Session List
Interactive Presentations
Reserve Papers
Monday, 10. September 2018
RaumTrack 1Track 2Track 3Track 4Track 5Track 6Track 7Track 8Track 9Track 10Track 11Track 12
07:00
08:00
Registration
08:00
09:00
Opening Ceremony
09:00
10:00
ICAS Daniel & Florence Guggenheim Memorial Lecture - Humberto Pereira, Embraer - Product Development Challenges in the Commercial Airplane Market - Chair: Susan Ying, ICAS President, US
10:00
10:30
Break
10:30
12:00
1.1
Novel Application of MDO in Aircraft Design 1
2.1
UAS 1
3.1
System of Systems Design
4.1
Unsteady Aerodynamics 1
5.1
Experiments in Flow Control
6.1
Fundamental Fluid Dynamics 1
7.1
Flow Control
8.1
Acustics and Vibrations 1
9.1
MDAO- multidisciplinary analysis and optimization
10.1
FT & RC
11.1
UAS Control 1
12.1
Safety Analysis
12:00
13:00
Lunch
13:00
14:30
1.2
Novel Application of MDO in Aircraft Design 2
2.2
UAS 2
3.2
Modeling and Simulation in Manufacturing
4.2
Unsteady Aerodynamics 2
5.2
Aerodynamic Effects of Propulsion Integration
6.2
Fundamental Fluid Dynamics 2
7.2
Unmanned Aircraft
8.2
New Structural Design 2: Morphing Structures
9.2
Combustion
10.2
Flight Handling Quality
11.2
UAS Trajectory
12.2
Cyber Security / Human Factors
14:30
15:00
Break
15:00
16:30
1.3
Design Education 1
2.3
UAS 3
3.3
Additive Manufacturing
4.3
Numerical Methods
5.3
Wind Tunnel Test Technology
6.3
Loads
7.3
Wing Optimisation
8.3
Aeroelasticity 1 : Fixed-wing Aircraft
9.3
Turbine Aerodynamics
10.3
Hydraulic Actuation
11.3
UAS VTOL
12.3
UAS - Unmanned Aircraft Systems
16:35
18:35
General Lecture I - Technology Leadership Forum - Intelligent and Autonomous Engineering in Aeronautics - Dr. P.Nielsen, Mr. J.Tylko , Mr. Y.Nakagawa, Dr. G. Holmberg, Maj L. Haberfeld - Chair: Shinji Suzuki, Chair ICAS Programme Committee, JP
Tuesday, 11. September 2018
RaumTrack 1Track 2Track 3Track 4Track 5Track 6Track 7Track 8Track 9Track 10Track 11Track 12
08:00
09:00
General Lecture II - Autonomy and the future of Aerospace - N. Pendleton, Boeing, USA - Chair: Gunnar Holmberg, ICAS Treasurer, , SE
09:00
10:00
Interactive Presentations - Chair: Artur Mirzoyan, , RU
10:00
12:00
1.4
Unconventional Concepts 1
2.4
Next Generation Commercial Transport Concept
3.4
Systems Architecting
4.4
Aerodynamic Design
5.4
Unsteady Flows and Aeroacoustics
6.4
Composites
7.4
Store Separation
8.4
Aeroelasticity 2 : Methods and Modeling
9.4
Engine Performance
10.4
Flight Testing
11.4
Flight Test and Equipment
12.4
Aircraft Operation 1
12:00
13:00
Lunch
13:00
13:45
ICAS Casimiro Montenegro Filho Lecture for Innovation in Aeronautics - AGILE Project Consortium - Chair: Michel Peters, ICAS EC Member, , NL
14:00
15:30
1.5
Alternative Energy and Distributed Propulsion Aircraft
2.5
Aircraft Design
3.5
Concept Design Methodology
4.5
High Lift Aerodynamics
5.5
Next Generation Commercial Transport Concept- Panel Session
6.5
Aircraft Structural Design I
7.5
Advanced Manufacturing
8.5
Acustics and Vibrations 2
9.5
Compressor Aerodynamics
10.5
Flight Modeling and Simulation
11.5
De-Icing
12.5
On Demand Mobility: Integration in Civil Airpace
15:30
16:00
Break
16:00
18:00
1.6
NATO Hybrid/Electric Initiative
2.6
Supersonic and Hypersonic Vehicles
3.6
Systems Engineering Cases
4.6
CFD Applications
5.6
Student Hands On Activities
6.6
New Structural Design 1: General
7.6
Optimization
8.6
Aeroelasticity 3: High Aspect Ratio Aircraft
9.6
MDO AGILE
10.6
Flight Trajectory Design
11.6
Electro Mechanical Actuation Systems
12.6
Air Transportation Efficiency
18:00
19:30
ICAS 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, , JP
Wednesday, 12. September 2018
RaumTrack 1Track 2Track 3Track 4Track 5Track 6Track 7Track 8Track 9Track 10Track 11Track 12
08:00
09:00
General lecture III - The Future of Propulsion, Dr. Ric Parker president ISABE - Chair: Sebastien Remy, , FR
09:00
09:30
Break
09:30
12:00
1.7
Design Method 1
2.7
Model Based System Engineering
3.7
Durability and Fatigue
4.7
Turbulence Modeling and LES
5.7
Wind Tunnel Systems Development
6.7
Complex Transition Phenomena
7.7
Propellors and Rotors
8.7
Aircraft Structural Design II
9.7
Fan and Propeller
10.7
Flight Control 1
11.7
UAS Control 2
12.7
Airport / TMA Procedures & Environmental Impact
12:00
13:00
Lunch
13:00
13:55
von 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: Dimitri Mavris, ICAS MRSC Chair, , US
14:00
15:30
1.8
Design Education 2
2.8
Maintenance Management
3.8
Structural Health Monitoring 1
4.8
Laminar Flow and Transition
5.8
Aerodynamic Experiments
6.8
Instability Control
7.8
Impact
8.8
Aeroelasticity 4 : General
9.8
High Speed Propulsion 1
10.8
Flight Dynamics & Identification 1
11.8
Air Data
12.8
Air Transportation Network
15:30
16:00
Break
16:00
18:00
1.9
Unconventional Concepts 2
2.9
Novel Application of MDO in Aircraft Design 3
3.9
Advanced Manufacturing and Non Destructive Testing
4.9
RANS Models
5.9
Optical Measurement Techniques
6.9
Buffet and Separation Control
7.9
High Speed Aerodynamics
8.9
Aeroelasticity 5 : General
9.9
High Speed Propulsion 2
10.9
Flight Dynamics & Identification 2
11.9
System Design
12.9
Human Factors
Thursday, 13. September 2018
RaumTrack 1Track 2Track 3Track 4Track 5Track 6Track 7Track 8Track 9Track 10Track 11Track 12
08:00
09:30
General 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: Joao L.F. Azevedo, PPSC Chair, , BR
09:30
10:00
Break
10:00
12:30
1.10
Design Method 2
2.10
Aircraft Operations 2
3.10
Crack and Impact Damage Propagation
4.10
Aerodynamic Optimization
5.10
History of Aeronautics
6.10
Student Final
7.10
Aircraft Aerodynamic Design
8.10
Aeroelasticity 6 : Controls
9.10
Hybrid-Electric Propulsion
10.10
Flight Control 2
11.10
UAS Flight Test
12.10
Operations - ATM (air traffic mamagement)
12:30
14:00
Lunch
14:00
15:30
1.11
Design History
2.11
Structural Health Monitoring 2
3.11
Physics Based Damage Modeling
4.11
Hypersonic Flow
5.11
tbd
6.11
High Speed Transition
7.11
New Structural Design 3: Material and Micro Structures
8.11
Structural Optimization
9.11
Personal Air Mobility
10.11
Control for Flexible Aircraft
11.11
UAS Navigation
12.11
Air Turbulence
15:30
16:00
Break
16:00
17:00
General Lecture IV - Dr. Charles Champion, Maurice Roy award winner - Aerospace in 2050 - Chair: Susan Ying, ICAS President, , US
17:00
17:30
Closing Ceremony
1.1Novel Application of MDO in Aircraft Design 1
Chair: B. Nagel
Track 1
01 - Aircraft Design and Integrated Systems
  10:30 11:00 1.1.1 CANCELED - STREAMLINING CROSS-ORGANIZATIONAL AIRCRAFT DEVELOPMENT PROCESSES: AN OVERVIEW OF THE AGILE PROJECT
P.D. Ciampa¹, B. Nagel¹; ¹DLR, Germany
  11:00 11:30 1.1.2 CANCELED - 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
  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: R. Gerhards
Track 2
01 - Aircraft Design and Integrated Systems
  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
  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
  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
3.1System of Systems Design
Chair: G. Holmberg
Track 3
02 - Systems Engineering and Integration
  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
  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
  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: P. Catalano
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  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
  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
  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: L. Manfriani
Track 5
03.2 - Experimental Aerodynamics
  10:30 11:00 5.1.1 EXPERIMENTAL INVESTIGATION OF WING LOAD CONTROL USING FLUIDIC DEVICES
A. Krzysiak, Institute of Aviation, Poland
  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. Linn¹, A.M. Awruch¹; ¹Federal University of Rio Grande do Sul, Brazil
  11:30 12:00 5.1.3 CANCELED - DEVELOPMENT OF NONLINEAR INSTABILITY IN SUPERSONIC 3D FLOW NEAR A PLATE
I.I. Lipatov, TsAGI, Russia
6.1Fundamental Fluid Dynamics 1
Chair: A. Cavalieri
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  10:30 11:00 6.1.1 DESTABILIZING EFFECT OF LONGITUDINAL WALL OSCILLATION ON OBLIQUE WAVES IN 2D CHANNEL FLOW
T. Atobe, JAXA, Japan
  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
  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: A. Volkova
Track 7
03.4 - Applied Aerodynamics
  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
  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
  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: O. Mello
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  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
  11:00 11:30 8.1.2 CANCELED - NUMERICAL SIMULATION ON THE FLOW-INDUCED VIBRATION CHARACTERISTIC OF MULTI-NOZZLE EJECTOR
Y.S. YANG, China Aerodynamics Research and Development Center, China
  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
9.1MDAO- multidisciplinary analysis and optimization
Chair: P. della Vecchia
Track 9
05 - Propulsion
  10:30 11:00 9.1.1 MULTI-DISCIPLINARY OPTIMISATION OF MEDIUM ALTITUDE LONG ENDURANCE UAVS
D. Verstraete, University of Sydney, Australia
  11:00 11:30 9.1.2 DYNAMIC MODEL FOR PLANETARY GEAR SETS OF GEARED TURBOFAN JET ENGINES
D. Kalinin¹, V. Golovanov¹, J. Temis, BMSTU, Russia; L. Magerramova¹; ¹CIAM, Russia
10.1FT & RC
Chair: Q. Wang
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  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
  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
  11:30 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: J. Bidinotto
Track 11
06.2 - Flight Dynamics and Control (UAV related)
  10:30 11:00 11.1.1 CANCELED - 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
  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
  11:30 12:00 11.1.3 CANCELED - COMPARATIVE ANALYSIS OF METHODS USED TO ACTIVE CONTROL OF MICRO AERIAL VEHICLE
K.-S Sibilski, Warsaw University of Technology, Poland
12.1Safety Analysis
Chair: S. Conway
Track 12
10 - Safety and Security
  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
  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
  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
1.2Novel Application of MDO in Aircraft Design 2
Chair: P.D. Ciampa
Track 1
01 - Aircraft Design and Integrated Systems
  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
  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
  14:00 14:30 1.2.3 INCLUDING AEROELASTIC TAILORING IN THE CONCEPTUAL DESIGN PROCESS OF A COMPOSITE STRUT BASED WING
D. Rajpal¹, R. De Breuker¹, H. Timmermans², W.F. Lammen², F. Torrigiani, German Aerospace Center, Germany; ¹Delft University of Technology, Netherlands ;²Netherlands Aerospace Centre, Netherlands
2.2UAS 2
Chair: F. Ogilvie
Track 2
01 - Aircraft Design and Integrated Systems
  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
  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
  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
3.2Modeling and Simulation in Manufacturing
Chair: H. Zhang
Track 3
08 - Manufacturing and Supply Chain Management
  13:00 13:30 3.2.1 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
  13:30 14:00 3.2.2 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
  14:00 14:30 3.2.3 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
4.2Unsteady Aerodynamics 2
Chair: A Da Ronch
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  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
  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
  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. Remy
Track 5
03.2 - Experimental Aerodynamics
  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
  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
  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: A. Cavalieri
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  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
  13:30 14:00 6.2.2 CANCELED - 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
  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: J. Monk
Track 7
03.4 - Applied Aerodynamics
  13:00 13:30 7.2.1 CANCELED - 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
  13:30 14:00 7.2.2 CANCELED - 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
  14:00 14:30 7.2.3 CANCELED - NUMERICAL FLOW ANALYSIS OF A CORRUGATED DRAGONFLY AIRFOIL AT LOW REYNOLDS NUMBER REGION USING CARTESIAN-MESH CFD
Y Yamaguchi, Japan
8.2New Structural Design 2: Morphing Structures
Chair: T. Ikeda
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  13:00 13:30 8.2.1 CANCELED - STRUCTURAL INTEGRITY DIAGNOSIS FOR AGING TRANSPORT AIRCRAFT BASED ON FLIGHT DATA
H. Wang, College of General Aviation, Wenzhou University, China
  13:30 14:00 8.2.2 APPLICATION RESEARCH OF ZIMMERMAN-WEISSENBURGER-YANG METHOD FOR PREDICTING FLUTTER BOUNDARY
Y. FEI, Shang Hai Aircraft Design and Research Institute of COMAC, China
  14:00 14:30 8.2.3 A RESEARCH OF MULTIDISCIPLINARY DESIGN OPTIMIZATION ALGORITHM FOR FIGHT VEHICLE DESIGN
X. Yan¹, Z. Liu¹, Y. Yang¹; ¹CARDC, China
9.2Combustion
Chair: P. Stezycki
Track 9
05 - Propulsion
  13:00 13:30 9.2.1 ENGINE TEST RESULTS OF FUEL-WATER MICROEMULSION
M. Kowalski¹, A. Jankowski¹; ¹AFIT, Poland
  13:30 14:00 9.2.2 PRECISE MEASUREMENT OF PROPAGATING FLAME IN 2-STROKE GASOLINE ENGINE BY MULTIPLE ION-PROBES
T. Yatsufusa¹, K. Kii¹, K. Takatani¹; ¹Hiroshima Institute of Technology, Japan
  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: J. Che
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  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
  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
  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:
Track 11
06.2 - Flight Dynamics and Control (UAV related)
  13:00 13:30 11.2.1 PERFORMANCE ANALYSIS OF UAV PERSISTENT SURVEILLANCE ALGORITHM
S. Lee¹, Y. Kim¹; ¹Seoul National University, South Korea
  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
  14:00 14:30 11.2.3 CANCELED - TOWARDS IMPLEMENTATION OF A FORMATION FLYING FOR EFFICIENT OPERATIONS
K.-S. Sibilski, Air Force Institute of Technology, Poland
12.2Cyber Security / Human Factors
Chair: A. Krein
Track 12
10 - Safety and Security
  13:00 13:30 12.2.1 3D PERSPECTIVE VIEWS ON IMMERSIVE HEAD-WORN DISPLAYS - CAN EXOCENTRIC VIEWS INCREASE PILOT SITUATIONAL AWARENESS?
J.M. Ernst, DLR, Germany
  13:30 14:00 12.2.2 HUMAN RELIABILITY ANALYSIS IN AN AIRCRAFT DECOMPRESSION EVENT
C. Reiser¹, A. Bayma¹, D.A. Fonseca¹; ¹Embraer S/A, Brazil
  14:00 14:30 12.2.3 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
1.3Design Education 1
Chair: K. Rinoie
Track 1
01 - Aircraft Design and Integrated Systems
  15:00 15:30 1.3.1 CANCELED - 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
  15:30 16:00 1.3.2 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
  16:00 16:30 1.3.3 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
2.3UAS 3
Chair: J. Melkert
Track 2
01 - Aircraft Design and Integrated Systems
  15:00 15:30 2.3.1 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
  15:30 16:00 2.3.2 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
  16:00 16:30 2.3.3 UAV INITIAL PARAMETER ESTIMATION
G.G. Silva¹, L.C. Carmona¹, E. Bauzer Medeiros¹; ¹UFMG, Brazil
3.3Additive Manufacturing
Chair: X. Zhou
Track 3
08 - Manufacturing and Supply Chain Management
  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
  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
  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: P- Greco Junior
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  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
  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
  16:00 16:30 4.3.3 CANCELED - LAUNCHER AERODYNAMIC ANALYSIS WITH PLUME EFFECTS
A. Viviani, University of Campania, Italy; G. Pezzella, Italian Aerospace Research Centre, Italy
5.3Wind Tunnel Test Technology
Chair: M. Guillaume
Track 5
03.2 - Experimental Aerodynamics
  15:00 15:30 5.3.1 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
  15:30 16:00 5.3.2 RLG BASED REAL-TIME MODEL ATTITUDE DETERMINATION SYSTEM DEVELOPMENT FOR LARGE LOW SPEED FACILITY OF CARDC
F. Litao¹, H. Zhiyuan¹, W. Zhigang¹; ¹CARDC, China
  16:00 16:30 5.3.3 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
6.3Loads
Chair: S.R. Conway
Track 6
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  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
  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
  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: F. Collier
Track 7
03.4 - Applied Aerodynamics
  15:00 15:30 7.3.1 THE STUDIES ON LOW-NOISE LAMINAR WING REGIONAL AIRCRAFT
N.A. Pushchin, TsAGI, Russia
  15:30 16:00 7.3.2 CANCELED - OPTIMIZATION DESIGN OF ADAPTIVE WING COUPLED AERODYNAMIC AND STRUCTURAL CONSTRAINTS
J Guan, China Aerodynamic Research and Development Center , China
  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: C. Chaves
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  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
  15:30 16:00 8.3.2 AEROELASTIC PROPERTIES OF ACTIVE WINGLETS
G.A. Amiryants¹, S.E. Paryshev¹, A.V. Grigoriev¹; ¹TsAGI, Russia
  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: P. Lourencao
Track 9
05 - Propulsion
  15:00 15:30 9.3.1 CANCELED - LOW-COST CERAMIC JET TURBINE
C.O. Oliveira, UFMG - ALFALAB, Brazil
  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
  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: Y. Fu
Track 10
07 - Systems, Subsystems and Equipment
  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
  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: C. Bil
Track 11
06.2 - Flight Dynamics and Control (UAV related)
  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
  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
  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: H. Toebben
Track 12
10 - Safety and Security
  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
  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
  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
1.4Unconventional Concepts 1
Chair: B. Kimmel
Track 1
01 - Aircraft Design and Integrated Systems
  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
  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
  11:00 11:30 1.4.3 EXPLORATION OF THE AIRBUS \"NAUTILIUS\" ENGINE INTEGRATION CONCEPT
L. Wiart, ONERA, France; C. Negulescu, AIRBUS, France
  11:30 12:00 1.4.4 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
2.4Next Generation Commercial Transport Concept
Chair: F. Collier
Track 2
01 - Aircraft Design and Integrated Systems
  10:00 10:30 2.4.1 BLENDED WING BODY TRANSPORT AIRCRAFT RESEARCH & DEVELOPMENT
J.T. Bonet, Boeing Research & Technology, United States
  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
  11:00 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
  11:30 12:00 2.4.4 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
3.4Systems Architecting
Chair: L. Marengo
Track 3
02 - Systems Engineering and Integration
  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
  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
  11:00 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
  11:30 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
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  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
  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
  11:00 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
5.4Unsteady Flows and Aeroacoustics
Chair: Y. Chen
Track 5
03.2 - Experimental Aerodynamics
  10:00 10:30 5.4.1 UNSTEADY AERODYNAMIC CHARACTERISTICS OF THE OSCILLATING AIRFOIL USING MSBS
Y.H. Sung¹, J.S. Han¹, J.H. Han¹; ¹KAIST, South Korea
  10:30 11:00 5.4.2 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
  11:00 11:30 5.4.3 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
  11:30 12:00 5.4.4 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
6.4Composites
Chair: M. Scott
Track 6
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  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
  10:30 11:00 6.4.2 DESIGNING PRIMARY STRUCTURES WITH STITCHED COMPOSITES
A. Velicki, The Boeing Company, United States
  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
  11:30 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: A. Cenko
Track 7
03.4 - Applied Aerodynamics
  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
  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
  11:00 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
  11:30 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: O. Mello
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  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
  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
  11:00 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
  11:30 12:00 8.4.4 CANCELED - AERODYNAMICS OPTIMIZATION DESIGN METHOD AND SHAPE PARAMETERIZATION
Z.Y Wang, The First Aircraft Institute, AVIC, China
9.4Engine Performance
Chair: S. Remy
Track 9
05 - Propulsion
  10:00 10:30 9.4.1 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
  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
  11:00 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
10.4Flight Testing
Chair: M. Naruoka
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  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
  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
  11:00 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
  11:30 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: R. Geister
Track 11
07 - Systems, Subsystems and Equipment
  10:00 10:30 11.4.1 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
  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
  11:00 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
  11:30 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: N. Tokuakid
Track 12
09 - Air Transport System Efficiency
  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
  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
  11:00 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
  11:30 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
1.5Alternative Energy and Distributed Propulsion Aircraft
Chair: Z. Goraj
Track 1
01 - Aircraft Design and Integrated Systems
  14:00 14:30 1.5.1 DEVELOPING THE UNMANNED UNCONVENTIONAL CARGO AIRPLANES WITH HYBRID PROPULSION SYSTEM
I. Gál¹, D. Rohács¹, J. Rohács¹; ¹Budapest University of Technology and Economics, Hungary
  14:30 15:00 1.5.2 OPTIMIZATION OF MOTOR FOR THE MAXIMIZATION OF SOLAR-POWERED AIRCRAFT PERFORMANCE
S. Serokhvostov, MIPT, Russia; T. Churkina, MAI, Russia
  15:00 15:30 1.5.3 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
2.5Aircraft Design
Chair: K. Rinoie
Track 2
01 - Aircraft Design and Integrated Systems
  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
  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
  15:00 15:30 2.5.3 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
3.5Concept Design Methodology
Chair: O. Pinon
Track 3
02 - Systems Engineering and Integration
  14:00 14:30 3.5.1 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
  14:30 15:00 3.5.2 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
  15:00 15:30 3.5.3 ROBUST DESIGN OPTIMIZATION OF BENCHMARK AERODYNAMIC CASE BASED ON POLYNOMIAL CHAOS EXPANSION
Z. Huan¹, G. Zhenghong¹; ¹Northwestern Polytechnical University , China
4.5High Lift Aerodynamics
Chair: L. Pedreiro
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  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
  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
  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: F. Collier
Track 5
14 - ECSC
6.5Aircraft Structural Design I
Chair: P. Krus
Track 6
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  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
  14:30 15:00 6.5.2 GLOBAL-LOCAL STRUCTURAL ANALYSIS OF COMPOSITE WINGS
E. Carrera¹, A. Pagani¹, G.H.C. Silva, Embraer S.A., Brazil; ¹Politecnico di Torino, Italy
  15:00 15:30 6.5.3 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
7.5Advanced Manufacturing
Chair: M. Zhu
Track 7
08 - Manufacturing and Supply Chain Management
  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
8.5Acustics and Vibrations 2
Chair: O. Mello
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  14:00 14:30 8.5.1 HIGH FREQUENCY MODAL TEST AND DYNAMIC PERFORMANCE EVALUATION OF TURBINE ROTOR BLADES
J. Qin¹, X. Gao¹, W.C. Huang¹, G. Yao¹; ¹ASRI, China
  14:30 15:00 8.5.2 HIGH PERFORMANCE PNEUMATIC SHOCK-ABSORBERS FOR AERONAUTICAL APPLICATIONS
R. Faraj, Institute of Fundamental Technological Research, Poland
9.5Compressor Aerodynamics
Chair: S. Pankov
Track 9
05 - Propulsion
  14:00 14:30 9.5.1 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
  14:30 15:00 9.5.2 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
  15:00 15:30 9.5.3 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
10.5Flight Modeling and Simulation
Chair: C. Doll
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  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
  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
  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: T. Dautermann
Track 11
07 - Systems, Subsystems and Equipment
  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
  14:30 15:00 11.5.2 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
  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
12.5On Demand Mobility: Integration in Civil Airpace
Chair: K. Kageyama
Track 12
09 - Air Transport System Efficiency
  14:00 14:30 12.5.1 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
  14:30 15:00 12.5.2 URBAN AIR TRANSPORTATION JOURNEY TIME COMPARISON FOR MELBOURNE METROPOLITAN AREA
L. Swadesir¹, C. Bil¹; ¹RMIT University, Australia
  15:00 15:30 12.5.3 ADAPTIVE LANDING SEQUENCING USING BIPARTITE GRAPHS AND PERFECT MATCHING
M. Hickson¹, C. Bil¹; ¹RMIT University, Australia
1.6NATO Hybrid/Electric Initiative
Chair: B. Nagel
Track 1
01 - Aircraft Design and Integrated Systems
  16:00 16:30 1.6.1 CANCELED - NATO RESEARCH TASK GROUP: HYBRID/ELECTRIC AIRCRAFT DESIGN AND STANDARDS FOR RESEARCH AND TECHNOLOGY (HEADSTART)
F. Grauer, Germany
  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
  17:00 17:30 1.6.3 CANCELED - KEY PERFORMANCE PARAMETERS FOR FUTURE NATO HYBRID/ELECTRIC MILITARY AIR VEHICLES
W. Dyson, National Aeronautics Space Administration (NASA), United States
  17:30 18:00 1.6.4 CANCELED - COORDINATING INTERNATIONAL RESEARCH AND DEVELOPMENT IN HYBRID/ELECTRIC FLIGHT
n/a Kloeckner, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany
2.6Supersonic and Hypersonic Vehicles
Chair: J. Melkert
Track 2
01 - Aircraft Design and Integrated Systems
  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
  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
  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
  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: J.C. Dunyach
Track 3
02 - Systems Engineering and Integration
  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
  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
  17:00 17:30 3.6.3 A 7D TRADE
D.K. Howarth, MEE Inc., United States
  17:30 18:00 3.6.4 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
4.6CFD Applications
Chair: L. Santos
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  16:00 16:30 4.6.1 CFD VERIFICATION AND VALIDATION FOR INDUSTRIAL APPLICATIONS
M. Mani¹, A. Cary¹; ¹Boeing, United States
  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
  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
  17:30 18:00 4.6.4 CANCELED - NUMERICAL SIMULATION OF OPERATING PROCESS ELEMENTS FOR COMBUSTION CHAMBERS OF PERSPECTIVE GTE
P.A. Semenev, Central Institute of Aviation Motors, Russia
Reserve Paper 4.6.R SIMULATION OF TRANSONIC FLOW OVER SPACE VEHICLE
N.V. Palchekovskaya, MIPT, Russia
5.6Student Hands On Activities
Chair: S. Suzuki
Track 5
14 - ECSC
  16:00 16:30 5.6.1 ALL JAPAN STUDENT\'S INDOOR FLYING ROBOT CONTEST
T. Tsuchiya, The University of Tokyo, Japan
  16:30 17:00 5.6.2 THE AERONAUTICAL SOCIETY OF SOUTH AFRICA AEROSPACE CHALLENGE
J.S. Monk, CSIR, South Africa
  17:00 17:30 5.6.3 CANCELED - SAE BRASIL AEROSPACE PROGRAMS – A SUCCESS STORY
H.A. Forjaz, SAEBRASIL, Brazil
6.6New Structural Design 1: General
Chair: T. Ikeda
Track 6
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  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
  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
  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
  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: K. Jamison
Track 7
03.4 - Applied Aerodynamics
  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
  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
  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
  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: C. Cesnik
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  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
  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
  17:00 17:30 8.6.3 CANCELED - NONLINEAR STATIC AEROELASTIC AND TRIM ANALYSIS OF HIGHLY FLEXIBLE AIRCRAFT
C. Zhang¹, Z. Zhou¹, P. Meng¹; ¹Northwestern Polytechnical University, China
  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: A. Mirzoyan
Track 9
05 - Propulsion
  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
  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
  17:00 17:30 9.6.3 CANCELED - COMMUNICATION BETWEEN PS AND AIRCRAFT SYSTEMS IN COLLECTIVE MDO SYSTEM IN AGILE PROJECT
P.D. Toktaliev, Central Institute of Aviation Motors, Russia
  17:30 18:00 9.6.4 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
10.6Flight Trajectory Design
Chair: S. Ueno
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  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
  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
  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
  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: J.C. Mare
Track 11
07 - Systems, Subsystems and Equipment
  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
  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
  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
  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: I. Tomoko
Track 12
09 - Air Transport System Efficiency
  16:00 16:30 12.6.1 CANCELED - DECISION-MAKING INFORMATION SYSTEM FOR MULTIMODAL DISRUPTION MANAGEMENT: SYSTEM ARCHITECTURE AND CONCEPT OF OPERATIONS
FJS Jiménez Serrano, Hamad International Airport (Qatar Airways), Qatar
  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
  17:00 17:30 12.6.3 CANCELED - AN ATC ORIENTED INTERFACE FOR MULTI-AIRCRAFT OPTIMISATION FOR CLIMBS AND DESCENTS
A. Spiteri, University of Malta, Malta
  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
1.7Design Method 1
Chair: S. Bagassi
Track 1
01 - Aircraft Design and Integrated Systems
  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
  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
  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
  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
  11:30 12:00 1.7.5 CANCELED - 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: L. Goes
Track 2
02 - Systems Engineering and Integration
  09:30 10:00 2.7.1 CANCELED - MBSE FLIGHT TESTING ARCHITECTURE RESEARCH
X. Hua, China; C. Qing, CFTE, China; S.J. Qi, cfte, China
  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
  10:30 11:00 2.7.3 A SYSML-BASED APPROACH TO EXPLORING INNOVATIVE SYSTEM IDEAS FOR AERONAUTICAL APPLICATIONS
J. Abulawi, HAW Hamburg, Germany
  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
  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: M. Poikelispää
Track 3
04.1 - Material Issues, Fatigue and Damage Tolerance
  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
  10:00 10:30 3.7.2 USING THE LEAD CRACK CONCEPT TO REDUCE DURABILITY TEST DURATION
L. Molent, DST, Australia
  10:30 11:00 3.7.3 CANCELED - INFLUENCE OF IRREGULAR LOADING PARAMETERS ON CFRP COMPONENTS FATIGUE LIFE
A.G. Kalinin, Central Aerohydrodynamic Institute, TsAGI, Russia
  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: J.L.F. Azevedo
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  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
  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
  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
  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
  11:30 12:00 4.7.5 A HYBRID LENGTH SCALE SIMILARITY SOLUTION FOR SWIRLING TURBULENT JETS
G. Andrews, Purdue University, United States
5.7Wind Tunnel Systems Development
Chair: M. Guillaume
Track 5
03.2 - Experimental Aerodynamics
  09:30 10:00 5.7.1 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
  10:00 10:30 5.7.2 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
  10:30 11:00 5.7.3 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
  11:00 11:30 5.7.4 CANCELED - 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
6.7Complex Transition Phenomena
Chair: L. Alves
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  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
  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
  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
  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
  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: J. Monk
Track 7
03.4 - Applied Aerodynamics
  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
  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
  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
  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
  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: T. Ireman
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  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
  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
  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
  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
  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: I. Yimer
Track 9
05 - Propulsion
  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
  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
  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
  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
  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: J. Vian
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  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
  10:00 10:30 10.7.2 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
  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
  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
  11:30 12:00 10.7.5 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
11.7UAS Control 2
Chair: C. Justin
Track 11
06.2 - Flight Dynamics and Control (UAV related)
  09:30 10:00 11.7.1 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
  10:00 10:30 11.7.2 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
  10:30 11:00 11.7.3 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
  11:00 11:30 11.7.4 ON WAKE VORTEX SAFETY ANALYSIS AND CONTROL FOR UAV
V. Golubev¹, P. Kazarin¹, C. Moreno¹, W. MacKunis¹; ¹ERAU, United States
  11:30 12:00 11.7.5 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
12.7Airport / TMA Procedures & Environmental Impact
Chair: J. Reichmuth
Track 12
09 - Air Transport System Efficiency
  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
  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
  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
  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
  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
1.8Design Education 2
Chair: P. della Vecchia
Track 1
01 - Aircraft Design and Integrated Systems
  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
  14:30 15:00 1.8.2 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: C. Chaves
Track 2
11 - Operations and Sustainment
  14:00 14:30 2.8.1 CANCELED - 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
  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
  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: T. Ikeda
Track 3
04.1 - Material Issues, Fatigue and Damage Tolerance
  14:00 14:30 3.8.1 CANCELED - 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
  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
  15:00 15:30 3.8.3 CANCELED - 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: L. Alves
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  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
  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
  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: E. Takara
Track 5
03.2 - Experimental Aerodynamics
  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
  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
  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
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  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
  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
  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
7.8Impact
Chair: J. Corman
Track 7
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  14:00 14:30 7.8.1 VERIFIED FUSELAGE SECTION WATER IMPACT MODELING
Y. Song¹, B. Harton¹, J. Bayandor¹; ¹CRashworthiness for Aerospace Structures and Hybrids (CRASH Lab), United States
  14:30 15:00 7.8.2 PREDICTING LOW-VELOCITY IMPACT DAMAGE IN COMPOSITE USING COHESIVE ELEMENT
H. Liu¹, S. Tan¹; ¹fai, China
  15:00 15:30 7.8.3 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
8.8Aeroelasticity 4 : General
Chair: G. Amiryants
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  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
  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
  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: N. Kukshinov
Track 9
05 - Propulsion
  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
  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
  15:00 15:30 9.8.3 CANCELED - 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: O. Korsun
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  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
  14:30 15:00 10.8.2 CANCELED - RECURSIVE AERODYNAMIC PARAMETER IDENTIFICATION OF A FIGHTER JET FLYING IN TURBULENT AIR
C. Grillo, Università di Palermo, Italy
  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: R. Sorbilli
Track 11
07 - Systems, Subsystems and Equipment
  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
  14:30 15:00 11.8.2 DESIGN CRITERIA OF A THERMAL MASS FLOW SENSOR FOR AIRCRAFT AIR DATA APPLICATIONS
L.C. Ribeiro¹, R.A. Souza¹, M.L. Oliveira¹, S.P.L. Vieira¹, W.O. Avelino, Labinfo Lab UFMG, Brazil; C.F.R. Oliveira¹, D.W. de Lima Monteiro¹, F.S. Torres¹, R.M.O. Hansen, University of Southern Denmark, Denmark; ¹UFMG, Brazil
  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
12.8Air Transportation Network
Chair: X. Zhang
Track 12
09 - Air Transport System Efficiency
  14:00 14:30 12.8.1 A SIMULATION MODELING STUDY FOR FREE ROUTING AIRSPACE IN JAPAN
K. Kageyama¹, Y. Nakamura¹; ¹ENRI, Japan
  14:30 15:00 12.8.2 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
  15:00 15:30 12.8.3 EULERIAN OPTIMAL CONTROL FORMULATION FOR DYNAMIC MORPHING OF AIRSPACE SECTORS
Y. Lim¹, N. Premlal¹, A. Gardi¹, R. Sabatini¹; ¹RMIT University, Australia
Reserve Paper 12.8.R STUDY ON LARGE-SCALE FLIGHT DELAY RECOVERY
Z. Zhang¹, J. Wang¹; ¹Civil Aviation University of China, China
1.9Unconventional Concepts 2
Chair: B. Kimmel
Track 1
01 - Aircraft Design and Integrated Systems
  16:00 16:30 1.9.1 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
  16:30 17:00 1.9.2 DEVELOPMENT OF THE REGENERATIVE SOARER: THEORETICAL AND PRACTICAL ASPECTS
R.C. Carvalho, EMBRAER S.A., Brazil
  17:00 17:30 1.9.3 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
  17:30 18:00 1.9.4 CANCELED - 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
2.9Novel Application of MDO in Aircraft Design 3
Chair: P. Shiva Prakasha
Track 2
01 - Aircraft Design and Integrated Systems
  16:00 16:30 2.9.1 STRUCTURAL DESIGN AND TESTING OF A TAILORED SKIN SINGLE DUCT (TSSD) FIN APPLICATION
M. Schneider¹, M. Horn¹, S. Ritt¹, A. Seitz¹; ¹DLR, Germany
  16:30 17:00 2.9.2 STUDIES ON THE APPLICATION OF MOEA/D TO AERODYNAMIC OPTIMIZATION DESIGN
X.Q. Zhu¹, Z.H Gao¹, Z.W. Chen¹; ¹Northwestern Polytechnical University, China
  17:00 17:30 2.9.3 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
  17:30 18:00 2.9.4 INTEGRATED SYSTEM FOR UNIFICATION OF AIRCRAFT CONCEPTUAL DESIGN APPLICATIONS
E. Vogiatzis¹, R. Chaitanya Munjulury¹, P. Krus¹; ¹Linköping University, Sweden
3.9Advanced Manufacturing and Non Destructive Testing
Chair: J. Jokinen
Track 3
04.1 - Material Issues, Fatigue and Damage Tolerance
  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
  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
  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
  17:30 18:00 3.9.4 CANCELED - NON-CONTACT MEASUREMENTS OF DEFORMATION OF LARGE-SIZED AIRCRAFT WING USING OPTICAL VIDEOGRAMMETRY METHOD
K.A. Kuruliuk, TsAGI, Russia
4.9RANS Models
Chair: C. Ilario
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  16:00 16:30 4.9.1 NUMERICAL INVESTIGATION OF FLOW STRUCTURE OF DIFFERENTIAL EJECTOR
H.Y. Zhang¹, Y.S. Yu¹, Q. Chen¹; ¹China Aerodynamics Research and Development Centre, China
  16:30 17:00 4.9.2 CANCELED - MULTIPHASE TURBULENCE MODELS FOR SCRAMJETS AND ABLATING WALLS
K.E.Son Son, Russia
  17:00 17:30 4.9.3 CANCELED - 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
  17:30 18:00 4.9.4 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
5.9Optical Measurement Techniques
Chair: E. Takara
Track 5
03.2 - Experimental Aerodynamics
  16:00 16:30 5.9.1 CANCELED - AN EXPERIMENT INVESTIGATION ON SHOCKINDUCED TURBULENT BOUNDARY LAYER SEPARATION FLOW-FIELD
W.H.-R. Ruan, China; X.J.-X. Xiang, China; G. Kang, China; X.J.-Z. Zhao, China; Q.-S. Shen, China
  16:30 17:00 5.9.2 PARTICLE IMAGE SURFACE FLOW VISUALIZATION AND SKIN-FRICTION MEASUREMENT
V. E. Mosharov¹, V. N. Radchenko¹, N. S. Tsipilev¹; ¹TsAGI, Russia
  17:00 17:30 5.9.3 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
  17:30 18:00 5.9.4 CANCELED - 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
6.9Buffet and Separation Control
Chair: S. Prince
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  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
  16:30 17:00 6.9.2 CONTROL OF STRONG SEPARATION OF FLOW VIA SIMULTANEOUS-BLOWING-SUCTION TECHNIQUE
W. Stalewski, INSTITUTE of AVIATION, Poland
  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
  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: R. Flatschart
Track 7
03.4 - Applied Aerodynamics
  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
  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
  17:00 17:30 7.9.3 HIGH SPEED DRAG REDUCTION OPTIMIZATION FOR PROJECTILES
T. Wan¹, H.-C. Chang¹, C.-M. Liu¹; ¹Tamkang University, China
  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: D. Djojodihardjo
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  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
  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
  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
  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: N. Kukshinov
Track 9
05 - Propulsion
  16:00 16:30 9.9.1 RESEARCH OF PROPULSION ENGINES FOR ADVANCE REUSABLE TSTO AEROSPACE SYSTEM
A.I. Lanshin¹, O.V. Sokolova¹, Yu.M. Shikhman¹, V.E. Shlyakotin¹; ¹CIAM, Russia
  16:30 17:00 9.9.2 CANCELED - CFD MODELLING TO OPTIMIZE THE MAXIMUM THRUST IN SCRAMJET ENGINE AND ANALYSIS OF ITS OPERATION PERFORMANCE
M-P Pires, IME, Brazil
  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
  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: C. Doll
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  16:00 16:30 10.9.1 CANCELED - BIO-DYNAMIC STABILITY ANALYSIS OF A GREBE DURING MIGRATION
J. Feaster¹, B. Gater, Virginia Tech, United States; L. Straker², L. Jehl², J. Bayandor¹; ¹CRashworthiness for Aerospace Structures and Hybrids (CRASH Lab), United States ;²U.S. National Museum of Natural Sciences, United States
  16:30 17:00 10.9.2 CANCELED - DYNAMIC REACTION OF AN AIRPLANE TO TRAILING VORTICES GENERATED BY ANOTHER AIRPLANE
G. Kowaleczko, Air Force Institute of Technology, Poland
  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
  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: M. Peters
Track 11
07 - Systems, Subsystems and Equipment
  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
  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
  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
  17:30 18:00 11.9.4 CANCELED - 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: M. Consiglio
Track 12
10 - Safety and Security
  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
  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
  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
  17:30 18:00 12.9.4 CREW TRAINING USING ANIMATION
P.M. Razaboni, Embraer SA, Brazil
1.10Design Method 2
Chair: K. Rinoie
Track 1
01 - Aircraft Design and Integrated Systems
  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
  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
  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
  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
  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
Track 2
11 - Operations and Sustainment
  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
  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
  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
  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
  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: J. Jokinen
Track 3
04.1 - Material Issues, Fatigue and Damage Tolerance
  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
  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
  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
  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
  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: H. Hoeijmakers
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  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
  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
  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
  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
  12:00 12:30 4.10.5 CANCELED - DESIGN SPACE EXPLORATION AND FLOW CONTROL FOR A TRANSONIC WING DRAG REDUCTION
Y UTAMA, INSTITUT TEKNOLOGI BANDUNG, Indonesia
5.10History of Aeronautics
Chair: M. Lott
Track 5
12 - Host nation
  10:00 10:30 5.10.1 THE SANTOS-DUMONT LEGACY TO AERONAUTICS
M. Pazini Brandão, Technological Institute of Aeronautics, Brazil
  10:30 11:00 5.10.2 BRAZILIAN AVIATION HISTORY: THE UNIVERSITY OF SÃO PAULO CASE
F.M. Catalano, University of São Paulo -EESC-USP, Brazil
  11:00 11:30 5.10.3 HISTORY OF AVIATION IN MINAS GERAIS
E. Bauzer Medeiros, Brazil
  11:30 12:00 5.10.4 THE STUDY OF TURBORAMJETS IN CIAM
M. Tskhovrebov¹, V. Solonin¹, V. Palkin¹, P. Kadjardouzov¹; ¹CIAM, Russia
  12:00 12:30 5.10.5 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
6.10Student Final
Chair: K. Rein Weston
Track 6
15 - Guest lectures
7.10Aircraft Aerodynamic Design
Chair: S. Sartorius
Track 7
03.4 - Applied Aerodynamics
  10:00 10:30 7.10.1 CONCEPT OF MEDIUM TWIN-ENGINE STOL TRANSPORT AIRPLANE
O. Pavlenko¹, A. Petrov¹, E. Pigusov¹; ¹TsAGI, Russia
  10:30 11:00 7.10.2 CANCELED - 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
  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
  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
  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: F. Daoud
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  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
  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
  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
  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
  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: A. Isikveren
Track 9
05 - Propulsion
  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
  10:30 11:00 9.10.2 PROPELLER OPTIMISATION FOR AN ELECTRICAL-POWERED TACTICAL UAS
R. MacNeill, The University of Sydney, Australia
  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
  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
  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: J. Che
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  10:00 10:30 10.10.1 EVALUATION OF ALTITUDE CONTROL FOR AN AIRBREATHING HYPERSONIC AIRCRAFT MODEL
Masaharu Hiruma, The University of Tokyo, Japan
  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
  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
  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
  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 Flight Test
Chair: I. Staack
Track 11
06.2 - Flight Dynamics and Control (UAV related)
  10:00 10:30 11.10.1 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
  10:30 11:00 11.10.2 VERTICAL LANDING OF A FIXED-WING UAV USING THE FLAT SPIN
S. Higashino, Kyushu University, Japan; K. Nakama, Kyushu University, Graduate Student, Japan
  11:00 11:30 11.10.3 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
  11:30 12:00 11.10.4 SAFETY FLIGHT TESTING FOR CARGO UAV DEVELOPMENT
Kakuya Iwata¹, Keisuke Yamada¹, Ryuzo Horiuchi¹, Akiya Kamimura¹; ¹National Institute of Advanced Industrial Science and Technology, Japan
  12:00 12:30 11.10.5 CANCELED - ON BOARD SLAM FOR INDOOR MAV USING A LASER RANGE FINDER
K.-S. Sibilski, Air Force Institute of Technology, Poland
12.10Operations - ATM (air traffic mamagement)
Chair: J. Melkert
Track 12
10 - Safety and Security
  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
  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
  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
  11:30 12:00 12.10.4 CANCELED - AIRCRAFT KEY PARTS INTELLIGENT FAULT DIAGNOSIS USING GAUSSIAN DEEP BELIEF NETWORK
H.D. Shao, School of Aeronautics, Northwestern Polytechnical University, China
  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
1.11Design History
Chair: J. Melkert
Track 1
01 - Aircraft Design and Integrated Systems
  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
  14:30 15:00 1.11.2 THE NUMERICAL HISTORY OF AIRPLANE MANUFACTURING IN XX CENTURY
Y.V. Kuzmin, TsAGI, Russia
  15:00 15:30 1.11.3 CANCELED - 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: P. Anchieta da Silva
Track 2
11 - Operations and Sustainment
  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
  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
  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: A. Blom
Track 3
04.1 - Material Issues, Fatigue and Damage Tolerance
  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
  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
  15:00 15:30 3.11.3 IMPORTANCE OF SECONDARY BENDING EVALUATION IN STRUCTURAL JOINT
W.R.P. Mendonça, EMBRAER S.A., Brazil
4.11Hypersonic Flow
Chair: L. Alves
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  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
  14:30 15:00 4.11.2 LONGITUDINAL STABILITY DESIGN CRITERIA FOR HYPERSONIC GLIDERS
B.Y. Chen, China Academy of Aerospace Aerodynamics, China
  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
5.11tbd
Chair:
Track 5
6.11High Speed Transition
Chair: C. Atkin
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  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
  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
  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: M. Guillaume
Track 7
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  14:00 14:30 7.11.1 CANCELED - METHOD FOR FLEXIBLE SKELETON COMPOSED OF THE TYPE OF INCIRCLE ELEMENT BASED ON EQUAL DISPLACEMENT AND ITS APPLICATION
Y.-C. Deng, SADRI, China
  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
  15:00 15:30 7.11.3 CANCELED - ON ELASTIC PSEUDO-ISOTROPIC ORTHOTROPIC PLATES
L.M.B.C. Campos, Instituto Superior Tecnico, Portugal
8.11Structural Optimization
Chair: B. Fredriksson
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  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
  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
  15:00 15:30 8.11.3 CANCELED - 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
9.11Personal Air Mobility
Chair: Z. Goraj
Track 9
01 - Aircraft Design and Integrated Systems
  14:00 14:30 9.11.1 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
  14:30 15:00 9.11.2 INVESTIGATION OF ‘JUMP TAKEOFF’ POSSIBILITY FOR THE NEW CONCEPT OF MODERN AUTOGYRO
R. Zurawski¹, D. Ulma¹; ¹Institute of Aviation, Poland
  15:00 15:30 9.11.3 A PERFORMANCE BENCHMARK OF RECENT PERSONAL AIR VEHICLE CONCEPTS FOR URBAN AIR MOBILITY
M. Shamiyeh¹, R. Rothfeld¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
10.11Control for Flexible Aircraft
Chair: S. Ueno
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  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
  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
  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 SENSORS
M.A.V. Morales¹, F.J. Silvestre¹, A.B. Guimarães Neto¹, G. Tissot, Université Paul Sabatier, France; ¹Instituto Tecnológico de Aeronáutica, Brazil
11.11UAS Navigation
Chair: P. Greco Jr.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
  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
  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
  15:00 15:30 11.11.3 CANCELED - SIMULTANEOUS LOCALIZATION AND MAPPING WITH OBJECT DETECTION FOR UAV APPLICATONS
T. Shim, KAIST, South Korea
12.11Air Turbulence
Chair: N. Moscati
Track 12
10 - Safety and Security
  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
  14:30 15:00 12.11.2 CANCELED - HAZARDOUS MITIGATION FOR TRANSPORT AIRCRAFT IN SEVERE ATMOSPHERIC TURBULENCE BASED ON IMPROVED CONTROL STRATEGY
C. Chang, College of General Aviation, Wenzhou University, China
  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