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, Ric Parker president ISABE
Chair: Parker, Anton, Cueille
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 ON THE DEVELOPMENT OF A FLEXIBLE KNOWLEDGE-BASED MODEL GENERATOR FOR APPLICATION IN MULTI-LEVEL MDO PROCESSES
J Jepsen, German Aerospace Center (DLR), Germany
12. Sep 18 10:00 10:30 1.1.2 AN ADVANCED SOFTWARE ENVIRONMENT FOR CONCEPTUAL AND PRELIMINARY AIRCRAFT DESIGN
M. Ruocco, Italy
12. Sep 18 10:30 11:00 1.1.3 COUPLED-ADJOINT AEROSTRUCTURAL OPTIMIZATION FRAMEWORK FOR PRELIMINARY AIRCRAFT DESIGN
A. Elham, Braunschweig University of Technology, Germany
12. Sep 18 11:00 11:30 1.1.4 AIRCRAFT LOADS PREDICTION USING ENHANCED SIMULATION
Y Lemmens, Siemens PLM Software, Belgium
12. Sep 18 11:30 12:00 1.1.5 SAFETY ORIENTED ODM VTOL PRE-DESIGN METHODOLOGY
F. Rougier, SAFRAN, France
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
X.H Xiao, China Flight Test Establishment, 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
3.1Advanced Manufacturing and Non Destructive Testing
Chair(s): Lewis, K.
Track 3
04.1 - Material Issues, Fatigue and Damage Tolerance
12. Sep 18 09:30 10:00 3.1.1 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 10:00 10:30 3.1.2 DAMAGE CHARACTERIZATION ON LIGHTWEIGHT STRUCTURES USING NON-DESTRUCTIVE TECHNIQUES
D. V. Vargas, Exova Materials Technology AB, Sweden
12. Sep 18 10:30 11:00 3.1.3 FUNDAMENTAL APPROACHES FOR METAL-COMPOSITE STRUCTURES LOADING PROGRAMS EQUIVALENCE FOR FULL-SCALE SERVICE LIFE TEST
V Pankov, TsAGI, Russia
12. Sep 18 11:00 11:30 3.1.4 ADDITIVE MANUFACTURING OF METALLIC COMPONENTS THROUGH DIRECT LASER DEPOSITION AND POWDER FEEDING
L. E. dos Santos Paes, Federal University of Santa Catarina, Brazil
12. Sep 18 11:30 12:00 3.1.5 STUDY OF EXTERNAL FACTORS COMBINATION EFFECT ON CFRP BULK STRUCTURE UTILIZING ULTRASONIC MICROSCOPY
T. Ryzhova, TsAGI, Russia
Reserve Paper 3.1.R NON-CONTACT MEASUREMENTS OF DEFORMATION OF LARGE-SIZED AIRCRAFT WING USING OPTICAL VIDEOGRAMMETRY METHOD
K.A. Kuruliuk, TsAGI, Russia
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 INSTABILITY ANALYSIS OF SUBSONIC COMPRESSBLE FLOWS OVER AN OPEN CAVITY
M.S. Mathias, São Carlos School of Engineering - University of São Paulo, Brazil
12. Sep 18 10:30 11:00 4.1.3 TURBULENCE MODEL CONDITIONING FOR VORTEX DOMINATED FLOWS BASED ON EXPERIMENTAL RESULTS
M. Moioli, Technical University of Munich, Germany
12. Sep 18 11:00 11:30 4.1.4 IMPROVED DELAYED DETACHED EDDY SIMULATION OF THE FLOWS AROUND S809 AIRFOIL FOR ANGLES OF ATTACK FROM 0 TO 90 DEGREES
Y. Wang, China
12. Sep 18 11:30 12:00 4.1.5 AERODYNAMIC EVALUATION OF THE EXTERNAL FLOW OVER NOTCHBACKS AND PICKUP TRUCKS
O.-A Almeida, Federal University of Uberlândia, 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
5.1Wind Tunnel Systems Development
Chair(s): Hermans, C.
Track 5
03.2 - Experimental Aerodynamics
12. Sep 18 09:30 10:00 5.1.1 DESIGN OF THE TRISONIC WIND TUNNEL FOR THE UNIVERSIDAD DEL VALLE
D. Mondragón Duque, Universidad del Valle, Colombia
12. Sep 18 10:00 10:30 5.1.2 OVERVIEW OF DYNAMIC TEST TECHNIQUES FOR FLIGHT DYNAMICS RESEARCH AT LOW SPEED AERODYNAMICS INSTITUTE, CARDC
LZT ZHITAO, CARDC, China
12. Sep 18 10:30 11:00 5.1.3 APPLICATION OF THE COMBINED BOUNDARIES TO REDUCE WALL INDUCTION FOR NACA 0012 AIRFOIL TESTS
E.V. Streltsov, TsAGI, Russia
12. Sep 18 11:00 11:30 5.1.4 EVALUATION OF WIND TUNNEL SIDEWALL BOUNDARY-LAYER CONTROL FOR 2-D HIGH-LIFT AERODYNAMIC AND AEROACOUSTIC TESTING
F. M. Catalano, Sao Carlos Engineering School University of Sao Paulo, Brazil
12. Sep 18 11:30 12:00 5.1.5 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
Reserve Paper 5.1.R APPLICATION OF NUMERICAL METHODS TO THE PROBLEM OF AERODYNAMIC DESIGN OF WIND TUNNEL FIN STING
A.R. Gorbushin, Central Aerohydrodynamic Institute, Russia
6.1Buffet and Separation Control
Chair(s): Breitsamter, C., Prince, S.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
12. Sep 18 09:30 10:00 6.1.1 EFFECTIVE PLASMA BUFFET AND DRAG CONTROL FOR LAMINAR TRANSONIC AEROFOIL
P.A. Polivanov, ITAM SB RAS, Russia
12. Sep 18 10:00 10:30 6.1.2 CONTROL OF STRONG SEPARATION OF FLOW VIA SIMULTANEOUS-BLOWING-SUCTION TECHNIQUE
W. STALEWSKI, Institute of Aviation, Poland
12. Sep 18 10:30 11:00 6.1.3 NUMERICAL OPTIMIZATION OF FLOW CONTROL BY TANGENTIAL JET BLOWING ON TRANSONIC AIRFOIL
V.G. Soudakov, TsAGI, Russia
12. Sep 18 11:00 11:30 6.1.4 ACTIVE CONTROL OF SHOCK-DOMINATED AIRFLOW BY STREAMWISE PLASMAS
S. B. Leonov, University of Notre Dame, United States
12. Sep 18 11:30 12:00 6.1.5 CFD ANALYSIS OF COAND? BLANKET CURVATURE ON COAND? DEVICE PERFORMANCE
R.H. Djojodihardjo, The Institute for the Advancement of Aerospace Sciece and Techno, Indonesia
Reserve Paper 6.1.R CO-FLOW JET EFFECT ON DYNAMIC STALL CHARACTERISTICS OF ROTOR AIRFOILS
X.D.-Y Yang, School of Aeronautics, Northwestern Polytechnical University, China
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
E.A. Pigusov, TsAGI, 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. Veldhuis, Delft 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. Zhu, China
12. Sep 18 11:30 12:00 7.1.5 OUTBOARD SPLIT FLAP AERODYNAMICS OF A FLYING WING CONFIGURATION
S. Pfnuer, Technical University of Munich, Germany
Reserve Paper 7.1.R ROBUST DESIGN OPTIMIZATION OF BENCHMARK AERODYNAMIC CASE BASED ON POLYNOMIAL CHAOS EXPANSION
Zhao.H. Huan, Northwestern Polytechnical University , China
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 AN EFFICIENT METHOD TO LOCATE AEROELASTIC STABILITY BOUNDARIES
A.N. Marques, MIT, United States
12. Sep 18 10:00 10:30 8.1.2 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 10:30 11:00 8.1.3 AEROELASTIC TAILORING OF COMPOSITE WING BY USING MULTIDISCIPLINARY DESIGN ENVIRONMENT
A. Balunov, TsAGI, Russia
12. Sep 18 11:00 11:30 8.1.4 INTERRELATION BETWEEN THE LOADING AND THE AEROELASTICITY CHARACTERISTICS OF MEDIUM RANGE AIRCRAFT IN TRANSONIC FLOW
A. Chizhov, TsAGI, Russia
12. Sep 18 11:30 12:00 8.1.5 VIRTUAL AIRCRAFT MODEL FOR AEROELASTIC SIMULATION AND LOAD PREDICTION OF A HIGH ASPECT RATIO COMPOSITE SWEPT WING
A. Hermanutz, TU Munich, Germany
Reserve Paper 8.1.R 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
9.1High Speed Propulsion 1
Chair(s): Kukshinov, N.
Track 9
05 - Propulsion
12. Sep 18 09:30 10:00 9.1.1 CFD MODELLING TO OPTIMIZE THE MAXIMUM THRUST IN SCRAMJET ENGINE AND ANALYSIS OF ITS OPERATION PERFORMANCE
M-P Pires, IME, Brazil
12. Sep 18 10:00 10:30 9.1.2 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 10:30 11:00 9.1.3 SIMULTANEOUS MEASUREMENTS OF TEMPERATURE AND HEAT FLUX IN SUPERSONIC COMBUSTOR BY ITO THIN FILM THERMOCOUPLE
X.H-J Jin, Northwestern Polytechnical University, China
12. Sep 18 11:00 11:30 9.1.4 GROUND FACILITY TESTS OF HIGH SPEED RAMJET DEMONSTRATORS
A Prokhorov, CIAM, Russia
12. Sep 18 11:30 12:00 9.1.5 HYBRID RANS/LES SIMULATION OF THE HIFIRE-2 GROUND TEST CONFIGURATION USING CRACKED KEROSENE-AIR FLAMELET APPROACH
H-G Sung, Korea Aerospace University, South Korea
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 DESIGN OF FLIGHT PATH ANGLE CONTROLLER BY USING CONTROL ALLOCATION
Y. Seo, Seoul National University, South Korea
12. Sep 18 10:30 11:00 10.1.3 A COMPARISON BETWEEN UNIVERSAL INTEGRAL REGULATOR AND LINEAR QUADRATIC TECHNIQUE FOR AN AIRCRAFT AUTOPILOT
Méndez Díaz, Federal University of Itajubá, Brazil
12. Sep 18 11:00 11:30 10.1.4 RESEARCH ON DISTRIBUTED INTEGRATED MANIPULATION SYSTEM OF AIRCRAFT
Y.-W. Cui, AVIC FACRI, China
12. Sep 18 11:30 12:00 10.1.5 MULTI-VARIABLE AIRCRAFT DIRECTIONAL CONTROL WITH ANTI-SKID DIFFERENTIAL BRAKES
G. Di Rito, Università di Pisa - Dip. di Ing. Civile ed Industriale, Italy
Reserve Paper 10.1.R A COMPLEX STEP DERIVATIVE APPROACH FOR OPTIMAL CONTROL USING SIMULINK MODELS
J. Diepolder, Institute of Flight System Dynamics (TUM), Germany
11.1System Design
Chair(s): Peters, M.
Track 11
07 - Systems, Subsystems and Equipment
12. Sep 18 09:30 10:00 11.1.1 WIND SHEAR PARAMETER ESTIMATION FOR DYNAMIC SOARING WITH UNMANNED AERIAL VEHICLES
D.-N. Liu, China Aerodynamics Research and Development Center , China
12. Sep 18 10:00 10:30 11.1.2 A METHODOLOGY FOR PRELIMINARY SIZING OF A VEHICLE ENERGY MANAGEMENT SYSTEM FOR A HYPERSONIC VEHICLE.
R. Fusaro, Politecnico di Torino, Italy
12. Sep 18 10:30 11:00 11.1.3 INTEGRATION OF ON-BOARD SYSTEMS PRELIMINARY DESIGN DISCIPLINE WITHIN A COLLABORATIVE 3RD GENERATION MDO FRAMEWORK
L. Boggero, Politecnico di Torino, Italy
12. Sep 18 11:00 11:30 11.1.4 FAULT DIAGNOSIS METHOD STUDY FOR COMPLEX SYSTEM BASED ON KALMAN FILTERS
W.N. Niu, AVIC Computing Technique Research Institute, China
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. Bagassi, University 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, 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 Toratani, Electronic Navigation Research Institute, Japan
12. Sep 18 11:00 11:30 12.1.4 NONLINEAR MODEL PREDICTIVE CONTROL FOR OPTIMAL AIRCRAFT SEQUENCING
B. Grüter, Technical University of Munich, Germany
12. Sep 18 11:30 12:00 12.1.5 APPLICATION OF A FRAMEWORK TO ASSESS IMPACTS ON FUTURE AIRPORT NOISE EXPOSURE
F. Will¹, M. Hornung¹; ¹Technical University of Munich, Germany
Reserve Paper 12.1.R ADAPTIVE LANDING SEQUENCING IN AIR TRAFFIC FLOW OPTIMISATION
M. Hickson¹, C. Bil¹; ¹RMIT University, Australia

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

1.2Unconventional Concepts 2
Chair(s): Kimmel, B.
Track 1
01 - Aircraft Design and Integrated Systems
12. Sep 18 14:00 14:30 1.2.1 FLEXFLOIL SHAPE ADAPTIVE CONTROL SURFACES—FLIGHT TEST AND NUMERICAL RESULTS
J. R. R. A. Martins, University of Michigan, United States
12. Sep 18 14:30 15:00 1.2.2 FEASIBILITY STUDY OF MODIFYING A KEROSENE AIRCRAFT TO A LH2 POWERED VERSION
W.-Q XIE, AVIC The First Aircraft Institute, China
12. Sep 18 15:00 15:30 1.2.3 DEVELOPMENT OF THE REGENERATIVE SOARER, THEORETICAL AND PRACTICAL ASPECTS
RC Carvalho, EMBRAER S.A., Brazil
Reserve Paper 1.2.R DEVELOPMENT OF A NOVEL AERIAL PLATFORM WHICH MERGES THE CONCEPT OF ARSHIPS AND TETHERED AEROSTATS
J S Santos, Brazil
2.2Structural Health Monitoring 2
Chair(s): Anchieta da Silva, P., Scott, M.
Track 2
11 - Operations and Sustainment
12. Sep 18 14:00 14:30 2.2.1 ADDRESSING TECHNICAL AND REGULATORY REQUIREMENTS TO DEPLOY STRUCTURAL HEALTH MONITORING SYSTEMS ON COMMERCIAL AIRCRAFT
D. Roach, Sandia National Laboratoies, United States
12. Sep 18 14:30 15:00 2.2.2 STRUCTURAL HEALTH MONITORING QUALIFICATION PROCESS AND THE FUTURE OF AIRCRAFT MAINTENANCE
R. P. Rulli¹, F. Dotta¹, P. A. da Silva¹, L. C. Vieira¹, A. K. F. Tamba¹, G. O. C. Prado¹, D. Roach², T. Rice²; ¹Embraer S.A., Brazil ;²Sandia National Labs, United States
12. Sep 18 15:00 15:30 2.2.3 CORROSION DETECTION IN AERONAUTICAL STRUCTURES USING LAMB WAVES SYSTEM FOR STRUCTURAL HEALTH MONITORING
A.K. F. Tamba¹, L.C. Vieira¹, F. Dotta¹, R.P. Rulli¹, G.O.C Prado¹, P.A. da Silva¹, R.R. Cunha¹, J.P da Costa¹; ¹Embraer S.A., Brazil
Reserve Paper 2.2.R STRUCTURAL HEALTH MONITORING WITH AUGMENTED REALITY FOR AIRCRAFT MAINTENANCE
G.O.C. Prado¹, P.A. Silva¹, F.M. Simomura¹, K.L.O. Pereira¹; ¹Embraer S.A., 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 Amaro de Oliveira, ITA, 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 Mendonca, Embraer, 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 BLADE FLIGHT TEST ANALYSIS OF SAABS INNOVATIVE LAMINAR FLOW WING PANEL
B Hackström, Saab Aeronautics, Sweden
12. Sep 18 14:30 15:00 4.2.2 VALIDATION OF INTERMITTENCY MODEL FOR TRANSITION PREDICTION IN A RANS FLOW SOLVER
D. de Rosa, CIRA, Italy
12. Sep 18 15:00 15:30 4.2.3 DEVELOPMENT OF A NUMERICAL ENVIRONMENT TO PREDICT BOUNDARY LAYER TRANSITION
A.P. Antunes¹, R. Cosin¹; ¹Embraer, Brazil
Reserve Paper 4.2.R MACHINE LEARNING APPROACH TO THE INTERMITTENCY TRANSITION TURBULENCE MODEL FOR WIND TURBINE APPLICATION
M.A Abd Bari, University 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 HIGH ASPECT-RATIO WINGS
L.A.V. Pelegrineli, 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. G. Granzoto, Embraer S.A., Brazil
12. Sep 18 15:00 15:30 5.2.3 EXPERIMENTAL AND CFD ANALYSIS OF A UAV FOR SUPERFICIAL VOLCANO SURVEILLANCE
P. D. Bravo-Mosquera, EESC-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. Sasaki, Brazil
12. Sep 18 14:30 15:00 6.2.2 ACTUATOR AND SENSOR PLACEMENT FOR CLOSED-LOOP CONTROL OF CONVECTIVE INSTABILITIES
G. A. Freire, Instituto Tecnológico de Aeronáutica, Brazil
12. Sep 18 15:00 15:30 6.2.3 RESOLVENT-BASED CONTROL OF STREAKS IN BOUNDARY LAYERS
P. A. Nogueira, Instituto Tecnológico de Aeronáutica, Brazil
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
Fei Yang Yang, Shanghai Aircaft Design and Research Institute of COMAC, China
Reserve Paper 7.2.R THE DYNAMICS CHARACTERISTIC ANALYSIS FOR SUPER-LONG SHAFT TRAIN OF A LARGE WEIND TUNNEL COMPRESSOR
X-Q YAN, China Aerodynamics Research and Development Center, China
8.2Aeroelasticity 6 : General
Chair(s): Amiryants, G.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
12. Sep 18 13:30 14:00 8.2.1 REDUCED ORDER MODELING OF A NONLINEAR COUPLED AERO-ELECTRO-ELASTIC ENERGY HARVESTING SYSTEM
Y. Wu, Beihang University, China
12. Sep 18 14:00 14:30 8.2.2 EXPERIMENTAL AND NUMERICAL STUDIES OF FLUTTER CHARACTERISTICS OF AN ALL-MOVING CONTROL SURFACE AGAINST GAP EFFECTS
Y.-G Bai, Dalian University of Technology, China
12. Sep 18 15:00 15:30 8.2.3 MULTIDISCIPLINARY METHOD FOR WING FLIGHT SHAPE ANALYSIS - EFFECT OF THE GEOMETRIC NONLINEAR STRUCTURE FOR STATIC PULL-UP
A. A. VERRI, EMBRAER S/A, Brazil
9.2High Speed Propulsion 2
Chair(s): Whurr, J.
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
R. C. Barbosa, ITA, 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 Neto, ITA, Brazil
Reserve Paper 10.2.R IDENTIFICATION OF THE LATERAL-DIRECTIONAL MODEL OF THE VECTOR-P, UNMANNED AERIAL VEHICLE
C.F Fischer, Instituto Tecnológico de Aeronáutica, 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 Rito, Universita' 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
Ribeiro, L. C. Ribeiro, Brazil
12. Sep 18 15:00 15:30 11.2.3 AN AIRBORNE DATA BUS NETWORK SYSTEM OF INTERFACE ADAPTIVE AND FLEXIBLE CONTROL
Lin Shi¹, Zheng Qiu, AVIC Xi’an Aviation Computing Technology Institute, China; Zhen Dai¹; ¹AVIC ChengDu Aircraft Design & Research Institute, China
12.2UAS - Unmanned Aircraft Systems
Chair(s): Lief, A.
Track 12
10 - Safety and Security
12. Sep 18 14:00 14:30 12.2.1 INVESTIGATION OF EMERGING HUMAN-MACHINE INTERFACE CONCEPTS FOR UAS OPERATIONS
Y. Lim, RMIT University, Australia
12. Sep 18 14:30 15:00 12.2.2 LOW LEVEL RPAS TRAFFIC IDENTIFICATION AND MANAGEMENT: CONCEPT OF OPERATION AND DEMONSTRATION OF A GROUND BASED SYSTEM
P. Le Blaye, ONERA, France
12. Sep 18 15:00 15:30 12.2.3 HUMAN FACTOR IN UNMANNED AIRCRAFT SYSTEM FLIGHT TEST
F-W Wang, Chinese Flight Test Establishment, China

15:30 - 16:00Break

1.3Design Education 2
Chair(s): Bagassi, S.
Track 1
01 - Aircraft Design and Integrated Systems
12. Sep 18 16:00 16:30 1.3.1 FROM REQUIREMENTS ANALYSIS TO FLYING MINI UAVS IN ONE SEMESTER: ENHANCING DESIGN TEACHING WITH THE HELP OF 3D PRINTING
Franz-Michael Sendner¹, Christian Roessler¹, Mirko Hornung¹; ¹Technical University of Munich, Germany
12. Sep 18 16:30 17:00 1.3.2 STUDY ON EVALUATION METHODS OF UNDERGRADUATE AIRCRAFT OVERALL DESIGN COURSE BASED ON TEAM DESIGN COMPETITION
Z.-C. CHEN, Beihang University, China
12. Sep 18 17:00 17:30 1.3.3 DESIGN AND FABRICATION OF THE CEA 311 ANEQUIM - A SPEED RECORDIST AIRPLANE
P. Iscold, UFMG, United States
12. Sep 18 17:30 18:00 1.3.4 AN OVERVIEW OF THE FIRST PARAGUAYAN NEAR SPACE EXPLORATION USING A HIGH ALTITUDE BALLOON
A. J. Jara, Universidad Nacional de Asuncion, Paraguay
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 AN AIRCRAFT DESIGN PROCESS TO DERIVE THE MOST SUITABLE HYBRID ELECTRIC PROPULSION SYSTEM FOR A GIVEN MISSION SCENARIO
M. Strack, DLR, Germany
12. Sep 18 16:30 17:00 2.3.2 INTEGRATED TURBO-ELECTRIC MOTIVE POWER SYSTEMS FOR REGIONAL TRANSPORT APPLICATIONS
A.T. Isikveren, SAFRAN S.A., France
12. Sep 18 17:00 17:30 2.3.3 DEVELOPING THE UNMANNED UNCONVENTIONAL CARGO AIRPLANES WITH HYBRID PROPULSION SYSTEM
J. Rohacs, Department of Aeronautics, Naval Architecture and Railway Vehicl, Hungary
12. Sep 18 17:30 18:00 2.3.4 OPTIMIZATION OF MOTOR FOR THE MAXIMIZATION OF SOLAR-POWERED AIRCRAFT PERFORMANCE
S. Serokhvostov, MIPT DAFE, Russia
Reserve Paper 2.3.R INVERSE AIRCRAFT DESIGN FOR MARKETSHARE
J.G. Gibbs, Savion Aerospace, United States
3.3Durability and Fatigue
Chair(s): Poikelispää, M., Angelin, R.
Track 3
04.1 - Material Issues, Fatigue and Damage Tolerance
12. Sep 18 16:00 16:30 3.3.1 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 16:30 17:00 3.3.2 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 17:00 17:30 3.3.3 USING THE LEAD CRACK CONCEPT TO REDUCE DURABILITY TEST DURATION
L Molent, DST, Australia
12. Sep 18 17:30 18:00 3.3.4 STRENGTH CHARACTERISTICS OF CURRENTLY ALUMINUM ALLOYS
A.V. Kulemin¹, G.I. Nesterenko¹, B.G. Nesterenko, National Research Center "Zhukovsky Institute", Russia; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
Reserve Paper 3.3.R INFLUENCE OF IRREGULAR LOADING PARAMETERS ON CFRP COMPONENTS FATIGUE LIFE
A.G. Kalinin, Central Aerohydrodynamic Institute, 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. Voevodenko, TsAGI, Russia
12. Sep 18 16:30 17:00 4.3.2 AERO-THERMAL DESIGN OF HEXAFLY-INT HYPERSONIC VEHICLE THERMAL PROTECTION SYSTEM
R. SCIGLIANO, Italian Aerospace Research Centre (CIRA), Italy
12. Sep 18 17:00 17:30 4.3.3 RANS AND DSMC FLOW SIMULATIONS OVER TYPICAL HYPERSONIC CONFIGURATIONS
R. R. P. P. Pereira, IAE, Brazil
12. Sep 18 17:30 18:00 4.3.4 UNSTRUCTURED COMPRESSIBLE NAVIER-STOKES SOLVER FOR HIGH ALTITUDE FLOWS
C. Baek, Inha university, South Korea
Reserve Paper 4.3.R LONGITUDINAL STABILITY DESIGN CRITERIA FOR HYPERSONIC GLIDERS
B.Y. Chen, China Academy of Aerospace Aerodynamics, China
5.3Optical Measurement Techniques
Chair(s): Klein, C.
Track 5
03.2 - Experimental Aerodynamics
12. Sep 18 16:00 16:30 5.3.1 FLOW UNSTEADINESS RESEARCHES ON THE BLUNT FIN-INDUCED SHOCK/BOUNDARY LAYER INTERACTIONS
X.J. Zhao, China Academy of Aerospace Aerodynamics, China
12. Sep 18 16:30 17:00 5.3.2 INVESTIGATION OF THE SHOCK WAVE/BOUNDARY LAYER INTERACTION PATTERN AT TRANSONIC SPEEDS
M.A. Brutyan, TsAGI, Russia
12. Sep 18 17:00 17:30 5.3.3 PARTICLE IMAGE SURFACE FLOW VISUALIZATION AND SKIN-FRICTION MEASUREMENT
V.E. Mosharov, TsAGI, Russia
12. Sep 18 17:30 18:00 5.3.4 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
Reserve Paper 5.3.R INVESTIGATION OF BDUNDARY LAYER TRANSITION MEASUREMENT IN SUBSONIC WIND TUNNEL USING TSP
J.-Y. Yu, China Academy of Aerospace Aerodynamics (CAAA), China
6.3Complex Transition Phenomena
Chair(s): Alves, L., Hanifi, A.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
12. Sep 18 16:00 16:30 6.3.1 EFFECTS OF THE INTRINSIC THREE-DIMENSIONALIZATION OF SEPARATION BUBBLES ON THE AMPLIFICATION OF EXTERNAL DISTURBANCES
D. Rodriguez, Universidade Federal Fluminense, Brazil
12. Sep 18 16:30 17:00 6.3.2 WAVEPACKETS IN TURBULENT FLOW OVER A NACA 4412 AIRFOIL
L. I. ABREU, ITA, Brazil
12. Sep 18 17:00 17:30 6.3.3 CONTROL OF COMPLEX DISTURBANCES IN THE BOUNDARY LAYER OVER A FLAT PLATE.
A. Hanifi, KTH Royal Institute of Technology, Sweden
12. Sep 18 17:30 18:00 6.3.4 DEVELOPMENT OF SECONDARY CROSSFLOW INSTABILITY NEAR BREAKDOWN TO TURBULENCE
C J Atkin, City, University of London, United Kingdom
Reserve Paper 6.3.R LAMINAR-TURBULENT TRANSITION MECHANISMS OVER WIDELY-SPACED SUCTION HOLES
C J Atkin, City, University of London, United Kingdom
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.-Y. YANG, School 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
X.-C. Xue, Northwestern 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.Z ZHOU, Northwestern Polytechnical University, China
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 COMPUTATIONAL AEROELASTICITY USING A COUPLED CFD-CSD SOLVER
W. Yuan, National Research Council Canada, Canada
12. Sep 18 16:30 17:00 8.3.2 COMPUTATIONAL STUDY OF THE AERODYNAMICS AND AEROELASTICITY OF FLAPPING WING
R.H. Djojodihardjo, The Institute for the Advancement of Aerospace Sciece and Techno, Indonesia
12. Sep 18 17:00 17:30 8.3.3 NUMERICAL AND EXPERIMENTAL VALIDATION OF UNITIZED BEAM MODEL
F--D. Danzi, Politecnico di Torino, Italy
12. Sep 18 17:30 18:00 8.3.4 STUDY OF FLUTTER CHARACTERISTIC SENSITIVITY TO STRUCTURE THICKNESS PARAMETER VARIATION OF A FIGHTER AIRCRAFT WING
R.A. Sasongko, FTMD Institut Teknologi Bandung, Indonesia
Reserve Paper 8.3.R A PROPOSAL FOR AIRCRAFT STRUCTURAL RISK ANALYSIS
C. Reiser, Embraer, Brazil
9.3MDO-2 AGILE
Chair(s): Mirzoyan, A.
Track 9
05 - Propulsion
12. Sep 18 16:00 16:30 9.3.1 MDO OF PROPULSION SYSTEM FOR ADVANCED CIVIL AIRCRAFT IN AGILE PROJECT COLLABORATIVE MDO ENVIRONMENT
A.A. Isyanov, CIAM, Russia
12. Sep 18 16:30 17:00 9.3.2 STUDIES IN AGILE PROJECT COLLABORATIVE MDO ENVIRONMENT ON PROPULSION AND ON-BOARD SYSTEMS MATCHING FOR ADVANCED AIRCRAFT
A. Mirzoyan¹, A. Isianov¹, A. Maximov¹, M. Fioriti², L. Boggero²; ¹CIAM, Russia ;²Politecnico di Torino, Italy
12. Sep 18 17:00 17:30 9.3.3 COMMUNICATION BETWEEN PS AND AIRCRAFT SYSTEMS IN COLLECTIVE MDO SYSTEM IN AGILE PROJECT
P.D. Toktaliev, Central Institute of Aviation Motors, Russia
12. Sep 18 17:30 18:00 9.3.4 PROPULSION SYSTEM - AIRFRAME INTEGRATION AND OPTIMIZATION OF CIVIL AIRCRAFT- AGILE EU PROJECT
P S Shivaprakasha, German Aerospace Center, Germany
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 IDENTIFICATION OF AERODYNAMIC AND FLIGHT-MECHANICAL CHARACTERISTICS USING REMOTELY-PILOTED SUBSCALE DEMONSTRATORS
A Sobron, Linköping University, Sweden
12. Sep 18 16:30 17:00 10.3.2 BIO-DYNAMIC STABILITY ANALYSIS OF A GREBE DURING MIGRATION
J Feaster, Virginia Tech, United States
12. Sep 18 17:00 17:30 10.3.3 DYNAMIC REACTION OF AN AIRPLANE TO TRAILING VORTICES GENERATED BY ANOTHER AIRPLANE
G. Kowaleczko, Air Force Institute of Technology, Poland
12. Sep 18 17:30 18:00 10.3.4 MATHEMATICAL MODEL OF COMMERCIAL AIRPLANE DYNAMICS AT STALL
P. V. Kuzmin, TsAGI, Russia
11.3Electro Mechanical Actuation Systems
Chair(s): Mare, J.C.
Track 11
07 - Systems, Subsystems and Equipment
12. Sep 18 16:00 16:30 11.3.1 FORCE FIGHT COMPENSATION FOR REDUNDANT ELECTRO-MECHANICAL FLIGHT CONTROL ACTUATORS
R. Kowalski¹, J. Windelberg¹, R. Ladner², M. Rottach²; ¹German Aerospace Center (DLR e.V.), Germany ;²Liebherr-Aerospace Lindenberg GmbH, Germany
12. Sep 18 16:30 17:00 11.3.2 A MORE INTEGRATED DESIGN APPROACH FOR EMBEDDED SYSTEMS: APPLICATION TO ELECTRICAL THRUST REVERSER ACTUATION SYSTEMS
S. Delbecq, France
12. Sep 18 17:00 17:30 11.3.3 POSITION SYNCHRONIZATION OF AEROSPACE ELECTROMECHANICAL ACTUATORS FOR DISTRIBUTED ELECTRICAL ACTUATION SYSTEM
J FU, Beihang University, China
12. Sep 18 17:30 18:00 11.3.4 PIO SUSCEPTIBILITY IN FLY-BY-WIRE SYSTEMS
H. C Moura¹, G. S. P. Alegre¹, J. H. Bidinotto¹, E. M. Belo¹; ¹University of São Paulo, Engineering School of São Carlos, Brazil
Reserve Paper 11.3.R THE DEVELOPMENT OF EMA FAULT EARLY DETECTION SYSTEM
A. Skryabin, Central Aerohydrodynamic Institute of Russia, Russia
12.3Safety Analysis
Chair(s): Conway, S., Ross, I.
Track 12
10 - Safety and Security
12. Sep 18 16:00 16:30 12.3.1 A METHOD FOR ESTIMATING THE PROBABILITY OF RARE ACCIDENTS IN COMPLEX SYSTEMS
I Romani de Oliveira, Boeing Research & Technology, Brazil
12. Sep 18 16:30 17:00 12.3.2 PROBABILISTIC FORECASTING IN AIRCRAFT EMERGENCY EVACUATION SIMULATION
L. Santos, EMBRAER, Brazil
12. Sep 18 17:00 17:30 12.3.3 STUDY ON AIRCRAFT EVACUATION MODELING AND MODEL PARAMETERS BASED ON SOCIAL FORCE
Kun Chen¹, Yibing Wu¹, Tianchun Zou¹; ¹Laboratory of Civil Aircraft Airworthiness Technology, CAUC, China
12. Sep 18 17:30 18:00 12.3.4 DEVELOPMENT OF PRELIMINARY ZONAL SAFETY ANALYSIS METHODOLOGY
J.P. FIELDING, CRANFIELD UNIVERSITY, United Kingdom
Reserve Paper 12.3.R DETECTING CONFLICTS BETWEEN SAFETY AND SECURITY CONSTRAINTS IN CONCEPT PHASE
D.P. PEREIRA, ITA, Brazil