30th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

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Monday, 10. Sep 2018


7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
07:00 - 08:00Registration

08:00 - 09:00Opening Ceremony

0.1ICAS Daniel & Florence Guggenheim Memorial Lecture - Humberto Perreira - Product Development Challenges in the Commercial Airplane Market
Chair: Susan Ying ICAS President
10. Sep 18 09:00 10:00

10:00 - 10:30Break

1.1Novel Application of MDO in Aircraft Design 1
Chair(s): Nagel, B.
Track 1
01 - Aircraft Design and Integrated Systems
10. Sep 18 10:30 11:00 1.1.1 COLLABORATIVE , MULTI-NATIONAL MDO OF CIVIL AIRCRAFT : AGILE EU PROJECT
P S Shiva Prakasha, German Aerospace Center, Germany
10. Sep 18 11:00 11:30 1.1.2 MULTIDISCIPLINARY DESIGN OPTIMIZATION OF BLENDED WING BODY AIRCRAFT THROUGH COLLABORATIVE DESIGN - AGILE EU PROJECT
P S Shivaprakasha, German Aerospace Center, Germany
10. Sep 18 11:30 12:00 1.1.3 AERO_STRUCTURAL OPTIMIZATION OF A MALE CONFIGURATION IN THE AGILE MDO FRAMEWORK
R. Maierl, Airbus Defence and Space, Germany
2.1UAS 1
Chair(s): Gerhards, R.
Track 2
01 - Aircraft Design and Integrated Systems
10. Sep 18 10:30 11:00 2.1.1 MULTIDISCIPLINARY DESIGN OPTIMIZATION OF UNMANNED AIRCRAFT IN A SYSTEM OF SYSTEMS CONTEXT
A. Papageorgiou, Link÷ping University, Sweden
10. Sep 18 11:00 11:30 2.1.2 DEVELOPMENT OF A COMPREHENSIVE ANALYSIS AND OPTIMIZED DESIGN FRAMEWORK FOR THE MULTIROTOR UAV
H.S. Kim, Seoul National University, South Korea
10. Sep 18 11:30 12:00 2.1.3 DEVELOPMENT AND PERFORMANCE COMPARISON OF OPTIMIZED ELECTRIC FIXED-WING VTOL UAV CONFIGURATIONS
Philipp Stahl╣, Christian R÷▀ler╣, Mirko Hornung╣; ╣Technical University of Munich, Germany
Reserve Paper 2.1.R RESEARCH ON DESIGN METHOD OF PETROL-ELECTRIC HYBRID DRIVE SYSTEM BASED ON MDO FOR A NOVEL VTOVL UAV
Z. X. YAO, Shenyang Aircraft Design and Research Institute, China
3.1System of Systems Design
Chair(s): Holmberg, G., Marengo, L.
Track 3
02 - Systems Engineering and Integration
10. Sep 18 10:30 11:00 3.1.1 MORPHOLOGICAL MATRICES FOR DECISION MAKING IN THE CONTEXT OF SIMULATION-BASED SYSTEMS OF SYSTEMS DESIGN
I. Staack, Link÷ping University, Sweden
10. Sep 18 11:00 11:30 3.1.2 CONTINUOUS MODELING IN AIRCRAFT TOP-LEVEL DEMONSTRATION
J. Zang╣, Q. Wang╣, J.-Q Zhu╣; ╣Aviation Industry Development Research Center of China, China
10. Sep 18 11:30 12:00 3.1.3 FORMULATION AND IMPLEMENTATION OF A METHOD FOR TECHNOLOGY EVALUATION OF SYSTEM OF SYSTEM
D. Mavris, United States
4.1Unsteady Aerodynamics 1
Chair(s): Catalano, P., Lima, L.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
10. Sep 18 10:30 11:00 4.1.1 A METHOD FOR MODELING UNSTEADY TRANSONIC FLOWS AT LOW COMPUTATIONAL COST
H. GŘner╣, G. Dimitriadis╣, V. Terrapon╣; ╣University of LiŔge, Belgium
10. Sep 18 11:00 11:30 4.1.2 FEASIBILITY OF NAVIER-STOKES HARMONIC BALANCE METHOD FOR MODELLING UNSTEADY AERODYNAMICS
J. Drofelnik╣, A. Da Ronch╣, M.S. Campobasso, University of Lancaster, United Kingdom; ╣University of Southampton, United Kingdom
10. Sep 18 11:30 12:00 4.1.3 COMPUTATIONAL AND EXPERIMENTAL UNSTEADY PRESSURE DISTRIBUTIONS OF WING OSCILLATING IN PITCH
G.R. Begnini, Embraer S.A., Brazil
Reserve Paper 4.1.R LATTICE-BOLTZMANN SIMULATIONS OF THE OSCILLATING BENCHMARK SUPERCRITICAL WING
F. P. Ribeiro, Exa GmbH, Germany
5.1Wind Tunnel Test Technology
Chair(s): Hermans, C.
Track 5
03.2 - Experimental Aerodynamics
10. Sep 18 10:30 11:00 5.1.1 ADAPTIVE DESIGN OF EXPERIMENT BASED ON GAUSSIAN PROCESS MODELS WITH NONSTATIONARY KERNEL APPLIED TO WIND TUNNEL TESTING
U.-H. Choi, KAIST, South Korea
10. Sep 18 11:00 11:30 5.1.2 RLG BASED REAL-TIME MODEL ATTITUDE DETERMINATION SYSTEM DEVELOPMENT FOR LARGE LOW SPEED FACILITY OF CARDC
L.T. Fan, CARDC, China
10. Sep 18 11:30 12:00 5.1.3 ROTATING SHAFT BALANCE DESIGN AND CALIBRATION FOR CROR TESTING
V.S. Manvelyan, TsAGI, Russia
Reserve Paper 5.1.R THE INFLUENCE OF SPIV DATA PROCESSING PARAMETERS ON AIRCRAFT WING WAKE VORTEX ASSESSMENT
K P Garry, Cranfield University, United Kingdom
6.1Fundamental Fluid Dynamics 1
Chair(s): Cavalieri, A., Brandao, M.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
10. Sep 18 10:30 11:00 6.1.1 DESTABILIZING EFFECT OF LONGITUDINAL WALL OSCILLATION ON OBLIQUE WAVES IN 2D CHANNEL FLOW
T Atobe, Japan Aerospace Exploration Agency, Japan
10. Sep 18 11:00 11:30 6.1.2 EXPERIMENTAL INVESTIGATION, MATHEMATICAL AND NUMERICAL SIMULATION OF AIRCRAFT ICING PHENOMENA
I.A. Amelyushkin, Central Aerohydrodynamic Institute (TsAGI), Russia
10. Sep 18 11:30 12:00 6.1.3 NUMERICAL INVESTIGATION OF THE INFLUENCE OF THE WALL TEMPERATURE ON THE BOUNDARY-LAYER STABILITY OF AN ABLATIVE WALL
F. Miro Miro, von Karman Institute for Fluid Dynamics, Belgium
7.1Flow Control
Chair(s): Heyns, J.
Track 7
03.4 - Applied Aerodynamics
10. Sep 18 10:30 11:00 7.1.1 GUST LOAD ALLEVIATION WITH A FLUIDIC CONTROL DEVICE APPLYING LINEARISED COMPUTATIONAL FLUID DYNAMICS
R. Thormann, University of Liverpool, United Kingdom
10. Sep 18 11:00 11:30 7.1.2 WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTING
V. Ciobaca, DLR, Germany
10. Sep 18 11:30 12:00 7.1.3 PASSIVE VENTILATION FLOW CONTROL FOR AIRCRAFT GUST LOAD ALLEVIATION
Y. Tani, Kyushu University, Japan
Reserve Paper 7.1.R INVESTIGATION ON THE POSSIBILITY OF FLOW CONTROL AROUND CAVITY USING CONTINUOUS TANGENTIAL JET
Y. Lee, Agency for Defense Development, South Korea
8.1Acustics and Vibrations 1
Chair(s): Sanches, L.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
10. Sep 18 10:30 11:00 8.1.1 CRITICAL STRUCTURAL DAMPING FOR ACOUSTIC SCATTERING BY POROELASTIC PLATES
M. M. Nilton, Instituto Tecnolˇgico de Aeronßutica, Brazil
10. Sep 18 11:00 11:30 8.1.2 NUMERICAL SIMULATION ON THE FLOW-INDUCED VIBRATION CHARACTERISTIC OF MULTI-NOZZLE EJECTOR
Y.S. YANG, China Aerodynamics Research and Development Center, China
10. Sep 18 11:30 12:00 8.1.3 GROUND VIBRATION TEST USING ACOUSTIC EXCITATION - APPLICATION ON A COMPOSITE WING
L. P. S. F Ferreira, UFMG, Brazil
Reserve Paper 8.1.R HIGH PERFORMANCE PNEUMATIC SHOCK-ABSORBERS FOR AERONAUTICAL APPLICATIONS
R. Faraj, Institute of Fundamental Technological Research, Poland
9.1Hybrid-Electric Propulsion
Chair(s): Isikveren, A.
Track 9
05 - Propulsion
10. Sep 18 10:30 11:00 9.1.1 DEVELOPMENT OF HYBRID GASOLINE-BATTERY PROPULSION SYSTEM FOR MULTI-COPTER PLATFORM
H. R. Gwon, KOREAN AIR, South Korea
10. Sep 18 11:00 11:30 9.1.2 PROPELLER OPTIMISATION FOR AN ELECTRICAL-POWERED TACTICAL UAV
D. Verstraete, The University of Sydney, Australia
10. Sep 18 11:30 12:00 9.1.3 DESIGN AND OFF-DESIGN PERFORMANCE OF ELECTRIC SYSTEM ARCHITECTURES FOR ELECTRIC POWERED AIRCRAFT
P. C. Vratny, Bauhaus Luftfahrt e.V., Germany
Reserve Paper 9.1.R SYSTEM ANALYSIS OF TURBO ELECTRIC AND HYBRID PROPULSION SYSTEMS ON A REGIONAL AIRCRAFT
H. Gesell╣, F. Wolters╣, M. Plohr╣; ╣DLR, Germany
10.1FT & RC
Chair(s): Wang, Q.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
10. Sep 18 10:30 11:00 10.1.1 NEURAL NETWORK-BASED FAULT TOLERANT CONTROL FOR AIRCRAFT
N. Yoshikawa, The Univercity of Tokyo, Japan
10. Sep 18 11:00 11:30 10.1.2 FAULT-TOLERANT FLIGHT CONTROL SYSTEM WITH SIMPLE ADAPTIVE CONTROL CONSIDERING PILOT INPUT
R. Takase╣, J.O. Entzinger╣, S. Suzuki╣; ╣The University of Tokyo, Japan
10. Sep 18 11:30 12:00 10.1.3 RECONFIGURABLE FLIGHT CONTROL SYSTEM OF AN AIRCRAFT MODEL
N. C. Pereira, Federal Instituto of SŃo Paulo, SŃo Carlos campus, Brazil
11.1UAS Navigation
Chair(s): Greco Jr., P.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
10. Sep 18 10:30 11:00 11.1.1 MODIFIED COMPOSITE GUIDANCE LAW AGAINST MOVING TARGET CONSIDERING NARROW FIELD-OF-VIEW LIMIT
Seokwon Lee╣, Sungjun Ann╣, Youdan Kim╣; ╣Seoul National University, South Korea
10. Sep 18 11:00 11:30 11.1.2 AUTONOMOUS FLIGHT OF UNMANNED MULTICOPTER USING SUPER WIDE-ANGLE STEREO VISION SYSTEM
T. Yamashita╣, Y. Kajiwara╣, C.T. Raabe▓, T. Tsuchiya▓, S. Suzuki▓; ╣Ricoh Co. Ltd, Japan ;▓the University of Tokyo, Japan
10. Sep 18 11:30 12:00 11.1.3 SIMULTANEOUS LOCALIZATION AND MAPPING WITH OBJECT DETECTION FOR UAV APPLICATONS
T. Shim, KAIST, South Korea
Reserve Paper 11.1.R ON BOARD SLAM FOR INDOOR MAV USING A LASER RANGE FINDER
K.-S. Sibilski, Air Force Institute of Technology, Poland
12.1Air Transportation Efficiency
Chair(s): Tomcko, I.
Track 12
09 - Air Transport System Efficiency
10. Sep 18 10:30 11:00 12.1.1 DECISION-MAKING INFORMATION SYSTEM FOR MULTIMODAL DISRUPTION MANAGEMENT: SYSTEM ARCHITECTURE AND CONCEPT OF OPERATIONS
FJS JimÚnez Serrano, Hamad International Airport (Qatar Airways), Qatar
10. Sep 18 11:00 11:30 12.1.2 IMPLEMENTATION OF ECO-EFFICIENT PROCEDURES TO MITIGATE THE CLIMATE IMPACT OF NON-CO2 EFFECTS
M. Nikla▀, DLR, Germany
10. Sep 18 11:30 12:00 12.1.3 AN ATC ORIENTED INTERFACE FOR MULTI-AIRCRAFT OPTIMISATION FOR CLIMBS AND DESCENTS
A. Spiteri, University of Malta, Malta
Reserve Paper 12.1.R QUANTIFICATION OF FORMATION FLIGHT BENEFITS UNDER CONSIDERATION OF UNCERTAINTIES ON FUEL PLANNING
M. Swaid, Hamburg University of Technology (TUHH), Germany

12:00 - 13:00Lunch

1.2Novel Application of MDO in Aircraft Design 2
Chair(s): Ciampa, P.D.
Track 1
01 - Aircraft Design and Integrated Systems
10. Sep 18 13:00 13:30 1.2.1 DESIGN OF THE STRUT BRACED WING AIRCRAFT IN THE AGILE COLLABORATIVE MDO FRAMEWORK
P.D. Ciampa, German Aerospace Center, DLR, Germany
10. Sep 18 13:30 14:00 1.2.2 MDO APPLICATIONS TO CONVENTIONAL AND NOVEL TURBOPROP AIRCRAFTS WITHIN AGILE EUROPEAN PROJECT
P. Della Vecchia, University of Naples Federico II, Italy
10. Sep 18 14:00 14:30 1.2.3 INCLUDING AEROELASTIC TAILORING IN THE CONCEPTUAL DESIGN PROCESS OF A COMPOSITE STRUT BASED WING
D Rajpal, Delft University of Technology, Netherlands
2.2UAS 2
Chair(s): Ogilvie, F.
Track 2
01 - Aircraft Design and Integrated Systems
10. Sep 18 13:00 13:30 2.2.1 A VTOL SMALL UNMANNED AIRCRAFT SYSTEM TO EXPAND PAYLOAD CAPABILITIES
S. Geuther╣, F. Capristan╣, J. Kirk, Georgia Institute of Technology, United States; R. Erhard, University of Denver, United States; ╣NASA Langley Research Center, United States
10. Sep 18 13:30 14:00 2.2.2 LIFECYCLE COSTS AND FEASIBILITY ANALYSIS OF THE DESIGNS OF UAVS FOR HUMANITARIAN RELIEF MISSIONS
O Hektor╣, Dr. T Melin╣; ╣Swedish Aeronautical Institute, Sweden
10. Sep 18 14:00 14:30 2.2.3 SOLAR-POWERED UAV PLATFORM SYSTEM: A CASE STUDY FOR GROUND CHANGE DETECTION
ACBR Brandao Ramos, UNIFEI, Brazil
Reserve Paper 2.2.R UAV INITIAL PARAMETER ESTIMATION
Lucas Campos Carmona╣, Eduardo Bauzer Medeiros╣; ╣UFMG, Brazil
3.2Concept Design Methodology
Chair(s): Mavris, D., Macedo, A-P.
Track 3
02 - Systems Engineering and Integration
10. Sep 18 13:00 13:30 3.2.1 COMBINED AIRFRAME AND SUBSYSTEMS EVOLVABILITY EXPLORATION DURING CONCEPTUAL DESIGN
M.D. Guenov, Cranfield University, United Kingdom
10. Sep 18 13:30 14:00 3.2.2 A TECHNIQUE FOR CAPTURING STAKEHOLDER PREFERENCES AND KNOWLEDGE IN EARLY DESIGN STUDIES
S. Sartorius, United States; M. Hornung, Technical University of Munich Institute of Aircraft Design, Germany
10. Sep 18 14:00 14:30 3.2.3 METHODOLOGY FOR THE DEVELOPMENT OF FUTURE AIRLINER PASSENGER CABINS FOR THE ASIAN MARKET
R. Kirenskis, Cranfield University, United Kingdom
4.2Unsteady Aerodynamics 2
Chair(s): Da Ronch, A, Azevedo, J.H.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
10. Sep 18 13:00 13:30 4.2.1 NUMERICAL DEVELOPMENT OF UNSTEADY VORTEX-LATTICE METHOD EXPANSION FOR LEADING-EDGE SHEDDING PREDICTION WITH EXPERIMENTAL VALIDATION
Monteiro, T.P. Monteiro, Instituto Tecnolˇgico de Aeronßutica, Brazil
10. Sep 18 13:30 14:00 4.2.2 NUMERICAL ANALYSIS OF THE FLOW AROUND A BACKWARD-FACING RAMP
P. Catalano, C.I.R.A. - Italian Aerospace Research Center, Italy
10. Sep 18 14:00 14:30 4.2.3 RECTANGULAR CAVITY FLOWFIELD EFFECTS ON STORES IN THE SHEAR LAYER
S. Kushan, TAI, Turkey
Reserve Paper 4.2.R EXPERIMENTAL AND NUMERICLA ANALYSIS OF DYNAMIC FUEL INDUCED LOADING ON AIRCRAFT STRUCTURES
J.A. Heyns, CSIR, South Africa
5.2Aerodynamic Effects of Propulsion Integration
Chair(s): Xumian, W.
Track 5
03.2 - Experimental Aerodynamics
10. Sep 18 13:00 13:30 5.2.1 THE AERODYNAMIC PERFORMANCE MEASUREMENT OF RIGID COAXIAL ROTOR WING IN HOVER
X ZHAO╣, N-Z HUANG╣, X LIANG╣, P ZHOU╣, Y-F LIN, China Helicopter Research and Development Institute, China; ╣Northwestern Polytechnical University, China
10. Sep 18 13:30 14:00 5.2.2 ADAPTIVE WING HIGH-LIFT SYSTEM
Vitaliy: V Gubskiy, TsAGI, Russia
10. Sep 18 14:00 14:30 5.2.3 INSTALLATION EFFECTS ON THE AERODYNAMICS AND AEROACOUSTICS OF A PYLON AND A PUSHER PROPELLER
L. Rego, University of SŃo Paulo, Brazil
Reserve Paper 5.2.R EXPERIMENTAL RESEARCH AND NUMERICAL ANALYSIS OF COLD AND HOT-JET SIMULATION OF TRUST VECTOR CONTROL BY JET TABS
G. Ocokoljic, Military Technical Institute, Belgrade, Serbia
6.2Fundamental Fluid Dynamics 2
Chair(s): Cavalieri, A.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
10. Sep 18 13:00 13:30 6.2.1 THE ROLE OF DUCT-LIKE PRESSURE MODES ON CYLINDER WAKE
E. Martini Rodrigues da Silva, ITA, Brazil
10. Sep 18 13:30 14:00 6.2.2 ANOMALOUS PRESSURE PULSE DUE TO BOW SHOCK COLLAPSING EFFECT AT THE INTERACTION OF BLUNT BODIES WITH GAS BUBBLES
V. Levin, Institute of Mechanics of Lomonosov Moscow State University, Russia
10. Sep 18 14:00 14:30 6.2.3 LONGITUDINAL VORTEXE FORMATION IN THE HYPERSONIC FLOW AROUND WINDWARD SIDE OF BLUNTED DELTA WING AND EFFECTS OF THEIR IN
V.I. Shalaev, Moscow Institute of Physics and Technology, Russia
Reserve Paper 6.2.R AERODYNAMICS VIA AEROACOUSTICS - THE CASE FOR CIRCULATION CAPTURE
M. P. BrandŃo, ITA, Brazil
7.2Unmanned Aircraft
Chair(s): Yutko, B.
Track 7
03.4 - Applied Aerodynamics
10. Sep 18 13:00 13:30 7.2.1 STUDY ON SMALL UAVS' DEEP STALL LANDING PROCEDURE
B C Cheng, China
10. Sep 18 13:30 14:00 7.2.2 AERODYNAMIC ANALYSIS OF A LOW-SPEED UNMANNED AERIAL VEHICLE IN FULL CONFIGURATION BASED TRANSITION MODEL
C.-L.L. Chen, National University of Defense Technology, China
10. Sep 18 14:00 14:30 7.2.3 AEROELASTIC ANALYSIS OF INSECT-LIKE FLAPPING WING USING MODIFIED IMPLICIT COUPLING METHOD
N. Lee, Inha University, South Korea
Reserve Paper 7.2.R SYSTEMATIC INVESTIGATION OF PROPELLERS UNDER INHOMOGENEOUS INFLOW
M. Cerny, Technical University Munich, Germany
8.2Acustics and Vibrations 2
Chair(s): Nitzsche, F.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
10. Sep 18 13:00 13:30 8.2.1 THE DIMENSIONING OF A NONLINEAR ENERGY SINK APPLIED TO A HELICOPTER THROUGH NONLINEAR NORMAL MODES
L. V. D. Sousa, Federal University of UberlÔndia, Brazil
10. Sep 18 13:30 14:00 8.2.2 CLOSED-LOOP CONTROL OF THE SMART SPRING ľ EFFECT OF THE CONTROL ALGORITHM ON THE DYNAMIC RESPONSE OF PERIODIC SYSTEMS
F. Nitzsche, Carleton University, Canada
10. Sep 18 14:00 14:30 8.2.3 INVESTIGATION ON HIGH-FREQUENCY MODAL TEST AND ANALYSIS FOR TURING BLADE
G-X Gao Xiang╣, Y-Q YAN QUN╣, H-WC HUANG Wenchao╣, YG YAO Gang╣; ╣ASRI, China
9.2Combustion
Chair(s): Stezycki, P.
Track 9
05 - Propulsion
10. Sep 18 13:00 13:30 9.2.1 PRECISE MEASUREMENT OF PROPAGATING FLAME IN 2-STROKE GASOLINE ENGINE BY MULTIPLE ION-PROBES
T. Yatsufusa, Hiroshima Institute of Technology, Japan
10. Sep 18 13:30 14:00 9.2.2 ON THE EXISTENCE OF MULTIPLE SELF-EXCITATION FREQUENCIES IN THE INSTABILITY OF INTERACTING PLANAR MIXING LAYER AND WAKE
H.R. De Aguiar Quintanilha Junior, United Kingdom
10. Sep 18 14:00 14:30 9.2.3 ENGINE TEST RESULTS OF FUEL-WATER MICROEMULSION
MK Kowalski, AFIT, Poland
Reserve Paper 9.2.R OPTIMIZATION OF THE FUEL INJECTOR TO AN INTERNAL COMBUSTION ENGINE BY MEANS OF LASER EQUIPMENT
MK Kowalski, AFIT, Poland
10.2Flight Handling Quality
Chair(s): Che, J.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
10. Sep 18 13:00 13:30 10.2.1 BEYOND BEDFORD; DEVELOPMENT OF A TWO-DIMENSIONAL PILOT WORKLOAD RATING SCALE
R Ridgway, QinetiQ, United Kingdom
10. Sep 18 13:30 14:00 10.2.2 INFLUENCE OF BIODYNAMIC FEEDTHROUGH ON HANDLING QUALITIES ANALYSIS
D. D. Drewiacki, Instituto Tecnolˇgico de Aeronßutica, Brazil
10. Sep 18 14:00 14:30 10.2.3 HANDLING QUALITIES OF ONERA\'S SMALL BUSINESS CONCEPT PLANE WITH DISTRIBUTED ELECTRIC PROPULSION
C. DOELL, ONERA, France
Reserve Paper 10.2.R STUDY OF FLYING QUALITY EVALUATION ON ELECTRIC POWERED LIGHT AIRCRAFT
S-.M Mochida, Hosei University, Japan
11.2UAS Trajectory
Chair(s): Sibilski, K.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
10. Sep 18 13:00 13:30 11.2.1 PERFORMANCE ANALYSIS OF UAV PERSISTENT SURVEILLANCE ALGORITHM
S. Lee╣, Y. Kim╣; ╣Seoul National University, South Korea
10. Sep 18 13:30 14:00 11.2.2 PLANNING AND CONTROL STRATEGIES FOR COLLABORATIVE AERIAL AND MARITIME AUTONOMOUS VEHICLES
G. Guglieri, Politecnico di Torino, Italy
10. Sep 18 14:00 14:30 11.2.3 AN EVALUATION OF VARIOUS GEOFENCE CONFLICT RESOLUTION ALGORITHMS AND THEIR IMPACT ON MISSION PERFORMANCE
. Balachandran, National Institute of Aerospace, United States
12.2Air Transportation Network
Chair(s): Zhang, X., Kuegler, D.
Track 12
09 - Air Transport System Efficiency
10. Sep 18 13:00 13:30 12.2.1 A SIMULATION MODELING STUDY FOR FREE ROUTING AIRSPACE IN JAPAN
K.K. Kageyama, ENRI, Japan
10. Sep 18 13:30 14:00 12.2.2 TACTICAL FLOW-CENTRIC GENERATION OF OPTIMIZED SECTOR CONFIGURATIONS ľ METHODOLOGY REPORT OF THE SESAR PJ8.1.5 EXERCIS
A. JOULIA, Onera - The French Aerospace Lab, France
10. Sep 18 14:00 14:30 12.2.3 EVALUATION OF THE POTENTIAL IMPACTS OF HYBRID-ELECTRIC AIRCRAFT ON THE GLOBAL AIR TRANSPORTATION NETWORK SYSTEM
G. Tay, Institute of Aircraft Design, Germany
Reserve Paper 12.2.R STUDY ON THE LARGE-AREA FLIGHT DELAY RECOVERY
JH.-W. Wang, Civil Aviation University of China, China

14:30 - 15:00Break

1.3Novel Application of MDO in Aircraft Design 3
Chair(s): Lefebvre, T.
Track 1
01 - Aircraft Design and Integrated Systems
10. Sep 18 15:00 15:30 1.3.1 INTERGRATED SYSTEM FOR UNIFICATION OF AIRCRAFT CONCEPTUAL DESIGN APPLICATIONS.
E. Vogiatzis╣, R. -C. Munjulury╣, P. Krus╣; ╣Link÷pings university, Sweden
10. Sep 18 15:30 16:00 1.3.2 STRUCTURAL DESIGN AND TESTING OF A TAILORED SKIN SINGLE DUCT (TSSD) FIN APPLICATION
M. Schneider, German Aerospce Center (DLR), Germany
10. Sep 18 16:00 16:30 1.3.3 AIRCRAFT OPTIMIZATION AT THE EARLY STAGES OF DESIGN WITH A HYBRID TECHNIQUE
N Cavus, German Aerospace Center, Germany
Reserve Paper 1.3.R STUDIES ON THE APPLICATION OF MOEA/D TO AERODYNAMIC OPTIMIZATION DESIGN
X.Q. Zhu╣, Z.H Gao╣, Z.W. Chen╣; ╣Northwestern Polytechnical University, China
2.3Supersonic and Hypersonic Vehicles
Chair(s): Goraj, Z.
Track 2
01 - Aircraft Design and Integrated Systems
10. Sep 18 15:00 15:30 2.3.1 NEURAL NETWORK DRIVEN ADJOINT SOLVER BETWEEN FLIGHT-PATH OPTIMIZATION AND PANEL METHOD FOR AIRCRAFT DESIGN
Morita Naoto, the University of Tokyo, Japan
10. Sep 18 15:30 16:00 2.3.2 RDTE AND PRODUCTION COSTS ESTIMANTION RELATIONSHIPS FOR THE CONCEPTUAL DESIGN OF HYPERSONIC TRANSPORTATION SYSTEMS
R. Fusaro, Politecnico di Torino, Italy
10. Sep 18 16:00 16:30 2.3.3 ANALYSIS OF THE INFLUENCE OF THE EXTERNAL CONFIGURATION ON THE WAVE DRAG OF SUPERSONIC BUSINESS JETS
A.M.A Abdalla, SŃo Carlos School of Engineering - University of SŃo Paulo (USP), Brazil
Reserve Paper 2.3.R AN EFFICIENT FRAMEWORK FOR AERODYNAMIC CONFIGURATION EVOLUTION OF REENTRY VEHICELES
Seyed Mahmoodzadeh Entezari, Aerospace Research Institute, Iran
3.3Additive Manufacturing
Chair(s): Sander, P.
Track 3
08 - Manufacturing and Supply Chain Management
10. Sep 18 15:00 15:30 3.3.1 AIRCRAFT STRCTURE TECHNOLONY OF ADDITIVE MANUFACTURING
Xiangming Wang╣, Hao Cui╣, Ping Xu╣, Shiquan Bi╣; ╣Shenyang Aircraft Design and Resesarch Institute, China
10. Sep 18 15:30 16:00 3.3.2 INVESTIGATION OF CRACK PROPAGATION PROPERTIES OF ADDITIVE MANUFACTURING PRODUCTS
-- Abramovich, Technion, I.I.T.,, Israel
10. Sep 18 16:00 16:30 3.3.3 EVALUATION OF MECHANICAL PROPERTIES OF TI6AL4V FABRICATED BY SELECTIVE LASER MELTING (SLM)
C MingQiang, China
4.3Numerical Methods
Chair(s): Tobaldini Neto, L., Greco Junior, P.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
10. Sep 18 15:00 15:30 4.3.1 A FINITE ELEMENT MODEL FOR AERODYNAMICS ANALYSIS OF LOW-REYNOLDS NUMBER ROTORS
A. Kolaei, Ryerson University, Canada
10. Sep 18 15:30 16:00 4.3.2 EFFECTS OF NUMERICAL MODELING CHOICES FOR JETS IN CROSSFLOW
D. Abreu, EMBRAER, Brazil
10. Sep 18 16:00 16:30 4.3.3 VISCOUS FLUID SIMULATION WITH THE VORTEX ELEMENT METHOD
O.S. Kotsur, Bauman Moscow State Technical University, Russia
Reserve Paper 4.3.R VALIDATION OF A DISCONTINUOUS GALERKIN BASED DES SOLVER IN FLOW PROBLEMS USING HIGH PERFORMANCE COMPUTING
A.V. Wolkov, TsAGI, Russia
5.3Student Hands On Activities
Chair(s): Suzuki, S.
Track 5
14 - ECSC
10. Sep 18 15:00 15:30 5.3.1 ALL JAPAN STUDENT\'S INDOOR FLYING ROBOT CONTEST
T. Tsuchiya, The University of Tokyo, Japan
10. Sep 18 15:30 16:00 5.3.2 THE AERONAUTICAL SOCIETY OF SOUTH AFRICA AEROSPACE CHALLENGE
JS Monk, CSIR, South Africa
10. Sep 18 16:00 16:30 5.3.3 SAE BRASIL STUDENT PROGRAMS - A SUCCESS STORY
H Forjaz, SAE BRASIL, Brazil
6.3New Structural Design 1: General
Chair(s): Ikeda, T.
Track 6
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
10. Sep 18 15:00 15:30 6.3.1 A PASSIVE-ADAPTIVE WING FOR DRAG REDUCTION
C. B. York, University of Glasgow, United Kingdom
10. Sep 18 15:30 16:00 6.3.2 INVESTIGATION OF INFLUENCE OF SYNERGETIC EFFECT ON STRENGTH AND WEIGHT OF PRIMARY FRAME AIRCRAFT STRUCTURES
A.N. Shanygin, Central Aerohydrodynamic Institute, Russia
10. Sep 18 16:00 16:30 6.3.3 A NUMERICAL AND EXPERIMENTAL ANALYSIS OF THE DYNAMICS OF A TENSEGRITY-MEMBRANE STRUCTURE
L. H. Teixeira, UNICAMP, Brazil
Reserve Paper 6.3.R AN XFEM FRAMEWORK FOR ONSET AND CRACK PROPAGATION FOR COMPOSITES BASED ON ACTION PLANE THEORY
M. V. Angelo╣, M. L. Ribeiro╣, V. Tita╣; ╣University of Sao Paulo, Brazil
7.3Store Separation
Chair(s): Cenko, A.
Track 7
03.4 - Applied Aerodynamics
10. Sep 18 15:00 15:30 7.3.1 EXHAUST PLUME EFFECT OF WINGED TWO-STAGE-TO-ORBIT SEPARATION AT ASCENT USING AERODYNAMIC-FLIGHT DYNAMICS TECHNIQUE
H.-I. Iwafuji, Tokyo Metropolitan University, Japan
10. Sep 18 15:30 16:00 7.3.2 NUMERICAL SIMULATION OF THE AERIAL DROP OF WATER FOR FIXED-WING AIRCRAFT IN FIREFIGHTING
X ZHAO╣, P zhou╣, X YAN, No. 38 Research Institute of CETC, China; Y WENG, Xiĺan Jiaotong University, China; X-L YANG, Chinese Flight Test Establishment, China; ╣Northwestern Polytechnical University, China
10. Sep 18 16:00 16:30 7.3.3 GRID-MODE TRANSONIC STORE SEPARATION ANALYSES USING MODERN DESIGN OF EXPERIMENTS
K.A. Jamison, Council of Scientific and Industrial Research, South Africa
Reserve Paper 7.3.R STORE SEPARATION TRAJECTORY PREDICTIONS AT LOW SPEEDS
Alex Cenko, AIWS LLC, United States
8.3Loads
Chair(s): Conway, S.R.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
10. Sep 18 15:00 15:30 8.3.1 VALIDATION OF A HYBRID OBSERVER METHOD FOR FLIGHT LOADS ESTIMATION
M. Montel, Hamburg University of Technology, Germany
10. Sep 18 15:30 16:00 8.3.2 STATIC LOADS EVALUATION IN A FLEXIBLE AIRCRAFT USING HIGH FIDELITY FLUID-STRUCTURE ITERATION TOOL (E2-FSI)
A. A. VERRI, EMBRAER S/A, Brazil
10. Sep 18 16:00 16:30 8.3.3 LOCAL MODEL NETWORKS APPLIED TO FLIGHT LOADS ESTIMATION
M. Halle, Hamburg University of Technology, Germany
9.3Turbine Aerodynamics
Chair(s): Yimer, I., Benzakein, M.
Track 9
05 - Propulsion
10. Sep 18 15:00 15:30 9.3.1 LOW-COST CERAMIC JET TURBINE
C.O. Oliveira, UFMG - ALFALAB, Brazil
10. Sep 18 15:30 16:00 9.3.2 THE INFLUENCE OF THE SHAPE OF THE COOLING CHANNEL AND PRESSURE GRADIENT ON THE EFFICIENCY OF FILM COOLING OF GTE BLADES
S. V. Belov╣, G. B. Zhestkov╣, D. V. Muravsky╣, S. V. Kharkovsky╣, E. V. Shcherbakova╣; ╣CIAM, Russia
10. Sep 18 16:00 16:30 9.3.3 PERFORMANCES OF LPT AND LINEAR CASCADES AT LOW REYNOLDS NUMBERS
A.D. Nepomnyashchiy╣, I.V. Tsvetkov╣, S.V. Suntsov╣, S.Y. Danilkin╣; ╣CIAM, Russia
Reserve Paper 9.3.R RESEARCH OF FLOW IN STAGE OF TURBINE AND OPTIMAL MODES OF MICRO GAS TURBINE POWER PLANT
A. Kartashev, Federal State Autonomous Educational Institution of Higher Educa, Russia
10.3Hydraulic Actuation
Chair(s): Fu, Y.
Track 10
07 - Systems, Subsystems and Equipment
10. Sep 18 15:00 15:30 10.3.1 A HYBRID DIGITAL-PROPORTIONAL HYDRAULIC ACTUATION SYSTEM FOR AIRCRAFT FLIGHT CONTROL
A Dell'Amico, Saab AB, Sweden
10. Sep 18 15:30 16:00 10.3.2 SELF INDUCED FAILURE OF A SERVO VALVE
T. seung, DLR, Germany
10. Sep 18 16:00 16:30 10.3.3 NUMERICAL AND EXPERIMENTAL STUDY OF A TWO DEGREES OF FREEDOM ELECTROHYDRAULIC MANIPULATOR
W. Cardozo, PUC-Rio, Brazil
11.3UAS VTOL
Chair(s): Bil, C., Alvarez, O.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
10. Sep 18 15:00 15:30 11.3.1 FLIGHT DYNAMICS MODELING AND TRIM CURVES OF A CONCEPTUAL SEMI-TANDEM WING VTOL UAV
A.C. Daud Filho, University of SŃo Paulo, Brazil
10. Sep 18 15:30 16:00 11.3.2 SCALABLE DESIGN APPROACH TO ANALYZE FLIGHT MECHANICAL PERFORMANCE FOR TILTWING UAVS
M Schuett, Institute of Flight System Dynamics, RWTH Aachen University, Germany
10. Sep 18 16:00 16:30 11.3.3 POTENTIAL BENEFITS ASSESSMENT ON HOME DELIVERY SERVICE USING MULTIPLE DRONES
Hiroki Omagari, Department of Aeronautics and Astronautics, Kyushu University, Japan
Reserve Paper 11.3.R MODELLING AND CONTROL OF A BI-TILT-ROTOR UAV WITH DOUBLE GIMBAL AND CAMERA FOR SURVEILLANCE SYSTEMS APPLICATION
J.C. Vendrichoski╣, T.L. Costa╣, E.S. El┤Youssef╣, E.R. de Pieri╣; ╣UFSC, Brazil
12.3On Demand Mobility: Integration in Civil Airpace
Chair(s): Kageyama, K.
Track 12
09 - Air Transport System Efficiency
10. Sep 18 15:00 15:30 12.3.1 SHAPING 4D SAFETY VOLUMES FOR UTM IN DENSE AREA
A. JOULIA, Onera - The French Aerospace Lab, France
10. Sep 18 15:30 16:00 12.3.2 A PROPOSAL OF DRONE SURVEILLANCE AND MANAGEMENT CONCEPT
K. Shiomi, Fukui Health Science University, Japan
10. Sep 18 16:00 16:30 12.3.3 SENSITIVITY ANALYSIS OF KEY PERSONAL AIR VEHICLE PROPERTIES IMPACTING URBAN TRANSPORT PERFORMANCE
R.L. Rothfeld, Bauhaus Luftfahrt e.V., Germany
Reserve Paper 12.3.R COST EFFECTIVE AND RELIABLE AIR TAXI OPERATIONS IN AUSTRALIA
C Bil, RMIT University, Australia

0.2General Lecture I - Technology Leadership Forum - Intelligent and Autonomous Engineering in Aeronautics - Dr. P.Nielsen, Dr. M.Evans, Dr. B.Yutko, Mr. Y.Nakagawa, FAA speaker
Chair: S. Suzuki Chair ICAS Programme Committee
10. Sep 18 16:35 18:35