30th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

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Monday, 10. Sep 2018


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

08:00 - 09:00Opening Ceremony

0.1ICAS Daniel & Florence Guggenheim Memorial Lecture - Humberto Perreira, 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 COLLABORATIVE , MULTI-NATIONAL MDO OF CIVIL AIRCRAFT : AGILE EU PROJECT
P S Shiva Prakasha, German Aerospace Center, Germany
10. Sep 18 11:00 11:30 1.1.2 MULTIDISCIPLINARY DESIGN OPTIMIZATION OF BLENDED WING BODY AIRCRAFT THROUGH COLLABORATIVE DESIGN - AGILE EU PROJECT
P S Shivaprakasha, German Aerospace Center, Germany
10. Sep 18 11:30 12:00 1.1.3 AERO_STRUCTURAL OPTIMIZATION OF A MALE CONFIGURATION IN THE AGILE MDO FRAMEWORK
R. 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 DESIGN 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
Philipp Stahl¹, Thomas Seren¹, Christian Rößler¹, Mirko 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
YAO Z.X., 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 SYSTEM
D. Mavris, United States
4.1Unsteady Aerodynamics 1
Chair(s): Catalano, P., Lima, L.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
10. Sep 18 10:30 11:00 4.1.1 INVISCID AND VISCOUS FLOW MODELING FOR FAST TRANSONIC FLUTTER CALCULATIONS
H. Güner¹, G. Dimitriadis¹, V. Terrapon¹; ¹University of Liège, Belgium
10. Sep 18 11:00 11:30 4.1.2 FEASIBILITY OF NAVIER-STOKES HARMONIC BALANCE METHOD FOR MODELLING 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 COMPUTATIONAL AND EXPERIMENTAL UNSTEADY PRESSURE DISTRIBUTIONS OF WING OSCILLATING IN PITCH
G.R. Begnini, Embraer S.A., Brazil
Reserve Paper 4.1.R LATTICE-BOLTZMANN SIMULATIONS OF THE OSCILLATING BENCHMARK SUPERCRITICAL WING
F. P. Ribeiro, Exa GmbH, Germany
5.1Experiments in Flow Control
Chair(s): Manfriani, L.
Track 5
03.2 - Experimental Aerodynamics
10. Sep 18 10:30 11:00 5.1.1 EXPERIMENTAL STUDY OF SYNTHETIC JET ACTUATOR FLOW CONTROL ON A NACA0015
N.D. Martin, Northumbria University, United Kingdom
10. Sep 18 11:00 11:30 5.1.2 EXPERIMENTAL INVESTIGATION OF WING LOAD CONTROL USING FLUIDIC DEVICES
Andrzej Krzysiak, Institute of Aviation, Poland
10. Sep 18 11:30 12:00 5.1.3 EXPERIMENTAL STUDY OF TRANSONIC FLOW OVER AN AIRFOIL ON LAMINAR FLOW AND LEADING EDGE TUBERCLES
R.G. Annes da Silva, ITA, Brazil
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
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 CONTINUOUS TANGENTIAL JET
Y. LEE, Agency for Defense Development, South Korea
8.1Acustics and Vibrations 1
Chair(s): Sanches, L.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
10. Sep 18 10:30 11:00 8.1.1 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
Reserve Paper 8.1.R HIGH PERFORMANCE PNEUMATIC SHOCK-ABSORBERS FOR AERONAUTICAL APPLICATIONS
Rami Faraj, Institute of Fundamental Technological Research, Poland
9.1Hybrid-Electric Propulsion
Chair(s): Isikveren, A.
Track 9
05 - Propulsion
10. Sep 18 10:30 11:00 9.1.1 DEVELOPMENT OF HYBRID GASOLINE-BATTERY PROPULSION SYSTEM FOR MULTI-COPTER PLATFORM
Hyuk Rok Gwon¹, Woo Bee Kim¹, Ki Woong Lee¹, Dae Won KIm¹, Hyeon Seok Lee¹; ¹Korean Air, South Korea
10. Sep 18 11:00 11:30 9.1.2 PROPELLER OPTIMISATION FOR AN ELECTRICAL-POWERED TACTICAL UAV
Rens MacNeill, The University of Sydney, Australia
10. Sep 18 11:30 12:00 9.1.3 DESIGN AND OFF-DESIGN PERFORMANCE OF ELECTRIC SYSTEM ARCHITECTURES FOR ELECTRIC POWERED AIRCRAFT
P.C. Vratny¹, F. Troeltsch¹, J. Bijewitz¹, J. Kaiser¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
Reserve Paper 9.1.R SYSTEM ANALYSIS OF TURBO ELECTRIC AND HYBRID PROPULSION SYSTEMS ON A REGIONAL AIRCRAFT
H. Gesell¹, F. Wolters¹, M. Plohr¹; ¹DLR, Germany
10.1FT & RC
Chair(s): Wang, Q.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
10. Sep 18 10:30 11:00 10.1.1 NEURAL NETWORK-BASED FAULT TOLERANT CONTROL FOR AIRCRAFT
N Yoshikawa, The 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
11.1UAS Navigation
Chair(s): Greco Jr., P.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
10. Sep 18 10:30 11:00 11.1.1 MODIFIED COMPOSITE GUIDANCE LAW AGAINST MOVING TARGET CONSIDERING NARROW FIELD-OF-VIEW LIMIT
Seokwon Lee¹, Sungjun Ann¹, Youdan Kim¹; ¹Seoul National University, South Korea
10. Sep 18 11:00 11:30 11.1.2 AUTONOMOUS FLIGHT OF UNMANNED MULTICOPTER USING SUPER WIDE-ANGLE STEREO VISION SYSTEM
T. Yamashita¹, Y. Kajiwara¹, C.T. Raabe², T. Tsuchiya², S. Suzuki²; ¹Ricoh Co. Ltd, Japan ;²the University of Tokyo, Japan
10. Sep 18 11:30 12:00 11.1.3 SIMULTANEOUS LOCALIZATION AND MAPPING WITH OBJECT DETECTION FOR UAV APPLICATONS
T. Shim, KAIST, South Korea
Reserve Paper 11.1.R ON BOARD SLAM FOR INDOOR MAV USING A LASER RANGE FINDER
K.-S. Sibilski, Air Force Institute of Technology, Poland
12.1Safety 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
Kun Chen¹, Yibing Wu¹, Tianchun 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, P.D. Ciampa¹; ¹German Aerospace Center, DLR, Germany
10. Sep 18 13:30 14:00 1.2.2 MDO APPLICATIONS TO CONVENTIONAL AND NOVEL TURBOPROP AIRCRAFTS WITHIN AGILE EUROPEAN PROJECT
P. Della Vecchia, University of Naples Federico II, Italy
10. Sep 18 14:00 14:30 1.2.3 INCLUDING AEROELASTIC TAILORING IN THE CONCEPTUAL DESIGN PROCESS OF A COMPOSITE STRUT BASED WING
D Rajpal, Delft University of Technology, Netherlands
2.2UAS 2
Chair(s): Ogilvie, F.
Track 2
01 - Aircraft Design and Integrated Systems
10. Sep 18 13:00 13:30 2.2.1 A VTOL SMALL UNMANNED AIRCRAFT SYSTEM TO EXPAND PAYLOAD CAPABILITIES
S. 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 UAVS FOR HUMANITARIAN RELIEF MISSIONS
O Hektor¹, Dr. 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
L. D. Jesus¹, M.S. Sousa¹, E.H. Shiguemori, IEAv, Brazil; S. Serokhvostov, MIPT, Russia; P.K. Gupta, JUIT, India; L. Zhong, CAUC, China; A. C. B. Ramos, Unifei, Brazil; ¹UNIFEI, Brazil
Reserve Paper 2.2.R DESIGN AND OPTIMIZATION OF A VERSATILE UAV FOR OBSERVATION AND RESEARCH USING THERMAL COLUMNS FOR EXTENDED ENDURANCE
P.A. Pacuszka, Poland; U. Golyska, Poland; M.K. Nowowiejski, Poland
Reserve Paper 2.2.R UAV INITIAL PARAMETER ESTIMATION
Lucas Campos Carmona¹, Eduardo Bauzer Medeiros¹, Gabriel George Silva¹; 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 Heerden, United Kingdom
10. Sep 18 13:30 14:00 3.2.2 A TECHNIQUE FOR CAPTURING STAKEHOLDER PREFERENCES AND KNOWLEDGE IN EARLY DESIGN STUDIES
S. Sartorius, United States; M. Hornung, Technical University of Munich Institute of Aircraft Design, Germany
10. Sep 18 14:00 14:30 3.2.3 METHODOLOGY FOR THE DEVELOPMENT OF FUTURE AIRLINER PASSENGER CABINS FOR THE ASIAN MARKET
R. Kirenskis, Cranfield University, United Kingdom
4.2Unsteady Aerodynamics 2
Chair(s): Da Ronch, A, Azevedo, J.H.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
10. Sep 18 13:00 13:30 4.2.1 NUMERICAL DEVELOPMENT OF UNSTEADY VORTEX-LATTICE METHOD EXPANSION FOR LEADING-EDGE SHEDDING PREDICTION WITH EXPERIMENTAL VALIDATION
T. P. Monteiro¹, F. Silvestre¹, K. Ramesh, Glasgow University, United Kingdom; 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
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
Alexis Cenko, AIWS, United States; Graham 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 RIGID COAXIAL ROTOR WING IN HOVER
X. Zhao¹, N.-Z. Huang¹, X. Liang¹, P. Zhou¹, 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
V.V. Gubskiy¹, A.V. Petrov¹, A.V. Potapchik¹, Yu.G. Stepanov¹; ¹TsAGI, Russia
10. Sep 18 14:00 14:30 5.2.3 INSTALLATION EFFECTS ON THE AERODYNAMICS AND AEROACOUSTICS OF A PYLON AND A PUSHER PROPELLER
L. Rego, University of São Paulo, Brazil
Reserve Paper 5.2.R EXPERIMENTAL RESEARCH AND NUMERICAL ANALYSIS OF COLD AND HOT-JET SIMULATION OF TRUST VECTOR CONTROL BY JET TABS
G. Ocokoljic, Military Technical Institute, Belgrade, Serbia
6.2Fundamental Fluid Dynamics 2
Chair(s): Cavalieri, A.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
10. Sep 18 13:00 13:30 6.2.1 ACOUSTIC MODES IN JETS AND WAKES AND THEIR ROLE IN ABSOLUTE INSTABILITY
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 IN
V.I. Shalaev, MIPT, Russia; S.V. Alexandrov¹, A.V. Vaganov¹, S.M. 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 Junior, University of Liverpool, United Kingdom; L. Santos de Brito Alves, Universidade Federal Fluminense, Brazil
7.2Unmanned Aircraft
Chair(s): Yutko, B.
Track 7
03.4 - Applied Aerodynamics
10. Sep 18 13:00 13:30 7.2.1 STUDY ON SMALL UAVS\' DEEP STALL LANDING PROCEDURE
Bochao Cheng¹, Zheng Guo¹, Peng Wang¹, Qingyang Chen¹, Bochao Cheng, No.32021 Troops of PLA, China; 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
Li-li Chen¹, Zheng Guo¹, Zhong-xi Hou¹, Wen-kai Wang¹, Bing-jie Zhu¹; ¹National University of Defense Technology, China
10. Sep 18 14:00 14:30 7.2.3 AEROELASTIC ANALYSIS OF INSECT-LIKE FLAPPING WING USING MODIFIED IMPLICIT COUPLING METHOD
N. Lee, Inha University, South Korea
Reserve Paper 7.2.R 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 THE DIMENSIONING OF A NONLINEAR ENERGY SINK APPLIED TO A HELICOPTER THROUGH NONLINEAR NORMAL MODES
L. V. D. Sousa, Federal University of Uberlândia, Brazil
10. Sep 18 13:30 14:00 8.2.2 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 14:00 14:30 8.2.3 INVESTIGATION ON HIGH-FREQUENCY MODAL TEST AND ANALYSIS FOR TURING BLADE
G-X Gao Xiang¹, Y-Q YAN QUN¹, H-WC HUANG Wenchao¹, YG YAO Gang¹; ¹ASRI, China
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.K. Kowalski¹, A.J. Jankowski¹, R.S. 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 INFLUENCE OF BIODYNAMIC FEEDTHROUGH ON HANDLING QUALITIES ANALYSIS
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
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 IN-SERVICE AIRCRAFT CYBERSECURITY RISK ASSESSMENT
G.C.B. Bertoli, Brazil
10. Sep 18 13:30 14:00 12.2.2 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
10. Sep 18 14:00 14:30 12.2.3 A METHOD TO DESIGN CYBER-PHYSICAL RESILIENT ARCHITECTURES
ET YANO, ITA, Brazil

14:30 - 15:00Break

1.3Novel Application of MDO in Aircraft Design 3
Chair(s): Lefebvre, T.
Track 1
01 - Aircraft Design and Integrated Systems
10. Sep 18 15:00 15:30 1.3.1 INTERGRATED SYSTEM FOR UNIFICATION OF AIRCRAFT CONCEPTUAL DESIGN APPLICATIONS.
E. Vogiatzis¹, R. -C. Munjulury¹, P. Krus¹; ¹Linköpings university, Sweden
10. Sep 18 15:30 16:00 1.3.2 STRUCTURAL DESIGN AND TESTING OF A TAILORED SKIN SINGLE DUCT (TSSD) FIN APPLICATION
M. Schneider¹, M. Horn¹, S. Ritt¹, A. Seitz¹; ¹DLR, Germany
10. Sep 18 16:00 16:30 1.3.3 AIRCRAFT OPTIMIZATION AT THE EARLY STAGES OF DESIGN WITH A HYBRID TECHNIQUE
N Cavus, German Aerospace Center, Germany
Reserve Paper 1.3.R STUDIES ON THE APPLICATION OF MOEA/D TO AERODYNAMIC OPTIMIZATION DESIGN
X.Q. Zhu¹, Z.H Gao¹, Z.W. Chen¹; ¹Northwestern Polytechnical University, China
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
D. Ulma¹, R. Zurawski¹; 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 STRCTURE TECHNOLONY OF ADDITIVE MANUFACTURING
Xiangming Wang¹, Hao Cui¹, Ping Xu¹, Shiquan 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
N. Broitman¹, A. Shirizly¹; ¹Technion, I.I.T., Israel
10. Sep 18 16:00 16:30 3.3.3 EVALUATION OF MECHANICAL PROPERTIES OF TI6AL4V FABRICATED BY SELECTIVE LASER MELTING (SLM)
MingQiang Chu¹, XiaoWei Zhou¹, XiaoFeng Sun¹, Lei 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 JETS IN CROSSFLOW
K. C. Morais¹, D. F. Abreu¹, L. Tobaldini Neto¹, R. Papa¹, 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 VALIDATION OF A DISCONTINUOUS GALERKIN BASED DES SOLVER IN FLOW PROBLEMS USING HIGH PERFORMANCE COMPUTING
A.V. Wolkov, TsAGI, Russia
Reserve Paper 4.3.R GENERATION OF STEADY-STATE FLOWS WITH MINIMAL GAIN MARCHING SCHEMES
R.D.S. Dias dos Santos, 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
Takeshi 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 John Steven Monk, CSIR, South Africa
10. Sep 18 16:00 16:30 5.3.3 SAE BRASIL STUDENT PROGRAMS - A SUCCESS STORY
Horacio 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
7.3Aeroacoustics and Icing
Chair(s): Collier, F.
Track 7
03.4 - Applied Aerodynamics
10. Sep 18 15:00 15:30 7.3.1 INVESTIGATION OF THE AEROACOUSTIC INFLUENCE OF A SEAL ATTACHED ON SLAT COVE USING LST AND POD TECHNIQUE
M. A. F. de Medeiros, Aeronautical Engineering Department - University of Sao Paulo, Brazil
10. Sep 18 15:30 16:00 7.3.2 AN INTEGRATED CFD-SEA METHODOLOGY TO ACCOUNT FOR AERODYNAMIC SOURCES INTO CABIN NOISE PREDICTIONS
B Guaraldo Neto, Embraer SA, Brazil
10. Sep 18 16:00 16:30 7.3.3 THE STUDIES ON LOW-NOISE LAMINAR WING REGIONAL AIRCRAFT
N.A. Pushchin, TsAGI, Russia
8.3Aeroelasticity 3 : 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
Qijing YU¹, Saeil 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. Amiryants, TsAGI, 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
D. Simon¹, S. Ward¹, L.P.G. Pinto², B. Lantto¹, V.J. 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 FAILURE OF A SERVO VALVE
T. Seung, Program Management Office Aeronautics Research / DLR del. iABG, Germany
10. Sep 18 16:00 16:30 10.3.3 NUMERICAL AND EXPERIMENTAL STUDY OF A TWO DEGREES OF FREEDOM ELECTROHYDRAULIC MANIPULATOR
W. Cardozo, PUC-Rio, Brazil
11.3UAS VTOL
Chair(s): Bil, C., Alvarez, O.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
10. Sep 18 15:00 15:30 11.3.1 FLIGHT DYNAMICS MODELING AND TRIM CURVES OF A CONCEPTUAL SEMI-TANDEM WING VTOL UAV
A.C. Daud 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 TILTWING 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 EVALUATION ON HOME DELIVERY SERVICE USING MULTIPLE DRONES
Hiroki Omagari, Department of Aeronautics and Astronautics, Kyushu University, Japan
Reserve Paper 11.3.R MODELLING AND CONTROL OF A BI-TILT-ROTOR UAV WITH DOUBLE GIMBAL AND CAMERA FOR SURVEILLANCE SYSTEMS APPLICATION
J.C. 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 INVESTIGATION OF EMERGING HUMAN-MACHINE INTERFACE CONCEPTS FOR UAS OPERATIONS
Yixiang: Y. Lim¹, Kavindu: K. Ranasinghe¹, Alessandro: A Gardi¹, Neta: N Ezer, Northrop Grumman Corporation, United States; Roberto: 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