30th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

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Thursday, 13. Sep 2018


7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
0.1General Lecture V - IFAR Plenary Lecture Global Cooperation Leading to New Commercial Supersonic Opportunity - NASA-Dr. Jaiwon Shin TsAGI-Dr. Sergey Chernychev JAXA-Dr. Fumikazu Itoh ONERA-Bruno Saijon DLR-Prof. Rolf Henke NLR-Michel Peters
Chair:
13. Sep 18 08:00 09:30

09:30 - 10:00Break

1.1Design Method 2
Chair(s): Rinoie, K., Nicolosi, F.
Track 1
01 - Aircraft Design and Integrated Systems
13. Sep 18 10:00 10:30 1.1.1 PRELIMINARY DESIGN OF A LONG RANGE WINDOWLESS AIRCRAFT CONCEPT
F. Lucchi, University of Bologna, Italy
13. Sep 18 10:30 11:00 1.1.2 COLLABORATIVE CONCEPTUAL DESIGN OF A MID-RANGE AIRCRAFT UNDER CONSIDERATION OF ADVANCED METHODS FOR TECHNOLOGY ASSESSMEN
T. Pfeiffer, DLR, Germany
13. Sep 18 11:00 11:30 1.1.3 STRATEGY AND IMPLEMENTATION OF A PARAMETRIC CAD MODEL FOR A330-300 R2035 STRUCTURE AND EXTERNAL CONFIGURATION
Z. Goraj, Politechnika Warszawska, Poland
13. Sep 18 11:30 12:00 1.1.4 AN APPROACH TO ASSESS AIRFRAME WEIGHT REDUCTION PERFORMANCE FOR STITCHED COMPOSITE TECHNOLOGIES
J. Corman, Georgia Institute of Technology, United States
13. Sep 18 12:00 12:30 1.1.5 DESIGN SPECIFICATIONS AND PAYLOAD-RANGE EFFICIENCY OF TRANSPORT AIRPLANES
R Martinez-Val, Universidad Politecnica de Madrid, Spain
Reserve Paper 1.1.R ENGINEERING CHALLENGES IN THE CONVERSION OF NARROW-BODY B737 NEXT-GENERATION FROM PASSENGER TO FREIGHTER
I. Berlowitz, Israel Aerospace Industries, Israel
2.1Aircraft Operations 2
Chair(s): Teixeirada da Cunha, S., Anderson, K.
Track 2
11 - Operations and Sustainment
13. Sep 18 10:00 10:30 2.1.1 PARAMETRIC APPROACH TO OPERATING COSTS ESTIMATION FOR AN INNOVATIVE REGIONAL AIRCRAFT
D. Ferretto, Politecnico di Torino, Italy
13. Sep 18 10:30 11:00 2.1.2 PROGNOSIS OF AIRCRAFT FUEL FLOW USING MACHINE LEARNING ALGORITHMS ON FLIGHT OPERATIONAL DATA
S. Baumann, Technische Universitaet Darmstadt, Germany
13. Sep 18 11:00 11:30 2.1.3 FUEL-BURN PENALTIES CAUSED BY IRREGULARITIES IN AIRCRAFT SURFACES (ASTEROID PROJECT)
DAVID D R PHILPOTT, IHS MARKIT, United Kingdom
13. Sep 18 11:30 12:00 2.1.4 COST-BENEFIT ASSESSMENT OF CLIMATE AND WEATHER OPTIMIZED TRAJECTORIES FOR DIFFERENT NORTH ATLANTIC WEATHER PATTERNS
B. Luehrs, Hamburg University of Technology, Germany
13. Sep 18 12:00 12:30 2.1.5 TIME AND ENERGY MANAGED OPERATIONS (TEMO)
RPM Verhoeven, Netherlands Aerospace Centre (NLR), Netherlands
Reserve Paper 2.1.R IDENTIFICATION OF OPTIMAL RENDEZVOUS AND SEPARATION AREAS FOR FORMATION FLIGHT UNDER CONSIDERATION OF WIND
T. Marks, German Aerospace Center, Germany
3.1Crack and Impact Damage Propagation
Chair(s): Fish, J., Blom, A.
Track 3
04.1 - Material Issues, Fatigue and Damage Tolerance
13. Sep 18 10:00 10:30 3.1.1 STUDY OF ACCIDENTAL IMPACT SCENARIOS FOR COMPOSITE WING DAMAGE TOLERANCE EVALUATION
V. Dubinskiy, TsAGI, Russia
13. Sep 18 10:30 11:00 3.1.2 MULTI-SITE DELAMINATION ANALYSIS USING VIRTUAL CRACK CLOSURE TECHNIQUE FOR A COMPOSITE AIRCRAFT WING FLAP
J. Jokinen¹, M. Kanerva¹, O. Saarela, Aalto University, Finland; ¹Tampere University of Technology, Finland
13. Sep 18 11:00 11:30 3.1.3 INVESTIGATION OF BULGING EFFECTS ON PROPAGATION OF 1-BAY AND 2-BAY LONGITUDINAL CRACKS WITH BROKEN/INTACT STIFFENER
A.S. Kim, TsAGI, Russia
13. Sep 18 11:30 12:00 3.1.4 BALLISTIC RESISTANT ANALYSIS FOR AIRCRAFT WING STRUCTURE
G.R. Zu, School of Aeronautics, Northwestern Polytechnical University, China
13. Sep 18 12:00 12:30 3.1.5 PLY THICKNESS INFLUENCE IN COMPRESSION AFTER IMPACT DAMAGE ON CARBON/EPOXY TEST SPECIMENS
T. H. L. Pinto, UFVJM, Brazil; C. A. Cimini Jr., UFMG, Brazil; S. K. Ha, Hanyang University, South Korea
Reserve Paper 3.1.R NUMERICAL INVESTIGATION OF INFLUENCE OF INITIAL DAMAGES ON STRENGTH PARAMETERS OF CFRP
E.A. Dubovikov, Central Aerohydrodynamic Institute, Russia
4.1Aerodynamic Optimization
Chair(s): Hoeijmakers, H., Conde de Resende, O.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
13. Sep 18 10:00 10:30 4.1.1 PERFORMANCE IMPROVEMENT OF A COMPOUND HELICOPTER ROTOR HEAD BY AERODYNAMIC SHAPE OPTIMIZATION
P. Pölzlbauer, Technical University of Munich, Germany
13. Sep 18 10:30 11:00 4.1.2 A RAPID AERODYNAMIC PREDICTION METHOD FOR UNCONVENTIONAL TRANSONIC AIRCRAFT CONFIGURATIONS
S. A. Prince, Cranfield University, United Kingdom
13. Sep 18 11:00 11:30 4.1.3 AERODYNAMIC DESIGN AND ANALYSIS OF AN INNOVATIVE REGIONAL TURBOPROP CONFIGURATION
F. NICOLOSI, University of Naples Federico II, Italy
13. Sep 18 11:30 12:00 4.1.4 EVALUATION OF DELTA WING EFFECTS ON THE STEALTH-AERODYNAMIC FEATURES FOR NON-CONVENTIONAL FIGHTER AIRCRAFT
P. D. Bravo-Mosquera, EESC-USP, Brazil
13. Sep 18 12:00 12:30 4.1.5 DESIGN SPACE EXPLORATION AND FLOW CONTROL FOR A TRANSONIC WING DRAG REDUCTION
Y UTAMA, INSTITUT TEKNOLOGI BANDUNG, Indonesia
Reserve Paper 4.1.R GLOBAL OPTIMIZATION BASED ON METAMODELS TECHNIQUES FOR RADIAL GAS TURBINE DESIGN
E. R. Da Silva, Federal Universtiy of Itajubá, Brazil
5.1History of Aeronautics
Chair(s): Lott, M., Brandao, M.P.
Track 5
12 - Host nation
13. Sep 18 10:00 10:30 5.1.1 THE SANTOS-DUMONT LEGACY TO AERONAUTICS
M. P. Brandão, ITA, Brazil
13. Sep 18 10:30 11:00 5.1.2 THE LEGACY OF A BRAZILIAN AERONAUTICAL ENGINEER PROFESSOR: CLÁUDIO PINTO DE BARROS
P. Iscold, IscoldWorks, Brazil
13. Sep 18 11:00 11:30 5.1.3 BRAZILIAN AVIATION HISTORY: THE UNIVERSITY OF SÃO PAULO CASE
F.M. Catalano, Sao Carlos Engineering School - University of Sao Paulo, Brazil
13. Sep 18 11:30 12:00 5.1.4 THE STUDY OF TURBORAMJETS IN CIAM
V. Palkin, Russia
13. Sep 18 12:00 12:30 5.1.5 AERONAUTICAL AND AVIATION HUB BRAZIL
BSM Silva de Mattos, ITA, Brazil
6.1Student Final
Chair(s): Rein Weston, K.
Track 6
15 - Guest lectures
7.1High Speed Aerodynamics
Chair(s): Gubanov, A.
Track 7
03.4 - Applied Aerodynamics
13. Sep 18 10:00 10:30 7.1.1 ENGINE EXHAUST NOZZLE PLUME EFFECTS ON THE SONIC BOOM FOR A TYPE OF HYPERSONIC LONG-RANGE CIVIL VEHICLE
Zhansen Qian, AVIC Aerodynamics Research Institute, China
13. Sep 18 10:30 11:00 7.1.2 PRELIMINARY STUDY OF THE AERODYNAMIC CHARACTERISTICS OF KRUEGER FLAP ON THE SST CONFIGURATION
D. Kwak, JAXA, Japan
13. Sep 18 11:00 11:30 7.1.3 EFFECTS OF STEP HEIGHT AND POSITION ON THE FLOWFIELD STRUCTURE OF A HYPERSONIC FLOW OVER COMBINED GAP/STEP GEOMETRIES
W. F. N. SANTOS, National Institute for Space Research (INPE), Brazil
13. Sep 18 11:30 12:00 7.1.4 AERODYNAMICS CAUSED BY ATTITUDE RATES OF A SUPERSONIC FLIGHT EXPERIMENT VEHICLE WITH A CRANCKED-ARROW MAIN WING
K. Mizobata, National University Corporation Muroran Institute of Technology, Japan
13. Sep 18 12:00 12:30 7.1.5 HIGH SPEED DRAG REDUCTION OPTIMIZATION FOR PROJECTILE WITH AERODISKS
T. Wan, Department of Aerospace Engineering, Tamkang University, Taiwan
8.1Aeroelasticity 2 : Controls
Chair(s): Breitsamter, C.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
13. Sep 18 10:00 10:30 8.1.1 DESIGN OF A RECEPTANCE-BASED ACTIVE AEROELASTIC CONTROLLER IN THE PRESENCE OF PARAMETRIC UNCERTAINTIES
S. Fichera, The University of Liverpool, United Kingdom
13. Sep 18 10:30 11:00 8.1.2 INCREASED FLUTTER VELOCITY WITH USE OF A PASSIVE CONTROL SYSTEM
F. I. Carvalho¹, ROBERTO G SILVA¹; ¹ITA, Brazil
13. Sep 18 11:00 11:30 8.1.3 AEROELASTIC MODELING AND VIBRATION ATTENUATION OF HELICOPTER ROTOR BLADES
C.P. Pagani, São Paulo State University, Campus of São João da Boa Vista., Brazil
13. Sep 18 11:30 12:00 8.1.4 EXPERIMENTAL STUDY OF AEROELASTIC RESPONSE OF A FLEXIBLE HIGH ASPECT RATIO WING WITH PASSIVE SMA ACTUATORS
O. T Tomaz da Silva Neto, Universidade Federal de Campina Grande, Brazil
13. Sep 18 12:00 12:30 8.1.5 EFFECTS OF NONLINEAR ENERGY SINK ON THE AEROELASTIC BEHAVIOR OF AN ELECTROMECHANICALLY COUPLED TYPICAL SECTION
T.M.P. Marinelli Pereira Silva, USP - EESC, Brazil
9.1Compressor Aerodynamics
Chair(s): Mari, C., Girgis, S.
Track 9
05 - Propulsion
13. Sep 18 10:00 10:30 9.1.1 MATCHING BETWEEN METAMODEL AND OPTIMIZATION TOOL APPLIED IN A MULTISTAGE AXIAL-FLOW COMPRESSOR AIMING DESIGN IMPROVEMENT
O.F.R.S Silva, ITA, Brazil
13. Sep 18 10:30 11:00 9.1.2 EVALUATION OF TURBULENCE MODELS APPLIED TO HIGH PERFORMANCE AXIAL COMPRESSOR CONSIDERING PASSIVE WALL TREATMENT
R.-B. Bruno Díaz, Brazil
13. Sep 18 11:00 11:30 9.1.3 NUMERICAL AND EXPERIMENTAL STUDY THE EFFECT OF CIRCUMFERENTIAL GROOVES ON HPC LAST STAGE PERFORMANCE
V.I. MILESHIN, Central Institute of Aviation Motors, Russia
13. Sep 18 11:30 12:00 9.1.4 ADAPTIVE GTE SURGE PROTECTION SYSTEM WITH SELECTIVE CONTROL OF THE ACTUATORS
G. Bliznyukov, Central Institute of Aviation Motors (CIAM), Russia
13. Sep 18 12:00 12:30 9.1.5 AXIAL AND CENTRIFUGAL HIGH PRESSURE COMPRESSORS FOR PROSPECTIVE ENGINES
A. Startsev, CIAM, Russia
10.1Flight Control 2
Chair(s): Vian, J.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
13. Sep 18 10:00 10:30 10.1.1 QUASI-LPV MODELING AND PARAMETER-DEPENDENT OPTIMAL CONTROL OF MORPHING WING AIRCRAFT
J Lee¹, Y Kim¹; ¹Seoul National University, South Korea
13. Sep 18 10:30 11:00 10.1.2 AERODYNAMIC ANALYSIS AND CONTROL ALLOCATION FOR ASYMMETRIC VARIABLE SWEEP AIRCRAFT WITH FLEXIBLE TRAILING EDGE
H Ma, School of Aeronautics, Northwestern Polytechnical University, China
13. Sep 18 11:00 11:30 10.1.3 EFFECTS OF TAILORED CONTROL SURFACE COMPLIANCE ON AIRCRAFT STABILITY AND CONTROL
P Krus, Linköping university, Sweden
13. Sep 18 11:30 12:00 10.1.4 USE OF DISSIMILAR SENSOR DATA IN FLIGHT CONTROL LAWS
D.P.T. Ferreira, EMBRAER, Brazil
13. Sep 18 12:00 12:30 10.1.5 DIGITAL HYDRAULICS IN AEROSPACE APPLICATIONS: SLIDING MODE BEHAVIORS OF QUANTIZED CONTROL AND AN LMI DESIGNING SOLUTION
L.P.G Pinto, Linköping University, Sweden
11.1UAS Control 2
Chair(s): Gunlach, J.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
13. Sep 18 10:00 10:30 11.1.1 SMOOTH TRAJECTORY GENERATION AND CONTROL OF MULTIROTOR WITH SLUNG PAYLOAD
J.S. Lee¹, N.H. Cho¹, Y.D. Kim¹; ¹Seoul National University, South Korea
13. Sep 18 10:30 11:00 11.1.2 MULTI-CHANNEL HUMAN-MACHINE INTERACTIVE SYSTEM FOR MULTIPLE UAVS\\\' CONTROL
Peng-cheng Wen¹, Ya-di Zhang¹, Ya-hui Li¹; ¹AVIC Xi'an Aeronautics Computing Technique Research Institute, China
13. Sep 18 11:00 11:30 11.1.3 FLIGHT PERFORMANCE OF STEERABLE CRUCIFORM PARACHUTE SYSTEMS
T. Fields, University of Missouri-Kansas City, United States
13. Sep 18 11:30 12:00 11.1.4 PID GAIN SCHEDULING FOR CONSISTENT MANEUVERABILITY OF HEXACOPTER UNDER BATTERY VOLTAGE DROP
S. Kim, Korea Advanced Institute of Science and Technology, South Korea
13. Sep 18 12:00 12:30 11.1.5 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
Reserve Paper 11.1.R ON WAKE VORTEX SAFETY ANALYSIS AND CONTROL FOR UAV
V. Golubev, ERAU, United States
12.1Operations - ATM (air traffic mamagement)
Chair(s): Peters, M.
Track 12
10 - Safety and Security
13. Sep 18 10:00 10:30 12.1.1 FLIGHT TECHNICAL ERROR EVALUATIONS FOR GBAS NAVIGATION REQUIREMENT DEFINITION
M. Felux, German Aerospace Center (DLR), Germany
13. Sep 18 10:30 11:00 12.1.2 LOAD MONITORING FOR OPERATORS’ LOAD MANAGEMENT
D. Rohacs, HungaroControl - Hungarian Air Navigation Services, Hungary
13. Sep 18 11:00 11:30 12.1.3 THRUST MODELS BASED ON OPERATIONAL FLIGHT DATA USED IN PARAMETER ESTIMATION FOR SAFETY ANALYSES
Phillip Koppitz¹, Jonas Kuerten¹, Florian Holzapfel¹; ¹Technical University of Munich - Flight System Dynamics, Germany
13. Sep 18 11:30 12:00 12.1.4 AIRCRAFT KEY PARTS INTELLIGENT FAULT DIAGNOSIS USING GAUSSIAN DEEP BELIEF NETWORK
H.D. Shao, School of Aeronautics, Northwestern Polytechnical University, China
13. Sep 18 12:00 12:30 12.1.5 LOSS OF CONTROL IN FLIGHT - HOW DO WE DEFINE IT?
A Bromfield, Coventry University, United Kingdom
Reserve Paper 12.1.R ADAPTING CAPACITY OF AIR NAVIGATION SERVICE PROVISION IN EUROPE - BETWEEN SCYLLA AND CHARYBDIS
T. Standfuß, DLR German Aerospace Center, Germany

12:30 - 14:00Lunch

1.2Design History
Chair(s): Melkert, J.
Track 1
01 - Aircraft Design and Integrated Systems
13. Sep 18 14:00 14:30 1.2.1 REPLICA 55 PROJECT: A WOOD SEAPLANE IN THE ERA OF COMPOSITE MATERIALS
E. Cestino, Politecnico di Torino, Italy
13. Sep 18 14:30 15:00 1.2.2 THE NUMERICAL HISTORY OF AIRPLANE MANUFACTURING IN XX CENTURY
Yu.V. Kuzmin, Institute for history of science and technology, Russia
13. Sep 18 15:00 15:30 1.2.3 THE HAWKER SIDDELEY AVIATION HS141. VERTICAL TAKE –OFF AND LANDING RESEARCH PROGRAMME IN THE LATE 1960 EARLY 1970S.
F. Ogilvie, United Kingdom
2.2Maintenance Management
Chair(s): Chaves, C., Scott, M.
Track 2
11 - Operations and Sustainment
13. 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
13. 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
13. 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
Reserve Paper 2.2.R DISCUSSION ON PRODUCING AND VERIFYING OF TECHNICAL PUBLICATIONS DURING THE INITIAL PHASE OF AIRCRAFT DEVELOPMENT
QL ZENG, Shanghai Aircraft Customer Service Corporation, China
3.2Structural Health Monitoring 1
Chair(s): Ikeda, T.
Track 3
04.1 - Material Issues, Fatigue and Damage Tolerance
13. Sep 18 14:00 14:30 3.2.1 OPTIMIZATION OF THE COEFFICIENT OF PROBABILITY DISTRIBUTION FUNCTION IN DAMAGE DETECTION USING GENETIC ALGORITHM
A. Abedian Abedian, Sharif University of Technology, Iran
13. 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. Bautin, Yu Bautin, TsAGI, Russia
13. Sep 18 15:00 15:30 3.2.3 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 DEVELOPMENT OF METHODS FOR DETERMINING CRACK RESISTANCE PARAMETERS FOR STATIC AND FATIGUE LOADING FOR POLYMER COMPOSITE
Yu.V. Koroleva¹, V.L. Tokar¹, Yu.A. Svirsky¹; ¹TsAGI, Russia
4.2RANS Models
Chair(s): Antunes, A., Viviani, A.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
13. Sep 18 14:00 14:30 4.2.1 MULTIPHASE TURBULENCE MODELS FOR SCRAMJETS AND ABLATING WALLS
K.E.Son Son, Russia
13. Sep 18 14:30 15:00 4.2.2 2D-RANS APPROACH TO STUDY A TURBULENT SEPARATED FLOW USING BSL EARSM MODEL
M.D.Q. De Queiroz, Pontificia Universidade Católica de Minas Gerais, Brazil
13. Sep 18 15:00 15:30 4.2.3 NUMERICAL COMPARISON OF STEADY DISTURBANCES IN THE WAKE OF PERIODIC BLOW-SUCTION AND ROUGHNESS ELEMENTS
P. V. Chuvakhov, Central Aerohydrodynamic Institute (TsAGI), Russia
Reserve Paper 4.2.R NUMERICAL INVESTIGATION OF FLOW STRUCTURE OF DIFFERENTIAL EJECTOR
H-Y Zhang, China Aerodynamics Research and Development Center, China
5.2Modeling and Simulation in Manufacturing
Chair(s): Soares, F.
Track 5
08 - Manufacturing and Supply Chain Management
13. Sep 18 14:00 14:30 5.2.1 ENABLING THE DIGITAL FACTORY THROUGH THE INTEGRATION OF DATA-DRIVEN AND SIMULATION MODELS
O Pinon Fischer, Georgia Institute of Technology, United States
13. Sep 18 14:30 15:00 5.2.2 ON-DEMAND SMALL UAS ARCHITECTURE SELECTION AND RAPID MANUFACTURING USING A MODEL-BASED SYSTEMS ENGINEERING APPROACH
C.Y. Justin, Georgia Institute of Technology, United States
13. Sep 18 15:00 15:30 5.2.3 MANUFACTURING OF CIVIL AIRCRAFT REAR FUSELAGE WITH AUTOMATED FIBER PLACEMENT PROCESS (AFP)
R. Andrade de Oliveira, Lightweight Structures Laboratory (LEL) / IPT, Brazil
Reserve Paper 5.2.R GEOMETRIC MODELING AND IDENTIFICATION OF SHAPE ERRORS AS NECESSARY STEPS FOR HSM MACHINING OF AIRCRAFT PARTS
S. Zietarski, Military University of Technology, United Kingdom
6.2High Speed Transition
Chair(s): Atkin, C.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
13. Sep 18 14:00 14:30 6.2.1 THEORETICAL STUDY OF RECEPTIVITY OF HIGH-SPEED BOUNDARY LAYER TO THREE DIMENSIONAL SURFACE VIBRATION
Youcheng Xi, School of Aerospace Engineering, Tsinghua University, China
13. Sep 18 14:30 15:00 6.2.2 DIRECT NUMERICAL SIMULATION OF MACH WAVE INFLUENCE ON LAMINAR-TURBULENT TRANSITION IN SUPERSONIC FLOW OVER A FLAT PLATE
I.V. Egorov, TsAGI, Russia
13. Sep 18 15:00 15:30 6.2.3 ENTROPY LAYER EFFECT ON ROUGHNESS-INDUCED LAMINAR-TURBULENT TRANSITION IN SUPERSONIC FLAT PLATE FLOW
P. V. Chuvakhov, Central Aerohydrodynamic Institute (TsAGI), Russia
Reserve Paper 6.2.R EFFECT OF CONTROLLED PERIODIC ROUGHNESS ON GOERTLER VORTICES IN HYPERSONIC COMPRESSION RAMP FLOW
P. V. Chuvakhov, Central Aerohydrodynamic Institute (TsAGI), Russia
7.2New Structural Design 3: Material and Micro Structures
Chair(s): Zanardi, H.
Track 7
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
13. Sep 18 14:00 14:30 7.2.1 METHOD FOR FLEXIBLE SKELETON COMPOSED OF THE TYPE OF INCIRCLE ELEMENT BASED ON EQUAL DISPLACEMENTAND ITS APPLICATION
Y.-C. DENG, SADRI, China
13. Sep 18 14:30 15:00 7.2.2 DEVELOPMENT OF STRUCTURE ELEMENTS BASED ON ARCHITECTURED MATERIALS FOR PERSPECTIVE CIVIL AIRCRAFTS
O. Kondakov, Central Aerohydrodynamic Institute n.a. prof. N.E. Zhukovsky, Russia
13. Sep 18 15:00 15:30 7.2.3 PREDICTIONOF THE CRACK PATTERN IN DUCTILE MATERIALS SUBJECT TO MECHANICAL LOADING USINGLATTICE MODELS
H Zanardi, Brazil
8.2Structural Optimization
Chair(s): Fredriksson, B.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
13. Sep 18 14:00 14:30 8.2.1 PROBABILISTIC METHOD OF DETERMINATION OF ALLOWABLE DESIGN PARAMETER SCATTERS ON FLUTTER AND STRENGTH CRITERIA
V.V. Chedrik¹, D.V. Chemisov¹; ¹Central Aerohydrodynamic Institute, Russia
13. Sep 18 14:30 15:00 8.2.2 STRUCTURES TOPOLOGIC OPTIMIZATION BASED ON DARWIN´S EVOLUTIONARY THEORY
M. P. Brandão, ITA, Brazil
13. Sep 18 15:00 15:30 8.2.3 STRESS-BASED TOPOLOGY OPTIMIZATION WITH USING GLOBAL-LOCAL APPROACH
V.V. Chedrik¹, S.A, Tuktarov¹; ¹Central Aerohydrodynamic Institute, Russia
Reserve Paper 8.2.R OPTIMIZATION OF SCARF JOINT ANGEL AND OVERPLY DOUBLER USING GENETIC ALGORITHM CONSIDERING ADHESIVE MATERIAL NONLINEARITY
A. Abedian, Aerospace Eng Dept, Sharif Uni of Tech, Iran
9.2ISABE
Chair(s): ,
Track 9
10.2Flight Testing
Chair(s): Naruoka, M.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
13. Sep 18 14:00 14:30 10.2.1 WIND TUNNEL VIRTUAL FLIGHT TEST FOR A TRANSPORT AIRCRAFT WITH SIMULATED ICE SHAPE
L.-L Guo, China Aerodynamic Research and Development Center , China
13. Sep 18 14:30 15:00 10.2.2 DEVELOPMENT OF A GENERIC FLIGHT TEST MANEUVER INJECTION MODULE
C Krause, Institute of Flight System Dynamics (TUM), Germany
13. Sep 18 15:00 15:30 10.2.3 CHARACTERISTIC HELICOPTER FLIGHT MECHANICS AND MOTION CUEING INTEGRATION INTO THE SIVOR ROBOTIC FLIGHT SIMULATOR
D.-F. Hidalgo, Universidad Pontificia Bolivariana, Colombia
Reserve Paper 10.2.R KNOWLEDGE ENGINEERING BASED FLIGHT TEST TECHNOLOGY FOR CIVIL AIRCRAFT AIRWORTHINESS CONFORMITY
LI ZHAOHUI¹, LI GANG¹; ¹Chinese Flight Test Establishment, China
11.2De-Icing
Chair(s): ,
Track 11
07 - Systems, Subsystems and Equipment
13. Sep 18 14:00 14:30 11.2.1 DE-ICING PHENOMENA MODELLED BY FINITE ELEMENT MODELS
R. SCIGLIANO, Italian Aerospace Research Centre (CIRA), Italy
13. Sep 18 14:30 15:00 11.2.2 DETECTING HIGH-ALTITUDE ICE CRYSTAL ICING EVENTS FROM TAT ANAOMALIES
R. M. Arnaldo Valdés, Universidad Politecnica de Madrid, Spain
13. Sep 18 15:00 15:30 11.2.3 NUMERICAL SIMULATION OF ICE ACCRETION INFLUENCED BY AN ANTI-ICING HEATING SYSTEM
K. Szilder, Aerospace, National Research Council, Canada
Reserve Paper 11.2.R CALCULATION OF WATER FILM FLOW AND HEAT TRANSFER ON THE AIRCRAFT ANTI-ICING SURFACE
W Dong, Shanghai Jiao Tong University, China
12.2Air Turbulence
Chair(s): Heinzinger, O.
Track 12
10 - Safety and Security
13. Sep 18 14:00 14:30 12.2.1 FLIGHT LOADS ON LIGHT AIRCRAFT IN LANDING TRAJECTORIES THROUGH WINDY ATMOSPHERE AND NEAR WIND FARMS
A. De Marco, University of Naples Federico II, Dept. Industrial Engineering, Italy
13. Sep 18 14:30 15:00 12.2.2 DEVELOPMENT AND FLIGHT DEMONSTRATION OF A NEW LIDAR-BASED ONBOARD TURBULENCE INFORMATION SYSTEM
N. M. Matayoshi, Japan Aerospace Exploration Agency, Japan
13. Sep 18 15:00 15:30 12.2.3 HAZARDOUS MITIGATION FOR TRANSPORT AIRCRAFT IN SEVERE ATMOSPHERIC TURBULENCE BASED ON IMPROVED CONTROL STRATEGY
C. Chang, College of General Aviation, Wenzhou University, China

15:30 - 16:00Break

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: Shinji Suzuki Chair ICAS Programme Committee
13. Sep 18 16:00 17:00

17:00 - 17:30Closing Ceremony