30th 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, 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 Pereira, Embraer - 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 STREAMLINING CROSS-ORGANIZATIONAL AIRCRAFT DEVELOPMENT PROCESSES: AN OVERVIEW OF THE AGILE PROJECT
P.D. Ciampa¹, B. Nagel¹; ¹DLR, Germany
10. Sep 18 11:00 11:30 1.1.2 MULTIDISCIPLINARY DESIGN ANALYSIS OF BLENDED WING BODY THROUGH COLLABORATIVE DESIGN APPROACH: AGILE EU PROJECT
P.S. Prakasha¹, P.D. Ciampa¹, P. Della Vecchia ², D. Ciliberti ², M. Voskuijl , TU Delft, Netherlands; D. Charbonnier³, A. Jungo³, M. Fioriti, Politecnico di Torino, Italy; K. Anisimov, TsAGI, Russia; A. Mirzoyan, CIAM, Russia; ¹German Aerospace Center DLR, Germany ;²University of Naples, Italy ;³CFSE, Switzerland
10. Sep 18 11:30 12:00 1.1.3 AERO-STRUCTURAL OPTIMIZATION OF A MALE CONFIGURATION IN THE AGILE MDO FRAMEWORK
R. Maierl¹, A.A. Gastaldi¹, F. Daoud¹, J.N. Walther², P.D. Ciampa², A. Jungo, CFSE, Switzerland; M. Zhang, AIRINNOVA, Sweden; ¹Airbus DS, Germany ;²DLR, 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 OPTIMIZATION OF UNMANNED AIRCRAFT IN A SYSTEM OF SYSTEMS CONTEXT
A. Papageorgiou¹, K. Amadori², C. Jouannet², J. Ölvander¹; ¹Linköping University, Sweden ;²SAAB Aeronautics, 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. Kim¹, D. Lim¹, K. Yee¹; ¹Seoul 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
P. Stahl¹, T. Seren¹, C. Rößler¹, M. Hornung¹; ¹Technical 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 A HOLISTIC ENGINEERING APPROACH FOR AERONAUTICAL PRODUCT DEVELOPMENT
I. Staack, Linköping University, Sweden; K. Amadori¹, C. Jouannet¹; ¹Saab Aeronautics, Sweden
10. Sep 18 11:00 11:30 3.1.2 CONTINUOUS MODELING IN AIRCRAFT TOP-LEVEL DEMONSTRATION
J. Zang¹, Q. Wang¹, J.-Q Zhu¹; ¹Aviation 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 SYSTEMS
D.N. Mavris¹, A. Sudol¹; ¹Georgia Institute of Technology, 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 INVISCID AND VISCOUS FLOW MODELING FOR FAST TRANSONIC FLUTTER CALCULATIONS
H. Güner¹, G. Dimitriadis¹, V.E. Terrapon¹; ¹University of Liège, Belgium
10. Sep 18 11:00 11:30 4.1.2 FEASIBILITY OF THE NAVIER-STOKES HARMONIC BALANCE METHOD FOR MODELLING AIRCRAFT UNSTEADY AERODYNAMICS
J. Drofelnik¹, A. Da Ronch¹, M.S. Campobasso, University of Lancaster, United Kingdom; ¹University of Southampton, United Kingdom
10. Sep 18 11:30 12:00 4.1.3 AERODYNAMIC AND AEROACOUSTIC INVESTIGATION OF SWIRL RECOVERY VANES FOR PROPELLER PROPULSION SYSTEMS
L.E. van den Ende¹, Q. Li¹, F. Avallone¹, D. Casalino¹, G. Eitelberg¹, L.L.M. Veldhuis¹; ¹Delft University of Technology, Netherlands
5.1Experiments in Flow Control
Chair(s): Manfriani, L.
Track 5
03.2 - Experimental Aerodynamics
10. Sep 18 10:30 11:00 5.1.1 EXPERIMENTAL INVESTIGATION OF WING LOAD CONTROL USING FLUIDIC DEVICES
A. Krzysiak, Institute of Aviation, Poland
10. Sep 18 11:00 11:30 5.1.2 LARGE EDDY SIMULATION OF A TRANSIENT SPOILER DEPLOYMENT IN A NACA0012 PROFILE IN SUBSONIC AND TRANSONIC SPEEDS
R. V. LINN, FEDERAL UNIVERSITY OF RIO GRANDE DO SUL (UFRGS), Brazil
10. Sep 18 11:30 12:00 5.1.3 DEVELOPMENT OF NONLINEAR INSTABILITY IN SUPERSONIC 3D FLOW NEAR A PLATE
I.I. Lipatov, TsAGI, Russia
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, JAXA, Japan
10. Sep 18 11:00 11:30 6.1.2 EXPERIMENTAL INVESTIGATION, MATHEMATICAL AND NUMERICAL SIMULATION OF AIRCRAFT ICING PHENOMENA
I.A. Amelyushkin, Russia; A.L. Stasenko, Russia; V.A. Zhbanov, Russia
10. Sep 18 11:30 12:00 6.1.3 IONIZATION AND DISSOCIATION EFFECTS ON HYPERSONIC BOUNDARY-LAYER STABILITY
F. Miró Miró¹, E.-S. Beyak², D. Mullen², F. Pinna¹, H.-L. Reed²; ¹von Kármán Institute for Fluid Dynamics, Belgium ;²Texas A&M University, United States
7.1Flow Control
Chair(s): Volkova, A.
Track 7
03.4 - Applied Aerodynamics
10. Sep 18 10:30 11:00 7.1.1 WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTING
V. Ciobaca¹, B. Stefes², A. de Bruin³, M. Bauer, NAVASTO GmbH, Germany; P. Schlösser, Airbus Defence and Space GmbH, Germany; A. de Blécourt³, N. Bier¹, J. Zhai, DNW-KKK, Germany; M. Meyer², J. Wild¹; ¹Deutsches Zentrum für Luft und Raumfahrt, DLR, Germany ;²Airbus Operations GmbH, Germany ;³NLR-Netherlands Aerospace Center, Netherlands
10. Sep 18 11:00 11:30 7.1.2 PASSIVE VENTILATION FLOW CONTROL FOR AIRCRAFT GUST LOAD ALLEVIATION
Y. Tani¹, S. Seki¹, S. Aso¹; ¹Kyushu University, Japan
10. Sep 18 11:30 12:00 7.1.3 INVESTIGATION ON THE POSSIBILITY OF FLOW CONTROL AROUND CAVITY USING 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 STRUCTURAL DAMPING EFFECTS ON THE ACOUSTIC SCATTERING BY ELASTIC PLATES
M.M. Nilton¹, A.V.G. Cavalieri¹, M.V. Donadon¹, W.R. Wolf, Universidade Estadual de Campinas, Brazil; ¹Instituto Tecnológico de Aeronáutica, 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. Ferreira¹, L.V. Donadon¹, P.H. Iscold¹; ¹UFMG, Brazil
9.1Compressor Aerodynamics
Chair(s): Pankov, S., Girgis, S.
Track 9
05 - Propulsion
10. Sep 18 10:30 11:00 9.1.1 MATCHING BETWEEN METAMODEL AND OPTIMIZATION TOOL APPLIED IN A MULTISTAGE AXIAL-FLOW COMPRESSOR AIMING DESIGN IMPROVEMENT
V. Monteiro¹, K. Iha¹, O.F.R. Silva¹, T. Ebel, Concepts Nrec, United States; ¹ITA, Brazil
10. Sep 18 11:00 11:30 9.1.2 NUMERICAL AND EXPERIMENTAL STUDY OF THE EFFECT OF CIRCUMFERENTIAL GROOVES ON HPC LAST STAGE PERFORMANCE
V.I. Mileshin¹, A.M. Petrovichev¹, S.I. Baeva¹, V.V. Zhdanov¹; ¹Central Institute of Aviation Motors, Russia
10. Sep 18 11:30 12:00 9.1.3 ADAPTIVE GTE SURGE PROTECTION SYSTEM WITH SELECTIVE CONTROL OF THE ACTUATORS
L.G. Bliznyukov¹, M.G. Kesselman¹, V.I. Chernyshov¹, S.A. Smetanin¹; ¹Central Institute of Aviation Motors, Russia
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 FAULT TOLERANT CONTROL SYSTEM OF AIRCRAFT BY FEEDBACK ERROR LEARNING WITH SYSTEM ESTIMATION
N. Yoshikawa, The university 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. Takase¹, J.O. Entzinger¹, S. Suzuki¹; ¹The University of Tokyo, Japan
10. Sep 18 11:30 12:00 10.1.3 DATA-DRIVEN FAILURE IDENTIFICATION USING A MOTION-BASED SIMULATOR
A.D. Kraemer¹, E. Villani¹; ¹Instituto Tecnológico de Aeronáutica (ITA), Brazil
11.1UAS Control 1
Chair(s): Bidinotto, J.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
10. Sep 18 10:30 11:00 11.1.1 COMPARATIVE ANALYSIS OF METHODS USED TO ACTIVE CONTROL OF MICRO AERIAL VEHICLE
K.-S Sibilski, Warsaw University of Technology, Poland
10. Sep 18 11:00 11:30 11.1.2 ROBUST TRAJECTORY OPTIMIZATION OF VTOL TRANSITION MANEUVER USING BI-LEVEL OPTIMAL CONTROL
P. Piprek¹, F. Holzapfel¹; ¹Technical University of Munich, Germany
10. Sep 18 11:30 12:00 11.1.3 FIXED-WING UAV ROBUST GUIDANCE STRATEGY BASED ON COMPOUND FLIGHT MISSION OF ON-GROUND TARGETS
J.L. Gomes Olavo¹, L.A. Borges Tôrres¹, T. Argolo Jesus, CEFET/MG, Brazil; ¹UFMG, Brazil
12.1Safety Analysis
Chair(s): Conway, S., Ross, I.
Track 12
10 - Safety and Security
10. Sep 18 10:30 11:00 12.1.1 A METHOD FOR ESTIMATING THE PROBABILITY OF RARE ACCIDENTS IN COMPLEX SYSTEMS
I. Romani de Oliveira¹, J.D. Musiak¹, G.C. Balvedi¹; ¹Boeing Research & Technology, Brazil
10. Sep 18 11:00 11:30 12.1.2 PROBABILISTIC FORECASTING IN AIRCRAFT EMERGENCY EVACUATION SIMULATION
D.B. Ferrari¹, R. Giarola¹, L.C.de C. Santos, EMBRAER, Brazil; ¹Instituto Tecnológico de Aeronáutica, Brazil
10. Sep 18 11:30 12:00 12.1.3 STUDY ON AIRCRAFT EVACUATION MODELING AND MODEL PARAMETERS BASED ON SOCIAL FORCE
K. Chen¹, Y. Wu¹, T. Zou¹; ¹Laboratory of Civil Aircraft Airworthiness Technology, CAUC, China

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
F. Torrigiani¹, J. Bussemaker¹, P.D. Ciampa¹, M. Fioriti², F. Tomasella², B. Aigner, RWTH Aachen, Germany; D. Rajpal, Delft University of Technology, Netherlands; H. Timmermans, Netherlands Aerospace Center (NLR), Netherlands; A. Savelyev, Central Aerohydrodynamic Institute (TsAGI), Russia; D. Charbonnier, CFS Engineering, Switzerland; ¹German Aerospace Center, DLR, Germany ;²Politecnico di Torino, Italy
10. Sep 18 13:30 14:00 1.2.2 MDO APPLICATIONS TO CONVENTIONAL AND NOVEL TURBOPROP AIRCRAFT WITHIN AGILE EUROPEAN PROJECT
L. Stingo¹, P. Della Vecchia¹, G. Cerino, Leonardo Company, Italy; F. Nicolosi¹, A. De Marco¹; ¹University of Naples, 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; H. Timmermans¹, F. Torrigiani, German Aerospace Center, Germany; W.F. Lammen¹; ¹Netherlands Aerospace Centre, 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. Geuther¹, F. Capristan¹, J. Kirk, Georgia Institute of Technology, United States; R. Erhard, University of Denver, United States; ¹NASA Langley Research Center, United States
10. Sep 18 13:30 14:00 2.2.2 LIFECYCLE COSTS AND FEASIBILITY ANALYSIS OF THE DESIGNS OF UAV\'S FOR HUMANITARIAN RELIEF MISSIONS
O. Hektor¹, T. Melin¹; ¹Swedish 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
A.C.B. Ramos¹, M.S. Santiago¹, E.H. Shiguemori, IEAV, Brazil; S. Serokhvostov, MIPT, Russia; P.K. Gupta, JUIT, India; L. Zhong, CAUC, China; ¹UNIFEI, Brazil
Reserve Paper 2.2.R DESIGN AND OPTIMIZATION OF A VERSATILE UAV FOR OBSERVATION AND RESEARCH USING THERMAL COLUMNS FOR EXTENDED ENDURANCE
U. Golyska¹, M. Nowowiejski¹, P. Pacuszka¹; ¹Warsaw University of Technology, Poland
Reserve Paper 2.2.R UAV INITIAL PARAMETER ESTIMATION
G.G. Silva¹, L.C. Carmona¹, E. Bauzer Medeiros¹; ¹UFMG, 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
A.S.J. van Heerden¹, M.D. Guenov¹, A. Molina-Cristóbal¹, A. Riaz¹, Y. Bile¹; ¹Cranfield 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 ROBUST DESIGN OPTIMIZATION OF BENCHMARK AERODYNAMIC CASE BASED ON POLYNOMIAL CHAOS EXPANSION
Z. Huan¹, G. Zhenghong¹; ¹Northwestern Polytechnical University , China
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
T.P. Monteiro¹, K. Ramesh, Glasgow University, United Kingdom; F. Silvestre¹; ¹Instituto Tecnologico de Aeronautica, Brazil
10. Sep 18 13:30 14:00 4.2.2 NUMERICAL ANALYSIS OF THE FLOW AROUND A BACKWARD-FACING RAMP
P. Catalano¹, A. Mastellone¹, M. Invigorito¹, F. Capuano, Università di Napoli Federico II, Italy; ¹CIRA, Italy
10. Sep 18 14:00 14:30 4.2.3 RECTANGULAR CAVITY FLOWFIELD EFFECTS ON STORES IN THE SHEAR LAYER
A. Cenko, AIWS, United States; G. Akroyd, Akroyd Aeronautics, Australia
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 COAXIAL ROTOR IN HOVER
X. Zhao¹, N.-Z. Huang¹, X. Liang¹, P. Zhou¹, W.-P. Song¹, Y.-F. Lin, China Helicopter Research and Development Institute, China; ¹Northwestern Polytechnical University, China
10. Sep 18 13:30 14:00 5.2.2 ADAPTIVE WING HIGH-LIFT SYSTEM
A.V. Petrov¹, A.V. Potapchik¹, J.G. Stepanov¹, V.V. Gubskiy¹; ¹TsAGI, Russia
10. Sep 18 14:00 14:30 5.2.3 NUMERICAL INVESTIGATION AERODYNAMICS NACELLE-STRAKE EFFECT
J.J. Broekhuijsen¹, G. Vidjaja², J.W. van der Burg², H.W.M. Hoeijmakers¹; ¹University of Twente, Netherlands ;²Airbus Operations GMBH, Germany
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 ACOUSTIC MODES AND GLOBAL INSTABILITIES IN WAKES AND JETS
E. Martini, ITA, Brazil; A. Cavalieri, ITA, Brazil; P. Jordan, Universite de Poitiers, France
10. Sep 18 13:30 14:00 6.2.2 LONGITUDINAL VORTEXE FORMATION IN THE HYPERSONIC FLOW AROUND WINDWARD SIDE OF BLUNTED DELTA WING AND EFFECTS OF THEIR INTERACTION WITH BOUNDARY LAYER
V.I. Shalaev, MIPT, Russia; S.V. Alexandrov¹, A.V. Vaganov¹, M.A. Starodubtsev¹; ¹TsAGI, Russia
10. Sep 18 14:00 14:30 6.2.3 ON THE EXISTENCE OF MULTIPLE SELF-EXCITATION FREQUENCIES IN THE INSTABILITY OF INTERACTING PLANAR MIXING LAYER AND WAKE
H.R. De Aguiar Quintanilha Jr., University of Liverpool, United Kingdom; L. Santos de Brito Alves, Universidade Federal Fluminense, Brazil
7.2Unmanned Aircraft
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
10. Sep 18 13:00 13:30 7.2.1 NUMERICAL SIMULATION RESEARCH ON SMALL UAVS’ DEEP STALL LANDING PROCEDURE
B. Cheng¹, Z. Guo¹, P. Wang¹, Q.Y. Chen¹; ¹National University of Defense Technology, 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
L. Chen¹, Z. Guo¹, Z.X. Hou¹, W.-K. Wang¹, B.-J. Zhu¹; ¹National University of Defense Technology, China
10. Sep 18 14:00 14:30 7.2.3 NUMERICAL FLOW ANALYSIS OF A CORRUGATED DRAGONFLY AIRFOIL AT LOW REYNOLDS NUMBER REGION USING CARTESIAN-MESH CFD
Y Yamaguchi, Japan
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 CLOSED-LOOP CONTROL OF THE SMART SPRING – EFFECT OF THE CONTROL ALGORITHM ON THE DYNAMIC RESPONSE OF PERIODIC SYSTEMS
F. Nitzsche, Carleton University, Canada
10. Sep 18 13:30 14:00 8.2.2 HIGH FREQUENCY MODAL TEST AND DYNAMIC PERFORMANCE EVALUATION OF TURBINE ROTOR BLADES
J. Qin¹, X. Gao¹, W.C. Huang¹, G. Yao¹; ¹ASRI, China
10. Sep 18 14:00 14:30 8.2.3 HIGH PERFORMANCE PNEUMATIC SHOCK-ABSORBERS FOR AERONAUTICAL APPLICATIONS
R. Faraj, Institute of Fundamental Technological Research, Poland
9.2Combustion
Chair(s): Stezycki, P.
Track 9
05 - Propulsion
10. Sep 18 13:00 13:30 9.2.1 ENGINE TEST RESULTS OF FUEL-WATER MICROEMULSION
M. Kowalski¹, A. Jankowski¹; ¹AFIT, Poland
10. Sep 18 13:30 14:00 9.2.2 PRECISE MEASUREMENT OF PROPAGATING FLAME IN 2-STROKE GASOLINE ENGINE BY MULTIPLE ION-PROBES
Tomoaki Yatsufusa¹, Keigo Kii¹, Kentaro Takatani¹; ¹Hiroshima Institute of Technology, Japan
10. Sep 18 14:00 14:30 9.2.3 OPTIMIZATION OF THE FUEL INJECTOR TO AN INTERNAL COMBUSTION ENGINE BY MEANS OF LASER EQUIPMENT
M. Kowalski¹, A. Jankowski¹, R. Szczepanik, Polish Air Force Academy Deblin, Poland; ¹AFIT, 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
G.R. Ridgway¹, H.R. Shattock¹, A.C.R. Hare¹; ¹QinetiQ, United Kingdom
10. Sep 18 13:30 14:00 10.2.2 THE INFLUENCE OF BIODYNAMIC FEEDTHROUGH ON HANDLING QUALITIES
D. Drewiacki, Embraer, Brazil; F.J. Silvestre¹, A.B. Guimarães Neto¹; ¹Instituto Tecnológico de Aeronáutica, Brazil
10. Sep 18 14:00 14:30 10.2.3 HANDLING QUALITIES OF ONERA’S SMALL BUSINESS CONCEPT PLANE WITH DISTRIBUTED ELECTRIC PROPULSION
E. Dillinger, ISAE-SUPAERO/ONERA, France; C. Döll¹, R. Liaboeuf¹, C. Toussaint¹, J. Hermetz¹, C. Verbeke¹, M. Ridel¹; ¹ONERA, France
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. Lee¹, Y. Kim¹; ¹Seoul National University, South Korea
10. Sep 18 13:30 14:00 11.2.2 AN EVALUATION OF VARIOUS GEOFENCE CONFLICT RESOLUTION ALGORITHMS AND THEIR IMPACT ON MISSION PERFORMANCE
S Balachandran, National Institute of Aerospace, United States; A Narkawicz¹, C Munoz¹, M Consiglio¹; ¹NASA Langley Research Center, United States
10. Sep 18 14:00 14:30 11.2.3 TOWARDS IMPLEMENTATION OF A FORMATION FLYING FOR EFFICIENT OPERATIONS
K.-S. Sibilski, Air Force Institute of Technology, Poland
12.2Cyber Security
Chair(s): ,
Track 12
10 - Safety and Security
10. Sep 18 13:00 13:30 12.2.1 IMPACT STUDY ON CYBER THREATS TO GNSS AND FMS SYSTEMS
R. Geister¹, J.-P. Buch¹, D. Niedermeier¹, G. Gamba², L. Canzian², O. Pozzobon²; ¹German Aerospace Center, Germany ;²Qascom S.r.l., Italy

14:30 - 15:00Break

1.3Alternative Energy and Distributed Propulsion Aircraft
Chair(s): Isikveren, A.
Track 1
01 - Aircraft Design and Integrated Systems
10. Sep 18 15:00 15:30 1.3.1 INTEGRATED TURBO-ELECTRIC MOTIVE POWER SYSTEMS FOR REGIONAL TRANSPORT APPLICATIONS
A.T. Isikveren, SAFRAN S.A., France
10. Sep 18 15:30 16:00 1.3.2 DEVELOPING THE UNMANNED UNCONVENTIONAL CARGO AIRPLANES WITH HYBRID PROPULSION SYSTEM
I. Gál¹, D. Rohács¹, J. Rohács¹; ¹Budapest University of Technology and Economics, Hungary
10. Sep 18 16:00 16:30 1.3.3 OPTIMIZATION OF MOTOR FOR THE MAXIMIZATION OF SOLAR-POWERED AIRCRAFT PERFORMANCE
S. Serokhvostov, MIPT, Russia; T. Churkina, MAI, Russia
2.3Personal Air Mobility
Chair(s): Melkert, J.
Track 2
01 - Aircraft Design and Integrated Systems
10. Sep 18 15:00 15:30 2.3.1 SMALL AIRCRAFT CONCEPT FOR REGIONAL ON-DEMAND AIR MOBILITY
E. Stumpf¹, M. Kreimeier¹, P. Strathoff¹, J. Lückhof¹, K.-U. Schröder, RWTH Aachen University, Institute of Structural Mechanics and Li, Germany; F. Janser, University of Applied Sciences Aachen, Aerodynamics Group, Germany; ¹RWTH Aachen University, Institute of Aerospace Systems, Germany
10. Sep 18 15:30 16:00 2.3.2 INVESTIGATION OF ‘JUMP TAKEOFF’ POSSIBILITY FOR THE NEW CONCEPT OF MODERN AUTOGYRO
R. Zurawski¹, D. Ulma¹; ¹Institute of Aviation, Poland
3.3Additive Manufacturing
Chair(s): Zhou, X.
Track 3
08 - Manufacturing and Supply Chain Management
10. Sep 18 15:00 15:30 3.3.1 AIRCRAFT STRUCTURE TECHNOLOGY OF ADDITIVE MANUFACTURING
X. Wang¹, H. Cui¹, P. Xu¹, S. Bi¹; ¹Shenyang 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
H. Abramovich¹, N. Broitman¹, A. Shirizly¹; ¹Technion, I.I.T., Israel
10. Sep 18 16:00 16:30 3.3.3 EVALUATION OF MECHANICAL PROPERTIES OF TI-6AL-4V FABRICATED BY SELECTIVE LASER MELTING (SLM)
M.Q. Chu¹, X.W. Zhou¹, X.F. Sun¹, L. Wang¹; ¹COMAC, 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 EFFECTS OF NUMERICAL MODELING CHOICES FOR HEATED JETS IN CROSS FLOW
K.C. Morais¹, D.F. Abreu¹, R. Papa¹, L. Tobaldini Neto¹, L.C.C. Santos¹; ¹EMBRAER S. A., Brazil
10. Sep 18 15:30 16:00 4.3.2 VISCOUS FLUID SIMULATION WITH THE VORTEX ELEMENT METHOD
O.S. Kotsur¹, G.A. Shcheglov¹; ¹Bauman Moscow State Technical University, Russia
10. Sep 18 16:00 16:30 4.3.3 EFFECTS OF NUMERICAL AND GEOMETRICAL ASPECTS IN VERTICAL-HORIZONTAL TAIL JUNCTION SIMULATIONS WITH TRANSONIC SEPARATION
M. R. N. Lopez, Embraer S.A., Brazil
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
J.S. Monk, CSIR, South Africa
10. Sep 18 16:00 16:30 5.3.3 SAE BRASIL AEROSPACE PROGRAMS – A SUCCESS STORY
H.A. Forjaz, SAEBRASIL, Brazil
6.3Loads
Chair(s): Conway, S.R.
Track 6
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
10. Sep 18 15:00 15:30 6.3.1 VALIDATION OF A HYBRID OBSERVER METHOD FOR FLIGHT LOADS ESTIMATION
M. Montel¹, F. Thielecke¹; ¹Hamburg University of Technology, Germany
10. Sep 18 15:30 16:00 6.3.2 STATIC LOADS EVALUATION IN A FLEXIBLE AIRCRAFT USING HIGH FIDELITY FLUID-STRUCTURE ITERATION TOOL (E2-FSI)
A.A. Verri¹, K.C. Morais¹, F.L.S. Bussamra, ITA, Brazil; G.G. Becker¹, C.E.S. Cesnik, UniMich, United States; ¹Embraer S/A, Brazil
10. Sep 18 16:00 16:30 6.3.3 LOCAL MODEL NETWORKS APPLIED TO FLIGHT LOADS ESTIMATION
M. Halle¹, F. Thielecke¹; ¹Hamburg University of Technology, Germany
7.3Wing Optimisation
Chair(s): Collier, F.
Track 7
03.4 - Applied Aerodynamics
10. Sep 18 15:00 15:30 7.3.1 THE STUDIES ON LOW-NOISE LAMINAR WING REGIONAL AIRCRAFT
N.A. Pushchin, TsAGI, Russia
10. Sep 18 15:30 16:00 7.3.2 OPTIMIZATION DESIGN OF ADAPTIVE WING COUPLED AERODYNAMIC AND STRUCTURAL CONSTRAINTS
J Guan, China Aerodynamic Research and Development Center , China
10. Sep 18 16:00 16:30 7.3.3 WING TWIST OPTIMISATION USING AERODYNAMIC SOLVERS OF DIFFERENT FIDELITY
G. Yang¹, A. Da Ronch¹, D. Kharlamov¹, J. Drofelnik¹; ¹University of Southampton, United Kingdom
8.3Aeroelasticity 1 : Fixed-wing Aircraft
Chair(s): Chizhov, A.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
10. Sep 18 15:00 15:30 8.3.1 MODELLING OF FLUTTER CHARACTERISTICS OF AIRCRAFT WING WITH PYLON-MOUNTED ENGINE NACELLE
Q. Yu¹, S. Lee¹, M. Damodaran¹, B.C. Khoo¹; ¹National University of Singapore, Singapore
10. Sep 18 15:30 16:00 8.3.2 AEROELASTIC PROPERTIES OF ACTIVE WINGLETS
G.A. Amiryants¹, S.E. Paryshev¹, A.V. Grigoriev¹; ¹TsAGI, Russia
10. Sep 18 16:00 16:30 8.3.3 FLUTTER ANALYSIS OF TWIN TURBOPROP AIRCRAFT WITH TIP-TANKS
J. Cecrdle¹, O. Vich¹; ¹Aeronautical Research and Test Institute (VZLU) , Czech Republic
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. Belov¹, G.B. Zhestkov¹, D.V. Muravsky¹, S.V. Kharkovsky¹, E.V. Shcherbakova¹; ¹CIAM, Russia
10. Sep 18 16:00 16:30 9.3.3 PERFORMANCES OF LPT AND LINEAR CASCADES AT LOW REYNOLDS NUMBERS
A.D. Nepomnyashchiy¹, I.V. Tsvetkov¹, S.V. Suntsov¹, S.Y. Danilkin¹; ¹CIAM, 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’Amico¹, D. Simon¹, S. Ward¹, L.P.G. Pinto², B. Lantto¹, V. De Negri², P. Krus, Linköping University, Sweden; ¹Saab AB, Sweden ;²Federal University of Santa Catarina, Brazil
10. Sep 18 15:30 16:00 10.3.2 SELF-INDUCED FAULT OF A HYDRAULIC SERVO VALVE
T. Seung, Program Management Office Aeronautics Research / DLR del. iABG, Germany
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 Filho¹, E.M. Belo¹; ¹EESC-USP, Brazil
10. Sep 18 15:30 16:00 11.3.2 SCALABLE DESIGN APPROACH TO ANALYZE FLIGHT MECHANICAL PERFORMANCE OF TILT-WING UAVS
M. Schütt¹, T. Islam¹, P. Hartmann¹, D. Moormann¹; ¹Institute 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
H. 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. Vendrichoski¹, T.L. Costa¹, E.S. El´Youssef¹, E.R. de Pieri¹; ¹UFSC, Brazil
12.3UAS - Unmanned Aircraft Systems
Chair(s): Lief, A.
Track 12
10 - Safety and Security
10. Sep 18 15:00 15:30 12.3.1 HUMAN-MACHINE INTERFACES AND INTERACTIONS FOR MULTI UAS OPERATIONS
Y. Lim¹, K. Ranasinghe¹, A. Gardi¹, N. Ezer, Northrop Grumman Corporation, United States; R. Sabatini¹; ¹RMIT University, Australia
10. Sep 18 15:30 16:00 12.3.2 LOW LEVEL TRAFFIC MONITORING: RPAS CONCEPT OF OPERATION AND DEVELOPEMENT OF A GROUND BASED SYSTEM
P. Le Blaye¹, C. Le Tallec¹; ¹ONERA - The French aerospace lab, France
10. Sep 18 16:00 16:30 12.3.3 HUMAN FACTOR IN UNMANNED AIRCRAFT SYSTEM FLIGHT TEST
F. Wang¹, S.-J. Qi¹, X.-L. Wu¹; ¹Chinese Flight Test Establishment, China

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, Mr. Vargas Rainho
Chair: S. Suzuki Chair ICAS Programme Committee
10. Sep 18 16:35 18:35

Tuesday, 11. Sep 2018


7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
0.3General Lecture II - Autonomy and the future of Aerospace - N. Pendleton, Boeing, USA
Chair:
11. Sep 18 08:00 09:00

0.4Interactive Presentations
Chair: Artur Mirzoyan
11. Sep 18 09:00 10:00

1.4Unconventional Concepts 1
Chair(s): Kimmel, B.
Track 1
01 - Aircraft Design and Integrated Systems
11. Sep 18 10:00 10:30 1.4.1 CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATION
A. Seitz¹, F. Peter¹, J. Bijewitz¹, A. Habermann¹, Z. Goraj², M. Kowalski², A. Castillo Pardo³, C.A. Hall³, F. Meller, Airbus Innovations, Germany; R. Merkler, MTU Aero Engines, Germany; O. Petit*, S. Samuelsson*, B. Della Corteº, M. van Sluisº, G. Wortmann, Siemens AG, Germany; M. Dietz, ARTTIC, Germany; ¹Bauhaus Luftfahrt e.V., Germany ;²Warsaw University of Technology, Poland ;³University of Cambridge, United Kingdom ;*Chalmers University of Technology, Sweden ;ºTechnical University of Delft, Netherlands
11. Sep 18 10:30 11:00 1.4.2 SYSTEM-LEVEL ASSESSMENT OF TAIL-MOUNTED PROPELLERS FOR REGIONAL AIRCRAFT
R. Vos¹, M.F.M. Hoogreef¹; ¹Delft University of Technology, Netherlands
11. Sep 18 11:00 11:30 1.4.3 EXPLORATION OF THE AIRBUS \"NAUTILIUS\" ENGINE INTEGRATION CONCEPT
L. Wiart, ONERA, France; C. Negulescu, AIRBUS, France
11. Sep 18 11:30 12:00 1.4.4 CONSTRAINED BIFURCATION AND CONTINUATION METHOD IN BLENDED-WING-BODY AIRCRAFT DESIGN
F. Cen¹, Q. Li¹, B.-W. Nie², Z.-T. Liu²; ¹Tsinghua University, China ;²China Aerodynamics Research and Development Center , China
2.4Next Generation Commercial Transport Concept
Chair(s): Collier, F.
Track 2
01 - Aircraft Design and Integrated Systems
11. Sep 18 10:00 10:30 2.4.1 BLENDED WING BODY TRANSPORT AIRCRAFT RESEARCH & DEVELOPMENT
J.T. Bonet, Boeing Research & Technology, United States
11. Sep 18 10:30 11:00 2.4.2 SINGLE-AISLE AIRLINER DISRUPTION WITH A SINGLE-DECK BLENDED-WING-BODY
M.A. Page¹, E.J. Smetak¹, S.L. Yang¹; ¹DZYNE Technologies Incorporated, United States
11. Sep 18 11:00 11:30 2.4.3 SUBSONIC ULTRA-GREEN AIRCRAFT RESEARCH: TRANSONIC TRUSS-BRACED WING TECHNICAL MATURATION
C.K. Droney¹, N.A. Harrison¹, G.M. Gatlin, NASA Langley Research Center, United States; ¹The Boeing Company, United States
3.4Systems Architecting
Chair(s): Tokasiki, C.
Track 3
02 - Systems Engineering and Integration
11. Sep 18 10:00 10:30 3.4.1 DIGITAL INNOVATION IN COMPLEX SYSTEMS-MANAGING CRITICAL APPLICATIONS AND GENERATIVITY
N. Lakemond, Linköping University, Sweden; G. Holmberg, Saab AB and Linköping University, Sweden
11. Sep 18 10:30 11:00 3.4.2 A PRACTICAL ANALYSIS ON THE COMPLEXITY OF AIRCRAFT SYSTEMS ARCHITECTURE AND REQUIREMENTS DEVELOPMENT
F.M.S. Turetta, Embraer, Brazil
11. Sep 18 11:00 11:30 3.4.3 AIRCRAFT SYSTEMS ARCHITECTING: LOGICAL-COMPUTATIONAL DOMAIN INTERFACE
M. Guenov¹, A. Molina-Cristóbal¹, A. Riaz¹, S. Sharma², A. Murton², J. Crockford²; ¹Cranfield University, United Kingdom ;²Airbus Operations Ltd, United Kingdom
11. Sep 18 11:30 12:00 3.4.4 SERVICE-ORIENTED ARCHITECTURE TO INTEGRATE FLIGHT SAFETY AND MISSION MANAGEMENT SUBSYSTEMS INTO UAVS
V. Vannini¹, J.S. Arantes¹, A.-P. Mattei², N. Figueira, Brazilian Army, Brazil; M.S. Arantes², C.F.M. Toledo¹, O. Trindade J.¹, P. Saqui-Sannes, Institut Supérieur de l’Aéronautique et de l’Espace, France; ¹University of São Paulo, Brazil ;²Innovation Institute for Embedded Systems, Brazil
4.4Aerodynamic Design
Chair(s): Prince, S., Grossi, F.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
11. Sep 18 10:00 10:30 4.4.1 \"FAST\" CFD METHODS IN AIRCRAFT SYSTEM DESIGN. APPLICATION TO C295W MODIFICATIONS.
C. González Biedma, Airbus D&S, Spain
11. Sep 18 10:30 11:00 4.4.2 MORPHING WING WITH SURFACE DISCONTINUITY - COMPARATIVE TESTS
A. Tarnowski¹, T. Goetzendorf-Grabowski¹, J. Mieloszyk¹; ¹Warsaw University of Technology, Poland
11. Sep 18 11:00 11:30 4.4.3 HIGHER FIDELITY TRANSONIC AERODYNAMIC MODELING IN PRELIMINARY AIRCRAFT DESIGN
A. Crovato¹, G. Dimitriadis¹, V.E. Terrapon¹; ¹University of Liege, Belgium
11. Sep 18 11:30 12:00 4.4.4 NUMERICAL ANALYSIS OF BLEND-WING-BODY AIRFRAME AND ENGINE AERODYNAMIC INTERFERENCE
Z. Tan, China; Y. Chen, China; J. Si, China; Y. Zhong, China
Reserve Paper 4.4.R COMPARISON AND APPLICATION OF DIFFERENTS TECHNIQUES OF MULTI-OBJECTIVE OPTIMIZATION FOR AERODYNAMIC WING DESIGN
N. Gautier¹, N. Manzanares-Filho¹, E.R. Da Silva¹; ¹UNIFEI, Brazil
5.4Wind Tunnel Systems Development
Chair(s): ,
Track 5
03.2 - Experimental Aerodynamics
11. Sep 18 10:00 10:30 5.4.1 OVERVIEW OF DYNAMIC TEST TECHNIQUES AT LOW SPEED AERODYNAMICS INSTITUTE, CARDC
Z. Liu¹, H. Sun¹, B. Nie¹, L. Guo¹, F. Cen¹; ¹China Aerodynamics Research and Development Center (CARDC), China
11. Sep 18 10:30 11:00 5.4.2 APPLICATION OF THE COMBINED BOUNDARIES TO REDUCE WALL INTERFERENCE FOR NACA 0012 AIRFOIL TESTS
S.L. Chernyshev¹, A.I. Ivanov¹, E.V. Streltsov¹, A.O. Volkova¹; ¹Central Aerohydrodynamic Institute n.a. prof. N.E. Zhukovsky, Russia
11. Sep 18 11:00 11:30 5.4.3 EVALUATION OF WIND TUNNEL WALL BOUNDARY-LAYER CONTROL FOR 2-D HIGH-LIFT AERODYNAMIC AND AEROACOUSTIC TESTING
F.M. Catalano, Aeronautical Engineering Dept. University of São Paulo , Brazil; L.T.L. Pereira, University of São Paulo , Brazil
11. Sep 18 11:30 12:00 5.4.4 EXPERIMENTAL INVESTIGATION OF SHEAR LAYER INDUCED FLUCTUATIONS IN A OPEN JET WIND TUNNEL
G.G. Gadzhimagomedov, Central Aerohydrodynamic Institute n.a. prof. N.E. Zhukovsky, Russia
6.4Composites
Chair(s): Scott, M., Shanygin, A.
Track 6
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
11. Sep 18 10:00 10:30 6.4.1 PREDICTIVE ANALYSIS OF STITCHED AEROSPACE STRUCTURES FOR ADVANCED AIRCRAFT
B. Horton¹, Y. Song¹, D. Jegley², F. Collier², J. Bayandor¹; ¹CRashworthiness for Aerospace Structures and Hybrids (CRASH) Lab, United States ;²NASA Langley Research Center, United States
11. Sep 18 10:30 11:00 6.4.2 DESIGNING PRIMARY STRUCTURES WITH STITCHED COMPOSITES
A. Velicki, The Boeing Company, United States
11. Sep 18 11:00 11:30 6.4.3 MULTIFUNCTIONAL COMPOSITE PROCESSED USING EMBROIDERY TECHNOLOGY
T. Ikeda, Chubu University, Japan; M. Ishigami¹, T. Nishihara¹; ¹Nagoya University, Japan
11. Sep 18 11:30 12:00 6.4.4 MODIFIED WHITNEY-NUISMER CRITERIA FOR PREDICTION OF NOTCHED STRENGTH OF COMPOSITE LAMINATES
C. Wallner, USP/Embraer, Brazil; S.F.M. Almeida, Universidade de Sao Paulo, Brazil; C. Kassapoglou, TU Delft, Netherlands
7.4Store Separation
Chair(s): Cenko, A.
Track 7
03.4 - Applied Aerodynamics
11. Sep 18 10:00 10:30 7.4.1 EXHAUST PLUME EFFECT OF WINGED TWO-STAGE-TO-ORBIT SEPARATION AT ASCENT USING AERODYNAMIC-FLIGHT DYNAMICS TECHNIQUE
H. Iwafuji, Tokyo Metropolitan University, Japan
11. Sep 18 10:30 11:00 7.4.2 NUMERICAL SIMULATION OF THE AERIAL DROP OF WATER FOR FIXED-WING AIRTANKERS
X. Zhao¹, P. Zhou¹, X. Yan, No. 38 Research Institute of CETC, China; Y. Weng, Xi’an Jiaotong University, China; X.-L. Yang, Chinese Flight Test Establishment, China; ¹Northwestern Polytechnical University, China
11. Sep 18 11:00 11:30 7.4.3 GRID-MODE TRANSONIC STORE SEPARATION ANALYSES USING MODERN DESIGN OF EXPERIMENTS
K.A. Jamison, Council of Scientific and Industrial Research (CSIR), South Africa
11. Sep 18 11:30 12:00 7.4.4 STORE SEPARATION TRAJECTORY PREDICTIONS AT LOW SPEEDS
A. Cenko, AIWS, United States; N. Stathopoulos, L3-MAS, Canada; R. Hobbins, Bombardier, Canada; G. Akroyd, Akroyd Aeronautics, Australia
8.4Aeroelasticity 2 : Methods and Modeling
Chair(s): Willcox, K., Gil, R.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
11. Sep 18 10:00 10:30 8.4.1 AEROELASTIC TAILORING OF COMPOSITE WING BY USING MULTIDISCIPLINARY DESIGN ENVIRONMENT
K.A. Balunov¹, V.V. Chedrik¹, F.Z. Ishmuratov¹; ¹TsAGI, Russia
11. Sep 18 10:30 11:00 8.4.2 VIRTUAL AIRCRAFT MODEL FOR AEROELASTIC SIMULATION AND LOAD PREDICTION OF A HIGH ASPECT RATIO COMPOSITE SWEPT WING
A. Hermanutz¹, M. Hornung¹; ¹Technical University of Munich, Germany
11. Sep 18 11:00 11:30 8.4.3 THERMAL-MECHNICAL COUPLING ANALYSIS AND OPTIMIZATION DESIGN ON TPS WITH GAP
S. Huo¹, Q. Yan¹, W. Xie, Harbin Institute of Technology , China; ¹Aircraft Strength Research Institute, China
11. Sep 18 11:30 12:00 8.4.4 AERODYNAMICS OPTIMIZATION DESIGN METHOD AND SHAPE PARAMETERIZATION
Z.Y Wang, The First Aircraft Institute, AVIC, China
9.4Engine Performance
Chair(s): Remy, S.
Track 9
05 - Propulsion
11. Sep 18 10:00 10:30 9.4.1 THE PHYSICS BEHIND MCHANICS AND FAILURE OF GAS TURBINE COMPONENTS IN AEROSPACE SYSTEMS
P. Patnaik, National Research Canada, Canada; K.Y. Chen¹, X.J. Wu¹; ¹National Research Council Canada, Canada
11. Sep 18 10:30 11:00 9.4.2 A COMPOSITE CYCLE ENGINE CONCEPT FOR YEAR 2050
S. Kaiser¹, H. Kellermann¹, M. Nickl¹, A. Seitz¹; ¹Bauhaus Luftfahrt e.V., Germany
11. Sep 18 11:00 11:30 9.4.3 APPLICATION OF "VIRTUAL" CONTROLLERS FOR INTEGRATED PROPULSION AND AIRCRAFT CONTROL
O.S. Gurevich¹, F.D. Golberg¹, S.A. Smetanin¹, N.E. Romanenko¹; ¹Central Institute of Aviation Motors, Russia
11. Sep 18 11:30 12:00 9.4.4 A ROBUST STABLE PI CONTROLLER DESIGN IN TIME-FREQUENCY DUAL DOMAINS FOR AIRCRAFT ENGINE
N. Liu, Shanghai Aircraft Design & Research Institute, China
10.4Flight Testing
Chair(s): Naruoka, M.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
11. Sep 18 10:00 10:30 10.4.1 WIND TUNNEL VIRTUAL FLIGHT TEST FOR A TRANSPORT AIRCRAFT WITH SIMULATED ICE SHAPE
L. Guo¹, M. Zhu¹, J. Guan¹, B. Nie¹; ¹China Aerodynamics Research and Development Centre, China
11. Sep 18 10:30 11:00 10.4.2 DEVELOPMENT OF A GENERIC FLIGHT TEST MANEUVER INJECTION MODULE
C. Krause¹, C. Göttlicher¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, Germany
11. Sep 18 11:00 11:30 10.4.3 CHARACTERISTIC HELICOPTER FLIGHT MECHANICS AND MOTION CUEING INTEGRATION INTO THE SIVOR ROBOTIC FLIGHT SIMULATOR: AN OBJECTIVE APPROACH
D.F. Hidalgo, Universidad pontificia bolivariana, Colombia; G.B. Rodamilans¹, W.R. de Oliveira¹; ¹CCM-Instituto Tecnologico de Aeronautica, Brazil
11. Sep 18 11:30 12:00 10.4.4 KNOWLEDGE ENGINEERING BASED FLIGHT TEST TECHNOLOGY FOR CIVIL AIRCRAFT AIRWORTHINESS CONFORMITY
L. ZHAOHUI¹, L. GANG¹; ¹Chinese Flight Test Establishment, China
11.4Flight Test and Equipment
Chair(s): ,
Track 11
07 - Systems, Subsystems and Equipment
11. Sep 18 10:00 10:30 11.4.1 CORE POWER SUPPLY, FROM ENGINES TO BATTERIES – A FLIGHT TEST APPROACH
F.M. Catalano, Sao Carlos School of Engineering - University of Sao Paulo, Brazil
11. Sep 18 10:30 11:00 11.4.2 GROUND AND FLIGHT TESTING OF A MULTI-SENSOR OBSTACLE DETECTION AND TRACKING SYSTEM FOR RPAS SITUATION AWARENESS
J. Gauci¹, K. Theuma¹, R. Archer, Hawk Aerospace, Malta; R. Grech, Idox Health, Malta; D. Zammit-Mangion¹; ¹University of Malta, Malta
11. Sep 18 11:00 11:30 11.4.3 POWER LINE COMMUNICATION APPLIED TO FLIGHT TEST INSTRUMENTATION
M.V. Ribeiro¹, F.P.V. de Campos¹, S.A. Souza, Smarti9 Ltd., Brazil; Â. Camponogara¹, E.S.B. de Castro², L.M.C.S. Evangelista², S.D. Penna²; ¹Universidade Federal de Juiz de Fora, Brazil ;²Embraer S.A., Brazil
11. Sep 18 11:30 12:00 11.4.4 THERMO-VACUUM TEST CHAMBER DEVELOPMENT FOR AIRBORNE AND SPACE EQUIPMENT TESTING IN SIMULATED EXTREME CONDITIONS
J. Mašek, Brno University of Technology,Institute of Aerospace Engineering, Czech Republic
12.4Aircraft Operation 1
Chair(s): Tokuakid, N., Lamiscarre, B.
Track 12
09 - Air Transport System Efficiency
11. Sep 18 10:00 10:30 12.4.1 ALGORITHMS AND SYSTEM FOR CURVED AND CONTINUOUS DESCENT TRAJECTORIES IMPROVING FUEL EFFICIENCY IN TMA
A. Errico¹, V. Di Vito¹; ¹CIRA – Italian Aerospace Research Center, Italy
11. Sep 18 10:30 11:00 12.4.2 PERFORMANCE COMPARISON OF A320 AND 737NG REGARDING THE VERTICAL AND AND SPEED PROFILES IN ADVANCED RNP TO XLS ARRIVALS
T. Dautermann¹, T. Ludwig¹, L. Altenscheidt¹, M. Altenscheidt, NavArt, Germany; R. Geister¹, M. Braschczok¹; ¹DLR, Germany
11. Sep 18 11:00 11:30 12.4.3 OPERATIONAL CONCEPT AND VALIDATION OF A NEW AIRPORT LOW-LEVEL WIND INFORMATION SYSTEM
T. Iijima¹, N. Matayoshi¹, S. Ueda¹; ¹JAXA, Japan
11. Sep 18 11:30 12:00 12.4.4 SEMANTICS-BASED SUMMARIZATION OF ATM DATA TO MANAGE INFORMATION OVERLOAD IN PILOT BRIEFINGS
C.G. Schuetz¹, B. Neumayr¹, M. Schrefl¹, E. Gringinger, Frequentis AG, Austria; S. Wilson, EUROCONTROL, Belgium; ¹Johannes Kepler University Linz, Austria

12:00 - 13:00Lunch

0.5ICAS Casimiro Montenegro Filho Lecture for Innovation in Aeronautics - AGILE Project Consortium
Chair:
11. Sep 18 13:00 13:45

1.5Design Education 1
Chair(s): Rinoie, K.
Track 1
01 - Aircraft Design and Integrated Systems
11. Sep 18 14:00 14:30 1.5.1 COLLABORATIVE OPEN SOURCE AIRCRAFT DESIGN FRAMEWORK FOR EDUCATION - AGILE ACADEMY INITIATIVES AND RESULTS
P. Della Vecchia, University of Naples, Italy; B. Aigner, RWTH Aachen University, Germany; I. van Gent , TU Delft, Netherlands; P.D. Ciampa¹, P.S. Prakasha¹; ¹German Aerospace Center DLR , Germany
11. Sep 18 14:30 15:00 1.5.2 MDO AS A SOCIO-TECHNICAL SYSTEM - A SMALL CONTRIBUTION TO COLLABORATIVE ENGINEERING
M. Spieck, Thelsys GmbH, Germany; B. Aigner, RWTH Aachen, Germany; P.S. Prakasha¹, P.D. Ciampa¹; ¹German Aerospace Center, Germany
11. Sep 18 15:00 15:30 1.5.3 EXPERIENCE WITH INTERNATIONAL COLLABORATIVE AIRCRAFT DESIGN EDUCATION: AREND UAV
L. Smith, University of Pretoria, South Africa; J.N. Koster, University of Colorado, United States; J. Schneider, University of Stuttgart, Germany
2.5Aircraft Design
Chair(s): Isikveren, A.
Track 2
01 - Aircraft Design and Integrated Systems
11. Sep 18 14:00 14:30 2.5.1 A CASE OF SUCESS: MDO APPLIED ON THE DEVELOPMENT OF EMBRAER 175 ENHANCED WINGTIP
J. Cavalcanti¹, P. London¹, R. Wallach¹, P. Ciloni¹; ¹Embraer, Brazil
11. Sep 18 14:30 15:00 2.5.2 CONTAINERIZED AIR FREIGHT SYSTEM POWERED BY CRYOGENIC FUEL
V.I. Chernousov¹, A.A. Krutov¹, E.A. Pigusov¹; ¹TsAGI, Russia
11. Sep 18 15:00 15:30 2.5.3 COMPARISON OF METHODS TO PREDICT AERODYNAMIC CENTER SHIFT DUE TO BODIES
W.A.J. Anemaat¹, D. van Dommelen¹, A. D'Silva¹, P.B. Sargent¹; ¹DARcorporation, United States
3.5Desktop Simulations
Chair(s): Dunyach, J.C., Nakashima, C.
Track 3
02 - Systems Engineering and Integration
11. Sep 18 14:00 14:30 3.5.1 RESEARCH ON DESKTOP VIRTUAL INTEGRATION AND VERIFICATION OF CIVIAL AIRCRAFT
Z. Yao¹, B. Guo, China-Russia Commercial Aircraft International Co., China; D. Xie¹, Z. Li¹; ¹Shanghai Aircraft Design and Research Institute, China
11. Sep 18 14:30 15:00 3.5.2 A NOVEL FMI AND TLM-BASED DESKTOP SIMULATOR FOR DETAILED STUDIES OF THERMAL PILOT COMFORT
R. Hällqvist¹, J. Schminder², M. Eek¹, R. Braun², R. Gårdhagen², P. Krus²; ¹Saab Aeronautics, Sweden ;²Linköping University, Sweden
4.5High Lift Aerodynamics
Chair(s): Pedreiro, L., Nicolosi, F.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
11. Sep 18 14:00 14:30 4.5.1 CFD INVESTIGATION OF AERODYNAMIC COEFFICIENTS AND STALL CHARACTERISTICS FOR HIGH LIFT CONFIGURATIONS
R.G. da Silva¹, L.M.M.O. Carvalho², A.C.V.M. Almeida², J.L.F. Azevedo¹; ¹Instituto de Aeronáutica e Espaço, Brazil ;²Instituto Tecnológico de Aeronáutica, Brazil
11. Sep 18 14:30 15:00 4.5.2 NUMERICAL HIGH LIFT PREDICTION ON THE JAXA STANDARD MODEL
V. Cusati¹, P. Della Vecchia¹, D. Ciliberti¹, S. Corcione¹, F. Nicolosi¹; ¹University of Naples Federico II, Italy
11. Sep 18 15:00 15:30 4.5.3 LATTICE BOLTZMANN HIGH-LIFT SIMULATIONS - A STEP BEYOND CLASSICAL CFD
B. Koenig¹, D. Singh¹, E. Fares¹; ¹Exa GmbH, Germany
Reserve Paper 4.5.R A COMPREHENSIVE FRAMEWORK FOR HIGH LIFT AERODYNAMIC PREDICTION BASED ON AN IMPROVED APPROACH
M. Ruocco¹, P. Della Vecchia¹, F. Nicolosi¹, A. De Marco¹; ¹University of Naples, Italy
5.5Next Generation Commercial Transport Concept- Panel Session
Chair(s): Collier, F.
Track 5
14 - ECSC
6.5Aircraft Structural Design I
Chair(s): Krus, P.
Track 6
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
11. Sep 18 14:00 14:30 6.5.1 A FRAMEWORK FOR UNCONVENTIONAL LANDING GEAR CONFIGURATION MODELLING
U. Kling¹, T. Brügge¹, F. Peter¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
11. Sep 18 14:30 15:00 6.5.2 BUCKLING/POSTBUCKLING OPTIMIZATION OF STIFFENED COMPOSITE PANELS BASED ON SENSITIVITY ANALYSIS
L. Dong¹, D. Cui, Science and Technology committee, China; R. Zhang¹; ¹Chinese Aeronautical Establishment, China
11. Sep 18 15:00 15:30 6.5.3 GLOBAL-LOCAL STRUCTURAL ANALYSIS OF COMPOSITE WINGS
E. Carrera¹, A. Pagani¹, G.H.C. Silva, Embraer S.A., Brazil; ¹Politecnico di Torino, Italy
7.5Advanced Manufacturing
Chair(s): Zhu, M.
Track 7
08 - Manufacturing and Supply Chain Management
11. Sep 18 14:00 14:30 7.5.1 MITIGATING RISK OF PRODUCIBILITY FAILURES IN PLATFORM CONCEPT DEVELOPMENT
J. Madrid¹, J. Landahl¹, R. Söderberg¹, H. Johannesson¹, J. Lööf, GKN Aerospace, Sweden; ¹Chalmers University of Technology, Sweden
11. Sep 18 14:30 15:00 7.5.2 STUDIES ON AIRCRAFT ROBOT AIDED MANUFACTURING
G.J.G. Lahr¹, J.V.R. Soares, Votorantim S.A., Brazil; J.O. Savazzi, EMBRAER-GPX, Brazil; G.A.P. Caurin¹; ¹University of Sao Paulo, Brazil
8.5Impact
Chair(s): Kurdelski, M.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
11. Sep 18 14:00 14:30 8.5.1 VERIFIED FUSELAGE SECTION WATER IMPACT MODELING
Y. Song¹, B. Harton¹, J. Bayandor¹; ¹University at Buffalo, CRASH Lab, United States
11. Sep 18 14:30 15:00 8.5.2 PREDICTING LOW-VELOCITY IMPACT DAMAGE IN COMPOSITE USING COHESIVE ELEMENT
H. Liu¹, S. Tan¹; ¹fai, China
11. Sep 18 15:00 15:30 8.5.3 ENERGY-ABSORBING CHARACTERISTICS ANALYSIS OF COMPOSITE THIN-WALLED C-CHANNELS UNDER LOW SPEED AXIAL COMPRESSION
J. XIE¹, Z. FENG¹, S. SONG¹, D. SONG¹, X. Zhang¹; ¹Civil Aviation University of China, China
9.5MDAO- multidisciplinary analysis and optimization
Chair(s): Garnier, V., Ciampa, P.
Track 9
05 - Propulsion
11. Sep 18 14:00 14:30 9.5.1 IN-FLIGHT ACOUSTIC LOADS MEASUREMENTS ON AN ENGINE FLYING TEST BED
Y. Sun¹, C. Breard¹, X.P. Li¹, Y. Mei², P. Liu², M.B. Pang²; ¹Shanghai Aircraft Design and Research Institute of COMAC, China ;²COMAC Flight Test Center, China
11. Sep 18 14:30 15:00 9.5.2 MULTI-DISCIPLINARY OPTIMISATION OF MEDIUM ALTITUDE LONG ENDURANCE UAVS
D. Verstraete, University of Sydney, Australia
11. Sep 18 15:00 15:30 9.5.3 DYNAMIC MODEL FOR PLANETARY GEAR SETS OF GEARED TURBOFAN JET ENGINES
D. Kalinin¹, V. Golovanov¹, J. Temis, BMSTU, Russia; L. Magerramova¹; ¹CIAM, Russia
10.5Flight Modeling and Simulation
Chair(s): Doll, C.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
11. Sep 18 14:00 14:30 10.5.1 ON REAL–TIME SIMULATION OF FLEXIBLE AIRCRAFT WITH PHYSICS–DERIVED MODELS
J.A. Paulino¹, A. Da Ronch, University of Southampton, United Kingdom; A.B. Guimarães Neto¹, F.J. Silvestre¹, M.A.V. Morales¹; ¹Instituto Tecnológico de Aeronáutica, Brazil
11. Sep 18 14:30 15:00 10.5.2 MANEUVERABILITY ASSESSMENT FOR FAULTY AIRPLANE BY IFS WITH SIMULTANEOUS MODEL-MATCHING FOR GUST AND HANDLING RESPONSES
M. Sato, Japan Aerospace Exploration Agency, Japan
11. Sep 18 15:00 15:30 10.5.3 BAYESIAN APPROACH TO FLIGHT CHARACTERISTICS MODELING WITH REAL FLIGHT DATA
M. Naruoka, Japan Aerospace Exploration Agency, Japan
11.5De-Icing
Chair(s): ,
Track 11
07 - Systems, Subsystems and Equipment
11. Sep 18 14:00 14:30 11.5.1 DE-ICING PHENOMENA MODELLED BY FINITE ELEMENT MODELS
V. De Simone¹, R. Scigliano¹, P. Catalano¹; ¹Italian Aerospace Research Centre (CIRA), Italy
11. Sep 18 14:30 15:00 11.5.2 DETECTING HIGH-ALTITUDE ICE CRYSTAL (HAIC) ICING EVENTS FROM TOTAL AIR TEMPERATURE
A. Rodríguez-Sanz¹, R.M. Arnaldo¹, E. Sánchez Ayra, Universidad Politécnica de Madrid (UPM) & IBERIA, Spain; F. Gómez Comendador¹; ¹Universidad Politécnica de Madrid (UPM), Spain
11. Sep 18 15:00 15:30 11.5.3 NUMERICAL SIMULATION OF ICE ACCRETION INFLUENCED BY AN ANTI-ICING HEATING SYSTEM
K. Szilder, Aerospace, National Research Council, Canada; E. Lozowski, University of Alberta, Canada
Reserve Paper 11.5.R CALCULATION OF WATER FILM FLOW AND HEAT TRANSFER ON THE AIRCRAFT ANTI-ICING SURFACE
M. Zheng¹, T. Wu¹, Z. Guo¹, W. Dong¹; ¹Shanghai Jiao Tong University, China
12.5Air Transportation Network
Chair(s): Zhang, X., Kuegler, D.
Track 12
09 - Air Transport System Efficiency
11. Sep 18 14:00 14:30 12.5.1 A SIMULATION MODELING STUDY FOR FREE ROUTING AIRSPACE IN JAPAN
K. Kageyama¹, Y. Nakamura¹; ¹ENRI, Japan
11. Sep 18 14:30 15:00 12.5.2 EVALUATION OF THE POTENTIAL IMPACTS OF HYBRID-ELECTRIC AIRCRAFT ON THE GLOBAL AIR TRANSPORTATION NETWORK
G. Tay¹, S. Gillen¹, R. Rothfeld, Bauhaus Luftfahrt e.V., Germany; M. Hornung¹; ¹Technical University of Munich, Germany
11. Sep 18 15:00 15:30 12.5.3 DYNAMIC AIRSPACE MANAGEMENT FOR ENHANCED ATM SAFETY AND EFFICIENCY
A. G. Gardi, RMIT University, Australia
Reserve Paper 12.5.R STUDY ON THE LARGE-AREA FLIGHT DELAY RECOVERY
Zhaoning Zhang¹, Jinghua Wang¹; ¹Civil Aviation University of China, China

15:30 - 16:00Break

1.6NATO Hybrid/Electric Initiative
Chair(s): Isikveren, A.
Track 1
01 - Aircraft Design and Integrated Systems
11. Sep 18 16:00 16:30 1.6.1 NATO RESEARCH TASK GROUP: HYBRID/ELECTRIC AIRCRAFT DESIGN AND STANDARDS FOR RESEARCH AND TECHNOLOGY (HEADSTART)
F. Grauer, Germany
11. Sep 18 16:30 17:00 1.6.2 FLIGHT TEST OF A FUEL-CELL/BATTERY/SUPERCAPACITOR TRIPLE HYBRID UAV PROPULSION SYSTEM
A. Gong¹, J.L. Palmer, Defence Science and Technology Group, Australia; D. Verstraete¹; ¹The University of Sydney, Australia
11. Sep 18 17:00 17:30 1.6.3 KEY PERFORMANCE PARAMETERS FOR FUTURE NATO HYBRID/ELECTRIC MILITARY AIR VEHICLES
W. Dyson, National Aeronautics Space Administration (NASA), United States
11. Sep 18 17:30 18:00 1.6.4 COORDINATING INTERNATIONAL RESEARCH AND DEVELOPMENT IN HYBRID/ELECTRIC FLIGHT
n/a Kloeckner, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany
2.6Supersonic and Hypersonic Vehicles
Chair(s): Goraj, Z.
Track 2
01 - Aircraft Design and Integrated Systems
11. Sep 18 16:00 16:30 2.6.1 NEURAL NETWORK DRIVEN ADJOINT SOLVER BETWEEN FLIGHT-PATH OPTIMIZATION AND PANEL METHOD FOR AIRCRAFT DESIGN
M. Naoto, the University of Tokyo, Japan
11. Sep 18 16:30 17:00 2.6.2 LIFE CYCLE COST ESTIMATION METHODOLOGY FOR HYPERSONIC TRANSPORTATION SYSTEMS
R. Fusaro¹, D. Ferretto¹, V. Vercella¹, N. Viola¹, V. Fernandez Villace², J. Steelant²; ¹Politecnico di Torino, Italy ;²ESA-ESTEC, Netherlands
11. Sep 18 17:00 17:30 2.6.3 ANALYSIS OF THE INFLUENCE OF THE EXTERNAL CONFIGURATION ON THE WAVE DRAG OFSUPERSONIC BUSINESS JETS
M.U. Quirino¹, M. Calvo, École de l’air - French Air Force Academy, France; R.C. Munjulury, Linkoping University, Sweden; A.M Abdalla¹; ¹University of São Paulo - USP - Brazil, Brazil
11. Sep 18 17:30 18:00 2.6.4 ANALYSIS OF LOW-BOOM CHARACTERISTICS OF SUPERSONIC WAVERIDER
P. Boonjaipetch, Tohoku University, Japan
Reserve Paper 2.6.R AN EFFICIENT FRAMEWORK FOR AERODYNAMIC CONFIGURATION EVOLUTION OF REENTRY VEHICELES
M.M. Entezari¹, M. Mohammadi-Amin¹; ¹ARI, Iran
3.6Systems Engineering Cases
Chair(s): Krus, P., Molino-Cristobal, A.
Track 3
02 - Systems Engineering and Integration
11. Sep 18 16:00 16:30 3.6.1 MODEL-BASED CONTROL LOGICS DEVELOPMENT OF AIRCRAFT SYSTEMS
V.L. Takase¹, H.H. Sano¹; ¹EMBRAER S.A., Brazil
11. Sep 18 16:30 17:00 3.6.2 COUPLING OF PREDESIGN AND PERFORMANCE TOOLS FOR TRANSIENT AIRCRAFT ENGINE ANALYSES
M. Vieweg¹, C. Klein¹, S. Reitenbach¹, F. Wolters¹, R.-G. Becker¹; ¹German Aerospace Center , Germany
11. Sep 18 17:00 17:30 3.6.3 A 7D TRADE
D.K. Howarth, MEE Inc., United States
11. Sep 18 17:30 18:00 3.6.4 BUILDING INNOVATIVE BUSINESS MODELS IN AERONAUTICS INDUSTRY: SOME LESSONS FROM THE BIONIC AIRCRAFT PROJECT
LP Pereira, Federal University of ABC, Brazil
4.6CFD Applications
Chair(s): Santos, L., Cenko, A.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
11. Sep 18 16:00 16:30 4.6.1 CFD VERIFICATION AND VALIDATION FOR INDUSTRIAL APPLICATIONS
M. Mani¹, A. Cary¹; ¹Boeing, United States
11. Sep 18 16:30 17:00 4.6.2 SHIP-HELICOPTER OPERATIONAL LIMITATION ENVELOPE DEFINITION WITH CFD RESULTS AND WIND TUNNEL DATA
C.F. Rafael¹, G.A.L. da Silva¹, M.J.M. Guedes, Brazilian Navy, Brazil; ¹Aerothermal Solutions and Software Distributor, Brazil
11. Sep 18 17:00 17:30 4.6.3 CFD-BASED STUDY OF DAMAGE LOCATION INFLUENCE ON AERODYNAMICS OF WINGS WITH SINGLE AND DOUBLE THROUGH HOLES
Z.W. Chen¹, Y. Pei¹, X.W. Yang¹, H. Ma¹; ¹Northwestern Polytechnical University, China
11. Sep 18 17:30 18:00 4.6.4 NUMERICAL SIMULATION OF OPERATING PROCESS ELEMENTS FOR COMBUSTION CHAMBERS OF PERSPECTIVE GTE
P.A. Semenev, Central Institute of Aviation Motors, Russia
Reserve Paper 4.6.R LAUNCHER AERODYNAMIC ANALYSIS WITH PLUME EFFECTS
A. Viviani, University of Campania, Italy; G. Pezzella, Italian Aerospace Research Centre, Italy
Reserve Paper 4.6.R SIMULATION OF TRANSONIC FLOW OVER SPACE VEHICLE
N.V. Palchekovskaya, MIPT, Russia
5.6Wind Tunnel Test Technology
Chair(s): ,
Track 5
03.2 - Experimental Aerodynamics
11. Sep 18 16:00 16:30 5.6.1 ADAPTIVE DESIGN OF EXPERIMENT BASED ON GAUSSIAN PROCESS MODELS WITH NONSTATIONARY KERNEL APPLIED TO WIND TUNNEL TESTING
U.H. Choi¹, J.H. Kim¹, Y.B. Lee, Agency for Defense Development, South Korea; J.M. Ahn¹; ¹KAIST, South Korea
11. Sep 18 16:30 17:00 5.6.2 RLG BASED REAL-TIME MODEL ATTITUDE DETERMINATION SYSTEM DEVELOPMENT FOR LARGE LOW SPEED FACILITY OF CARDC
F. Litao¹, H. Zhiyuan¹, W. Zhigang¹; ¹CARDC, China
11. Sep 18 17:00 17:30 5.6.3 ROTATING SHAFT BALANCE DESIGN AND CALIBRATION FOR CROR TESTING
V.S. Manvelyan, TsAGI, Russia
11. Sep 18 17:30 18:00 5.6.4 THE INFLUENCE OF HIGH-SPEED SPIV DATA PROCESSING PARAMETERS ON AIRCRAFT WING VORTEX WAKE ASSESSMENT
K. Garry¹, D. Di Pasquale¹, S. Prince¹, N.J. Lawson¹; ¹Cranfield University, United Kingdom
6.6New Structural Design 1: General
Chair(s): Ikeda, T.
Track 6
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
11. Sep 18 16:00 16:30 6.6.1 A PASSIVE-ADAPTIVE WING FOR DRAG REDUCTION
C.B. York, University of Glasgow, United Kingdom; Y.B. Murta, Embraer, Brazil; S.F.M. Almeida, University of Sao Paulo, Brazil
11. Sep 18 16:30 17:00 6.6.2 INVESTIGATION OF SYNERGETIC EFFECT INFLUENCE ON STRENGTH CHARACTERISTICS AND WEIGHT EFFICIENCY OF LOAD-BEARING AVIATION STRUCTURES
E.A. Dubovikov¹, M.C. Zichenkov¹, I.V. Mareskin¹, A.V. Chernov¹, A.N. Shanygin¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
11. Sep 18 17:00 17:30 6.6.3 A NUMERICAL ANALYSIS OF THE DYNAMICS OF A TENSEGRITY-MEMBRANE STRUCTURE
L.H. Teixeira¹, J.H. Izuka, Faculty of Applied Sciences - UNICAMP, Brazil; P. Gonzalez¹, P. Kurka¹; ¹Faculty of Mechanical Engineering - UNICAMP, Brazil
11. Sep 18 17:30 18:00 6.6.4 AN XFEM FRAMEWORK FOR ONSET AND CRACK PROPAGATION FOR COMPOSITES BASED ON ACTION PLANE THEORY
M.V. Angelo¹, M.L. Ribeiro¹, V. Tita¹; ¹University of Sao Paulo, Brazil
7.6Optimization
Chair(s): Jamison, K.
Track 7
03.4 - Applied Aerodynamics
11. Sep 18 16:00 16:30 7.6.1 MULTI-POINT AERODYNAMIC OPTIMIZATION DESIGN OF A DUAL-AISLE AIRPLANE WING
R.Z. Li¹, M. Zhang², M.H. Zhang², Y.F. Zhang¹, H.X. Chen¹; ¹Tsinghua University, China ;²Shanghai Aircraft Design and Research Institute, China
11. Sep 18 16:30 17:00 7.6.2 MULTILEVEL COLLABORATIVE AERODYNAMIC DESIGN OPTIMIZATION BASED ON SOBOL’ GLOBAL SENSITIVITY ANALYSIS
C. Wang¹, Z. Gao¹, P. Liu¹, Y. Na¹, X. Zhu¹; ¹Northwestern Polytechnical University, China
11. Sep 18 17:00 17:30 7.6.3 SURROGATE-BASED OPTIMIZATION METHOD APPLIED TO MULTIDISCIPLINARY DESIGN OPTIMIZATION ARCHITECTURES
C.-Z. Xu¹, Z.-H. Han¹, K.-S. Zhang¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China
11. Sep 18 17:30 18:00 7.6.4 COMBINING ADJOINT-BASED AND SURROGATE-BASED OPTIMIZATIONS FOR BENCHMARK AERODYNAMIC DESIGN PROBLEMS
H. Wang¹, Z.-H. Han¹, S.-Q. Han¹, Y. Zhang¹, C.-Z. Xu¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China
8.6Aeroelasticity 3: High Aspect Ratio Aircraft
Chair(s): Cesnik, C., Amiryants, G.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
11. Sep 18 16:00 16:30 8.6.1 PROPELLER INFLUENCE ON THE STABILITY OF HALE AIRCRAFT
P.C. Teixeira¹, C.E.S. Cesnik¹; ¹University of Michigan, United States
11. Sep 18 16:30 17:00 8.6.2 NONLINEAR AEROELASTIC REDUCED ORDER MODELS USING MODAL COORDINATES
R.R. Medeiros¹, C.E.S. Cesnik¹, E.B. Coetzee, Airbus Operations, United Kingdom; ¹University of Michigan, United States
11. Sep 18 17:00 17:30 8.6.3 NONLINEAR STATIC AEROELASTIC AND TRIM ANALYSIS OF HIGHLY FLEXIBLE AIRCRAFT
C. Zhang¹, Z. Zhou¹, P. Meng¹; ¹Northwestern Polytechnical University, China
11. Sep 18 17:30 18:00 8.6.4 AEROELASTIC WIND TUNNEL EXPERIMENT OF A HIGH-ASPECT-RATIO WING MODEL AGAINST GEOMETRICAL NON-LINEARITY
W. Qian¹, Y. Bai¹, H. Zeng, Shenyang Aircraft Design Institute, China; R. Yang¹; ¹Dalian University of Technology, China
9.6MDO AGILE
Chair(s): Mirzoyan, A.
Track 9
05 - Propulsion
11. Sep 18 16:00 16:30 9.6.1 MULTIOBJECTIVE MULTIPARAMETRIC OPTIMIZATION OF PROPULSION SYSTEM FOR ADVANCED CIVIL AIRCRAFT IN DISTRIBUTED ENVIRONMENT OF COLLABORATIVE MDO SYSTEM DEVELOPED IN AGILE PROJECT
A. Mirzoyan¹, A. Isyanov¹, D. Fokin¹, R. D´Ippolito², R. Lombardi²; ¹CIAM, Russia ;²Noesis, Belgium
11. Sep 18 16:30 17:00 9.6.2 STUDIES ON PROPULSION AND ON-BOARD SYSTEMS MATCHING IN AGILE PROJECT DISTRIBUTED COLLABORATIVE MDO ENVIRONMENT APPLYING FOR ADVANCED REGIONAL AND MEDIUM HAUL JET
M. Fioriti, Politecnico di Torino, Italy; L. Boggero, German Aerospace Center (DLR), Germany; A. Mirzoyan¹, A. Isyanov¹; ¹CIAM, Russia
11. Sep 18 17:00 17:30 9.6.3 COMMUNICATION BETWEEN PS AND AIRCRAFT SYSTEMS IN COLLECTIVE MDO SYSTEM IN AGILE PROJECT
P.D. Toktaliev, Central Institute of Aviation Motors, Russia
11. Sep 18 17:30 18:00 9.6.4 PROPULSION SYSTEM - AIRFRAME INTEGRATION AND OPTIMIZATION OF CIVIL AIRCRAFT- AGILE EU PROJECT
K. Anisimov, TSAGI, Russia
10.6Flight Trajectory Design
Chair(s): Tsuchiya, T.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
11. Sep 18 16:00 16:30 10.6.1 BI-LEVEL TRAJECTORY OPTIMIZATION BY STOCHASTIC COLLOCATION FOR UNCERTAINTY INTERVAL CALCULATION
P. Piprek¹, F. Holzapfel¹; ¹Technical University of Munich, Germany
11. Sep 18 16:30 17:00 10.6.2 LNAS - A PILOT ASSISTANCE SYSTEM FOR LOW-NOISE APPROACHES WITH MINIMAL FUEL CONSUMPTION
F. Abdelmoula¹, M. Scholz¹; ¹DLR Institute of Flight Systems, Germany
11. Sep 18 17:00 17:30 10.6.3 USING SENSITIVITY PENALTIES TO ROBUSTIFY THE OPTIMAL REENTRY TRAJECTORY OF A HYPERSONIC VEHICLE
T. Akman¹, J. Diepolder¹, B. Grüter¹, F. Holzapfel¹; ¹Technical University of Munich, Germany
11. Sep 18 17:30 18:00 10.6.4 NEW APPROACH FOR INVESTIGATION OF MAXIMUM-RANGE AIRCRAFT TRAJECTORIES
A.E. Sagalakov¹, A.S. Filatyev¹; ¹TsAGI, Russia
11.6Electro Mechanical Actuation Systems
Chair(s): Mare, J.C.
Track 11
07 - Systems, Subsystems and Equipment
11. Sep 18 16:00 16:30 11.6.1 FORCE FIGHT COMPENSATION FOR REDUNDANT ELECTRO-MECHANICAL FLIGHT CONTROL ACTUATORS
R. Kowalski¹, J. Windelberg¹, R. Ladner², M. Rottach²; ¹German Aerospace Center (DLR e.V.), Germany ;²Liebherr-Aerospace Lindenberg GmbH, Germany
11. Sep 18 16:30 17:00 11.6.2 A MORE INTEGRATED DESIGN APPROACH FOR EMBEDDED MECHATRONIC SYSTEMS: APPLICATION TO ELECTRICAL THRUST REVERSER ACTUATION SYSTEMS
S. Delbecq¹, M. Budinger, Institut Clément Ader (UMR CNRS 5312), France; J. Piaton¹; ¹Safran Electronics & Defense, France
11. Sep 18 17:00 17:30 11.6.3 POSITION SYNCHRONIZATION OF AEROSPACE ELECTROMECHANICAL ACTUATORS FOR DISTRIBUTED ELECTRICAL ACTUATION SYSTEM
J. Fu¹, J.-C. Mare, INSA-Toulouse, France; Y. Fu¹; ¹Beihang University, China
11. Sep 18 17:30 18:00 11.6.4 PIO SUSCEPTIBILITY IN FLY-BY-WIRE SYSTEMS
H.C. Moura¹, G.S.P. Alegre¹, J.H. Bidinotto¹, E.M. Belo¹; ¹University of São Paulo, Engineering School of São Carlos, Brazil
12.6Air Transportation Efficiency
Chair(s): Tomcko, I.
Track 12
09 - Air Transport System Efficiency
11. Sep 18 16:00 16:30 12.6.1 DECISION-MAKING INFORMATION SYSTEM FOR MULTIMODAL DISRUPTION MANAGEMENT: SYSTEM ARCHITECTURE AND CONCEPT OF OPERATIONS
FJS Jiménez Serrano, Hamad International Airport (Qatar Airways), Qatar
11. Sep 18 16:30 17:00 12.6.2 IMPLEMENTATION OF ECO-EFFICIENT PROCEDURES TO MITIGATE THE CLIMATE IMPACT OF NON-CO2 EFFECTS
M. Niklaß¹, B. Lührs, Technische Universität Hamburg (TUHH), Germany; V. Grewe¹, V. Gollnick¹; ¹ Deutsches Zentrum für Luft- und Raumfahrt (DLR), Germany
11. Sep 18 17:00 17:30 12.6.3 AN ATC ORIENTED INTERFACE FOR MULTI-AIRCRAFT OPTIMISATION FOR CLIMBS AND DESCENTS
A. Spiteri, University of Malta, Malta
11. Sep 18 17:30 18:00 12.6.4 THE GLOBAL FUEL SAVING POTENTIAL OF INTERMEDIATE STOP OPERATIONS CONSIDERING METEOROLOGICAL AND OPERATIONAL INFLUENCES
F. Linke, German Aerospace Center (DLR), Germany
Reserve Paper 12.6.R QUANTIFICATION OF FORMATION FLIGHT BENEFITS UNDER CONSIDERATION OF UNCERTAINTIES ON FUEL PLANNING
M. Swaid¹, T. Marks², B. Lührs¹, V. Gollnick²; ¹Hamburg University of Technology, Germany ;²German Aerospace Center, Germany

0.6ICAS Speed Mentoring: For all early careers (students and young professionals) Meeting professionals from companies, research institutes, and universities in aeronautics all over the world
Chair: E. Itoh
11. Sep 18 18:00 19:30

Wednesday, 12. Sep 2018


7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
0.7General lecture III - The Future of Propulsion, Dr. Ric Parker president ISABE
Chair: D. Müller-Wiesner
12. Sep 18 08:00 09:00

09:00 - 09:30Break

1.7Design Method 1
Chair(s): Bagassi, S.
Track 1
01 - Aircraft Design and Integrated Systems
12. Sep 18 09:30 10:00 1.7.1 MULTI-DISCIPLINARY ANALYSIS AND OPTIMIZATION JAVA TOOL FOR AIRCRAFT DESIGN
V. Trifari¹, M. Ruocco¹, V. Cusati¹, F. Nicolosi¹, A. De Marco¹; ¹University of Naples Federico II, Italy
12. Sep 18 10:00 10:30 1.7.2 COUPLED ADJOINT AEROSTRUCTURAL OPTIMIZATION FRAMEWORK FOR PRELIMINARY AIRCRAFT DESIGN
C.M. Boozer¹, A. Elham¹; ¹Braunschweig University of Technology, Germany
12. Sep 18 10:30 11:00 1.7.3 AIRCRAFT LOADS PREDICTION USING ENHANCED SIMULATION
Y. Lemmens, Siemens PLM, Belgium; T. Wilson, Airbus Operations Ltd, United Kingdom; J.E. Cooper, University of Bristol, United Kingdom
12. Sep 18 11:00 11:30 1.7.4 GENERAL PARAMETERS DESIGN METHOD OF CANARD ROTARY WING AIRPLANE UNDER THE INFLUENCE OF POWER SYSTEM
Y. Na, School of Aeronautics Northwestern Polytechnical University, China; Z.-H. Gao¹, Y.-P. Deng¹, L. Tian¹, H.-G. Gao¹; ¹School of Aeronautics Northwestern Polytechnical University, China
12. Sep 18 11:30 12:00 1.7.5 RESERCH ON KEY TECHNOLOGY OF INTELLIGENT CIVIL AIRCRAFT
Zhengqiang Li¹, Dianhang Xie¹, Bin Gao¹, Zhichao Yao¹; ¹Shanghai Aircraft Design and Research Institute, China
2.7Model Based System Engineering
Chair(s): Goes, L., Stoufflet, B.
Track 2
02 - Systems Engineering and Integration
12. Sep 18 09:30 10:00 2.7.1 MBSE FLIGHT TESTING ARCHITECTURE RESEARCH
X. Hua, China; C. Qing, CFTE, China; S.J. Qi, cfte, China
12. Sep 18 10:00 10:30 2.7.2 UTILIZATION OF SCALING LAWS AND UNCERTAINTY QUANTIFICATION TO INFORM TECHNOLOGY DEVELOPMENT EXPERIMENTATION
K.G. Schwartz¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States
12. Sep 18 10:30 11:00 2.7.3 A SYSML-BASED APPROACH TO EXPLORING INNOVATIVE SYSTEM IDEAS FOR AERONAUTICAL APPLICATIONS
J. Abulawi, HAW Hamburg, Germany
12. Sep 18 11:00 11:30 2.7.4 APPLICATION OF AGILE MODEL-BASED SYSTEMS ENGINEERING IN AIRCRAFT CONCEPTUAL DESIGN
G.P. Krupa, Federal University of Itajubá, Brazil
12. Sep 18 11:30 12:00 2.7.5 A BOND GRAPH-ORIENTED METHOD FOR ASSESSMENT OF FAILURES IN AN AIRCRAFT HYDRAULIC BRAKE SYSTEM
M. Maia Neto¹, L.C.S. Goes¹; ¹ITA, Brazil
3.7Durability and Fatigue
Chair(s): Poikelispää, M., Angelin, R.
Track 3
04.1 - Material Issues, Fatigue and Damage Tolerance
12. Sep 18 09:30 10:00 3.7.1 FATIGUE AND CRACK PROPAGATION LIFE IMPROVEMENT QUANTIFICATION FOR COLD-WORKED HOLES OUTSIDE NOMINAL CONDITIONS
L. Zaplana ¹, I. Rivero¹, B. García-Fogeda ¹, J. Gómez-Escalonilla¹; ¹AIRBUS DS, Spain
12. Sep 18 10:00 10:30 3.7.2 USING THE LEAD CRACK CONCEPT TO REDUCE DURABILITY TEST DURATION
L. Molent, DST, Australia
12. Sep 18 10:30 11:00 3.7.3 INFLUENCE OF IRREGULAR LOADING PARAMETERS ON CFRP COMPONENTS FATIGUE LIFE
A.G. Kalinin, Central Aerohydrodynamic Institute, TsAGI, Russia
12. Sep 18 11:00 11:30 3.7.4 THE EFFECT OF STRUCTURAL PARAMETERS OF AIRCRAFT PANEL ON VIBRATION FATIGUE LIFE
P. Li¹, J. Ma¹; ¹Aircraft strength research institute, China
4.7Turbulence Modeling and LES
Chair(s): Hackström, M., Bigarella, E.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
12. Sep 18 09:30 10:00 4.7.1 TOWARDS INDUSTRIAL LARGE EDDY SIMULATION AND AERO-ACOUSTIC NOISE COMPUTATION WITH THE HIGH-ORDER FR/CPR METHOD
Z. J. Wang, University of Kansas, United States
12. Sep 18 10:00 10:30 4.7.2 TURBULENCE MODEL CONDITIONING FOR VORTEX DOMINATED FLOWS BASED ON EXPERIMENTAL RESULTS
M. Moioli¹, C. Breitsamter¹, K.A. Sørensen, Airbus Defence and Space, Germany; ¹Technical University of Munich, Germany
12. Sep 18 10:30 11:00 4.7.3 IMPROVED DELAYED DETACHED EDDY SIMULATION OF THE FLOWS AROUND S809 AIRFOIL FOR ANGLES OF ATTACK FROM 0 TO 90 DEGREES
W. Yue¹, L. Kang¹, S. Wenping¹, H. Zhonghua¹; ¹Northwestern Polytechnical University, China
12. Sep 18 11:00 11:30 4.7.4 AERODYNAMIC EVALUATION OF THE EXTERNAL FLOW OVER PICKUP TRUCKS
E.-K. Mascia¹, O. de Almeida¹; ¹Federal University of Uberlandia, Brazil
12. Sep 18 11:30 12:00 4.7.5 A HYBRID LENGTH SCALE SIMILARITY SOLUTION FOR SWIRLING TURBULENT JETS
G. Andrews, Purdue University, United States
5.7Unsteady Flows and Aeroacoustics
Chair(s): Chen, Y.
Track 5
03.2 - Experimental Aerodynamics
12. Sep 18 09:30 10:00 5.7.1 UNSTEADY AERODYNAMIC CHARACTERISTICS OF THE OSCILLATING AIRFOIL USING MSBS
Y.H. Sung¹, J.S. Han¹, J.H. Han¹; ¹KAIST, South Korea
12. Sep 18 10:00 10:30 5.7.2 DESIGN OF AN INSTRUMENTED STATOR VANE FOR UNSTEADY PRESSURE MEASUREMENTS USING MEMS MICROPHONES
B. Martinez R Jr.¹, L.C. Caldas¹, R.G. Cuenca, Federal University of Santa Catarina, Brazil; R. Lauterjung Q, Embraer S/A, Brazil; P.C. Greco Jr¹; ¹University of Sao Paulo, Brazil
12. Sep 18 10:30 11:00 5.7.3 EVALUATION OF TRANSONIC BUFFETING ONSET BOUNDARY ESTIMATED BY TRAILING EDGE PRESSURE DIVERGENCE AND RMS DATA OF WING VIBRATION
Rodrigo Sorbilli Sousa, EMBRAER, Brazil; Roberto Gil A. da Silva¹, Roberto da Motta Girardi¹; ¹ITA, Brazil
12. Sep 18 11:00 11:30 5.7.4 CHALLENGES OF AERO-ACOUSTIC MEASUREMENTS IN WIND TUNNEL: IDENTIFICATION AND ELIMINATION OF \"PARASITE\" NOISE
Y. Sun¹, C. Breard¹, X. Li¹, Y. Chen¹; ¹Shanghai Aircraft Design and Research Institute of COMAC, China
12. Sep 18 11:30 12:00 5.7.5 TIME-RESOLVED PRESSURE MEASUREMENTS FOR AN AIRFOIL WITH SELF-SUSTAINED SHOCK OSCILATIONS
H.F. Leite¹, R.G.A. da Silva¹, A.C. Avelar, IAE, Brazil; ¹ITA, Brazil
6.7Complex Transition Phenomena
Chair(s): Alves, L., Hanifi, A.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
12. Sep 18 09:30 10:00 6.7.1 DEVELOPMENT OF SECONDARY CROSSFLOW INSTABILITY NEAR BREAKDOWN INTO TURBULENCE
E. van Bokhorst¹, C. Atkin¹; ¹University of London, United Kingdom
12. Sep 18 10:00 10:30 6.7.2 EFFECTS OF THE INTRINSIC THREE-DIMENSIONALIZATION OF LAMINAR SEPARATION BUBBLES ON THE AMPLIFICATION OF EXTERNAL DISTURBANCES
D. Rodriguez, Universidade Federal Fluminense, Brazil; E.M. Gennaro, Sao Paulo State University, Brazil
12. Sep 18 10:30 11:00 6.7.3 WAVEPACKETS IN TURBULENT FLOW OVER A NACA 4412 AIRFOIL
L.I. Abreu¹, A.V.G. Cavalieri¹, P. Schlatter², R. Vinuesa², D. Henningson²; ¹ITA, Brazil ;²KTH, Sweden
12. Sep 18 11:00 11:30 6.7.4 CONTROL OF STREAKY DISTURBANCES IN THE BOUNDARY LAYER OVER A FLAT PLATE
P. Morra¹, K. Sasaki², A. Cavalieri², A. Hanifi¹, D. Henningson¹; ¹KTH Royal Institute of Technology, Sweden ;²Instituto Tecnológico de Aeronáutica, Brazil
12. Sep 18 11:30 12:00 6.7.5 LAMINAR-TURBULENT TRANSITION MECHANISMS OVER WIDELY-SPACED SUCTION HOLES
B. Crowley¹, C. Atkin¹; ¹City University of London, United Kingdom
7.7Propellors and Rotors
Chair(s): Monk, J.
Track 7
03.4 - Applied Aerodynamics
12. Sep 18 09:30 10:00 7.7.1 APPLICATION OF HIGH-ROBUSTNESS BEMT FOR SIMULATION OF UAV-VTOL PROPELLER AT LOW/HIGH ADVANCE RATIO
Z. Fan¹, Z. Zhou¹, X. Zhu, Science and Technology on UAV Laboratory, NPU, China; ¹School of Aeronautics,Northwestern Polytechnical University, China
12. Sep 18 10:00 10:30 7.7.2 AERODYNAMIC DESIGN OF A RIGID COAXIAL ROTOR AIRFOIL IN UNSTEADY FLOW
X.-D. Yang¹, M. Huang¹; ¹School of Aeronautics Northwestern Polytechnical University, China
12. Sep 18 10:30 11:00 7.7.3 INVESTIGATION ON APPROACH TO CONTROL LIFT DISTRIBUTION OF WING BY DISTRIBUTED PROPELLERS
C. Xue¹, Z. Zhou¹, H.-B. Wang¹; ¹Northwestern Polytechnical University, China
12. Sep 18 11:00 11:30 7.7.4 ANALYSIS OF XH-59A ROTOR IN FORWARD FIGHT WITH HIGH EFFICIENCY TRIM METHOD
P. Zhou¹, X. Zhao¹, L. Deng¹, Y.-F. Lin, China Helicopter Research and Development Institute, China; ¹Northwestern Polytechnical University, China
12. Sep 18 11:30 12:00 7.7.5 SIMULATIONS OF UNSTEADY AIRWAKES BEHIND SHIPS IN MOTION
W.X. Yuan¹, A. Wall¹, R. Lee¹; ¹National Research Council Canada, Canada
8.7Aircraft Structural Design II
Chair(s): Ireman, T.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
12. Sep 18 09:30 10:00 8.7.1 PRELIMINARY ASSESSMENT OF A WARPING WING CONFIGURATION IN ROLLING CONTROL
E. Cestino¹, G. Frulla¹, A. Lanzillotti¹; ¹Politecnico di Torino, Italy
12. Sep 18 10:00 10:30 8.7.2 STRUCTURAL DESIGN AND ANALYSIS OF A QUADROTOR FIXED-WING HYBRID UAV WING
W. Fang, China; H. Ma, China; H. Zhang, China
12. Sep 18 10:30 11:00 8.7.3 STRUCTURAL SIZING OF A ROTORCRAFT FUSELAGE USING AN INTEGRATED DESIGN APPROACH
D.B. Schwinn¹, P. Weiand¹, M. Schmid¹, M. Buchwald¹; ¹German Aerospace Center (DLR), Germany
12. Sep 18 11:00 11:30 8.7.4 AN ACTIVE-PASSIVE NONLINEAR FINITE ELEMENT MODEL FOR ELECTROMECHANICAL COMPOSITE MORPHING BEAMS
R.B. Olympio¹, M.V. Donadon¹, S.G.P Castro, EMBRAER, Brazil; ¹ITA, Brazil
12. Sep 18 11:30 12:00 8.7.5 STRUCTURAL OPTIMIZATION AND PROPOSITION OF PRE-SIZING PARAMETERS FOR UAVS WING SPARS
F.A. Fenelon¹, G.F.S. Neves¹, R.S. Martins¹; ¹Universidade Federal de Minas Gerais, Brazil
9.7Fan and Propeller
Chair(s): Yimer, I., Lamiscarre, B.
Track 9
05 - Propulsion
12. Sep 18 09:30 10:00 9.7.1 STUDY ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLERS WITH PROPLETS
X. Yang¹, J. Xu¹, B. Wang¹, C. Song¹, S. Zhang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
12. Sep 18 10:00 10:30 9.7.2 NOVEL JET ENGINE ACOUSTIC LINER WITH IMPROVED BROADBAND NOISE ABSORPTION
K. Hoeschler, Brandenburg Technische Universität Cottbus-Senftenberg, Germany; E. Sarradj, Technische Universität Berlin, Germany; N. Modler, Technische Universität Dresden, Germany; L. Enghardt, German Aerospace Center, Germany
12. Sep 18 10:30 11:00 9.7.3 CERTAIN ASPECTS OF FAN MODEL STAGE DESIGNING FOR ADVANCED TURBOFANS
S.V. Pankov¹, V.I. Mileshin¹, I.K. Orekhov¹, V.A. Fateev¹; ¹Central Institute of Aviation Motors, Russia
12. Sep 18 11:00 11:30 9.7.4 BIMODAL UNMANNED VEHICLE: PROPULSION SYSTEM INTEGRATION AND WATER/AIR INTERFACE TESTING
A. Bacciaglia¹, D. Guo², P. Marzocca², C. Bil², A. Ceruti¹; ¹University of Bologna, Italy ;²RMIT University, Australia
12. Sep 18 11:30 12:00 9.7.5 PARAMETRIC INVESTIGATION OF EESC-USP AEROACOUSTIC FAN RIG
R.G. Cuenca, UFSC, Brazil; P. Celso Jr.¹, B.M. Rocamora¹; ¹EESC-USP, Brazil
10.7Flight Control 1
Chair(s): Vian, J.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
12. Sep 18 09:30 10:00 10.7.1 QUASI-LPV MODELING AND PARAMETER-DEPENDENT OPTIMAL CONTROL OF MORPHING WING AIRCRAFT
J. Lee¹, Y. Kim¹; ¹Seoul National University, South Korea
12. Sep 18 10:00 10:30 10.7.2 AERODYNAMIC ANALYSIS AND CONTROL ALLOCATION FOR ASYMMETRIC VARIABLE SWEEP AIRCRAFT WITH FLEXIBLE TRAILING EDGE
H. Ma¹, B.F. Song¹, Y. Pei¹, Z.W. Chen¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
12. Sep 18 10:30 11:00 10.7.3 EFFECTS OF TAILORED CONTROL SURFACE COMPLIANCE ON AIRCRAFT STABILITY AND CONTROL
P. Krus, Linköping university, Sweden; B. Lantto, Saab AB, Sweden; M.A. Rodriguez¹, E. Villani¹; ¹Instituto Technologico Aeronautica, Italy
12. Sep 18 11:00 11:30 10.7.4 DIGITAL HYDRAULICS IN AEROSPACE APPLICATIONS: SLIDING MODE OF QUANTIZED CONTROL AND LMI APPROACH
L.P.G. Pinto¹, P. Krus¹, V.J. De Negri, Universidade Federal de Santa Catarina, Brazil; ¹Linköping University, Sweden
12. Sep 18 11:30 12:00 10.7.5 A LOW COST MODEL AIRCRAFT FLIGHT RESEARCH FACILITY IN WIND TUNNEL
B.W. Nie, National University of Defense Technology, China; L.L. Guo¹, F. Cen¹, O. Sename², L. Dugard²; ¹China Aerodynamics Research and Development Center, China ;²Univ. Grenoble Alpes, CNRS, Grenoble INP, GIPSA-lab, France
11.7UAS Flight Test
Chair(s): Götzendorf-Grabowski, T.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
12. Sep 18 09:30 10:00 11.7.1 METHODS FOR EFFICIENT FLIGHT TESTING AND MODELLING OF REMOTELY PILOTED AIRCRAFT WITHIN VISUAL LINE-OF-SIGHT
A. Sobron¹, D. Lundström¹, R. Larsson², P. Krus¹, C. Jouannet²; ¹Linköping University, Sweden ;²Saab Aeronautics, Sweden
12. Sep 18 10:00 10:30 11.7.2 VERTICAL LANDING OF A FIXED-WING UAV USING THE FLAT SPIN
S. Higashino, Kyushu University, Japan; K. Nakama, Kyushu University, Graduate Student, Japan
12. Sep 18 10:30 11:00 11.7.3 PLANNING, IMPLEMENTATION, AND EXECUTION OF AN AUTOMATIC FIRST FLIGHT OF A UAV
M.E. Kügler¹, F. Holzapfel¹; ¹Technical University of Munich, Inst. of Flight System Dynamics, Germany
12. Sep 18 11:00 11:30 11.7.4 SAFETY FLIGHT TESTING FOR CARGO UAV DEVELOPMENT
Kakuya Iwata¹, Keisuke Yamada¹, Ryuzo Horiuchi¹, Akiya Kamimura¹; ¹National Institute of Advanced Industrial Science and Technology, Japan
12. Sep 18 11:30 12:00 11.7.5 ON BOARD SLAM FOR INDOOR MAV USING A LASER RANGE FINDER
K.-S. Sibilski, Air Force Institute of Technology, Poland
12.7Airport / TMA Procedures & Environmental Impact
Chair(s): Reichmuth, J., Senac, P.
Track 12
09 - Air Transport System Efficiency
12. Sep 18 09:30 10:00 12.7.1 THE USE OF SYNTHETIC VISION TOOLS IN THE CONTROL TOWER ENVIRONMENT: THE RETINA CONCEPT
S. Bagassi¹, F. De Crescenzio ¹, S. Piastra¹; ¹University of Bologna, Italy
12. Sep 18 10:00 10:30 12.7.2 A NOVEL CONTROL APPROACH TO IMPROVE SPEED COMMANDS AND PILOT WORKLOAD FOR FLIGHT-DECK BASED INTERVAL MANAGEMENT
T. Riedel, Keio University / Electronic Navigation Research Institute, Japan
12. Sep 18 10:30 11:00 12.7.3 STUDY ON THE ARRIVAL MANAGER MAXIMIZING THE BENEFIT OF FOUR-DIMENSIONAL TRAJECTORY BASED OPERATIONS
D. Toratani¹, N.K. Wickramasinghe¹, E. Itoh¹; ¹Electronic Navigation Research Institute, Japan
12. Sep 18 11:00 11:30 12.7.4 NONLINEAR MODEL PREDICTIVE CONTROL FOR OPTIMAL AIRCRAFT SEQUENCING
B. Grüter¹, J. Diepolder¹, P. Piprek¹, T. Akman¹, F. Holzapfel¹; ¹Technical University of Munich, Germany
12. Sep 18 11:30 12:00 12.7.5 A FRAMEWORK TO ASSESS FUTURE AIRPORT NOISE APPLIED TO A TWO-RUNWAY AIRPORT
F. Will¹, M. Hornung¹; ¹Technical University of Munich, Germany
Reserve Paper 12.7.R INTEGRATED ARRIVAL AND DEPARTURE MANAGEMENT FOR JEJU INTERNATIONAL AIRPORT
D. Jeon¹, Y. Eun¹, H. Kim¹, S. Kim¹, E. Oh¹, M. Jeong¹; ¹Korea Aerospace Research Institute, South Korea

12:00 - 13:00Lunch

0.8General Lecture IV - Developing and flying the Gripen E - M. Wandt, SAAB, Sweden
Chair: G. Holmberg, ICAS treasurer
12. Sep 18 13:00 13:45

1.8Design Education 2
Chair(s): Bagassi, S.
Track 1
01 - Aircraft Design and Integrated Systems
12. Sep 18 14:00 14:30 1.8.1 STUDY ON EVALUATION METHODS OF UNDERGRADUATE AIRCRAFT OVERALL DESIGN COURSE BASED ON TEAM DESIGN COMPETITION
Z.-K. Chen¹, H. Liu¹, C.-G. Yang¹; ¹School of Aeronautic Science and Engineering, Beihang University, China
12. Sep 18 14:30 15:00 1.8.2 AN OVERVIEW OF THE FIRST PARAGUAYAN NEAR-SPACE EXPLORATION USING A HIGH ALTITUDE BALLOON
A. Jara¹, F. Kanazawa¹, L. Vielman, AEP, Paraguay; J. Kurita¹; ¹FPUNA, Paraguay
12. Sep 18 15:00 15:30 1.8.3 ELECTRIC VTOL UAV CONFIGURATION STUDIES AND OPTIMIZATION WITHIN AIRCRAFT DESIGN PRACTICAL COURSE AT TECHNICAL UNIVERSITY OF MUNICH
C. Rößler¹, M. Hornung¹; ¹Technical University of Munich, Institute of Aircraft Design, Germany
2.8Maintenance Management
Chair(s): Chaves, C., Scott, M.
Track 2
11 - Operations and Sustainment
12. Sep 18 14:00 14:30 2.8.1 DRONES AS AN EMERGING PREDICTIVE MAINTENANCE TOOL: IMPLEMENTATION OF A DRONE WORKSHOP, FOR THE ENRICHMENT OF NEW PROFESSIONAL SKILLS IN THE STUDENTS OF MAINTENANCE CAREERS OF THE TECHNOLOGICAL UNIVERSITY OF JALISCO
J. Sandoval, Universidad Autónoma Metropolitana Unidad Lerma, Mexico; J.-J. Barron, Universidad Tecnológica de Jalisco, Mexico
12. Sep 18 14:30 15:00 2.8.2 AIRLINE MAINTENANCE: A PROPOSAL ENVISIONING DIGITAL TRANSFORMATION
L.B. Koslosky¹, N. Fisk, Boeing, United States; P. Krus, Linköping University, Sweden; L. Pereira¹; ¹Universidade Federal do ABC, Brazil
12. Sep 18 15:00 15:30 2.8.3 OPTIMAL SHAPE OF REPAIR PATCHES IN COMPOSITES
L. Echer¹, C.E. de Souza, Federal University of Santa Maria, Brazil; R.J. Marczak¹; ¹Federal University of Rio Grande do Sul, Brazil
3.8Structural Health Monitoring 1
Chair(s): Ikeda, T.
Track 3
04.1 - Material Issues, Fatigue and Damage Tolerance
12. Sep 18 14:00 14:30 3.8.1 OPTIMIZATION OF THE COEFFICIENT OF PROBABILITY DISTRIBUTION FUNCTION OF THE SENSING PATHS FOR INSTANTANEOUS BASELINE DAMAGE DETECTION USING GENETIC ALGORITHM
P.K. Motamed¹, A. Abedian¹, M. Nasiri¹; ¹Sharif University of Technology, Iran
12. Sep 18 14:30 15:00 3.8.2 DEVELOPMENT OF STRUCTURAL HEALTH MONITORING METHODS THROUGH THE ANALYSIS OF KINETICS OF LOCAL STRESS-STRAIN STATE
A.A. Bautin¹, Y.A. Svirskiy¹; ¹TsAGI, Russia
12. Sep 18 15:00 15:30 3.8.3 DETECTION OF HIDDEN FATIGUE CRACKS IN RIVETED LAP JOINTS USING WAVELET TRANSFORM AND NEURAL NETWORKS
A.Abedian abedian, sharif university of technology, Iran
Reserve Paper 3.8.R DEVELOPMENT OF METHODS FOR DETERMINING CRACK RESISTANCE PARAMETERS FOR STATIC AND FATIGUE LOADING FOR POLYMER COMPOSITE MATERIALS
V.L. Tokar¹, Y.V. Koroleva¹, Y.A. Svirsky¹; ¹TsAGI, Russia
4.8Laminar Flow and Transition
Chair(s): Alves, L., Castro, L.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
12. Sep 18 14:00 14:30 4.8.1 VALIDATION OF INTERMITTENCY MODEL FOR TRANSITION PREDICTION IN A RANS FLOW SOLVER
D. de Rosa¹, P. Catalano¹; ¹CIRA - Italian Aerospace Research Centre, Italy
12. Sep 18 14:30 15:00 4.8.2 ON THE CALIBRATION OF THE INTERMITTENCY TRANSITION TURBULENCE MODEL FOR WIND TURBINE AIRFOIL BY MACHINE LEARNING ALGORITHM
M.A. Abd Bari¹, A. Da Ronch¹, M. Panzeri, Noesis Solutions, Belgium; J. Drofelnik¹; ¹University of Southampton, United Kingdom
12. Sep 18 15:00 15:30 4.8.3 EFFECT OF CONTROLLED PERIODIC ROUGHNESS ON GOERTLER VORTICES IN HYPERSONIC COMPRESSION RAMP FLOW
P.V. Chuvakhov¹, V.N. Radchenko¹, E.A. Alexandrova¹, V.Y. Borovoy¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
5.8Aerodynamic Experiments
Chair(s): Takana, E.
Track 5
03.2 - Experimental Aerodynamics
12. Sep 18 14:00 14:30 5.8.1 INFLUENCE OF AIRFRAME STIFFNESS ON THE AERODYNAMIC COEFFICIENTS OF A HIGH ASPECT RATIO WING
L.A.V. Pelegrineli¹, F.F. Liorbano¹, H.O.H. Natori¹, R.A. Angélico¹; ¹ University of São Paulo, São Carlos School of Engineering, Brazil
12. Sep 18 14:30 15:00 5.8.2 HORIZONTAL TAIL LOCAL ANGLE-OF-ATTACK AND TOTAL PRESSURE MEASUREMENTS THROUGH STATIC PRESSURE PORTS AND KIEL PITOT
R.M. Granzoto¹, L.A. Algodoal¹, G.J. Zambrano¹, G.G. Becker¹; ¹Embraer, Brazil
12. Sep 18 15:00 15:30 5.8.3 EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF A UAV FOR SUPERFICIAL VOLCANO SURVEILLANCE
P.D. Bravo-Mosquera¹, L. Botero-Bolivar¹, D. Acevedo-Giraldo¹, H.D. Cerón-Muñoz¹, F.M. Catalano¹; ¹EESC-USP, Brazil
6.8Instability Control
Chair(s): Fu, S.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
12. Sep 18 14:00 14:30 6.8.1 ON THE WAVE-CANCELLING NATURE OF BOUNDARY LAYER TRANSITION CONTROL
K. SASAKI¹, P. Morra², A.V.G. Cavalieri¹, A. Hanifi², D.S. Henningson²; ¹ITA, Brazil ;²KTH, Sweden
12. Sep 18 14:30 15:00 6.8.2 ACTUATOR AND SENSOR PLACEMENT FOR CLOSED-LOOP CONTROL OF CONVECTIVE INSTABILITIES
G.A. Freire¹, A.V.G. Cavalieri¹, F.J. Silvestre¹; ¹ITA, Brazil
12. Sep 18 15:00 15:30 6.8.3 RESOLVENT-BASED CONTROL OF STREAKS IN BOUNDARY LAYERS
P.A.S. Nogueira¹, A.V.G. Cavalieri¹, A. Hanifi², D.S. Henningson²; ¹Instituto Tecnológico de Aeronáutica, Brazil ;²KTH Royal Institute of Technology, Sweden
7.8New Structural Design 2: Morphing Structures
Chair(s): Ikeda, T.
Track 7
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
12. Sep 18 14:00 14:30 7.8.1 STRUCTURAL INTEGRITY DIAGNOSIS FOR AGING TRANSPORT AIRCRAFT BASED ON FLIGHT DATA
H. Wang, College of General Aviation, Wenzhou University, China
12. Sep 18 14:30 15:00 7.8.2 APPLICATION RESEARCH OF ZIMMERMAN-WEISSENBURGER-YANG METHOD FOR PREDICTING FLUTTER BOUNDARY
Y. FEI, Shang Hai Aircraft Design and Research Institute of COMAC, China
12. Sep 18 15:00 15:30 7.8.3 A RESEARCH OF MULTIDISCIPLINARY DESIGN OPTIMIZATION ALGORITHM FOR FIGHT VEHICLE DESIGN
X. Yan¹, Z. Liu¹, Y. Yang¹; ¹CARDC, China
8.8Aeroelasticity 4 : General
Chair(s): Amiryants, G.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
12. Sep 18 14:00 14:30 8.8.1 EXPERIMENTAL AND NUMERICAL STUDIES OF FLUTTER CHARACTERISTICS OF AN ALL-MOVING CONTROL SURFACE AGAINST GAP EFFECTS
Y. Bai¹, W. Qian¹, X. Chen¹; ¹Dalian University of Technology, China
12. Sep 18 14:30 15:00 8.8.2 MULTIDISCIPLINARY METHODS FOR WING FLIGHT SHAPE ANALYSIS - EFFECT OF THE GEOMETRIC NONLINEAR STRUCTURE FOR STATIC PULL-UP
A.A. Verri¹, C.T. Jorge¹, A.F. Bizarro¹, F.L.S. Bussamra, ITA, Brazil; H.N.S. Júnior¹, C.E.S. Cesnik, UniMich, United States; ¹Embraer S/A, Brazil
12. Sep 18 15:00 15:30 8.8.3 RESULTS AND COMPARISON OF NUMERICAL SIMULATION AND THE TESTING OF LUG MANUFACTURED BY COMPOSITE MATERIAL BY RTM PROCESS
G.C. Fonseca, Embraer - Centro de Engenharia e Tecnologia - Minas Gerais, Brazil; S.F.M. Almeida, ITA - Instituto Tecnológico de Aeronáutica, Brazil
9.8High Speed Propulsion 1
Chair(s): Kukshinov, N.
Track 9
05 - Propulsion
12. Sep 18 14:00 14:30 9.8.1 INVESTIGATION ON AERO-PROPULSIVE BALANCE FOR HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECT
A.A. Gubanov¹, D.S. Ivanyushkin¹, N.V. Kukshinov², A.N. Prokhorov², V.A. Talyzin¹, N.V. Voevodenko¹; ¹Central Aerohydrodynamic Institute named after Professor N.E. Zh, Russia ;²Central Institute of Aviation Motors named after P.I. Baranov, Russia
12. Sep 18 14:30 15:00 9.8.2 COMPLEX NUMERICAL AND EXPERIMENTAL RESEARCH OF HEXAFLY-INT HIGH-SPEED CIVIL AICRAFT MODEL
V.Y. Aleksandrov¹, S.N. Batura¹, O.V. Gouskov¹, N.V. Kukshinov¹, A.N. Prokhorov¹, A.V. Rudinsky¹; ¹Central Institute of Aviation Motors named after P.I. Baranov , Russia
12. Sep 18 15:00 15:30 9.8.3 INFLUENCE OF TEMPERATURE FACTOR ON THE CHARACTERISTICS OF HIGH-SPEED AIR-BREATHING ENGINE INLETS
O.V. GUSKOV, MIPT, Russia
10.8Flight Dynamics & Identification 1
Chair(s): Korsun, O.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
12. Sep 18 14:00 14:30 10.8.1 CLOSED-LOOP SYSTEM IDENTIFICATION OF A LARGE FLEXIBLE AIRCRAFT USING SUBSPACE METHODS
R.C.M.G. Barbosa¹, L.C.S. Góes¹; ¹ITA, Brazil
12. Sep 18 14:30 15:00 10.8.2 RECURSIVE AERODYNAMIC PARAMETER IDENTIFICATION OF A FIGHTER JET FLYING IN TURBULENT AIR
C. Grillo, Università di Palermo, Italy
12. Sep 18 15:00 15:30 10.8.3 APPLICABILITY OF GEOMETRICALLY-LINEAR STRUCTURAL-DYNAMIC MODELS FOR THE FLIGHT DYNAMICS OF ARBITRARILY-FLEXIBLE AIRCRAFT
A.B. Guimarães Neto¹, F.L. Cardoso-Ribeiro¹, F.J. Silvestre¹; ¹ITA, Brazil
Reserve Paper 10.8.R SYSTEM IDENTIFICATION OF A SUBSCALE FIGHTER AIRCRAFT
L. M. Nepomuceno, ITA Technological Institute of Aeronautics, Brazil
11.8Air Data
Chair(s): ,
Track 11
07 - Systems, Subsystems and Equipment
12. Sep 18 14:00 14:30 11.8.1 SMART FAULT-TOLERANT AIR-DATA SENSOR FOR AIRCRAFT FLOW ANGLES MEASUREMENT
G. Di Rito¹, F. Schettini¹; ¹Università di Pisa - Dip. di Ing. Civile ed Industriale, Italy
12. Sep 18 14:30 15:00 11.8.2 DESIGN CRITERIA OF A THERMAL MASS FLOW SENSOR FOR AIRCRAFT AIR DATA APPLICATIONS
R.A. Souza¹, M.L. Oliveira¹, S.P.L. Vieira¹, W.O. Avelino¹, C.F.R. Oliveira¹, D.W. de Lima Monteiro¹, F.S. Torres¹, R.M.O. Hansen, SDU, Denmark; ¹UFMG, Brazil
12. Sep 18 15:00 15:30 11.8.3 AN AIRBORNE DATA BUS NETWORK SYSTEM OF INTERFACE ADAPTIVE AND FLEXIBLE CONTROL
Z. Dai¹, Z. Qiu, Xi'an Aeronautics Computing Technique Research Institute, China; L. Shi¹; ¹ChengDu Aircraft Design & Research Institute, China
12.8On Demand Mobility: Integration in Civil Airpace
Chair(s): Kageyama, K.
Track 12
09 - Air Transport System Efficiency
12. Sep 18 14:00 14:30 12.8.1 SIMULATION STUDY FOR VFR AIRCRAFT AND SMALL UNMANNED AIRCRAFT SYSTEMS (SUAS) MIXED OPERATIONS IN LOW LEVEL AIRSPACE
H. Hirabayashi¹, D. Toratani¹, A. Kohmura¹; ¹ENRI, Japan
12. Sep 18 14:30 15:00 12.8.2 URBAN AIR TRANSPORTATION JOURNEY TIME COMPARISON FOR MELBOURNE METROPOLITAN AREA
L. Swadesir¹, C. Bil¹; ¹RMIT University, Australia
12. Sep 18 15:00 15:30 12.8.3 ADAPTIVE LANDING SEQUENCING USING BIPARTITE GRAPHS AND PERFECT MATCHING
M. Hickson¹, C. Bil¹; ¹RMIT University, Australia

15:30 - 16:00Break

1.9Unconventional Concepts 2
Chair(s): Kimmel, B.
Track 1
01 - Aircraft Design and Integrated Systems
12. Sep 18 16:00 16:30 1.9.1 FLEXFLOIL SHAPE ADAPTIVE CONTROL SURFACES-FLIGHT TEST AND NUMERICAL RESULTS
S. Kota, FlexSys Inc, United States; J.R.R.A. Martins, University of Michigan, United States
12. Sep 18 16:30 17:00 1.9.2 FEASIBILITY STUDY OF MODIFYING A BASELINE KEROSENE AIRCRAFT TO A LH2 POWERED VERSION
W. Xie¹, Z. Duan¹, H. Smith, Cranfield University, United Kingdom; ¹AVIC The First Aircraft Institute, China
12. Sep 18 17:00 17:30 1.9.3 DEVELOPMENT OF THE REGENERATIVE SOARER: THEORETICAL AND PRACTICAL ASPECTS
R.C. Carvalho, EMBRAER S.A., Brazil
12. Sep 18 17:30 18:00 1.9.4 DEVELOPMENT OF A NOVEL AERIAL PLATFORM WHICH MERGES THE CONCEPT OF AIRSHIPS AND TETHERED AEROSTATS
J.S. Santos¹, B.A. de Azevedo¹, L.C.S. Góes¹, R.S. Pant, Indian Institute of Technology Bombay, India; ¹Instituto Tecnológico de Aeronáutica, Brazil
2.9Novel Application of MDO in Aircraft Design 3
Chair(s): Lefebvre, T.
Track 2
01 - Aircraft Design and Integrated Systems
12. Sep 18 16:00 16:30 2.9.1 INTERGRATED SYSTEM FOR UNIFICATION OF AIRCRAFT CONCEPTUAL DESIGN APPLICATIONS
E. Vogiatzis¹, R.-C. Munjulury¹, P. Krus¹; ¹Linköpings university, Sweden
12. Sep 18 16:30 17:00 2.9.2 STRUCTURAL DESIGN AND TESTING OF A TAILORED SKIN SINGLE DUCT (TSSD) FIN APPLICATION
M. Schneider¹, M. Horn¹, S. Ritt¹, A. Seitz¹; ¹DLR, Germany
12. Sep 18 17:00 17:30 2.9.3 STUDIES ON THE APPLICATION OF MOEA/D TO AERODYNAMIC OPTIMIZATION DESIGN
X.Q. Zhu¹, Z.H Gao¹, Z.W. Chen¹; ¹Northwestern Polytechnical University, China
3.9Advanced Manufacturing and Non Destructive Testing
Chair(s): ,
Track 3
04.1 - Material Issues, Fatigue and Damage Tolerance
12. Sep 18 16:00 16:30 3.9.1 ARAMID-FIBER REINFORCED ELASTOMERS AS FUTURE AIRCRAFT ACTUATORS - A PROOF-OF-CONCEPT INVESTIGATION
M. Kanerva¹, M. Poikelispää¹, P. Antunes, Aveiro University, Portugal; ¹Tampere University of Technology, Finland
12. Sep 18 16:30 17:00 3.9.2 ON EQUIVALENCE OF POLYMER COMPOSITE MATERIALS STRUCTURES LOADING PROGRAMS UNDER FULL-SCALED SERVICE CYCLE TESTING
A.V. Pankov¹, V.V. Konovalov¹; ¹TsAGI, Russia
12. Sep 18 17:00 17:30 3.9.3 STUDY OF EXTERNAL FACTOR COMBINATIONS EFFECT ON CFRP STRUCTURE UTILYZING ULTRASONIC MICROSCOPY
T. Ryzhova¹, A. Shanygin¹, V. Scherbakov¹, Y. Petronyuk², V. Levin², E. Morokov²; ¹Central Aerohydrodynamic Institute, Russia ;²Institute of Biochemical Physics of RAS, Russia
12. Sep 18 17:30 18:00 3.9.4 NON-CONTACT MEASUREMENTS OF DEFORMATION OF LARGE-SIZED AIRCRAFT WING USING OPTICAL VIDEOGRAMMETRY METHOD
K.A. Kuruliuk, TsAGI, Russia
4.9RANS Models
Chair(s): Antunes, A., Viviani, A.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
12. Sep 18 16:00 16:30 4.9.1 MULTIPHASE TURBULENCE MODELS FOR SCRAMJETS AND ABLATING WALLS
K.E.Son Son, Russia
12. Sep 18 16:30 17:00 4.9.2 2D-RANS APPROACH TO STUDY A TURBULENT SEPARATED FLOW USING BSL EARSM MODEL
S.M. Hanriot¹, M.D. Queiroz¹, G.L.F. Vasconcellos¹; ¹PUC Minas, Brazil
12. Sep 18 17:00 17:30 4.9.3 NUMERICAL COMPARISON OF STEADY DISTURBANCES IN THE WAKE OF PERIODIC BLOW-SUCTION AND ROUGHNESS ELEMENTS
P.V. Chuvakhov¹, S.V. Alexandrov¹, E.A. Alexandrova, Central Aerohydrodynamic Institute (TsAGI), Russia; ¹Moscow Institute of Physics and Technology (MIPT), Russia
12. Sep 18 17:30 18:00 4.9.4 NUMERICAL INVESTIGATION OF FLOW STRUCTURE OF DIFFERENTIAL EJECTOR
H.Y. Zhang¹, Y.S. Yu¹, Q. Chen¹; ¹China Aerodynamics Research and Development Centre, China
5.9History of Aeronautics
Chair(s): Lott, M., Brandao, M.P.
Track 5
12 - Host nation
12. Sep 18 16:00 16:30 5.9.1 THE SANTOS-DUMONT LEGACY TO AERONAUTICS
M. Pazini Brandão, Technological Institute of Aeronautics, Brazil
12. Sep 18 16:30 17:00 5.9.2 BRAZILIAN AVIATION HISTORY: THE UNIVERSITY OF SÃO PAULO CASE
F.M. Catalano, University of São Paulo -EESC-USP, Brazil
12. Sep 18 17:00 17:30 5.9.3 THE STUDY OF TURBORAMJETS IN CIAM
M. Tskhovrebov¹, V. Solonin¹, V. Palkin¹, P. Kadjardouzov¹; ¹CIAM, Russia
12. Sep 18 17:30 18:00 5.9.4 HISTORY OF AVIATION IN MINAS GERAIS
E. Bauzer Medeiros, Brazil
6.9Buffet and Separation Control
Chair(s): Breitsamter, C., Prince, S.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
12. Sep 18 16:00 16:30 6.9.1 EFFECTIVE PLASMA BUFFET AND DRAG CONTROL FOR LAMINAR TRANSONIC AIROFOIL
P.A. Polivanov¹, A.A. Sidorenko¹; ¹ITAM SB RAS, Russia
12. Sep 18 16:30 17:00 6.9.2 CONTROL OF STRONG SEPARATION OF FLOW VIA SIMULTANEOUS-BLOWING-SUCTION TECHNIQUE
W. Stalewski, INSTITUTE of AVIATION, Poland
12. Sep 18 17:00 17:30 6.9.3 NUMERICAL OPTIMIZATION OF FLOW CONTROL BY TANGENTIAL JET BLOWING ON TRANSONIC AIRFOIL
K.A. Abramova¹, V.G. Soudakov¹; ¹TsAGI, Russia
12. Sep 18 17:30 18:00 6.9.4 OVERVIEW ON THE INFLUENCE OF COANDA BLANKET CURVATURE ON COANDA DEVICE PERFORMANCE
Harijono DJOJODIHARDJO, Insitute for the Advancement of Aerospace Science and Technology, Indonesia
7.9High Speed Aerodynamics
Chair(s): Gubanov, A.
Track 7
03.4 - Applied Aerodynamics
12. Sep 18 16:00 16:30 7.9.1 ENGINE EXHAUST NOZZLE PLUME EFFECTS ON THE SONIC BOOM FOR A TYPE OF HYPERSONIC LONG-RANGE CIVIL VEHICLE
Zhansen Qian¹, Yan Leng¹, Zhongchen Liu¹; ¹AVIC Aerodynamics Research Institute, China
12. Sep 18 16:30 17:00 7.9.2 PRELIMINARY STUDY OF THE AERODYNAMIC CHARACTERISTICS OF KRUEGER FLAP ON THE SST CONFIGURATION
D. Kwak, JAXA, Japan; K. Ohira, Ryoyu Systems, Japan
12. Sep 18 17:00 17:30 7.9.3 HIGH SPEED DRAG REDUCTION OPTIMIZATION FOR PROJECTILES
T. Wan, Department of Aerospace Engineering, Tamkang University, Taiwan
12. Sep 18 17:30 18:00 7.9.4 ADVANCED SONIC BOOM ANALYSIS USING FULL-FIELD SIMULATION
R. Yamashita, The University of Cambridge, United Kingdom
8.9Aeroelasticity 5 : General
Chair(s): Djojodihardjo, D.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
12. Sep 18 16:00 16:30 8.9.1 GLOBAL SENSITIVITY ANALYSIS OF TRANSONIC FLUTTER USING A COUPLED CFD-CSD SOLVER
R. Sandhu, Carleton University, Canada; W.X. Yuan, National Research Council (NRC) Canada, Canada; D. Poirel, Royal Military College (RMC) of Canada, Canada
12. Sep 18 16:30 17:00 8.9.2 NUMERICAL AND EXPERIMENTAL VALIDATION OF UNITIZED BEAM MODEL
F. Danzi¹, E. Cestino¹, G. Frulla¹, J.-M. Gibert, Purdue University, United States; ¹Politecnico di Torino, Italy
12. Sep 18 17:00 17:30 8.9.3 ASSESSMENT OF THE AERODYNAMICS AND AEROELASTICITY OF FLAPPING WING USING LINEARIZED COMPUTATIONAL METHOD
H. Djojodihardjo, Insitute for the Advancement of Aerospace Science and Technology, Indonesia; A.K. Joyodiharjo, The Institute for the Advancement of Aerospace Science and Techn, Indonesia
12. Sep 18 17:30 18:00 8.9.4 STRAIN GAGES FULL BRIDGE INSIDE COMPOSITE LAYERS TARGETING WING SHAPE FEEDBACK FOR FLIGHT CONTROL LAWS
A.A. Verri¹, J. Barros¹, F.L.S. Bussamra², F.J. Silvestre², F.J.O. Moreira¹, A.B. Guimarães Neto², C.E.S. Cesnik, UniMich, United States; J.S. Martins²; ¹Embraer S/A, Brazil ;²ITA, Brazil
9.9High Speed Propulsion 2
Chair(s): Kukshinov, N.
Track 9
05 - Propulsion
12. Sep 18 16:00 16:30 9.9.1 CFD MODELLING TO OPTIMIZE THE MAXIMUM THRUST IN SCRAMJET ENGINE AND ANALYSIS OF ITS OPERATION PERFORMANCE
M-P Pires, IME, Brazil
12. Sep 18 16:30 17:00 9.9.2 RESEARCH OF PROPULSION ENGINES FOR ADVANCE REUSABLE TSTO AEROSPACE SYSTEM
A.I. Lanshin¹, O.V. Sokolova¹, Yu.M. Shikhman¹, V.E. Shlyakotin¹; ¹CIAM, Russia
12. Sep 18 17:00 17:30 9.9.3 SIMULTANEOUS MEASUREMENTS OF TEMPERATURE AND HEAT FLUX IN SUPERSONIC COMBUSTOR BY ITO THIN FILM THERMOCOUPLE
X.H. Jin¹, B.H. Ma¹, T. Qiu¹; ¹Northwestern Polytechnical University, China
12. Sep 18 17:30 18:00 9.9.4 GROUND FACILITY TESTS OF HIGH SPEED RAMJET DEMONSTRATORS
V.Y. Aleksandrov¹, A.N. Prokhorov¹, V.L. Semenov¹; ¹Central Institute of Aviation Motors , Russia
10.9Flight Dynamics & Identification 2
Chair(s): Watanabe, Y.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
12. Sep 18 16:00 16:30 10.9.1 BIO-DYNAMIC STABILITY ANALYSIS OF A GREBE DURING MIGRATION
J Feaster, Virginia Tech, United States
12. Sep 18 16:30 17:00 10.9.2 DYNAMIC REACTION OF AN AIRPLANE TO TRAILING VORTICES GENERATED BY ANOTHER AIRPLANE
G. Kowaleczko, Air Force Institute of Technology, Poland
12. Sep 18 17:00 17:30 10.9.3 MATHEMATICAL MODEL OF COMMERCIAL AIRPLANE DYNAMICS AT STALL
P.V. Kuzmin¹, N.A. Surkov¹, Y.F. Shelyukhin¹; ¹TsAGI, Russia
12. Sep 18 17:30 18:00 10.9.4 IDENTIFICATION OF THE LATERAL-DIRECTIONAL MODEL OF THE VECTOR-P, UNMANNED AERIAL VEHICLE
C. Fischer, Instituto Tecnológico de Aeronáutica and IFSP, Brazil; L.M. Nepomuceno¹, R.G.A. Silva¹, L.C.S. Góes¹; ¹Instituto Tecnológico de Aeronáutica, Brazil
11.9System Design
Chair(s): Peters, M.
Track 11
07 - Systems, Subsystems and Equipment
12. Sep 18 16:00 16:30 11.9.1 WIND SHEAR PARAMETER ESTIMATION FOR DYNAMIC SOARING WITH UNMANNED AERIAL VEHICLES
D. Liu, China Aerodynamics Research and Development Center, China; X. Gao, National University of Defense Technology, China
12. Sep 18 16:30 17:00 11.9.2 A METHODOLOGY FOR PRELIMINARY SIZING OF A VEHICLE ENERGY MANAGEMENT SYSTEM FOR A HYPERSONIC VEHICLE.
R. Fusaro¹, D. Ferretto¹, V. Vercella¹, N. Viola¹, V. Fernandez Villace², J. Steelant ²; ¹Politecnico di Torino, Italy ;²ESA-ESTEC, Netherlands
12. Sep 18 17:00 17:30 11.9.3 INTEGRATION OF ON-BOARD SYSTEMS PRELIMINARY DESIGN DISCIPLINE WITHIN A COLLABORATIVE 3RD GENERATION MDO FRAMEWORK
L. Boggero¹, M. Fioriti², F. Tomasella², P.D. Ciampa¹; ¹German Aerospace Center, Germany ;²Politecnico di Torino, Italy
12. Sep 18 17:30 18:00 11.9.4 FAULT DIAGNOSIS METHOD STUDY FOR COMPLEX SYSTEM BASED ON KALMAN FILTERS
W. Niu¹, J. Cheng, Xi’an Institute of Applied Optics, China; W. Niu¹; ¹AVIC Computing Technique Research Institute, China
12.9Human Factors
Chair(s): Consiglio, M.
Track 12
10 - Safety and Security
12. Sep 18 16:00 16:30 12.9.1 3D AUDIO SUPPORT FOR HELICOPTER PILOTS DURING CONFINED AREA LANDINGS
C. A. Niermann, German Aerospace Center (DLR), Germany
12. Sep 18 16:30 17:00 12.9.2 INDIVIDUALIZING FLIGHT SKILL TRAINING USING SIMULATOR DATA ANALYSIS AND BIOFEEDBACK
J.O. Entzinger¹, T. Uemura¹, S. Suzuki¹; ¹The University of Tokyo, Japan
12. Sep 18 17:00 17:30 12.9.3 DESIGN OF A DISTRIBUTED HUMAN FACTORS LABORATORY FOR FUTURE AIR SYSTEMS
J. Alfredson, Saab, Sweden; B.J.E. Johansson¹, L.G. Trabasso, ITA, Brazil; J. Schminder¹, R. Granlund, RISE, Sweden; R. Gårdhagen¹; ¹Linköping University, Sweden
12. Sep 18 17:30 18:00 12.9.4 CREW TRAINING USING ANIMATION
P.M. Razaboni, Embraer SA, Brazil
Reserve Paper 12.9.R HUMAN RELIABILITY ANALYSIS IN AN AIRCRAFT DECOMPRESSION EVENT
C. Reiser¹, A. Bayma¹, D.A. Fonseca¹; ¹Embraer S/A, Brazil
Reserve Paper 12.9.R 3D PERSPECTIVE VIEWS ON IMMERSIVE HEAD-WORN DISPLAYS - CAN EXOCENTRIC VIEWS INCREASE PILOT SITUATIONAL AWARENESS?
J.M. Ernst, DLR, Germany

Thursday, 13. Sep 2018


7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
0.9General Lecture V - IFAR Plenary Lecture Global Cooperation Leading to New Commercial Supersonic Opportunity - NASA-Dr. Jaiwon Shin TsAGI-Dr. Sergey Chernyshev JAXA-Dr. Hisashi Sano ONERA-Bruno Saijon DLR-Prof. Rolf Henke NLR-Michel Peters
Chair:
13. Sep 18 08:00 09:30

09:30 - 10:00Break

1.10Design Method 2
Chair(s): Rinoie, K., Nicolosi, F.
Track 1
01 - Aircraft Design and Integrated Systems
13. Sep 18 10:00 10:30 1.10.1 PRELIMINARY DESIGN OF A LONG RANGE WINDOWLESS AIRCRAFT CONCEPT
S. Bagassi¹, F. Lucchi¹, M.C. Moruzzi¹; ¹University of Bologna, Italy
13. Sep 18 10:30 11:00 1.10.2 COLLABORATIVE CONCEPTUAL DESIGN OF A MID-RANGE AIRCRAFT UNDER CONSIDERATION OF ADVANCED METHODS FOR TECHNOLOGY ASSESSMEN
J. Hartmann¹, T. Pfeiffer¹, B. Breymann¹, D. Silberhorn¹, E. Moerland¹, M. Weiss¹, B. Nagel¹; ¹DLR, Germany
13. Sep 18 11:00 11:30 1.10.3 STRATEGY AND IMPLEMENTATION OF A PARAMETRIC CAD MODEL FOR R2035 AIRCRAFT STRUCTURE AND EXTERNAL CONFIGURATION
Z.-J. Goraj¹, B. Goliszek¹, M. Kowalski¹, A. Seitz², F. Peter², F. Meller, Airbus Defence and Space GmbH, Germany; ¹Warsaw University of Technology, Poland ;²Bauhaus Luftfahrt e.V., Germany
13. Sep 18 11:30 12:00 1.10.4 AN APPROACH TO ASSESS AIRFRAME WEIGHT REDUCTION PERFORMANCE OF STITCHED COMPOSITE TECHNOLOGIES
J.A. Corman¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States
13. Sep 18 12:00 12:30 1.10.5 NARROW-BODY B737NG PASSENGER CONVERSION TO FREIGHTER
I. Berlowitz, Israel Aerospace Industries, Israel
2.10Aircraft Operations 2
Chair(s): Teixeirada da Cunha, S., Molent, L.
Track 2
11 - Operations and Sustainment
13. Sep 18 10:00 10:30 2.10.1 FUEL-BURN PENALTIES CAUSED BY IRREGULARITIES IN AIRCRAFT SURFACES (ASTEROID PROJECT)
D. Philpott¹, K. Hackett¹, A. Shires², B. Hinchliffe²; ¹IHS Markit (ESDU), United Kingdom ;²University of Leeds, United Kingdom
13. Sep 18 10:30 11:00 2.10.2 PARAMETRIC APPROACH TO OPERATING COSTS ESTIMATION FOR AN INNOVATIVE REGIONAL AIRCRAFT
M. Fioriti¹, N. Viola¹, D. Ferretto¹, V. Vercella¹, S. Cresto Aleina¹, F. Nicolosi², V. Cusati²; ¹Politecnico di Torino, Italy ;²Università di Napoli Federico II, Italy
13. Sep 18 11:00 11:30 2.10.3 COST-BENEFIT ASSESSMENT OF CLIMATE AND WEATHER OPTIMIZED TRAJECTORIES FOR DIFFERENT NORTH ATLANTIC WEATHER PATTERNS
B. Lührs, TUHH, Germany; M. Niklaß¹, C. Frömming¹, V. Grewe¹, V. Gollnick¹; ¹DLR, Germany
13. Sep 18 11:30 12:00 2.10.4 IDENTIFICATION OF OPTIMAL RENDEZVOUS AND SEPARATION AREAS FOR FORMATION FLIGHT UNDER CONSIDERATION OF WIND
T. Marks¹, M. Swaid², B. Lührs², V. Gollnick¹; ¹German Aerospace Center, Germany ;²Technical University Hamburg, Germany
13. Sep 18 12:00 12:30 2.10.5 AIRCRAFT BOARDING AS PART OF AN EFFICIENT 4D TRAJECTORY
M. Schultz, DLR, Germany
3.10Crack and Impact Damage Propagation
Chair(s): Fish, J.
Track 3
04.1 - Material Issues, Fatigue and Damage Tolerance
13. Sep 18 10:00 10:30 3.10.1 STUDY OF ACCIDENTAL IMPACT SCENARIOS FOR COMPOSITE WING DAMAGE TOLERANCE EVALUATION
S. Dubinskii¹, Y. Feygenbaum², V. Senik¹, E. Metelkin²; ¹TsAGI, Russia ;²GosNII GA, Russia
13. Sep 18 10:30 11:00 3.10.2 MULTI-SITE DELAMINATION ANALYSIS USING VIRTUAL CRACK CLOSURE TECHNIQUE FOR A COMPOSITE AIRCRAFT WING FLAP
J. Jokinen¹, M. Kanerva¹, O. Saarela, Aalto University, Finland; ¹Tampere University of Technology, Finland
13. Sep 18 11:00 11:30 3.10.3 INVESTIGATION OF BULGING EFFECTS ON PROPAGATION OF 1-BAY AND 2-BAY LONGITUDINAL CRACKS WITH BROKEN/INTACT STIFFENER
A.S. Kim, TsAGI, Russia
13. Sep 18 11:30 12:00 3.10.4 BALLISTIC RESISTANT ANALYSIS FOR AIRCRAFT WING STRUCTURE
G.R. Zu¹, Y. Pei¹, X.W. Yang¹; ¹Northwestern Polytechnical University, China
13. Sep 18 12:00 12:30 3.10.5 PLY THICKNESS INFLUENCE IN COMPRESSION AFTER IMPACT DAMAGE ON CARBON/EPOXY TEST SPECIMENS
T.H.L. Pinto, UFVJM, Brazil; C.A. Cimini Jr., UFMG, Brazil; S.K. Ha, Hanyang University, South Korea
Reserve Paper 3.10.R NUMERICAL INVESTIGATION OF INFLUENCE OF INITIAL DAMAGES ON STRENGTH PARAMETERS OF CFRP
E. Dubovikov¹, V. Fomin¹, D. Fomin¹, V. Notkin¹, N. Perchits¹, G. Vodovozov¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
4.10Aerodynamic Optimization
Chair(s): Hoeijmakers, H., Conde de Resende, O.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
13. Sep 18 10:00 10:30 4.10.1 AERODYNAMIC DESIGN AND ANALYSIS OF AN INNOVATIVE REGIONAL TURBOPROP CONFIGURATION
F. Nicolosi¹, S. Corcione¹, P. Della Vecchia¹, V. Trifari¹, M. Ruocco¹; ¹University of Study of Naples Federico II, Italy
13. Sep 18 10:30 11:00 4.10.2 PERFORMANCE IMPROVEMENT OF A COMPOUND HELICOPTER ROTOR HEAD BY AERODYNAMIC SHAPE OPTIMIZATION
P. Pölzlbauer¹, D. Desvigne, Airbus Helicopters, France; C. Breitsamter¹; ¹Technical University of Munich, Germany
13. Sep 18 11:00 11:30 4.10.3 A RAPID AERODYNAMIC PREDICTION METHOD FOR UNCONVENTIONAL TRANSONIC AIRCRAFT CONFIGURATIONS
S.A. Prince¹, D. Di Pasquale¹, K.P. Garry¹, C. Nuzzo, Politecnico di Torino, Italy; ¹Cranfield University, United Kingdom
13. Sep 18 11:30 12:00 4.10.4 EVALUATION OF DELTA WING EFFECTS ON THE STEALTH-AERODYNAMIC FEATURES FOR NON-CONVENTIONAL FIGHTER AIRCRAFT
P.D. Bravo-Mosquera¹, A.M. Abdalla¹, F.M. Catalano¹; ¹EESC-USP, Brazil
13. Sep 18 12:00 12:30 4.10.5 DESIGN SPACE EXPLORATION AND FLOW CONTROL FOR A TRANSONIC WING DRAG REDUCTION
Y UTAMA, INSTITUT TEKNOLOGI BANDUNG, Indonesia
5.10Optical Measurement Techniques
Chair(s): Klein, C.
Track 5
03.2 - Experimental Aerodynamics
13. Sep 18 10:00 10:30 5.10.1 FLOW UNSTEADINESS RESEARCHES ON THE BLUNT FIN-INDUCED SHOCK/BOUNDARY LAYER INTERACTIONS
W.H.-R. Ruan, China; X.J.-Z. Zhao, China; X.J.-X. Xiang, China; Q.-S. Shen, China
13. Sep 18 10:30 11:00 5.10.2 PARTICLE IMAGE SURFACE FLOW VISUALIZATION AND SKIN-FRICTION MEASUREMENT
V. E. Mosharov¹, V. N. Radchenko¹, N. S. Tsipilev¹; ¹TsAGI, Russia
13. Sep 18 11:00 11:30 5.10.3 RELEASE OF DYNAMICALLY SCALED OBJECTS FROM A HELICOPTER WIND TUNNEL MODEL
K.H. Lammers, NLR, Netherlands; I. Philipsen, DNW, Netherlands; M.H. Ryu, KAI, South Korea
13. Sep 18 11:30 12:00 5.10.4 INVESTIGATION OF BDUNDARY LAYER TRANSITION MEASUREMENT IN SUBSONIC WIND TUNNEL USING TSP
J. Yu¹, L. Wei¹, X. Xiang¹, H. Wang¹, Z. Huang¹; ¹China Academy of Aerospace Aerodynamics, China
6.10Student Final
Chair(s): Rein Weston, K.
Track 6
15 - Guest lectures
7.10Aircraft Aerodynamic Design
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
13. Sep 18 10:00 10:30 7.10.1 CONCEPT OF MEDIUM TWIN-ENGINE STOL TRANSPORT AIRPLANE
O. Pavlenko¹, A. Petrov¹, E. Pigusov¹; ¹TsAGI, Russia
13. Sep 18 10:30 11:00 7.10.2 ANALYSIS AND DESIGN OF WING TRAILING EDGE MOUNTED OVER-THE-WING DISTRIBUTED PROPELLER PROPULSION
L. Veldhuis¹, A. Khajehzadeh¹, S. Hullshoff¹; ¹Delft University of Technology, Netherlands
13. Sep 18 11:00 11:30 7.10.3 A COMPARISON STUDY ON TRANSITION CHARACTERISTICS OF NLF FORWARD-SWEPT-WING AND AFT-SWEPT-WING
Z. Zhu¹, W.-P. Song¹, Z.-H. Han¹, J.-H. Xu¹; ¹Northwestern Polytechnical University, China
13. Sep 18 11:30 12:00 7.10.4 OUTBOARD SPLIT FLAP AERODYNAMICS OF A FLYING WING CONFIGURATION
S. Pfnür¹, C. Breitsamter¹; ¹Technical University of Munich, Germany
13. Sep 18 12:00 12:30 7.10.5 PRACTICAL APPLICATIONS OF VISCOUS FULL-POTENTIAL CFD CODES
D. Philpott¹, K. Hackett¹; ¹IHS Markit (ESDU), United Kingdom
8.10Aeroelasticity 6 : Controls
Chair(s): Breitsamter, C.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
13. Sep 18 10:00 10:30 8.10.1 DESIGN OF A RECEPTANCE-BASED ACTIVE AEROELASTIC CONTROLLER IN THE PRESENCE OF PARAMETRIC UNCERTAINTIES
S. Fichera¹, T.A.M. Guimaraes, Federal University of Uberlandia, Brazil; S. Jiffri, Swansea University, United Kingdom; D.A. Rade, Technological Institute of Aeronautics, Brazil; J.E. Mottershead¹; ¹University of Liverpool, United Kingdom
13. Sep 18 10:30 11:00 8.10.2 INCREASED FLUTTER VELOCITY WITH USE OF A PASSIVE CONTROL SYSTEM
F.I. Carvalho¹, R.G. SILVA¹; ¹ITA, Brazil
13. Sep 18 11:00 11:30 8.10.3 EXPERIMENTAL STUDY OF AEROELASTIC RESPONSE OF A FLEXIBLE HIGH ASPECT RATIO WING WITH PASSIVE SMA ACTUATORS
O.T. Silva Neto, Federal University of Uberlândia, Brazil; R.N.C. Duarte, Universidade Federal de Campina Grande, Brazil; R.G.A. Silva, Instituto Tecnológico de Aeronáutica, Brazil
13. Sep 18 11:30 12:00 8.10.4 EFFECTS OF NONLINEAR ENERGY SINK ON THE AEROELASTIC BEHAVIOR OF AN ELECTROMECHANICALLY COUPLED TYPICAL SECTION
G.M. Otsubo¹, T.M.P. Silva¹, D. D'Assunção¹, C. De Marqui Jr.¹; ¹EESC-USP, Brazil
13. Sep 18 12:00 12:30 8.10.5 REPLICA 55 PROJECT: AERODYNAMIC AND FEM ANALYSIS OF A WOODEN SEAPLANE
F. Favalli¹, M. Ferrara¹, C. Patuelli¹, A. Polla¹, S. Scarso¹, D. Tomasello¹; ¹Polytechnic of Turin, Italy
9.10Hybrid-Electric Propulsion
Chair(s): Isikveren, A.
Track 9
05 - Propulsion
13. Sep 18 10:00 10:30 9.10.1 DEVELOPMENT OF HYBRID GASOLINE-BATTERY PROPULSION SYSTEM FOR MULTI-COPTER PLATFORM
H.R. Gwon¹, W.B. Kim¹, K.W. Lee¹, D.W. Kim¹, H.S. Lee¹; ¹Korean Air, South Korea
13. Sep 18 10:30 11:00 9.10.2 PROPELLER OPTIMISATION FOR AN ELECTRICAL-POWERED TACTICAL UAS
R. MacNeill, The University of Sydney, Australia
13. Sep 18 11:00 11:30 9.10.3 DESIGN AND OFF-DESIGN PERFORMANCE OF ELECTRIC SYSTEM ARCHITECTURES FOR ELECTRIC POWERED AIRCRAFT
P.C. Vratny¹, F. Troeltsch¹, J. Bijewitz¹, J. Kaiser¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
13. Sep 18 11:30 12:00 9.10.4 SYSTEM ANALYSIS OF TURBO ELECTRIC AND HYBRID ELECTRIC PROPULSION SYSTEMS ON A REGIONAL AIRCRAFT
H. Gesell¹, F. Wolters¹, M. Plohr¹; ¹DLR, Germany
13. Sep 18 12:00 12:30 9.10.5 CHARACTERISTICS OF SYSTEMS WITH ELECTRICALLY DRIVEN UNITS - EXPERIMENTAL STUDIES IN A GAS TURBINE ENGINE DEMONSTRATOR
O.S. Gurevich¹, A.I. Gulienko¹, M.V. Gordin¹; ¹CIAM, Russia
10.10Flight Control 2
Chair(s): Che, J.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
13. Sep 18 10:00 10:30 10.10.1 EVALUATION OF ALTITUDE CONTROL FOR AN AIRBREATHING HYPERSONIC AIRCRAFT MODEL
Masaharu Hiruma, The University of Tokyo, Japan
13. Sep 18 10:30 11:00 10.10.2 A COMPARISON BETWEEN UNIVERSAL INTEGRAL REGULATOR AND LINEAR QUADRATIC TECHNIQUE FOR AN AIRCRAFT AUTOPILOT
Y.A. Díaz-Méndez¹, M.S. Sousa¹, S.S. Cunha Jr.¹, G.F. Gomes¹; ¹Federal University of Itajubá, Brazil
13. Sep 18 11:00 11:30 10.10.3 MULTI-VARIABLE AIRCRAFT DIRECTIONAL CONTROL WITH ANTI-SKID DIFFERENTIAL BRAKES
G. Di Rito¹, R. Galatolo¹, F. Schettini¹; ¹Università di Pisa - Dip. Ing. Civile ed Industriale, Italy
13. Sep 18 11:30 12:00 10.10.4 PASSIVE CONTROL METHOD IN ATTENUATING SELF-INDUCED ROLL OSCILLATIONS OF LOW-ASPECT-RATIO WINGS USING OBLIQUE SLOT BLEED
T. Hou¹, C. Chen¹, T. Hu¹; ¹Lu Shijia Labortory, Beihang University, China
13. Sep 18 12:00 12:30 10.10.5 MONTE-CARLO EVALUATION OF CONTROL LAW FOR HIGH ALTITUDE FLIGHT TEST OF MARS AIRPLANE
K. Fujita¹, H. Nagai¹, H. Tokutake, Kanazawa University, Japan; A. Oyama, Institute of Space and Astronautical Science, JAXA, Japan; ¹Institute of Fluid Science, Tohoku University, Japan
11.10UAS Control 2
Chair(s): Anemaat, W.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
13. Sep 18 10:00 10:30 11.10.1 MULTI-CHANNEL HUMAN-MACHINE INTERACTIVE SYSTEM FOR MULTIPLE UAVS\' CONTROL
P.-C. Wen¹, Y.-D. Zhang¹, Y.-H. Li¹; ¹AVIC Xi'an Aeronautics Computing Technique Research Institute, China
13. Sep 18 10:30 11:00 11.10.2 FLIGHT PERFORMANCE OF STEERABLE CRUCIFORM PARACHUTE SYSTEMS
S.M. Herrington¹, T.D. Fields¹, O.A. Yakimenko, Naval Postgraduate School, United States; ¹University of Missouri-Kansas City, United States
13. Sep 18 11:00 11:30 11.10.3 A STRATEGY FOR UAV PERFORMANCE ENHANCEMENT THROUGH ATMOSPHERIC ENERGY EXTRACTION USING MPC TECHNIQUES
G. Pogorzelski, CENIC Engenharia, Brazil; F.J. Silvestre, ITA - Instituto Tecnológico de Aeronáutica, Brazil
13. Sep 18 11:30 12:00 11.10.4 ON WAKE VORTEX SAFETY ANALYSIS AND CONTROL FOR UAV
V. Golubev¹, P. Kazarin¹, C. Moreno¹, W. MacKunis¹; ¹ERAU, United States
13. Sep 18 12:00 12:30 11.10.5 MODELING, CONTROL AND HARDWARE-IN-THE-LOOP SIMULATION OF A GENERIC TILTING MULTI-ROTOR
F. Machini¹, I.O. Tarifa¹, R.M.F. Neto¹, L. Sanches¹; ¹Universidade Federal de Uberlândia, Brazil
12.10Operations - ATM (air traffic mamagement)
Chair(s): Peters, M.
Track 12
10 - Safety and Security
13. Sep 18 10:00 10:30 12.10.1 FLIGHT TECHNICAL ERROR EVALUATIONS FOR GBAS NAVIGATION REQUIREMENT DEFINITION
M. Felux, DLR, Germany; J. Lee, KAIST, South Korea; F. Holzapfel, TUM, Germany
13. Sep 18 10:30 11:00 12.10.2 LOAD MONITORING FOR OPERATORS’ LOAD MANAGEMENT
U. Kale¹, I. Jankovics¹, J. Rohacs¹, D. Rohacs, Budapest University of Technology and Economics, Hungarian Air N, Hungary; ¹Budapest University of Technology and Economics, Hungary
13. Sep 18 11:00 11:30 12.10.3 THRUST MODELS BASED ON OPERATIONAL FLIGHT DATA USED IN PARAMETER ESTIMATION FOR SAFETY ANALYSES
P. Koppitz¹, J. Kuerten¹, F. Holzapfel¹; ¹Technical University of Munich - Flight System Dynamics, Germany
13. Sep 18 11:30 12:00 12.10.4 AIRCRAFT KEY PARTS INTELLIGENT FAULT DIAGNOSIS USING GAUSSIAN DEEP BELIEF NETWORK
H.D. Shao, School of Aeronautics, Northwestern Polytechnical University, China
13. Sep 18 12:00 12:30 12.10.5 ADAPTING CAPACITY OF AIR NAVIGATION SERVICE PROVISION IN EUROPE - BETWEEN SCYLLA AND CHARYBDIS
T. Standfuss, DLR German Aerospace Center, Germany; F. Fichert, University of Applied Sciences, Germany; M. Whittome, DFS, Germany

12:30 - 14:00Lunch

1.11Design History
Chair(s): Melkert, J.
Track 1
01 - Aircraft Design and Integrated Systems
13. Sep 18 14:00 14:30 1.11.1 REPLICA 55 PROJECT: A WOOD SEAPLANE IN THE ERA OF COMPOSITE MATERIALS
E. Cestino¹, G. Frulla¹, V. Sapienza, Aeronautical Consultant, Italy; P. Pinto, 3Data analysis consultant, Italy; F. Rizzi, Replica 55 Project coordinator, Italy; F. Zaramella , BETA CAE Italy, Italy; D. Banfi , CAD Consultant, Italy; ¹Politecnico di Torino, Italy
13. Sep 18 14:30 15:00 1.11.2 THE NUMERICAL HISTORY OF AIRPLANE MANUFACTURING IN XX CENTURY
Y.V. Kuzmin, TsAGI, Russia
13. Sep 18 15:00 15:30 1.11.3 THE HAWKER SIDDELEY AVIATION HS141. VERTICAL TAKE –OFF AND LANDING RESEARCH PROGRAMME IN THE LATE 1960 EARLY 1970S.
F. Ogilvie, United Kingdom
2.11Structural Health Monitoring 2
Chair(s): Anchieta da Silva, P., Scott, M.
Track 2
11 - Operations and Sustainment
13. Sep 18 14:00 14:30 2.11.1 ADDRESSING TECHNICAL AND REGULATORY REQUIREMENTS TO DEPLOY STRUCTURAL HEALTH MONITORING SYSTEMS ON COMMERCIAL AIRCRAFT
D. Roach¹, T. Rice¹; ¹Sandia National Laboratories, United States
13. Sep 18 14:30 15:00 2.11.2 SHM QUALIFICATION PROCESS AND THE FUTURE OF AIRCRAFT MAINTENANCE
F. Dotta¹, R.P. Rulli¹, P.A. da Silva¹, L.C. Vieira¹, A.K.F. Tamba¹, G.O.C. Prado¹, D. Roach², T. Rice²; ¹Embraer S.A., Brazil ;²Sandia National Labs, United States
13. Sep 18 15:00 15:30 2.11.3 SHM WITH AUGMENTED REALITY FOR AIRCRAFT MAINTENANCE
G.O.C. Prado¹, P.A. Silva¹, F.M. Simomura¹, K.L.O. Pereira¹; ¹Embraer S.A., Brazil
Reserve Paper 2.11.R CORROSION DETECTION IN AERONAUTICAL STRUCTURES USING LAMB WAVES SYSTEM FOR SHM
A.K.F. Tamba¹, L.C. Vieira¹, G.O.C Prado¹, F. Dotta¹, R.P. Rulli¹, P.A. da Silva¹, R.R. Cunha¹, J.P. da Costa¹; ¹Embraer S.A., Brazil
3.11Physics Based Damage Modeling
Chair(s): Blom, A.
Track 3
04.1 - Material Issues, Fatigue and Damage Tolerance
13. Sep 18 14:00 14:30 3.11.1 MODELLING OF MIXED MODE FATIGUE-INDUCED DELAMINATION IN COMPOSITES: A COMPARATIVE STUDY
L.A. de Oliveira¹, D.S. Alves¹, M.V. Donadon¹; ¹Instituto Tecnológico de Aeronáutica, Brazil
13. Sep 18 14:30 15:00 3.11.2 COMPARISON OF TWO DIFFERENT INDICATORS FOR HOT CRACKING IN WELDED STRUCTURES
J. Edberg¹, J. Draxler¹, J. Andersson, University West, Sweden; ¹Luleå University of Technology, Sweden
13. Sep 18 15:00 15:30 3.11.3 IMPORTANCE OF SECONDARY BENDING EVALUATION IN STRUCTURAL JOINT
W.R.P. Mendonça, EMBRAER S.A., Brazil
Reserve Paper 3.11.R ON ELASTIC PSEUDO-ISOTROPIC ORTHOTROPIC PLATES
L.M.B.C. Campos, Instituto Superior Tecnico, Portugal
4.11Hypersonic Flow
Chair(s): Alves, L.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
13. Sep 18 14:00 14:30 4.11.1 RESEARCH ON EXTERNAL AERODYNAMICS OF THE HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECT
A.A. Gubanov¹, N.V. Voevodenko¹, V.A. Talyzin¹, D.S. Ivanyushkin¹, A.O. Podosinnikov¹, V.A. Yakovleva¹; ¹TsAGI, Russia
13. Sep 18 14:30 15:00 4.11.2 LONGITUDINAL STABILITY DESIGN CRITERIA FOR HYPERSONIC GLIDERS
B.Y. Chen, China Academy of Aerospace Aerodynamics, China
13. Sep 18 15:00 15:30 4.11.3 CFD PACKAGE \"FLOW VISION\" FOR SIMULATIONS AND IMITATION MODELING OF HYPERSONIC VEHICLES
E.E. Son¹, V.G. Degtyar², A.A Aksenov¹, S.V. Zhluktov¹, V.I. Hlybov², S.T. Kalashnikov, Federal State Budgetary Scientific Institute, Russia; K.E. Son¹; ¹Moscow Institute of Physics and Technology, Russia ;²Academician V.P. Makeyev Space Rocket Centre, Russia
5.11Modeling and Simulation in Manufacturing
Chair(s): Zhang, H.
Track 5
08 - Manufacturing and Supply Chain Management
13. Sep 18 14:00 14:30 5.11.1 ENABLING THE DIGITAL FACTORY THROUGH THE INTEGRATION OF DATA-DRIVEN AND SIMULATION MODELS
O.L. Pinon¹, D.J.L. Siedlak¹, D. Mavris¹; ¹Georgia Institute of Technology, United States
13. Sep 18 14:30 15:00 5.11.2 ON-DEMAND SMALL UAS ARCHITECTURE SELECTION AND RAPID MANUFACTURING USING A MODEL-BASED SYSTEMS ENGINEERING APPROACH
C. Justin¹, A. Ramamurthy¹, N. Beals², E. Spero², D. Mavris¹; ¹GEORGIA INSTITUTE OF TECHNOLOGY, United States ;²U.S. ARMY RESEARCH LABORATORY, United States
13. Sep 18 15:00 15:30 5.11.3 IDENTIFICATION METHOD OF THE SIMULATION MODEL “VIRTUAL ENGINE” BUILT INTO THE DIGITAL ENGINE CONTROL SYSTEM
F.D. Golberg¹, O.S. Gurevich¹, A.A. Petukhov¹; ¹CIAM, Russia
6.11High Speed Transition
Chair(s): Atkin, C.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
13. Sep 18 14:00 14:30 6.11.1 ENTROPY LAYER EFFECT ON ROUGHNESS-INDUCED LAMINAR-TURBULENT TRANSITION IN SUPERSONIC FLAT PLATE FLOW
P.V. Chuvakhov, Central Aerohydrodynamic Institute (TsAGI), Russia
13. Sep 18 14:30 15:00 6.11.2 THEORETICAL STUDY OF RECEPTIVITY OF HIGH-SPEED BOUNDARY LAYER TO SURFACE PERTURBATIONS
Y. Xi¹, S. Fu¹; ¹Tsinghua University, China
13. Sep 18 15:00 15:30 6.11.3 DIRECT NUMERICAL SIMULATION OF MACH WAVE INFLUENCE ON LAMINAR-TURBULENT TRANSITION IN SUPERSONIC FLOW OVER A FLAT PLATE
I.V. Egorov¹, A.V. Fedorov¹, K.H. Ding, Central Aerohydrodynamic Institute, Russia; ¹TsAGI, Russia
7.11New Structural Design 3: Material and Micro Structures
Chair(s): Zanardi, H.
Track 7
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
13. Sep 18 14:00 14:30 7.11.1 METHOD FOR FLEXIBLE SKELETON COMPOSED OF THE TYPE OF INCIRCLE ELEMENT BASED ON EQUAL DISPLACEMENT AND ITS APPLICATION
Y.-C. Deng, SADRI, China
13. Sep 18 14:30 15:00 7.11.2 DEVELOPMENT OF STRUCTURE ELEMENTS BASED ON ARCHITECTURED MATERIALS FOR PERSPECTIVE CIVIL AIRCRAFTS
I. Kondakov¹, I. Mareskin¹, D. Vedernikov¹, Y. Mirgorodsky¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
8.11Structural Optimization
Chair(s): Fredriksson, B.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
13. Sep 18 14:00 14:30 8.11.1 PROBABILISTIC METHOD OF DETERMINATION OF ALLOWABLE DESIGN PARAMETER SCATTERS ON FLUTTER AND STRENGTH CRITERIA
V.V. Chedrik, Central Aerohydrodynamic Institute, Russia
13. Sep 18 14:30 15:00 8.11.2 STRESS-BASED TOPOLOGY OPTIMIZATION WITH USING GLOBAL-LOCAL APPROACH
V.V. Chedrik¹, S.A. Tuktarov¹; ¹Central Aerohydrodynamic Institute, Russia
13. Sep 18 15:00 15:30 8.11.3 OPTIMIZATION OF SCARF JOINT ANGEL AND OVERPLY DOUBLER USING GENETIC ALGORITHM CONSIDERING ADHESIVE MATERIAL NONLINEARITY
A. Abedian, Aerospace Eng Dept, Sharif Uni of Tech, Iran
9.11ISABE
Chair(s): ,
Track 9
10.11Control for Flexible Aircraft
Chair(s): Ueno, S.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
13. Sep 18 14:00 14:30 10.11.1 IMPLEMENTATION AND FLIGHT TESTING OF AN ENHANCED STABILITY SYSTEM FOR A VERY FLEXIBLE AIRCRAFT
P.J. Gonzalez¹, C.E.S. Cesnik ¹, F.J. Silvestre, Instituto Tecnologico de Aeronautica, Brazil; ¹University of Michigan, United States
13. Sep 18 14:30 15:00 10.11.2 ADAPTIVE OUTPUT-FEEDBACK GAIN SCHEDULING APPLIED TO FLEXIBLE AIRCRAFT
R.M. Bertolin¹, A.B. Guimarães Neto¹, G.C. Barbosa¹, F.J. Silvestre¹; ¹Instituto Tecnológico de Aeronáutica, Brazil
13. Sep 18 15:00 15:30 10.11.3 CONTROL OF A VERY FLEXIBLE WING WITH SIMULTANEOUS OPTIMIZATION OF THE GAIN MATRIX AND THE SPATIAL DISTRIBUTION OF THE SE
M. A. V. Morales, Brazil
11.11UAS Navigation
Chair(s): Greco Jr., P.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
13. Sep 18 14:00 14:30 11.11.1 MODIFIED COMPOSITE GUIDANCE LAW AGAINST MOVING TARGET CONSIDERING NARROW FIELD-OF-VIEW LIMIT
S. Lee¹, S. Ann¹, Y. Kim¹; ¹Seoul National University, South Korea
13. Sep 18 14:30 15:00 11.11.2 AUTONOMOUS FLIGHT OF UNMANNED MULTICOPTER USING SUPER WIDE-ANGLE STEREO VISION SYSTEM
T. Yamashita¹, Y. Kajiwara¹, C.T. Raabe², T. Tsuchiya², S. Suzuki²; ¹Ricoh Co. Ltd, Japan ;²the University of Tokyo, Japan
13. Sep 18 15:00 15:30 11.11.3 SIMULTANEOUS LOCALIZATION AND MAPPING WITH OBJECT DETECTION FOR UAV APPLICATONS
T. Shim, KAIST, South Korea
12.11Air Turbulence
Chair(s): Heinzinger, O.
Track 12
10 - Safety and Security
13. Sep 18 14:00 14:30 12.11.1 DEVELOPMENT AND FLIGHT DEMONSTRATION OF A NEW LIDAR-BASED ONBOARD TURBULENCE INFORMATION SYSTEM
N. Matayoshi¹, T. Iijima¹, E. Yoshikawa¹, J.O. Entzinger², T. Uemura², T. Akiyama¹, H. Inokuchi¹; ¹JAXA, Japan ;²Univ. of Tokyo, Japan
13. Sep 18 14:30 15:00 12.11.2 HAZARDOUS MITIGATION FOR TRANSPORT AIRCRAFT IN SEVERE ATMOSPHERIC TURBULENCE BASED ON IMPROVED CONTROL STRATEGY
C. Chang, College of General Aviation, Wenzhou University, China
13. Sep 18 15:00 15:30 12.11.3 FLIGHT DEMONSTRATION OF A LONG RANGE ONBOARD DOPPLER LIDAR
H. Inokuchi¹, T. Akiyama¹, K. Sasaki¹; ¹Japan Aerospace Exploration Agency, Japan

15:30 - 16:00Break

0.10von Karman Lecture - International Committee on Aeronautical Fatigue and Structural Integrity (ICAF) – Achievements, Activities, and Future Challenges, Anders Blom, David Simpson, Carlos Chaves, Marcel Bos
Chair: Shinji Suzuki Chair ICAS Programme Committee
13. Sep 18 16:00 17:00

17:00 - 17:30Closing Ceremony