30th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

Please use your browser's search function (Ctrl+F) to look up a specific author or title.

Attention: Be advised that there might be changes till the congress, so please do not adjust your travel plans based on this preliminary programme.

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:
11. Sep 18 08:00 09:00

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

1.1Design Education 1
Chair(s): Rinoie, K.
Track 1
01 - Aircraft Design and Integrated Systems
11. Sep 18 10:00 10:30 1.1.1 COLLABORATIVE OPEN SOURCE AIRCRAFT DESIGN FRAMEWORK FOR EDUCATION - AGILE ACADEMY INITIATIVES AND RESULTS
P S Shivaprakasha, Germany
11. Sep 18 10:30 11:00 1.1.2 WHAT WE CAN DO TODAY TO EDUCATE AND TRAIN THE COLLABORATIVE ENGINEER OF TOMORROW
M. Spieck, Thelsys, Germany
11. Sep 18 11:00 11:30 1.1.3 EXPERIENCE WITH INTERNATIONAL COLLABORATIVE AIRCRAFT DESIGN EDUCATION: AREND UAV
L Smith, University of Pretoria, South Africa
11. Sep 18 11:30 12:00 1.1.4 ELECTRIC VTOL UAV CONFIGURATION STUDIES AND OPTIMIZATION WITHIN AIRCRAFT DESIGN PRACTICAL COURSE AT TECHNICAL UNIVERSITY
C. Rößler, Technical University of Munich, Germany
Reserve Paper 1.1.R DESIGN AND FABRICATION OF A SAILPLANE FLY-BY-WIRE HIGH-ASPECT-RATIO WING
P. Iscold, UFMG, Brazil
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 Bonet, The Boeing Company, United States
11. Sep 18 10:30 11:00 2.1.2 SINGLE-AISLE AIRLINER DISRUPTION WITH A SINGLE-DECK BLENDED WING BODY
M. Page, DZYNE Technologies, Inc., United States
11. Sep 18 11:00 11:30 2.1.3 CONCEPTUAL DESIGN OF THE D8, A HIGHLY-EFFICIENT SUBSONIC COMMERCIAL TRANSPORT AIRCRAFT
B.Y. Yutko, Aurora Flight Sciences, United States
11. Sep 18 11:30 12:00 2.1.4 SUBSONIC ULTRA-GREEN AIRCRAFT RESEARCH: TRANSONIC TRUSS-BRACED WING TECHNICAL MATURATION UPDATE
C. Droney, Boeing, United States
3.1Systems Architecting
Chair(s): Schwartz, K., Guimearaes, F.
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.J.M. Lakemond, 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
FMST Turetta, EMBRAER, Brazil
11. Sep 18 11:00 11:30 3.1.3 AIRCRAFT SYSTEMS ARCHITECTING: LOGICAL-COMPUTATIONAL DOMAIN INTERFACE
M. D. Guenov, Cranfield University, 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
A.-P. Mattei, Senai Innovation Institute, 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.
Gonzalez-Biedma: Gonzalez-Biedma, Airbus Defence & Space, Spain
11. Sep 18 10:30 11:00 4.1.2 MORPHING WING WITH SURFACE DISCONTINUITY - COMPARATIVE WIND TUNNEL TESTS.
TGG Goetzendorf-Grabowski, Warsaw 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
11. Sep 18 11:30 12:00 4.1.4 NUMERICAL ANALYSIS OF BLEND WING BODY AIRFRAME AND ENGINE AERODYNAMIC INTERFERENCE
Zhaoguang Tan, China; Yingchun Chen, China; Jiangtao Si, China; Yuan Zhong, China
Reserve Paper 4.1.R COMPARISON AND APPLICATION OF DIFFERENT TECHNIQUES OF MULTI-OBJECTIVE OPTIMIZATION FOR AERODYNAMICS WINGS DESIGN
N Manzanares-Filho¹, E-R Da Silva¹; ¹UNIFEI, Brazil
5.1Unsteady Flows and Aeroacoustics
Chair(s): Yingchun, C.
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 USING MEMS MICROPHONES FOR UNSTEADY PRESSURE MEASUREMENTS AT THE EESC-USP FAN RIG
B. Martinez R. Junior, University 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 CHALLENGES OF AERO-ACOUSTIC MEASUREMENTS IN WIND TUNNEL: IDENTIFICATION AND ELIMINATION OF “PARASITE” NOISE
Y.F. Sun, COMAC, China
Reserve Paper 5.1.R TIME-RESOLVED PRESSURE FIELDS FOR AN AIRFOIL WITH SELF-SUSTAINED SHOCK OSCILATIONS
H. Leite, Instituto Tecnológico de Aeronáutica, 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. Horton, Virginia Tech, 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
11. Sep 18 11:30 12:00 6.1.4 MODIFIED WHITNEY-NUISMER CRITERIA FOR PREDICTION OF NOTCHED STRENGTH OF COMPOSITE LAMINATES
S. F, M. Almeida, Departmen of Mechatronics - University of Sao Paulo, Brazil
Reserve Paper 6.1.R RESULTS AND COMPARISON OF NUMERICAL SIMULATION AND THE TESTING OF LUG MANUFACTURED BY COMPOSITE MATERIAL BY RTM PROCESS
Cássio da Fonseca, Embraer S/A, Brazil
7.1Aeroacoustics and Icing
Chair(s): Collier, F.
Track 7
03.4 - Applied Aerodynamics
11. Sep 18 10:00 10:30 7.1.1 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
11. Sep 18 10:30 11:00 7.1.2 VALIDATION OF LIQUID WATER CONTENT SIMULATION USING THE FILM THICKNESS AT STAGNATION POINT
D. de Rosa, CIRA, Italy
11. Sep 18 11:00 11:30 7.1.3 AN INTEGRATED CFD-SEA METHODOLOGY TO ACCOUNT FOR AERODYNAMIC SOURCES INTO CABIN NOISE PREDICTIONS
B Guaraldo Neto, Embraer SA, Brazil
11. Sep 18 11:30 12:00 7.1.4 THE STUDIES ON LOW-NOISE LAMINAR WING REGIONAL AIRCRAFT
N.A. Pushchin, TsAGI, Russia
Reserve Paper 7.1.R ANALYSIS OF WEATHER BALLOON DATA TO EVALUATE THE AERODYNAMIC INFLUENCE ON THE LAUNCH PHASE OF SHEFEX II
M. Franze, DLR, Germany
8.1Aeroelasticity 3 : Fixed-wing Aircraft
Chair(s): Chizhov, A.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
11. Sep 18 10:00 10:30 8.1.1 AEROELASTIC PROPERTIES OF ACTIVE WINGLETS
G. Amiryants, TsAGI, Russia
11. Sep 18 10:30 11:00 8.1.2 MODELLING OF FLUTTER CHARACTERISTICS OF AIRCRAFT WING WITH PYLON-MOUNTED ENGINE NACELLE
YU QIJING¹, LEE Saeil¹, M. Damodaran¹, B.C. Khoo¹; ¹National University of Singapore, Singapore
11. Sep 18 11:00 11:30 8.1.3 MODELING BY INTERCONNECTION OF A FLEXIBLE WING WITH TIP TANK AND APPLICATION TO AEROELASTICITY
F.L. Cardoso-Ribeiro, Instituto Tecnologico de Aeronautica, Brazil
11. Sep 18 11:30 12:00 8.1.4 FLUTTER ANALYSIS OF TWIN TURBOPROP AIRCRAFT WITH TIP-TANKS
J. Cecrdle¹, O. Vich¹; ¹Aeronautical Research and Test Institute (VZLU) , Czech Republic
Reserve Paper 8.1.R EDGELESS AERODYNAMIC CONTROL SURFACES WITH A MORPHING SKIN AND GAP COVER CONCEPT
M. Mahl, TU Munich, Germany
9.1Engine Performance
Chair(s): Remy, S.
Track 9
05 - Propulsion
11. Sep 18 10:00 10:30 9.1.1 THE PHYSICS BEHIND MCHANICS AND FAILURE OF GAS TURBINE COMPONENTS IN AEROSPACE SYSTEMS
Prakash Patnaik , National 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
A. Smetanin, Central Institute of Aviation Motors (CIAM), Russia
10.1Control for Flexible Aircraft
Chair(s): Ueno, S.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
11. Sep 18 10:00 10:30 10.1.1 IMPLEMENTATION OF A STABILITY AUGMENTATION SYSTEM ON A VERY FLEXIBLE AIRCRAFT
P. J. González, Instituto Tecnologico de Aeronautica (ITA), Brazil
11. Sep 18 10:30 11:00 10.1.2 ADAPTIVE NEURAL NETWORK CONTROLLER APPLIED FOR A FLEXIBLE AIRCRAFT
G. Barbosa, Instituto Tecnológico de Aeronáutica, Brazil
11. Sep 18 11:00 11:30 10.1.3 ADAPTIVE OUTPUT-FEEDBACK GAIN SCHEDULING APPLIED FOR FLEXIBLE AIRCRAFT
R.B. Bertolin, ITA, Brazil
11. Sep 18 11:30 12:00 10.1.4 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
Reserve Paper 10.1.R FLIGHT TESTING AN ADAPTIVE GUST LOADS ALLEVIATION ON A FLEXIBLE AIRCRAFT
Y. Wang, China Academy of Aerospace Aerodynamics, China
11.1UAS Flight Test
Chair(s): Götzendorf-Grabowski, T.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
11. Sep 18 10:00 10:30 11.1.1 IN-FLIGHT AEROELASTIC TESTING OF A FLEXIBLE UAV USING A MIXED ACCELERATION/STRAIN SENSORS OPERATIONAL MODAL ANALYSIS
D. F. Castillo Zúñiga, Instituto Tecnologico de Aeronáutica, Brazil
11. Sep 18 10:30 11:00 11.1.2 METHODS FOR EFFICIENT FLIGHT TESTING AND MODELLING OF REMOTELY-PILOTED AIRCRAFT WITHIN VISUAL LINE-OF-SIGHT
A Sobron, Linköping University, Sweden
11. Sep 18 11:00 11:30 11.1.3 VERTICAL LANDING OF A FIXED-WING UAV USING THE FLAT SPIN
S. Higashino, Kyushu University, Japan; K. Nakama, Kyushu University, Graduate Student, Japan
11. Sep 18 11:30 12:00 11.1.4 FLIGHT PLANNING, IMPLEMENTATION, AND CONDUCT OF AN AUTOMATIC FIRST FLIGHT OF A UAV
M. E. Kuegler, Inst. of Flight System Dynamics, Technical University of Munich, Germany
Reserve Paper 11.1.R SAFETY FLIGHT TESTING FOR CARGO UAV DEVELOPMENT
I.K Iwata, National Institute of Advanced Industrial Science and Technology, Japan
12.1Aircraft Operation 1
Chair(s): Tokuakid@mpat.go.jp, 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 Dautermann, DLR, Germany
11. Sep 18 11:00 11:30 12.1.3 OPERATIONAL CONCEPT AND VALIDATION OF A NEW AIRPORT LOW-LEVEL WIND INFORMATION SYSTEM
Tomoko Iijima, 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
Reserve Paper 12.1.R OPERATIONAL ASSESSMENT OF PASSENGER BOARDING STRATEGIES FOR COMMERCIAL AIRCRAFT
M. Schmidt, Bauhaus Luftfahrt, Germany

12:00 - 13:00Lunch

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

1.2Unconventional Concepts 1
Chair(s): Kimmel, B.
Track 1
01 - Aircraft Design and Integrated Systems
11. Sep 18 14:00 14:30 1.2.1 CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATION
A. Seitz, Bauhaus Luftfahrt e.V., Germany
11. Sep 18 14:30 15:00 1.2.2 SYSTEM-LEVEL ASSESSMENT OF TAIL-MOUNTED PROPELLERS FOR REGIONAL AIRCRAFT
R. Vos, TU Delft, Netherlands
11. Sep 18 15:00 15:30 1.2.3 EXPLORATION OF THE AIRBUS “NAUTILIUS” ENGINE INTEGRATION CONCEPT
L. Wiart, ONERA, France
Reserve Paper 1.2.R CONSTRAINED BIFURCATION AND CONTINUATION METHOD IN BLENDED-WING-BODY AIRCRAFT DESIGN
F. Cen, China Aerodynamics Research and Development Center, China
2.2Aircraft Design
Chair(s): Isikveren, A.
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. M. T. Cavalcanti, Embraer, Brazil
11. Sep 18 14:30 15:00 2.2.2 CONTAINERIZED AIR FREIGHT SYSTEM POWERED BY CRYOGENIC FUEL
E.A. Pigusov, TsAGI, Russia
11. Sep 18 15:00 15:30 2.2.3 DESINING A NOVEL MODULAR, FLEXIBLE AIRCRAFT
JN Reis, Embraer Portugal, Portugal
3.2Desktop Simulations
Chair(s): Dunyach@airbus.com, J.C., Nakashima, C.
Track 3
02 - Systems Engineering and Integration
11. Sep 18 14:00 14:30 3.2.1 VIRTUAL ENGINE: CONCEPTION, SIMULATION, MODELS, STRUCTURE AND PARTS OPTIMIZATION
Y. Temis, Central Institute of Aviation Motors, Russia
11. Sep 18 14:30 15:00 3.2.2 RESEARCH ON DESKTOP VIRTUAL INTEGRATION AND VERIFICATION OF CIVIAL AIRCRAFT
Zhichao Yao¹, Bozhi Guo, China-Russia Commercial Aircraft International Co., China; Dianhuang Xie¹, Zhengqiang Li¹; ¹Shanghai Aircraft Design and Research Institute, China
11. Sep 18 15:00 15:30 3.2.3 A NOVEL FMI AND TLM-BASED DESKTOP SIMULATOR FOR DETAILED STUDIES OF THERMAL PILOT COMFORT
G. R. Hällqvist, Saab Aeronautics, Sweden
4.2High Lift Aerodynamics
Chair(s): Pedreiro, L., Nicolosi, F.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
11. Sep 18 14:00 14:30 4.2.1 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
C.-V. Cusati, University 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 Koenig, Exa GmbH, Germany
Reserve Paper 4.2.R NUMERICAL INVESTIGATION AERODYNAMICS NACELLE-STRAKE EFFECT
H.W.M. Hoeijmakers, University of Twente, Netherlands
5.2Advanced Transport Aircraft Concepts for Environmentally Responsible Aviation
Chair(s): ,
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. Kling, Bauhaus Luftfahrt e.V., Germany
11. Sep 18 14:30 15:00 6.2.2 BUCKLING/POSTBUCKLING OPTIMIZATION OF STIFFENED COMPOSITE PANELS BASED ON SENSITIVITY ANALYSIS
Dong L.-J Dong, China
11. Sep 18 15:00 15:30 6.2.3 GLOBAL-LOCAL STRUCTURAL ANALYSIS OF COMPOSITE WINGS
E. Carrera, Politecnico di Torino, Italy
Reserve Paper 6.2.R AERODYNAMIC AND FEM ANALYSIS OF A WOODEN SEAPLANE
M. Ferrara, politecnico di Torino, Italy
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 RISK ASSESSMENT PROCESS FOR AUTOMATED SEALING APPLICATION IN A HUMAN ROBOT COLLABORATION ENVIRONMENT - A 3D SIMULATION A
DQ Queiroz, Embraer, Brazil
11. Sep 18 14:30 15:00 7.2.2 MITIGATING THE RISKS OF PRODUCIBILITY FAILURES DURING CONCEPT PLATFORM DEVELOPMENT
J. Madrid¹, J. Landahl¹, R. Söderberg¹, H. Johsnnesson¹, J. Lööf, GKN Aerospace, Sweden; ¹Chalmers University of Technology, Sweden
11. Sep 18 15:00 15:30 7.2.3 STUDIES ON AIRCRAFT ROBOT AIDED MANUFACTURING
G. J. G Lahr¹, J. V. R. Soares¹, G. A. P. Caurin¹; ¹University of Sao Paulo, Brazil
8.2Impact
Chair(s): Kurdelski, M.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
11. Sep 18 14:00 14:30 8.2.1 VERIFIED FUSELAGE SECTION WATER IMPACT MODELING
YK Song, Virginia Tech, United States
11. Sep 18 14:30 15:00 8.2.2 PREDICTING LOW-VELOCITY IMPACT DAMAGE IN COMPOSITE PANELS USING COHESIVE ELEMENT
no liu, FAI AVIC, China
11. Sep 18 15:00 15:30 8.2.3 THE STUDY OF THE IMPACT OF SELECTED LOAD SEQUENCES ON AIRCRAFT FATIGUE LIFE
MK Kurdelski, Air Force Institute of Technology, Poland
Reserve Paper 8.2.R ENERGY-ABSORBING CHARACTERISTICS ANALYSIS OF COMPOSITE THIN-WALLED C-CHANNELS UNDER LOW SPEED AXIAL COMPRESSION
J.-X. XIE, Civil Aviation University of China, China
9.2MDO-1
Chair(s): Garnier, V.
Track 9
05 - Propulsion
11. Sep 18 14:00 14:30 9.2.1 IN-FLIGHT ACOUSTIC LOADS MEASUREMENTS ON AN ENGINE FLYING TEST BED
Y.F. Sun, COMAC, China
11. Sep 18 14:30 15:00 9.2.2 MULTI-DISCIPLINARY OPTIMISATION OF A TURBOPROP-POWERED UNMANNED AERIAL VEHICLE
D. Verstraete, The University of Sydney, Australia
11. Sep 18 15:00 15:30 9.2.3 AN AEROTHERMODYNAMIC MODEL OF AIRCRAFT ENGINE PROPULSION SYSTEMS USING OBJECT-ORIENTED PROGRAMMING
F. B. O. Oliveira, UFMG, Brazil
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. Paulino, Instituto Tecnologico de Aeronautica, 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. S. 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
Reserve Paper 10.2.R DATA-DRIVEN FAILURE IDENTIFICATION USING A MOTION-BASED SIMULATOR
A. D. Kraemer¹, E. Villani¹; ¹Instituto Tecnológico de Aeronáutica (ITA), Brazil
11.2UAS Control 1
Chair(s): Bidinotto, J.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
11. Sep 18 14:00 14:30 11.2.1 COMPARATIVE ANALYSIS OF METHODS USED TO ACTIVE CONTROL OF MICRO AERIAL VEHICLE
K.-S Sibilski, Warsaw University of Technology, Poland
11. Sep 18 14:30 15:00 11.2.2 ROBUST TRAJECTORY OPTIMIZATION OF VTOL TRANSITION MANEUVER USING BI-LEVEL OPTIMAL CONTROL
P. Piprek¹, F. Holzapfel¹; ¹Technical University of Munich, Germany
11. Sep 18 15:00 15:30 11.2.3 FIXED-WING UAV ROBUST GUIDANCE STRATEGY BASED ON COMPOUND FLIGHT MISSION OF ON-GROUND TARGETS
JL Gomes Olavo, Federal University of Minas Gerais (UFMG), Brazil
Reserve Paper 11.2.R MODELING, CONTROL AND HARDWARE-IN-THE-LOOP SIMULATION OF A GENERIC TILTING MULTI-ROTOR
F.M.M Machini Malachias Marques, Universidade Federal de Uberlândia, Brazil
12.2Cyber Security
Chair(s): ,
Track 12
10 - Safety and Security
11. Sep 18 14:00 14:30 12.2.1 IN-SERVICE AIRCRAFT CYBERSECURITY RISK ASSESSMENT
G.C.B. Bertoli, Brazil
11. Sep 18 14:30 15:00 12.2.2 IMPACT STUDY ON CYBER THREATS TO GNSS AND FMS SYSTEMS
R. Geister, DLR, Germany
11. Sep 18 15:00 15:30 12.2.3 A METHOD TO DESIGN CYBER-PHYSICAL RESILIENT ARCHITECTURES
ET YANO, ITA, Brazil

15:30 - 16:00Break

1.3NATO Hybrid/Electric Initiative
Chair(s): Isikveren, A.
Track 1
01 - Aircraft Design and Integrated Systems
11. Sep 18 16:00 16:30 1.3.1 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 1.3.2 FLIGHT TEST OF A FUEL-CELL/BATTERY/SUPERCAPACITOR TRIPLE HYBRID UAV PROPULSION SYSTEM
D. Verstraete, Australia; J. Palmer, Australia
11. Sep 18 17:00 17:30 1.3.3 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 1.3.4 COORDINATING INTERNATIONAL RESEARCH AND DEVELOPMENT IN HYBRID/ELECTRIC FLIGHT
n/a Kloeckner, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany
2.3Personal Air Mobility
Chair(s): Melkert, J.
Track 2
01 - Aircraft Design and Integrated Systems
11. Sep 18 16:00 16:30 2.3.1 VTOL DISTRIBUTED ELECTRIC PROPULSION VEHICLE ARCHITECTURES FOR URBAN AND INTERURBAN AIR TAXI
Cl. Le Tallec, ONERA, France
11. Sep 18 16:30 17:00 2.3.2 A PERFORMANCE BENCHMARK OF RECENT PERSONAL AIR VEHICLE CONCEPTS FOR URBAN AIR MOBILITY
M. Shamiyeh¹, R. Rothfeld¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
11. Sep 18 17:00 17:30 2.3.3 SMALL AIRCRAFT CONCEPT FOR REGIONAL ON-DEMAND AIR MOBILITY
P. Strathoff, RWTH Aachen University, Germany
11. Sep 18 17:30 18:00 2.3.4 INVESTIGATION OF ‘JUMP TAKEOFF’ POSSIBILITY FOR THE NEW CONCEPT OF MODERN AUTOGYRO
R. Zurawski, Institute of Aviation, Poland
3.3Systems Engineering Cases
Chair(s): Krus, P., Guenov, M.
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, F. Wolters¹, R.-G. Becker¹, C. Klein¹, S. Reitenbach¹; ¹German Aerospace Center , Germany
11. Sep 18 17:00 17:30 3.3.3 A 7D TRADE
Doug Howarth, MEE Inc., United States
11. Sep 18 17:30 18:00 3.3.4 BUILDING INNOVATIVE BUSINESS MODELS IN AERONAUTICS INDUSTRY: SOME LESSONS FROM THE BIONIC AIRCRAFT PROJECT
LP Pereira, Federal University of ABC, Brazil
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. Mani, The Boeing Company, 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
G. A. L. da Silva, ATS Aerothermal 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. Chen, School of Aeronautics, Northwestern Polytechnical University, China
11. Sep 18 17:30 18:00 4.3.4 NUMERICAL SIMULATION OF OPERATING PROCESS ELEMENTS FOR COMBUSTION CHAMBERS OF PERSPECTIVE GTE
P.A. Semenev, Central Institute of Aviation Motors, Russia
Reserve Paper 4.3.R LAUNCHER AERODYNAMIC ANALYSIS WITH PLUME EFFECTS
. Viviani, Università della Campania, Italy
5.3Experiments in Flow Control
Chair(s): Manfriani, L.
Track 5
03.2 - Experimental Aerodynamics
11. Sep 18 16:00 16:30 5.3.1 EXPERIMENTAL ANALYSIS OF THE S1223 AIRFOIL WITH A LEADING-EDGE DEVICE AT LOW REYNOLDS NUMBERS
G.B.B. Hübbe, Brazil
11. Sep 18 16:30 17:00 5.3.2 EXPERIMENTAL STUDY OF SYNTHETIC JET ACTUATOR FLOW CONTROL ON A NACA0015
N.D. Martin, Northumbria University, United Kingdom
11. Sep 18 17:00 17:30 5.3.3 EXPERIMENTAL INVESTIGATION OF WING LOAD CONTROL USING FLUIDIC DEVICES
Krzysiak A. Krzysiak, Institute of Aviation, Poland
11. Sep 18 17:30 18:00 5.3.4 EXPERIMENTAL STUDY OF TRANSONIC FLOW OVER AN AIRFOIL ON LAMINAR FLOW AND LEADING EDGE TUBERCLES
R.G. Annes da Silva, ITA, Brazil
6.3Aircraft Structural Design II
Chair(s): Ireman, T.
Track 6
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
11. Sep 18 16:00 16:30 6.3.1 STRUCTURAL DESIGN OF THE LARUS QR-15 SAILPLANE WING
J. Laguardia, Univesidade Federal de Minas Gerais, Brazil; L. Pereira, Universidade Federal de Minhas Gerais, Brazil; D. Azevedo, Universidade Federal de Minas Gerais, Brazil
11. Sep 18 16:30 17:00 6.3.2 PRELIMINARY ASSESSMENT OF A WARPING WING CONFIGURATION IN ROLLING CONTROL
E. Cestino, Politecnico di Torino, Italy
11. Sep 18 17:00 17:30 6.3.3 STRUCTURAL DESIGN AND ANALYSIS OF A QUADROTOR FIXED-WING HYBRID UAV WING
W.F. Fang, Northwestern Polytechnical University, China
11. Sep 18 17:30 18:00 6.3.4 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
Reserve Paper 6.3.R 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
7.3Optimization
Chair(s): Jamison, K.
Track 7
03.4 - Applied Aerodynamics
11. Sep 18 16:00 16:30 7.3.1 MULTI-POINTS 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
Chao Wang, China
11. Sep 18 17:00 17:30 7.3.3 SURROGATE-BASED OPTIMIZATION METHOD APPLIED TO MULTIDISCIPLINARY DESIGN OPTIMIZATION ARCHITECTURES
C.-Z Xu, China
11. Sep 18 17:30 18:00 7.3.4 COMBINING ADJOINT-BASED AND SURROGATE-BASED OPTIMIZATIONS FOR BENCHMARK AERODYNAMIC DESIGN PROBLEMS
H Wang, China
Reserve Paper 7.3.R WING TWIST OPTIMISATION OF A BENCHMARK PROBLEM USING TWO AERODYNAMIC SOLVERS
G. Yang, University of Southampton, United Kingdom
8.3Aeroelasticity 4: 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 INVESTIGATION OF PROPELLER INFLUENCE ON STALL AND DYNAMIC BEHAVIOR OF VERY FLEXIBLE AIRCRAFT
P Teixeira, University of Michigan, United States
11. Sep 18 16:30 17:00 8.3.2 REDUCED ORDER MODELS FOR NONLINEAR AEROELASTICITY
R. R. Medeiros, University of Michigan, United States
11. Sep 18 17:00 17:30 8.3.3 NONLINEAR STATIC AEROELASTIC AND TRIM ANALYSIS OF HIGHLY FLEXIBLE AIRCRAFT
Chi Zhang¹, Zhou Zhou¹, Pu 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
wei Qian, Dalian University of Technology, China
Reserve Paper 8.3.R 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
9.3Fan and Propeller
Chair(s): Yimer, I., Lamiscarre, B.
Track 9
05 - Propulsion
11. Sep 18 16:00 16:30 9.3.1 STUDY ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLERS WITH PROPLETS
X.D.-Y Yang, Northwestern Polytechnical University , China
11. Sep 18 16:30 17:00 9.3.2 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
11. Sep 18 17:00 17:30 9.3.3 CERTAIN ASPECTS OF FAN MODEL STAGES DESIGNING FOR ADVANCED AIRCRAFT ENGINES
Sergey Pankov¹, Victor Mileshin¹, Igor Orekhov¹, Victor Fateev¹; ¹Central Institute of Aviation Motors, Russia
11. Sep 18 17:30 18:00 9.3.4 AN INTEGRATED PROPULSION SYSTEM FOR BI-MODAL UNMANNED VEHICLES
A. Bacciaglia¹, D. Guo², P. Marzocca², C. Bil², A. Ceruti¹; ¹University of Bologna, Italy ;²RMIT University, Australia
Reserve Paper 9.3.R PARAMETRIC INVESTIGATION OF EESC-USP AEROACOUSTIC FAN RIG
R.G Cuenca, UFSC, Brazil
10.3Flight Trajectory Design
Chair(s): Tsuchiya, T.
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 WORST-CASE 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. Abdelmoula, German Aerospace Center DLR, Germany
11. Sep 18 17:00 17:30 10.3.3 ROBUST TRAJECTORY OPTIMIZATION OF A HYPERSONIC VEHICLE VIA SENSITIVITY PENALTY
T. Akman, Technical 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. Sagalakov, Central Aerohydrodynamic Institute, Russia
11.3Flight Test and Equipment
Chair(s): ,
Track 11
07 - Systems, Subsystems and Equipment
11. Sep 18 16:00 16:30 11.3.1 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 16:30 17:00 11.3.2 GROUND AND FLIGHT TESTING OF A MULTI-SENSOR OBSTACLE DETECTION AND TRACKING SYSTEM FOR RPAS SITUATION AWARENESS
J Gauci, University of Malta, Malta
11. Sep 18 17:00 17:30 11.3.3 DESIGNING A VISION-BASED SYSTEM TO MEASURE IN-FLIGHT WING DEFORMATION
A Sanches, Aeronautics Institute of Technology , Brazil
11. Sep 18 17:30 18:00 11.3.4 POWER LINE COMMUNICATION APPLIED TO FLIGHT TEST INSTRUMENTATION
M. Ribeiro, Federal University of Juiz de Fora, Brazil
Reserve Paper 11.3.R REQUIREMENTS AND CONSIDERATIONS FOR A HARDWARE-IN-THE-LOOP TEST BENCH FOR UNMANNED AERIAL VEHICLE
L. Anastasopoulos, Institute of Aircraft Design, Technical University of Munich, Germany
12.3Human Factors
Chair(s): Consiglio, M.
Track 12
10 - Safety and Security
11. Sep 18 16:00 16:30 12.3.1 3D AUDIO SUPPORT FOR HELICOPTER PILOTS DURING CONFINED AREA LANDINGS
C. A. Niermann, German Aerospace Center (DLR), Germany
11. Sep 18 16:30 17:00 12.3.2 INDIVIDUALIZING FLIGHT SKILL TRAINING USING SIMULATOR DATA ANALYSIS AND BIOFEEDBACK
J.O. Entzinger¹, T. Uemura¹, S. Suzuki¹; ¹The University of Tokyo, Japan
11. Sep 18 17:00 17:30 12.3.3 DESIGN OF A DISTRIBUTED HUMAN FACTORS LABORATOTY FOR FUTURE AIR SYSTEMS
- Alfredson, Saab, Sweden
11. Sep 18 17:30 18:00 12.3.4 CREW TRAINING USING ANIMATION
P. M. Razaboni, Embraer SA, Brazil
Reserve Paper 12.3.R HUMAN RELIABILITY ANALYSIS IN AN AIRCRAFT DECOMPRESSION EVENT
C. Reiser, Embraer, Brazil