, R. Degenhardt¹, T. Klimmek¹; ¹DLR, Germany
  11:30 12:00 6.10.4 AEROELASTIC RESPONSE SIMULATION FOR DIFFERENT EXCITATION TECHNIQUES IN FLIGHT FLUTTER TEST OF MODERN CIVIL
F. Yang, Shanghai Aircraft Design and Research Institute of COMAC, China; J. Xie, Civil Aviation University of China, China
  12:00 12:30 6.10.5 NUMERICAL SIMULATION AND PARAMETRIC STUDY OF SUPERSONIC WING FLUTTER
M.M. Entezari¹, M. Mohammadi-Amin¹, M.M. Alishahi, Shiraz University, Iran; ¹Astronautics Research Institute, Iran
7.10Nozzles and ducts 1
Chair: Jin Soo Cho
Track 7
04 - Propulsion
  10:00 10:30 7.10.1 EXPERIMENTAL STUDY OF SYNTHETIC JETS FOR THE CONTROL OF FLOWS SEPARATION IN THE ENGINE'S DUCTS
V.A. Stepanov¹, A.Y. Makarov¹, V.P. Maslov¹; ¹CIAM, Russia
  10:30 11:00 7.10.2 GEOMETRIC AND FLOW PARAMETERS EFFECTING THE AERO-THERMAL PERFORMANCE OF TURBOFAN FORCED MIXERS
A. Mahallati, National Research Council of Canada, Canada
  11:00 11:30 7.10.3 AERODYNAMIC DESIGN OF SINGLE-EXPANSION-RAMP NOZZLE FOR AIRCRAFT WITH SUPERSONIC CRUISE SPEED OF FLIGHT
A.V. Shenkin¹, A.P. Mazurov¹, A.P. Bykov¹; ¹TsAGI, Russia
  11:30 12:00 7.10.4 NUMERICAL INVESTIGATION OF CHARACTIRISTICS OF DUAL-CIRCUIT NOZZLES WITH CONSIDERING THE EXTERNAL FLOW
M.B. Guzairov¹, I.A. Krivosheev¹, D.A. Akhmedzyanov¹, A.E. Kishalov¹, K.V. Markina¹; ¹Ufa State Aviation Technical University, Russia
  12:00 12:30 7.10.5 SUPERSONIC NOZZLE THRUST AUGMENTATION
S.A. Takovitskii, TsAGI, Russia
8.10Flight optimization 1
Chair: Takeshi Tsuchiya
Track 8
05.1 - Flight Dynamics and Control (Control & Modelling)
  10:00 10:30 8.10.1 TRAJECTORY SIMULATION AND OPTIMIZATION OF THE LAPCAT-MR2 HYPERSONIC CRUISER CONCEPT
T. Langener¹, S. Erb¹, J. Steelant¹; ¹ESA, Netherlands
  10:30 11:00 8.10.2 REAL-TIME AIRCRAFT CONTINUOUS DESCENT TRAJECTORY OPTIMIZATION WITH ATC TIME CONSTRAINTS USING DIRECT COLLOCATION METHODS
R. Verhoeven¹, R. Dalmau², X. Prats², N. de Gelder¹; ¹NLR, Netherlands ;²UPC, Spain
  11:00 11:30 8.10.3 THROUGH OPTIMIZATION OF A WINGED BOOSTER TRAJECTORY OF REUSABLE AEROSPACE SYSTEM AND PECULIARITIES OF ITS FLIGHT TRY-OUT
A.S. Filatyev¹, O.V. Yanova¹, N.N. Ryabukha, Gromov Flight Research Institute (FRI), Russia; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
  11:30 12:00 8.10.4 NEW PERIODIC SOLUTIONS IN THE AIRCRAFT MAXIMUM RANGE PROBLEM
A.E. Sagalakov¹, A.S. Filatyev¹; ¹Central Aerohydrodynamic institute (TsAGI), Russia
  12:00 12:30 8.10.5 CRUISE FLIGHT THROTTLE OPTIMIZATION BY APPROXIMATE DYNAMIC PROGRAMMING
M. Dobrovinsky¹, J. Z. Ben-Asher¹; ¹Technion, Israel
9.10Ecodesign
Chair: Jeanne Yu
Track 9
10 - Challenge of the Environment
  10:00 10:30 9.10.1 CONCEPTUAL AIRCRAFT DESIGN BASED ON LIFE CYCLE ASSESSMENT
A. Johanning¹, D. Scholz¹; ¹Hamburg University of Applied Sciences, Germany
  10:30 11:00 9.10.2 HYDRAULIC SYSTEM NOISE REDUCTION BY A COMBINED CONSIDERATION OF FLUID BORNE NOISE AND STRUCTURE BORNE NOISE
A. Waitschat¹, V. Pommier-Budinger, Institut Supérieur de l\'Aéronautique et de l\'Espace , France; F. Thielecke¹; ¹Hamburg University of Technology, Germany
  11:00 11:30 9.10.3 ON SOUND ABSORPTION BY AN ACOUSTIC LINER WITH BIAS FLOW
C. Legendre, Free Field Technologies, Belgium; L.M.B.C. Campos, Instituto Superior Tecnico, Portugal
10.10Simulation of systems and sub-systems
Chair: Michel Ravachoz
Track 10
06 - Systems, Subsystems and Equipment
  10:00 10:30 10.10.1 RESEARCH ON INTEGRATION OF VAPOR CYCLE/LIQUID-COOLED REFRIGERATION SYSTEM FOR HELICOPTERS
L. Hu, Nanjing Engineering Institute of Aircraft Systems,AVIC, China
  10:30 11:00 10.10.2 OPTIMIZATION OF ADSORPTION-BASED DEHUMIDIFICATION DEVICES FOR FUEL-TANK INERTING APPLICATIONS
R. Trott, EADS Innovation Works Germany, Germany
  11:00 11:30 10.10.3 HEAT EXCHANGER THERMAL STRATIFICATION MODEL
C.Y. Nakashima¹, L. Tobaldini Neto¹; ¹Embraer, Brazil
  11:30 12:00 10.10.4 MODELING, SIMULATION AND VALIDATION OF A BLEED SYSTEM MODEL
C.Y. Nakashima, Embraer, Brazil
  12:00 12:30 10.10.5 THE EFFECT OF THE HUMIDITY ON THE CORRECTION COEFFICIENT OF THE SONIC THERMOCOUPLE USED IN AVIATION
Q. Yuwu¹, Z. Ning¹, Z. Xingmin¹; ¹Xi’an Aero-engine ( Group ) Ltd., China
11.10Safety and security enhancement
Chair: Carmine Cifuldi
Track 11
09 - Safety and Security
  10:00 10:30 11.10.1 INCIDENT PREDICTION USING SUBSET SIMULATION
C. Wang¹, L. Drees¹, F. Holzapfel¹; ¹Technische Universität München - Inst. of Flight System Dynamics, Germany
  10:30 11:00 11.10.2 FE-TO-SPH APPROACH APPLIED TO THE ANALYSIS OF SOFT BODY IMPACT: BIRD STRIKE AND HAIL IMPACT
A. Prato¹, M. Anghileri¹, A. Milanese¹, L.M.L. Castelletti¹; ¹Politecnico di Milano, Italy
  11:00 11:30 11.10.3 SUPPRESSION EFFECTIVENESS OF WATER MIST ON ACCIDENTAL AIRCRAFT FIRES
A. Yoshida¹, W. Ebina¹, T. Okawa¹; ¹Tokyo Denki University, Japan
  11:30 12:00 11.10.4 USING LINEAR SHAPED CHARGE(LSC) TO FORM BAILOUT EMERGENCY EXIT
F. Wenchun¹, S. Wenjuan¹; ¹First Aircraft Institute, China
  12:00 12:30 11.10.5 NOTES TRAINING IN ATM – A NEW APPROACH USING COMPUTER-BASED SIMULATION METHODS: RESEARCH METHODS
C.M. Muehlethaler¹, C.P. Knecht¹; ¹Centre for Aviation, Zurich University of Applied Sciences, Switzerland
12.10Fundamental Problems of Aeronautics
Chair: Sergey Chernyshev
Track 12
  10:00 10:30 12.10.1 FINIT DIFFERENCE MODELS FOR MECHANICS OF CONTINIUA, PROBLEM OF ACCURACY AND DOMAIN OF APPLICABILITY
S.K. Godunov, Institute of Mathematics, Siberian Department of Russian Academ, Russia
  10:30 11:00 12.10.2 CFD FOR ROTORCRAFT – RECENT PROGRESS AND NEW CHALLENGES WITH THE GOAHEAD CASE
G.N. Barakos¹, R. Steijl¹, M. Woodgate¹; ¹School of Engineering - The University of Liverpool, United Kingdom
  11:00 11:30 12.10.3 EXTREMELY HIGH ORDER AND HIGH RESOLUTION MULTIOPERATORS – BASED SCHEMES FOR CFD APPLICATIONS
A.I. Tolstykh, Dorodnicyn Computing Center of Russian Academy of Sciences, Russia
  11:30 12:00 12.10.4 SHOCK WAVE BOUNDARY LAYER INTERACTION PROCESSES. BUFFET CONTROL METHODS
I.I. Lipatov¹, R.J. Tugazakov¹, F.T. Vihn¹; ¹TsAGI, Russia
  12:00 12:30 12.10.5 PROTECTION PROBLEM FOR THIN-WALLED COMPOSITE CONSTRUCTIONS OF AIRCRAFT FROM ACTION OF RADIATIONS AND PARTICLES FLUXES
A.V. Ostrik, Institute of Problems of Chemical Physics RAS, Russia; V.N. Bakulin, Institute of Applied Mechanics RAS, Russia; A.M. Matveenko, Moscow Aviation Institute, Russia
1.11UAS 2
Chair: Seiya Ueno
Track 1
01 - Aircraft and Systems Integration
  14:00 14:30 1.11.1 INVERTED JOINED WING SCALED DEMONSTRATOR PROGRAMME
C. Galinski, Instytut Lotnictwa, Poland; J. Hajduk, Instytut Techniczny Wojsk Lotniczych, Poland; M. Kalinowski, Politechnika Warszawska, Poland; M. Wichulski¹, L. Stefanek¹; ¹MSP, Poland
  14:30 15:00 1.11.2 A SPECIALIZED UAV FOR SURVEILLANCE IN WINDY, TURBULENT ENVIRONMENT OF THE ANTARCTIC COAST
Z.-J. Goraj, Warsaw University of Technology, Poland
  15:00 15:30 1.11.3 DESIGN AND EXPERIMENT OF TWO-ROTORED UAV CYCLOCOPTER
C.H. Lee¹, S.Y. Min², J.W. Lee², S.J. Kim¹; ¹Seoul National University, South Korea ;²Korea Aerospace Research Institute, South Korea
2.11Computational aeroacoustics
Chair: J W Delfs
Track 2
02.1 - Aerodynamics - CFD Methods and Validation
  14:00 14:30 2.11.1 FRAMEWORK FOR LOW-NOISE WIND TURBINE BLADE DESIGN
S.S. Rodrigues¹, A.C. Marta¹; ¹LAETA, CCTAE, Instituto Superior Técnico, Universidade de Lisboa, Portugal
  14:30 15:00 2.11.2 EFFICIENT JET NOISE PREDICTION USING SYNTHETIC EDDY METHOD AND BLOCK-STRUCTURED CARTESIAN MESH
Y. Fukushima, Institute of Fluid Science, Tohoku University, Japan
  15:00 15:30 2.11.3 RESEARCH ON CORRECTIONS OF CFD SIMULATION TECHNIQUE FOR COMPLEX SHAPED CAVITY FLOW BASED ON THE WIND TUNNEL TEST DATA
H.H. Huang Hu¹, J.W. Jin Wei¹, F.H.B. Fu Huanbing¹; ¹CADI 611, China
3.11New analysis / phenomena 2
Chair: I. Lipatov
Track 3
02.3 - Basic Fluid Dynamics and Flow Control
  14:00 14:30 3.11.1 SINGULARITIES IN LAMINAR BOUNDARY LAYER AND FLOW STRUCTURE NEAR SINK PLANE ON CONICAL BODIES
V.I. Shalaev, Moscow Institute of Physics and technology, Russia
  14:30 15:00 3.11.2 PHYSICS PHENOMENA ACCOMPANIED STREAMLINING OF A BODY BY THE GAS-PARICLE SUPERSONIC JET
A.L. Stasenko¹, G.V. Molleson¹; ¹TsAGI, Russia
  15:00 15:30 3.11.3 EXISTENCE CRITERIA OF NON-VISCOUS VORTICAL STRUCTURES IN SHOCK LAYERS OF CONICAL GAS FLOWS
F. Maksimov, Institute of Computer Aided Design, Russian Academy of Sciences, Russia
4.11Optimization
Chair: Bennie Broughton
Track 4
02.4 - Applied Aerodynamics
  14:00 14:30 4.11.1 MULTI OBJECTIVE OPTIMIZATION OF TRANSONIC AIRFOIL USING CST METHODOLOGY WITH GENERAL AND EVOLVED SUPERCRITICAL CLASS FUNCTION
P.S. Palar, The University of Tokyo, Japan
5.11Operational simulation 2
Chair: Matthias Meyer
Track 5
11 - Operations and Sustainment
  14:00 14:30 5.11.1 INNOVATIVE TECHNOLOGIES AND VIDEO CONFERENCE SYSTEMS IN TECHNOLOGICAL PROCESS OF AIRCRAFT ENGINE PRODUCTION
A.M. Kachalin, Moscow Aviation Institute, Russia
  14:30 15:00 5.11.2 UAV BASED ADVANCED MONITORING SYSTEM: FLEET AND LOGISTIC SYSTEM SIZING BY OBJECT-BASED MODEL AND MONTE-CARLO SIMULATION
S. Chiesa¹, M. Fioriti¹, R. Fusaro¹; ¹Politecnico di Torino, Italy
  15:00 15:30 5.11.3 COMPUTING SIMULATION FOR FIRE-FIGHTING HELICOPTER OPERATION ANALYSIS
I.V. Borisov, Southern Federal University, Taganrog Institute of Technology, Russia; A.V. Tsipenko, Moscow Aviation Institute, Russia
6.11Dynamic load 2
Chair: S. Paryshev
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  14:00 14:30 6.11.1 WAKE VORTEX ENCOUNTER LOADS. FLIGHT TESTS AND NUMERICAL SIMULATIONS
M.A. Torralba¹, J. Cerezo¹, S. Claverías¹, M. Reyes¹, H. Climent¹, C. Suñer¹, M. Karpel, Technion-Israel Institute of Technology, Israel; ¹Airbus Defence and Space, Spain
  14:30 15:00 6.11.2 OPTIMALITY CRITERIA FOR STRUCTURAL DESIGN OF AIRFRAMES WITH DYNAMIC REQUIREMENTS
A.I. Danilin, Samara State Aerospace University, Russia
  15:00 15:30 6.11.3 NONLINEAR STABILITY ANALYSIS OF CARBON NANOTUBES BASED ON TIMOSHENKO BEAM THEORY AND MODIFIED COUPLE STRESS THEORY
H. Dastoom Laatleyli, Sharif University of Technology, Dep. of Aerospace Eng., Iran
7.11Nozzles and ducts 2
Chair: Alex Whight
Track 7
04 - Propulsion
  14:00 14:30 7.11.1 NUMERICAL INVESTIGATION ON THE CORRELATION BETWEEN SHOCK STRUCTURE AND THRUST PERFORMANCE IN AN OVEREXPANDED NOZZLE
H.A. Choi¹, H.D. Kam, Hanwha Corp., South Korea; J.S. Kim¹; ¹Pukyong National University, South Korea
  14:30 15:00 7.11.2 EFFECT OF TEMPERATURE ON FLOW CHARACTERISTICS IN SUPERSONIC IMPINGING JET USING RANS/ILES HIGH RESOLUTION METHOD
L.A. Benderskiy, CIAM, Russia
  15:00 15:30 7.11.3 INVESTIGATION OF SYNTHETIC JETS EFFICIENCY ON SEPARATION FLOW IN DIFFUSERS OF DIFFERENT GEOMETRY WITH RANS/ILES-METHOD
D.A. Lyubimov¹, I.V. Potekhina¹; ¹CIAM, Russia
8.11Flight control 4
Chair: Fernando Moreira
Track 8
05.1 - Flight Dynamics and Control (Control & Modelling)
  14:00 14:30 8.11.1 ADAPTIVE CONTROL OF AEROELASTIC SYSTEMS: AN IMMERSION AND INVARIANCE APPROACH
A. Mannarino¹, P. Mantegazza¹; ¹Politecnico di Milano, Italy
  14:30 15:00 8.11.2 L1 ADAPTIVE CONTROLLER DESIGN FOR GUST LOAD ALLEVIATION
E. Capello¹, G. Guglieri¹, F. Quagliotti¹; ¹Politecnico di Torino, Italy
  15:00 15:30 8.11.3 CONSTRAINED PREDICTIVE STRATEGIES FOR FLIGHT CONTROL SYSTEMS
G. Franzè, DIMES- Università della Calabria, Italy; M. Mattei, DIII- Seconda Università di Napoli, Italy; V. Scordamaglia, DIIES - Università di Reggio Calabria, Italy
9.11UAV navigation
Chair: Gunnar Holmberg
Track 9
05.2 - Flight Dynamics and Control (UAV related)
  14:00 14:30 9.11.1 AUTONOMOUS TARGETED FLIGHT OF A ROTARY-WING MICRO AERIAL VEHICLE IN INDOOR, GPS-DENIED ENVIRONMENTS
S. Potyagaylo¹, O. Rand¹; ¹Technion, Israel
  14:30 15:00 9.11.2 AN APPLICATION OF DIGITAL IMAGE PROCESSING FOR UAV’S AUTOMATIC LANDING SYSTEM AID
M.P. Degrande¹, E.E.T. Moreira¹, E.M. Belo¹; ¹Escola de Engenharia de São Carlos - Universidade de São Paulo, Brazil
  15:00 15:30 9.11.3 NAVIGATION FOR VERTICAL PRECISION LANDING BASED ON OPTICAL TRACKING OF A SPATIAL RETROREFLECTIVE MARKER ARRAY
P. Hartmann¹, C. Ben¹, D. Moormann¹; ¹RWTH Aachen, Germany
10.11Future scenarios
Chair: Bruno Stoufflet
Track 10
07 - Systems Engineering and Supply Chain
  14:00 14:30 10.11.1 AUTOMATION IN FUTURE AIR TRANSPORT: A SCENARIO-BASED APPROACH TO THE DEFINITION OF OPERATIONAL REQUIREMENTS
N.P. Randt, Technical University of Munich, Germany; S. Wolf, Munich Airport, Germany
  14:30 15:00 10.11.2 A BIBLIOMETRICS APPLICATION FOR EVALUATING CONTRIBUTION OF A RESEARCH INSTITUTE TO SCIENCE
H. Nakamura¹, Y. Kajikawa, Tokyo Institute of Technology, Japan; S. Suzuki¹; ¹The University of Tokyo, Japan
  15:00 15:30 10.11.3 AIMING AND MISSING IN MULTIPLE DIMENSIONS
D.K. Howarth, MEE Inc., United States
11.11Safety and synthetic vision systems
Chair: Tim Etheriugton
Track 11
09 - Safety and Security
  14:00 14:30 11.11.1 ENHANCED AND SYNTHETIC VISION SYSTEMS DEVELOPMENT BASED ON INTEGRATED MODULAR AVIONICS
S.Y. Zheltov¹, Y.V. Vizilter¹, O.V. Vygolov¹; ¹State Research Institute of Aviation Systems (FGUP “GosNIIAS”), Russia
  14:30 15:00 11.11.2 SAFETY ASPECT OF MISSION SUPPORT DISPLAY FOR HIGH-DEMAN DAERIAL WORK
K. Funabiki¹, H. Tsuda¹, G. Tsuchiya¹; ¹JAXA, Japan
  15:00 15:30 11.11.3 EMERGENCY LANDING SITE LOCATION USING AERIAL IMAGE SEGMENTATION
T. Levora¹, O. Bruna¹, P. Paces¹; ¹Czech Technical University in Prague, Czech Republic
12.11International Cooperation in Aeronautics Research
Chair: R. Burger
Track 12
  14:00 14:30 12.11.1 PRESENTATION OF HORIZON 2020 PROGRAMME
R. Burger, EC, France
  14:30 15:00 12.11.2 EREA AND FUTURE SKY
J. Kaspar, EREA, Czech Republic
  15:00 15:30 12.11.3 OVERVIEW AND RESULTS OF FP7 PROJECT AFLONEXT
M. Fischer, Airbus, Germany