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 Perreira, 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
Hybrid-Electric Propulsion
10.1
FT & RC
11.1
UAS Navigation
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
Concept Design Methodology
4.2
Unsteady Aerodynamics 2
5.2
Aerodynamic Effects of Propulsion Integration
6.2
Fundamental Fluid Dynamics 2
7.2
Unmanned Aircraft
8.2
Acustics and Vibrations 2
9.2
Combustion
10.2
Flight Handling Quality
11.2
UAS Trajectory
12.2
Cyber Security
14:30
15:00
Break
15:00
16:30
1.3
Novel Application of MDO in Aircraft Design 3
2.3
Personal Air Mobility
3.3
Additive Manufacturing
4.3
Numerical Methods
5.3
Student Hands On Activities
6.3
Loads
7.3
Aeroacoustics and Icing
8.3
Aeroelasticity 3 : 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, Dr. M.Evans, Dr. B.Yutko, Mr. Y.Nakagawa, Mr. Vargas Rainho - Chair: S. 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
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
Wind Tunnel Systems Development
6.4
Composites
7.4
Store Separation
8.4
New Structural Design 1: General
9.4
Engine Performance
10.4
Control for Flexible Aircraft
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
14:00
15:30
1.5
Design Education 1
2.5
Aircraft Design
3.5
Desktop Simulations
4.5
High Lift Aerodynamics
5.5
Advanced Transport Aircraft Concepts for Environmentally responsible Aviation
6.5
Aircraft Structural Design I
7.5
Advanced Manufacturing
8.5
Impact
9.5
MDO-1
10.5
Flight Modeling and Simulation
11.5
De-Icing
12.5
Air Transportation Network
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
Wind Tunnel Test Technology
6.6
Aircraft Structural Design II
7.6
Optimization
8.6
Aeroelasticity 4: High Aspect Ratio Aircraft
9.6
MDO-2 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: E. Itoh, , 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 - Future of Propulsion, Dr. Ric Parker president ISABE, Dr. Frank Anton AIRBUS industries - Chair: D. Müller-Wiesner, , DE
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
Unsteady Flows and Aeroacoustics
6.7
Complex Transition Phenomena
7.7
Aircraft Aerodynamic Design
8.7
Aeroelasticity 1 : Methods and Modeling
9.7
Fan and Propeller
10.7
Flight Control 1
11.7
UAS Flight Test
12.7
Airport / TMA Procedures & Environmental Impact
12:00
13:00
Lunch
13:00
13:45
General Lecture IV - Developing and flying the Gripen E - M. Wandt, SAAB, Sweden
14:00
15:30
1.8
Design Education 2
2.8
Maintenance Management
3.8
Physics Based Damage Modeling
4.8
Laminar Flow and Transition
5.8
Aerodynamic Experiments
6.8
Instability Control
7.8
New Structural Design 2: Morphing Structures
8.8
Aeroelasticity 6 : General
9.8
High Speed Propulsion 1
10.8
Flight Dynamics & Identification 1
11.8
Air Data
12.8
On Demand Mobility: Integration in Civil Airpace
15:30
16:00
Break
16:00
18:00
1.9
Unconventional Concepts 2
2.9
Alternative Energy and Distributed Propulsion Aircraft
3.9
Advanced Manufacturing and Non Destructive Testing
4.9
Hypersonic Flow
5.9
History of Aeronautics
6.9
Buffet and Separation Control
7.9
Propellors and Rotors
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. Fumikazu Itoh ONERA-Bruno Saijon DLR-Prof. Rolf Henke NLR-Michel Peters
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
Optical Measurement Techniques
6.10
Student Final
7.10
High Speed Aerodynamics
8.10
Aeroelasticity 2 : Controls
9.10
Compressor Aerodynamics
10.10
Flight Control 2
11.10
UAS Control 1
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
Structural Health Monitoring 1
4.11
RANS Models
5.11
Modeling and Simulation in Manufacturing
6.11
High Speed Transition
7.11
New Structural Design 3: Material and Micro Structures
8.11
Structural Optimization
9.11
ISABE
10.11
Flight Testing
11.11
UAS Control 2
12.11
Air Turbulence
15:30
16:00
Break
16:00
17:00
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: Shinji Suzuki, Chair ICAS Programme Committee, JP
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 COLLABORATIVE , MULTI-NATIONAL MDO OF CIVIL AIRCRAFT : AGILE EU PROJECT
P S Shiva Prakasha, German Aerospace Center, Germany
  11:00 11:30 1.1.2 MULTIDISCIPLINARY DESIGN OPTIMIZATION OF BLENDED WING BODY AIRCRAFT THROUGH COLLABORATIVE DESIGN - AGILE EU PROJECT
P S Shivaprakasha, German Aerospace Center, Germany
  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 DESIGN OPTIMIZATION OF UNMANNED AIRCRAFT IN A SYSTEM OF SYSTEMS CONTEXT
A. Papageorgiou¹, K. Amadori², C. Jouannet², J. Ölvander¹; ¹Linköping University, Sweden ;²SAAB Aeronautics, Sweden
  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
Philipp Stahl¹, Thomas Seren¹, Christian Rößler¹, Mirko Hornung¹; ¹Technical University of Munich, Germany
Reserve Paper 2.1.R RESEARCH ON DESIGN METHOD OF PETROL-ELECTRIC HYBRID DRIVE SYSTEM BASED ON MDO FOR A NOVEL VTOVL UAV
YAO Z.X., China
3.1System of Systems Design
Chair: 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 SYSTEM
D. Mavris, 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. Terrapon¹; ¹University of Liège, Belgium
  11:00 11:30 4.1.2 FEASIBILITY OF NAVIER-STOKES HARMONIC BALANCE METHOD FOR MODELLING UNSTEADY AERODYNAMICS
J. Drofelnik¹, A. Da Ronch¹, M.S. Campobasso, University of Lancaster, United Kingdom; ¹University of Southampton, United Kingdom
  11:30 12:00 4.1.3 COMPUTATIONAL AND EXPERIMENTAL UNSTEADY PRESSURE DISTRIBUTIONS OF WING OSCILLATING IN PITCH
G.R. Begnini, Embraer S.A., Brazil
Reserve Paper 4.1.R LATTICE-BOLTZMANN SIMULATIONS OF THE OSCILLATING BENCHMARK SUPERCRITICAL WING
F. P. Ribeiro, Exa GmbH, Germany
5.1Experiments in Flow Control
Chair: L. Manfriani
Track 5
03.2 - Experimental Aerodynamics
  10:30 11:00 5.1.1 EXPERIMENTAL STUDY OF SYNTHETIC JET ACTUATOR FLOW CONTROL ON A NACA0015
N.D. Martin, Northumbria University, United Kingdom
  11:00 11:30 5.1.2 EXPERIMENTAL INVESTIGATION OF WING LOAD CONTROL USING FLUIDIC DEVICES
Andrzej Krzysiak, Institute of Aviation, Poland
  11:30 12:00 5.1.3 EXPERIMENTAL STUDY OF TRANSONIC FLOW OVER AN AIRFOIL ON LAMINAR FLOW AND LEADING EDGE TUBERCLES
R.G. Annes da Silva, ITA, Brazil
6.1Fundamental Fluid Dynamics 1
Chair: 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
  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 CONTINUOUS TANGENTIAL JET
Y. LEE, Agency for Defense Development, South Korea
8.1Acustics and Vibrations 1
Chair: L. Sanches
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 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
Reserve Paper 8.1.R HIGH PERFORMANCE PNEUMATIC SHOCK-ABSORBERS FOR AERONAUTICAL APPLICATIONS
Rami Faraj, Institute of Fundamental Technological Research, Poland
9.1Hybrid-Electric Propulsion
Chair: A. Isikveren
Track 9
05 - Propulsion
  10:30 11:00 9.1.1 DEVELOPMENT OF HYBRID GASOLINE-BATTERY PROPULSION SYSTEM FOR MULTI-COPTER PLATFORM
Hyuk Rok Gwon¹, Woo Bee Kim¹, Ki Woong Lee¹, Dae Won KIm¹, Hyeon Seok Lee¹; ¹Korean Air, South Korea
  11:00 11:30 9.1.2 PROPELLER OPTIMISATION FOR AN ELECTRICAL-POWERED TACTICAL UAV
Rens MacNeill, The University of Sydney, Australia
  11:30 12:00 9.1.3 DESIGN AND OFF-DESIGN PERFORMANCE OF ELECTRIC SYSTEM ARCHITECTURES FOR ELECTRIC POWERED AIRCRAFT
P.C. Vratny¹, F. Troeltsch¹, J. Bijewitz¹, J. Kaiser¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
Reserve Paper 9.1.R SYSTEM ANALYSIS OF TURBO ELECTRIC AND HYBRID PROPULSION SYSTEMS ON A REGIONAL AIRCRAFT
H. Gesell¹, F. Wolters¹, M. Plohr¹; ¹DLR, Germany
10.1FT & RC
Chair: Q. Wang
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  10:30 11:00 10.1.1 NEURAL NETWORK-BASED FAULT TOLERANT CONTROL FOR AIRCRAFT
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
11.1UAS Navigation
Chair: P. Greco Jr.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
  10:30 11:00 11.1.1 MODIFIED COMPOSITE GUIDANCE LAW AGAINST MOVING TARGET CONSIDERING NARROW FIELD-OF-VIEW LIMIT
Seokwon Lee¹, Sungjun Ann¹, Youdan Kim¹; ¹Seoul National University, South Korea
  11:00 11:30 11.1.2 AUTONOMOUS FLIGHT OF UNMANNED MULTICOPTER USING SUPER WIDE-ANGLE STEREO VISION SYSTEM
T. Yamashita¹, Y. Kajiwara¹, C.T. Raabe², T. Tsuchiya², S. Suzuki²; ¹Ricoh Co. Ltd, Japan ;²the University of Tokyo, Japan
  11:30 12:00 11.1.3 SIMULTANEOUS LOCALIZATION AND MAPPING WITH OBJECT DETECTION FOR UAV APPLICATONS
T. Shim, KAIST, South Korea
Reserve Paper 11.1.R ON BOARD SLAM FOR INDOOR MAV USING A LASER RANGE FINDER
K.-S. Sibilski, Air Force Institute of Technology, Poland
12.1Safety Analysis
Chair: S. Conway
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
Kun Chen¹, Yibing Wu¹, Tianchun 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, P.D. Ciampa¹; ¹German Aerospace Center, DLR, Germany
  13:30 14:00 1.2.2 MDO APPLICATIONS TO CONVENTIONAL AND NOVEL TURBOPROP AIRCRAFTS WITHIN AGILE EUROPEAN PROJECT
P. Della Vecchia, University of Naples Federico II, Italy
  14:00 14:30 1.2.3 INCLUDING AEROELASTIC TAILORING IN THE CONCEPTUAL DESIGN PROCESS OF A COMPOSITE STRUT BASED WING
D Rajpal, Delft University of Technology, Netherlands
2.2UAS 2
Chair: 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 UAVS FOR HUMANITARIAN RELIEF MISSIONS
O Hektor¹, Dr. 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
L. D. Jesus¹, M.S. Sousa¹, E.H. Shiguemori, IEAv, Brazil; S. Serokhvostov, MIPT, Russia; P.K. Gupta, JUIT, India; L. Zhong, CAUC, China; A. C. B. Ramos, Unifei, Brazil; ¹UNIFEI, Brazil
Reserve Paper 2.2.R UAV INITIAL PARAMETER ESTIMATION
Lucas Campos Carmona¹, Eduardo Bauzer Medeiros¹, Gabriel George Silva¹; ¹UFMG, Brazil
3.2Concept Design Methodology
Chair: D. Mavris
Track 3
02 - Systems Engineering and Integration
  13:00 13:30 3.2.1 COMBINED AIRFRAME AND SUBSYSTEMS EVOLVABILITY EXPLORATION DURING CONCEPTUAL DESIGN
A.S.J. van Heerden, United Kingdom
  13:30 14:00 3.2.2 A TECHNIQUE FOR CAPTURING STAKEHOLDER PREFERENCES AND KNOWLEDGE IN EARLY DESIGN STUDIES
S. Sartorius, United States; M. Hornung, Technical University of Munich Institute of Aircraft Design, Germany
  14:00 14:30 3.2.3 METHODOLOGY FOR THE DEVELOPMENT OF FUTURE AIRLINER PASSENGER CABINS FOR THE ASIAN MARKET
R. Kirenskis, Cranfield University, United Kingdom
4.2Unsteady Aerodynamics 2
Chair: 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, F. Silvestre¹, K. Ramesh, Glasgow University, United Kingdom; ¹Instituto Tecnologico de Aeronautica, Brazil
  13:30 14:00 4.2.2 NUMERICAL ANALYSIS OF THE FLOW AROUND A BACKWARD-FACING RAMP
A. Mastellone¹, M. Invigorito¹, F. Capuano, Università di Napoli Federico II, Italy; ¹CIRA, Italy
  14:00 14:30 4.2.3 RECTANGULAR CAVITY FLOWFIELD EFFECTS ON STORES IN THE SHEAR LAYER
Alexis Cenko, AIWS, United States; Graham Akroyd, Akroyd Aeronautics, Australia
5.2Aerodynamic Effects of Propulsion Integration
Chair: W. Xumian
Track 5
03.2 - Experimental Aerodynamics
  13:00 13:30 5.2.1 THE AERODYNAMIC PERFORMANCE MEASUREMENT OF RIGID COAXIAL ROTOR WING IN HOVER
X. Zhao¹, N.-Z. Huang¹, X. Liang¹, P. Zhou¹, Y.-F. Lin, China Helicopter Research and Development Institute, China; ¹Northwestern Polytechnical University, China
  13:30 14:00 5.2.2 ADAPTIVE WING HIGH-LIFT SYSTEM
V.V. Gubskiy¹, A.V. Petrov¹, A.V. Potapchik¹, Yu.G. Stepanov¹; ¹TsAGI, Russia
  14:00 14:30 5.2.3 INSTALLATION EFFECTS ON THE AERODYNAMICS AND AEROACOUSTICS OF A PYLON AND A PUSHER PROPELLER
L. Rego, University of São Paulo, Brazil
Reserve Paper 5.2.R EXPERIMENTAL RESEARCH AND NUMERICAL ANALYSIS OF COLD AND HOT-JET SIMULATION OF TRUST VECTOR CONTROL BY JET TABS
G. Ocokoljic, Military Technical Institute, Belgrade, Serbia
6.2Fundamental Fluid Dynamics 2
Chair: A. Cavalieri
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  13:00 13:30 6.2.1 ACOUSTIC MODES IN JETS AND WAKES AND THEIR ROLE IN ABSOLUTE INSTABILITY
A. Cavalieri, ITA, Brazil; P. Jordan, Universite de Poitiers , France
  13:30 14:00 6.2.2 LONGITUDINAL VORTEXE FORMATION IN THE HYPERSONIC FLOW AROUND WINDWARD SIDE OF BLUNTED DELTA WING AND EFFECTS OF THEIR IN
V.I. Shalaev, MIPT, Russia; S.V. Alexandrov¹, A.V. Vaganov¹, S.M. Starodubtsev¹; ¹TsAGI, Russia
  14:00 14:30 6.2.3 ON THE EXISTENCE OF MULTIPLE SELF-EXCITATION FREQUENCIES IN THE INSTABILITY OF INTERACTING PLANAR MIXING LAYER AND WAKE
H. R. De Aguiar Quintanilha Junior, University of Liverpool, United Kingdom; L. Santos de Brito Alves, Universidade Federal Fluminense, Brazil
7.2Unmanned Aircraft
Chair: B. Yutko
Track 7
03.4 - Applied Aerodynamics
  13:00 13:30 7.2.1 STUDY ON SMALL UAVS\' DEEP STALL LANDING PROCEDURE
Bochao Cheng¹, Zheng Guo¹, Peng Wang¹, Qingyang Chen¹, Bochao Cheng, No.32021 Troops of PLA, China; ¹National University of Defense Technology, China
  13:30 14:00 7.2.2 AERODYNAMIC ANALYSIS OF A LOW-SPEED UNMANNED AERIAL VEHICLE IN FULL CONFIGURATION BASED TRANSITION MODEL
Li-li Chen¹, Zheng Guo¹, Zhong-xi Hou¹, Wen-kai Wang¹, Bing-jie Zhu¹; ¹National University of Defense Technology, China
  14:00 14:30 7.2.3 AEROELASTIC ANALYSIS OF INSECT-LIKE FLAPPING WING USING MODIFIED IMPLICIT COUPLING METHOD
N. Lee, Inha University, South Korea
Reserve Paper 7.2.R NUMERICAL FLOW ANALYSIS OF A CORRUGATED DRAGONFLY AIRFOIL AT LOW REYNOLDS NUMBER REGION USING CARTESIAN-MESH CFD
Y Yamaguchi, Japan
8.2Acustics and Vibrations 2
Chair: F. Nitzsche
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  13:00 13:30 8.2.1 THE DIMENSIONING OF A NONLINEAR ENERGY SINK APPLIED TO A HELICOPTER THROUGH NONLINEAR NORMAL MODES
L. V. D. Sousa, Federal University of Uberlândia, Brazil
  13:30 14:00 8.2.2 CLOSED-LOOP CONTROL OF THE SMART SPRING – EFFECT OF THE CONTROL ALGORITHM ON THE DYNAMIC RESPONSE OF PERIODIC SYSTEMS
F. Nitzsche, Carleton University, Canada
  14:00 14:30 8.2.3 INVESTIGATION ON HIGH-FREQUENCY MODAL TEST AND ANALYSIS FOR TURING BLADE
G-X Gao Xiang¹, Y-Q YAN QUN¹, H-WC HUANG Wenchao¹, YG YAO Gang¹; ¹ASRI, China
9.2Combustion
Chair: 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
Tomoaki Yatsufusa¹, Keigo Kii¹, Kentaro 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.K. Kowalski¹, A.J. Jankowski¹, R.S. 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 INFLUENCE OF BIODYNAMIC FEEDTHROUGH ON HANDLING QUALITIES ANALYSIS
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
E. Dillinger, ISAE-SUPAERO/ONERA, France; C. Döll¹, R. Liaboeuf¹, C. Toussaint¹, J. Hermetz¹, C. Verbeke¹, M. Ridel¹; ¹ONERA, France
11.2UAS Trajectory
Chair: K. Sibilski
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 TOWARDS IMPLEMENTATION OF A FORMATION FLYING FOR EFFICIENT OPERATIONS
K.-S. Sibilski, Air Force Institute of Technology, Poland
12.2Cyber Security
Chair:
Track 12
10 - Safety and Security
  13:00 13:30 12.2.1 IN-SERVICE AIRCRAFT CYBERSECURITY RISK ASSESSMENT
G.C.B. Bertoli, Brazil
  13:30 14:00 12.2.2 IMPACT STUDY ON CYBER THREATS TO GNSS AND FMS SYSTEMS
R. Geister¹, J.-P. Buch¹, D. Niedermeier¹, G. Gamba², L. Canzian², O. Pozzobon²; ¹German Aerospace Center, Germany ;²Qascom S.r.l., Italy
  14:00 14:30 12.2.3 A METHOD TO DESIGN CYBER-PHYSICAL RESILIENT ARCHITECTURES
ET YANO, ITA, Brazil
1.3Novel Application of MDO in Aircraft Design 3
Chair: T. Lefebvre
Track 1
01 - Aircraft Design and Integrated Systems
  15:00 15:30 1.3.1 INTERGRATED SYSTEM FOR UNIFICATION OF AIRCRAFT CONCEPTUAL DESIGN APPLICATIONS.
E. Vogiatzis¹, R. -C. Munjulury¹, P. Krus¹; ¹Linköpings university, Sweden
  15:30 16:00 1.3.2 STRUCTURAL DESIGN AND TESTING OF A TAILORED SKIN SINGLE DUCT (TSSD) FIN APPLICATION
M. Schneider¹, M. Horn¹, S. Ritt¹, A. Seitz¹; ¹DLR, Germany
  16:00 16:30 1.3.3 AIRCRAFT OPTIMIZATION AT THE EARLY STAGES OF DESIGN WITH A HYBRID TECHNIQUE
N Cavus, German Aerospace Center, Germany
Reserve Paper 1.3.R STUDIES ON THE APPLICATION OF MOEA/D TO AERODYNAMIC OPTIMIZATION DESIGN
X.Q. Zhu¹, Z.H Gao¹, Z.W. Chen¹; ¹Northwestern Polytechnical University, China
2.3Personal Air Mobility
Chair: J. Melkert
Track 2
01 - Aircraft Design and Integrated Systems
  15:00 15:30 2.3.1 SMALL AIRCRAFT CONCEPT FOR REGIONAL ON-DEMAND AIR MOBILITY
E. Stumpf¹, M. Kreimeier¹, P. Strathoff¹, J. Lückhof¹, K.-U. Schröder, RWTH Aachen University, Institute of Structural Mechanics and Li, Germany; F. Janser, University of Applied Sciences Aachen, Aerodynamics Group, Germany; ¹RWTH Aachen University, Institute of Aerospace Systems, Germany
  15:30 16:00 2.3.2 INVESTIGATION OF ‘JUMP TAKEOFF’ POSSIBILITY FOR THE NEW CONCEPT OF MODERN AUTOGYRO
D. Ulma¹, R. Zurawski¹; ¹Institute of Aviation, Poland
3.3Additive Manufacturing
Chair: X. Zhou
Track 3
08 - Manufacturing and Supply Chain Management
  15:00 15:30 3.3.1 AIRCRAFT STRCTURE TECHNOLONY OF ADDITIVE MANUFACTURING
Xiangming Wang¹, Hao Cui¹, Ping Xu¹, Shiquan Bi¹; ¹Shenyang Aircraft Design and Resesarch Institute, China
  15:30 16:00 3.3.2 INVESTIGATION OF CRACK PROPAGATION PROPERTIES OF ADDITIVE MANUFACTURING PRODUCTS
N. Broitman¹, A. Shirizly¹; ¹Technion, I.I.T., Israel
  16:00 16:30 3.3.3 EVALUATION OF MECHANICAL PROPERTIES OF TI6AL4V FABRICATED BY SELECTIVE LASER MELTING (SLM)
MingQiang Chu¹, XiaoWei Zhou¹, XiaoFeng Sun¹, Lei Wang¹; ¹COMAC, China
4.3Numerical Methods
Chair: L. Tobaldini Neto
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  15:00 15:30 4.3.1 EFFECTS OF NUMERICAL MODELING CHOICES FOR JETS IN CROSSFLOW
K. C. Morais¹, D. F. Abreu¹, L. Tobaldini Neto¹, R. Papa¹, L. C. C. Santos¹; ¹EMBRAER S. A., Brazil
  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 VALIDATION OF A DISCONTINUOUS GALERKIN BASED DES SOLVER IN FLOW PROBLEMS USING HIGH PERFORMANCE COMPUTING
A.V. Wolkov, TsAGI, Russia
Reserve Paper 4.3.R GENERATION OF STEADY-STATE FLOWS WITH MINIMAL GAIN MARCHING SCHEMES
R.D.S. Dias dos Santos, Brazil
5.3Student Hands On Activities
Chair: S. Suzuki
Track 5
14 - ECSC
  15:00 15:30 5.3.1 ALL JAPAN STUDENT'S INDOOR FLYING ROBOT CONTEST
Takeshi Tsuchiya, The University of Tokyo, Japan
  15:30 16:00 5.3.2 THE AERONAUTICAL SOCIETY OF SOUTH AFRICA AEROSPACE CHALLENGE
J S John Steven Monk, CSIR, South Africa
  16:00 16:30 5.3.3 SAE BRASIL STUDENT PROGRAMS - A SUCCESS STORY
Horacio A. Forjaz, SAEBRASIL, Brazil
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
7.3Aeroacoustics and Icing
Chair: F. Collier
Track 7
03.4 - Applied Aerodynamics
  15:00 15:30 7.3.1 INVESTIGATION OF THE AEROACOUSTIC INFLUENCE OF A SEAL ATTACHED ON SLAT COVE USING LST AND POD TECHNIQUE
M. A. F. de Medeiros, Aeronautical Engineering Department - University of Sao Paulo, Brazil
  15:30 16:00 7.3.2 AN INTEGRATED CFD-SEA METHODOLOGY TO ACCOUNT FOR AERODYNAMIC SOURCES INTO CABIN NOISE PREDICTIONS
B Guaraldo Neto, Embraer SA, Brazil
  16:00 16:30 7.3.3 THE STUDIES ON LOW-NOISE LAMINAR WING REGIONAL AIRCRAFT
N.A. Pushchin, TsAGI, Russia
8.3Aeroelasticity 3 : Fixed-wing Aircraft
Chair: A. Chizhov
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
Qijing YU¹, Saeil LEE¹, M. Damodaran¹, B.C. Khoo¹; ¹National University of Singapore, Singapore
  15:30 16:00 8.3.2 AEROELASTIC PROPERTIES OF ACTIVE WINGLETS
G. Amiryants, TsAGI, 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: I. Yimer
Track 9
05 - Propulsion
  15:00 15:30 9.3.1 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
D. Simon¹, S. Ward¹, L.P.G. Pinto², B. Lantto¹, V.J. De Negri², P. Krus, Linköping University, Sweden; ¹Saab AB, Sweden ;²Federal University of Santa Catarina, Brazil
  15:30 16:00 10.3.2 SELF INDUCED FAILURE OF A SERVO VALVE
T. Seung, Program Management Office Aeronautics Research / DLR del. iABG, Germany
  16:00 16:30 10.3.3 NUMERICAL AND EXPERIMENTAL STUDY OF A TWO DEGREES OF FREEDOM ELECTROHYDRAULIC MANIPULATOR
W. Cardozo, PUC-Rio, Brazil
11.3UAS VTOL
Chair: 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 TILTWING 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 EVALUATION ON HOME DELIVERY SERVICE USING MULTIPLE DRONES
Hiroki Omagari, Department of Aeronautics and Astronautics, Kyushu University, Japan
Reserve Paper 11.3.R MODELLING AND CONTROL OF A BI-TILT-ROTOR UAV WITH DOUBLE GIMBAL AND CAMERA FOR SURVEILLANCE SYSTEMS APPLICATION
J.C. Vendrichoski¹, T.L. Costa¹, E.S. El´Youssef¹, E.R. de Pieri¹; ¹UFSC, Brazil
12.3UAS - Unmanned Aircraft Systems
Chair: A. Lief
Track 12
10 - Safety and Security
  15:00 15:30 12.3.1 INVESTIGATION OF EMERGING HUMAN-MACHINE INTERFACE CONCEPTS FOR UAS OPERATIONS
Yixiang: Y. Lim¹, Kavindu: K. Ranasinghe¹, Alessandro: A Gardi¹, Neta: N Ezer, Northrop Grumman Corporation, United States; Roberto: R Sabatini¹; ¹RMIT University, Australia
  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. L. 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
Roelof Vos, 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 CONSTRAINED BIFURCATION AND CONTINUATION METHOD IN BLENDED-WING-BODY AIRCRAFT DESIGN
F. Cen¹, Q. Li¹, B.-W. Nie², Z.-T. Liu²; ¹Tsinghua University, China ;²China Aerodynamics Research and Development Center , China
2.4Next Generation Commercial Transport Concept
Chair: 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 Bonet, The Boeing Company, United States
  10:30 11:00 2.4.2 SINGLE-AISLE AIRLINER DISRUPTION WITH A SINGLE-DECK BLENDED WING BODY
M. Page¹, E. Smetak¹, S. Yang¹; ¹DZYNE Technologies Incorporated, United States
  11:00 11:30 2.4.3 CONCEPTUAL DESIGN OF THE D8, A HIGHLY-EFFICIENT SUBSONIC COMMERCIAL TRANSPORT AIRCRAFT
B.Y. Yutko, Aurora Flight Sciences, United States
  11:30 12:00 2.4.4 SUBSONIC ULTRA-GREEN AIRCRAFT RESEARCH: TRANSONIC TRUSS-BRACED WING TECHNICAL MATURATION UPDATE
C. K. Droney¹, N. A. Harrison¹, G. M. Gatlin, NASA Langley Research Center, United States; ¹The Boeing Company, United States
3.4Systems Architecting
Chair: K. Schwartz
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.
Gonzalez-Biedma: Gonzalez-Biedma, Airbus Defence & Space, 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
  11:30 12:00 4.4.4 NUMERICAL ANALYSIS OF BLEND WING BODY AIRFRAME AND ENGINE AERODYNAMIC INTERFERENCE
Zhaoguang Tan, China; Yingchun Chen, China; Jiangtao Si, China; Yuan Zhong, China
Reserve Paper 4.4.R COMPARISON AND APPLICATION OF DIFFERENT TECHNIQUES OF MULTI-OBJECTIVE OPTIMIZATION FOR AERODYNAMICS WINGS DESIGN
N Gautier¹, N Manzanares-Filho¹, E-R Da Silva¹; ¹UNIFEI, Brazil
5.4Wind Tunnel Systems Development
Chair: C. Hermans
Track 5
03.2 - Experimental Aerodynamics
  10:00 10:30 5.4.1 OVERVIEW OF DYNAMIC TEST TECHNIQUES FOR FLIGHT DYNAMICS RESEARCH AT LOW SPEED AERODYNAMICS INSTITUTE, CARDC
Zhitao Liu¹, Haisheng Sun¹, Bowen Nie¹, Linliang Guo¹, Fei Cen¹; ¹China Aerodynamics Research and Development Center (CARDC), China
  10:30 11:00 5.4.2 APPLICATION OF THE COMBINED BOUNDARIES TO REDUCE WALL INTERFERENCE FOR NACA 0012 AIRFOIL TESTS
S. Chernyshev¹, A. Ivanov¹, E. Streltsov¹, A. Volkova¹; ¹Central Aerohydrodynamic Institute n.a. prof. N.E. Zhukovsky, Russia
  11:00 11:30 5.4.3 EVALUATION OF WIND TUNNEL SIDEWALL 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
  11:30 12:00 5.4.4 EXPERIMENTAL INVESTIGATION OF SHEAR LAYER INDUCED FLUCTUATIONS IN A OPEN JET WIND TUNNEL
G.G. Gadzhimagomedov, Central Aerohydrodynamic Institute n.a. prof. N.E. Zhukovsky, Russia
6.4Composites
Chair: 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. Horton, Virginia Tech, 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
Tadashige Ikeda, Chubu University, Japan; Makoto Ishigami¹, Tsuyoshi 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
Reserve Paper 6.4.R RESULTS AND COMPARISON OF NUMERICAL SIMULATION AND THE TESTING OF LUG MANUFACTURED BY COMPOSITE MATERIAL BY RTM PROCESS
Giovane Fonseca, Embraer - Centro de Engenharia e Tecnologia - Minas Gerais, Brazil; Sérgio Frascino, ITA - Instituto Tecnológico de Aeronáutica, Brazil
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 AIRCRAFT IN FIREFIGHTING
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
Kevin 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
Alexis cenko, AIWS, United States; Nick Stathopoulos, L3-MAS, Canada; Robert Hobbins, Bombardier, Canada; Graham Akroyd, Akroyd Aeronautics, Australia
8.4New Structural Design 1: General
Chair: T. Ikeda
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  10:00 10:30 8.4.1 A PASSIVE-ADAPTIVE WING FOR DRAG REDUCTION
C. B. York, University of Glasgow, United Kingdom
  10:30 11:00 8.4.2 INVESTIGATION OF INFLUENCE OF SYNERGETIC EFFECT ON STRENGTH AND WEIGHT OF PRIMARY FRAME AIRCRAFT STRUCTURES
E. Dubovikov¹, M. Zichenkov¹, I. Mareskin¹, A. Chernov¹, A. Shanygin¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
  11:00 11:30 8.4.3 A NUMERICAL AND EXPERIMENTAL ANALYSIS OF THE DYNAMICS OF A TENSEGRITY-MEMBRANE STRUCTURE
L. H. Teixeira¹, J. H. Izuka, Faculty of Applied Sciences - UNICAMP, Brazil; P. Gonzalez¹, P. Kurka¹; ¹Faculty of Mechanical Engineering - UNICAMP, Brazil
  11:30 12:00 8.4.4 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
9.4Engine Performance
Chair: S. Remy
Track 9
05 - Propulsion
  10:00 10:30 9.4.1 THE PHYSICS BEHIND MCHANICS AND FAILURE OF GAS TURBINE COMPONENTS IN AEROSPACE SYSTEMS
Prakash Patnaik, National Research Canada, Canada; Kuiying Chen¹, Xijia 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
  11:30 12:00 9.4.4 A ROBUST STABLE PI CONTROLLER DESIGN IN TIME-FREQUENCY DUAL DOMAINS FOR AIRCRAFT ENGINE
Nan Liu, Shanghai Aircraft Design & Research Institute, China
10.4Control for Flexible Aircraft
Chair: S. Ueno
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  10:00 10:30 10.4.1 IMPLEMENTATION OF A STABILITY AUGMENTATION SYSTEM ON A VERY FLEXIBLE AIRCRAFT
P. J. González, Instituto Tecnologico de Aeronautica (ITA), Brazil
  10:30 11:00 10.4.2 ADAPTIVE OUTPUT-FEEDBACK GAIN SCHEDULING APPLIED FOR FLEXIBLE AIRCRAFT
R.B. Bertolin, ITA, Brazil
  11:00 11:30 10.4.3 CONTROL OF A VERY FLEXIBLE WING WITH SIMULTANEOUS OPTIMIZATION OF THE GAIN MATRIX AND THE SPATIAL DISTRIBUTION OF THE SE
M. A. V. Morales, Brazil
  11:30 12:00 10.4.4 FLIGHT TESTING AN ADAPTIVE GUST LOADS ALLEVIATION ON A FLEXIBLE AIRCRAFT
Y. Wang, China Academy of Aerospace Aerodynamics, China
11.4Flight Test and Equipment
Chair:
Track 11
07 - Systems, Subsystems and Equipment
  10:00 10:30 11.4.1 CORE POWER SUPPLY, FROM ENGINES TO BATTERIES – A FLIGHT TEST APPROACH
F.M. Catalano, Sao Carlos School of Engineering - University of Sao Paulo, Brazil
  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
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@mpat.go.jp
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, R Geister¹, L Altenscheidt¹, M Altenscheidt, NavArt, Germany; M Braschczok¹; ¹DLR, Germany
  11:00 11:30 12.4.3 OPERATIONAL CONCEPT AND VALIDATION OF A NEW AIRPORT LOW-LEVEL WIND INFORMATION SYSTEM
Tomoko Iijima¹, Naoki Matayoshi¹, Shoh 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
Reserve Paper 12.4.R OPERATIONAL ASSESSMENT OF PASSENGER BOARDING STRATEGIES FOR COMMERCIAL AIRCRAFT
M. Schmidt, Bauhaus Luftfahrt, Germany
1.5Design Education 1
Chair: K. Rinoie
Track 1
01 - Aircraft Design and Integrated Systems
  14:00 14:30 1.5.1 COLLABORATIVE OPEN SOURCE AIRCRAFT DESIGN FRAMEWORK FOR EDUCATION - AGILE ACADEMY INITIATIVES AND RESULTS
P S Shivaprakasha, Germany
  14:30 15:00 1.5.2 WHAT WE CAN DO TODAY TO EDUCATE AND TRAIN THE COLLABORATIVE ENGINEER OF TOMORROW
M. Spieck, Thelsys, Germany
  15:00 15:30 1.5.3 EXPERIENCE WITH INTERNATIONAL COLLABORATIVE AIRCRAFT DESIGN EDUCATION: AREND UAV
Lelanie Smith, University of Pretoria, South Africa; Jean, N Koster, University of Colorado, United States; Johannes Schneider, University of Stuttgart, Germany
2.5Aircraft Design
Chair: A. Isikveren
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 PREDICTING AERODYNAMIC CENTER SHIFT FROM BODY EFFECTS USING NUMERICAL AND SEMI EMPIRICAL METHODS
Willem A.J. Anemaat¹, Dennis van Dommelen¹, Adam D'Silva¹, Pierson B. Sargent¹; ¹DARcorporation, United States
3.5Desktop Simulations
Chair: J.C. Dunyach@airbus.com
Track 3
02 - Systems Engineering and Integration
  14:00 14:30 3.5.1 VIRTUAL ENGINE: CONCEPTION, SIMULATION, MODELS, STRUCTURE AND PARTS OPTIMIZATION
Y. Temis, Central Institute of Aviation Motors, Russia
  14:30 15:00 3.5.2 RESEARCH ON DESKTOP VIRTUAL INTEGRATION AND VERIFICATION OF CIVIAL AIRCRAFT
Zhichao Yao¹, Bozhi Guo, China-Russia Commercial Aircraft International Co., China; Dianhuang Xie¹, Zhengqiang Li¹; ¹Shanghai Aircraft Design and Research Institute, China
  15:00 15:30 3.5.3 A NOVEL FMI AND TLM-BASED DESKTOP SIMULATOR FOR DETAILED STUDIES OF THERMAL PILOT COMFORT
R. Hällqvist¹, J. Schminder², M. Eek¹, R. Braun², P. Krus², R. Gårdhagen²; ¹Saab Aeronautics, Sweden ;²Linköping University, Sweden
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 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
5.5Advanced Transport Aircraft Concepts for Environmentally responsible Aviation
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
Ulrich Kling¹, Tobias Brügge¹, Fabian Peter¹, Mirko Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
  14:30 15:00 6.5.2 BUCKLING/POSTBUCKLING OPTIMIZATION OF STIFFENED COMPOSITE PANELS BASED ON SENSITIVITY ANALYSIS
Lijun Dong, Chinese Aeronautical Establishment, China
  15:00 15:30 6.5.3 GLOBAL-LOCAL STRUCTURAL ANALYSIS OF COMPOSITE WINGS
E. Carrera¹, A. Pagani¹, G. HC Silva, Embraer S.A., Brazil; ¹Politecnico di Torino, Italy
Reserve Paper 6.5.R AERODYNAMIC AND FEM ANALYSIS OF A WOODEN SEAPLANE
F. Favalli¹, M. Ferrara¹, C. Patuelli¹, A. Polla¹, S. Scarso¹, D. Tomasello¹; ¹Polytechnic of Turin, Italy
7.5Advanced Manufacturing
Chair: M. Zhu
Track 7
08 - Manufacturing and Supply Chain Management
  14:00 14:30 7.5.1 RISK ASSESSMENT PROCESS FOR AUTOMATED SEALING APPLICATION IN A HUMAN ROBOT COLLABORATION ENVIRONMENT - A 3D SIMULATION A
DQ Queiroz, Embraer, Brazil
  14:30 15:00 7.5.2 MITIGATING THE RISKS OF PRODUCIBILITY FAILURES DURING CONCEPT PLATFORM DEVELOPMENT
J. Madrid¹, J. Landahl¹, R. Söderberg¹, H. Johsnnesson¹, J. Lööf, GKN Aerospace, Sweden; ¹Chalmers University of Technology, Sweden
  15:00 15:30 7.5.3 STUDIES ON AIRCRAFT ROBOT AIDED MANUFACTURING
G. J. G Lahr¹, J. V. R. Soares, Votorantim S.A., Brazil; J. O. Savazzi, EMBRAER-GPX, Brazil; G. A. P. Caurin¹; ¹University of Sao Paulo, Brazil
8.5Impact
Chair: M. Kurdelski
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  14:00 14:30 8.5.1 VERIFIED FUSELAGE SECTION WATER IMPACT MODELING
YK Song, Virginia Tech, United States
  14:30 15:00 8.5.2 PREDICTING LOW-VELOCITY IMPACT DAMAGE IN COMPOSITE PANELS USING COHESIVE ELEMENT
hongquan liu¹, shengang tan¹; ¹fai, China
  15:00 15:30 8.5.3 ENERGY-ABSORBING CHARACTERISTICS ANALYSIS OF COMPOSITE THIN-WALLED C-CHANNELS UNDER LOW SPEED AXIAL COMPRESSION
Jiang XIE¹, Zhenyu FENG¹, Shanshan SONG¹, Dongfang SONG¹, Xuehan Zhang¹; ¹Civil Aviation University of China, China
9.5MDO-1
Chair: V. Garnier
Track 9
05 - Propulsion
  14:00 14:30 9.5.1 IN-FLIGHT ACOUSTIC LOADS MEASUREMENTS ON AN ENGINE FLYING TEST BED
Yifeng Sun¹, Cyrille Breard¹, Xianping Li¹, Yadong Mei², Peng Liu², Mingbao Pang²; ¹Shanghai Aircraft Design and Research Institute of COMAC, China ;²COMAC Flight Test Center, China
  14:30 15:00 9.5.2 MULTI-DISCIPLINARY OPTIMISATION OF A TURBOPROP-POWERED UNMANNED AERIAL VEHICLE
NA NA, NA, Australia
  15:00 15:30 9.5.3 AN AEROTHERMODYNAMIC MODEL OF AIRCRAFT ENGINE PROPULSION SYSTEMS USING OBJECT-ORIENTED PROGRAMMING
F. B. O. Oliveira, UFMG, Brazil
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. Paulino, Instituto Tecnologico de Aeronautica, Brazil
  14:30 15:00 10.5.2 MANEUVERABILITY ASSESSMENT FOR FAULTY AIRPLANE BY IFS WITH SIMULTANEOUS MODEL-MATCHING FOR GUST AND HANDLING RESPONSES
SATO Masayuki, 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
Reserve Paper 10.5.R 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
11.5De-Icing
Chair:
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 DETECTING HIGH-ALTITUDE ICE CRYSTAL ICING EVENTS FROM TAT ANAOMALIES
R. M. Arnaldo Valdés, Universidad Politecnica de Madrid, Spain
  15:00 15:30 11.5.3 NUMERICAL SIMULATION OF ICE ACCRETION INFLUENCED BY AN ANTI-ICING HEATING SYSTEM
Krzysztof Szilder, Aerospace, National Research Council, Canada; Edward P. Lozowski, University of Alberta, Canada
Reserve Paper 11.5.R CALCULATION OF WATER FILM FLOW AND HEAT TRANSFER ON THE AIRCRAFT ANTI-ICING SURFACE
Mei Zheng¹, Tao Wu¹, Zhiqiang Guo¹, Wei Dong¹; ¹Shanghai Jiao Tong University, China
12.5Air Transportation Network
Chair: X. Zhang
Track 12
09 - Air Transport System Efficiency
  14:00 14:30 12.5.1 A SIMULATION MODELING STUDY FOR FREE ROUTING AIRSPACE IN JAPAN
Kota: K. Kageyama¹, Y: Y. Yoichi¹; ¹ENRI, Japan
  14:30 15:00 12.5.2 EVALUATION OF THE POTENTIAL IMPACTS OF HYBRID-ELECTRIC AIRCRAFT ON THE GLOBAL AIR TRANSPORTATION NETWORK SYSTEM
G. Tay¹, S. Gillen¹, R. Rothfeld, Bauhaus Luftfahrt e.V., Germany; M. Hornung¹; ¹Technical University of Munich, Germany
  15:00 15:30 12.5.3 DYNAMIC AIRSPACE MANAGEMENT FOR ENHANCED ATM SAFETY AND EFFICIENCY
A. G. Gardi, RMIT University, Australia
Reserve Paper 12.5.R STUDY ON THE LARGE-AREA FLIGHT DELAY RECOVERY
Zhaoning Zhang¹, Jinghua Wang¹; ¹Civil Aviation University of China, China
1.6NATO Hybrid/Electric Initiative
Chair: A. Isikveren
Track 1
01 - Aircraft Design and Integrated Systems
  16:00 16:30 1.6.1 NATO RESEARCH TASK GROUP: HYBRID/ELECTRIC AIRCRAFT DESIGN AND STANDARDS FOR RESEARCH AND TECHNOLOGY (HEADSTART)
F. Grauer, Germany
  16:30 17:00 1.6.2 FLIGHT TEST OF A FUEL-CELL/BATTERY/SUPERCAPACITOR TRIPLE HYBRID UAV PROPULSION SYSTEM
A. Gong¹, J. Palmer, Defence Science and Technology Group, Australia; D. Verstraete¹; ¹The University of Sydney, Australia
  17:00 17:30 1.6.3 KEY PERFORMANCE PARAMETERS FOR FUTURE NATO HYBRID/ELECTRIC MILITARY AIR VEHICLES
W. Dyson, National Aeronautics Space Administration (NASA), United States
  17:30 18:00 1.6.4 COORDINATING INTERNATIONAL RESEARCH AND DEVELOPMENT IN HYBRID/ELECTRIC FLIGHT
n/a Kloeckner, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany
2.6Supersonic and Hypersonic Vehicles
Chair: Z. Goraj
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
Morita Naoto, the University of Tokyo, Japan
  16:30 17:00 2.6.2 RDTE AND PRODUCTION COSTS ESTIMANTION RELATIONSHIPS FOR THE CONCEPTUAL DESIGN OF HYPERSONIC TRANSPORTATION SYSTEMS
R. Fusaro¹, V Vercella¹, D. Ferretto¹, 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 OF SUPERSONIC BUSINESS JETS
A.M Abdalla¹, M.U. Urzedo¹, M. Calvo, École de l’air - French Air Force Academy, France; R.C. Munjulury, Linkoping University, Sweden; ¹University of São Paulo - USP - Brazil, Brazil
  17:30 18:00 2.6.4 ANALYSIS OF LOW-BOOM CHARACTERISTICS OF SUPERSONIC WAVERIDER
Potsawat Boonjaipetch, Tohoku University, Japan
Reserve Paper 2.6.R AN EFFICIENT FRAMEWORK FOR AERODYNAMIC CONFIGURATION EVOLUTION OF REENTRY VEHICELES
Moein M. Entezari¹, Meysam Mohammadi-Amin¹; ¹ARI, Iran
3.6Systems Engineering Cases
Chair: P. Krus
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, F. Wolters¹, R.-G. Becker¹, C. Klein¹, S. Reitenbach¹; ¹German Aerospace Center , Germany
  17:00 17:30 3.6.3 A 7D TRADE
Doug Howarth, MEE Inc., United States
  17:30 18:00 3.6.4 BUILDING INNOVATIVE BUSINESS MODELS IN AERONAUTICS INDUSTRY: SOME LESSONS FROM THE BIONIC AIRCRAFT PROJECT
LP Pereira, Federal University of ABC, Brazil
4.6CFD Applications
Chair: 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-W 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 NUMERICAL SIMULATION OF OPERATING PROCESS ELEMENTS FOR COMBUSTION CHAMBERS OF PERSPECTIVE GTE
P.A. Semenev, Central Institute of Aviation Motors, Russia
Reserve Paper 4.6.R LAUNCHER AERODYNAMIC ANALYSIS WITH PLUME EFFECTS
Giuseppe Pezzella, Italian Aerospace Research Centre, Italy
5.6Wind Tunnel Test Technology
Chair: C. Hermans
Track 5
03.2 - Experimental Aerodynamics
  16:00 16:30 5.6.1 ADAPTIVE DESIGN OF EXPERIMENT BASED ON GAUSSIAN PROCESS MODELS WITH NONSTATIONARY KERNEL APPLIED TO WIND TUNNEL TESTING
U.H. Choi¹, J.H. Kim¹, Y.B. Lee, Agency for Defense Development, South Korea; J.M. Ahn¹; ¹KAIST, South Korea
  16:30 17:00 5.6.2 RLG BASED REAL-TIME MODEL ATTITUDE DETERMINATION SYSTEM DEVELOPMENT FOR LARGE LOW SPEED FACILITY OF CARDC
Fan Litao¹, Huang Zhiyuan¹, Wu Zhigang¹; ¹CARDC, China
  17:00 17:30 5.6.3 ROTATING SHAFT BALANCE DESIGN AND CALIBRATION FOR CROR TESTING
V.S. Manvelyan, TsAGI, Russia
  17:30 18:00 5.6.4 THE INFLUENCE OF SPIV DATA PROCESSING PARAMETERS ON AIRCRAFT WING WAKE VORTEX ASSESSMENT
K. Garry¹, D. Di Pasquale¹, S. Prince¹, N. Lawson¹; ¹Cranfield University, United Kingdom
6.6Aircraft Structural Design II
Chair: T. Ireman
Track 6
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  16:00 16:30 6.6.1 STRUCTURAL DESIGN OF THE LARUS QR-15 SAILPLANE WING
J. Laguardia, Univesidade Federal de Minas Gerais, Brazil; L. Pereira, Universidade Federal de Minhas Gerais, Brazil; D. Azevedo, Universidade Federal de Minas Gerais, Brazil
  16:30 17:00 6.6.2 PRELIMINARY ASSESSMENT OF A WARPING WING CONFIGURATION IN ROLLING CONTROL
E. Cestino¹, G. Frulla¹, A. Lanzillotti¹; ¹Politecnico di Torino, Italy
  17:00 17:30 6.6.3 STRUCTURAL DESIGN AND ANALYSIS OF A QUADROTOR FIXED-WING HYBRID UAV WING
W Fang, China; H Ma, China; H Zhang, China
  17:30 18:00 6.6.4 STRUCTURAL SIZING OF A ROTORCRAFT FUSELAGE USING AN INTEGRATED DESIGN APPROACH
D.B. Schwinn¹, P. Weiand¹, M. Schmid¹, M. Buchwald¹; ¹German Aerospace Center (DLR), Germany
Reserve Paper 6.6.R AN ACTIVE-PASSIVE NONLINEAR FINITE ELEMENT MODEL FOR ELECTROMECHANICAL COMPOSITE MORPHING BEAMS
R. B Olympio¹, M. V. Donadon¹, S. G. P Castro, EMBRAER, Brazil; ¹ITA, Brazil
7.6Optimization
Chair: K. Jamison
Track 7
03.4 - Applied Aerodynamics
  16:00 16:30 7.6.1 MULTI-POINTS AERODYNAMIC OPTIMIZATION DESIGN OF A DUAL-AISLE AIRPLANE WING
R.Z. LI¹, M. ZHANG², M.H. ZHANG², Y.F. ZHANG¹, H.X. CHEN¹; ¹Tsinghua University, China ;²Shanghai Aircraft Design and Research Institute, China
  16:30 17:00 7.6.2 MULTILEVEL COLLABORATIVE AERODYNAMIC DESIGN OPTIMIZATION BASED ON SOBOL’ GLOBAL SENSITIVITY ANALYSIS
Chao Wang¹, Zhenghong Gao¹, Pei Liu¹, Yang Na¹, Xinqi 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
Reserve Paper 7.6.R WING TWIST OPTIMISATION OF A BENCHMARK PROBLEM USING TWO AERODYNAMIC SOLVERS
G. Yang¹, A. Da Ronch¹, D. Kharlamov¹, J. Drofelnik¹; ¹University of Southampton, United Kingdom
8.6Aeroelasticity 4: 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 INVESTIGATION OF PROPELLER INFLUENCE ON STALL AND DYNAMIC BEHAVIOR OF VERY FLEXIBLE AIRCRAFT
P. C. Teixeira¹, C. E. S. Cesnik¹; ¹University of Michigan, United States
  16:30 17:00 8.6.2 REDUCED ORDER MODELS FOR NONLINEAR AEROELASTICITY
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 NONLINEAR STATIC AEROELASTIC AND TRIM ANALYSIS OF HIGHLY FLEXIBLE AIRCRAFT
Chi Zhang¹, Zhou Zhou¹, Pu 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
Qian Wei¹, Bai Yuguang¹, Zeng Huihua, Shenyang Aircraft Design Institute, China; Yang Rui¹; ¹Dalian University of Technology, China
9.6MDO-2 AGILE
Chair: A. Mirzoyan
Track 9
05 - Propulsion
  16:00 16:30 9.6.1 MDO OF PROPULSION SYSTEM FOR ADVANCED CIVIL AIRCRAFT IN AGILE PROJECT COLLABORATIVE MDO ENVIRONMENT
A.A. Isyanov, CIAM, Russia
  16:30 17:00 9.6.2 STUDIES IN AGILE PROJECT COLLABORATIVE MDO ENVIRONMENT ON PROPULSION AND ON-BOARD SYSTEMS MATCHING FOR ADVANCED AIRCRAFT
A. Mirzoyan¹, A. Isianov¹, A. Maximov¹, M. Fioriti², L. Boggero²; ¹CIAM, Russia ;²Politecnico di Torino, Italy
  17:00 17:30 9.6.3 COMMUNICATION BETWEEN PS AND AIRCRAFT SYSTEMS IN COLLECTIVE MDO SYSTEM IN AGILE PROJECT
P.D. Toktaliev, Central Institute of Aviation Motors, Russia
  17:30 18:00 9.6.4 PROPULSION SYSTEM - AIRFRAME INTEGRATION AND OPTIMIZATION OF CIVIL AIRCRAFT- AGILE EU PROJECT
P S Shivaprakasha, German Aerospace Center, Germany
10.6Flight Trajectory Design
Chair: T. Tsuchiya
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 SYSTEMS: APPLICATION TO ELECTRICAL THRUST REVERSER ACTUATION SYSTEMS
Scott Delbecq¹, Marc Budinger, Institut Clément Ader (UMR CNRS 5312), France; Jérôme 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. Tomcko
Track 12
09 - Air Transport System Efficiency
  16:00 16:30 12.6.1 DECISION-MAKING INFORMATION SYSTEM FOR MULTIMODAL DISRUPTION MANAGEMENT: SYSTEM ARCHITECTURE AND CONCEPT OF OPERATIONS
FJS Jiménez Serrano, Hamad International Airport (Qatar Airways), Qatar
  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 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. Swaid, Hamburg University of Technology (TUHH), Germany
1.7Design Method 1
Chair: S. Bagassi
Track 1
01 - Aircraft Design and Integrated Systems
  09:30 10:00 1.7.1 AN ADVANCED SOFTWARE ENVIRONMENT FOR CONCEPTUAL AND PRELIMINARY 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
Charles M. Boozer¹, Ali 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 SAFETY ORIENTED ODM VTOL PRE-DESIGN METHODOLOGY
F. Rougier, SAFRAN, France
  11:30 12:00 1.7.5 HURRICANE-CS: CONTROL SURFACES AND HIGH LIFT DEVICES MODELING AND SIZING PROGRAM
C. López Sánchez, Spain; D. Sánchez Franco, Spain; Raghu Chaitanya Munjulurynjulury, Sweden
Reserve Paper 1.7.R 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
2.7Model Based System Engineering
Chair: L. Goes
Track 2
02 - Systems Engineering and Integration
  09:30 10:00 2.7.1 MBSE FLIGHT TEST ARCHITECTURE RESEARCH
xiao hua¹, chen qing¹, shengjun qi, cfte, China; ¹CFTE, China
  10:00 10:30 2.7.2 UTILIZATION OF SCALING LAWS AND UNCERTAINTY QUANTIFICATION TO INFORM TECHNOLOGY DEVELOPMENT EXPERIMENTATION
K.G. Schwartz, Georgia 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, UNIFEI, 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, B. García-Fogeda ¹, I. Rivero¹, J. Gómez-Escalonilla¹; ¹AIRBUS DS, Spain
  10:00 10:30 3.7.2 MODE I FATIGUE INDUCED DELAMINATION IN CO-CURED AND CO-BONDED COMPOSITE STRUCTURAL JOINTS
F. M. Gonzalez Ramirez, Instituto Tecnológico de Aeronáutica, Brazil
  10:30 11:00 3.7.3 USING THE LEAD CRACK CONCEPT TO REDUCE DURABILITY TEST DURATION
Loris Molent, DST, Australia
  11:00 11:30 3.7.4 INFLUENCE OF IRREGULAR LOADING PARAMETERS ON CFRP COMPONENTS FATIGUE LIFE
A.G. Kalinin, Central Aerohydrodynamic Institute, TsAGI, Russia
  11:30 12:00 3.7.5 OPTIMIZATION OF REINFORCEMENT HEIGHT PARAMETERS FOR AIRCRAFT PANEL STRUCTURES BASED ON VIBRATION FATIGUE DAMAGE ANALYSIS
Peng LI¹, Junfeng MA¹; ¹Aircraft strength research institute, China
4.7Turbulence Modeling and LES
Chair: M. Hackström
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
Matteo Moioli¹, Christian Breitsamter¹, Kaare 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
Wang Yue¹, Liu Kang¹, Song Wenping¹, Han Zhonghua¹; ¹Northwestern Polytechnical University, China
  11:00 11:30 4.7.4 AERODYNAMIC EVALUATION OF THE EXTERNAL FLOW OVER NOTCHBACKS AND PICKUP TRUCKS
E.-K. Mascia, Federal University of Uberlandia, Brazil
Reserve Paper 4.7.R LARGE EDDY SIMULATION OF A TRANSIENT SPOILER DEPLOYMENT IN A NACA0012 PROFILE IN SUBSONIC AND TRANSONIC SPEEDS
R. V. LINN, FEDERAL UNIVERSITY OF RIO GRANDE DO SUL (UFRGS), Brazil
5.7Unsteady Flows and Aeroacoustics
Chair: C. Yingchun
Track 5
03.2 - Experimental Aerodynamics
  09:30 10:00 5.7.1 UNSTEADY AERODYNAMIC CHARACTERISTICS OF THE OSCILLATING AIRFOIL USING MSBS
Y.H. Sung¹, J.S. Han¹, J.H. Han¹; ¹KAIST, South Korea
  10:00 10:30 5.7.2 DESIGN OF AN INSTRUMENTED STATOR VANE USING MEMS MICROPHONES FOR UNSTEADY PRESSURE MEASUREMENTS AT THE EESC-USP FAN RIG
B Martinez R Jr¹, LC Caldas¹, RG Cuenca, Federal University of Santa Catarina, Brazil; R Lauterjung Q, Embraer S/A, Brazil; PC Greco Jr¹; ¹University of Sao Paulo, Brazil
  10:30 11:00 5.7.3 EVALUATION OF TRANSONIC BUFFETING ONSET BOUNDARY ESTIMATED BY TRAILING EDGE PRESSURE DIVERGENCE AND RMS DATA OF WING VIBRATION
Rodrigo Sorbilli Sousa, EMBRAER, Brazil; Roberto Gil A. da Silva¹, Roberto da Motta Girardi¹; ¹ITA, Brazil
  11:00 11:30 5.7.4 CHALLENGES OF AERO-ACOUSTIC MEASUREMENTS IN WIND TUNNEL: IDENTIFICATION AND ELIMINATION OF “PARASITE” NOISE
Yifeng Sun¹, Cyrille Breard¹, Xianping Li¹, Yingchun Chen¹; ¹Shanghai Aircraft Design and Research Institute of COMAC, China
  11:30 12:00 5.7.5 TIME-RESOLVED PRESSURE MEASUREMENTS FOR AN AIRFOIL WITH SELF-SUSTAINED SHOCKWAVE OSCILLATIONS
H. F. Leite¹, A. C. Avelar, Brazil; R. G. A. Silva¹; ¹ITA, Brazil
6.7Complex Transition Phenomena
Chair: L. Alves
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  09:30 10:00 6.7.1 EFFECTS OF THE INTRINSIC THREE-DIMENSIONALIZATION OF SEPARATION BUBBLES ON THE AMPLIFICATION OF EXTERNAL DISTURBANCES
Daniel Rodriguez, Universidade Federal Fluminense, Brazil; Elmer Mateus Gennaro, Sao Paulo State University, Brazil
  10:00 10:30 6.7.2 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
  10:30 11:00 6.7.3 CONTROL OF COMPLEX DISTURBANCES IN THE BOUNDARY LAYER OVER A FLAT PLATE.
P. Morra¹, K. Sasaki², A. Cavalieri², A. Hanifi¹, D.S. Henningson¹; ¹KTH Royal Institute of Technology, Sweden ;²Instituto Tecnológico de Aeronáutica, Brazil
  11:00 11:30 6.7.4 DEVELOPMENT OF SECONDARY CROSSFLOW INSTABILITY NEAR BREAKDOWN TO TURBULENCE
C J Atkin, City, University of London, United Kingdom
  11:30 12:00 6.7.5 LAMINAR-TURBULENT TRANSITION MECHANISMS OVER WIDELY-SPACED SUCTION HOLES
C J Atkin, City, University of London, United Kingdom
7.7Aircraft Aerodynamic Design
Chair:
Track 7
03.4 - Applied Aerodynamics
  09:30 10:00 7.7.1 CONCEPT OF MEDIUM TWIN-ENGINE STOL TRANSPORT AIRPLANE
O.V. Pavlenko¹, A.V. Petrov¹, E.A. Pigusov¹; ¹TsAGI, Russia
  10:00 10:30 7.7.2 ANALYSIS AND DESIGN OF WING TRAILING EDGE MOUNTED OVER-THE-WING DISTRIBUTED PROPULSION
L.L.M. Veldhuis¹, A Khajehzadeh¹, S.J. Hullshoff¹; ¹Delft University of Technology, Netherlands
  10:30 11:00 7.7.3 CEA ENGINEERING IMPACTING THE RED BULL AIR RACE
G. A. Santana, Aeron Engenharia, Brazil
  11:00 11:30 7.7.4 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 7.7.5 OUTBOARD SPLIT FLAP AERODYNAMICS OF A FLYING WING CONFIGURATION
S. Pfnür¹, C. Breitsamter¹; ¹Technical University of Munich, Germany
Reserve Paper 7.7.R ROBUST DESIGN OPTIMIZATION OF BENCHMARK AERODYNAMIC CASE BASED ON POLYNOMIAL CHAOS EXPANSION
Zhao Huan¹, Gao Zhenghong¹; ¹Northwestern Polytechnical University , China
8.7Aeroelasticity 1 : Methods and Modeling
Chair: K. Willcox
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  09:30 10:00 8.7.1 NUMERICAL AND EXPERIMENTAL INVESTIGATION OF AEROELASTIC TAILORED SWEPT WINGS MADE OF UNIDIRECTIONAL AND TOW-STEERED FRC
H. L. Lebkuchen, Instituto Tecnológico de Aeronáutica , Brazil; C. E. de Souza, Universidade Federal de Santa Maria, Brazil; R. G. A. da Silva, Instituto Tecnológico de Aeronáutica, Brazil
  10:00 10:30 8.7.2 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 8.7.3 INTERRELATION BETWEEN THE LOADING AND THE AEROELASTICITY CHARACTERISTICS OF MEDIUM RANGE AIRCRAFT IN TRANSONIC FLOW
A. Chizhov, TsAGI, Russia
  11:00 11:30 8.7.4 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
  11:30 12:00 8.7.5 THERMAL-MECHNICAL COUPLING ANALYSIS AND OPTIMIZATION DESIGN ON TPS WITH GAP
Shiyu Huo¹, Qun Yan¹, Weihua Xie, Harbin Institute of Technology , China; ¹Aircraft Strength Research Institute, China
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
Xudong Yang¹, Jianhua Xu¹, Bo Wang¹, Chao Song¹, Shunlei 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 STAGES DESIGNING FOR ADVANCED AIRCRAFT ENGINES
Sergey Pankov¹, Victor Mileshin¹, Igor Orekhov¹, Victor Fateev¹; ¹Central Institute of Aviation Motors, Russia
  11:00 11:30 9.7.4 AN INTEGRATED PROPULSION SYSTEM FOR BI-MODAL UNMANNED VEHICLES
A. Bacciaglia¹, D. Guo², P. Marzocca², C. Bil², A. Ceruti¹; ¹University of Bologna, Italy ;²RMIT University, Australia
  11:30 12:00 9.7.5 PARAMETRIC INVESTIGATION OF EESC-USP AEROACOUSTIC FAN RIG
R. G. Cuenca, UFSC, Brazil; EESC-USP EESC-USP¹, B. M. dit245¹; ¹EESC-USP, Brazil
10.7Flight Control 1
Chair:
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  09:30 10:00 10.7.1 EVALUATION OF ALTITUDE CONTROL FOR AN AIRBREATHING HYPERSONIC AIRCRAFT MODEL
Masaharu Hiruma, The University of Tokyo, Japan
  10:00 10:30 10.7.2 A COMPARISON BETWEEN UNIVERSAL INTEGRAL REGULATOR AND LINEAR QUADRATIC TECHNIQUE FOR AN AIRCRAFT AUTOPILOT
Y. A. Díaz-Méndez¹, M. S. Sousa¹, S. S. Cunha¹, G. F. Gomes¹; ¹Federal University of Itajubá, Brazil
  10:30 11:00 10.7.3 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
  11:00 11:30 10.7.4 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
11.7UAS Flight Test
Chair: T. Götzendorf-Grabowski
Track 11
06.2 - Flight Dynamics and Control (UAV related)
  09:30 10:00 11.7.1 METHODS FOR EFFICIENT FLIGHT TESTING AND MODELLING OF REMOTELY PILOTED AIRCRAFT WITHIN VISUAL LINE-OF-SIGHT
A. Sobron¹, D. Lundström¹, R. Larsson², P. Krus¹, C. Jouannet²; ¹Linköping University, Sweden ;²Saab Aeronautics, Sweden
  10:00 10:30 11.7.2 VERTICAL LANDING OF A FIXED-WING UAV USING THE FLAT SPIN
S. Higashino, Kyushu University, Japan; K. Nakama, Kyushu University, Graduate Student, Japan
  10:30 11:00 11.7.3 PLANNING, IMPLEMENTATION, AND EXECUTION OF AN AUTOMATIC FIRST FLIGHT OF A UAV
M. E. Kügler¹, F. Holzapfel¹; ¹Technical University of Munich, Inst. of Flight System Dynamics, Germany
  11:00 11:30 11.7.4 SAFETY FLIGHT TESTING FOR CARGO UAV DEVELOPMENT
Kakuya Iwata¹, Keisuke Yamada¹, Ryuzo Horiuchi¹, Akiya Kamimura¹; ¹National Institute of Advanced Industrial Science and Technology, Japan
12.7Airport / 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 AIRPORT 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
Timo 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 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
DK Jeon, Korea Aerospace Research Institute, South Korea
1.8Design Education 2
Chair: S. Bagassi
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 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
  15:00 15:30 1.8.3 ELECTRIC VTOL UAV CONFIGURATION STUDIES AND OPTIMIZATION WITHIN AIRCRAFT DESIGN PRACTICAL COURSE AT TECHNICAL UNIVERSITY
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 DRONES AS AN EMERGING PREDICTIVE MAINTENANCE TOOL.
J Sandoval, Universidad Autónoma Metropolitana Unidad Lerma, Mexico; J-J Barron, Universidad Tecnológica de Jalisco, Mexico
  14:30 15:00 2.8.2 DIGITAL TRANSFORMATION IN AIRLINE MAINTENANCE
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
3.8Physics Based Damage Modeling
Chair: S. Nutt
Track 3
04.1 - Material Issues, Fatigue and Damage Tolerance
  14:00 14:30 3.8.1 MODELING AND SIMULATION OF MIXED MODE FATIGUE-INDUCED DELAMINATION IN COMPOSITE: A COMPARATIVE STUDY
L. A. de Oliveira¹, D. S. Alves¹, M. V. Donadon¹; ¹Instituto Tecnológico de Aeronáutica, Brazil
  14:30 15:00 3.8.2 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 3.8.3 THE IMPORTANCE OF SECONDARY BENDING EVALUATION IN STRUCTURAL JOINT ANALYSIS
W. R. P. Mendonça, EMBRAER S.A., Brazil
Reserve Paper 3.8.R ON ELASTIC PSEUDO-ISOTROPIC ORTHOTROPIC PLATES
L.M.B.C. Campos, Instituto Superior Tecnico, Portugal
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 DEVELOPMENT OF A NUMERICAL ENVIRONMENT TO PREDICT BOUNDARY LAYER TRANSITION
A.P. Antunes¹, R. Cosin¹; ¹Embraer, Brazil
  15:00 15:30 4.8.3 MACHINE LEARNING APPROACH TO THE INTERMITTENCY TRANSITION TURBULENCE MODEL FOR WIND TURBINE APPLICATION
M.A. Abd Bari¹, A. Da Ronch¹, M. Panzeri, Noesis Solutions, Belgium; J. Drofelnik¹; ¹University of Southampton, United Kingdom
5.8Aerodynamic Experiments
Chair: E. Takana
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. Granzoto Granzoto¹, G.J. Zambrano Zambrano¹, G.G. Becker Becker¹, L. A. Algodoal Algodoal¹; ¹Embraer, Brazil
  15:00 15:30 5.8.3 EXPERIMENTAL AND CFD ANALYSIS OF A UAV FOR SUPERFICIAL VOLCANO SURVEILLANCE
L Botero-Bolivar¹, D Acevedo-Giraldo¹, H D Cerón-Muñoz¹, F 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
Guilherme A Freire¹, André V G Cavalieri¹, Flávio 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
7.8New Structural Design 2: Morphing Structures
Chair: T. Ikeda
Track 7
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  14:00 14:30 7.8.1 STRUCTURAL INTEGRITY DIAGNOSIS FOR AGING TRANSPORT AIRCRAFT BASED ON FLIGHT DATA
H. Wang, College of General Aviation, Wenzhou University, China
  14:30 15:00 7.8.2 INFLUENCE OF UNCERTAIN PARAMETERS AFFECTING THE DYNAMIC BEHAVIOR OF A FLEXIBLE DISC
A.A.C.J. Cavalini Jr, Federal University of Uberlandia, Brazil
  15:00 15:30 7.8.3 A RESEARCH OF ZIMMERMAN-WEISSENBURGER-YANG METHOD FOR FLUTTER BOUNDARY PREDICTION
YANG FEI, Shang Hai Aircraft Design and Research Institute of COMAC, China
Reserve Paper 7.8.R A RESEARCH OF MULTIDISCIPLINARY DESIGN OPTIMIZATION ALGORITHM FOR FIGHT VEHICLE DESIGN
Xiqiang YAN¹, Zongzheng LIU¹, Yisheng YANG¹; ¹CARDC, China
8.8Aeroelasticity 6 : 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
Bai Yuguang¹, Qian Wei¹, Chen Xiangyan¹; ¹Dalian University of Technology, China
  14:30 15:00 8.8.2 MULTIDISCIPLINARY METHOD 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
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
N V Kukshinov, CIAM, Russia
  14:30 15:00 9.8.2 COMPLEX NUMERICAL AND EXPERIMENTAL RESEARCH OF HEXAFLY-INT HIGH-SPEED CIVIL AICRAFT MODEL
N V Kukshinov, CIAM, Russia
  15:00 15:30 9.8.3 INFLUENCE OF TEMPERATURE FACTOR ON THE CHARACTERISTICS OF HIGH-SPEED AIR-BREATHING ENGINE INLETS
O.V. GUSKOV, MIPT, Russia
10.8Flight Dynamics & Identification 1
Chair: O. Korsun
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  14:00 14:30 10.8.1 SYSTEM IDENTIFICATION USING SUBSPACE METHOD OF A FLEXIBLE AIRCRAFT OPERATING IN CLOSED-LOOP
Raphaela C M G Barbosa¹, Luiz C S Góes¹; ¹ITA, Brazil
  14:30 15:00 10.8.2 RECURSIVE AERODYNAMIC PARAMETER IDENTIFICATION OF A FIGHTER JET FLYING IN TURBULENT AIR
C. Grillo, Università di Palermo, Italy
  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:
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
R. A. Souza¹, M. L. Oliveira¹, S. P. L. Vieira¹, W. O. Avelino¹, C. F. R. Oliveira¹, D. W. de Lima Monteiro¹, F. S. Torres¹, R. M. O. Hansen, SDU, Denmark; ¹UFMG, Brazil
  15:00 15:30 11.8.3 AN AIRBORNE DATA BUS NETWORK SYSTEM OF INTERFACE ADAPTIVE AND FLEXIBLE CONTROL
Z. Dai¹, Z. Qiu, Xi'an Aeronautics Computing Technique Research Institute, China; L. Shi¹; ¹ChengDu Aircraft Design & Research Institute, China
12.8On Demand Mobility: Integration in Civil Airpace
Chair: K. Kageyama
Track 12
09 - Air Transport System Efficiency
  14:00 14:30 12.8.1 SIMULATION STUDY FOR VFR AIRCRAFT AND SMALL UNMANNED AIRCRAFT SYSTEMS (SUAS) MIXED OPERATIONS IN LOW LEVEL AIRSPACE
H Hirabayashi¹, D Toratani¹, A Kohmura¹; ¹ENRI, Japan
  14:30 15:00 12.8.2 URBAN AIR TRANSPORTATION JOURNEY TIME COMPARISON FOR MELBOURNE METROPOLITAN AREA
Lewis Swadesir¹, Cees Bil¹; ¹RMIT University, Australia
  15:00 15:30 12.8.3 ADAPTIVE LANDING SEQUENCING IN AIR TRAFFIC FLOW OPTIMISATION
M. Hickson¹, C. Bil¹; ¹RMIT University, Australia
1.9Unconventional Concepts 2
Chair: B. Kimmel
Track 1
01 - Aircraft Design and Integrated Systems
  16:00 16:30 1.9.1 FLEXFLOIL SHAPE ADAPTIVE CONTROL SURFACES—FLIGHT TEST AND NUMERICAL RESULTS
Sridhar Kota, FlexSys Inc, United States; Joaquim Martins, University of Michigan, United States
  16:30 17:00 1.9.2 FEASIBILITY STUDY OF MODIFYING A KEROSENE AIRCRAFT TO A LH2 POWERED VERSION
Wenqing XIE¹, Zhuoyi Duan¹, Howard Smith, Cranfield University, United Kingdom; ¹AVIC The First Aircraft Institute, China
  17:00 17:30 1.9.3 DEVELOPMENT OF THE REGENERATIVE SOARER, THEORETICAL AND PRACTICAL ASPECTS
R.C. Carvalho, EMBRAER S.A., Brazil
  17:30 18:00 1.9.4 DEVELOPMENT OF A NOVEL AERIAL PLATFORM WHICH MERGES THE CONCEPT OF ARSHIPS AND TETHERED AEROSTATS
J. S. Santos¹, B. A. de Azevedo¹, L. C. S. Góes¹, R. S. Pant, Indian Institute of Technology Bombay, India; ¹Instituto Tecnológico de Aeronáutica, Brazil
2.9Alternative Energy and Distributed Propulsion Aircraft
Chair: A. Isikveren
Track 2
01 - Aircraft Design and Integrated Systems
  16:00 16:30 2.9.1 INTEGRATED TURBO-ELECTRIC MOTIVE POWER SYSTEMS FOR REGIONAL TRANSPORT APPLICATIONS
A.T. Isikveren, SAFRAN S.A., France
  16:30 17:00 2.9.2 DEVELOPING THE UNMANNED UNCONVENTIONAL CARGO AIRPLANES WITH HYBRID PROPULSION SYSTEM
J. Rohacs, Department of Aeronautics, Naval Architecture and Railway Vehicl, Hungary
  17:00 17:30 2.9.3 OPTIMIZATION OF MOTOR FOR THE MAXIMIZATION OF SOLAR-POWERED AIRCRAFT PERFORMANCE
Sergey Serokhvostov, MIPT, Russia; Tatyana Churkina, MAI, Russia
  17:30 18:00 2.9.4 INVERSE AIRCRAFT DESIGN FOR MARKETSHARE
J.G. Gibbs, Savion Aerospace, United States
3.9Advanced Manufacturing and Non Destructive Testing
Chair: K. Lewis
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 FUNDAMENTAL APPROACHES FOR METAL-COMPOSITE STRUCTURES LOADING PROGRAMS EQUIVALENCE FOR FULL-SCALE SERVICE LIFE TEST
Andrey Pankov¹, Viktor Konovalov¹; ¹TsAGI, Russia
  17:00 17:30 3.9.3 STUDY OF EXTERNAL FACTORS COMBINATION EFFECT ON CFRP BULK STRUCTURE UTILIZING ULTRASONIC MICROSCOPY
Tatiana Ryzhova¹, Alexander Shanygin¹, Vladimir Scherbakov¹, Yulia Petronyuk², Vadim Levin², Egor Morokov²; ¹Central Aerohydrodynamic Institute, Russia ;²Institute of Biochemical Physics of RAS, Russia
  17:30 18:00 3.9.4 NON-CONTACT MEASUREMENTS OF DEFORMATION OF LARGE-SIZED AIRCRAFT WING USING OPTICAL VIDEOGRAMMETRY METHOD
K.A. Kuruliuk, TsAGI, Russia
4.9Hypersonic Flow
Chair: L. Alves
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  16:00 16:30 4.9.1 RESEARCH ON EXTERNAL AERODYNAMICS OF THE HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJ
N.V. Voevodenko¹, A.A. Gubanov¹; ¹TsAGI, Russia
  16:30 17:00 4.9.2 RANS AND DSMC FLOW SIMULATIONS OVER TYPICAL HYPERSONIC CONFIGURATIONS
R. R. P. P. Pereira, IAE, Brazil
  17:00 17:30 4.9.3 UNSTRUCTURED COMPRESSIBLE NAVIER-STOKES SOLVER FOR HIGH ALTITUDE FLOWS
C. Baek, Inha university, South Korea
  17:30 18:00 4.9.4 TRIM DRAG MINIMIZATION AT CRUISE FLIGHT OF A HIGH-SPEED PASSENGER VEHICLE
S.A. Takovitskii, Central Aerohydrodynamic Institute, Russia; V.F. Villace, European Space Agency, Netherlands
Reserve Paper 4.9.R LONGITUDINAL STABILITY DESIGN CRITERIA FOR HYPERSONIC GLIDERS
B.Y. Chen, China Academy of Aerospace Aerodynamics, China
5.9History of Aeronautics
Chair: M. Lott
Track 5
12 - Host nation
  16:00 16:30 5.9.1 THE SANTOS-DUMONT LEGACY TO AERONAUTICS
M. P. Brandão, ITA, Brazil
  16:30 17:00 5.9.2 BRAZILIAN AVIATION HISTORY: THE UNIVERSITY OF SÃO PAULO CASE
F.M. catalano, University of São Paulo -EESC-USP, Brazil
  17:00 17:30 5.9.3 THE STUDY OF TURBORAMJETS IN CIAM
Vladimir Palkin¹, Pavel Kadjardouzov¹, Valentin Solonin¹, Mikhail Tskhovrebov¹; ¹CIAM, Russia
  17:30 18:00 5.9.4 HISTORY OF AVIATION IN MINAS GERAIS
E. Bauzer, Brazil
6.9Buffet and Separation Control
Chair: C. Breitsamter
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 AEROFOIL
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
V.G. Soudakov¹, K.A. Abramova¹; ¹TsAGI, Russia
  17:30 18:00 6.9.4 CFD ANALYSIS OF COAND? BLANKET CURVATURE ON COAND? DEVICE PERFORMANCE
Harijono DJOJODIHARDJO, Insitute for the Advancement of Aerospace Science and Technology, Indonesia
7.9Propellors and Rotors
Chair: J. Monk
Track 7
03.4 - Applied Aerodynamics
  16:00 16:30 7.9.1 APPLICATION OF HIGH-ROBUSTNESS BEMT FOR SIMULATION OF UAV-VTOL PROPELLER AT LOW/HIGH ADVANCE RATIO
Zhongyun Fan¹, Zhou Zhou¹, Xiaoping Zhu, Science and Technology on UAV Laboratory, NPU, China; ¹School of Aeronautics,Northwestern Polytechnical University, China
  16:30 17:00 7.9.2 DESIGN OFA DOUBLE-ENDED AIRFOIL IN UNSTEAD REVERSE FLOW
X. -D. YANG¹, M. HUANG¹; ¹School of Aeronautics Northwestern Polytechnical University, China
  17:00 17:30 7.9.3 INVESTIGATION ON APPROACH TO CONTROL LIFT DISTRIBUTION OF WING BY DISTRIBUTED PROPELLERS
Zhou Zhou¹, Hong-bo Wang¹; ¹Northwestern Polytechnical University, China
  17:30 18:00 7.9.4 CFD SIMULATION OF XH-59A ROTOR IN HOVER AND 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
Reserve Paper 7.9.R THE EFFECTS OF BLADE ASPECT RATIO AND TAPER RATIO ON THE HOVERING PERFORMANCE OF THE CYCLOIDAL ROTOR
Y.Hu Hu, Northwestern polytechnich university, China
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
Rimple Sandhu, Carleton University, Canada; Weixing Yuan, National Research Council (NRC) Canada, Canada; Dominique 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 COMPUTATIONAL STUDY OF THE AERODYNAMICS AND AEROELASTICITY OF FLAPPING WING
Harijono DJOJODIHARDJO, Insitute for the Advancement of Aerospace Science and Technology, Indonesia; Airlangga 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 CFD MODELLING TO OPTIMIZE THE MAXIMUM THRUST IN SCRAMJET ENGINE AND ANALYSIS OF ITS OPERATION PERFORMANCE
M-P Pires, IME, Brazil
  16:30 17:00 9.9.2 RESEARCH OF PROPULSION ENGINES FOR ADVANCE REUSABLE TSTO AEROSPACE SYSTEM
A.I. Lanshin¹, O.V. Sokolova¹, Yu.M. Shikhman¹, V.E. Shlyakotin¹; ¹CIAM, Russia
  17:00 17:30 9.9.3 SIMULTANEOUS MEASUREMENTS OF TEMPERATURE AND HEAT FLUX IN SUPERSONIC COMBUSTOR BY ITO THIN FILM THERMOCOUPLE
Jin Xinhang¹, Ma Binghe¹, Qiu Tao¹; ¹Northwestern Polytechnical University, China
  17:30 18:00 9.9.4 GROUND FACILITY TESTS OF HIGH SPEED RAMJET DEMONSTRATORS
A Prokhorov, CIAM, Russia
10.9Flight Dynamics & Identification 2
Chair: Y. Watanabe
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  16:00 16:30 10.9.1 BIO-DYNAMIC STABILITY ANALYSIS OF A GREBE DURING MIGRATION
J Feaster, Virginia Tech, United States
  16:30 17:00 10.9.2 DYNAMIC REACTION OF AN AIRPLANE TO TRAILING VORTICES GENERATED BY ANOTHER AIRPLANE
G. Kowaleczko, Air Force Institute of Technology, Poland
  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.F Fischer, Instituto 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
Duoneng Liu, China Aerodynamics Research and Development Center, China; Xianzhong 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
Luca Boggero¹, Marco Fioriti², Francesca Tomasella², Pier Davide Ciampa¹; ¹German Aerospace Center, Germany ;²Politecnico di Torino, Italy
  17:30 18:00 11.9.4 FAULT DIAGNOSIS METHOD STUDY FOR COMPLEX SYSTEM BASED ON KALMAN FILTERS
Wei Niu¹, Juan Cheng, Xi’an Institute of Applied Optics, China; Wensheng 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 LABORATOTY 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
Reserve Paper 12.9.R HUMAN RELIABILITY ANALYSIS IN AN AIRCRAFT DECOMPRESSION EVENT
C. Reiser¹, A. Bayma¹, D.A. Fonseca¹; ¹Embraer S/A, 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. 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 A330-300 R2035 STRUCTURE AND EXTERNAL CONFIGURATION
Z.-J. Goraj¹, M. Kowalski¹, A. Seitz, Bauhaus Luftfahrt e.V., Germany; ¹Warsaw University of Technology, Poland
  11:30 12:00 1.10.4 AN APPROACH TO ASSESS AIRFRAME WEIGHT REDUCTION PERFORMANCE FOR STITCHED COMPOSITE TECHNOLOGIES
J. Corman, Georgia Institute of Technology, United States
  12:00 12:30 1.10.5 NARROW-BODY B737NG PASSENGER CONVERSION TO FREIGHTER
Ilan Berlowitz, Israel Aerospace Industries, Israel
Reserve Paper 1.10.R RESERCH ON KEY TECHNOLOGY OF INTELLIGENT CIVIL AIRCRAFT
Zhengqiang Li¹, Dianhang Xie¹, Bin Gao¹, Zhichao Yao¹; ¹Shanghai Aircraft Design and Research Institute, China
2.10Aircraft Operations 2
Chair: S. Teixeirada da Cunha
Track 2
11 - Operations and Sustainment
  10:00 10:30 2.10.1 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
  10:30 11:00 2.10.2 PROGNOSIS OF AIRCRAFT FUEL FLOW USING MACHINE LEARNING ALGORITHMS ON FLIGHT OPERATIONAL DATA
S. Baumann, Technische Universitaet Darmstadt, Germany
  11:00 11:30 2.10.3 FUEL-BURN PENALTIES CAUSED BY IRREGULARITIES IN AIRCRAFT SURFACES (ASTEROID PROJECT)
David Philpott¹, Kevin Hackett¹, Andrew Shires², Ben Hinchliffe²; ¹IHS Markit (ESDU), United Kingdom ;²University of Leeds, United Kingdom
  11:30 12:00 2.10.4 COST-BENEFIT ASSESSMENT OF CLIMATE AND WEATHER OPTIMIZED TRAJECTORIES FOR DIFFERENT NORTH ATLANTIC WEATHER PATTERNS
Benjamin Lührs, TUHH, Germany; Malte Niklaß¹, Christine Frömming¹, Volker Grewe¹, Volker Gollnick¹; ¹DLR, Germany
  12:00 12:30 2.10.5 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
3.10Crack and Impact Damage Propagation
Chair: J. Fish
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
Stanislav DUBINSKII¹, Yuri Feygenbaum², Vitaliy Senik¹, Evgeniy 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 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
  10:30 11:00 4.10.2 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
  11:00 11:30 4.10.3 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
  11:30 12:00 4.10.4 EVALUATION OF DELTA WING EFFECTS ON THE STEALTH-AERODYNAMIC FEATURES FOR NON-CONVENTIONAL FIGHTER AIRCRAFT
A Abdalla¹, F Catalano¹; ¹EESC-USP, Brazil
  12:00 12:30 4.10.5 DESIGN SPACE EXPLORATION AND FLOW CONTROL FOR A TRANSONIC WING DRAG REDUCTION
Y UTAMA, INSTITUT TEKNOLOGI BANDUNG, Indonesia
Reserve Paper 4.10.R AERODYNAMICS OPTIMIZATION DESIGN METHOD AND SHAPE PARAMETERIZATION
Z.Y Wang, The First Aircraft Institute, AVIC, China
5.10Optical Measurement Techniques
Chair: C. Klein
Track 5
03.2 - Experimental Aerodynamics
  10:00 10:30 5.10.1 FLOW UNSTEADINESS RESEARCHES ON THE BLUNT FIN-INDUCED SHOCK/BOUNDARY LAYER INTERACTIONS
W.H.-R. Ruan, China; X.J.-Z. Zhao, China; X.J.-X. Xiang, China; Q.-S. Shen, China
  10:30 11:00 5.10.2 INVESTIGATION OF THE SHOCK WAVE/BOUNDARY LAYER INTERACTION PATTERN AT TRANSONIC SPEEDS
M.A. Brutyan, TsAGI, Russia
  11:00 11:30 5.10.3 PARTICLE IMAGE SURFACE FLOW VISUALIZATION AND SKIN-FRICTION MEASUREMENT
V. E. Mosharov¹, V. N. Radchenko¹, N. S. Tsipilev¹; ¹TsAGI, Russia
  11:30 12:00 5.10.4 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
  12:00 12:30 5.10.5 INVESTIGATION OF BDUNDARY LAYER TRANSITION MEASUREMENT IN SUBSONIC WIND TUNNEL USING TSP
Jingbo Yu¹, lianfeng Wei¹, xingju Xiang¹, hongwei Wang¹, zhan Huang¹; ¹China Academy of Aerospace Aerodynamics, China
6.10Student Final
Chair: K. Rein Weston
Track 6
15 - Guest lectures
7.10High Speed Aerodynamics
Chair: A. Gubanov
Track 7
03.4 - Applied Aerodynamics
  10:00 10:30 7.10.1 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
  10:30 11:00 7.10.2 PRELIMINARY STUDY OF THE AERODYNAMIC CHARACTERISTICS OF KRUEGER FLAP ON THE SST CONFIGURATION
Dongyoun Kwak, JAXA, Japan; Keisuke Ohira, Ryoyu Systems, Japan
  11:00 11:30 7.10.3 AERODYNAMICS CAUSED BY ATTITUDE RATES OF A SUPERSONIC FLIGHT EXPERIMENT VEHICLE WITH A CRANCKED-ARROW MAIN WING
K. Mizobata, National University Corporation Muroran Institute of Technology, Japan
  11:30 12:00 7.10.4 HIGH SPEED DRAG REDUCTION OPTIMIZATION FOR PROJECTILES
T. Wan, Department of Aerospace Engineering, Tamkang University, Taiwan
  12:00 12:30 7.10.5 ADVANCED SONIC BOOM ANALYSIS USING FULL-FIELD SIMULATION
R. Yamashita, The University of Cambridge, United Kingdom
8.10Aeroelasticity 2 : Controls
Chair: C. Breitsamter
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, ROBERTO G SILVA¹; ¹ITA, Brazil
  11:00 11:30 8.10.3 AEROELASTIC MODELING AND VIBRATION ATTENUATION OF HELICOPTER ROTOR BLADES
C.P. Pagani, São Paulo State University, Campus of São João da Boa Vista., Brazil
  11:30 12:00 8.10.4 EXPERIMENTAL STUDY OF AEROELASTIC RESPONSE OF A FLEXIBLE HIGH ASPECT RATIO WING WITH PASSIVE SMA ACTUATORS
R. N. C Duarte, Universidade Federal de Campina Grande, Brazil; R. G. A Silva, Instituto Tecnológico de Aeronáutica, Brazil
  12:00 12:30 8.10.5 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
9.10Compressor Aerodynamics
Chair: S. Pankov
Track 9
05 - Propulsion
  10:00 10:30 9.10.1 MATCHING BETWEEN METAMODEL AND OPTIMIZATION TOOL APPLIED IN A MULTISTAGE AXIAL-FLOW COMPRESSOR AIMING DESIGN IMPROVEMENT
Vinicius Monteiro¹, Iha Koshun¹, Osmar Silva¹, Thiago Ebel, Concepts Nrec, United States; ¹ITA, Brazil
  10:30 11:00 9.10.2 NUMERICAL AND EXPERIMENTAL STUDY THE EFFECT OF CIRCUMFERENTIAL GROOVES ON HPC LAST STAGE PERFORMANCE
V.I. MILESHIN, Central Institute of Aviation Motors, Russia
  11:00 11:30 9.10.3 ADAPTIVE GTE SURGE PROTECTION SYSTEM WITH SELECTIVE CONTROL OF THE ACTUATORS
L.G. Bliznyukov¹, M.G. Kesselman¹, V.I. Chernyshov¹, S.A. Smetanin¹; ¹Central Institute of Aviation Motors, Russia
  11:30 12:00 9.10.4 AXIAL AND CENTRIFUGAL HIGH PRESSURE COMPRESSORS FOR PROSPECTIVE ENGINES
A. Startsev, CIAM, Russia
10.10Flight Control 2
Chair: J. Vian
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  10:00 10:30 10.10.1 QUASI-LPV MODELING AND PARAMETER-DEPENDENT OPTIMAL CONTROL OF MORPHING WING AIRCRAFT
J Lee¹, Y Kim¹; ¹Seoul National University, South Korea
  10:30 11:00 10.10.2 AERODYNAMIC ANALYSIS AND CONTROL ALLOCATION FOR ASYMMETRIC VARIABLE SWEEP AIRCRAFT WITH FLEXIBLE TRAILING EDGE
H Ma¹, B.F Song¹, Y Pei¹, Z.W Chen¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
  11:00 11:30 10.10.3 EFFECTS OF TAILORED CONTROL SURFACE COMPLIANCE ON AIRCRAFT STABILITY AND CONTROL
Petter Krus, Linköping university, Sweden
  11:30 12:00 10.10.4 USE OF DISSIMILAR SENSOR DATA IN FLIGHT CONTROL LAWS
D.P.T. Ferreira, EMBRAER, Brazil
  12:00 12:30 10.10.5 DIGITAL HYDRAULICS IN AEROSPACE APPLICATIONS: SLIDING MODE BEHAVIORS OF QUANTIZED CONTROL AND AN LMI DESIGNING SOLUTION
P. Krus, Linköping University, Sweden; V.J. De Negri, Universidade Federal de Santa Catarina, Brazil
11.10UAS Control 1
Chair: J. Gunlach
Track 11
06.2 - Flight Dynamics and Control (UAV related)
  10:00 10:30 11.10.1 MULTI-CHANNEL HUMAN-MACHINE INTERACTIVE SYSTEM FOR MULTIPLE UAVS\\\' CONTROL
Peng-cheng Wen¹, Ya-di Zhang¹, Ya-hui Li¹; ¹AVIC Xi'an Aeronautics Computing Technique Research Institute, China
  10:30 11:00 11.10.2 FLIGHT PERFORMANCE OF STEERABLE CRUCIFORM PARACHUTE SYSTEMS
S. Herrington¹, T. Fields¹, O. Yakimenko, Naval Postgraduate School, United States; ¹University of Missouri-Kansas City, United States
  11:00 11:30 11.10.3 PID GAIN SCHEDULING FOR CONSISTENT MANEUVERABILITY OF HEXACOPTER UNDER BATTERY VOLTAGE DROP
S. Kim, Korea Advanced Institute of Science and Technology, South Korea
  11:30 12:00 11.10.4 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
  12:00 12:30 11.10.5 ON WAKE VORTEX SAFETY ANALYSIS AND CONTROL FOR UAV
Vladimir Golubev¹, Petr Kazarin¹, Claudia Moreno¹, William MacKunis¹; ¹ERAU, United States
12.10Operations - ATM (air traffic mamagement)
Chair: M. Peters
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
D. Rohacs, HungaroControl - Hungarian Air Navigation Services, Hungary
  11:00 11:30 12.10.3 THRUST MODELS BASED ON OPERATIONAL FLIGHT DATA USED IN PARAMETER ESTIMATION FOR SAFETY ANALYSES
Phillip Koppitz¹, Jonas Kuerten¹, Florian Holzapfel¹; ¹Technical University of Munich - Flight System Dynamics, Germany
  11:30 12:00 12.10.4 AIRCRAFT KEY PARTS INTELLIGENT FAULT DIAGNOSIS USING GAUSSIAN DEEP BELIEF NETWORK
H.D. Shao, School of Aeronautics, Northwestern Polytechnical University, China
  12:00 12:30 12.10.5 ADAPTING CAPACITY OF AIR NAVIGATION SERVICE PROVISION IN EUROPE - BETWEEN SCYLLA AND CHARYBDIS
Thomas Standfuss, DLR German Aerospace Center, Germany; Frank Fichert, University of Applied Sciences, Germany; Matthias 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
Yu. V. Kuzmin, TsAGI, Russia
  15:00 15:30 1.11.3 THE HAWKER SIDDELEY AVIATION HS141. VERTICAL TAKE –OFF AND LANDING RESEARCH PROGRAMME IN THE LATE 1960 EARLY 1970S.
F. Ogilvie, United Kingdom
2.11Structural Health Monitoring 2
Chair: 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
Dennis Roach¹, Tom Rice¹; ¹Sandia National Laboratories, United States
  14:30 15:00 2.11.2 STRUCTURAL HEALTH MONITORING QUALIFICATION PROCESS AND THE FUTURE OF AIRCRAFT MAINTENANCE
R. P. Rulli¹, F. Dotta¹, 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 STRUCTURAL HEALTH MONITORING 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 STRUCTURAL HEALTH MONITORING
A.K. F. Tamba¹, L.C. Vieira¹, F. Dotta¹, R.P. Rulli¹, G.O.C Prado¹, P.A. da Silva¹, R.R. Cunha¹, J.P da Costa¹; ¹Embraer S.A., Brazil
3.11Structural Health Monitoring 1
Chair: T. Ikeda
Track 3
04.1 - Material Issues, Fatigue and Damage Tolerance
  14:00 14:30 3.11.1 OPTIMIZATION OF THE COEFFICIENT OF PROBABILITY DISTRIBUTION FUNCTION IN DAMAGE DETECTION USING GENETIC ALGORITHM
Pouyan K. Motamed¹, Ali Abedian¹, Mostafa Nasiri¹; ¹Sharif University of Technology, Iran
  14:30 15:00 3.11.2 DEVELOPMENT OF STRUCTURAL HEALTH MONITORING METHODS THROUGH THE ANALYSIS OF KINETICS OF LOCAL STRESS-STRAIN STATE
A. A. Bautin¹, Yu. A. Svirskiy¹; ¹TsAGI, Russia
  15:00 15:30 3.11.3 DETECTION OF HIDDEN FATIGUE CRACKS IN RIVETED LAP JOINTS USING WAVELET TRANSFORM AND NEURAL NETWORKS
A.Abedian abedian, sharif university of technology, Iran
Reserve Paper 3.11.R DEVELOPMENT OF METHODS FOR DETERMINING CRACK RESISTANCE PARAMETERS FOR STATIC AND FATIGUE LOADING FOR POLYMER COMPOSITE
V.L. Tokar¹, Yu.V. Koroleva¹, Yu.A. Svirsky¹; ¹TsAGI, Russia
4.11RANS Models
Chair: A. Antunes
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
  14:00 14:30 4.11.1 MULTIPHASE TURBULENCE MODELS FOR SCRAMJETS AND ABLATING WALLS
K.E.Son Son, Russia
  14:30 15:00 4.11.2 2D-RANS APPROACH TO STUDY A TURBULENT SEPARATED FLOW USING BSL EARSM MODEL
M.D.Q. De Queiroz, Pontificia Universidade Católica de Minas Gerais, Brazil
  15:00 15:30 4.11.3 NUMERICAL COMPARISON OF STEADY DISTURBANCES IN THE WAKE OF PERIODIC BLOW-SUCTION AND ROUGHNESS ELEMENTS
P. V. Chuvakhov¹, S. V. Alexandrov¹, E. A. Alexandrova, Central Aerohydrodynamic Institute (TsAGI), Russia; ¹Moscow Institute of Physics and Technology (MIPT), Russia
Reserve Paper 4.11.R NUMERICAL INVESTIGATION OF FLOW STRUCTURE OF DIFFERENTIAL EJECTOR
Zhang HaiYang¹, Yu YongSheng¹, Chen Qin¹; ¹China Aerodynamics Research and Development Centre, China
5.11Modeling and Simulation in Manufacturing
Chair: H. Zhang
Track 5
08 - Manufacturing and Supply Chain Management
  14:00 14:30 5.11.1 ENABLING THE DIGITAL FACTORY THROUGH THE INTEGRATION OF DATA-DRIVEN AND SIMULATION MODELS
O Pinon Fischer, Georgia Institute of Technology, United States
  14:30 15:00 5.11.2 ON-DEMAND SMALL UAS ARCHITECTURE SELECTION AND RAPID MANUFACTURING USING A MODEL-BASED SYSTEMS ENGINEERING APPROACH
C. Y. JUSTIN¹, A. RAMAMURTHY¹, N. BEALS², E. SPERO², D. N. MAVRIS¹; ¹GEORGIA INSTITUTE OF TECHNOLOGY, United States ;²U.S. ARMY RESEARCH LABORATORY, United States
6.11High Speed Transition
Chair: C. Atkin
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
  14:00 14:30 6.11.1 THEORETICAL STUDY OF RECEPTIVITY OF HIGH-SPEED BOUNDARY LAYER TO THREE DIMENSIONAL SURFACE VIBRATION
Youcheng Xi¹, Song Fu¹; ¹Tsinghua University, China
  14:30 15:00 6.11.2 DIRECT NUMERICAL SIMULATION OF MACH WAVE INFLUENCE ON LAMINAR-TURBULENT TRANSITION IN SUPERSONIC FLOW OVER A FLAT PLATE
Ivan V. Egorov, TsAGI, Russia
  15:00 15:30 6.11.3 ENTROPY LAYER EFFECT ON ROUGHNESS-INDUCED LAMINAR-TURBULENT TRANSITION IN SUPERSONIC FLAT PLATE FLOW
P. V. Chuvakhov, Central Aerohydrodynamic Institute (TsAGI), Russia
Reserve Paper 6.11.R EFFECT OF CONTROLLED PERIODIC ROUGHNESS ON GOERTLER VORTICES IN HYPERSONIC COMPRESSION RAMP FLOW
P. V. Chuvakhov¹, V. N. Radchenko¹, E. A. Alexandrova¹, V. Ya. Borovoy¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
7.11New Structural Design 3: Material and Micro Structures
Chair: H. Zanardi
Track 7
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
  14:00 14:30 7.11.1 METHOD FOR FLEXIBLE SKELETON COMPOSED OF THE TYPE OF INCIRCLE ELEMENT BASED ON EQUAL DISPLACEMENTAND 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, Y. Mirgorodsky¹, D. Vedernikov¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
  15:00 15:30 7.11.3 PREDICTIONOF THE CRACK PATTERN IN DUCTILE MATERIALS SUBJECT TO MECHANICAL LOADING USINGLATTICE MODELS
H Zanardi, Brazil
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 OPTIMIZATION OF SCARF JOINT ANGEL AND OVERPLY DOUBLER USING GENETIC ALGORITHM CONSIDERING ADHESIVE MATERIAL NONLINEARITY
A. Abedian, Aerospace Eng Dept, Sharif Uni of Tech, Iran
9.11ISABE
Chair:
Track 9
10.11Flight Testing
Chair: M. Naruoka
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
  14:00 14:30 10.11.1 WIND TUNNEL VIRTUAL FLIGHT TEST FOR A TRANSPORT AIRCRAFT WITH SIMULATED ICE SHAPE
GUO Linliang¹, ZHU Minghong¹, GUAN Jian¹, NIE Bowen¹; ¹China Aerodynamics Research and Development Centre, China
  14:30 15:00 10.11.2 DEVELOPMENT OF A GENERIC FLIGHT TEST MANEUVER INJECTION MODULE
Christoph Krause¹, Christoph Göttlicher¹, Florian Holzapfel¹; ¹Institute of Flight System Dynamics, Germany
  15:00 15:30 10.11.3 CHARACTERISTIC HELICOPTER FLIGHT MECHANICS AND MOTION CUEING INTEGRATION INTO THE SIVOR ROBOTIC FLIGHT SIMULATOR
D.F. Hidalgo, Universidad pontificia bolivariana, Colombia; G.B. Rodamilans¹, W.R. de Oliveira¹; ¹CCM-Instituto Tecnologico de Aeronautica, Brazil
Reserve Paper 10.11.R KNOWLEDGE ENGINEERING BASED FLIGHT TEST TECHNOLOGY FOR CIVIL AIRCRAFT AIRWORTHINESS CONFORMITY
LI ZHAOHUI¹, LI GANG¹; ¹Chinese Flight Test Establishment, China
11.11UAS Control 2
Chair: J. Bidinotto
Track 11
06.2 - Flight Dynamics and Control (UAV related)
  14:00 14:30 11.11.1 COMPARATIVE ANALYSIS OF METHODS USED TO ACTIVE CONTROL OF MICRO AERIAL VEHICLE
K.-S Sibilski, Warsaw University of Technology, Poland
  14:30 15:00 11.11.2 ROBUST TRAJECTORY OPTIMIZATION OF VTOL TRANSITION MANEUVER USING BI-LEVEL OPTIMAL CONTROL
P. Piprek¹, F. Holzapfel¹; ¹Technical University of Munich, Germany
  15:00 15:30 11.11.3 FIXED-WING UAV ROBUST GUIDANCE STRATEGY BASED ON COMPOUND FLIGHT MISSION OF ON-GROUND TARGETS
J. L. Gomes Olavo¹, L. A. Borges Tôrres¹, T. Argolo Jesus, CEFET/MG, Brazil; ¹UFMG, Brazil
Reserve Paper 11.11.R MODELING, CONTROL AND HARDWARE-IN-THE-LOOP SIMULATION OF A GENERIC TILTING MULTI-ROTOR
F. M. M. Marques¹, I. O. Tarifa¹, R. M. F. Neto¹, L. Sanches¹; ¹Universidade Federal de Uberlândia, Brazil
12.11Air Turbulence
Chair: O. Heinzinger
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. M. Matayoshi, Japan Aerospace Exploration Agency, Japan
  14:30 15:00 12.11.2 HAZARDOUS MITIGATION FOR TRANSPORT AIRCRAFT IN SEVERE ATMOSPHERIC TURBULENCE BASED ON IMPROVED CONTROL STRATEGY
C. Chang, College of General Aviation, Wenzhou University, China