29th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

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Attention: Be advised that there might be changes till the congress, so please do not adjust your travel plans based on this preliminary programme.
7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room

Monday, 26. Sep 2016


7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
0.1Registration
Chair:
26. Sep 16 07:00 08:00

0.2Opening ceremony
Chair: Christian Mari ICAS president
26. Sep 16 08:00 09:00

0.3ICAS DANIEL & FLORENCE GUGGENHEIM MEMORIAL LECTURE
Chair: Christian Mari ICAS president
26. Sep 16 09:00 10:00 Design, Development and Flight test of Vertical Take-Off and Landing UAV, Cyclocopter
Seung Jo Kim

 Break

1.1Unconventional Aircraft
Chair(s): , , Rinoie, K.
Track1
01 - Aircraft and Systems Integration
26. Sep 16 10:30 11:00 1.1.1 UNCONVENTIONAL CONFIGURATIONS - DESIGN AND OPTIMIZATION
T. Goetzendorf-Grabowski¹, J. Mieloszyk¹; ¹Warsaw University of Technology, Poland
26. Sep 16 11:00 11:30 1.1.2 INFLUENCE OF POWER UNIT CONFIGURATION LAYOUT OF A REGIONAL JET ON PERFORMANCE AND DIRECT OPERATING COST
Z. Goraj¹, A. Sieradzki¹; ¹Institute of Aviation, Poland
26. Sep 16 11:30 12:00 1.1.3 DEVELOPMENT OF THE SMALL-SCALE MODEL OF MAGLEV SYSTEM ASSISTED AIRCRAFT SAFETY TAKE-OFF AND LANDING
K. Sibilski¹, K. Fakkowski, Military University of Technology Technology, Poland; R. Kaleta, Air Force Institute of Technology, Poland; E. Ladyzynska-Kozdras¹, A.-M. Sibilska-Mroziewicz¹, W. Wróblewski, Wroclaw University of Technology, Poland; ¹Warsaw University of Technology, Poland
2.1Fluid-Structure Interaction
Chair(s): Lott, M.
Track 2
02.1 - Aerodynamics - CFD Methods and Validation
26. Sep 16 10:30 11:00 2.1.1 A COMPUTATIONAL STUDY ON AVIAN FLAPPING FLIGHT AND THE INFLUENCE OF FEATHER SEPARATION
J. Feaster¹, F. Battaglia¹, J. Bayandor¹; ¹Virginia Tech, United States
26. Sep 16 11:00 11:30 2.1.2 EFFECT OF ELASTIC DEFORMATION ON FLIGHT DYNAMICS OF PROJECTILES WITH LARGE SLENDERNESS RATIO
R.H. Hua ¹, Z.Y. Ye¹, L. Yang¹; ¹Northwestern Polytechnical University, China
3.1Experiments in Flow Control
Chair(s): Consigny, H.
Track 3
02.2 - Experimental Aerodynamics
26. Sep 16 10:30 11:00 3.1.1 THE ROUGHNESS POSITION INFLUENCE ON LAMINAR AEROFOIL AERODYNAMIC CHARACTERISTIC IN TRANSONIC FLOW REGIME
R. Placek¹, M. Miller¹, P. Ruchala¹; ¹Institute of Aviation, Poland
4.1(Aerodynamic) Control Methods
Chair(s): Collier, F.
Track 4
02.4 - Applied Aerodynamics
26. Sep 16 10:30 11:00 4.1.1 IMPORTANCE OF TRANSIENT AERODYNAMIC DERIVATIVES FOR V-TAIL AIRCRAFT FLIGHT DYNAMIC DESIGN
N.A. Musa¹, S. Mansor¹, A. Ali¹, W.Z. Wan Omar¹; ¹AeroLAB, Universiti Teknologi Malaysia, Malaysia
26. Sep 16 11:00 11:30 4.1.2 AFLONEXT – ACTIVE FLOW_LOADS AND NOISE CONTROL ON NEXT GENERATION ACTIVE WING
C. Atkin, City University London, United Kingdom
5.1Avionics & Real Time Monitoring
Chair(s): ,
Track 5
06 - Systems, Subsystems and Equipment
26. Sep 16 10:30 11:00 5.1.1 GENERAL MESSAGE RACES IN DATA DISTRIBUTION SERVICE PROGRAMS FOR AIRBORNE SOFTWARE
H.-J. Kim¹, O.-K. Ha¹, Y.-K. Jun¹; ¹Gyeongsang National University, South Korea
26. Sep 16 11:00 11:30 5.1.2 A KNOWLEDGE-BASED REAL TIME MONITORING AND DIAGNOSITC APPROACH FOR AIRCRAFT BREAKING SYSTEM
X. Chen¹, H. Ren¹, J. Wang, University of Illinois at Urbana-Champaign, United States; Y. Chen¹, J. Chen¹, L. Zhi¹; ¹COMAC, China
6.1Structural System Design
Chair(s): Park, J., Degenhardt, R.
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
26. Sep 16 10:30 11:00 6.1.1 EVALUATION OF CONCEPTUAL DESIGN BASED ON MANUFACTURED ACTUAL UNMANNED SOLAR PLANE
N. Arai¹, W. Harasani, King Abdruaziz Univ., Saudi Arabia; K. Hiraoka¹; ¹Tokai Univ., Japan
26. Sep 16 11:00 11:30 6.1.2 NEW DESIGN SCENARIO FOR FUTURE COMPOSITE LAUNCHER STRUCTURES
R. Degenhardt, DLR, Germany
26. Sep 16 11:30 12:00 6.1.3 MULTIDISCIPLINARY TOPOLOGY-BASED OPTIMIZATION IN DESIGN OF AIRCRAFT STRUCTURAL LAYOUTS
K.A. Balunov¹, V.V. Chedrik¹, S.A. Tuktarov¹, V.M. Uskov¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
7.1Advanced Engines 1
Chair(s): Mirzoyan, A., Ryemill, M.
Track 7
04 - Propulsion
26. Sep 16 10:30 11:00 7.1.1 KEY TECHNOLOGIES FOR THE NEXT GENERATION OF CIVIL AIRCRAFT ENGINES
F. Haselbach, Rolls-Royce plc, United Kingdom
26. Sep 16 11:00 11:30 7.1.2 THE ROLLS-ROYCE PLC ULTRAFAN HEAT MANAGEMENT CHALLENGE
M. Ryemill¹, C. Bewick¹, J.K. Min, Pusan UTC, South Korea; ¹Rolls-Royce plc, United Kingdom
26. Sep 16 11:30 12:00 7.1.3 DEVELOPMENT OF TECHNOLOGY ADVANCE FOR FUTURE PROPULSION SYSTEMS OF HAUL AIRCRAFT
A. Lanshin¹, A. Mirzoyan¹, A. Polev¹; ¹CIAM, Russia
8.1Flight Control 1
Chair(s): Che, J., Ueno, S.
Track 8
05.1 - Flight Dynamics and Control (Control & Modelling)
26. Sep 16 10:30 11:00 8.1.1 AUGMENTED POLYNOMIAL GUIDANCE FOR TERMINAL VELOCITY CONSTRAINTS
G.-H. Moon¹, S.-W. Shim¹, M.-J. Tahk¹; ¹KAIST, South Korea
26. Sep 16 11:00 11:30 8.1.2 IMPACT ANGLE CONTROL GUIDANCE CONSIDERING GRAVITY EFFECT
H.-G. Kim¹, H.-J. Kim¹; ¹Seoul National University, South Korea
26. Sep 16 11:30 12:00 8.1.3 TERMINAL IMPACT ANGLE AND ANGLE-OF-ATTACK CONTROL GUIDANCE FOR SURFACE-TO-AIR MISSILE USING TVC
S.-M. Hong¹, M.-G. Seo¹, M.-J. Tahk¹; ¹KAIST, South Korea
9.1UAV Control 1
Chair(s): Maroney, D., Krus, P.
Track 9
05.2 - Flight Dynamics and Control (UAV related)
26. Sep 16 10:30 11:00 9.1.1 ADAPTIVE NEURAL NETWORK CONTROLLER DESIGN FOR BLENDED-WING UAV WITH COMPLEX DAMAGE
K.J. Kim¹, J.M. Ahn, Agency for Defense and Development, South Korea; S.K. Kim¹, J.Y. Suk¹; ¹Chungnam national university, South Korea
26. Sep 16 11:00 11:30 9.1.2 MODELING AND CONTROL OF HIGHLY FLEXIBLE FLYING-WING UAV WITH MULTIPLE ELEVONS AND PROPELLERS
R. Wang¹, X.P. Zhu¹, Z. Zhou¹, Z.P. Wang¹; ¹Northwestern Polytechnical University, China
26. Sep 16 11:30 12:00 9.1.3 ON SAFETY ASSESSMENT OF NOVEL APPROACH TO ROBUST UAV FLIGHT CONTROL IN GUSTY ENVIRONMENTS
V. Golubev¹, P. Kazarin¹, W. MacKunis¹, S. Borener², D. Hufty²; ¹ERAU, United States ;²FAA, United States
10.1Reduced Order Modeling
Chair(s): , , Pechloff, A.
Track 10
02.3 - Basic Fluid Dynamics and Flow Control
26. Sep 16 10:30 11:00 10.1.1 ON APPLYING PISTON THEORY IN INTERFERENCE FLOWS
M.-C. Meijer, University of Pretoria, South Africa; L. Dala, Council for Scientific and Industrial Research, South Africa; P.G. Karkle, Central Aerohydrodynamic Institute, Russia
26. Sep 16 11:00 11:30 10.1.2 UNSTEADY AERODYNAMICS MODELLING AND ITS APPLICATION IN AEROELASTIC STABILITY ANALYSIS
X. Li¹, W. Zhang ¹; ¹School of aeronautics, Northwestern Polytechnical University, China
11.1Network Operations
Chair(s): Jeon, D., Hoekstra, J.
Track 11
08 - Air Transport System Efficiency
26. Sep 16 10:30 11:00 11.1.1 AN EXPLORATION OF EVOLUTION PATHS FOR AIR TRANSPORTATION NETWORKS
J.-H. Lewe¹, K. Song¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States
26. Sep 16 11:00 11:30 11.1.2 A REVIEW AND A CLASSIFICATION SCHEME FOR AIR TRANSPORTATION NETWORK RESEARCH
K. Song¹, J.-H. Lewe¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States
26. Sep 16 11:30 12:00 11.1.3 AUTOMATED SEPARATION ASSURANCE AND COLLISION AVOIDANCE FUNCTIONS IN THE CNS+A CONTEXT
S. Ramasamy¹, R. Sabatini¹, Y. Lim¹, A. Gardi¹; ¹RMIT University, Australia
12.1ISABE 1
Chair(s): Remy, S.
Track 12
26. Sep 16 10:30 11:00 12.1.1 RTO\\\'S AND TECHNOLOGY DE-RISKING
I. Potter, National Research Council Canada, Canada

 Lunch

1.2MDO Application
Chair(s): Prince, S., Ogilvie, F.
Track1
01 - Aircraft and Systems Integration
26. Sep 16 13:00 13:30 1.2.1 TOWARDS THE 3RD GENERATION MDO COLLABORATIVE ENVIRONMENT
P.D. Ciampa¹, B. Nagel¹; ¹German Aerospace Center, DLR, Germany
26. Sep 16 13:30 14:00 1.2.2 STRUCTURAL CONSTRAINTS INVESTIGATION IN WING AERODYNAMIC/STRUCTURAL OPTIMIZATION
K.-S. Zhang¹, H. Zhang¹, Z.-H. Han¹; ¹Northwestern Polytechnical University, China
26. Sep 16 14:00 14:30 1.2.3 MULTIDISCIPLINARY DESIGN OPTIMIZATION FOR FIGHTER AIRCRAFT CONFIGURATION
C. Lee, Korea Aerospace Industries, LTD., South Korea
2.2Vortical Flows
Chair(s): , , Stumpf, E.
Track 2
02.1 - Aerodynamics - CFD Methods and Validation
26. Sep 16 13:00 13:30 2.2.1 APPLICATION OF PROPER ORTHOGONAL DECOMPOSITION FOR AVIATION SAFETY
J.H. Cho¹, S.K. Jeong, Kyung Hee University, South Korea; K.J. Yee¹; ¹Seoul National University, South Korea
26. Sep 16 13:30 14:00 2.2.2 LARGE-SCALE VORTEX STRUCTURE OF FLOW IN THE NEAR WAKE BEHIND AN AIRLINER DURING TAKEOFF AND LANDING
Y.M. Tsirkunov¹, M.A. Lobanova¹, A.I. Tsvetkov², B.A. Schepanyuk²; ¹Baltic State Technical University, Russia ;²Saint Petersburg State University, Russia
3.2Intake Aerodynamics
Chair(s): Haselbach, F.
Track 3
02.2 - Experimental Aerodynamics
26. Sep 16 13:00 13:30 3.2.1 INLET DUCT ENGINE TEST FACILITIES IN INDONESIA LOW SPEED TUNNEL (ILST)
S. Subagyo, BBTA3-BPPT, Indonesia
26. Sep 16 13:30 14:00 3.2.2 AERODYNAMIC TESTING OF HELICOPTER NOVEL AIR INTAKES
F. Knoth¹, C. Breitsamter¹; ¹Chair of Aerodynamics and Fluid Mechanics, TU Munich, Germany
26. Sep 16 14:00 14:30 3.2.3 KAI SURION HELICOPTER FULL-SCALE AIR INTAKE TESTING AT CIRA ICING WIND TUNNEL
A.C. de Bruin, NLR, Netherlands; G. Fatigati, CIRA, Italy; H.B. Shin, KAI, South Korea
4.2Super- and Hypersonic Aerodynamics 1
Chair(s): Philpott, D.
Track 4
02.4 - Applied Aerodynamics
26. Sep 16 13:00 13:30 4.2.1 THE EFFECT OF LEADING EDGE ROUNDING ON A CARET WAVERIDER CONFIGURATION AT MACH 8.2
B. McCartney¹, S. Prince¹, N. Qin, University of Sheffield, United Kingdom; ¹Cranfield University, United Kingdom
5.2Thermal Modeling
Chair(s): Fu, Y., Derrien, J.C.
Track 5
06 - Systems, Subsystems and Equipment
26. Sep 16 13:00 13:30 5.2.1 SPECIAL CONSIDERATIONS TO THERMAL BEHAVIOR MODELING AND SIMULATION OF AN AEROSPACE ELECTROMECHANICAL ACTUATION SYSTEM
J. Fu¹, Y. Fu¹, J.-C. Mare, Institut Clément Ader, INSA-Toulouse, France; ¹Beihang University, China
26. Sep 16 13:30 14:00 5.2.2 COUPLED EMC-THERMAL MODELING OF ELECTRICAL HARNESSES WITHIN \"MORE ELECTRICAL AIRCRAFT\"
F. Mahiddini¹, M. Ridel¹, P. Reulet¹, D. Donjat¹, P. Millan¹; ¹ONERA, France
6.2Loads
Chair(s): Han, J.
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
26. Sep 16 13:00 13:30 6.2.1 UNSTEADY AERODYNAMIC FORCE SENSING FROM MEASURED STRAIN
C.-G. Pak, NASA Armstrong Flight Research Center, United States
26. Sep 16 13:30 14:00 6.2.2 NONLINEAR DAMAGE MODELING AND ANALYSIS OF VISCOPLASTIC COMPOSITE MATERIALS
I.K. Park¹, T.-U. Kim¹, S.-H. Kim¹; ¹KARI, South Korea
7.2Advanced Engines 2
Chair(s): Remy, S.
Track 7
04 - Propulsion
26. Sep 16 13:00 13:30 7.2.1 MISSION BASED COMPARISON OF SINGLE- AND COUNTER-ROTATING FAN DESIGNS
T. Otten¹, T. Lengyel-Kampmann¹; ¹German Aerospace Center (DLR), Germany
26. Sep 16 13:30 14:00 7.2.2 AERODYNAMIC OPTIMIZATION OF AIRPLANE PROPULSION SYSTEM WITHIN THE FRAMEWORK OF AGILE PROJECT
K. Anisimov¹, A.A. Savelyev¹; ¹TsAGI, Russia
26. Sep 16 14:00 14:30 7.2.3 APPLICATION OF FLAME MEASUREMENT TECHNIC BY DENSELY INSTALLED ION-PROBES ON 2-STROKE GASOLINE ENGINE
T. Yatsufusa¹, K. Takatani¹, S. Miyata¹; ¹Hiroshima Institute of Technology, Japan
8.2Flight Control 2
Chair(s): Vian, J., Watanabe, Y.
Track 8
05.1 - Flight Dynamics and Control (Control & Modelling)
26. Sep 16 13:00 13:30 8.2.1 MISSILE AUTOPILOT DESIGN USING CONTRACTION THEORY-BASED OUTPUT FEEDBACK CONTROL
H.-H. Kwon¹, H.-L. Choi¹; ¹KAIST, South Korea
26. Sep 16 13:30 14:00 8.2.2 FLIGHT CONTROL LAW CLEARANCE USING WORST-CASE INPUTS
J. Diepolder¹, J.Z. Ben-Asher, Faculty of Aerospace Engineering - Technion, Israel; A. Gabrys¹, S. Schatz¹, M. Bittner¹, M. Rieck¹, B. Grüter¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics - TUM, Germany
26. Sep 16 14:00 14:30 8.2.3 AN INVESTIGATION OF EFFECTS OF FLIGHT MANEUVERS ON A SUPERSONIC AIRCRAFT WITH HORIZONTAL TAIL ACTUATOR FAILURE
S. Oh¹, I. Cho¹, C. McLaughlin, The University of Kansas, United States; ¹Korea Aerospace Industries, LTD, South Korea
9.2UAV Control 2
Chair(s): , , Bil, C.
Track 9
05.2 - Flight Dynamics and Control (UAV related)
26. Sep 16 13:00 13:30 9.2.1 GUIDANCE AND CONTROL OF AUTOMATIC SHORT LANDING WITH STEEP GLIDE SLOPE FOR UAV
J. Moon¹, S. Choi¹, S. Cho¹, H. Kim¹; ¹KOREANAIR, South Korea
26. Sep 16 13:30 14:00 9.2.2 NONLINEAR DYNAMIC INVERSION WITH NEURAL NETWORKS FOR THE FLIGHT CONTROL OF A LOW COST TILT ROTOR UAV
E. D\'Amato¹, G. Tartaglione, University of Naples Parthenope, Italy; L. Blasi¹, M. Mattei¹; ¹Second University of Naples, Italy
26. Sep 16 14:00 14:30 9.2.3 DEPTH IMAGE BASED DIRECT SLAM FOR SMALL UAVS
S.Y. Park¹, D.H. Shim¹; ¹KAIST, South Korea
10.2Synthetic Jets
Chair(s): Goraj, Z., Wood, N.
Track 10
02.3 - Basic Fluid Dynamics and Flow Control
26. Sep 16 13:00 13:30 10.2.1 EXPERIMENTAL STUDY ON AERODYNAMIC LOAD CONTROL USING SYNTHETIC JET ACTUATORS
T.A. Berk¹, H.W.M. Hoeijmakers¹; ¹University of Twente, Netherlands
26. Sep 16 13:30 14:00 10.2.2 NUMERICAL SIMULATION OF FLOW SEPARATION CONTROL OVER A HUMP USING DBD PLASMA ACTUATOR
A. Jahangirian¹, R. Khoshkhoo¹; ¹Amirkabir University of Technology, Iran
11.2Formation Flight
Chair(s): Doll, T.
Track 11
08 - Air Transport System Efficiency
26. Sep 16 13:00 13:30 11.2.1 PLANNING AIR TEAM MISSIONS WITH MULTIPLE OBJECTIVES
T. Erlandsson, University of Skövde, Sweden
26. Sep 16 13:30 14:00 11.2.2 APPLYING REQUIRED NAVIGATION PERFORMANCE CONCEPT FOR TRAFFIC MANAGEMENT OF SMALL UNMANNED AIRCRAFT SYSTEMS
J. Jung¹, S.N. D\'Souza¹, M.A. Johnson¹, A.K. Ishihara², H.C. Modi², B. Nikaido³, H. Hasseeb³; ¹NASA Ames Research Center, United States ;²SGT Inc., United States ;³Science & Technology Corp., United States
26. Sep 16 14:00 14:30 11.2.3 INFLUENCE OF AIRCRAFT TYPE AND ORDER ON FUEL SAVINGS GAINED BY TWO-AIRCRAFT FORMATIONS
T. Marks¹, V. Gollnick¹; ¹German Aerospace Center, Germany
12.2Vehicle Optimization and Design
Chair(s): Yee, K., Hua, J.
Track 12
02.1 - Aerodynamics - CFD Methods and Validation
26. Sep 16 13:00 13:30 12.2.1 KNOWLEDGE-BASED INTEGRATED AIRCRAFT WINDSHIELD OPTIMIZATION
R.C. Munjulury¹, R. Gårdhagen¹, P. Berry¹, P. Krus¹; ¹Linköping University, Sweden
26. Sep 16 13:30 14:00 12.2.2 OPTIMISATION OF A WING-BODY-TAIL CONFIGURATION WITH AN ALTERNATIVE LOW DRAG FUSELAGE AND BODY TRAILING EDGE
L. Smith¹, K.J. Craig¹, J.P. Meyer¹, G.R. Spedding, University of Southern California, United States; ¹University of Pretoria, South Africa
26. Sep 16 14:00 14:30 12.2.3 DESIGN OPTIMIZATION OF HELICOPTER BLADE USING CLASS SHAPE FUNCTION BASED GEOMETRY REPRESENTATION
A. Ariyarit¹, M. Sugiura², Y. Tanabe², M. Kanazaki¹; ¹Tokyo Metropolitan University, Japan ;²Japan Aerospace Exploration Agency, Japan

 Break

0.4General Lecture 1 Part 1
Chair: Christian Mari ICAS president
26. Sep 16 15:00 16:30 Airframer vision of the aircraft of the future
Sebstien Remy, Airbus / Keoki Jackson LMCO / Mike Sinnett Boeing

0.5General Lecture 1 Part 2
Chair: Christian Mari ICAS president
26. Sep 16 16:30 18:00 What do Airframers want from Equipment makers in terms of leading edge technologies
Frank Haselbach, Rolls Royce / Bruno Stoufflet, Dassault Aviation / Sung Sub Jang, Korean Aerospace Industry

Tuesday, 27. Sep 2016


7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
0.6General Lecture 2
Chair: Shinji Suzuki SPSC Chair
27. Sep 16 08:00 09:00 D-SEND#2 - Flight tests for low sonic boom design technology
Kenji Yoshida

0.7Interactive presentations
Chair: Artur Mirzoyan
27. Sep 16 09:00 10:00

1.3Design Method 1
Chair(s): Lee, D., Mavris, D.
Track1
01 - Aircraft and Systems Integration
27. Sep 16 10:00 10:30 1.3.1 KNOWLEDGE-BASED FUTURE COMBAT AIRCRAFT OPTIMIZATION
R.C. Munjulury¹, A.M. Abdalla, University of São Paulo, Brazil; I. Staack¹, P. Krus¹; ¹Linköping University, Sweden
27. Sep 16 10:30 11:00 1.3.2 COLLABORATIVE AIRCRAFT DESIGN USING AN INTEGRATED AND DISTRIBUTED MULTIDISCIPLINARY PRODUCT DEVELOPMENT PROCESS
E. Moerland¹, S. Deinert², F. Daoud², J. Dornwald², B. Nagel¹; ¹German Aerospace Centre (DLR), Germany ;²Airbus Defence & Space, Germany
27. Sep 16 11:00 11:30 1.3.3 USING OPENVSP IN A CONCEPTUAL AIRCRAFT DESIGN ENVIRONMENT IN MATLAB
S. Herbst¹, A. Staudenmaier¹; ¹Technical University of Munich / Institute of Aircraft Design, Germany
27. Sep 16 11:30 12:00 1.3.4 INTEGRATED CONCEPTUAL DESIGN METHOD CONSIDERING ADVANCED AIRCRAFT SYSTEMS AND AIRCRAFT TRAJECTORY
T. Chiba¹, K. Rinoie¹; ¹The University of Tokyo, Japan
2.3tbd
Chair(s): ,
Track 2
3.3Wing Aerodynamics
Chair(s): Atkin, C.
Track 3
02.2 - Experimental Aerodynamics
27. Sep 16 10:00 10:30 3.3.1 AN EXPERIMENTAL INVESTIGATION ON THE FREESTREAM TURBULENCE UPSTREAM OF A SWEPT WING
I. Fumarola, City University London, United Kingdom
27. Sep 16 10:30 11:00 3.3.2 EFFECTS OF REYNOLDS NUMBER ON THE ONSET OF LEADING EDGE VORTEX SEPARATION ABOVE BLUNT-EDGE DELTA WING VFE-2 CONFIGURATIONS
M. Said¹, S. Mat¹; ¹AeroLab, Universiti Teknologi Malaysia, Malaysia
27. Sep 16 11:00 11:30 3.3.3 LOW ORDER MODELING OF THE UNSTEADY AND 3D EFFECTS OF CONTINUOUS WAKE FLAPPING FLIGHT
A. Matta¹, J. Bayandor¹; ¹Virginia Tech, United States
27. Sep 16 11:30 12:00 3.3.4 EFFECTS OF PROPELLER LOCATIONS ON THE VORTEX SYSTEM ABOVE DELTA-SHAPED UAV MODEL
K.A. Kasim¹, S. Mat¹, I.S. Ishak¹, M. Said¹; ¹Universiti Teknologi Malaysia, Malaysia
4.3Vortical Flow
Chair(s): Gustaffson, A.
Track 4
02.4 - Applied Aerodynamics
27. Sep 16 10:00 10:30 4.3.1 SIMULATION OF UNSTEADY SHIP AIRWAKES USING OPENFOAM
W. Yuan¹, R. Lee¹, A. Wall¹; ¹National Research Council Canada, Canada
27. Sep 16 10:30 11:00 4.3.2 EXTRACTION OF LINEAR INFLOW MODEL FOR MANEUVERING HELICOPTER FROM FREE-WAKE ANALYSIS
O. Rand¹, V. Khromov¹; ¹Israel Institute of Technology, Israel
5.3Operations & Sustainment 1
Chair(s): Liao, M., Anderson, K.
Track 5
11 - Operations and Sustainment
27. Sep 16 10:00 10:30 5.3.1 TRANSFORMING MILITARY AEROSPACE SUSTAINMENT
D. Holmes¹, A. Goodwin¹, R. Vodicka¹; ¹DSTG, Australia
27. Sep 16 10:30 11:00 5.3.2 LCC ESTIMATION AND CASE STUDY USING RELIABILITY AND MAINTAINABILITY ANALYSIS
S.-Y. Lee, Korean Air, South Korea
27. Sep 16 11:00 11:30 5.3.3 INVESTIGATIONS OF GROUND INFRASTRUCTURES FOR UAS FLIGHT MONITORING
S. Cresto Aleina¹, R. Fusaro¹, N. Viola¹; ¹Politecnico di Torino, Italy
6.3Structural Design 1 SHELLS
Chair(s): Cho, J.Y., Pranata, B.
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
27. Sep 16 10:00 10:30 6.3.1 WEIGHT REDUCTION OF CYLINDRICAL GRID STRUCTURES USING AXIAL-HELICAL-DESIGN
M. Beerhorst¹, C. Hühne¹; ¹DLR, Germany
27. Sep 16 10:30 11:00 6.3.2 CHAOS THEORY APPLIED TO BUCKLING ANALYSIS OF COMPOSITE CYLINDRICAL SHELL
M. Alfano, Politecnico di Milano, Italy; C. Bisagni, Delft University of Technology, Netherlands
27. Sep 16 11:00 11:30 6.3.3 DEVELOPMENT OF LIGHTWEIGHT AND RELIABLE JOINTS FOR AIRFRAMES BASED ON UNIDIRECTIONAL COMPOSITE ELEMENTS
A.N. Shanygin¹, A.V. Chernov¹, D.Y. Fomin¹, V.I. Grishin, TsAGI, Russia; I.N. Kacharava¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
27. Sep 16 11:30 12:00 6.3.4 PANEL VIBRO-ACOUSTIC RESPONSE PREDICTION BASED ON TURBULENT BOUNDARY LAYER MEASUREMENT
X.J. Zhao¹, B. Ai¹; ¹China Academy of Aerospace Aerodynamics, China
7.3Fan & Compressors: MDO
Chair(s): , , Chen, H.
Track 7
04 - Propulsion
27. Sep 16 10:00 10:30 7.3.1 MULTI-POINT DESIGN OPTIMIZATION OF A HIGH BYPASS RATIO FAN BLADE
S. Qiu¹, X.Y. Deng¹; ¹AVIC Commercial Aircraft Engine CO.LTD, China
27. Sep 16 10:30 11:00 7.3.2 DEVELOPMENT OF THE FAN STAGE WITH ULTRA-LOW ROTATIONAL SPEED
S.V. Pankov, CIAM , Russia; V.I. Mileshin¹, I.K. Orekhov¹, V.A. Fateev¹; ¹CIAM, Russia
27. Sep 16 11:00 11:30 7.3.3 ADVANCED PROPULSION COLLISION DAMAGE DUE TO UNMANNED AERIAL SYSTEM INGESTION
Y.K. Song¹, K. Schroeder¹, B. Horton¹, J. Bayandor¹; ¹Virginia Tech, United States
27. Sep 16 11:30 12:00 7.3.4 MULTI-DISCIPLINARY DESIGN OF HIGH-SPEED COMPRESSORS FOR PROSPECTIVE TURBO-SHAFT ENGINE
A.N. Startsev¹, Y.M. Temis¹, E.G. Steshakov¹, D.A. Yakushev¹; ¹CIAM, Russia
8.3Flight Control 3
Chair(s): Kim, H.
Track 8
05.1 - Flight Dynamics and Control (Control & Modelling)
27. Sep 16 10:00 10:30 8.3.1 PRECISION LANDING BASED ON ATMOSPHERIC DISTURBANCE MONITORING AND MODEL PREDICTIVE CONTROL
N. Siepenkötter¹, D. Moormann¹; ¹RWTH Aachen University, Germany
27. Sep 16 10:30 11:00 8.3.2 ELASTIC MODES ADAPTIVE CANCELLATION ALGORITHM FOR THE A330 MRTT FLYING BOOM CONTROL LAWS
R. Rodríguez Robles¹, A. Sanz de Blas¹; ¹Airbus Defence & Space, Spain
27. Sep 16 11:00 11:30 8.3.3 ON STABILITY MARGIN OF A LQR-BASED VEHICLE NETWORK
Y. Kim¹, G. Seo¹; ¹Gyeongsang National University, South Korea
9.3UAV Test & Integration
Chair(s): Vian, J., Rein Weston, K.
Track 9
05.2 - Flight Dynamics and Control (UAV related)
27. Sep 16 10:00 10:30 9.3.1 LAND-BASED FLIGHT TEST FOR SHIPBOARD LANDING OF TILT ROTOR UAV
C.-S. Yoo¹, E.-Y. Jang¹, B.-S. Song¹, A. Cho¹, B.-J. Park¹, Y.-S. Kim¹, Y.-S. Kang¹, S.-O. Koo¹; ¹Korea Aerospace Research Institute, South Korea
27. Sep 16 10:30 11:00 9.3.2 ANALYSIS ON OFFLINE AND ONLINE IDENTIFICATION METHODS FOR AIRCRAFT STABILITY AND CONTROL DERIVATIVES
D. Ding¹, W.Q. Qian¹, Q. Wang¹; ¹Computational Aerodynamics Institute of CARDC, China
27. Sep 16 11:00 11:30 9.3.3 FLIGHT PATH RECONSTRUCTION FOR AN UNMANNED AERIAL VEHICLE USING LOW-COST SENSORS
C. Göttlicher¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, TU Munich, Germany
27. Sep 16 11:30 12:00 9.3.4 SYSTEM IDENTIFICATION OF A SCALE HELICOPTER IN HOVERING FLIGHT
F.C. Reis¹, E.M. Belo¹; ¹Escola de Engenharia de São Carlos - USP, Brazil
10.3Flow Separation and Control
Chair(s): Prince, S., Gowree, E.
Track 10
02.3 - Basic Fluid Dynamics and Flow Control
27. Sep 16 10:00 10:30 10.3.1 ACTIVE VORTEX FLOW CONTROL ON A GENERIC DELTA WING
A. Buzica¹, J. Bartasevicius¹, C. Breitsamter¹; ¹Chair of Aerodynamics and Fluid Mechanics, TUM, Germany
27. Sep 16 10:30 11:00 10.3.2 EFFECTIVENESS OF VORTEX GENERATORS IN HIGHLY 3D FLOWS
H.S. Mudhar, City University London, United Kingdom
27. Sep 16 11:00 11:30 10.3.3 EXPERIMENTAL INVESTIGATION OF FLOW AROUND AIRFOILS WITH UNDULATING LEADING EDGES
J. Pellicer, City University London, United Kingdom
27. Sep 16 11:30 12:00 10.3.4 AN EXPERIMENTAL AND COMPUTATIONAL STUDY OF THE AERODYNAMIC CHARACTERISTICS AN OSCILLATORY PITCHING NACA0012 AEROFOIL
A. Yadav¹, S. Prince¹, J. Holt¹; ¹Cranfield University, United Kingdom
11.3Airport Capacity
Chair(s): Reichmuth, J., Dubot, T.
Track 11
08 - Air Transport System Efficiency
27. Sep 16 10:00 10:30 11.3.1 AN INTERFACE CONCEPT TO SUPPORT THE COCKPIT CREW DURING TRAJECTORY-BASED DISPATCH TOWING
T. Bernatzky¹, S. Baumann¹, U. Klingauf¹; ¹Technische Universitaet Darmstadt, Germany
27. Sep 16 10:30 11:00 11.3.2 IMPROVEMENT OF PUSHBACK TIME ASSIGNMENT UNDER UNCERTAINTIES
R. Mori, Electronic Navigation Research Institute, Japan
27. Sep 16 11:00 11:30 11.3.3 TAXIING ROUTE PLANNING BASED ON AIRPORT HOTSPOTS
W.J. Pan¹, X. Wang¹, X.L. Luo, NORTHWEST AIR TRAFFIC CONTROL BUREAU OF CIVIL AVIATION OF CHINA, China; ¹CIVIAL AVIATION FLIGHT UNVIERSITY OF CHINA, China
27. Sep 16 11:30 12:00 11.3.4 SENSOR CONCEPT OF HIGHLY-AUTOMATED AIRPORT TUGS FOR REDUCED EMISSION TAXI OPERATIONS
S. Frank¹, P.M. Schachtebeck¹, P. Hecker¹; ¹TU Braunschweig, Institute of Flight Guidance, Germany
12.3Structural Design 5
Chair(s): Li, D.
Track 12
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
27. Sep 16 10:00 10:30 12.3.1 A STUDY ON FAILURE BEHAVIORS OF REPAIRED COMPOSITE STRUCTURES WITH SCARF BONDED PATCH
K.H. Nguyen¹, V.H. Truong¹, J.H. Kweon¹; ¹Gyeongsang National University, South Korea
27. Sep 16 10:30 11:00 12.3.2 RESEARCH ON VIBRATION CHARACTERISTIC FOR VARIABLE ROTATING VELOCITY BLADES
J. Qin¹, B.-W. Wang¹; ¹ASRI, China

 Lunch

0.8ICAS PAUL KEUK CHANG LECTURE FOR INNOVATION IN AERONAUTICS
Chair: Joao Luiz Azevedo EC member
27. Sep 16 13:00 14:00 The JSF Lift System
Gregg Pyers

1.4Innovative Concept-Super Heavy Cargo
Chair(s): Spieck, M.
Track1
01 - Aircraft and Systems Integration
27. Sep 16 14:00 14:30 1.4.1 A CONCEPTUAL DESIGN PLATFORM FOR BLENDED-WING-BODY TRANSPORTS
M. Zhang¹, Z. Chen¹, B. Zhang¹; ¹Northwestern Polytechnical University, China
2.4CFD Applications
Chair(s): Volkov, A.
Track 2
02.1 - Aerodynamics - CFD Methods and Validation
27. Sep 16 14:00 14:30 2.4.1 DYNAMICS MODELLING FOR CONTROL OF AN UNSTEADY HYDRODYNAMIC STINGRAY ROBOT
B. Gater, Virginia Tech , United States; J. Bayandor, Virginia Tech, United States
27. Sep 16 14:30 15:00 2.4.2 COMPUTATIONAL INVESTIGATION FOR FREE-FLIGHT AERODYNAMICS AND FLIGHT DYNAMICS OF SUBSONIC AND SUPERSONIC PROJECTILES
Q. Zhang¹, Z. Ye¹, S. Wang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
27. Sep 16 15:00 15:30 2.4.3 STORE SEPARATION FROM WEAPON BAYS
M. Tutty, JAIME Enterprises Australia, Australia; G. Akroyd, Akroyd Aeronautics, Australia; A. Cenko¹, A. Piranian¹; ¹AIWS LLC, United States
3.4Wind Tunnel Technology
Chair(s): Manfriani, L.
Track 3
02.2 - Experimental Aerodynamics
27. Sep 16 14:00 14:30 3.4.1 HYPERPARAMETERS OPTIMIZATION FOR ADAPTIVE DESIGN OF EXPERIMENTS APPLIED TO WIND TUNNEL TESTING
H. Jin¹, D. Lee¹, J. Lee¹, J. Ahn¹; ¹Department of Aerospace Engineering, KAIST, South Korea
27. Sep 16 14:30 15:00 3.4.2 DESIGN AND TEST OF THE HIGH AERODYNAMIC PERFORMANCE LOW-NOISE FAN FOR 5.5- BY 4-M ACOUSTIC WIND TUNNEL
X. Qu¹, Y. Yu¹, D. Liao¹, G. Yang¹, Q. Chen¹, G. Tang¹; ¹CARDC, China
4.4Propeller/Wing Aerodynamics
Chair(s): Monk, J.
Track 4
02.4 - Applied Aerodynamics
27. Sep 16 14:00 14:30 4.4.1 LOW REYNOLDS PROPELLER META-MODEL FOR MULTIDICIPLYNARY OPTIMIZATION
V.D. Tavernari¹, F.M. Catalano¹; ¹Aeronautical Engineering Department _EESC-USP, Brazil
27. Sep 16 14:30 15:00 4.4.2 DISTRIBUTED PROPELLERS SLIPSTREAM EFFECTS ON WING AT LOW REYNOLDS NUMBER
K. Wang¹, X.P. Zhu¹, Z. Zhou¹; ¹NWPU University, China
27. Sep 16 15:00 15:30 4.4.3 NUMERICAL SIMULATION OF THE PROPELLER/WING INTERACTIONS AT LOW REYNOLDS NUMBER
H.-B. Wang¹, X.-P. Zhu, UAV Laboratory, Northwestern Polytechnical University, China; Z. Zhou¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
5.4Landing Gear & Taxiing
Chair(s): Mari, C.
Track 5
06 - Systems, Subsystems and Equipment
27. Sep 16 14:00 14:30 5.4.1 EXPERIMENTAL AND SIMULATION STUDY OF THE DYNAMICS OF AN ELECTRO-MECHANICAL LANDING GEAR ACTUATOR
G. Di Rito¹, R. Galatolo¹, F. Schettini¹; ¹Università di Pisa - Dip. Ingegneria Civile ed Industriale, Italy
6.4Structural Design 2 BLADES
Chair(s): Park, J.
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
27. Sep 16 14:00 14:30 6.4.1 MULTIDISCIPLINARY DESIGN CHAIN FOR MODEL ROTOR BLADES
B. van de Kamp¹, S. Kalow¹, J. Riemenschneider¹, R. Bartels¹, H. Mainz¹; ¹German Aerospace Center (DLR), Germany
27. Sep 16 14:30 15:00 6.4.2 NUMERICAL INVESTIGATION OF FAN-BLADE OUT USING MESO-SCALE COMPOSITE MODELING
B. Horton¹, J. Bayandor¹; ¹Virginia Tech, United States
7.4Hybrid / Electric Propulsion
Chair(s): Isikveren, A., Mirzoyan, A.
Track 7
04 - Propulsion
27. Sep 16 14:00 14:30 7.4.1 INTEGRATION OF HYBRID PROPULSION SYSTEM IN A CS23 COMMUTER DESIGN
M. Strack¹, T. Zill¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany
27. Sep 16 14:30 15:00 7.4.2 INVESTIGATION OF CHARACTERISTICS OF THE OIL SYSTEM WITH ELECTRICALLY DRIVEN PUMPS FOR GAS TURBINE ENGINE
Y.M. Shchurovskiy, Central Institute of Aviation Motors (CIAM), Russia
27. Sep 16 15:00 15:30 7.4.3 METHODS FOR IMPROVING THE RELIABILITY OF FUEL SUPPLY SYSTEM OF GAS TURBINE ENGINES WITH USING ELECTRICALLY DRIVEN PUMPS
O.S. Gurevich¹, A.I. Gulienko¹; ¹Central Institute of Aviation Motors (CIAM), Russia
8.4Flight Modeling & Simulation
Chair(s): Doll, C.
Track 8
05.1 - Flight Dynamics and Control (Control & Modelling)
27. Sep 16 14:00 14:30 8.4.1 FLIGHT DYNAMIC STABILITY ANALYSIS OF A FLEXIBLE FLYING WING
L. Wang, China; C. Tang, China
27. Sep 16 14:30 15:00 8.4.2 BIFURCATION ANALYSIS OF A GENERIC PUSHER TYPE TRANSPORT AIRCRAFT CONFIGURATION IN NEAR-STALL FLIGHT
A.K. Khatri¹, V. Kumar¹; ¹CSIR-NAL, India
27. Sep 16 15:00 15:30 8.4.3 HEURISTIC MODEL OF NON-STEADY LONGITUDINAL AERODYNAMIC CHARACTERISTICS AT HIGH ANGLES OF ATTACK
P.V. Kuzmin¹, B.A. Meleshin¹, Y.F. Shelyukhin¹, D.V. Shukhovtsov¹; ¹TsAGI, Russia
9.4UAV Design Configuration 1
Chair(s): Krus, P.
Track 9
05.2 - Flight Dynamics and Control (UAV related)
27. Sep 16 14:00 14:30 9.4.1 OVERVIEW OF THE INVERTED JOINED WING SCALED DEMONSTRATOR PROGRAMME
C. Galinski¹, W. Stalewski¹, M. Lis¹, J. Hajduk, Air Force Institute of Technology, Poland; ¹Institute of Aviation, Poland
27. Sep 16 14:30 15:00 9.4.2 IS TO BE THE MICRODRONE
M. Babiak¹, A. Garstka¹, M. Mazur¹, I. Skawinski¹; ¹Warsaw University of Technology, Poland
27. Sep 16 15:00 15:30 9.4.3 STRATEGIES FOR MANUAL LANDING OF REMOTELY PILOTED AIRPLANES WITH LARGE TIME DELAY
T. Fricke¹, F. Holzapfel¹; ¹Technische Universität München, Germany
10.4Experiments on Basic Flows
Chair(s): Pechloff, A.
Track 10
02.3 - Basic Fluid Dynamics and Flow Control
27. Sep 16 14:00 14:30 10.4.1 INFLUENCE OF SURFACE FRACTAL MICROSTRUCTURE ON THE CHARACTERISTICS OF A TURBULENT BOUNDARY LAYER
M.A. Brutyan¹, V.P. Budaev, NRCKI, Russia; A.V. Wolkov¹; ¹TsAGI, Russia
27. Sep 16 14:30 15:00 10.4.2 GEOMETRIC ROUGHNESS EFFECTS ON THE AERODYNAMIC CHARACTERISTICS OF A SPINNING CYLINDER IN CROSSFLOW
S. Prince¹, J. Holt¹, P. Episkopou¹; ¹Cranfield University, United Kingdom
27. Sep 16 15:00 15:30 10.4.3 STAGGERED THREE-DIMENSIONAL CAVITIES AS A POSSIBLE METHOD FOR SKIN FRICTION DRAG REDUCTION
E.R. Gowree¹, C.J. Atkin¹; ¹City University London, United Kingdom
11.4Environment Friendly Operations
Chair(s): Reichmuth, J.
Track 11
10 - Challenge of the Environment
27. Sep 16 14:00 14:30 11.4.1 CONCEPT OF OPERATIONS OF AN ATC TOOL FOR TRAJECTORY OPTIMISATION
A. Spiteri¹, K. Chircop¹, D. Zammit-Mangion¹, A. Muscat², K. Falzon², J. Degiorgio³, F. Bezzina³; ¹University of Malta, Malta ;²Quaero Ltd., Malta ;³Malta Air Traffic Services Ltd., Malta
27. Sep 16 14:30 15:00 11.4.2 FLEET DEVELOPMENT PLANNING OF AIRLINES: INCORPORATING THE AIRCRAFT OPERATING ECONOMICS FACTOR
O. Oguntona, Munich Aerospace e.V., Germany; A. Cui, Technische Universität München, Germany; K. Ploetner¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
12.4Estimation and Testing
Chair(s): Hwang, I., Kanerva, M.
Track 12
03.1 - Materials issues, Fatigue and Damage Tolerance
27. Sep 16 14:00 14:30 12.4.1 DETERMINATION OF DESIGN ALLOWABLES FOR AIRCRAFT COMPOSITE STRUCTURES
J.Y. Choung¹, J.W. Kim¹, I.H. Hwang¹; ¹Korea Aerospace Research Institute, South Korea
27. Sep 16 14:30 15:00 12.4.2 A STRESS INTENSITY FACTOR SOLUTION INSPIRED BY SOAP BUBBLES FRAMEWORK
R. de Moura Pinho¹, D. Soria¹, L. Dimithe Aboumou¹; ¹Safran Aircraft Engines, France
27. Sep 16 15:00 15:30 12.4.3 ESTIMATION OF TEMPERATURE-DEPENDANT THERMAL CONDUCTIVITY OF MATERIAL WITH GENETIC ALGORITHM
Q. Wei-qi¹, Z. Yu¹; ¹CARDC, China

 Break

1.5Education
Chair(s): Szodruch, J., Imamura, T.
Track1
01 - Aircraft and Systems Integration
27. Sep 16 16:00 16:30 1.5.1 USING INTERNATIONAL COLLABORATIVE AIRCRAFT DESIGN PROJECTS TO ENHANCE UNDERGRADUATE DESIGN EDUCATION: LESSONS LEARNED
P. Raj, Virginia Polytechnic Institute & State University, United States; J. Abulawi, Hochschule für Angewandte Wissenschaften, Germany
27. Sep 16 16:30 17:00 1.5.2 STUDENT DESIGN PROCESSES IN INTERDISCIPLINARY COLLABORATION ACTIVITIES IN AERONAUTICS ENGINEERING EDUCATION
J. Kimura, The University of Tokyo, Japan
27. Sep 16 17:00 17:30 1.5.3 AIRCRAFT DESIGN EDUCATION FOR UNDERGRADUATE AND GRADUATE STUDENTS AT THE UNIVERSITY OF TOKYO
K. Rinoie, The University of Tokyo, Japan
27. Sep 16 17:30 18:00 1.5.4 THE COLLABORATIVE ENGINEER: HOW EDUCATION SHOULD BRING FORTH THE NEW GENERATION OF ENGINEERS
E. Moerland, German Aerospace Center (DLR), Germany; B. Nagel, German Aerospace Centre (DLR), Germany
2.5High AOA and Unsteady Aerodynamics
Chair(s): Stumpf, E.
Track 2
02.1 - Aerodynamics - CFD Methods and Validation
27. Sep 16 16:00 16:30 2.5.1 MODELLING NONLINEAR HIGH-PRECISION UNSTEADY AERODYNAMICS FOR ADVANCED AIRCRAFT AT HIGH ANGLE OF ATTACK
B.-G. Mi¹, H. Zhan¹, M.-H. Yang¹; ¹Northwestern Polytechnical University, China
27. Sep 16 16:30 17:00 2.5.2 EFFECTS OF THE BOUNDARY LAYER TRANSITION ON THE GLOBAL AERODYNAMIC COEFFICIENTS
G.L.O. Halila¹, A.P. Antunes¹, R.G. da Silva², J.L.F. Azevedo²; ¹Embraer S.A., Brazil ;²Instituto de Aeronautica e Espaco, Brazil
27. Sep 16 17:00 17:30 2.5.3 EFFECTS OF SOME NUMERICAL FORMULATION ASPECTS IN HIGH-LIFT CONFIGURATION SIMULATIONS
E.D.V. Bigarella¹, P.A.G. Ciloni¹, L.C. Scalabrin¹; ¹Embraer S.A., Brazil
27. Sep 16 17:30 18:00 2.5.4 CFD OF BLENDED WING BODY UCAV WITH VORTEX GENERATOR
S. Park¹, K. Chang¹, d.-J. Sheen¹; ¹Hanseo University, South Korea
3.5Flow Visualisation 1
Chair(s): Goraj, Z.
Track 3
02.2 - Experimental Aerodynamics
27. Sep 16 16:00 16:30 3.5.1 NON-INTRUSIVE UNSTEADY PSP TECHNIQUE FOR INVESTIGATION OF TRANSONIC BUFFETING
Y. Sugioka¹, K. Nakakita, JAXA, Japan; K. Asai¹; ¹Tohoku Univ., Japan
27. Sep 16 16:30 17:00 3.5.2 UNSTEADY AERODYNAMIC INFORMATION EXTRACTION USING FFT-BASED UNSTEADY PRESSURE-SENSITIVE PAINT MEASUREMENT
K. Nakakita, Japan Aerospace Exploration Agency, Japan
27. Sep 16 17:00 17:30 3.5.3 EXPERIMENTAL STUDY OF GEOMETRIC VARIATIONS EFFECT ON THE FLOW PATTERNS ON A HAMMERHEAD SATELLITE LAUNCH VEHICLE
J.G. Medeiros, Instituto Tecnológico de Aeronáutica, Brazil; A.C. Avelar, Instituto de Aeronautica e Espaço, Brazil; J.B.P. Falcão Filho, Instituto de Aeronáutica e Espaço, Brazil
4.5Special Topics
Chair(s): Consigny, H.
Track 4
02.4 - Applied Aerodynamics
27. Sep 16 16:00 16:30 4.5.1 NUMERICAL SIMULATION OF DROPLET IMPINGEMENT ON A MULTI-ELEMENT HIGH-LIFT AIRFOIL
L. Prince Raj¹, R.S. Myong¹; ¹Gyeongsang National University, South Korea
27. Sep 16 16:30 17:00 4.5.2 STRATEGIES FOR ACHIEVING BACKWARD FLIGHT BY A DRAGONFLY
A.T. Bode-Oke¹, S. Zeyghami, Lehigh University, United States; H. Dong¹; ¹University of Virginia, United States
5.5Modeling and Tests of Systems & Subsystems 1
Chair(s): Stoufflet, B.
Track 5
06 - Systems, Subsystems and Equipment
27. Sep 16 16:00 16:30 5.5.1 SURROGATE MODELING TECHNIQUE FOR THE CONCEPTUAL AND PRELIMINARY DESIGN OF EMBEDDED ACTUATION SYSTEMS AND COMPONENTS
F. Sanchez, Institut Clément Ader/Paul Sabatier University, France; S. Delbecq, Institut Clément Ader/Safran Electronics & Defense, France
27. Sep 16 16:30 17:00 5.5.2 SELECTION OF AN UAV CONFIGURATION LAYOUT FOR OPTIMISATION OF TELEDETECTION MISSION USING HYPERSPECTRAL SENSORS
R. Fusaro¹, Z. Goraj, Warsaw University of Technology, Poland; N. Viola¹; ¹Politecnico di Torino, Italy
27. Sep 16 17:00 17:30 5.5.3 STATISTICAL MODELING OF AIRCRAFT ENGINE FUEL FLOW RATE
Y.S. Chati¹, H. Balakrishnan¹; ¹Massachusetts Institute of Technology, United States
27. Sep 16 17:30 18:00 5.5.4 METHODS FOR AUTOMATING MODEL VALIDATION: STEADY-STATE IDENTIFICATION APPLIED ON GRIPEN FIGHTER ENVIRONMENTAL CONTROL SYSTEM MEASUREMENTS
R. Hällqvist¹, M. Eek¹, R. Braun², P. Krus²; ¹Saab Aeronautics, Sweden ;²Linköping University, Sweden
6.5Structural Design 3
Chair(s): Bisagni, C., Kim, I.
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
27. Sep 16 16:00 16:30 6.5.1 GENERATIVE DESIGN: ADVANCED DESIGN OPTIMIZATION PROCESSES FOR AERONAUTICAL APPLICATIONS
S. Bagassi¹, F. Lucchi¹, F. De Crescenzio¹, F. Persiani¹; ¹University of Bologna, Italy
27. Sep 16 16:30 17:00 6.5.2 DESIGNING OF AIRFRAMES HAVING MINIMUM MASS UNDER SEVERAL LOADINGS (NOT ONLY FULLY STRESSED)
A.I. Danilin, Samara State Aerospace University, Russia
27. Sep 16 17:00 17:30 6.5.3 APPLICATIONS OF DISPLACEMENT TRANSFER FUNCTIONS TO DEFORMED SHAPE PREDICTIONS OF THE G-III SWEPT-WING STRUCTURE
S.-F. Lung, Jacobs, United States; W.L. Ko, NASA, United States
27. Sep 16 17:30 18:00 6.5.4 FAIRING OPTIMIZATION DESIGN OF WING STRUCTURE
R. Zhang, Chinese Aeronautical Establishment, China; D.-G. Cui, Aviation of China, China; G. Song, Beihang University, China
7.5Turbines
Chair(s): Melkert, J.
Track 7
04 - Propulsion
27. Sep 16 16:00 16:30 7.5.1 EFFECT OF REYNOLDS NUMBER, OPERATING MODE, TURBULENCE PARAMETERS ON PROFILE AND SECONDARY LOSSES OF LPT
A.D. Nepomnyashchiy¹, S.V. Suntsov ¹, S.Y. Danilkin¹, V.P. Maslov¹; ¹Central Institute of Aviation Motors (CIAM), Russia
8.5Conceptual Design and Evaluation
Chair(s): Kanazaki, M.
Track 8
01 - Aircraft and Systems Integration
27. Sep 16 16:00 16:30 8.5.1 STOCHASTIC TRANSONIC AERODYNAMICS ANALYSIS
X. Wu, China; W. Zhang, China
27. Sep 16 16:30 17:00 8.5.2 MULTIDISCIPLINARY DESIGN OPTIMIZATION OF STRATOSPHERIC AIRSHIP
M.I. Alam, Indian Institute of Technology Bombay, India
27. Sep 16 17:00 17:30 8.5.3 REDUCED ORDER MODELING OF AVIATION ENVIRONMENTAL DESIGN TOOL WITH PROPER ORTHOGONAL DECOMPOSITION AND KRIGING
S. Kim¹, K. Lee¹; ¹Pusan National University, South Korea
9.5Advanced Materials
Chair(s): Ikeda, T., Blom, A.
Track 9
03.1 - Materials issues, Fatigue and Damage Tolerance
27. Sep 16 15:30 16:00 9.5.1 PLASTIC DEFORMATION OF POWDER METALLURGY TUNGSTEN ALLOY FOILS FOR SATELLITE ENCLOSURES
M. Kanerva¹, E. Sarlin, Tampere University of Technology, Department of Material Science, Finland; A. Hållbro, Plansee SE, Sweden; J. Jokinen¹; ¹Aalto University, Department of Mechanical Engineering, Finland
27. Sep 16 16:00 16:30 9.5.2 MODERN MATERIALS IN AEROSPACE INDUSTRY - MAGNESIUM ALLOY CONTROL SYSTEM LEVER OF THE UNMANNED ILX - 27 HELICOPTER
M. Wojtas¹, A. Sobieszek¹, L. Czajkowski¹, R. Zurawski¹; ¹Institute of Aviation, Poland
10.5Transition Forcing and Control
Chair(s): Gowree, E., Breitsamter, C.
Track 10
02.3 - Basic Fluid Dynamics and Flow Control
27. Sep 16 16:00 16:30 10.5.1 EXPERIMENTAL STUDY OF AEROFOIL-WAKE INDUCED TRANSITION IN BOUNDARY LAYERS
D. Veerasamy, United Kingdom
27. Sep 16 16:30 17:00 10.5.2 DISTURBANCES IN AN ACCELERATED BOUNDARY LAYER UNDER INFLUENCE OF MODERATE FREE-STREAM TURBULENCE
D.S. Sboev, TsAGI, Russia
27. Sep 16 17:00 17:30 10.5.3 EFFECT OF A 3D INDENTATION ON BOUNDARY LAYER INSTABILITY
H. Xu¹, S. Mughal¹, E.R. Gowree, Centre of Aeronautics,City University London, United Kingdom; S.-J. Sherwin, Department of Aeronautics, Imperial College London, United Kingdom; ¹Department of Mathematics,Imperial College London, United Kingdom
11.5Noise & Emission
Chair(s): Kügler, D.
Track 11
10 - Challenge of the Environment
27. Sep 16 16:00 16:30 11.5.1 ACOUSTICAL COMPARISON OF CONVENTIONAL TAXIING AND DISPATCH TOWING - TAXIBOT´S CONTRIBUTION TO GROUND NOISE ABATEMENT
K. Hein¹, S. Baumann¹; ¹TU Darmstadt, Germany
27. Sep 16 16:30 17:00 11.5.2 QUANTITATIVE EMISSIONS OF NOX, CO AND CO2 DURING AIRCRAFT OPERATIONS
P. Glowacki¹, M. Kawalec¹; ¹Institute of Aviation, Poland
12.5Boundary Layer Asymptotic Analysis
Chair(s): Atkin, C.
Track 12
02.3 - Basic Fluid Dynamics and Flow Control
27. Sep 16 16:00 16:30 12.5.1 EXTENDED LOCAL SCATTERING THEORY AND THE ROLE OF A SCATTER ON BOUNDARY-LAYER INSTABILITY AND ACOUSTIC RADIATION
M. Dong¹, X. Wu¹; ¹Imperial College London, United Kingdom

Wednesday, 28. Sep 2016


7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
0.9GENERAL LECTURE 3
Chair: Gunnar Holmberg ICAS treasurer
28. Sep 16 08:00 09:00 Complex System Architecture
Ed Crawley

 Break

1.6Design Method 2
Chair(s): Prince, S., Ogilvie, F.
Track1
01 - Aircraft and Systems Integration
28. Sep 16 09:30 10:00 1.6.1 COMMERCIAL DERIVATIVE AIRCRAFT AND TURBINE ENGINE
I. Berlowitz, Israel Aerospace Industries, Israel
28. Sep 16 10:00 10:30 1.6.2 ENHANCING THE EXPLORATION OF AIRCRAFT CHANGEABILITY DURING CONCEPTUAL DESIGN
A.S.J. van Heerden¹, M.D. Guenov¹, A. Molina-Cristobal¹, A. Riaz¹; ¹Cranfield University, United Kingdom
28. Sep 16 10:30 11:00 1.6.3 ROTORCRAFT SYSTEMS MODELLING FOR TWIN-ENGINE HEAVY HELICOPTER
F. Hashim¹, C.P. Lawson¹, D.M. Judt¹; ¹Cranfield University, United Kingdom
28. Sep 16 11:00 11:30 1.6.4 IDENTIFYING THE BEST DESIGN FOR UNCERTAIN MARKETS
A.A. Desai¹, P. Hollingsworth¹, P. Chinchapatnam, Rolls-Royce plc, United Kingdom; ¹University of Manchester, United Kingdom
28. Sep 16 11:30 12:00 1.6.5 DETAILED AERO-STRUCTURAL DESIGN OF WINGLET FOR BUSINESS JET
N.R. El Haddad¹, L. Gonzalez¹; ¹EMBRY RIDDLE AERONAUTICAL UNIVERSITY, United States
2.6Current Developments in CFD 1
Chair(s): Pedreiro, L.
Track 2
02.1 - Aerodynamics - CFD Methods and Validation
28. Sep 16 09:30 10:00 2.6.1 DEVELOPMENT OF HIGH-ORDER AND HIGH-RESOLUTION SCHEMES FOR EFFICIENT SHOCK CAPTURING IN HIGH-SPEED FLOWS
M.H. Ahn¹, D.J. Lee¹; ¹Korea Advanced Institute of Science and Technolgy, South Korea
28. Sep 16 10:00 10:30 2.6.2 COMPUTATIONAL EFFICIENCY AND QUALITY OF DIFFERENT VERSIONS OF DISCONTINUOUS GALERKIN METHOD FOR LES/DES APPLICATIONS
I. Bosnyakov¹, A.I. Troshin¹, V.V. Vlasenko¹, A.V. Wolkov¹; ¹TsAGI, Russia
28. Sep 16 10:30 11:00 2.6.3 EXTENDED VALIDATION OF A TRANSONIC LATTICEBOLTZMANN METHOD ON THE EXAMPLE OF THE NASA COMMON RESEARCH MODEL
B. Koenig¹, A.F.P. Ribeiro¹, E. Fares¹, R. Zhang², P. Gopalakrishnan², Y. Li²; ¹Exa GmbH, Germany ;²Exa Corp., United States
28. Sep 16 11:00 11:30 2.6.4 EFFICIENT MULTI-RESOLUTION ANALYSIS FOR IMPLICIT TEMPORAL INTEGRATION
S. Chae¹, H. Kang, Dongyang Mirae University, South Korea; S. Oh, Pusan National University, South Korea; K. Yee¹; ¹Seoul National University, South Korea
28. Sep 16 11:30 12:00 2.6.5 INFLUENCE OF THE RHOMBOID ZONE ON AEROELASTIC EXPERIMENTS OF SUPERSONIC AIRCRAFT
Y.-G. Bai¹, W. Qian¹; ¹Dalian University of Technology, China
3.6High Lift/Multielement Aerodynamics
Chair(s): Consigny, H.
Track 3
02.4 - Applied Aerodynamics
28. Sep 16 09:30 10:00 3.6.1 FLOW CONTROL ON HELICOPTER-ROTOR BLADES VIA ACTIVE GURNEY FLAP
W. Stalewski, INSTITUTE of AVIATION, Poland
28. Sep 16 10:00 10:30 3.6.2 STUDY ON THE SYSTEM INTEGRATION FOR MULTI-ELEMENT AIRFOIL AERODYNAMIC ANALYSIS
D. Nam¹, J. Lee¹, B. KIim¹; ¹Chungnam National University, South Korea
28. Sep 16 10:30 11:00 3.6.3 THE INFLUENCE OF A LOCAL CHANGE IN WING DIHEDRAL ON THE LOW SPEED FLOW CHARACTERISTICS OF RECTANGULAR PLANFORM WINGS
K.P. Garry¹, J.C. Holt¹, G. Tanguy¹, S.A. Prince¹; ¹Cranfield University, United Kingdom
28. Sep 16 11:00 11:30 3.6.4 IMPROVED DESIGN OF A HIGH LIFT SYSTEM FOR GENERAL AVIATION AIRCRAFT
D. Florjancic¹, D. Steenhuizen¹, L.L.M. Veldhuis¹; ¹TU Delft, Netherlands
28. Sep 16 11:30 12:00 3.6.5 BROADBAND TRAILING-EDGE NOISE: A STATUS REPORT ON CURRENT PREDICTION CAPABILITIES
M. Herr, German Aerospace Center (DLR), Germany
4.6Design Optimization 1
Chair(s): Philpott, D.
Track 4
02.4 - Applied Aerodynamics
28. Sep 16 09:30 10:00 4.6.1 AERODYNAMIC SHAPES DESIGN ON THE BASE OF DIRECT NEWTON TYPE OPTIMIZATION METHOD
A.V. Grachev¹, A.N. Kraiko, CIAM, Russia; S.A. Takovitskii¹; ¹TsAGI, Russia
28. Sep 16 10:00 10:30 4.6.2 CFD-BASED AERODYNAMIC SHAPE OPTIMIZATION OF A MANNED RE-ENTRY VEHICLE
M.M. Entezari, Aerospace Research Institute, Iran; M. Mohammadi-Amin, Aerospace Research Institue, Iran
28. Sep 16 10:30 11:00 4.6.3 AERODYNAMIC SHAPE OPTIMIZATION WITH A NEW PARALLEL EVOLUTIONARY ALGORITHM AND NUMERICAL FLOW MODELLING
A. Jahangirian¹, M. Ebrahimi¹; ¹Amirkabir University of Technology, Iran
5.6Operations & Sustainment 2
Chair(s): Holmes, D., Anderson, K.
Track 5
11 - Operations and Sustainment
28. Sep 16 09:30 10:00 5.6.1 RESEARCH DEVELOPMENTS IN NONDESTRUCTIVE EVALUATION AND STRUCTURAL HEALTH MONITORING FOR THE SUSTAINMENT OF COMPOSITE AEROSPACE STRUCTURES AT NASA
K.E. Cramer, NASA, United States
28. Sep 16 10:00 10:30 5.6.2 IN-FLIGHT VIBRATION-BASED STRUCTURAL HEALTH MONITORING OF AIRCRAFT WINGS
E. Neu¹, F. Janser¹, A.A. Khatibi², A.C. Orifici²; ¹FH Aachen UAS, Germany ;²RMIT University, Australia
28. Sep 16 10:30 11:00 5.6.3 QUALIFICATION OF KAI KUH-1M ON BOARD ROKN SHIPS USING THE DUTCH APPROACH
J. van der Vorst¹, P.J.A. Booij¹, J.F. Hakkaart¹, T.I. Lee, KAI, South Korea; ¹NLR, Netherlands
28. Sep 16 11:00 11:30 5.6.4 3D IMAGING OF GEOMETRICAL STRUCTURE AND DEFECT LOCATION OF INNER CAVITY IN AVIATION DEVICES BY POSITRON INJECTION
H. Xiao, China; M. Zhao, China; M. Yao, China; J. Liu, China; H. Chen, China; M. Li, China; M. Du, China
6.6Aeroelasticity 1
Chair(s): Amiryants, G.
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
28. Sep 16 09:30 10:00 6.6.1 THE ACTIVE AEROELASTICITY CONCEPT - THE MAIN STAGES AND PROSPECTS OF DEVELOPMENT
G.A. Amiryants, Russia; A.V. Grigorev, Russia; Y.A. Nayko, Russia; S.E. Paryshev, Russia
28. Sep 16 10:00 10:30 6.6.2 DESIGN, MANUFACTURE AND FREQUENCY EXPERIMENT OF A NOVEL FLUTTER MODEL FOR AGARD WING 445.6 WITH STRUCTURE-SIMILARITY
W. Qian¹, Y.-G. Bai¹, D. Wang, AVIC Aerodynamics Research Institute, China; ¹Dalian University of Technology, China
28. Sep 16 10:30 11:00 6.6.3 FLUID-STRUCTURE INTERACTION ANALYSIS REGARDING THE INFLUENCE OF STRUCTURAL BOUNDARY CONDITION ON A FLAPPING WING
H. Cho¹, N. Lee², S.J. Shin¹, S. Lee², S.Y. Kim, Agency for Defense Development, South Korea; ¹Seoul National Univ., South Korea ;²Inha Univ., South Korea
28. Sep 16 11:00 11:30 6.6.4 THE INFLUENCE OF MORPHING PROCESS ON THE AEROELASTIC CHARACTERISTICS OF A FOLDING WING
W. Hu¹, Z.C. Yang¹, Y.S. Gu¹; ¹Northwestern Polytechnical University, China
28. Sep 16 11:30 12:00 6.6.5 UNCERTAINTY QUANTIFICATION AND GLOBAL SENSITIVITY ANALYSIS FOR HYPERSONIC AEROTHERMOELASTIC ANALYSIS
K. Ye¹, Z.Y. Ye¹, Z.H. Chen¹, Z. Qu¹; ¹Northwestern Polytechnical University, China
7.6Inlet, Fan and Compressors
Chair(s): Pankov, S.
Track 7
04 - Propulsion
28. Sep 16 09:30 10:00 7.6.1 STUDY ON EFFICIENT FULL ANNULUS URANS COMPUTATIONS OF AN INTAKE COMPRESSOR CONFIGURATION
T. Kächele¹, T. Schneider, MTU Aero Engines AG, Germany; R. Niehuis¹; ¹Universität der Bundeswehr, Germany
28. Sep 16 10:00 10:30 7.6.2 DESIGN AND DEVELOPMENT OF A MILITARY ENGINE INLET RESEARCH DUCT
R.P.M. Rademakers¹, J.P. Haug¹, R. Niehuis¹, M. Stoeßel, Wehrtechnische Dienststelle für Luftfahrzeuge u Luftfahrtgeräte, Germany; ¹Institute of Jet Propulsion (UniBwM), Germany
28. Sep 16 10:30 11:00 7.6.3 ANALYSES OF AIRFLOW AROUND DUCTED FAN PROPULSION SYSTEM IN PUSHER CONFIGURATION USING PIV METHOD
P. Ruchala¹, K. Bogdanski, Politechnika Warszawska, Poland; W. Stryczniewicz¹; ¹Instytut Lotnictwa, Poland
28. Sep 16 11:00 11:30 7.6.4 THE INVESTIGATION OF TIP CLEARANCE EFFECTS IN DUCTED ROTOR AERODYNAMIC CHARACTERISTICS USED IN UNMANNED AERIAL VEHICLES
X. Li¹, Z. Guo¹, Z. Hou¹; ¹National University of Defense Technology, China
28. Sep 16 11:30 12:00 7.6.5 CHARACTERIZATION OF DISTORTED FLUID FLOW ALONG ADVANCED HIGH-BYPASS PROPULSION SYSTEM
Y.K. Song¹, J. Bayandor¹; ¹Virginia Tech, United States
8.6UAV Collaborative Operations
Chair(s): Belo, E.
Track 8
05.2 - Flight Dynamics and Control (UAV related)
28. Sep 16 09:30 10:00 8.6.1 SAMPLING-BASED MOTION PLANNING FOR COOPERATIVE AERIAL MANIPULATION
H.I. Kim¹, H.B. Lee¹, H.J. Kim¹; ¹Seoul National Univ., South Korea
28. Sep 16 10:00 10:30 8.6.2 A NOVEL FLIGHT CONTORL ALGORITHM FOR MULTICOPTERS
O. Tekinalp, Middle East Tecnical University, Turkey; S. Kumbasar, Middle East Technical University, Turkey
28. Sep 16 10:30 11:00 8.6.3 DESIGN THE GUIDANCE LAW FOR FORMATION FLIGHT OF MULTIPLE UAVS
H. Shin¹, H. Kim¹, J. Lee¹, D.H. Shim¹; ¹Korea Advance Institute of Science and Technology, South Korea
28. Sep 16 11:00 11:30 8.6.4 NON-COOPERATIVE GROUND VEHICLE TRACKING AND INTERCEPTION BY MULTI-RPA COLLABORATION
Y. Watanabe¹, A. Manecy¹, A. Amiez¹, C. Lesire¹, C. Grand¹; ¹ONERA, France
9.6UAV Nav & Operations
Chair(s): Vian, J., Esteban Campillo, D.
Track 9
05.2 - Flight Dynamics and Control (UAV related)
28. Sep 16 09:30 10:00 9.6.1 APPROXIMATE THREE-DIMENSIONAL PATH GENERATION FOR UAV PATH-FOLLOWING
N. Cho, South Korea; Y. Kim, South Korea
28. Sep 16 10:00 10:30 9.6.2 DEVELOPMENT OF PEST\\\'S BIOLOGICAL CONTROL TOOL USING VTOL UAV SYSTEMS
R.K. Rangel, BRVANT / BRV UAV& Flight Systems, Brazil
28. Sep 16 10:30 11:00 9.6.3 FLIGHT TESTS OF THE VISION-BASED TARGET SENSING AND APPROACHING
S. Cho¹, Y. Jung, Korea Aerospace Research Institute, South Korea; D.H. Shim¹; ¹Korea Advanced Institute of Science and Technology, South Korea
28. Sep 16 11:00 11:30 9.6.4 OPTICAL FLOW ON A FLAPPING WING-MICRO AIR VEHICLE TO AVOID COLLISIONS AND STEER
S.W. Ryu¹, J.G. Lee¹, H.J. Kim¹; ¹Seoul National University, South Korea
28. Sep 16 11:30 12:00 9.6.5 REAL-TIME GENERATION OF WAYPOINTS ENHANCING UAV SURVIVABILITY
S.-H. Park, LIG Nex1., South Korea; K.-K. Park¹, S.-S. Park¹, C.-K. Ryoo¹; ¹Inha Univ., South Korea
10.6Hybrid-Electric and Distributed Propulsion Aircraft 1
Chair(s): Isikveren, A.
Track 10
01 - Aircraft and Systems Integration
28. Sep 16 09:30 10:00 10.6.1 HYBRID-ELECTRIC TRANSPORT AIRCRAFT: OPPORTUNITIES AND PERSPECTIVES
A.T. Isikveren¹, P.-A. Lambert¹, J. Stuhlberger, Airbus Group, Germany; M.K. Bradley, Boeing Commercial Airplanes, United States; J.H. Stromberger, General Electric, Germany; J. Whurr, Rolls Royce, United Kingdom; F. Anton, Siemens, Germany; ¹SAFRAN S.A., France
28. Sep 16 10:00 10:30 10.6.2 THE E-FAN ALL ELECTRICAL AIRCRAFT DEMONSTRATOR AND ITS INDUSTRIALIZATION
E. Joubert¹, D. Chapuis¹, D. Esteyne¹, J.-C. Lambert¹, O. Siri¹, D. Müller-Wiesner¹; ¹Airbus, France
28. Sep 16 10:30 11:00 10.6.3 HYBRID TURBO-ELECTRIC DISTRIBUTED PROPULSION APPLIED TO SHORT RANGE AIRCRAFT
P. Laskaridis, Cranfield University, United Kingdom
28. Sep 16 11:00 11:30 10.6.4 THE D8 AIRCRAFT CONCEPT AND ITS BOUNDARY LAYER INGESTION BENEFIT
A. Uranga, University of Southern California, United States
28. Sep 16 11:30 12:00 10.6.5 ELECTRIC PROPULSION FOR AIRCRAFT
O. Otto, Siemens AG, Germany
11.6Flow Management
Chair(s): Itoh, E.
Track 11
08 - Air Transport System Efficiency
28. Sep 16 09:30 10:00 11.6.1 A STUDY ON SAFETY ASSURANCE FOR INCREASINGLY AUTONOMOUS TRAFFIC FLOW MANAGEMENT SYSTEM
Y. Wu, University of Missouri St. Louis D of Maths and Computer Science, United States; T.A. Lauderdale, NASA Ames Research Center / Aviation Systems Division, United States; H. Chen, Johnson C. Smith University Computer Science & Engineering Dept., United States
28. Sep 16 10:00 10:30 11.6.2 MODELLING, GENERATING AND EVALUATING SECTOR CONFIGURATION PLANS - METHODOLOGY REPORT OF THE SESAR VP-755 EXERCISE
T. Dubot¹, J. Bedouet¹, S. Degrémont, DSNA, France; ¹ONERA, France
28. Sep 16 10:30 11:00 11.6.3 TOWARDS A MORE HARMONISED AND WIDER USE OF SHORT-TERM ATFCM MEASURES (STAM)
P. Choroba¹, L. van der Hoorn¹; ¹Eurocontrol, France
28. Sep 16 11:00 11:30 11.6.4 VISUALIZATION OF AIRSPACE COMPLEXITY BASED ON AIR TRAFFIC CONTROL DIFFICULTY
H. Hirabayashi¹, M. Brown¹, S. Nagaoka¹; ¹Electronic Navigation Research Institute, Japan
28. Sep 16 11:30 12:00 11.6.5 DEVELOPMENT OF AN ADVANCED ATCO WORKSTATION
D. Rohacs¹, I. Jankovics¹, J. Rohacs¹; ¹Budapest University of Technology and Economics, Hungary
12.6Safety & Operations of Unmanned Aircraft Systems
Chair(s): Lief, A.
Track 12
09 - Safety and Security
28. Sep 16 09:30 10:00 12.6.1 FORMAL VERIFICATION OF AUTOPILOTS IN UMANNED AIRCRAFT SYSTEMS
B.J. Yang¹, P. Dutta¹, I. Hwang, Purdue University, United States; ¹Optimal Synthesis Inc., United States
28. Sep 16 10:00 10:30 12.6.2 DETECT AND AVOID FOR REMOTELY PILOTED AIRCRAFT IN AIR TRAFFIC CONTROL SIMULATIONS
J. Alfredson, Saab/LiU, Sweden; P. Hagström, Saab, Sweden
28. Sep 16 10:30 11:00 12.6.3 THE DRONE AVIATION NAVIGATION SYSTEMS
M. Tanaka, Nagoya Univ, Japan; T. Okubo, iisec, Japan; S. Yamada¹, G. Idei¹, M. Takase¹, R. Hosomi¹; ¹Kyoto Institute of Technology, Japan
28. Sep 16 11:00 11:30 12.6.4 VERTICAL POSITION ERROR BOUNDING FOR INTEGRATED GPS/BAROMETER SENSORS TO SUPPORT UNMANNED AERIAL VEHICLE (UAV)
J. Lee¹, E. Hyeon¹, M. Kim¹, J. Lee¹; ¹Korea Advanced Institute of Science and Technology, South Korea
28. Sep 16 11:30 12:00 12.6.5 SECURE ESTIMATION FOR UNMANNED AERIAL VEHICLES AGAINST ADVERSARIAL ATTACKS
Q. Hu¹, Y.H. Chang, Oregon Health and Science University, United States; C.J. Tomlin¹; ¹University of California Berkeley, United States

 Lunch

0.10GENERAL LECTURE 4
Chair: Detlef Müller-Wiesner Honorary fellow
28. Sep 16 13:00 13:45 Experience and Lessons of a full composite passenger aircraft development
Chantal Fualdes

1.7Design for Uncertainty
Chair(s): Imamura, T.
Track1
01 - Aircraft and Systems Integration
28. Sep 16 14:00 14:30 1.7.1 LINKING TECHNOLOGY READINESS TO UNCERTAINTY REDUCTION
K.G. Schwartz¹, D. Mavris¹; ¹Georgia Institute of Technology, United States
28. Sep 16 14:30 15:00 1.7.2 EXPLORING PROPAGATED UNCERTAINTIES IN A MULTI-DISCIPLINARY AIRCRAFT DESIGN FRAMEWORK
T. Pfeiffer¹, E. Moerland¹, J. Gibbs¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany
28. Sep 16 15:00 15:30 1.7.3 UNCERTAINTY QUANTIFICATION OF AIRFOIL DESIGN FOR ADVANCED PROPELLER MODELS
H.D. Schwartz¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States
2.7CFD for Wind Tunnel Effects
Chair(s): Avelar, A.C.
Track 2
02.1 - Aerodynamics - CFD Methods and Validation
28. Sep 16 14:00 14:30 2.7.1 EXPERIENCE IN AERODYNAMICAL TESTS AND CFD SIMULATIONS OF OVERSIZED WING DEMONSTRATOR IN LARGE LOW-SPEED WIND TUNNEL
G.M. Carossa, LEONARDO S.p A., Italy; K. Anisimov¹, A. Chevagin¹, R. Efimov¹, I. Kursakov¹, A. Lysenkov¹, V. Malenko¹, A. Saprykin¹; ¹TsAGI, Russia
28. Sep 16 14:30 15:00 2.7.2 STUDY OF MODEL DEFORMATION AND STING INTERFERENCE TO THE AERODYNAMIC ESTIMATIONS OF THE CAE-AVM MODEL
M. Zhong¹, G.L. Wang¹, J. Hua¹; ¹Chinese Aeronautical Establishment, China
3.7Experimental
Chair(s): Ricci, S., Han, J.
Track 3
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
28. Sep 16 14:00 14:30 3.7.1 DEFORMATION MEASUREMENT IN THE WIND TUNNEL FOR AN UAV LEADING EDGE WITH A MORPHING MECHANISM
M. Radestock¹, J. Riemenschneider¹, H.P. Monner¹, O. Huxdorf¹, N.P.M. Werter², R. De Breuker²; ¹German Aerospace Center, Germany ;²Delft University of Technology, Netherlands
28. Sep 16 14:30 15:00 3.7.2 SEMI-A VIBRATION SUPPRESSION OF AIRCRAFT PANEL USING PIEZOELECTRIC ACTUATOR WITH SYNCHRONIZED SWITCH DAMPING TECHNIQUE
K. Li¹, L. Zhang¹, K. Pan¹, W. Huang¹; ¹Aircraft strength research institute of China, China
28. Sep 16 15:00 15:30 3.7.3 DESIGN, MANUFACTURING AND VALIDATION OF A GUST GENERATOR FOR WIND TUNNEL TEST OF A LARGE SCALE AEROELASTIC MODEL
F. Fonte¹, L. Riccobene¹, S. Ricci¹, S. Adden², M. Martegani²; ¹Politecnico di Milano, Italy ;²IBK Technologie, Germany
4.7MAV-related Aerodynamics
Chair(s): Egorov, I.
Track 4
02.4 - Applied Aerodynamics
28. Sep 16 13:30 14:00 4.7.1 AN EXPERIMENTAL STUDY OF MICRO-ELECTROMECHANICAL FLYING INSECT FLAPPING WINGS AERODYNAMIC PERFORMANCE
P. Czekalowski, Air Force Institute of Technology, Poland; K.-S. Sibilski, Institute of Aviation, Poland; A. Zyluk, Air Force Academy, Poland
28. Sep 16 14:00 14:30 4.7.2 THE PROPULSIVE EFFICIENCY OF FLEXIBLE FLAPPING-WING
W. Yang¹, B. Song¹, D. Xue¹; ¹Northwestern Polytechnical University, China
5.7Operations & Sustainment 3
Chair(s): Cramer, E., Anderson, K.
Track 5
11 - Operations and Sustainment
28. Sep 16 14:00 14:30 5.7.1 RESEARCH ADVANCES ON AIRCRAFT STRUCTURAL INTEGRITY AND SUSTAINMENT AT NRC
M. Liao¹, M. Yanishevsky¹, P. Patnaik¹; ¹Aerospace, National Research Council Canada, Canada
28. Sep 16 14:30 15:00 5.7.2 DESIGN AND PRELIMINARY EVALUATION OF AN INTEGRATED AIRCRAFT OPERATION SYSTEM FOR DISASTER RELIEF
A. Andreeva-Mori¹, K. Kobayashi¹, M. Shindo¹, Y. Okuno¹; ¹Japan Aerospace Exploration Agency, Japan
28. Sep 16 15:00 15:30 5.7.3 BOARDING PROCESS ASSESSMENT OF NOVEL AIRCRAFT CABIN CONCEPTS
M. Schmidt, Munich Aerospace e.V., Germany; M. Engelmann¹, R. Rothfeld¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
6.7Impact
Chair(s): Bisagni, C.
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
28. Sep 16 14:00 14:30 6.7.1 FRACTURE BEHAVIOR OF RIVETED LAP JOINTS DUE TO PROJECTILE IMPACTS
T. Matsuda¹, K. Mizutani¹, S. Enomoto¹, M. Nishida², T. Moroe², K. Yamada²; ¹CHURYO ENGINEERING CO., LTD., Japan ;²Nagoya Institute of Technology, Japan
28. Sep 16 14:30 15:00 6.7.2 MODELING AND ANALYSIS METHOD ON CRASHWORTHINESS OF CIVILIAN AIRCRAFT FUSELAGE STRUCTURES
H. Huang, China; M. Zhao, China; W. Wang, China
28. Sep 16 15:00 15:30 6.7.3 AIRFRAME STRUCTURAL SURVIVABILITY STUDY THROUGH HYDRODYNAMIC RAM OF WELDED METALLIC WATER TANKS
J. Kim¹, C. Kim, Korea Advanced Institute of Science and Technology, South Korea; S. Jun¹; ¹Agency for Defense Development, South Korea
7.7Propeller
Chair(s): Remy, S., Startsev, A.
Track 7
04 - Propulsion
28. Sep 16 14:00 14:30 7.7.1 ANALYSIS OF SWIRL RECOVERY VANES FOR INCREASED PROPULSIVE EFFICIENCY IN TRACTOR PROPELLER AIRCRAFT
L. Veldhuis¹, T. Stokkermans¹, T. Sinnige¹, G. Eitelberg, TU Delft / DNW, Netherlands; ¹TU Delft, Netherlands
28. Sep 16 14:30 15:00 7.7.2 MULTI-OBJECTIVE OPTIMAL DESIGN OF THE PROPELLER FOR HIGH ALTITUDE AIRSHIPS BASED ON HIGH EFFICIENCY AND LIGHT WEIGHT
J. Jiao¹, Y.-G. Zhang¹, B.-F. Song¹; ¹Northwestern Polytechnical University, China
28. Sep 16 15:00 15:30 7.7.3 SMALL HEIGHT DUCT DESIGN FOR MULTICOPTER FAN
K. Stremousov¹, M. Arkhipov¹, S. Serokhvostov¹; ¹Moscow Institute of Physics and Technology, Russia
8.7Flight Testing
Chair(s): Naruoka, M., Esteban-Campillo, D.
Track 8
05.1 - Flight Dynamics and Control (Control & Modelling)
28. Sep 16 13:30 14:00 8.7.1 WIND TUNNEL THREE-DEGREE-OF-FREEDOM DYNAMIC RIG FOR CONTROL VALIDATION
D.I. Ignatyev ¹, M.E. Sidoryuk¹, K.A. Kolinko¹, A.N. Khrabrov¹; ¹Central Aerohydrodynamic Institute named after N.E. Zhukovsky, Russia
28. Sep 16 14:00 14:30 8.7.2 WIND TUNNEL FREE-FLIGHT TEST FOR FLIGHT DYNAMICS AND CONTROL SYSTEM EXPERIMENTS
F. Cen¹, Q. Li¹, B.-W. Nie², Z.-T. Liu², H.-S. Sun²; ¹Tsinghua University, China ;²China Aerodynamics Research and Development Center, China
9.7UAV Design Configuration 2
Chair(s): Kim, S.
Track 9
05.2 - Flight Dynamics and Control (UAV related)
28. Sep 16 14:00 14:30 9.7.1 DYNAMIC MODELING AND STABILITY ANALYSIS OF A HIGH ALTITUDE AIRSHIP
R. Hun¹, N.K. Sinha¹, D. Chakraborti, ADRDE, India; P. Balasubramanian, RIC, India; ¹Indian Institute of Technology,Madras, India
28. Sep 16 14:30 15:00 9.7.2 PERCH LANDING ASSISTED BY THRUSTER (PLAT): SIX D.O.F. TRAJECTORY OPTIMIZATION
S.Y. Han¹, B.Y. Lee¹, J.M. Ahn¹, M.J. Tahk¹; ¹KAIST, South Korea
28. Sep 16 15:00 15:30 9.7.3 ADAPTIVE SLIDING MODE CONTROLLER DESIGN FOR RECONFIGURATION OF ORGANIC FLIGHT ARRAY
J. Jeong¹, S. Kim¹, J. Suk¹; ¹Chungnam National University, South Korea
10.7Hypersonic/Transitional Boundary Layers
Chair(s): Lipatov, I., Prince, S.
Track 10
02.3 - Basic Fluid Dynamics and Flow Control
28. Sep 16 14:00 14:30 10.7.1 DIRECT NUMERICAL SIMULATION OF DISTURBANCES IN A THREE-DIMENSIONAL HYPERSONIC NEAR-WALL FLOW OVER FLAT PLATE AND COMPRESSION CORNER
A.V. Novikov¹, I.V. Egorov¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
28. Sep 16 14:30 15:00 10.7.2 STUDY OF THE UNSTEADY STRUCTURES EVOLUTION IN SHOCK WAVE / BOUNDARY LAYER INTERACTION FOR VARIOUS UPSTREAM CONDITIONS
P.A. Polivanov¹, A.A. Sidorenko¹, A.A. Maslov¹; ¹ITAM SB RAS, Russia
11.7Operational Efficiency
Chair(s): Rein Weston, K.
Track 11
08 - Air Transport System Efficiency
28. Sep 16 14:00 14:30 11.7.1 AN IN-FLIGHT AID TO NEGOTIATE A MORE EFFICIENT FLIGHT PATH
C. Posse, United States; K. Rein-Weston, United States
28. Sep 16 14:30 15:00 11.7.2 PLANNING AND NEGOTIATION OF OPTIMIZED 4D-TRAJECTORIES IN STRATEGIC AND TACTICAL RE-ROUTING OPERATIONS
A. Gardi¹, Y. Lim¹, T. Kistan, THALES Australia, Australia; R. Sabatini¹; ¹RMIT University, Australia
12.7Humans in the Loop
Chair(s): Müller-Wiesner, D.
Track 12
09 - Safety and Security
28. Sep 16 14:00 14:30 12.7.1 CAN 3D-AUDIO IMPROVE STATE-OF-THE-ART PILOT-ASSISTANCE SYSTEMS?
C.A. Niermann, German Aerospace Center (DLR), Institute of Flight Guidance, Germany
28. Sep 16 14:30 15:00 12.7.2 OBJECTIVE EVALUATION OF HUMAN PILOT OPERATIONS IN WIND SHEAR USING PSYCHOPHYSIOLOGICAL MEASUREMENTS
J.O. Entzinger¹, T. Uemura¹, T. Iijima², N. Matayoshi², S. Suzuki¹; ¹The University of Tokyo, Japan ;²JAXA (Japan Aerospace Exploration Agency), Japan
28. Sep 16 15:00 15:30 12.7.3 EVALUATION METHODS OF AIRCRAFT FLIGHT SAFETY
J. Rajchel, Polish Air Force Academy, Poland; J. Zurek¹, R. Kaleta¹; ¹Air Force Institute of Technology, Poland

 Break

1.8UAS
Chair(s): Ueno, S., Kimmel, W.
Track1
01 - Aircraft and Systems Integration
28. Sep 16 16:00 16:30 1.8.1 CONCEPTUAL STUDY OF AN INNOVATIVE HIGH ALTITUDE SOLAR POWERED FLIGHT VEHICLE
J. Hanjie¹, D. Zhuoyi¹, P. Hongbin¹, S. Liying¹; ¹AVIC, China
28. Sep 16 16:30 17:00 1.8.2 TOWARDS A 4D TRAFFIC MANAGEMENT OF SMALL UAS OPERATING AT VERY LOW LEVEL
A. Joulia¹, T. Dubot¹, J. Bedouet¹; ¹ONERA - The French Aerospace Lab, France
28. Sep 16 17:00 17:30 1.8.3 FEASIBILITY ANALYSIS OF SPAN EXTENSION OF MORPHING HALE UAV WING
T. Prakash, Indian Institute of Technology Bombay, India
28. Sep 16 17:30 18:00 1.8.4 CONCEPTUAL AND AERODYNAMIC DESIGN OF A UAV FOR SUPERFICIAL VOLCANO MONITORING
P.D. Bravo-Mosquera¹, A. Martins-Abdalla¹, H.D. Cerón-Muñoz¹, F.M. Catalano¹; ¹Aerodynamic Laboratory, São Carlos Engineering School-University, Brazil
2.8Hypersonic Aerodynamics
Chair(s): , , Fonseca, G.C.
Track 2
02.1 - Aerodynamics - CFD Methods and Validation
28. Sep 16 16:00 16:30 2.8.1 NUMERICAL SIMULATION OF MIXING IN AN INLET-FUELED HYPERSONIC AIR-BREATHING PROPULSION
J.W. Kim¹, O.J. Kwon¹; ¹Korea Advanced Institute of Science and Technology, South Korea
28. Sep 16 16:30 17:00 2.8.2 AEROTHERMODYNAMICS CHARACTERISTICS OF A SPACE PROBE IN THE MARTIAN ATMOSPHERE
I.V. Egorov¹, N.V. Palchekovskaya¹, M.A. Pugach¹; ¹TsAGI, Russia
28. Sep 16 17:00 17:30 2.8.3 A MESHLESS METHOD FOR SIMULATION OF HYPERSONIC VISCOUS FLOWS
J.Y. Huh¹, J.S. Rhee¹, K.H. Kim¹, S.Y. Jung, Agency for Defense Development, South Korea; ¹Seoul National University, South Korea
3.8Flow Visualisation 2
Chair(s): Geotzendorf-Grabowski, T.
Track 3
02.2 - Experimental Aerodynamics
28. Sep 16 16:00 16:30 3.8.1 PRESSURE ANALYSIS BASED ON PIV MEASUREMENT IN AIRPLANE WAKES
K. Matsushima¹, R. Namba¹, H. Kato, JAXA, Japan; ¹Univ. of Toyama, Japan
28. Sep 16 16:30 17:00 3.8.2 THE RESEARCH AND VALIDATION OF GLOBAL SKIN FRICTION FIELDMEASUREMENT BASED ON FLUORESCENT OIL FILM
H.W. Wang¹, Z. Huang¹, L. Li¹, L.F. Wei¹, H.L. Xiong¹; ¹China Academy of Aerospace Aerodynamics, China
28. Sep 16 17:00 17:30 3.8.3 MATHEMATICAL MODELS AND OPTICAL INVESTIGATION OF TWO PHASE FLOWS IN WIND TUNNELS
I.A. Amelyushkin, TsAGI, Russia
4.8Super- and Hypersonic Aerodynamics 2
Chair(s): Atkin, C.
Track 4
02.4 - Applied Aerodynamics
28. Sep 16 16:00 16:30 4.8.1 LOW-DRAG / LOW-BOOM SHAPE OPTIMIZATION OF A BIPLANE WING / TWIN-BODY FUSELAGE SST CONFIGURATION
N. Ban, Nagaoka University of Technology, Japan
28. Sep 16 16:30 17:00 4.8.2 NUMERICAL STUDY OF ACTIVE SHOCK WAVE-TURBULENT BOUNDARY LAYER INTERACTION CONTROL FOR TRANSONIC AERODYNAMICS
Z. Seifollahi Moghadam ¹, A. Jahangirian¹; ¹Amirkabir University of Technology, Iran
5.8Damage Tolerance
Chair(s): , , Bayandor, J.
Track 5
03.1 - Materials issues, Fatigue and Damage Tolerance
28. Sep 16 16:00 16:30 5.8.1 DAMAGE TOLERANCE AND REPAIR OF UD-RIBS OF LATTICE COMPOSITE FUSELAGE STRUCTURES
E. Dubovikov¹, V. Fomin¹, M. Glebova¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
28. Sep 16 16:30 17:00 5.8.2 NUMERICAL ASSESSSMENT OF DAMAGE TOLERANCE ALLOWABLES FOR NEW DESIGN CONCEPTS OF STIFFENED COMPOSITE PANELS
T. Bach, German Aerospace Center (DLR), Germany
28. Sep 16 17:00 17:30 5.8.3 XFEM-BASED FRACTURE MECHANICS ANALYSIS OF AERONAUTICAL STRUCTURES AFFECTED BY RESIDUAL STRESSES
I. Rivero Arevalo¹, J. Gomez-Escalonilla Martin¹, V. Ramirez Gonzalez², A. Garcia Martinez-Pardo², D. Garijo Hernandez, IMDEA Materials Institute, Spain; ¹Airbus Defence and Space, Spain ;²Safran Engineering Services, Spain
28. Sep 16 17:30 18:00 5.8.4 INVESTIGATION OF DEFORMATION FIELDS IN AIRCRAFT PANELS BY NON-CONTACT OPTICAL VIDEOGRAMMETRY METHOD
K. Kuruliuk, Central Aerohydrodynamic Institute named after Zhukovsky, Russia
6.8Structural Design 4
Chair(s): Kuzmins, S.
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
28. Sep 16 16:00 16:30 6.8.1 NUMERICAL AND EXPERIMENTAL STRENGTH ANALYSIS OF LATTICE COMPOSITE FUSELAGE STRUCTURES
A. Dzuba¹, A. Shanygin¹, I. Kondakov¹, A. Razin², V. Vassiliev²; ¹Central Aerohydrodynamic Institute (TsAGI), Russia ;²Central Research Institute for Special Machinery (CRISM), Russia
28. Sep 16 16:30 17:00 6.8.2 EXPERIENCE OF USING NONLINEAR NUMERICAL ANALYSIS TO ESTIMATE AIRCRAFT PRIMARY STRUCTURE STRENGTH
Y.I. Dudarkov¹, E.A. Levchenko¹, M.V. Limonin¹, A.S. Dzuba¹; ¹TsAGI, Russia
28. Sep 16 17:00 17:30 6.8.3 APPLICATION OF BUCKLING/POST-BUCKLING ANALYSIS FOR COMPOSITE STIFFENED PANELS
L.-J. Dong, Chinese Aeronautical Establishment, China; G. Song, Beijing University of Aeronautics and Astronautics, China; D.-G. Cui, Aircraft Design and Research Institute of Shenyang, China
28. Sep 16 17:30 18:00 6.8.4 OPTIMIZATION OF COMPOSITE PATCH REPAIR FOR INCLINED CRACK ON ALUMINUM PLATE USING GENETIC ALGORITHM
B. Talebi¹, A. Abedian¹, S. Firooz¹; ¹Aerospace Engineering, Sharif University of Technology, Iran
7.8System of Systems Design & Operation
Chair(s): Holmberg, G., Anderson, K.
Track 7
07 - Systems Engineering and Supply Chain
28. Sep 16 16:00 16:30 7.8.1 UNMANNED VEHICLE COLLABORATION RESEARCH ENVIRONMENT FOR MARITIME SEARCH AND RESCUE
W. Roberts¹, K. Griendling¹, A. Gray¹, D.N. Mavris¹; ¹Georgia Tech, United States
28. Sep 16 16:30 17:00 7.8.2 EVOLUTIONARY GAME BASED MULTI-OBJECTIVE OPTIMIZATION FOR MULTI-AGENT NETWORK RESILIENCE
H.-I. Lee¹, H.-S. Shin¹, A. Tsourdos¹; ¹Cranfield University, United Kingdom
28. Sep 16 17:00 17:30 7.8.3 SYSTEMS ENGINEERING: AN INTERDISCIPLINARY CHALLENGE
P. Krus, Linköping University, Sweden; L. Pereira, Federal University of ABC, Brazil
8.8Flight Trajectory Design
Chair(s): Tsuchiya, T., Miyazawa, Y.
Track 8
05.1 - Flight Dynamics and Control (Control & Modelling)
28. Sep 16 16:00 16:30 8.8.1 MULTI-STEP TRAJECTORY OPTIMIZATION FOR ATM BASED ON APPROXIMATED OPTIMAL PATH
S. Bae¹, H.-S. Shin¹, A. Tsourdos¹; ¹Cranfield University, United Kingdom
28. Sep 16 16:30 17:00 8.8.2 BENEFITS ASSESSMENT ON TIME-BASED OCEANIC ARRIVALS TO THE TOKYO METROPOLITAN AREA
N.K. Wickramasinghe¹, S. Fukushima¹, H. Hirabayashi¹; ¹Electronic Navigation Research Institute, Japan
28. Sep 16 17:00 17:30 8.8.3 TRAJECTORY DESIGN WITH PATH PREDICTION FOR TERRAIN FOLLOWING
M.K. Kim¹, M.-H. Cho¹, M.-J. Tahk¹; ¹KAIST, South Korea
28. Sep 16 17:30 18:00 8.8.4 MINIMUM-TIME FORMATION USING OPTIMAL SOLUTIONS OF SINGLE FIXED-WING AIRCRAFT
H. Fukumoto¹, S. Ueno¹; ¹Yokohama National University, Japan
9.8History of Aeronautics
Chair(s): Kim, Y.
Track 9
28. Sep 16 16:00 16:30 9.8.1 HISTORY OF RAPID GROWTH IN KOREAN AERONAUTICAL INDUSTRY
D.-M. Ahn, Hanseo University, South Korea; W.-H. Kang, Yanbian University, China; S.-Y. Lee, KM Engineering, Former Head of Aircraft Sys. Int. Div. ADD, South Korea
28. Sep 16 16:30 17:00 9.8.2 DEVELOPMENT OF SMART TILT-ROTOR UAS AND THE BEGINNINGS OF KOREAN CIVILIAN DRONES
C.H. Lim¹, W.G. Kang¹, J.W. Kim¹; ¹KARI, South Korea
28. Sep 16 17:00 17:30 9.8.3 FROM 500MD TO LAH - CHALLENGE TOWARD VERTICAL LIFT IN KOREA
J.B. Yim, Agency for Defense Development, South Korea
28. Sep 16 17:30 18:00 9.8.4 THE ORIGIN OF WIND TUNNELS IN RUSSIA
A.R. Gorbushin, Central Aerohydrodynamic Institute, Russia
10.8Shock Waves and Control
Chair(s): Goraj, Z.
Track 10
02.3 - Basic Fluid Dynamics and Flow Control
28. Sep 16 16:00 16:30 10.8.1 INVESTIGATION ON OBLIQUE SHOCK WAVE CONTROL BY SURFACE ARC DISCHARGE PLASMA
F. Liu¹, H. Yan¹, J. Xu¹; ¹Northwestern Polytechnical University, China
28. Sep 16 16:30 17:00 10.8.2 CHARACTERISATION OF NS-DBD PLASMA ACTUATORS FOR SUPERSONIC FLOW CONTROL
A. Russell¹, H. Zare-Behtash¹, K. Kontis¹; ¹University of Glasgow, United Kingdom
28. Sep 16 17:00 17:30 10.8.3 THE DEVELOPMENT OF A SIMPLE METHOD FOR DRAG ESTIMATION FOR WEDGE-LIKE FAIRINGS IN HYPERSONIC FLOW
A. Roussel¹, S. Prince¹, M. Viguer¹, A. Kshitij¹, J. Stollery¹, K. Garry¹; ¹Cranfield University, United Kingdom
11.8Separation Management
Chair(s): Meckiff, C., Conway, S.
Track 11
08 - Air Transport System Efficiency
28. Sep 16 16:00 16:30 11.8.1 OPTIMAL SEQUENCING IN ATM COMBINING GENETIC ALGORITHMS AND GRADIENT BASED METHODS TO A BILEVEL APPROACH
B. Grüter¹, M. Bittner¹, M. Rieck¹, J. Diepolder¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, TU München, Germany
28. Sep 16 16:30 17:00 11.8.2 WAKE TURBULENCE RE-CATEGORISATION ON APPROACH AND DEPARTURE FOR SAFE AND MORE EFFICIENT AIR TRAFFIC MANAGEMENT
F. Rooseleer¹, V. Treve¹, I. De Visscher, Wake Prediction Technologies (WaPT), Belgium; R. Graham¹; ¹EUROCONTROL, Belgium
28. Sep 16 17:00 17:30 11.8.3 AIRBORNE COLLISION AVOIDANCE CONSIDERATIONS FOR SIMULTANEOUS PARALLEL APPROACH OPERATIONS
S.R. Conway¹, M.B. Lapis¹, J.D. Musiak¹, M.L. Ulrey¹, C. Hanses, German Aerospace Center, Germany; ¹Boeing, United States
28. Sep 16 17:30 18:00 11.8.4 NONLINEAR OPTIMAL CONFLICT RESOLUTION SOLVED WITH PARTICLE SWARM OPTIMIZATION
Y.K. Hong¹, Y.D. Kim¹, K.J. Lee, Korea Aerospace University, South Korea; ¹Seoul National University, South Korea
12.8Icing & Jet Engine Safety
Chair(s): Haselbach, F.
Track 12
09 - Safety and Security
28. Sep 16 16:00 16:30 12.8.1 EULERIAN METHOD FOR IN-ENGINE ICING: WITH APPLICATION TO ICE CRYSTAL TRAJECTORIES AND IMPACT IN A GENERIC TURBOFAN COMPRESSOR
E. Norde¹, E.T.A. van der Weide¹, H.W.M. Hoeijmakers¹; ¹University of Twente, Netherlands
28. Sep 16 16:30 17:00 12.8.2 RESEARCH ON AIRWORTHINESS REQUIREMENTS OF SUPERCOOLED LARGE DROP ICING PROTECTION FOR AIRCRAFT (§25.1420)
T. Hu¹, L. Jin¹; ¹China Aero-Polytechnology Establishment, AVIC, China
28. Sep 16 17:00 17:30 12.8.3 RESTARTING OF A JET ENGINE DURING FLYING AND FLIGHT SAFETY
M. Kowalski¹, A. Jankowski¹, J. Rajchel, Polish Air Force Academy, Poland; ¹Air Force Institute of Technology, Poland
28. Sep 16 17:30 18:00 12.8.4 DISPATCH RELIABILITY ORIENTED MMEL FORMULATION TECHNOLOGY RESEARCH
Z. Wang, NEIAS-AVIC, China

Thursday, 29. Sep 2016


7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
0.11GLOBALLY ADRESSING AIR TRAFFIC MANAGEMENT CHALLENGES
Chair: Murray Scott, AU, ICAS past president, Joachim Szodruch, GER, IFAR
29. Sep 16 08:00 09:30 IFAR Plenary Lecture
Fumikazu Itoh (JAXA), Jaiwon Shin (NASA), Michel Peters (NLR), Kim Eung-Tai (KARI), Akbar Sultan (NASA)

 Break

1.9Environmentally Responsible Aviation
Chair(s): Collier, F.
Track1
01 - Aircraft and Systems Integration
29. Sep 16 10:00 10:30 1.9.1 ENVIRONMENTALLY RESPONSIBLE AVIATION PROJECT OVERVIEW
F. Collier, United States
29. Sep 16 10:30 11:00 1.9.2 STITCHED, RESIN-INFUSED, HWB AIRCRAFT STRUCTURAL DEVELOPMENTS
A. Velicki, United States
29. Sep 16 11:00 11:30 1.9.3 FUEL-FLEXIBLE, COMBUSTOR AND FAN DEVELOPMENTS FOR UHB ENGINES
A. Epstein, United States
29. Sep 16 11:30 12:00 1.9.4 UHB ENGINE INTEGRATION FOR HYBRID WING BODY AIRCRAFT
J.T. Bonet, United States
29. Sep 16 12:00 12:30 1.9.5 TECHNOLOGY INTEGRATION AND SYSTEM ASSESSMENTS WITH UNCERTAINTY MODELLING
D.N. Mavris¹, K.G. Schwartz¹, J. Tai¹; ¹Georgia Institute of Technology, United States
2.9Current Developments in CFD 2
Chair(s): Pedreiro, L.
Track 2
02.1 - Aerodynamics - CFD Methods and Validation
29. Sep 16 10:00 10:30 2.9.1 ENGINEERING APPLICATION OF GAO-YONG RATIONAL TURBULENCE MODEL TO AN INTER-COOLED DUCT
X. Li¹, W. Zheng¹; ¹AVIC, China
29. Sep 16 10:30 11:00 2.9.2 NUMERICAL SIMULATIONS OF TURBULENT FLOWS OVER THE ONERA-M6 AND DLR-F6 CONFIGURATIONS
R.G. da Silva¹, J.L.F. Azevedo¹; ¹Instituto de Aeronautica e Espaco, Brazil
29. Sep 16 11:00 11:30 2.9.3 NUMERICAL INVESTIGATION OF SUBSONIC RAREFIED FLOWS USING DSMC-IP METHODS
Y.-J. Choi¹, O.-J. Kwon¹; ¹Korea Advanced Institute of Science and Technology, South Korea
29. Sep 16 11:30 12:00 2.9.4 A MESH-LESS METHOD FOR COMPRESSIBLE FLOW CALCULATIONS AT ALL SPEED CONDITIONS
A. Jahangirian¹, S. Sattarzadeh¹; ¹Amirkabir University of Technology, Iran
3.9Student Final
Chair(s): Rein Weston, K.
Track 3
4.9Design Optimization 2
Chair(s): Takovitskii, S.
Track 4
02.4 - Applied Aerodynamics
29. Sep 16 10:00 10:30 4.9.1 COLLABORATIVE MULTI-LEVEL MDO PROCESS DEVELOPMENT AND APPLICATION TO LONG-RANGE TRANSPORT AIRCRAFT
S. Görtz¹, C. Ilic¹, M. Abu-Zurayk¹, R. Liepelt¹, J. Jepsen¹, T. Führer¹, R. Becker¹, J. Scherer¹, T. Kier¹, M. Siggel¹; ¹German Aerospace Center (DLR), Germany
29. Sep 16 10:30 11:00 4.9.2 ON MORE EFFECTIVE AERODYNAMIC DATA GENERATION FOR SIMULATION BASED AIRCRAFT CONCEPTUAL DESIGN
J. Park¹, S. Choi¹, P. Raj¹; ¹Virginia Tech, United States
29. Sep 16 11:00 11:30 4.9.3 SURROOPT: A GENERIC SURROGATE-BASED OPTIMIZATION CODE FOR AERODYNAMIC AND MULTIDISCIPLINARY DESIGN
Z.-H. Han, Northwestern Polytechnical University, China
29. Sep 16 11:30 12:00 4.9.4 DEVELOPMENT OF A THREE-DIMENSIONAL TIGHTLY COUPLED EULER/POTENTIAL FLOW SOLVER FOR TRANSONIC FLOW
Y.M. Jo ¹, S.H. Park¹, D.J. Lee¹, S. Choi, Virginia Polytechnic Institute and State University, United States; ¹Korea Advanced Institute of Science and Technology, South Korea
5.9Fatigue and Corrosion
Chair(s): Nutt, S., Rand, O.
Track 5
03.1 - Materials issues, Fatigue and Damage Tolerance
29. Sep 16 10:00 10:30 5.9.1 VERIFICATION OF CFRP COMPONENTS FATIGUE EVALUATION PROCEDURE UNDER IRREGULAR CYCLING LOADING
A.V. Pankov¹, V.V. Konovalov¹; ¹TsAGI, Russia
29. Sep 16 10:30 11:00 5.9.2 PREDICTION OF WFD OCCURRENCE IN LONGITUDINAL JOINTS OF A FUSELAGE FOR COMMERCIAL AIRPLANE
A.A. Sviridov¹, I.G. Khlebnikova¹; ¹TsAGI, Russia
29. Sep 16 11:00 11:30 5.9.3 LIFE PREDICTION MODEL OF AIRCRAFT STRUCTURE UNDER CORROSION ENVIRONMENT
C. Li¹, Y. He¹, T. Zhang¹, X. Li¹, S. Zhang¹; ¹Air Force Engineering University, China
29. Sep 16 11:30 12:00 5.9.4 PREDICTION OF FRACTURE STRENGTH FOR NOTCHED LAMINATE SUBJECTED TO COMPRESSION LOADING
M. Lee, Agency for Defense Development, South Korea; J. Kim, Chungnam National University, South Korea
6.9Aeroelasticity 2
Chair(s): Shin, S.
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
29. Sep 16 10:00 10:30 6.9.1 ELASTO-STATIC AND MODAL MODELING OF FLEXIBLE WINGS CARRYING MULTIPLE EXTERNAL STORES
E.M. Amato¹, C. Polsinelli¹, E. Cestino¹, G. Frulla¹, R. Carrese², P. Marzocca²; ¹Politecnico di Torino, Italy ;²RMIT University, Australia
29. Sep 16 10:30 11:00 6.9.2 CHARACTERIZATION OF THE NONLINEAR AEROELASTIC BEHAVIOR OF AN AIRFOIL WITH FREEPLAY AND AERODYNAMIC NONLINEARITY
M. Candon¹, R. Carrese¹, H. Ogawa¹, P. Marzocca¹; ¹RMIT University, Australia
29. Sep 16 11:00 11:30 6.9.3 SENSITIVITY ANALYSIS OF UNSTEADY AERODYNAMIC REDUCED-ORDER MODELS ROBUST TO FREESTREAM PARAMETER VARIATIONS
M. Winter¹, C. Breitsamter¹; ¹Technische Universität München, Germany
7.9Hybrid-Electric and Distributed Propulsion Aircraft 2
Chair(s): Isikveren, A., Fielding, J.
Track 7
01 - Aircraft and Systems Integration
29. Sep 16 10:00 10:30 7.9.1 A REVIEW OF RECENT AIRCRAFT CONCEPTS EMPLOYING SYNERGISTIC PROPULSION-AIRFRAME INTEGRATION
J. Bijewitz¹, A. Seitz¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
29. Sep 16 10:30 11:00 7.9.2 COMPARATIVE EFFICIENCY ANALYSIS OF DISTRIBUTED PROPULSION SYSTEMS FOR PROPULSIVE FUSELAGE AND HYBRID WING BODY CONCEPTS IN FP7 PROJECT \"DISPURSAL\"
A. Mirzoyan¹, A. Isyanov¹, A.T. Isikveren, Safran Tech, France; ¹CIAM, Russia
29. Sep 16 11:00 11:30 7.9.3 AEROPROPULSIVE PERFORMANCE ANALYSIS OF THE NOVA CONFIGURATIONS
L. Wiart¹, O. Atinault¹, J.-C. Boniface¹, R. Barrier¹; ¹ONERA, France
29. Sep 16 11:30 12:00 7.9.4 HYBRID-ELECTRIC MOTIVE POWER SYSTEMS FOR COMMUTER TRANSPORT APPLICATIONS
Y. Fefermann¹, C. Maury¹, C. Level¹, K. Zarati¹, J.-P. Salanne¹, C. Pornet¹, B. Thoraval¹, A.T. Isikveren¹; ¹SAFRAN S.A., France
29. Sep 16 12:00 12:30 7.9.5 DISTRIBUTED ELECTRIC PROPULSION FOR SMALL BUSINESS AIRCRAFT A CONCEPT-PLANE FOR KEY-TECHNOLOGIES INVESTIGATIONS
J. Hermetz¹, M. Ridel¹, C. Döll¹; ¹ONERA, The French Aerospace Lab, France
8.9Handling Quality
Chair(s): Mori, R.
Track 8
05.1 - Flight Dynamics and Control (Control & Modelling)
29. Sep 16 10:00 10:30 8.9.1 NOVEL PILOT CONTROL MODEL WITH STOCHASTIC AND PERIODICAL MOVEMENT
R. Mori, Electronic Navigation Research Institute, Japan
29. Sep 16 10:30 11:00 8.9.2 THE FLYING QUALITIES IMPROVEMENT FOR THE VEHICLES WITH TIME DELAY IN THEIR DYNAMICS
A.V. Efremov ¹, M.S. Tyaglik¹, A.S. Tyaglik¹, V.V. Aleksandrov¹; ¹Moscow aviation institute, Russia
29. Sep 16 11:00 11:30 8.9.3 PILOT\'S CG LOCATION AND ATTITUDE CONTROL FOR LATERAL MANEUVER OF A HANG GLIDER
Y. Ochi, National Defense Academy, Japan
29. Sep 16 11:30 12:00 8.9.4 ADVANCED REFUELING BOOM SYSTEM (ARBS) DEVELOPMENT AND HANDLING QUALITIES EVALUATION
A. Anton Diez¹, F. Asensio Nieto¹; ¹AIRBUS DEFENCE & SPACE, Spain
29. Sep 16 12:00 12:30 8.9.5 EFFECT OF FEEL SYSTEM CHARACTERISTICS ON PILOT MODEL PARAMETERS
K. Grinev¹, S. Sorokin¹; ¹The Central Aerohydrodynamic Institute (TsAGI), Russia
9.9UAV Flight Dynamics and Control
Chair(s): Shin, H:, Kim, H.
Track 9
05.2 - Flight Dynamics and Control (UAV related)
29. Sep 16 10:00 10:30 9.9.1 ONE-VERSUS-ONE AIR-TO-AIR COMBAT MANEUVER GENERATION BASED ON THE DIFFERENTIAL GAME
B.-Y. Lee¹, S. Han¹, H.-J. Park², D.-W. Yoo², M.-J. Tahk¹; ¹Korea Advanced Institute of Science and Technology, South Korea ;²Agency for Defense Development , South Korea
29. Sep 16 10:30 11:00 9.9.2 CAPTURE REGION ANALYSIS FOR MISSILE GUIDANCE WITH FIELD-OF-VIEW CONSTRAINT AGAINST MOVING TARGET
S. Lee¹, Y. Kim¹, T.-Y. Um, Agency for Defense Development, South Korea; ¹Seoul National University, South Korea
29. Sep 16 11:00 11:30 9.9.3 A NEW SOLUTION METHOD FOR SIX DEGREE OF FREEDOM FLIGHT DYNAMICS SIMULATION OF A HIGH ASPECT RATIO WING VEHICLE
Y.B. Been¹, Y.J. Kang¹, S.J. Shin¹; ¹Seoul National Univ., South Korea
29. Sep 16 11:30 12:00 9.9.4 OPERATION SCENARIOS OF UNMANNED AIRCRAFT SYSTEMS INTEGRATED INTO THE KOREAN NATIONAL AIRSPACE SYSTEM
T.M. Shim¹, Y.J. Kim¹, H.C. Bang¹; ¹KAIST, South Korea
29. Sep 16 12:00 12:30 9.9.5 EFFECT OF YAW-TILTED HINGE AXIS ON DEPLOYMENT ROBUSTNESS OF MARS AIRPLANE
K. Fujita¹, H. Nagai, Tohoku University, Japan; A. Oyama¹; ¹ISAS/JAXA, Japan
10.9Transsonic Buffet Control
Chair(s): Wegner, W., Ogilvie, F.
Track 10
02.3 - Basic Fluid Dynamics and Flow Control
29. Sep 16 10:00 10:30 10.9.1 NEW METHOD OF TRANSONIC BUFFET DECREASING ON SUPERCRITICAL AIRFOIL
M.A. Brutyan¹, A.V. Petrov¹, A.V. Potapchik¹; ¹TsAGI, Russia
29. Sep 16 10:30 11:00 10.9.2 INVESTIGATION OF FLOW CONTROL OVER THE SUPERCRITICAL AIRFOIL BY TANGENTIAL JET BLOWING AT TRANSONIC SPEEDS
A.V. Petrov¹, A.V. Potapchik¹, V.G. Soudakov¹; ¹TsAGI, Russia
29. Sep 16 11:00 11:30 10.9.3 NUMERICAL STUDY ON TRANSONIC BUFFET ACTIVE CONTROL BY OPEN AND CLOSED-LOOP STRATEGIES
C.Q. Gao¹, W.W. Zhang¹, Z.Y. Ye¹; ¹Northwestern Polytechnical University , China
29. Sep 16 11:30 12:00 10.9.4 EFFECTS OF LAMINAR-TURBULENT TRANSITION ON BUFFET ONSET AND TRANSONIC CHARACTERISTICS OF LAMINAR AIRFOIL
W. Stalewski¹, K. Surmacz¹, J. Sznajder¹; ¹INSTITUTE of AVIATION, Poland
11.9Trajectories
Chair(s): Kügler, D., Lamiscarre, B.
Track 11
08 - Air Transport System Efficiency
29. Sep 16 10:00 10:30 11.9.1 ADVANCED RNP TO ILS AUTOLAND APPROACHES FOR OPTIMAL BENEFITS FROM PBN: FLIGHT TESTING PROCEDURES WITH AN A320
T. Dautermann¹, T. Ludwig¹, R. Geister¹, T. Blase, MBDA Systems, Germany; ¹DLR Institute of Flight Guidance, Germany
29. Sep 16 10:30 11:00 11.9.2 IMPACT OF WEATHER UNCERTAINTIES ON NOISE CONTOURS AND NOISE ABATEMENT DESCENT TRAJECTORIES
A. Andreeva-Mori¹, H. Ishii¹; ¹Japan Aerospace Exploration Agency (JAXA), Japan
29. Sep 16 11:00 11:30 11.9.3 OPTIMAL APPROACH TRAJECTORIES FOR MULTIPLE AIRCRAFT CONSIDERING DISTURBANCES AND CONFIGURATION CHANGES
M. Bittner¹, M. Rieck¹, B. Grüter¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, TUM, Germany
29. Sep 16 11:30 12:00 11.9.4 AIR TRAFFIC EFFICIENCY EVALUATION BY TRAJECTORY OPTIMIZATION AND ADS-B DATA
A. Harada, Kochi University of Technology, Japan
29. Sep 16 12:00 12:30 11.9.5 EFFICIENT CONTROL OF ARRIVAL TIME AT A CONGESTED AIRPORT\'S TERMINAL AREA
Y. Higuchi¹, N. Kitazume¹, T. Kozuka¹, K. Tamura¹, Y. Miyazawa¹, M. Brown, Electronic Navigation Research Institute, Japan; ¹Kyushu University, Japan
12.9Aircraft Operations and Safety
Chair(s): Lief, A.
Track 12
09 - Safety and Security
29. Sep 16 10:00 10:30 12.9.1 THE DESIGN OF AN AUTOMATIC BEACON EJECTING SYSTEM FOR AIRCRAFT
L. Peters¹, C. Bil¹; ¹RMIT University, Australia
29. Sep 16 10:30 11:00 12.9.2 AIRCRAFT SECURITY ENHANCEMENT: ROTATING MACHINERY FAULT DIAGNOSIS AND HEALTH ASSESSMENT USING MANIFOLD LEARNING AND DYNAMIC TIME WARPING
Y. Tian¹, C. Lu¹, Z.-L. Wang¹; ¹School of Reliability and Systems Engineering,Beihang University, China
29. Sep 16 11:00 11:30 12.9.3 INFLUENCE OF ETHNICITY ON PASSENGER STANDARD WEIGHT
C. Bil, RMIT University, Australia; G. Hanlon, Five Rings Aerospace, Australia
29. Sep 16 11:30 12:00 12.9.4 FUEL STARVATION CAUSED BY HUB CLOSURE
C. Wang¹, L. Drees¹, F. Holzapfel¹; ¹Technische Universität München, Germany
29. Sep 16 12:00 12:30 12.9.5 RESEARCH ON LOAD SPECTRUM OF AERO HYDRAULIC PUMP BASED ON ACCELERATED DEGRADATION TESTING
J. Chen¹, J. Zhang¹, J. Li, Siemens Industry Software (Beijing), Germany; ¹Beihang University, China

 Lunch

1.10High Speed and Access to Space
Chair(s): , , Kimmel, W.
Track1
01 - Aircraft and Systems Integration
29. Sep 16 14:00 14:30 1.10.1 CABIN ESCAPE SYSTEM: A WAY TO ENSURE CREW SAFETY DURING SUBORBITAL FLIGHTS
R. Fusaro¹, N. Viola¹, D. Ferretto¹, F. Santoro, Altec S.p.A, Italy; F. Fenoglio, Thales Alenia Space, Italy; ¹Politecnico di Torino, Italy
29. Sep 16 14:30 15:00 1.10.2 SUPERSONIC BUSINESS JET TECHNOLOGY AND MISSION TRADE STUDIES
L. Gonzalez, EMBRY RIDDLE AERONAUTICAL UNIVERSITY, United States
2.10Space Vehicle Configurations
Chair(s): Voevodenko, N.
Track 2
02.1 - Aerodynamics - CFD Methods and Validation
29. Sep 16 14:00 14:30 2.10.1 NUMERICAL SIMULATION OF AEROTHERMODYNAMIC CHARACTERISTICS OF FLOW OVER SPACE VEHICLE MODEL
I. Egorov¹, N. Palchekovskaya¹; ¹TsAGI, Russia
29. Sep 16 14:30 15:00 2.10.2 AERODYNAMIC ANALYSIS WITH SEPARATION DYNAMICS OF A LAUNCHER AT STAGING CONDITIONS
A. Viviani¹, G. Pezzella, Centro Italiano Ricerche Aerospaziali, Italy; E. D'Amato¹; ¹Seconda Università di Napoli, Italy
29. Sep 16 15:00 15:30 2.10.3 NUMERICAL SIMULATION OF HYDRODYNAMIC LOADINGS ON REENTRY VEHICLE DURING SPLASHDOWN
A.A. Aksenov, TESIS; JIHT RAS, Russia; A.A. Dyadkin ¹, M.K. Mikhailova ², A.E. Schelyaev ², T.V. Simakova ¹, V.V. Zharckova ²; ¹JSV «RSC Energia» , Russia ;²TESIS, Russia
3.10Aircraft Model Testing
Chair(s): Krus, P.
Track 3
02.2 - Experimental Aerodynamics
29. Sep 16 14:00 14:30 3.10.1 SUBSCALE FLIGHT TESTING OF A GENERIC FIGHTER AIRCRAFT
D. Lundström¹, A. Sobron¹, P. Krus¹, C. Jouannet, SAAB AB, Sweden; R.G.A. da Silva, Instituto Tecnológico de Aeronáutica, Brazil; ¹Linköping University, Sweden
29. Sep 16 14:30 15:00 3.10.2 DESIGN AND TESTING OF A LOW-COST FLIGHT CONTROL AND DATA ACQUISITION SYSTEM FOR UNSTABLE SUBSCALE AIRCRAFT
A. Sobron¹, D. Lundström¹, I. Staack¹, P. Krus¹; ¹Linköping University, Sweden
29. Sep 16 15:00 15:30 3.10.3 DEVELOPMENT OF HALF-MODEL TEST CAPABILITY AT THE NF-3 WIND TUNNEL
D. Lei¹, H. Zenghong¹, G. Yongwei¹; ¹Northwestern Polytechnical university, China
4.10HEXAFLY-INT Project
Chair(s): Gubanov, A.
Track 4
02.4 - Applied Aerodynamics
29. Sep 16 14:00 14:30 4.10.1 NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT
J. Steelant¹, V. Villace¹, M. Marini², G. Pezzella², B. Reimann, DLR, Germany; S.L. Chernyshev³, A.A. Gubanov³, V.A. Talyzin³, N.V. Voevodenko³, N.V. Kukshinov*, A.N. Prokhorov*, A.J. Neelyº, C. Kennellº, D. Verstraete, University of Sydney, Australia; D. Buttsworth, Univ. of Southern Queensland, Australia; ¹ESA-ESTEC, Netherlands ;²CIRA, Italy ;³TsAGI, Russia ;*CIAM, Russia ;ºUniv. of New South Wales, Australia
29. Sep 16 14:30 15:00 4.10.2 BOUNDARY LAYER STATE INFLUENCE ON START OF THE INWARD-TURNING INTAKE
N.V. Voevodenko¹, A.A. Gubanov¹, D.Y. Gusev¹, M.A. Ivankin, TsAGi, Russia; D.S. Ivanyushkin¹, V.Y. Lunin¹, P.A. Meshennikov¹, Y.G. Shvalev¹, V.A. Talyzin¹, V.A. Yakovleva¹; ¹TsAGI, Russia
29. Sep 16 15:00 15:30 4.10.3 NUMERICAL AND EXPERIMENTAL INVESTIGATION OF DIFFERENT INTAKE CONFIGURATIONS OF HEXAFLY-INT FACILITY MODULE
V.Y. Aleksandrov¹, M.K. Danilov¹, O.V. Gouskov¹, S.V. Gusev¹, N.V. Kukshinov¹, A.N. Prokhorov¹, V.S. Zakharov¹; ¹CIAM, Russia
5.10Modeling and Tests of Systems & Subsystems 2
Chair(s): Stoufflet, B.
Track 5
06 - Systems, Subsystems and Equipment
29. Sep 16 14:00 14:30 5.10.1 COLLABORATIVE SYSTEMS DRIVEN AIRCRAFT CONFIGURATION DESIGN OPTIMIZATION
P. Shiva Prakasha¹, P.D. Ciampa¹, B. Nagel¹, L. Boggero², M. Fioriti²; ¹German Aerospace Center, Germany ;²Politecnico di Torino, Italy
29. Sep 16 14:30 15:00 5.10.2 HIL TEST BENCH FOR ENGINE\'S FUEL CONTROL SYSTEMS INVESTIGATION
S. Gafurov¹, L. Rodionov¹, A. Kryuchkov¹, H. Handroos, Lappeenranta University of Technology, Finland; ¹Samara National Research University, Russia
29. Sep 16 15:00 15:30 5.10.3 STRATEGIES TO ENHANCE A CONFIGURATION FOR HIGH-PRECISION MULTI DISCIPLINARY OPTIMIZATION
H. Liu, China
6.10Structural Dynamics
Chair(s): , , Park, C.
Track 6
03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
29. Sep 16 14:00 14:30 6.10.1 THE SUPPORT PROCESS, SIMULATION RESEARCH DESIGN AND STRUCTURE OF THE NEW HELICOPTER\'S CONSTRUCTION SCHEMATICS WITH SPECIAL EMPHASIS ON GROUND RESONANCE PHENOMENON
G. Kowaleczko¹, T. Gorecki¹; ¹Air Force Institute of Technology , Poland
29. Sep 16 14:30 15:00 6.10.2 A STUDY OF THE ACCURACY OF GROUND VIBRATION TEST DATA USING A REPLICA OF THE GARTEUR SM-AG19 TESTBED STRUCTURE
P. Gustafsson, SAAB AB, Sweden; A. Linderholt, Linnaeus University, Sweden
7.10Combustion and High Speed
Chair(s): Yan, H.
Track 7
04 - Propulsion
29. Sep 16 14:00 14:30 7.10.1 COMBUSTION INSTABILITY FREQUENCY MODE SHIFT OF H2/CH4 RATIO AND COMBUSTOR LENGTH IN A MODEL GAS TURBINE
S. Joo¹, J. Yoon¹, J. Kim¹, S. Kim¹, Y. Yoon¹; ¹seoul national university, South Korea
29. Sep 16 14:30 15:00 7.10.2 INVESTIGATION OF THE HYDROGEN COMBUSTION CHAMBER PERFORMANCE WITHIN THE HEXAFLY-INT PROJECT
M.A. Ivankin¹, A.A. Nikolaev¹, V.A. Talyzin¹, O.V. Voloschenko¹; ¹TsAGI, Russia
8.10Flight Optimization and Identification
Chair(s): Suzuki, S.
Track 8
05.1 - Flight Dynamics and Control (Control & Modelling)
29. Sep 16 14:00 14:30 8.10.1 A WAVELET BASED FLIGHT DATA PREPROCESSING METHOD FOR FLIGHT CHARACTERISTICS ESTIMATION AND FAULT DETECTION
M. Naruoka, Japan Aerospace Exploration Agency, Japan
29. Sep 16 14:30 15:00 8.10.2 WIND VELOCITY ESTIMATION WITHOUT AN AIR SPEED SENSOR USING KALMAN FILTER UNDER THE COLORED MEASUREMENT NOISE
Y.G.J. Park¹, C.G. Park¹; ¹Seoul National University, South Korea
29. Sep 16 15:00 15:30 8.10.3 INFERENCE OF FLIGHT INTENT BASED ON INVERSE OPTIMAL CONTROL
N. Yokoyama, National Defense Academy of Japan, Japan
9.10UAV Flight Dynamics
Chair(s): Rein Weston, K.
Track 9
05.2 - Flight Dynamics and Control (UAV related)
29. Sep 16 14:00 14:30 9.10.1 THE EFFECTS OF BODY AERODYNAMICS ON THE DYNAMIC STABILITY OF INSECT FLIGHT
A.-T. Nguyen¹, J.-K. Kim¹, J.-H. Han¹; ¹Korea Advanced Institute of Science and Technology, South Korea
10.10Lateral Jets
Chair(s): Atkin, C.
Track 10
02.3 - Basic Fluid Dynamics and Flow Control
29. Sep 16 14:00 14:30 10.10.1 COMPUTATIONS OF SUPERSONIC LATERAL JET
J. Huh¹, S. Lee¹; ¹Inha univ., South Korea
29. Sep 16 14:30 15:00 10.10.2 EXPERIMENTAL INVESTIGATION OF LATERAL PULSE JET INTERACTION FLOWFIELD IN HYPERSONIC FLOW
Z.-Y. Ni¹, N. Cao¹, L. Xu¹; ¹CAAA, China
11.10Systems Engineering & Integration
Chair(s): Fredriksson, B.
Track 11
07 - Systems Engineering and Supply Chain
29. Sep 16 14:00 14:30 11.10.1 REPORT FROM ICAS WORKSHOP ON COMPLEX SYSTEMS INTEGRATION IN AERONAUTICS
S.X. Ying, COMAC, China
29. Sep 16 14:30 15:00 11.10.2 CO-EVOLUTION OF COMPLEX AERONAUTICAL SYSTEM & COMPLEX SYSTEM ENGINEERING
X.G. Zhang, Aviation Industry Corporation of China (AVIC), China
29. Sep 16 15:00 15:30 11.10.3 VIRTUAL EXPERIMENTATION AND VISUAL ANALYTICS IN SUPPORT OF SYSTEMS ENGINEERING AND SYSTEMS OF SYSTEMS ENGINEERING EFFORTS
K. Griendling¹, O.J. Pinon¹, D.N. Mavris¹; ¹Georgia Tech, United States
12.10ISABE 2
Chair(s): Melkert, J.
Track 12
29. Sep 16 14:00 14:30 12.10.1 THE FUTURE JOURNEY OF CIVIL AEROSPACE: WEATHER, ENVIRONMENT AND CLIMATE
R. Singh, Emeritus Cranfield University, United Kingdom
29. Sep 16 14:30 15:00 12.10.2 THE FUTURE OF SUSTAINABLE COMMERCIAL PROPULSION
A. Epstein, Pratt & Whitney, United States

 Break

0.12VON KARMAN LECTURE
Chair: Susan Ying Chair ICAS Programme Committee
29. Sep 16 16:00 17:00 The Airbus 350 XWB Programme
Gordon McConnel

0.13CLOSING CEREMONY
Chair: Christian Mari ICAS president
29. Sep 16 17:00 17:30