30th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

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Tuesday, 11. Sep 2018


7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
0.1General Lecture II - Autonomy and the future of Aerospace - N. Pendleton, Boeing, USA
Chair: Gunnar Holmberg, ICAS Treasurer
11. Sep 18 08:00 09:00

0.2Interactive Presentations
Chair: Artur Mirzoyan
11. Sep 18 09:00 10:00

1.1Unconventional Concepts 1
Chair(s): Kimmel, B.
Track 1
01 - Aircraft Design and Integrated Systems
11. Sep 18 10:00 10:30 1.1.1 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 1.1.2 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 1.1.3 EXPLORATION OF THE AIRBUS \"NAUTILIUS\" ENGINE INTEGRATION CONCEPT
L. Wiart, ONERA, France; C. Negulescu, AIRBUS, France
11. Sep 18 11:30 12:00 1.1.4 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
2.1Next Generation Commercial Transport Concept
Chair(s): Collier, F.
Track 2
01 - Aircraft Design and Integrated Systems
11. Sep 18 10:00 10:30 2.1.1 BLENDED WING BODY TRANSPORT AIRCRAFT RESEARCH & DEVELOPMENT
J.T. Bonet, Boeing Research & Technology, United States
11. Sep 18 10:30 11:00 2.1.2 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 2.1.3 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
11. Sep 18 11:30 12:00 2.1.4 DESIGN AND DEVELOPMENT OF THE D8 COMMERCIAL TRANSPORT CONCEPT
B. Yutko¹, N. Titchener¹, C. Courtin¹, W. Lieu¹, L. Wirsing¹, D. Hall¹, J. Tylko¹, J. Chambers¹, T. Roberts¹, C. Church¹; ¹Aurora Flight Sciences, United States
3.1Systems Architecting
Chair(s): Marengo, L.
Track 3
02 - Systems Engineering and Integration
11. Sep 18 10:00 10:30 3.1.1 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 3.1.2 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 3.1.3 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 3.1.4 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
4.1Aerodynamic Design
Chair(s): Prince, S., Grossi, F.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
11. Sep 18 10:00 10:30 4.1.1 \"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 4.1.2 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 4.1.3 HIGHER FIDELITY TRANSONIC AERODYNAMIC MODELING IN PRELIMINARY AIRCRAFT DESIGN
A. Crovato¹, G. Dimitriadis¹, V.E. Terrapon¹; ¹University of Liege, Belgium
5.1Unsteady Flows and Aeroacoustics
Chair(s): Chen, Y.
Track 5
03.2 - Experimental Aerodynamics
11. Sep 18 10:00 10:30 5.1.1 UNSTEADY AERODYNAMIC CHARACTERISTICS OF THE OSCILLATING AIRFOIL USING MSBS
Y.H. Sung¹, J.S. Han¹, J.H. Han¹; ¹KAIST, South Korea
11. Sep 18 10:30 11:00 5.1.2 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
11. Sep 18 11:00 11:30 5.1.3 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
11. Sep 18 11:30 12:00 5.1.4 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
6.1Composites
Chair(s): Scott, M., Shanygin, A.
Track 6
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
11. Sep 18 10:00 10:30 6.1.1 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 6.1.2 DESIGNING PRIMARY STRUCTURES WITH STITCHED COMPOSITES
A. Velicki, The Boeing Company, United States
11. Sep 18 11:00 11:30 6.1.3 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 6.1.4 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
7.1Store Separation
Chair(s): Cenko, A.
Track 7
03.4 - Applied Aerodynamics
11. Sep 18 10:00 10:30 7.1.1 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 7.1.2 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 7.1.3 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 7.1.4 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
8.1Aeroelasticity 2 : Methods and Modeling
Chair(s): Mello, O.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
11. Sep 18 10:00 10:30 8.1.1 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 8.1.2 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 8.1.3 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 8.1.4 CANCELED - AERODYNAMICS OPTIMIZATION DESIGN METHOD AND SHAPE PARAMETERIZATION
Z.Y Wang, The First Aircraft Institute, AVIC, China
9.1Engine Performance
Chair(s): Remy, S.
Track 9
05 - Propulsion
11. Sep 18 10:00 10:30 9.1.1 CANCELED - 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 9.1.2 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 9.1.3 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
10.1Flight Testing
Chair(s): Naruoka, M.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
11. Sep 18 10:00 10:30 10.1.1 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 10.1.2 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 10.1.3 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 10.1.4 KNOWLEDGE ENGINEERING BASED FLIGHT TEST TECHNOLOGY FOR CIVIL AIRCRAFT AIRWORTHINESS CONFORMITY
L. ZHAOHUI¹, L. GANG¹; ¹Chinese Flight Test Establishment, China
11.1Flight Test and Equipment
Chair(s): Geister, R.
Track 11
07 - Systems, Subsystems and Equipment
11. Sep 18 10:00 10:30 11.1.1 CANCELED - 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 11.1.2 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 11.1.3 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 11.1.4 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
12.1Aircraft Operation 1
Chair(s): Tokuakid, N., Lamiscarre, B.
Track 12
09 - Air Transport System Efficiency
11. Sep 18 10:00 10:30 12.1.1 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 12.1.2 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 12.1.3 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 12.1.4 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

0.3ICAS Casimiro Montenegro Filho Lecture for Innovation in Aeronautics - AGILE Project Consortium
Chair: Michel Peters, ICAS EC Member
11. Sep 18 13:00 13:45

1.2Alternative Energy and Distributed Propulsion Aircraft
Chair(s): Goraj, Z.
Track 1
01 - Aircraft Design and Integrated Systems
11. Sep 18 14:00 14:30 1.2.1 DEVELOPING THE UNMANNED UNCONVENTIONAL CARGO AIRPLANES WITH HYBRID PROPULSION SYSTEM
I. Gál¹, D. Rohács¹, J. Rohács¹; ¹Budapest University of Technology and Economics, Hungary
11. Sep 18 14:30 15:00 1.2.2 OPTIMIZATION OF MOTOR FOR THE MAXIMIZATION OF SOLAR-POWERED AIRCRAFT PERFORMANCE
S. Serokhvostov, MIPT, Russia; T. Churkina, MAI, Russia
11. Sep 18 15:00 15:30 1.2.3 NUMERICAL AND EXPERIMENTAL INVESTIGATION OF COOLING CONCEPT FOR AN ELECTRIC PROPULSION SYSTEM FOR AEROBATIC AIRCRAFTS
X. Liu¹, F. Ferrari¹, L. Manfriani¹; ¹Zurich University for Applied Science, Switzerland
2.2Aircraft Design
Chair(s): Rinoie, K.
Track 2
01 - Aircraft Design and Integrated Systems
11. Sep 18 14:00 14:30 2.2.1 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 2.2.2 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 2.2.3 DESIGN FOR COMFORT: AIRCRAFT INTERIORS DESIGN ASSESSMENT THROUGH A HUMAN CENTERED RESPONSE MODEL APPROACH
S. Bagassi¹, F. Lucchi¹, F. De Crescenzio¹, S. Piastra¹; ¹University of Bologna, Italy
3.2Concept Design Methodology
Chair(s): Pinon, O., Macedo, A-P.
Track 3
02 - Systems Engineering and Integration
11. Sep 18 14:00 14:30 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
11. Sep 18 14:30 15:00 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
11. Sep 18 15:00 15:30 3.2.3 ROBUST DESIGN OPTIMIZATION OF BENCHMARK AERODYNAMIC CASE BASED ON POLYNOMIAL CHAOS EXPANSION
Z. Huan¹, G. Zhenghong¹; ¹Northwestern Polytechnical University , China
4.2High Lift Aerodynamics
Chair(s): Pedreiro, L.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
11. Sep 18 14:00 14:30 4.2.1 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 4.2.2 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 4.2.3 LATTICE BOLTZMANN HIGH-LIFT SIMULATIONS - A STEP BEYOND CLASSICAL CFD
B. Koenig¹, D. Singh¹, E. Fares¹; ¹Exa GmbH, Germany
Reserve Paper 4.2.R CANCELED - 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
5.2Next Generation Commercial Transport Concept- Panel Session
Chair(s): Collier, F.
Track 5
14 - ECSC
6.2Aircraft 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 6.2.1 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 6.2.2 GLOBAL-LOCAL STRUCTURAL ANALYSIS OF COMPOSITE WINGS
E. Carrera¹, A. Pagani¹, G.H.C. Silva, Embraer S.A., Brazil; ¹Politecnico di Torino, Italy
11. Sep 18 15:00 15:30 6.2.3 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
7.2Advanced Manufacturing
Chair(s): Zhu, M.
Track 7
08 - Manufacturing and Supply Chain Management
11. Sep 18 14:00 14:30 7.2.1 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
8.2Acustics and Vibrations 2
Chair(s): Mello, O.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
11. Sep 18 14:00 14:30 8.2.1 HIGH FREQUENCY MODAL TEST AND DYNAMIC PERFORMANCE EVALUATION OF TURBINE ROTOR BLADES
J. Qin¹, X. Gao¹, W.C. Huang¹, G. Yao¹; ¹ASRI, China
11. Sep 18 14:30 15:00 8.2.2 HIGH PERFORMANCE PNEUMATIC SHOCK-ABSORBERS FOR AERONAUTICAL APPLICATIONS
R. Faraj, Institute of Fundamental Technological Research, Poland
9.2Compressor Aerodynamics
Chair(s): Pankov, S., Girgis, S.
Track 9
05 - Propulsion
11. Sep 18 14:00 14:30 9.2.1 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
11. Sep 18 14:30 15:00 9.2.2 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
11. Sep 18 15:00 15:30 9.2.3 ADAPTTIVE GTE SURGE PROTECTION SYSTEM WITH SELECTIVE CONTROL OF ACTUATORS
L.G. Bliznyukov¹, M.G. Kesselman¹, V.I. Chernyshov¹, S.A. Smetanin¹; ¹Central Institute of Aviation Motors, Russia
10.2Flight Modeling and Simulation
Chair(s): Doll, C.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
11. Sep 18 14:00 14:30 10.2.1 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 10.2.2 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 10.2.3 BAYESIAN APPROACH TO FLIGHT CHARACTERISTICS MODELING WITH REAL FLIGHT DATA
M. Naruoka, Japan Aerospace Exploration Agency, Japan
11.2De-Icing
Chair(s): Dautermann, T.
Track 11
07 - Systems, Subsystems and Equipment
11. Sep 18 14:00 14:30 11.2.1 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 11.2.2 CANCELED - 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 11.2.3 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 11.2.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
12.2On Demand Mobility: Integration in Civil Airpace
Chair(s): Kageyama, K.
Track 12
09 - Air Transport System Efficiency
11. Sep 18 14:00 14:30 12.2.1 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
11. Sep 18 14:30 15:00 12.2.2 URBAN AIR TRANSPORTATION JOURNEY TIME COMPARISON FOR MELBOURNE METROPOLITAN AREA
L. Swadesir¹, C. Bil¹; ¹RMIT University, Australia
11. Sep 18 15:00 15:30 12.2.3 ADAPTIVE LANDING SEQUENCING USING BIPARTITE GRAPHS AND PERFECT MATCHING
M. Hickson¹, C. Bil¹; ¹RMIT University, Australia

15:30 - 16:00Break

1.3NATO Hybrid/Electric Initiative
Chair(s): Nagel, B.
Track 1
01 - Aircraft Design and Integrated Systems
11. Sep 18 16:00 16:30 1.3.1 CANCELED - 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 1.3.2 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 1.3.3 CANCELED - 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 1.3.4 CANCELED - COORDINATING INTERNATIONAL RESEARCH AND DEVELOPMENT IN HYBRID/ELECTRIC FLIGHT
n/a Kloeckner, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany
2.3Supersonic and Hypersonic Vehicles
Chair(s): Melkert, J.
Track 2
01 - Aircraft Design and Integrated Systems
11. Sep 18 16:00 16:30 2.3.1 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 2.3.2 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 2.3.3 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 2.3.4 ANALYSIS OF LOW-BOOM CHARACTERISTICS OF SUPERSONIC WAVERIDER
P. Boonjaipetch, Tohoku University, Japan
Reserve Paper 2.3.R AN EFFICIENT FRAMEWORK FOR AERODYNAMIC CONFIGURATION EVOLUTION OF REENTRY VEHICELES
M.M. Entezari¹, M. Mohammadi-Amin¹; ¹ARI, Iran
3.3Systems Engineering Cases
Chair(s): Dunyach, J.C., Molina-Cristobal, A.
Track 3
02 - Systems Engineering and Integration
11. Sep 18 16:00 16:30 3.3.1 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 3.3.2 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 3.3.3 A 7D TRADE
D.K. Howarth, MEE Inc., United States
11. Sep 18 17:30 18:00 3.3.4 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
4.3CFD Applications
Chair(s): Santos, L., Cenko, A.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
11. Sep 18 16:00 16:30 4.3.1 CFD VERIFICATION AND VALIDATION FOR INDUSTRIAL APPLICATIONS
M. Mani¹, A. Cary¹; ¹Boeing, United States
11. Sep 18 16:30 17:00 4.3.2 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 4.3.3 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 4.3.4 CANCELED - NUMERICAL SIMULATION OF OPERATING PROCESS ELEMENTS FOR COMBUSTION CHAMBERS OF PERSPECTIVE GTE
P.A. Semenev, Central Institute of Aviation Motors, Russia
Reserve Paper 4.3.R CANCELED - SIMULATION OF TRANSONIC FLOW OVER SPACE VEHICLE
N.V. Palchekovskaya, MIPT, Russia
5.3Student Hands On Activities
Chair(s): Suzuki, S.
Track 5
14 - ECSC
11. Sep 18 16:00 16:30 5.3.1 ALL JAPAN STUDENT\'S INDOOR FLYING ROBOT CONTEST
T. Tsuchiya, The University of Tokyo, Japan
11. Sep 18 16:30 17:00 5.3.2 THE AERONAUTICAL SOCIETY OF SOUTH AFRICA AEROSPACE CHALLENGE
J.S. Monk, CSIR, South Africa
11. Sep 18 17:00 17:30 5.3.3 CANCELED - SAE BRASIL AEROSPACE PROGRAMS – A SUCCESS STORY
H.A. Forjaz, SAEBRASIL, Brazil
6.3New 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 6.3.1 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 6.3.2 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 6.3.3 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 6.3.4 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
7.3Optimization
Chair(s): Jamison, K.
Track 7
03.4 - Applied Aerodynamics
11. Sep 18 16:00 16:30 7.3.1 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 7.3.2 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 7.3.3 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 7.3.4 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
8.3Aeroelasticity 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 8.3.1 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 8.3.2 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 8.3.3 CANCELED - 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 8.3.4 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
9.3MDO AGILE
Chair(s): Mirzoyan, A.
Track 9
05 - Propulsion
11. Sep 18 16:00 16:30 9.3.1 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 9.3.2 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 9.3.3 CANCELED - 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 9.3.4 PROPULSION SYSTEM - AIRFRAME INTEGRATION AND OPTIMIZATION OF CIVIL AIRCRAFT- AGILE EU PROJECT
K.S. Anisimov¹, A.A. Savelyev¹, I.A. Kursakov¹, A.V. Lysenkov¹, A.A. Mirzoyan, CIAM, Russia; P.S. Prakasha, Institute of System Architectures in Aeronautics, DLR, Germany; ¹TSAGI, Russia
10.3Flight Trajectory Design
Chair(s): Ueno, S.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
11. Sep 18 16:00 16:30 10.3.1 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 10.3.2 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 10.3.3 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 10.3.4 NEW APPROACH FOR INVESTIGATION OF MAXIMUM-RANGE AIRCRAFT TRAJECTORIES
A.E. Sagalakov¹, A.S. Filatyev¹; ¹TsAGI, Russia
11.3Electro Mechanical Actuation Systems
Chair(s): Mare, J.C.
Track 11
07 - Systems, Subsystems and Equipment
11. Sep 18 16:00 16:30 11.3.1 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 11.3.2 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 11.3.3 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 11.3.4 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
12.3Air Transportation Efficiency
Chair(s): Tomoko, I.
Track 12
09 - Air Transport System Efficiency
11. Sep 18 16:00 16:30 12.3.1 CANCELED - 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 12.3.2 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 12.3.3 CANCELED - 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 12.3.4 THE GLOBAL FUEL SAVING POTENTIAL OF INTERMEDIATE STOP OPERATIONS CONSIDERING METEOROLOGICAL AND OPERATIONAL INFLUENCES
F. Linke, German Aerospace Center (DLR), Germany
Reserve Paper 12.3.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

0.4ICAS 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: Eri Itoh, ECSC Chair
11. Sep 18 18:00 19:30