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 - Future of Propulsion, Dr. Ric Parker president ISABE, Dr. Frank Anton AIRBUS industries
Chair: D. Müller-Wiesner
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 AN ADVANCED SOFTWARE ENVIRONMENT FOR CONCEPTUAL AND PRELIMINARY 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
Charles M. Boozer¹, Ali 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 SAFETY ORIENTED ODM VTOL PRE-DESIGN METHODOLOGY
F. Rougier, SAFRAN, France
12. Sep 18 11:30 12:00 1.1.5 HURRICANE-CS: CONTROL SURFACES AND HIGH LIFT DEVICES MODELING AND SIZING PROGRAM
C. López Sánchez, Spain; D. Sánchez Franco, Spain; Raghu Chaitanya Munjulurynjulury, Sweden
Reserve Paper 1.1.R 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
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 MBSE FLIGHT TEST ARCHITECTURE RESEARCH
xiao hua¹, chen qing¹, shengjun qi, cfte, China; ¹CFTE, 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. Schwartz, Georgia 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, UNIFEI, 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, B. García-Fogeda ¹, I. Rivero¹, J. Gómez-Escalonilla¹; ¹AIRBUS DS, Spain
12. Sep 18 10:00 10:30 3.1.2 MODE I FATIGUE INDUCED DELAMINATION IN CO-CURED AND CO-BONDED COMPOSITE STRUCTURAL JOINTS
F. M. Gonzalez Ramirez, Instituto Tecnológico de Aeronáutica, Brazil
12. Sep 18 10:30 11:00 3.1.3 USING THE LEAD CRACK CONCEPT TO REDUCE DURABILITY TEST DURATION
Loris Molent, DST, Australia
12. Sep 18 11:00 11:30 3.1.4 INFLUENCE OF IRREGULAR LOADING PARAMETERS ON CFRP COMPONENTS FATIGUE LIFE
A.G. Kalinin, Central Aerohydrodynamic Institute, TsAGI, Russia
12. Sep 18 11:30 12:00 3.1.5 OPTIMIZATION OF REINFORCEMENT HEIGHT PARAMETERS FOR AIRCRAFT PANEL STRUCTURES BASED ON VIBRATION FATIGUE DAMAGE ANALYSIS
Peng LI¹, Junfeng MA¹; ¹Aircraft strength research institute, China
4.1Turbulence Modeling and LES
Chair(s): Hackström, M., Bigarella, E.
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, University of Kansas, United States
12. Sep 18 10:00 10:30 4.1.2 TURBULENCE MODEL CONDITIONING FOR VORTEX DOMINATED FLOWS BASED ON EXPERIMENTAL RESULTS
Matteo Moioli¹, Christian Breitsamter¹, Kaare 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
Wang Yue¹, Liu Kang¹, Song Wenping¹, Han Zhonghua¹; ¹Northwestern Polytechnical University, China
12. Sep 18 11:00 11:30 4.1.4 AERODYNAMIC EVALUATION OF THE EXTERNAL FLOW OVER NOTCHBACKS AND PICKUP TRUCKS
E.-K. Mascia, Federal University of Uberlandia, Brazil
Reserve Paper 4.1.R LARGE EDDY SIMULATION OF A TRANSIENT SPOILER DEPLOYMENT IN A NACA0012 PROFILE IN SUBSONIC AND TRANSONIC SPEEDS
R. V. LINN, FEDERAL UNIVERSITY OF RIO GRANDE DO SUL (UFRGS), Brazil
5.1Unsteady Flows and Aeroacoustics
Chair(s): Yingchun, C.
Track 5
03.2 - Experimental Aerodynamics
12. Sep 18 09:30 10:00 5.1.1 UNSTEADY AERODYNAMIC CHARACTERISTICS OF THE OSCILLATING AIRFOIL USING MSBS
Y.H. Sung¹, J.S. Han¹, J.H. Han¹; ¹KAIST, South Korea
12. Sep 18 10:00 10:30 5.1.2 DESIGN OF AN INSTRUMENTED STATOR VANE USING MEMS MICROPHONES FOR UNSTEADY PRESSURE MEASUREMENTS AT THE EESC-USP FAN RIG
B Martinez R Jr¹, LC Caldas¹, RG Cuenca, Federal University of Santa Catarina, Brazil; R Lauterjung Q, Embraer S/A, Brazil; PC Greco Jr¹; ¹University of Sao Paulo, Brazil
12. Sep 18 10:30 11:00 5.1.3 EVALUATION OF TRANSONIC BUFFETING ONSET BOUNDARY ESTIMATED BY TRAILING EDGE PRESSURE DIVERGENCE AND RMS DATA OF WING VIBRATION
Rodrigo Sorbilli Sousa, EMBRAER, Brazil; Roberto Gil A. da Silva¹, Roberto da Motta Girardi¹; ¹ITA, Brazil
12. Sep 18 11:00 11:30 5.1.4 CHALLENGES OF AERO-ACOUSTIC MEASUREMENTS IN WIND TUNNEL: IDENTIFICATION AND ELIMINATION OF “PARASITE” NOISE
Yifeng Sun¹, Cyrille Breard¹, Xianping Li¹, Yingchun Chen¹; ¹Shanghai Aircraft Design and Research Institute of COMAC, China
12. Sep 18 11:30 12:00 5.1.5 TIME-RESOLVED PRESSURE MEASUREMENTS FOR AN AIRFOIL WITH SELF-SUSTAINED SHOCKWAVE OSCILLATIONS
H. F. Leite¹, A. C. Avelar, Brazil; R. G. A. Silva¹; ¹ITA, Brazil
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 EFFECTS OF THE INTRINSIC THREE-DIMENSIONALIZATION OF SEPARATION BUBBLES ON THE AMPLIFICATION OF EXTERNAL DISTURBANCES
Daniel Rodriguez, Universidade Federal Fluminense, Brazil; Elmer Mateus Gennaro, Sao Paulo State University, Brazil
12. Sep 18 10:00 10:30 6.1.2 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 10:30 11:00 6.1.3 CONTROL OF COMPLEX DISTURBANCES IN THE BOUNDARY LAYER OVER A FLAT PLATE.
P. Morra¹, K. Sasaki², A. Cavalieri², A. Hanifi¹, D.S. Henningson¹; ¹KTH Royal Institute of Technology, Sweden ;²Instituto Tecnológico de Aeronáutica, Brazil
12. Sep 18 11:00 11:30 6.1.4 DEVELOPMENT OF SECONDARY CROSSFLOW INSTABILITY NEAR BREAKDOWN TO TURBULENCE
C J Atkin, City, University of London, United Kingdom
12. Sep 18 11:30 12:00 6.1.5 LAMINAR-TURBULENT TRANSITION MECHANISMS OVER WIDELY-SPACED SUCTION HOLES
C J Atkin, City, University of London, United Kingdom
7.1Aircraft Aerodynamic Design
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
12. Sep 18 09:30 10:00 7.1.1 CONCEPT OF MEDIUM TWIN-ENGINE STOL TRANSPORT AIRPLANE
O.V. Pavlenko¹, A.V. Petrov¹, E.A. Pigusov¹; ¹TsAGI, Russia
12. Sep 18 10:00 10:30 7.1.2 ANALYSIS AND DESIGN OF WING TRAILING EDGE MOUNTED OVER-THE-WING DISTRIBUTED PROPULSION
L.L.M. Veldhuis¹, A Khajehzadeh¹, S.J. Hullshoff¹; ¹Delft University of Technology, Netherlands
12. Sep 18 10:30 11:00 7.1.3 CEA ENGINEERING IMPACTING THE RED BULL AIR RACE
G. A. Santana, Aeron Engenharia, Brazil
12. Sep 18 11:00 11:30 7.1.4 A COMPARISON STUDY ON TRANSITION CHARACTERISTICS OF NLF FORWARD-SWEPT WING AND AFT-SWEPT-WING
Z. Zhu¹, W.-P. Song¹, Z.-H. Han¹, J.-H. Xu¹; ¹Northwestern Polytechnical University, China
12. Sep 18 11:30 12:00 7.1.5 OUTBOARD SPLIT FLAP AERODYNAMICS OF A FLYING WING CONFIGURATION
S. Pfnür¹, C. Breitsamter¹; ¹Technical University of Munich, Germany
Reserve Paper 7.1.R ROBUST DESIGN OPTIMIZATION OF BENCHMARK AERODYNAMIC CASE BASED ON POLYNOMIAL CHAOS EXPANSION
Zhao Huan¹, Gao Zhenghong¹; ¹Northwestern Polytechnical University , China
Reserve Paper 7.1.R PRACTICAL APPLICATIONS OF VISCOUS FULL-POTENTIAL CFD CODES
David Philpott¹, Kevin Hackett¹; ¹IHS Markit (ESDU), United Kingdom
8.1Aeroelasticity 1 : Methods and Modeling
Chair(s): Willcox, K., Gil, R.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
12. Sep 18 09:30 10:00 8.1.1 NUMERICAL AND EXPERIMENTAL INVESTIGATION OF AEROELASTIC TAILORED SWEPT WINGS MADE OF UNIDIRECTIONAL AND TOW-STEERED FRC
H. L. Lebkuchen, Instituto Tecnológico de Aeronáutica , Brazil; C. E. de Souza, Universidade Federal de Santa Maria, Brazil; R. G. A. da Silva, Instituto Tecnológico de Aeronáutica, Brazil
12. Sep 18 10:00 10:30 8.1.2 AEROELASTIC TAILORING OF COMPOSITE WING BY USING MULTIDISCIPLINARY DESIGN ENVIRONMENT
K.A. Balunov¹, V.V. Chedrik¹, F.Z. Ishmuratov¹; ¹TsAGI, Russia
12. Sep 18 10:30 11:00 8.1.3 INTERRELATION BETWEEN THE LOADING AND THE AEROELASTICITY CHARACTERISTICS OF MEDIUM RANGE AIRCRAFT IN TRANSONIC FLOW
A. Chizhov, TsAGI, Russia
12. Sep 18 11:00 11:30 8.1.4 VIRTUAL AIRCRAFT MODEL FOR AEROELASTIC SIMULATION AND LOAD PREDICTION OF A HIGH ASPECT RATIO COMPOSITE SWEPT WING
A. Hermanutz¹, M. Hornung¹; ¹Technical University of Munich, Germany
12. Sep 18 11:30 12:00 8.1.5 THERMAL-MECHNICAL COUPLING ANALYSIS AND OPTIMIZATION DESIGN ON TPS WITH GAP
Shiyu Huo¹, Qun Yan¹, Weihua Xie, Harbin Institute of Technology , China; ¹Aircraft Strength Research Institute, China
9.1Fan and Propeller
Chair(s): Yimer, I., Lamiscarre, B.
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
Xudong Yang¹, Jianhua Xu¹, Bo Wang¹, Chao Song¹, Shunlei 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 STAGES DESIGNING FOR ADVANCED AIRCRAFT ENGINES
Sergey Pankov¹, Victor Mileshin¹, Igor Orekhov¹, Victor Fateev¹; ¹Central Institute of Aviation Motors, Russia
12. Sep 18 11:00 11:30 9.1.4 AN INTEGRATED PROPULSION SYSTEM FOR BI-MODAL UNMANNED VEHICLES
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; EESC-USP EESC-USP¹, B. M. dit245¹; ¹EESC-USP, Brazil
10.1Flight Control 1
Chair(s): ,
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
12. Sep 18 09:30 10:00 10.1.1 EVALUATION OF ALTITUDE CONTROL FOR AN AIRBREATHING HYPERSONIC AIRCRAFT MODEL
Masaharu Hiruma, The University of Tokyo, Japan
12. Sep 18 10:00 10:30 10.1.2 A COMPARISON BETWEEN UNIVERSAL INTEGRAL REGULATOR AND LINEAR QUADRATIC TECHNIQUE FOR AN AIRCRAFT AUTOPILOT
Y. A. Díaz-Méndez¹, M. S. Sousa¹, S. S. Cunha¹, G. F. Gomes¹; ¹Federal University of Itajubá, Brazil
12. Sep 18 10:30 11:00 10.1.3 MULTI-VARIABLE AIRCRAFT DIRECTIONAL CONTROL WITH ANTI-SKID DIFFERENTIAL BRAKES
G. Di Rito¹, R. Galatolo¹, F. Schettini¹; ¹Università di Pisa - Dip. Ing. Civile ed Industriale, Italy
12. Sep 18 11:00 11:30 10.1.4 PASSIVE CONTROL METHOD IN ATTENUATING SELF-INDUCED ROLL OSCILLATIONS OF LOW-ASPECT-RATIO WINGS USING OBLIQUE SLOT BLEED
T. Hou¹, C. Chen¹, T Hu¹; ¹Lu Shijia Labortory, Beihang University, China
11.1UAS Flight Test
Chair(s): Götzendorf-Grabowski, T.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
12. Sep 18 09:30 10:00 11.1.1 METHODS FOR EFFICIENT FLIGHT TESTING AND MODELLING OF REMOTELY PILOTED AIRCRAFT WITHIN VISUAL LINE-OF-SIGHT
A. Sobron¹, D. Lundström¹, R. Larsson², P. Krus¹, C. Jouannet²; ¹Linköping University, Sweden ;²Saab Aeronautics, Sweden
12. Sep 18 10:00 10:30 11.1.2 VERTICAL LANDING OF A FIXED-WING UAV USING THE FLAT SPIN
S. Higashino, Kyushu University, Japan; K. Nakama, Kyushu University, Graduate Student, Japan
12. Sep 18 10:30 11:00 11.1.3 PLANNING, IMPLEMENTATION, AND EXECUTION OF AN AUTOMATIC FIRST FLIGHT OF A UAV
M. E. Kügler¹, F. Holzapfel¹; ¹Technical University of Munich, Inst. of Flight System Dynamics, Germany
12. Sep 18 11:00 11:30 11.1.4 SAFETY FLIGHT TESTING FOR CARGO UAV DEVELOPMENT
Kakuya Iwata¹, Keisuke Yamada¹, Ryuzo Horiuchi¹, Akiya Kamimura¹; ¹National Institute of Advanced Industrial Science and Technology, Japan
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 AIRPORT 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
Timo 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 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
DK Jeon, Korea Aerospace Research Institute, South Korea

12:00 - 13:00Lunch

0.2General Lecture IV - Developing and flying the Gripen E - M. Wandt, SAAB, Sweden
Chair:
12. Sep 18 13:00 13:45

1.2Design Education 2
Chair(s): Bagassi, S.
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 AN OVERVIEW OF THE FIRST PARAGUAYAN NEAR SPACE EXPLORATION USING A HIGH ALTITUDE BALLOON
A. Jara¹, F. Kanazawa¹, L. Vielman, AEP, Paraguay; J. Kurita¹; ¹FPUNA, Paraguay
12. Sep 18 15:00 15:30 1.2.3 ELECTRIC VTOL UAV CONFIGURATION STUDIES AND OPTIMIZATION WITHIN AIRCRAFT DESIGN PRACTICAL COURSE AT TECHNICAL UNIVERSITY
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 DRONES AS AN EMERGING PREDICTIVE MAINTENANCE TOOL.
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 DIGITAL TRANSFORMATION IN AIRLINE MAINTENANCE
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
3.2Physics Based Damage Modeling
Chair(s): Nutt, S.
Track 3
04.1 - Material Issues, Fatigue and Damage Tolerance
12. Sep 18 14:00 14:30 3.2.1 MODELING AND SIMULATION OF MIXED MODE FATIGUE-INDUCED DELAMINATION IN COMPOSITE: A COMPARATIVE STUDY
L. A. de Oliveira¹, D. S. Alves¹, M. V. Donadon¹; ¹Instituto Tecnológico de Aeronáutica, Brazil
12. Sep 18 14:30 15:00 3.2.2 COMPARISON OF TWO DIFFERENT INDICATORS FOR HOT CRACKING IN WELDED STRUCTURES
J Edberg¹, J Draxler¹, J Andersson, University West, Sweden; ¹Luleå University of Technology, Sweden
12. Sep 18 15:00 15:30 3.2.3 THE IMPORTANCE OF SECONDARY BENDING EVALUATION IN STRUCTURAL JOINT ANALYSIS
W. R. P. Mendonça, EMBRAER S.A., Brazil
Reserve Paper 3.2.R ON ELASTIC PSEUDO-ISOTROPIC ORTHOTROPIC PLATES
L.M.B.C. Campos, Instituto Superior Tecnico, Portugal
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 DEVELOPMENT OF A NUMERICAL ENVIRONMENT TO PREDICT BOUNDARY LAYER TRANSITION
A.P. Antunes¹, R. Cosin¹; ¹Embraer, Brazil
12. Sep 18 15:00 15:30 4.2.3 MACHINE LEARNING APPROACH TO THE INTERMITTENCY TRANSITION TURBULENCE MODEL FOR WIND TURBINE APPLICATION
M.A. Abd Bari¹, A. Da Ronch¹, M. Panzeri, Noesis Solutions, Belgium; J. Drofelnik¹; ¹University of Southampton, United Kingdom
5.2Aerodynamic Experiments
Chair(s): Takana, 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. Granzoto Granzoto¹, G.J. Zambrano Zambrano¹, G.G. Becker Becker¹, L. A. Algodoal Algodoal¹; ¹Embraer, Brazil
12. Sep 18 15:00 15:30 5.2.3 EXPERIMENTAL AND CFD ANALYSIS OF A UAV FOR SUPERFICIAL VOLCANO SURVEILLANCE
L Botero-Bolivar¹, D Acevedo-Giraldo¹, H D Cerón-Muñoz¹, F 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
Guilherme A Freire¹, André V G Cavalieri¹, Flávio 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
7.2New Structural Design 2: Morphing Structures
Chair(s): Ikeda, T.
Track 7
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
12. Sep 18 14:00 14:30 7.2.1 STRUCTURAL INTEGRITY DIAGNOSIS FOR AGING TRANSPORT AIRCRAFT BASED ON FLIGHT DATA
H. Wang, College of General Aviation, Wenzhou University, China
12. Sep 18 14:30 15:00 7.2.2 INFLUENCE OF UNCERTAIN PARAMETERS AFFECTING THE DYNAMIC BEHAVIOR OF A FLEXIBLE DISC
A.A.C.J. Cavalini Jr, Federal University of Uberlandia, Brazil
12. Sep 18 15:00 15:30 7.2.3 A RESEARCH OF ZIMMERMAN-WEISSENBURGER-YANG METHOD FOR FLUTTER BOUNDARY PREDICTION
YANG FEI, Shang Hai Aircraft Design and Research Institute of COMAC, China
Reserve Paper 7.2.R A RESEARCH OF MULTIDISCIPLINARY DESIGN OPTIMIZATION ALGORITHM FOR FIGHT VEHICLE DESIGN
Xiqiang YAN¹, Zongzheng LIU¹, Yisheng YANG¹; ¹CARDC, China
8.2Aeroelasticity 6 : 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
Bai Yuguang¹, Qian Wei¹, Chen Xiangyan¹; ¹Dalian University of Technology, China
12. Sep 18 14:30 15:00 8.2.2 MULTIDISCIPLINARY METHOD 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
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
N V Kukshinov, CIAM, Russia
12. Sep 18 14:30 15:00 9.2.2 COMPLEX NUMERICAL AND EXPERIMENTAL RESEARCH OF HEXAFLY-INT HIGH-SPEED CIVIL AICRAFT MODEL
N V Kukshinov, CIAM, Russia
12. Sep 18 15:00 15:30 9.2.3 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 SYSTEM IDENTIFICATION USING SUBSPACE METHOD OF A FLEXIBLE AIRCRAFT OPERATING IN CLOSED-LOOP
Raphaela C M G Barbosa¹, Luiz 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, ITA Technological Institute of Aeronautics, Brazil
11.2Air Data
Chair(s): ,
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
R. A. Souza¹, M. L. Oliveira¹, S. P. L. Vieira¹, W. O. Avelino¹, C. F. R. Oliveira¹, D. W. de Lima Monteiro¹, F. S. Torres¹, R. M. O. Hansen, SDU, 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
12.2On Demand Mobility: Integration in Civil Airpace
Chair(s): Kageyama, K.
Track 12
09 - Air Transport System Efficiency
12. Sep 18 14:00 14:30 12.2.1 SIMULATION STUDY FOR VFR AIRCRAFT AND SMALL UNMANNED AIRCRAFT SYSTEMS (SUAS) MIXED OPERATIONS IN LOW LEVEL AIRSPACE
H Hirabayashi¹, D Toratani¹, A Kohmura¹; ¹ENRI, Japan
12. Sep 18 14:30 15:00 12.2.2 URBAN AIR TRANSPORTATION JOURNEY TIME COMPARISON FOR MELBOURNE METROPOLITAN AREA
Lewis Swadesir¹, Cees Bil¹; ¹RMIT University, Australia
12. Sep 18 15:00 15:30 12.2.3 ADAPTIVE LANDING SEQUENCING IN AIR TRAFFIC FLOW OPTIMISATION
M. Hickson¹, C. Bil¹; ¹RMIT University, Australia

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 FLEXFLOIL SHAPE ADAPTIVE CONTROL SURFACES—FLIGHT TEST AND NUMERICAL RESULTS
Sridhar Kota, FlexSys Inc, United States; Joaquim Martins, University of Michigan, United States
12. Sep 18 16:30 17:00 1.3.2 FEASIBILITY STUDY OF MODIFYING A KEROSENE AIRCRAFT TO A LH2 POWERED VERSION
Wenqing XIE¹, Zhuoyi Duan¹, Howard Smith, Cranfield University, United Kingdom; ¹AVIC The First Aircraft Institute, China
12. Sep 18 17:00 17:30 1.3.3 DEVELOPMENT OF THE REGENERATIVE SOARER, THEORETICAL AND PRACTICAL ASPECTS
R.C. Carvalho, EMBRAER S.A., Brazil
12. Sep 18 17:30 18:00 1.3.4 DEVELOPMENT OF A NOVEL AERIAL PLATFORM WHICH MERGES THE CONCEPT OF ARSHIPS 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
2.3Alternative Energy and Distributed Propulsion Aircraft
Chair(s): Isikveren, A.
Track 2
01 - Aircraft Design and Integrated Systems
12. Sep 18 16:00 16:30 2.3.1 INTEGRATED TURBO-ELECTRIC MOTIVE POWER SYSTEMS FOR REGIONAL TRANSPORT APPLICATIONS
A.T. Isikveren, SAFRAN S.A., France
12. Sep 18 16:30 17:00 2.3.2 DEVELOPING THE UNMANNED UNCONVENTIONAL CARGO AIRPLANES WITH HYBRID PROPULSION SYSTEM
J. Rohacs, Department of Aeronautics, Naval Architecture and Railway Vehicl, Hungary
12. Sep 18 17:00 17:30 2.3.3 OPTIMIZATION OF MOTOR FOR THE MAXIMIZATION OF SOLAR-POWERED AIRCRAFT PERFORMANCE
Sergey Serokhvostov, MIPT, Russia; Tatyana Churkina, MAI, Russia
12. Sep 18 17:30 18:00 2.3.4 INVERSE AIRCRAFT DESIGN FOR MARKETSHARE
J.G. Gibbs, Savion Aerospace, United States
3.3Advanced Manufacturing and Non Destructive Testing
Chair(s): Lewis, K.
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 FUNDAMENTAL APPROACHES FOR METAL-COMPOSITE STRUCTURES LOADING PROGRAMS EQUIVALENCE FOR FULL-SCALE SERVICE LIFE TEST
Andrey Pankov¹, Viktor Konovalov¹; ¹TsAGI, Russia
12. Sep 18 17:00 17:30 3.3.3 STUDY OF EXTERNAL FACTORS COMBINATION EFFECT ON CFRP BULK STRUCTURE UTILIZING ULTRASONIC MICROSCOPY
Tatiana Ryzhova¹, Alexander Shanygin¹, Vladimir Scherbakov¹, Yulia Petronyuk², Vadim Levin², Egor Morokov²; ¹Central Aerohydrodynamic Institute, Russia ;²Institute of Biochemical Physics of RAS, Russia
12. Sep 18 17:30 18:00 3.3.4 NON-CONTACT MEASUREMENTS OF DEFORMATION OF LARGE-SIZED AIRCRAFT WING USING OPTICAL VIDEOGRAMMETRY METHOD
K.A. Kuruliuk, TsAGI, Russia
4.3Hypersonic Flow
Chair(s): Alves, L.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
12. Sep 18 16:00 16:30 4.3.1 RESEARCH ON EXTERNAL AERODYNAMICS OF THE HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJ
N.V. Voevodenko¹, A.A. Gubanov¹; ¹TsAGI, Russia
12. Sep 18 16:30 17:00 4.3.2 RANS AND DSMC FLOW SIMULATIONS OVER TYPICAL HYPERSONIC CONFIGURATIONS
R. R. P. P. Pereira, IAE, Brazil
12. Sep 18 17:00 17:30 4.3.3 UNSTRUCTURED COMPRESSIBLE NAVIER-STOKES SOLVER FOR HIGH ALTITUDE FLOWS
C. Baek, Inha university, South Korea
12. Sep 18 17:30 18:00 4.3.4 TRIM DRAG MINIMIZATION AT CRUISE FLIGHT OF A HIGH-SPEED PASSENGER VEHICLE
S.A. Takovitskii, Central Aerohydrodynamic Institute, Russia; V.F. Villace, European Space Agency, Netherlands
Reserve Paper 4.3.R LONGITUDINAL STABILITY DESIGN CRITERIA FOR HYPERSONIC GLIDERS
B.Y. Chen, China Academy of Aerospace Aerodynamics, China
Reserve Paper 4.3.R CFD PACKAGE \"FLOW VISION\", FOR SIMULATIONS AND IMITATION MODELING OF HYPERSONIC VEHICLES
E.E.Son Son, Joint Institute for High Temperature RAS, Russia
5.3History of Aeronautics
Chair(s): Lott, M., Brandao, M.P.
Track 5
12 - Host nation
12. Sep 18 16:00 16:30 5.3.1 THE SANTOS-DUMONT LEGACY TO AERONAUTICS
M. P. Brandão, ITA, Brazil
12. Sep 18 16:30 17:00 5.3.2 BRAZILIAN AVIATION HISTORY: THE UNIVERSITY OF SÃO PAULO CASE
F.M. catalano, University of São Paulo -EESC-USP, Brazil
12. Sep 18 17:00 17:30 5.3.3 THE STUDY OF TURBORAMJETS IN CIAM
Vladimir Palkin¹, Pavel Kadjardouzov¹, Valentin Solonin¹, Mikhail Tskhovrebov¹; ¹CIAM, Russia
12. Sep 18 17:30 18:00 5.3.4 HISTORY OF AVIATION IN MINAS GERAIS
E. Bauzer, Brazil
6.3Buffet and Separation Control
Chair(s): Breitsamter, C., 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 AEROFOIL
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
V.G. Soudakov¹, K.A. Abramova¹; ¹TsAGI, Russia
12. Sep 18 17:30 18:00 6.3.4 CFD ANALYSIS OF COAND? BLANKET CURVATURE ON COAND? DEVICE PERFORMANCE
Harijono DJOJODIHARDJO, Insitute for the Advancement of Aerospace Science and Technology, Indonesia
7.3Propellors and Rotors
Chair(s): Monk, J.
Track 7
03.4 - Applied Aerodynamics
12. Sep 18 16:00 16:30 7.3.1 APPLICATION OF HIGH-ROBUSTNESS BEMT FOR SIMULATION OF UAV-VTOL PROPELLER AT LOW/HIGH ADVANCE RATIO
Zhongyun Fan¹, Zhou Zhou¹, Xiaoping Zhu, Science and Technology on UAV Laboratory, NPU, China; ¹School of Aeronautics,Northwestern Polytechnical University, China
12. Sep 18 16:30 17:00 7.3.2 DESIGN OFA DOUBLE-ENDED AIRFOIL IN UNSTEAD REVERSE FLOW
X. -D. YANG¹, M. HUANG¹; ¹School of Aeronautics Northwestern Polytechnical University, China
12. Sep 18 17:00 17:30 7.3.3 INVESTIGATION ON APPROACH TO CONTROL LIFT DISTRIBUTION OF WING BY DISTRIBUTED PROPELLERS
Zhou Zhou¹, Hong-bo Wang¹; ¹Northwestern Polytechnical University, China
12. Sep 18 17:30 18:00 7.3.4 CFD SIMULATION OF XH-59A ROTOR IN HOVER AND 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
Reserve Paper 7.3.R SIMULATIONS OF UNSTEADY AIRWAKES BEHIND SHIPS IN MOTION
Weixing Yuan¹, Alanna Wall¹, Richard Lee¹; ¹National Research Council Canada, Canada
Reserve Paper 7.3.R THE EFFECTS OF BLADE ASPECT RATIO AND TAPER RATIO ON THE HOVERING PERFORMANCE OF THE CYCLOIDAL ROTOR
Y.Hu Hu, Northwestern polytechnich university, China
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
Rimple Sandhu, Carleton University, Canada; Weixing Yuan, National Research Council (NRC) Canada, Canada; Dominique 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 COMPUTATIONAL STUDY OF THE AERODYNAMICS AND AEROELASTICITY OF FLAPPING WING
Harijono DJOJODIHARDJO, Insitute for the Advancement of Aerospace Science and Technology, Indonesia; Airlangga 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 CFD MODELLING TO OPTIMIZE THE MAXIMUM THRUST IN SCRAMJET ENGINE AND ANALYSIS OF ITS OPERATION PERFORMANCE
M-P Pires, IME, Brazil
12. Sep 18 16:30 17:00 9.3.2 RESEARCH OF PROPULSION ENGINES FOR ADVANCE REUSABLE TSTO AEROSPACE SYSTEM
A.I. Lanshin¹, O.V. Sokolova¹, Yu.M. Shikhman¹, V.E. Shlyakotin¹; ¹CIAM, Russia
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
Jin Xinhang¹, Ma Binghe¹, Qiu Tao¹; ¹Northwestern Polytechnical University, China
12. Sep 18 17:30 18:00 9.3.4 GROUND FACILITY TESTS OF HIGH SPEED RAMJET DEMONSTRATORS
A Prokhorov, CIAM, Russia
10.3Flight Dynamics & Identification 2
Chair(s): Watanabe, Y.
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 Feaster, Virginia Tech, United States
12. Sep 18 16:30 17:00 10.3.2 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.F Fischer, Instituto 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
Duoneng Liu, China Aerodynamics Research and Development Center, China; Xianzhong Gao, National University of Defense Technology, China
12. Sep 18 16:30 17:00 11.3.2 A METHODOLOGY FOR PRELIMINARY SIZING OF A VEHICLE 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
Luca Boggero¹, Marco Fioriti², Francesca Tomasella², Pier Davide 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
Wei Niu¹, Juan Cheng, Xi’an Institute of Applied Optics, China; Wensheng 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 LABORATOTY 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
Reserve Paper 12.3.R HUMAN RELIABILITY ANALYSIS IN AN AIRCRAFT DECOMPRESSION EVENT
C. Reiser¹, A. Bayma¹, D.A. Fonseca¹; ¹Embraer S/A, Brazil
Reserve Paper 12.3.R 3D PERSPECTIVE VIEWS ON IMMERSIVE HEAD-WORN DISPLAYS - CAN EXOCENTRIC VIEWS INCREASE PILOT SITUATIONAL AWARENESS?
J. M. Ernst, DLR, Germany