30th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

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Wednesday, 12. Sep 2018


7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
0.1General lecture III - The Future of Propulsion, Dr. Ric Parker president ISABE
Chair: Sebastien Remy
12. Sep 18 08:00 09:00

09:00 - 09:30Break

1.1Design Method 1
Chair(s): Bagassi, S.
Track 1
01 - Aircraft Design and Integrated Systems
12. Sep 18 09:30 10:00 1.1.1 MULTI-DISCIPLINARY ANALYSIS AND OPTIMIZATION JAVA TOOL FOR AIRCRAFT DESIGN
V. Trifari¹, M. Ruocco¹, V. Cusati¹, F. Nicolosi¹, A. De Marco¹; ¹University of Naples Federico II, Italy
12. Sep 18 10:00 10:30 1.1.2 COUPLED ADJOINT AEROSTRUCTURAL OPTIMIZATION FRAMEWORK FOR PRELIMINARY AIRCRAFT DESIGN
C.M. Boozer¹, A. Elham¹; ¹Braunschweig University of Technology, Germany
12. Sep 18 10:30 11:00 1.1.3 AIRCRAFT LOADS PREDICTION USING ENHANCED SIMULATION
Y. Lemmens, Siemens PLM, Belgium; T. Wilson, Airbus Operations Ltd, United Kingdom; J.E. Cooper, University of Bristol, United Kingdom
12. Sep 18 11:00 11:30 1.1.4 GENERAL PARAMETERS DESIGN METHOD OF CANARD ROTARY WING AIRPLANE UNDER THE INFLUENCE OF POWER SYSTEM
Y. Na, School of Aeronautics Northwestern Polytechnical University, China; Z.-H. Gao¹, Y.-P. Deng¹, L. Tian¹, H.-G. Gao¹; ¹School of Aeronautics Northwestern Polytechnical University, China
12. Sep 18 11:30 12:00 1.1.5 RESERCH ON KEY TECHNOLOGY OF INTELLIGENT CIVIL AIRCRAFT
Z. Li¹, D. Xie¹, B. Gao¹, Z. Yao¹; ¹Shanghai Aircraft Design and Research Institute, China
2.1Model Based System Engineering
Chair(s): Goes, L., Stoufflet, B.
Track 2
02 - Systems Engineering and Integration
12. Sep 18 09:30 10:00 2.1.1 CANCELED - MBSE FLIGHT TESTING ARCHITECTURE RESEARCH
X. Hua, China; C. Qing, CFTE, China; S.J. Qi, cfte, China
12. Sep 18 10:00 10:30 2.1.2 UTILIZATION OF SCALING LAWS AND UNCERTAINTY QUANTIFICATION TO INFORM TECHNOLOGY DEVELOPMENT EXPERIMENTATION
K.G. Schwartz¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States
12. Sep 18 10:30 11:00 2.1.3 A SYSML-BASED APPROACH TO EXPLORING INNOVATIVE SYSTEM IDEAS FOR AERONAUTICAL APPLICATIONS
J. Abulawi, HAW Hamburg, Germany
12. Sep 18 11:00 11:30 2.1.4 APPLICATION OF AGILE MODEL-BASED SYSTEMS ENGINEERING IN AIRCRAFT CONCEPTUAL DESIGN
G.P. Krupa, Federal University of Itajubá, Brazil
12. Sep 18 11:30 12:00 2.1.5 A BOND GRAPH-ORIENTED METHOD FOR ASSESSMENT OF FAILURES IN AN AIRCRAFT HYDRAULIC BRAKE SYSTEM
M. Maia Neto¹, L.C.S. Goes¹; ¹ITA, Brazil
3.1Durability and Fatigue
Chair(s): Poikelispää, M., Angelin, R.
Track 3
04.1 - Material Issues, Fatigue and Damage Tolerance
12. Sep 18 09:30 10:00 3.1.1 FATIGUE AND CRACK PROPAGATION LIFE IMPROVEMENT QUANTIFICATION FOR COLD-WORKED HOLES OUTSIDE NOMINAL CONDITIONS
L. Zaplana ¹, I. Rivero¹, B. García-Fogeda ¹, J. Gómez-Escalonilla¹; ¹AIRBUS DS, Spain
12. Sep 18 10:00 10:30 3.1.2 USING THE LEAD CRACK CONCEPT TO REDUCE DURABILITY TEST DURATION
L. Molent, DST, Australia
12. Sep 18 10:30 11:00 3.1.3 CANCELED - INFLUENCE OF IRREGULAR LOADING PARAMETERS ON CFRP COMPONENTS FATIGUE LIFE
A.G. Kalinin, Central Aerohydrodynamic Institute, TsAGI, Russia
12. Sep 18 11:00 11:30 3.1.4 THE EFFECT OF STRUCTURAL PARAMETERS OF AIRCRAFT PANEL ON VIBRATION FATIGUE LIFE
P. Li¹, J. Ma¹; ¹Aircraft strength research institute, China
4.1Turbulence Modeling and LES
Chair(s): Azevedo, J.L.F.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
12. Sep 18 09:30 10:00 4.1.1 TOWARDS INDUSTRIAL LARGE EDDY SIMULATION AND AERO-ACOUSTIC NOISE COMPUTATION WITH THE HIGH-ORDER FR/CPR METHOD
Z.J. Wang, United States
12. Sep 18 10:00 10:30 4.1.2 TURBULENCE MODEL CONDITIONING FOR VORTEX DOMINATED FLOWS BASED ON EXPERIMENTAL RESULTS
M. Moioli¹, C. Breitsamter¹, K.A. Sørensen, Airbus Defence and Space, Germany; ¹Technical University of Munich, Germany
12. Sep 18 10:30 11:00 4.1.3 IMPROVED DELAYED DETACHED EDDY SIMULATION OF THE FLOWS AROUND S809 AIRFOIL FOR ANGLES OF ATTACK FROM 0 TO 90 DEGREES
W. Yue¹, L. Kang¹, S. Wenping¹, H. Zhonghua¹; ¹Northwestern Polytechnical University, China
12. Sep 18 11:00 11:30 4.1.4 AERODYNAMIC EVALUATION OF THE EXTERNAL FLOW OVER PICKUP TRUCKS
E.-K. Mascia¹, O. de Almeida¹; ¹Federal University of Uberlandia, Brazil
12. Sep 18 11:30 12:00 4.1.5 A HYBRID LENGTH SCALE SIMILARITY SOLUTION FOR SWIRLING TURBULENT JETS
G. Andrews, Purdue University, United States
5.1Wind Tunnel Systems Development
Chair(s): Guillaume, M.
Track 5
03.2 - Experimental Aerodynamics
12. Sep 18 09:30 10:00 5.1.1 OVERVIEW OF DYNAMIC TEST TECHNIQUES AT LOW SPEED AERODYNAMICS INSTITUTE, CARDC
Z. Liu¹, H. Sun¹, B. Nie¹, L. Guo¹, F. Cen¹; ¹China Aerodynamics Research and Development Center (CARDC), China
12. Sep 18 10:00 10:30 5.1.2 APPLICATION OF THE COMBINED BOUNDARIES TO REDUCE WALL INTERFERENCE FOR NACA 0012 AIRFOIL TESTS
S.L. Chernyshev¹, A.I. Ivanov¹, E.V. Streltsov¹, A.O. Volkova¹; ¹Central Aerohydrodynamic Institute n.a. prof. N.E. Zhukovsky, Russia
12. Sep 18 10:30 11:00 5.1.3 EVALUATION OF WIND TUNNEL WALL BOUNDARY-LAYER CONTROL FOR 2-D HIGH-LIFT AERODYNAMIC AND AEROACOUSTIC TESTING
F.M. Catalano, Aeronautical Engineering Dept. University of São Paulo , Brazil; L.T.L. Pereira, University of São Paulo , Brazil
12. Sep 18 11:00 11:30 5.1.4 CANCELED - EXPERIMENTAL INVESTIGATION OF SHEAR LAYER INDUCED FLUCTUATIONS IN A OPEN JET WIND TUNNEL
G.G. Gadzhimagomedov, Central Aerohydrodynamic Institute n.a. prof. N.E. Zhukovsky, Russia
6.1Complex Transition Phenomena
Chair(s): Alves, L., Hanifi, A.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
12. Sep 18 09:30 10:00 6.1.1 DEVELOPMENT OF SECONDARY CROSSFLOW INSTABILITY NEAR BREAKDOWN INTO TURBULENCE
E. van Bokhorst¹, C. Atkin¹; ¹University of London, United Kingdom
12. Sep 18 10:00 10:30 6.1.2 EFFECTS OF THE INTRINSIC THREE-DIMENSIONALIZATION OF LAMINAR SEPARATION BUBBLES ON THE AMPLIFICATION OF EXTERNAL DISTURBANCES
D. Rodriguez, Universidade Federal Fluminense, Brazil; E.M. Gennaro, Sao Paulo State University, Brazil
12. Sep 18 10:30 11:00 6.1.3 WAVEPACKETS IN TURBULENT FLOW OVER A NACA 4412 AIRFOIL
L.I. Abreu¹, A.V.G. Cavalieri¹, P. Schlatter², R. Vinuesa², D. Henningson²; ¹ITA, Brazil ;²KTH, Sweden
12. Sep 18 11:00 11:30 6.1.4 CONTROL OF STREAKY DISTURBANCES IN THE BOUNDARY LAYER OVER A FLAT PLATE
P. Morra¹, K. Sasaki², A. Cavalieri², A. Hanifi¹, D. Henningson¹; ¹KTH Royal Institute of Technology, Sweden ;²Instituto Tecnológico de Aeronáutica, Brazil
12. Sep 18 11:30 12:00 6.1.5 LAMINAR-TURBULENT TRANSITION MECHANISMS OVER WIDELY-SPACED SUCTION HOLES
B. Crowley¹, C. Atkin¹; ¹City University of London, United Kingdom
7.1Propellors and Rotors
Chair(s): Monk, J.
Track 7
03.4 - Applied Aerodynamics
12. Sep 18 09:30 10:00 7.1.1 APPLICATION OF HIGH-ROBUSTNESS BEMT FOR SIMULATION OF UAV-VTOL PROPELLER AT LOW/HIGH ADVANCE RATIO
Z. Fan¹, Z. Zhou¹, X. Zhu, Science and Technology on UAV Laboratory, NPU, China; ¹School of Aeronautics,Northwestern Polytechnical University, China
12. Sep 18 10:00 10:30 7.1.2 AERODYNAMIC DESIGN OF A RIGID COAXIAL ROTOR AIRFOIL IN UNSTEADY FLOW
X.-D. Yang¹, M. Huang¹; ¹School of Aeronautics Northwestern Polytechnical University, China
12. Sep 18 10:30 11:00 7.1.3 INVESTIGATION ON APPROACH TO CONTROL LIFT DISTRIBUTION OF WING BY DISTRIBUTED PROPELLERS
C. Xue¹, Z. Zhou¹, H.-B. Wang¹; ¹Northwestern Polytechnical University, China
12. Sep 18 11:00 11:30 7.1.4 ANALYSIS OF XH-59A ROTOR IN FORWARD FIGHT WITH HIGH EFFICIENCY TRIM METHOD
P. Zhou¹, X. Zhao¹, L. Deng¹, Y.-F. Lin, China Helicopter Research and Development Institute, China; ¹Northwestern Polytechnical University, China
12. Sep 18 11:30 12:00 7.1.5 SIMULATIONS OF UNSTEADY AIRWAKES BEHIND SHIPS IN MOTION
W.X. Yuan¹, A. Wall¹, R. Lee¹; ¹National Research Council Canada, Canada
8.1Aircraft Structural Design II
Chair(s): Ireman, T.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
12. Sep 18 09:30 10:00 8.1.1 PRELIMINARY ASSESSMENT OF A WARPING WING CONFIGURATION IN ROLLING CONTROL
E. Cestino¹, G. Frulla¹, A. Lanzillotti¹; ¹Politecnico di Torino, Italy
12. Sep 18 10:00 10:30 8.1.2 STRUCTURAL DESIGN AND ANALYSIS OF A QUADROTOR FIXED-WING HYBRID UAV WING
W. Fang, China; H. Ma, China; H. Zhang, China
12. Sep 18 10:30 11:00 8.1.3 STRUCTURAL SIZING OF A ROTORCRAFT FUSELAGE USING AN INTEGRATED DESIGN APPROACH
D.B. Schwinn¹, P. Weiand¹, M. Schmid¹, M. Buchwald¹; ¹German Aerospace Center (DLR), Germany
12. Sep 18 11:00 11:30 8.1.4 AN ACTIVE-PASSIVE NONLINEAR FINITE ELEMENT MODEL FOR ELECTROMECHANICAL COMPOSITE MORPHING BEAMS
R.B. Olympio¹, M.V. Donadon¹, S.G.P Castro, EMBRAER, Brazil; ¹ITA, Brazil
12. Sep 18 11:30 12:00 8.1.5 STRUCTURAL OPTIMIZATION AND PROPOSITION OF PRE-SIZING PARAMETERS FOR UAVS WING SPARS
F.A. Fenelon¹, G.F.S. Neves¹, R.S. Martins¹; ¹Universidade Federal de Minas Gerais, Brazil
9.1Fan and Propeller
Chair(s): Yimer, I.
Track 9
05 - Propulsion
12. Sep 18 09:30 10:00 9.1.1 STUDY ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLERS WITH PROPLETS
X. Yang¹, J. Xu¹, B. Wang¹, C. Song¹, S. Zhang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
12. Sep 18 10:00 10:30 9.1.2 NOVEL JET ENGINE ACOUSTIC LINER WITH IMPROVED BROADBAND NOISE ABSORPTION
K. Hoeschler, Brandenburg Technische Universität Cottbus-Senftenberg, Germany; E. Sarradj, Technische Universität Berlin, Germany; N. Modler, Technische Universität Dresden, Germany; L. Enghardt, German Aerospace Center, Germany
12. Sep 18 10:30 11:00 9.1.3 CERTAIN ASPECTS OF FAN MODEL STAGE DESIGNING FOR ADVANCED TURBOFANS
S.V. Pankov¹, V.I. Mileshin¹, I.K. Orekhov¹, V.A. Fateev¹; ¹Central Institute of Aviation Motors, Russia
12. Sep 18 11:00 11:30 9.1.4 BIMODAL UNMANNED VEHICLE: PROPULSION SYSTEM INTEGRATION AND WATER/AIR INTERFACE TESTING
A. Bacciaglia¹, D. Guo², P. Marzocca², C. Bil², A. Ceruti¹; ¹University of Bologna, Italy ;²RMIT University, Australia
12. Sep 18 11:30 12:00 9.1.5 PARAMETRIC INVESTIGATION OF EESC-USP AEROACOUSTIC FAN RIG
R.G. Cuenca, UFSC, Brazil; P. Celso Jr.¹, B.M. Rocamora¹; ¹EESC-USP, Brazil
10.1Flight Control 1
Chair(s): Vian, J.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
12. Sep 18 09:30 10:00 10.1.1 QUASI-LPV MODELING AND PARAMETER-DEPENDENT OPTIMAL CONTROL OF MORPHING WING AIRCRAFT
J. Lee¹, Y. Kim¹; ¹Seoul National University, South Korea
12. Sep 18 10:00 10:30 10.1.2 A LOW COST MODEL AIRCRAFT FLIGHT RESEARCH FACILITY IN WIND TUNNEL
B.W. Nie, National University of Defense Technology, China; L.L. Guo¹, F. Cen¹, O. Sename², L. Dugard²; ¹China Aerodynamics Research and Development Center, China ;²Univ. Grenoble Alpes, CNRS, Grenoble INP, GIPSA-lab, France
12. Sep 18 10:30 11:00 10.1.3 EFFECTS OF TAILORED CONTROL SURFACE COMPLIANCE ON AIRCRAFT STABILITY AND CONTROL
P. Krus, Linköping university, Sweden; B. Lantto, Saab AB, Sweden; M.A. Rodriguez¹, E. Villani¹; ¹Instituto Technologico Aeronautica, Italy
12. Sep 18 11:00 11:30 10.1.4 DIGITAL HYDRAULICS IN AEROSPACE APPLICATIONS: SLIDING MODE OF QUANTIZED CONTROL AND LMI APPROACH
L.P.G. Pinto¹, P. Krus¹, V.J. De Negri, Universidade Federal de Santa Catarina, Brazil; ¹Linköping University, Sweden
12. Sep 18 11:30 12:00 10.1.5 AERODYNAMIC ANALYSIS AND CONTROL ALLOCATION FOR ASYMMETRIC VARIABLE SWEEP AIRCRAFT WITH FLEXIBLE TRAILING EDGE
H. Ma¹, B.F. Song¹, Y. Pei¹, Z.W. Chen¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
11.1UAS Control 2
Chair(s): Justin, C.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
12. Sep 18 09:30 10:00 11.1.1 MULTI-CHANNEL HUMAN-MACHINE INTERACTIVE SYSTEM FOR MULTIPLE UAVS\' CONTROL
P.-C. Wen¹, Y.-D. Zhang¹, Y.-H. Li¹; ¹AVIC Xi'an Aeronautics Computing Technique Research Institute, China
12. Sep 18 10:00 10:30 11.1.2 FLIGHT PERFORMANCE OF STEERABLE CRUCIFORM PARACHUTE SYSTEMS
S.M. Herrington¹, T.D. Fields¹, O.A. Yakimenko, Naval Postgraduate School, United States; ¹University of Missouri-Kansas City, United States
12. Sep 18 10:30 11:00 11.1.3 A STRATEGY FOR UAV PERFORMANCE ENHANCEMENT THROUGH ATMOSPHERIC ENERGY EXTRACTION USING MPC TECHNIQUES
G. Pogorzelski, CENIC Engenharia, Brazil; F.J. Silvestre, ITA - Instituto Tecnológico de Aeronáutica, Brazil
12. Sep 18 11:00 11:30 11.1.4 ON WAKE VORTEX SAFETY ANALYSIS AND CONTROL FOR UAV
V. Golubev¹, P. Kazarin¹, C. Moreno¹, W. MacKunis¹; ¹ERAU, United States
12. Sep 18 11:30 12:00 11.1.5 MODELING, CONTROL AND HARDWARE-IN-THE-LOOP SIMULATION OF A GENERIC TILTING MULTI-ROTOR
F. Machini¹, I.O. Tarifa¹, R.M.F. Neto¹, L. Sanches¹; ¹Universidade Federal de Uberlândia, Brazil
12.1Airport / TMA Procedures & Environmental Impact
Chair(s): Reichmuth, J., Senac, P.
Track 12
09 - Air Transport System Efficiency
12. Sep 18 09:30 10:00 12.1.1 THE USE OF SYNTHETIC VISION TOOLS IN THE CONTROL TOWER ENVIRONMENT: THE RETINA CONCEPT
S. Bagassi¹, F. De Crescenzio ¹, S. Piastra¹; ¹University of Bologna, Italy
12. Sep 18 10:00 10:30 12.1.2 A NOVEL CONTROL APPROACH TO IMPROVE SPEED COMMANDS AND PILOT WORKLOAD FOR FLIGHT-DECK BASED INTERVAL MANAGEMENT
T. Riedel, Keio University / Electronic Navigation Research Institute, Japan
12. Sep 18 10:30 11:00 12.1.3 STUDY ON THE ARRIVAL MANAGER MAXIMIZING THE BENEFIT OF FOUR-DIMENSIONAL TRAJECTORY BASED OPERATIONS
D. Toratani¹, N.K. Wickramasinghe¹, E. Itoh¹; ¹Electronic Navigation Research Institute, Japan
12. Sep 18 11:00 11:30 12.1.4 NONLINEAR MODEL PREDICTIVE CONTROL FOR OPTIMAL AIRCRAFT SEQUENCING
B. Grüter¹, J. Diepolder¹, P. Piprek¹, T. Akman¹, F. Holzapfel¹; ¹Technical University of Munich, Germany
12. Sep 18 11:30 12:00 12.1.5 A FRAMEWORK TO ASSESS FUTURE AIRPORT NOISE APPLIED TO A TWO-RUNWAY AIRPORT
F. Will¹, M. Hornung¹; ¹Technical University of Munich, Germany
Reserve Paper 12.1.R INTEGRATED ARRIVAL AND DEPARTURE MANAGEMENT FOR JEJU INTERNATIONAL AIRPORT
D. Jeon¹, Y. Eun¹, H. Kim¹, S. Kim¹, E. Oh¹, M. Jeong¹; ¹Korea Aerospace Research Institute, South Korea

12:00 - 13:00Lunch

0.2von Karman Lecture - International Committee on Aeronautical Fatigue and Structural Integrity (ICAF) – Achievements, Activities, and Future Challenges, Anders Blom, David Simpson, Carlos Chaves, Marcel Bos
Chair: Dimitri Mavris, ICAS MRSC Chair
12. Sep 18 13:00 13:55

1.2Design Education 2
Chair(s): della Vecchia, P.
Track 1
01 - Aircraft Design and Integrated Systems
12. Sep 18 14:00 14:30 1.2.1 STUDY ON EVALUATION METHODS OF UNDERGRADUATE AIRCRAFT OVERALL DESIGN COURSE BASED ON TEAM DESIGN COMPETITION
Z.-K. Chen¹, H. Liu¹, C.-G. Yang¹; ¹School of Aeronautic Science and Engineering, Beihang University, China
12. Sep 18 14:30 15:00 1.2.2 ELECTRIC VTOL UAV CONFIGURATION STUDIES AND OPTIMIZATION WITHIN AIRCRAFT DESIGN PRACTICAL COURSE AT TECHNICAL UNIVERSITY OF MUNICH
C. Rößler¹, M. Hornung¹; ¹Technical University of Munich, Institute of Aircraft Design, Germany
2.2Maintenance Management
Chair(s): Chaves, C., Scott, M.
Track 2
11 - Operations and Sustainment
12. Sep 18 14:00 14:30 2.2.1 CANCELED - DRONES AS AN EMERGING PREDICTIVE MAINTENANCE TOOL: IMPLEMENTATION OF A DRONE WORKSHOP, FOR THE ENRICHMENT OF NEW PROFESSIONAL SKILLS IN THE STUDENTS OF MAINTENANCE CAREERS OF THE TECHNOLOGICAL UNIVERSITY OF JALISCO
J. Sandoval, Universidad Autónoma Metropolitana Unidad Lerma, Mexico; J.-J. Barron, Universidad Tecnológica de Jalisco, Mexico
12. Sep 18 14:30 15:00 2.2.2 AIRLINE MAINTENANCE: A PROPOSAL ENVISIONING DIGITAL TRANSFORMATION
L.B. Koslosky¹, N. Fisk, Boeing, United States; P. Krus, Linköping University, Sweden; L. Pereira¹; ¹Universidade Federal do ABC, Brazil
12. Sep 18 15:00 15:30 2.2.3 OPTIMAL SHAPE OF REPAIR PATCHES IN COMPOSITES
L. Echer¹, C.E. de Souza, Federal University of Santa Maria, Brazil; R.J. Marczak¹; ¹Federal University of Rio Grande do Sul, Brazil
3.2Structural Health Monitoring 1
Chair(s): Ikeda, T.
Track 3
04.1 - Material Issues, Fatigue and Damage Tolerance
12. Sep 18 14:00 14:30 3.2.1 CANCELED - OPTIMIZATION OF THE COEFFICIENT OF PROBABILITY DISTRIBUTION FUNCTION OF THE SENSING PATHS FOR INSTANTANEOUS BASELINE DAMAGE DETECTION USING GENETIC ALGORITHM
P.K. Motamed¹, A. Abedian¹, M. Nasiri¹; ¹Sharif University of Technology, Iran
12. Sep 18 14:30 15:00 3.2.2 DEVELOPMENT OF STRUCTURAL HEALTH MONITORING METHODS THROUGH THE ANALYSIS OF KINETICS OF LOCAL STRESS-STRAIN STATE
A.A. Bautin¹, Y.A. Svirskiy¹; ¹TsAGI, Russia
12. Sep 18 15:00 15:30 3.2.3 CANCELED - DETECTION OF HIDDEN FATIGUE CRACKS IN RIVETED LAP JOINTS USING WAVELET TRANSFORM AND NEURAL NETWORKS
A.Abedian abedian, sharif university of technology, Iran
Reserve Paper 3.2.R CANCELED - DEVELOPMENT OF METHODS FOR DETERMINING CRACK RESISTANCE PARAMETERS FOR STATIC AND FATIGUE LOADING FOR POLYMER COMPOSITE MATERIALS
V.L. Tokar¹, Y.V. Koroleva¹, Y.A. Svirsky¹; ¹TsAGI, Russia
4.2Laminar Flow and Transition
Chair(s): Alves, L., Castro, L.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
12. Sep 18 14:00 14:30 4.2.1 VALIDATION OF INTERMITTENCY MODEL FOR TRANSITION PREDICTION IN A RANS FLOW SOLVER
D. de Rosa¹, P. Catalano¹; ¹CIRA - Italian Aerospace Research Centre, Italy
12. Sep 18 14:30 15:00 4.2.2 ON THE CALIBRATION OF THE INTERMITTENCY TRANSITION TURBULENCE MODEL FOR WIND TURBINE AIRFOIL BY MACHINE LEARNING ALGORITHM
M.A. Abd Bari¹, A. Da Ronch¹, M. Panzeri, Noesis Solutions, Belgium; J. Drofelnik¹; ¹University of Southampton, United Kingdom
12. Sep 18 15:00 15:30 4.2.3 EFFECT OF CONTROLLED PERIODIC ROUGHNESS ON GOERTLER VORTICES IN HYPERSONIC COMPRESSION RAMP FLOW
P.V. Chuvakhov¹, V.N. Radchenko¹, E.A. Alexandrova¹, V.Y. Borovoy¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
5.2Aerodynamic Experiments
Chair(s): Takara, E.
Track 5
03.2 - Experimental Aerodynamics
12. Sep 18 14:00 14:30 5.2.1 INFLUENCE OF AIRFRAME STIFFNESS ON THE AERODYNAMIC COEFFICIENTS OF A HIGH ASPECT RATIO WING
L.A.V. Pelegrineli¹, F.F. Liorbano¹, H.O.H. Natori¹, R.A. Angélico¹; ¹ University of São Paulo, São Carlos School of Engineering, Brazil
12. Sep 18 14:30 15:00 5.2.2 HORIZONTAL TAIL LOCAL ANGLE-OF-ATTACK AND TOTAL PRESSURE MEASUREMENTS THROUGH STATIC PRESSURE PORTS AND KIEL PITOT
R.M. Granzoto¹, L.A. Algodoal¹, G.J. Zambrano¹, G.G. Becker¹; ¹Embraer, Brazil
12. Sep 18 15:00 15:30 5.2.3 EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF A UAV FOR SUPERFICIAL VOLCANO SURVEILLANCE
P.D. Bravo-Mosquera¹, L. Botero-Bolivar¹, D. Acevedo-Giraldo¹, H.D. Cerón-Muñoz¹, F.M. Catalano¹; ¹EESC-USP, Brazil
6.2Instability Control
Chair(s): Fu, S.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
12. Sep 18 14:00 14:30 6.2.1 ON THE WAVE-CANCELLING NATURE OF BOUNDARY LAYER TRANSITION CONTROL
K. Sasaki¹, P. Morra², A.V.G. Cavalieri¹, A. Hanifi², D.S. Henningson²; ¹ITA, Brazil ;²KTH, Sweden
12. Sep 18 14:30 15:00 6.2.2 ACTUATOR AND SENSOR PLACEMENT FOR CLOSED-LOOP CONTROL OF CONVECTIVE INSTABILITIES
G.A. Freire¹, A.V.G. Cavalieri¹, F.J. Silvestre¹; ¹ITA, Brazil
12. Sep 18 15:00 15:30 6.2.3 RESOLVENT-BASED CONTROL OF STREAKS IN BOUNDARY LAYERS
P.A.S. Nogueira¹, A.V.G. Cavalieri¹, A. Hanifi², D.S. Henningson²; ¹Instituto Tecnológico de Aeronáutica, Brazil ;²KTH Royal Institute of Technology, Sweden
7.2Impact
Chair(s): Corman, J.
Track 7
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
12. Sep 18 14:00 14:30 7.2.1 VERIFIED FUSELAGE SECTION WATER IMPACT MODELING
Y. Song¹, B. Harton¹, J. Bayandor¹; ¹CRashworthiness for Aerospace Structures and Hybrids (CRASH Lab), United States
12. Sep 18 14:30 15:00 7.2.2 PREDICTING LOW-VELOCITY IMPACT DAMAGE IN COMPOSITE USING COHESIVE ELEMENT
H. Liu¹, S. Tan¹; ¹fai, China
12. Sep 18 15:00 15:30 7.2.3 ENERGY-ABSORBING CHARACTERISTICS ANALYSIS OF COMPOSITE THIN-WALLED C-CHANNELS UNDER LOW SPEED AXIAL COMPRESSION
J. Xie¹, Z. Feng¹, S. Song¹, D. Song¹, X. Zhang¹; ¹Civil Aviation University of China, China
8.2Aeroelasticity 4 : General
Chair(s): Amiryants, G.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
12. Sep 18 14:00 14:30 8.2.1 EXPERIMENTAL AND NUMERICAL STUDIES OF FLUTTER CHARACTERISTICS OF AN ALL-MOVING CONTROL SURFACE AGAINST GAP EFFECTS
Y. Bai¹, W. Qian¹, X. Chen¹; ¹Dalian University of Technology, China
12. Sep 18 14:30 15:00 8.2.2 MULTIDISCIPLINARY METHODS FOR WING FLIGHT SHAPE ANALYSIS - EFFECT OF THE GEOMETRIC NONLINEAR STRUCTURE FOR STATIC PULL-UP
A.A. Verri¹, C.T. Jorge¹, A.F. Bizarro¹, F.L.S. Bussamra, ITA, Brazil; H.N.S. Júnior¹, C.E.S. Cesnik, UniMich, United States; ¹Embraer S/A, Brazil
12. Sep 18 15:00 15:30 8.2.3 RESULTS AND COMPARISON OF NUMERICAL SIMULATION AND THE TESTING OF LUG MANUFACTURED BY COMPOSITE MATERIAL BY RTM PROCESS
G.C. Fonseca, Embraer - Centro de Engenharia e Tecnologia - Minas Gerais, Brazil; S.F.M. Almeida, ITA - Instituto Tecnológico de Aeronáutica, Brazil
9.2High Speed Propulsion 1
Chair(s): Kukshinov, N.
Track 9
05 - Propulsion
12. Sep 18 14:00 14:30 9.2.1 INVESTIGATION ON AERO-PROPULSIVE BALANCE FOR HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECT
A.A. Gubanov¹, D.S. Ivanyushkin¹, N.V. Kukshinov², A.N. Prokhorov², V.A. Talyzin¹, N.V. Voevodenko¹; ¹Central Aerohydrodynamic Institute named after Professor N.E. Zh, Russia ;²Central Institute of Aviation Motors named after P.I. Baranov, Russia
12. Sep 18 14:30 15:00 9.2.2 COMPLEX NUMERICAL AND EXPERIMENTAL RESEARCH OF HEXAFLY-INT HIGH-SPEED CIVIL AICRAFT MODEL
V.Y. Aleksandrov¹, S.N. Batura¹, O.V. Gouskov¹, N.V. Kukshinov¹, A.N. Prokhorov¹, A.V. Rudinsky¹; ¹Central Institute of Aviation Motors named after P.I. Baranov , Russia
12. Sep 18 15:00 15:30 9.2.3 CANCELED - INFLUENCE OF TEMPERATURE FACTOR ON THE CHARACTERISTICS OF HIGH-SPEED AIR-BREATHING ENGINE INLETS
O.V. GUSKOV, MIPT, Russia
10.2Flight Dynamics & Identification 1
Chair(s): Korsun, O.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
12. Sep 18 14:00 14:30 10.2.1 CLOSED-LOOP SYSTEM IDENTIFICATION OF A LARGE FLEXIBLE AIRCRAFT USING SUBSPACE METHODS
R.C.M.G. Barbosa¹, L.C.S. Góes¹; ¹ITA, Brazil
12. Sep 18 14:30 15:00 10.2.2 RECURSIVE AERODYNAMIC PARAMETER IDENTIFICATION OF A FIGHTER JET FLYING IN TURBULENT AIR
C. Grillo, Università di Palermo, Italy
12. Sep 18 15:00 15:30 10.2.3 APPLICABILITY OF GEOMETRICALLY-LINEAR STRUCTURAL-DYNAMIC MODELS FOR THE FLIGHT DYNAMICS OF ARBITRARILY-FLEXIBLE AIRCRAFT
A.B. Guimarães Neto¹, F.L. Cardoso-Ribeiro¹, F.J. Silvestre¹; ¹ITA, Brazil
Reserve Paper 10.2.R SYSTEM IDENTIFICATION OF A SUBSCALE FIGHTER AIRCRAFT
L.M. Nepomuceno, Brazil
11.2Air Data
Chair(s): Sorbilli, R.
Track 11
07 - Systems, Subsystems and Equipment
12. Sep 18 14:00 14:30 11.2.1 SMART FAULT-TOLERANT AIR-DATA SENSOR FOR AIRCRAFT FLOW ANGLES MEASUREMENT
G. Di Rito¹, F. Schettini¹; ¹Università di Pisa - Dip. di Ing. Civile ed Industriale, Italy
12. Sep 18 14:30 15:00 11.2.2 DESIGN CRITERIA OF A THERMAL MASS FLOW SENSOR FOR AIRCRAFT AIR DATA APPLICATIONS
L.C. Ribeiro¹, R.A. Souza¹, M.L. Oliveira¹, S.P.L. Vieira¹, W.O. Avelino, Labinfo Lab UFMG, Brazil; C.F.R. Oliveira¹, D.W. de Lima Monteiro¹, F.S. Torres¹, R.M.O. Hansen, University of Southern Denmark, Denmark; ¹UFMG, Brazil
12. Sep 18 15:00 15:30 11.2.3 AN AIRBORNE DATA BUS NETWORK SYSTEM OF INTERFACE ADAPTIVE AND FLEXIBLE CONTROL
Z. Dai¹, Z. Qiu, Xi'an Aeronautics Computing Technique Research Institute, China; L. Shi¹; ¹ChengDu Aircraft Design & Research Institute, China
12.2Air Transportation Network
Chair(s): Zhang, X.
Track 12
09 - Air Transport System Efficiency
12. Sep 18 14:00 14:30 12.2.1 A SIMULATION MODELING STUDY FOR FREE ROUTING AIRSPACE IN JAPAN
K. Kageyama¹, Y. Nakamura¹; ¹ENRI, Japan
12. Sep 18 14:30 15:00 12.2.2 EVALUATION OF THE POTENTIAL IMPACTS OF HYBRID-ELECTRIC AIRCRAFT ON THE GLOBAL AIR TRANSPORTATION NETWORK
G. Tay¹, S. Gillen¹, R. Rothfeld, Bauhaus Luftfahrt e.V., Germany; M. Hornung¹; ¹Technical University of Munich, Germany
12. Sep 18 15:00 15:30 12.2.3 EULERIAN OPTIMAL CONTROL FORMULATION FOR DYNAMIC MORPHING OF AIRSPACE SECTORS
Y. Lim¹, N. Premlal¹, A. Gardi¹, R. Sabatini¹; ¹RMIT University, Australia
Reserve Paper 12.2.R STUDY ON LARGE-SCALE FLIGHT DELAY RECOVERY
Z. Zhang¹, J. Wang¹; ¹Civil Aviation University of China, China

15:30 - 16:00Break

1.3Unconventional Concepts 2
Chair(s): Kimmel, B.
Track 1
01 - Aircraft Design and Integrated Systems
12. Sep 18 16:00 16:30 1.3.1 FEASIBILITY STUDY OF MODIFYING A BASELINE KEROSENE AIRCRAFT TO A LH2 POWERED VERSION
W. Xie¹, Z. Duan¹, H. Smith, Cranfield University, United Kingdom; ¹AVIC The First Aircraft Institute, China
12. Sep 18 16:30 17:00 1.3.2 DEVELOPMENT OF THE REGENERATIVE SOARER: THEORETICAL AND PRACTICAL ASPECTS
R.C. Carvalho, EMBRAER S.A., Brazil
12. Sep 18 17:00 17:30 1.3.3 DEVELOPMENT OF A NOVEL AERIAL PLATFORM WHICH MERGES THE CONCEPT OF AIRSHIPS AND TETHERED AEROSTATS
J.S. Santos¹, B.A. de Azevedo¹, L.C.S. Góes¹, R.S. Pant, Indian Institute of Technology Bombay, India; ¹Instituto Tecnológico de Aeronáutica, Brazil
12. Sep 18 17:30 18:00 1.3.4 CANCELED - CONSTRAINED BIFURCATION AND CONTINUATION METHOD IN BLENDED-WING-BODY AIRCRAFT DESIGN
F. Cen¹, Q. Li¹, B.-W. Nie², Z.-T. Liu²; ¹Tsinghua University, China ;²China Aerodynamics Research and Development Center , China
2.3Novel Application of MDO in Aircraft Design 3
Chair(s): Shiva Prakasha, P.
Track 2
01 - Aircraft Design and Integrated Systems
12. Sep 18 16:00 16:30 2.3.1 STRUCTURAL DESIGN AND TESTING OF A TAILORED SKIN SINGLE DUCT (TSSD) FIN APPLICATION
M. Schneider¹, M. Horn¹, S. Ritt¹, A. Seitz¹; ¹DLR, Germany
12. Sep 18 16:30 17:00 2.3.2 STUDIES ON THE APPLICATION OF MOEA/D TO AERODYNAMIC OPTIMIZATION DESIGN
X.Q. Zhu¹, Z.H Gao¹, Z.W. Chen¹; ¹Northwestern Polytechnical University, China
12. Sep 18 17:00 17:30 2.3.3 COMPARISON AND APPLICATION OF DIFFERENTS TECHNIQUES OF MULTI-OBJECTIVE OPTIMIZATION FOR AERODYNAMIC WING DESIGN
N. Gautier¹, N. Manzanares-Filho¹, E.R. Da Silva¹; ¹UNIFEI, Brazil
12. Sep 18 17:30 18:00 2.3.4 INTEGRATED SYSTEM FOR UNIFICATION OF AIRCRAFT CONCEPTUAL DESIGN APPLICATIONS
E. Vogiatzis¹, R. Chaitanya Munjulury¹, P. Krus¹; ¹Linköping University, Sweden
3.3Advanced Manufacturing and Non Destructive Testing
Chair(s): Jokinen, J.
Track 3
04.1 - Material Issues, Fatigue and Damage Tolerance
12. Sep 18 16:00 16:30 3.3.1 ARAMID-FIBER REINFORCED ELASTOMERS AS FUTURE AIRCRAFT ACTUATORS - A PROOF-OF-CONCEPT INVESTIGATION
M. Kanerva¹, M. Poikelispää¹, P. Antunes, Aveiro University, Portugal; ¹Tampere University of Technology, Finland
12. Sep 18 16:30 17:00 3.3.2 ON EQUIVALENCE OF POLYMER COMPOSITE MATERIALS STRUCTURES LOADING PROGRAMS UNDER FULL-SCALED SERVICE CYCLE TESTING
A.V. Pankov¹, V.V. Konovalov¹; ¹TsAGI, Russia
12. Sep 18 17:00 17:30 3.3.3 STUDY OF EXTERNAL FACTOR COMBINATIONS EFFECT ON CFRP STRUCTURE UTILYZING ULTRASONIC MICROSCOPY
T. Ryzhova¹, A. Shanygin¹, V. Scherbakov¹, Y. Petronyuk², V. Levin², E. Morokov²; ¹Central Aerohydrodynamic Institute, Russia ;²Institute of Biochemical Physics of RAS, Russia
12. Sep 18 17:30 18:00 3.3.4 CANCELED - NON-CONTACT MEASUREMENTS OF DEFORMATION OF LARGE-SIZED AIRCRAFT WING USING OPTICAL VIDEOGRAMMETRY METHOD
K.A. Kuruliuk, TsAGI, Russia
4.3RANS Models
Chair(s): Ilario, C.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
12. Sep 18 16:00 16:30 4.3.1 NUMERICAL INVESTIGATION OF FLOW STRUCTURE OF DIFFERENTIAL EJECTOR
H.Y. Zhang¹, Y.S. Yu¹, Q. Chen¹; ¹China Aerodynamics Research and Development Centre, China
12. Sep 18 16:30 17:00 4.3.2 MULTIPHASE TURBULENCE MODELS FOR SCRAMJETS AND ABLATING WALLS
K.E. Son, Russia
12. Sep 18 17:00 17:30 4.3.3 CANCELED - 2D-RANS APPROACH TO STUDY A TURBULENT SEPARATED FLOW USING BSL EARSM MODEL
S.M. Hanriot¹, M.D. Queiroz¹, G.L.F. Vasconcellos¹; ¹PUC Minas, Brazil
12. Sep 18 17:30 18:00 4.3.4 NUMERICAL COMPARISON OF STEADY DISTURBANCES IN THE WAKE OF PERIODIC BLOW-SUCTION AND ROUGHNESS ELEMENTS
P.V. Chuvakhov¹, S.V. Alexandrov¹, E.A. Alexandrova, Central Aerohydrodynamic Institute (TsAGI), Russia; ¹Moscow Institute of Physics and Technology (MIPT), Russia
5.3Optical Measurement Techniques
Chair(s): Takara, E.
Track 5
03.2 - Experimental Aerodynamics
12. Sep 18 16:00 16:30 5.3.1 CANCELED - AN EXPERIMENT INVESTIGATION ON SHOCKINDUCED TURBULENT BOUNDARY LAYER SEPARATION FLOW-FIELD
W.H.-R. Ruan, China; X.J.-X. Xiang, China; G. Kang, China; X.J.-Z. Zhao, China; Q.-S. Shen, China
12. Sep 18 16:30 17:00 5.3.2 PARTICLE IMAGE SURFACE FLOW VISUALIZATION AND SKIN-FRICTION MEASUREMENT
V.E. Mosharov¹, V.N. Radchenko¹, N.S. Tsipilev¹; ¹TsAGI, Russia
12. Sep 18 17:00 17:30 5.3.3 RELEASE OF DYNAMICALLY SCALED OBJECTS FROM A HELICOPTER WIND TUNNEL MODEL
K.H. Lammers, NLR, Netherlands; I. Philipsen, DNW, Netherlands; M.H. Ryu, KAI, South Korea
12. Sep 18 17:30 18:00 5.3.4 CANCELED - INVESTIGATION OF BDUNDARY LAYER TRANSITION MEASUREMENT IN SUBSONIC WIND TUNNEL USING TSP
J. Yu¹, L. Wei¹, X. Xiang¹, H. Wang¹, Z. Huang¹; ¹China Academy of Aerospace Aerodynamics, China
6.3Buffet and Separation Control
Chair(s): Prince, S.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
12. Sep 18 16:00 16:30 6.3.1 EFFECTIVE PLASMA BUFFET AND DRAG CONTROL FOR LAMINAR TRANSONIC AIROFOIL
P.A. Polivanov¹, A.A. Sidorenko¹; ¹ITAM SB RAS, Russia
12. Sep 18 16:30 17:00 6.3.2 CONTROL OF STRONG SEPARATION OF FLOW VIA SIMULTANEOUS-BLOWING-SUCTION TECHNIQUE
W. Stalewski, INSTITUTE of AVIATION, Poland
12. Sep 18 17:00 17:30 6.3.3 NUMERICAL OPTIMIZATION OF FLOW CONTROL BY TANGENTIAL JET BLOWING ON TRANSONIC AIRFOIL
K.A. Abramova¹, V.G. Soudakov¹; ¹TsAGI, Russia
12. Sep 18 17:30 18:00 6.3.4 OVERVIEW ON THE INFLUENCE OF COANDA BLANKET CURVATURE ON COANDA DEVICE PERFORMANCE
H. Djojodihardjo, Insitute for the Advancement of Aerospace Science and Technology, Indonesia
7.3High Speed Aerodynamics
Chair(s): Flatschart, R.
Track 7
03.4 - Applied Aerodynamics
12. Sep 18 16:00 16:30 7.3.1 ENGINE EXHAUST NOZZLE PLUME EFFECTS ON THE SONIC BOOM FOR A TYPE OF HYPERSONIC LONG-RANGE CIVIL VEHICLE
Z. Qian¹, Y. Leng¹, Z. Liu¹; ¹AVIC Aerodynamics Research Institute, China
12. Sep 18 16:30 17:00 7.3.2 PRELIMINARY STUDY OF THE AERODYNAMIC CHARACTERISTICS OF KRUEGER FLAP ON THE SST CONFIGURATION
D. Kwak, JAXA, Japan; K. Ohira, Ryoyu Systems, Japan
12. Sep 18 17:00 17:30 7.3.3 HIGH SPEED DRAG REDUCTION OPTIMIZATION FOR PROJECTILES
T. Wan¹, H.-C. Chang¹, C.-M. Liu¹; ¹Tamkang University, China
12. Sep 18 17:30 18:00 7.3.4 ADVANCED SONIC BOOM ANALYSIS USING FULL-FIELD SIMULATION
R. Yamashita, The University of Cambridge, United Kingdom
8.3Aeroelasticity 5 : General
Chair(s): Djojodihardjo, D.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
12. Sep 18 16:00 16:30 8.3.1 GLOBAL SENSITIVITY ANALYSIS OF TRANSONIC FLUTTER USING A COUPLED CFD-CSD SOLVER
R. Sandhu, Carleton University, Canada; W.X. Yuan, National Research Council (NRC) Canada, Canada; D. Poirel, Royal Military College (RMC) of Canada, Canada
12. Sep 18 16:30 17:00 8.3.2 NUMERICAL AND EXPERIMENTAL VALIDATION OF UNITIZED BEAM MODEL
F. Danzi¹, E. Cestino¹, G. Frulla¹, J.-M. Gibert, Purdue University, United States; ¹Politecnico di Torino, Italy
12. Sep 18 17:00 17:30 8.3.3 ASSESSMENT OF THE AERODYNAMICS AND AEROELASTICITY OF FLAPPING WING USING LINEARIZED COMPUTATIONAL METHOD
H. Djojodihardjo, Insitute for the Advancement of Aerospace Science and Technology, Indonesia; A.K. Joyodiharjo, The Institute for the Advancement of Aerospace Science and Techn, Indonesia
12. Sep 18 17:30 18:00 8.3.4 STRAIN GAGES FULL BRIDGE INSIDE COMPOSITE LAYERS TARGETING WING SHAPE FEEDBACK FOR FLIGHT CONTROL LAWS
A.A. Verri¹, J. Barros¹, F.L.S. Bussamra², F.J. Silvestre², F.J.O. Moreira¹, A.B. Guimarães Neto², C.E.S. Cesnik, UniMich, United States; J.S. Martins²; ¹Embraer S/A, Brazil ;²ITA, Brazil
9.3High Speed Propulsion 2
Chair(s): Kukshinov, N.
Track 9
05 - Propulsion
12. Sep 18 16:00 16:30 9.3.1 RESEARCH OF PROPULSION ENGINES FOR ADVANCE REUSABLE TSTO AEROSPACE SYSTEM
A.I. Lanshin¹, O.V. Sokolova¹, Y.M. Shikhman¹, V.E. Shlyakotin¹; ¹CIAM, Russia
12. Sep 18 16:30 17:00 9.3.2 CANCELED - CFD MODELLING TO OPTIMIZE THE MAXIMUM THRUST IN SCRAMJET ENGINE AND ANALYSIS OF ITS OPERATION PERFORMANCE
M-P Pires, IME, Brazil
12. Sep 18 17:00 17:30 9.3.3 SIMULTANEOUS MEASUREMENTS OF TEMPERATURE AND HEAT FLUX IN SUPERSONIC COMBUSTOR BY ITO THIN FILM THERMOCOUPLE
X.H. Jin¹, B.H. Ma¹, T. Qiu¹; ¹Northwestern Polytechnical University, China
12. Sep 18 17:30 18:00 9.3.4 GROUND FACILITY TESTS OF HIGH SPEED RAMJET DEMONSTRATORS
V.Y. Aleksandrov¹, A.N. Prokhorov¹, V.L. Semenov¹; ¹Central Institute of Aviation Motors , Russia
10.3Flight Dynamics & Identification 2
Chair(s): Doll, C.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
12. Sep 18 16:00 16:30 10.3.1 BIO-DYNAMIC STABILITY ANALYSIS OF A GREBE DURING MIGRATION
J. Feaster¹, B. Gater, Virginia Tech, United States; L. Straker², L. Jehl², J. Bayandor¹; ¹CRashworthiness for Aerospace Structures and Hybrids (CRASH Lab), United States ;²U.S. National Museum of Natural Sciences, United States
12. Sep 18 16:30 17:00 10.3.2 CANCELED - DYNAMIC REACTION OF AN AIRPLANE TO TRAILING VORTICES GENERATED BY ANOTHER AIRPLANE
G. Kowaleczko, Air Force Institute of Technology, Poland
12. Sep 18 17:00 17:30 10.3.3 MATHEMATICAL MODEL OF COMMERCIAL AIRPLANE DYNAMICS AT STALL
P.V. Kuzmin¹, N.A. Surkov¹, Y.F. Shelyukhin¹; ¹TsAGI, Russia
12. Sep 18 17:30 18:00 10.3.4 IDENTIFICATION OF THE LATERAL-DIRECTIONAL MODEL OF THE VECTOR-P, UNMANNED AERIAL VEHICLE
C. Fischer, Instituto Tecnológico de Aeronáutica and IFSP, Brazil; L.M. Nepomuceno¹, R.G.A. Silva¹, L.C.S. Góes¹; ¹Instituto Tecnológico de Aeronáutica, Brazil
11.3System Design
Chair(s): Peters, M.
Track 11
07 - Systems, Subsystems and Equipment
12. Sep 18 16:00 16:30 11.3.1 WIND SHEAR PARAMETER ESTIMATION FOR DYNAMIC SOARING WITH UNMANNED AERIAL VEHICLES
D. Liu, China Aerodynamics Research and Development Center, China; X. Gao, National University of Defense Technology, China
12. Sep 18 16:30 17:00 11.3.2 A METHODOLOGY FOR PRELIMINARY SIZING OF A THERMAL AND ENERGY MANAGEMENT SYSTEM FOR A HYPERSONIC VEHICLE
R. Fusaro¹, D. Ferretto¹, V. Vercella¹, N. Viola¹, V. Fernandez Villace², J. Steelant ²; ¹Politecnico di Torino, Italy ;²ESA-ESTEC, Netherlands
12. Sep 18 17:00 17:30 11.3.3 INTEGRATION OF ON-BOARD SYSTEMS PRELIMINARY DESIGN DISCIPLINE WITHIN A COLLABORATIVE 3RD GENERATION MDO FRAMEWORK
L. Boggero¹, M. Fioriti², F. Tomasella², P.D. Ciampa¹; ¹German Aerospace Center, Germany ;²Politecnico di Torino, Italy
12. Sep 18 17:30 18:00 11.3.4 FAULT DIAGNOSIS METHOD STUDY FOR COMPLEX SYSTEM BASED ON KALMAN FILTERS
W. Niu¹, J. Cheng, Xi’an Institute of Applied Optics, China; W. Niu¹; ¹AVIC Computing Technique Research Institute, China
12.3Human Factors
Chair(s): Consiglio, M.
Track 12
10 - Safety and Security
12. Sep 18 16:00 16:30 12.3.1 3D AUDIO SUPPORT FOR HELICOPTER PILOTS DURING CONFINED AREA LANDINGS
C.A. Niermann, German Aerospace Center (DLR), Germany
12. Sep 18 16:30 17:00 12.3.2 INDIVIDUALIZING FLIGHT SKILL TRAINING USING SIMULATOR DATA ANALYSIS AND BIOFEEDBACK
J.O. Entzinger¹, T. Uemura¹, S. Suzuki¹; ¹The University of Tokyo, Japan
12. Sep 18 17:00 17:30 12.3.3 DESIGN OF A DISTRIBUTED HUMAN FACTORS LABORATORY FOR FUTURE AIR SYSTEMS
J. Alfredson, Saab, Sweden; B.J.E. Johansson¹, L.G. Trabasso, ITA, Brazil; J. Schminder¹, R. Granlund, RISE, Sweden; R. Gårdhagen¹; ¹Linköping University, Sweden
12. Sep 18 17:30 18:00 12.3.4 CREW TRAINING USING ANIMATION
P.M. Razaboni, Embraer SA, Brazil