| |||||||
| 10:30 | 11:00 | 1.1.1 |
UNCONVENTIONAL CONFIGURATIONS - DESIGN AND OPTIMIZATION T. Goetzendorf-Grabowski¹, J. Mieloszyk¹; ¹Warsaw University of Technology, Poland | ||||
| 11:00 | 11:30 | 1.1.2 |
INFLUENCE OF POWER UNIT CONFIGURATION LAYOUT OF A REGIONAL JET ON PERFORMANCE AND DIRECT OPERATING COST Z. Goraj¹, A. Sieradzki¹; ¹Institute of Aviation, Poland | ||||
| 11:30 | 12:00 | 1.1.3 |
DEVELOPMENT OF THE SMALL-SCALE MODEL OF MAGLEV SYSTEM ASSISTED AIRCRAFT SAFETY TAKE-OFF AND LANDING K. Sibilski¹, K. Fakkowski, Military University of Technology Technology, Poland; R. Kaleta, Air Force Institute of Technology, Poland; E. Ladyzynska-Kozdras¹, A.-M. Sibilska-Mroziewicz¹, W. Wróblewski, Wroclaw University of Technology, Poland; ¹Warsaw University of Technology, Poland | ||||
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| 10:30 | 11:00 | 2.1.1 |
A COMPUTATIONAL STUDY ON AVIAN FLAPPING FLIGHT AND THE INFLUENCE OF FEATHER SEPARATION J. Feaster¹, F. Battaglia¹, J. Bayandor¹; ¹Virginia Tech, United States | ||||
| 11:00 | 11:30 | 2.1.2 |
EFFECT OF ELASTIC DEFORMATION ON FLIGHT DYNAMICS OF PROJECTILES WITH LARGE SLENDERNESS RATIO R.H. Hua ¹, Z.Y. Ye¹, L. Yang¹; ¹Northwestern Polytechnical University, China | ||||
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| 10:30 | 11:00 | 3.1.1 |
THE ROUGHNESS POSITION INFLUENCE ON LAMINAR AEROFOIL AERODYNAMIC CHARACTERISTIC IN TRANSONIC FLOW REGIME R. Placek¹, M. Miller¹, P. Ruchala¹; ¹Institute of Aviation, Poland | ||||
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| 10:30 | 11:00 | 4.1.1 |
IMPORTANCE OF TRANSIENT AERODYNAMIC DERIVATIVES FOR V-TAIL AIRCRAFT FLIGHT DYNAMIC DESIGN N.A. Musa¹, S. Mansor¹, A. Ali¹, W.Z. Wan Omar¹; ¹AeroLAB, Universiti Teknologi Malaysia, Malaysia | ||||
| 11:00 | 11:30 | 4.1.2 |
AFLONEXT – ACTIVE FLOW_LOADS AND NOISE CONTROL ON NEXT GENERATION ACTIVE WING C. Atkin, City University London, United Kingdom | ||||
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| 10:30 | 11:00 | 5.1.1 |
GENERAL MESSAGE RACES IN DATA DISTRIBUTION SERVICE PROGRAMS FOR AIRBORNE SOFTWARE H.-J. Kim¹, O.-K. Ha¹, Y.-K. Jun¹; ¹Gyeongsang National University, South Korea | ||||
| 11:00 | 11:30 | 5.1.2 |
A KNOWLEDGE-BASED REAL TIME MONITORING AND DIAGNOSITC APPROACH FOR AIRCRAFT BREAKING SYSTEM X. Chen¹, H. Ren¹, J. Wang, University of Illinois at Urbana-Champaign, United States; Y. Chen¹, J. Chen¹, L. Zhi¹; ¹COMAC, China | ||||
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| 10:30 | 11:00 | 6.1.1 |
EVALUATION OF CONCEPTUAL DESIGN BASED ON MANUFACTURED ACTUAL UNMANNED SOLAR PLANE N. Arai¹, W. Harasani, King Abdruaziz Univ., Saudi Arabia; K. Hiraoka¹; ¹Tokai Univ., Japan | ||||
| 11:00 | 11:30 | 6.1.2 |
NEW DESIGN SCENARIO FOR FUTURE COMPOSITE LAUNCHER STRUCTURES R. Degenhardt, DLR, Germany | ||||
| 11:30 | 12:00 | 6.1.3 |
MULTIDISCIPLINARY TOPOLOGY-BASED OPTIMIZATION IN DESIGN OF AIRCRAFT STRUCTURAL LAYOUTS K.A. Balunov¹, V.V. Chedrik¹, S.A. Tuktarov¹, V.M. Uskov¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia | ||||
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| 10:30 | 11:00 | 7.1.1 |
KEY TECHNOLOGIES FOR THE NEXT GENERATION OF CIVIL AIRCRAFT ENGINES F. Haselbach, Rolls-Royce plc, United Kingdom | ||||
| 11:00 | 11:30 | 7.1.2 |
THE ROLLS-ROYCE PLC ULTRAFAN HEAT MANAGEMENT CHALLENGE M. Ryemill¹, C. Bewick¹, J.K. Min, Pusan UTC, South Korea; ¹Rolls-Royce plc, United Kingdom | ||||
| 11:30 | 12:00 | 7.1.3 |
DEVELOPMENT OF TECHNOLOGY ADVANCE FOR FUTURE PROPULSION SYSTEMS OF HAUL AIRCRAFT A. Lanshin¹, A. Mirzoyan¹, A. Polev¹; ¹CIAM, Russia | ||||
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| 10:30 | 11:00 | 8.1.1 |
AUGMENTED POLYNOMIAL GUIDANCE FOR TERMINAL VELOCITY CONSTRAINTS G.-H. Moon¹, S.-W. Shim¹, M.-J. Tahk¹; ¹KAIST, South Korea | ||||
| 11:00 | 11:30 | 8.1.2 |
IMPACT ANGLE CONTROL GUIDANCE CONSIDERING GRAVITY EFFECT H.-G. Kim¹, H.-J. Kim¹; ¹Seoul National University, South Korea | ||||
| 11:30 | 12:00 | 8.1.3 |
TERMINAL IMPACT ANGLE AND ANGLE-OF-ATTACK CONTROL GUIDANCE FOR SURFACE-TO-AIR MISSILE USING TVC S.-M. Hong¹, M.-G. Seo¹, M.-J. Tahk¹; ¹KAIST, South Korea | ||||
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| 10:30 | 11:00 | 9.1.1 |
ADAPTIVE NEURAL NETWORK CONTROLLER DESIGN FOR BLENDED-WING UAV WITH COMPLEX DAMAGE K.J. Kim¹, J.M. Ahn, Agency for Defense and Development, South Korea; S.K. Kim¹, J.Y. Suk¹; ¹Chungnam national university, South Korea | ||||
| 11:00 | 11:30 | 9.1.2 |
MODELING AND CONTROL OF HIGHLY FLEXIBLE FLYING-WING UAV WITH MULTIPLE ELEVONS AND PROPELLERS R. Wang¹, X.P. Zhu¹, Z. Zhou¹, Z.P. Wang¹; ¹Northwestern Polytechnical University, China | ||||
| 11:30 | 12:00 | 9.1.3 |
ON SAFETY ASSESSMENT OF NOVEL APPROACH TO ROBUST UAV FLIGHT CONTROL IN GUSTY ENVIRONMENTS V. Golubev¹, P. Kazarin¹, W. MacKunis¹, S. Borener², D. Hufty²; ¹ERAU, United States ;²FAA, United States | ||||
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| 10:30 | 11:00 | 10.1.1 |
ON APPLYING PISTON THEORY IN INTERFERENCE FLOWS M.-C. Meijer, University of Pretoria, South Africa; L. Dala, Council for Scientific and Industrial Research, South Africa; P.G. Karkle, Central Aerohydrodynamic Institute, Russia | ||||
| 11:00 | 11:30 | 10.1.2 |
UNSTEADY AERODYNAMICS MODELLING AND ITS APPLICATION IN AEROELASTIC STABILITY ANALYSIS X. Li¹, W. Zhang ¹; ¹School of aeronautics, Northwestern Polytechnical University, China | ||||
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| 10:30 | 11:00 | 11.1.1 |
AN EXPLORATION OF EVOLUTION PATHS FOR AIR TRANSPORTATION NETWORKS J.-H. Lewe¹, K. Song¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States | ||||
| 11:00 | 11:30 | 11.1.2 |
A REVIEW AND A CLASSIFICATION SCHEME FOR AIR TRANSPORTATION NETWORK RESEARCH K. Song¹, J.-H. Lewe¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States | ||||
| 11:30 | 12:00 | 11.1.3 |
AUTOMATED SEPARATION ASSURANCE AND COLLISION AVOIDANCE FUNCTIONS IN THE CNS+A CONTEXT S. Ramasamy¹, R. Sabatini¹, Y. Lim¹, A. Gardi¹; ¹RMIT University, Australia | ||||
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| 10:30 | 11:00 | 12.1.1 |
RTO\'S AND TECHNOLOGY DE-RISKING I. Potter, National Research Council Canada, Canada | ||||
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| 13:00 | 13:30 | 1.2.1 |
TOWARDS THE 3RD GENERATION MDO COLLABORATIVE ENVIRONMENT P.D. Ciampa¹, B. Nagel¹; ¹German Aerospace Center, DLR, Germany | ||||
| 13:30 | 14:00 | 1.2.2 |
STRUCTURAL CONSTRAINTS INVESTIGATION IN WING AERODYNAMIC/STRUCTURAL OPTIMIZATION K.-S. Zhang¹, H. Zhang¹, Z.-H. Han¹; ¹Northwestern Polytechnical University, China | ||||
| 14:00 | 14:30 | 1.2.3 |
MULTIDISCIPLINARY DESIGN OPTIMIZATION FOR FIGHTER AIRCRAFT CONFIGURATION C. Lee, Korea Aerospace Industries, LTD., South Korea | ||||
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| 13:00 | 13:30 | 2.2.1 |
APPLICATION OF PROPER ORTHOGONAL DECOMPOSITION FOR AVIATION SAFETY J.H. Cho¹, S.K. Jeong, Kyung Hee University, South Korea; K.J. Yee¹; ¹Seoul National University, South Korea | ||||
| 13:30 | 14:00 | 2.2.2 |
LARGE-SCALE VORTEX STRUCTURE OF FLOW IN THE NEAR WAKE BEHIND AN AIRLINER DURING TAKEOFF AND LANDING Y.M. Tsirkunov¹, M.A. Lobanova¹, A.I. Tsvetkov², B.A. Schepanyuk²; ¹Baltic State Technical University, Russia ;²Saint Petersburg State University, Russia | ||||
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| 13:00 | 13:30 | 3.2.1 |
INLET DUCT ENGINE TEST FACILITIES IN INDONESIA LOW SPEED TUNNEL (ILST) S. Subagyo, BBTA3-BPPT, Indonesia | ||||
| 13:30 | 14:00 | 3.2.2 |
AERODYNAMIC TESTING OF HELICOPTER NOVEL AIR INTAKES F. Knoth¹, C. Breitsamter¹; ¹Chair of Aerodynamics and Fluid Mechanics, TU Munich, Germany | ||||
| 14:00 | 14:30 | 3.2.3 |
KAI SURION HELICOPTER FULL-SCALE AIR INTAKE TESTING AT CIRA ICING WIND TUNNEL A.C. de Bruin, NLR, Netherlands; G. Fatigati, CIRA, Italy; H.B. Shin, KAI, South Korea | ||||
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| 13:00 | 13:30 | 4.2.1 |
THE EFFECT OF LEADING EDGE ROUNDING ON A CARET WAVERIDER CONFIGURATION AT MACH 8.2 B. McCartney¹, S. Prince¹, N. Qin, University of Sheffield, United Kingdom; ¹Cranfield University, United Kingdom | ||||
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| 13:00 | 13:30 | 5.2.1 |
SPECIAL CONSIDERATIONS TO THERMAL BEHAVIOR MODELING AND SIMULATION OF AN AEROSPACE ELECTROMECHANICAL ACTUATION SYSTEM J. Fu¹, Y. Fu¹, J.-C. Mare, Institut Clément Ader, INSA-Toulouse, France; ¹Beihang University, China | ||||
| 13:30 | 14:00 | 5.2.2 |
COUPLED EMC-THERMAL MODELING OF ELECTRICAL HARNESSES WITHIN "MORE ELECTRICAL AIRCRAFT" F. Mahiddini¹, M. Ridel¹, P. Reulet¹, D. Donjat¹, P. Millan¹; ¹ONERA, France | ||||
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| 13:00 | 13:30 | 6.2.1 |
UNSTEADY AERODYNAMIC FORCE SENSING FROM MEASURED STRAIN C.-G. Pak, NASA Armstrong Flight Research Center, United States | ||||
| 13:30 | 14:00 | 6.2.2 |
NONLINEAR DAMAGE MODELING AND ANALYSIS OF VISCOPLASTIC COMPOSITE MATERIALS I.K. Park¹, T.-U. Kim¹, S.-H. Kim¹; ¹KARI, South Korea | ||||
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| 13:00 | 13:30 | 7.2.1 |
MISSION BASED COMPARISON OF SINGLE- AND COUNTER-ROTATING FAN DESIGNS T. Otten¹, T. Lengyel-Kampmann¹; ¹German Aerospace Center (DLR), Germany | ||||
| 13:30 | 14:00 | 7.2.2 |
AERODYNAMIC OPTIMIZATION OF AIRPLANE PROPULSION SYSTEM WITHIN THE FRAMEWORK OF AGILE PROJECT K. Anisimov¹, A.A. Savelyev¹; ¹TsAGI, Russia | ||||
| 14:00 | 14:30 | 7.2.3 |
APPLICATION OF FLAME MEASUREMENT TECHNIC BY DENSELY INSTALLED ION-PROBES ON 2-STROKE GASOLINE ENGINE T. Yatsufusa¹, K. Takatani¹, S. Miyata¹; ¹Hiroshima Institute of Technology, Japan | ||||
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| 13:00 | 13:30 | 8.2.1 |
MISSILE AUTOPILOT DESIGN USING CONTRACTION THEORY-BASED OUTPUT FEEDBACK CONTROL H.-H. Kwon¹, H.-L. Choi¹; ¹KAIST, South Korea | ||||
| 13:30 | 14:00 | 8.2.2 |
FLIGHT CONTROL LAW CLEARANCE USING WORST-CASE INPUTS J. Diepolder¹, J.Z. Ben-Asher, Faculty of Aerospace Engineering - Technion, Israel; A. Gabrys¹, S. Schatz¹, M. Bittner¹, M. Rieck¹, B. Grüter¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics - TUM, Germany | ||||
| 14:00 | 14:30 | 8.2.3 |
AN INVESTIGATION OF EFFECTS OF FLIGHT MANEUVERS ON A SUPERSONIC AIRCRAFT WITH HORIZONTAL TAIL ACTUATOR FAILURE S. Oh¹, I. Cho¹, C. McLaughlin, The University of Kansas, United States; ¹Korea Aerospace Industries, LTD, South Korea | ||||
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| 13:00 | 13:30 | 9.2.1 |
GUIDANCE AND CONTROL OF AUTOMATIC SHORT LANDING WITH STEEP GLIDE SLOPE FOR UAV J. Moon¹, S. Choi¹, S. Cho¹, H. Kim¹; ¹KOREANAIR, South Korea | ||||
| 13:30 | 14:00 | 9.2.2 |
NONLINEAR DYNAMIC INVERSION WITH NEURAL NETWORKS FOR THE FLIGHT CONTROL OF A LOW COST TILT ROTOR UAV E. D\'Amato¹, G. Tartaglione, University of Naples Parthenope, Italy; L. Blasi¹, M. Mattei¹; ¹Second University of Naples, Italy | ||||
| 14:00 | 14:30 | 9.2.3 |
DEPTH IMAGE BASED DIRECT SLAM FOR SMALL UAVS S.Y. Park¹, D.H. Shim¹; ¹KAIST, South Korea | ||||
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| 13:00 | 13:30 | 10.2.1 |
EXPERIMENTAL STUDY ON AERODYNAMIC LOAD CONTROL USING SYNTHETIC JET ACTUATORS T.A. Berk¹, H.W.M. Hoeijmakers¹; ¹University of Twente, Netherlands | ||||
| 13:30 | 14:00 | 10.2.2 |
NUMERICAL SIMULATION OF FLOW SEPARATION CONTROL OVER A HUMP USING DBD PLASMA ACTUATOR A. Jahangirian¹, R. Khoshkhoo¹; ¹Amirkabir University of Technology, Iran | ||||
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| 13:00 | 13:30 | 11.2.1 |
PLANNING AIR TEAM MISSIONS WITH MULTIPLE OBJECTIVES T. Erlandsson, University of Skövde, Sweden | ||||
| 13:30 | 14:00 | 11.2.2 |
APPLYING REQUIRED NAVIGATION PERFORMANCE CONCEPT FOR TRAFFIC MANAGEMENT OF SMALL UNMANNED AIRCRAFT SYSTEMS J. Jung¹, S.N. D\'Souza¹, M.A. Johnson¹, A.K. Ishihara², H.C. Modi², B. Nikaido³, H. Hasseeb³; ¹NASA Ames Research Center, United States ;²SGT Inc., United States ;³Science & Technology Corp., United States | ||||
| 14:00 | 14:30 | 11.2.3 |
INFLUENCE OF AIRCRAFT TYPE AND ORDER ON FUEL SAVINGS GAINED BY TWO-AIRCRAFT FORMATIONS T. Marks¹, V. Gollnick¹; ¹German Aerospace Center, Germany | ||||
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| 13:00 | 13:30 | 12.2.1 |
KNOWLEDGE-BASED INTEGRATED AIRCRAFT WINDSHIELD OPTIMIZATION R.C. Munjulury¹, R. Gårdhagen¹, P. Berry¹, P. Krus¹; ¹Linköping University, Sweden | ||||
| 13:30 | 14:00 | 12.2.2 |
OPTIMISATION OF A WING-BODY-TAIL CONFIGURATION WITH AN ALTERNATIVE LOW DRAG FUSELAGE AND BODY TRAILING EDGE L. Smith¹, K.J. Craig¹, J.P. Meyer¹, G.R. Spedding, University of Southern California, United States; ¹University of Pretoria, South Africa | ||||
| 14:00 | 14:30 | 12.2.3 |
DESIGN OPTIMIZATION OF HELICOPTER BLADE USING CLASS SHAPE FUNCTION BASED GEOMETRY REPRESENTATION A. Ariyarit¹, M. Sugiura², Y. Tanabe², M. Kanazaki¹; ¹Tokyo Metropolitan University, Japan ;²Japan Aerospace Exploration Agency, Japan | ||||
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| 10:00 | 10:30 | 1.3.1 |
KNOWLEDGE-BASED FUTURE COMBAT AIRCRAFT OPTIMIZATION R.C. Munjulury¹, A.M. Abdalla, University of São Paulo, Brazil; I. Staack¹, P. Krus¹; ¹Linköping University, Sweden | ||||
| 10:30 | 11:00 | 1.3.2 |
COLLABORATIVE AIRCRAFT DESIGN USING AN INTEGRATED AND DISTRIBUTED MULTIDISCIPLINARY PRODUCT DEVELOPMENT PROCESS E. Moerland¹, S. Deinert², F. Daoud², J. Dornwald², B. Nagel¹; ¹German Aerospace Centre (DLR), Germany ;²Airbus Defence & Space, Germany | ||||
| 11:00 | 11:30 | 1.3.3 |
USING OPENVSP IN A CONCEPTUAL AIRCRAFT DESIGN ENVIRONMENT IN MATLAB S. Herbst¹, A. Staudenmaier¹; ¹Technical University of Munich / Institute of Aircraft Design, Germany | ||||
| 11:30 | 12:00 | 1.3.4 |
INTEGRATED CONCEPTUAL DESIGN METHOD CONSIDERING ADVANCED AIRCRAFT SYSTEMS AND AIRCRAFT TRAJECTORY T. Chiba¹, K. Rinoie¹; ¹The University of Tokyo, Japan | ||||
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| 10:00 | 10:30 | 3.3.1 |
AN EXPERIMENTAL INVESTIGATION ON THE FREESTREAM TURBULENCE UPSTREAM OF A SWEPT WING I. Fumarola, City University London, United Kingdom | ||||
| 10:30 | 11:00 | 3.3.2 |
EFFECTS OF REYNOLDS NUMBER ON THE ONSET OF LEADING EDGE VORTEX SEPARATION ABOVE BLUNT-EDGE DELTA WING VFE-2 CONFIGURATIONS M. Said¹, S. Mat¹; ¹AeroLab, Universiti Teknologi Malaysia, Malaysia | ||||
| 11:00 | 11:30 | 3.3.3 |
LOW ORDER MODELING OF THE UNSTEADY AND 3D EFFECTS OF CONTINUOUS WAKE FLAPPING FLIGHT A. Matta¹, J. Bayandor¹; ¹Virginia Tech, United States | ||||
| 11:30 | 12:00 | 3.3.4 |
EFFECTS OF PROPELLER LOCATIONS ON THE VORTEX SYSTEM ABOVE DELTA-SHAPED UAV MODEL K.A. Kasim¹, S. Mat¹, I.S. Ishak¹, M. Said¹; ¹Universiti Teknologi Malaysia, Malaysia | ||||
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| 10:00 | 10:30 | 4.3.1 |
SIMULATION OF UNSTEADY SHIP AIRWAKES USING OPENFOAM W. Yuan¹, R. Lee¹, A. Wall¹; ¹National Research Council Canada, Canada | ||||
| 10:30 | 11:00 | 4.3.2 |
EXTRACTION OF LINEAR INFLOW MODEL FOR MANEUVERING HELICOPTER FROM FREE-WAKE ANALYSIS O. Rand¹, V. Khromov¹; ¹Israel Institute of Technology, Israel | ||||
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| 10:00 | 10:30 | 5.3.1 |
TRANSFORMING MILITARY AEROSPACE SUSTAINMENT D. Holmes¹, A. Goodwin¹, R. Vodicka¹; ¹DSTG, Australia | ||||
| 10:30 | 11:00 | 5.3.2 |
LCC ESTIMATION AND CASE STUDY USING RELIABILITY AND MAINTAINABILITY ANALYSIS S.-Y. Lee, Korean Air, South Korea | ||||
| 11:00 | 11:30 | 5.3.3 |
INVESTIGATIONS OF GROUND INFRASTRUCTURES FOR UAS FLIGHT MONITORING S. Cresto Aleina¹, R. Fusaro¹, N. Viola¹; ¹Politecnico di Torino, Italy | ||||
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| 10:00 | 10:30 | 6.3.1 |
WEIGHT REDUCTION OF CYLINDRICAL GRID STRUCTURES USING AXIAL-HELICAL-DESIGN M. Beerhorst¹, C. Hühne¹; ¹DLR, Germany | ||||
| 10:30 | 11:00 | 6.3.2 |
CHAOS THEORY APPLIED TO BUCKLING ANALYSIS OF COMPOSITE CYLINDRICAL SHELL M. Alfano, Politecnico di Milano, Italy; C. Bisagni, Delft University of Technology, Netherlands | ||||
| 11:00 | 11:30 | 6.3.3 |
DEVELOPMENT OF LIGHTWEIGHT AND RELIABLE JOINTS FOR AIRFRAMES BASED ON UNIDIRECTIONAL COMPOSITE ELEMENTS A.N. Shanygin¹, A.V. Chernov¹, D.Y. Fomin¹, V.I. Grishin, TsAGI, Russia; I.N. Kacharava¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia | ||||
| 11:30 | 12:00 | 6.3.4 |
PANEL VIBRO-ACOUSTIC RESPONSE PREDICTION BASED ON TURBULENT BOUNDARY LAYER MEASUREMENT X.J. Zhao¹, B. Ai¹; ¹China Academy of Aerospace Aerodynamics, China | ||||
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| 10:00 | 10:30 | 7.3.1 |
MULTI-POINT DESIGN OPTIMIZATION OF A HIGH BYPASS RATIO FAN BLADE S. Qiu¹, X.Y. Deng¹; ¹AVIC Commercial Aircraft Engine CO.LTD, China | ||||
| 10:30 | 11:00 | 7.3.2 |
DEVELOPMENT OF THE FAN STAGE WITH ULTRA-LOW ROTATIONAL SPEED S.V. Pankov, CIAM , Russia; V.I. Mileshin¹, I.K. Orekhov¹, V.A. Fateev¹; ¹CIAM, Russia | ||||
| 11:00 | 11:30 | 7.3.3 |
ADVANCED PROPULSION COLLISION DAMAGE DUE TO UNMANNED AERIAL SYSTEM INGESTION Y.K. Song¹, K. Schroeder¹, B. Horton¹, J. Bayandor¹; ¹Virginia Tech, United States | ||||
| 11:30 | 12:00 | 7.3.4 |
MULTI-DISCIPLINARY DESIGN OF HIGH-SPEED COMPRESSORS FOR PROSPECTIVE TURBO-SHAFT ENGINE A.N. Startsev¹, Y.M. Temis¹, E.G. Steshakov¹, D.A. Yakushev¹; ¹CIAM, Russia | ||||
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| 10:00 | 10:30 | 8.3.1 |
PRECISION LANDING BASED ON ATMOSPHERIC DISTURBANCE MONITORING AND MODEL PREDICTIVE CONTROL N. Siepenkötter¹, D. Moormann¹; ¹RWTH Aachen University, Germany | ||||
| 10:30 | 11:00 | 8.3.2 |
ELASTIC MODES ADAPTIVE CANCELLATION ALGORITHM FOR THE A330 MRTT FLYING BOOM CONTROL LAWS R. Rodríguez Robles¹, A. Sanz de Blas¹; ¹Airbus Defence & Space, Spain | ||||
| 11:00 | 11:30 | 8.3.3 |
ON STABILITY MARGIN OF A LQR-BASED VEHICLE NETWORK Y. Kim¹, G. Seo¹; ¹Gyeongsang National University, South Korea | ||||
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| 10:00 | 10:30 | 9.3.1 |
LAND-BASED FLIGHT TEST FOR SHIPBOARD LANDING OF TILT ROTOR UAV C.-S. Yoo¹, E.-Y. Jang¹, B.-S. Song¹, A. Cho¹, B.-J. Park¹, Y.-S. Kim¹, Y.-S. Kang¹, S.-O. Koo¹; ¹Korea Aerospace Research Institute, South Korea | ||||
| 10:30 | 11:00 | 9.3.2 |
ANALYSIS ON OFFLINE AND ONLINE IDENTIFICATION METHODS FOR AIRCRAFT STABILITY AND CONTROL DERIVATIVES D. Ding¹, W.Q. Qian¹, Q. Wang¹; ¹Computational Aerodynamics Institute of CARDC, China | ||||
| 11:00 | 11:30 | 9.3.3 |
FLIGHT PATH RECONSTRUCTION FOR AN UNMANNED AERIAL VEHICLE USING LOW-COST SENSORS C. Göttlicher¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, TU Munich, Germany | ||||
| 11:30 | 12:00 | 9.3.4 |
SYSTEM IDENTIFICATION OF A SCALE HELICOPTER IN HOVERING FLIGHT F.C. Reis¹, E.M. Belo¹; ¹Escola de Engenharia de São Carlos - USP, Brazil | ||||
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| 10:00 | 10:30 | 10.3.1 |
ACTIVE VORTEX FLOW CONTROL ON A GENERIC DELTA WING A. Buzica¹, J. Bartasevicius¹, C. Breitsamter¹; ¹Chair of Aerodynamics and Fluid Mechanics, TUM, Germany | ||||
| 10:30 | 11:00 | 10.3.2 |
EFFECTIVENESS OF VORTEX GENERATORS IN HIGHLY 3D FLOWS H.S. Mudhar, City University London, United Kingdom | ||||
| 11:00 | 11:30 | 10.3.3 |
EXPERIMENTAL INVESTIGATION OF FLOW AROUND AIRFOILS WITH UNDULATING LEADING EDGES J. Pellicer, City University London, United Kingdom | ||||
| 11:30 | 12:00 | 10.3.4 |
AN EXPERIMENTAL AND COMPUTATIONAL STUDY OF THE AERODYNAMIC CHARACTERISTICS AN OSCILLATORY PITCHING NACA0012 AEROFOIL A. Yadav¹, S. Prince¹, J. Holt¹; ¹Cranfield University, United Kingdom | ||||
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| 10:00 | 10:30 | 11.3.1 |
AN INTERFACE CONCEPT TO SUPPORT THE COCKPIT CREW DURING TRAJECTORY-BASED DISPATCH TOWING T. Bernatzky¹, S. Baumann¹, U. Klingauf¹; ¹Technische Universitaet Darmstadt, Germany | ||||
| 10:30 | 11:00 | 11.3.2 |
IMPROVEMENT OF PUSHBACK TIME ASSIGNMENT UNDER UNCERTAINTIES R. Mori, Electronic Navigation Research Institute, Japan | ||||
| 11:00 | 11:30 | 11.3.3 |
TAXIING ROUTE PLANNING BASED ON AIRPORT HOTSPOTS W.J. Pan¹, X. Wang¹, X.L. Luo, NORTHWEST AIR TRAFFIC CONTROL BUREAU OF CIVIL AVIATION OF CHINA, China; ¹CIVIAL AVIATION FLIGHT UNVIERSITY OF CHINA, China | ||||
| 11:30 | 12:00 | 11.3.4 |
SENSOR CONCEPT OF HIGHLY-AUTOMATED AIRPORT TUGS FOR REDUCED EMISSION TAXI OPERATIONS S. Frank¹, P.M. Schachtebeck¹, P. Hecker¹; ¹TU Braunschweig, Institute of Flight Guidance, Germany | ||||
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| 10:00 | 10:30 | 12.3.1 |
A STUDY ON FAILURE BEHAVIORS OF REPAIRED COMPOSITE STRUCTURES WITH SCARF BONDED PATCH K.H. Nguyen¹, V.H. Truong¹, J.H. Kweon¹; ¹Gyeongsang National University, South Korea | ||||
| 10:30 | 11:00 | 12.3.2 |
RESEARCH ON VIBRATION CHARACTERISTIC FOR VARIABLE ROTATING VELOCITY BLADES J. Qin¹, B.-W. Wang¹; ¹ASRI, China | ||||
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| 14:00 | 14:30 | 1.4.1 |
A CONCEPTUAL DESIGN PLATFORM FOR BLENDED-WING-BODY TRANSPORTS M. Zhang¹, Z. Chen¹, B. Zhang¹; ¹Northwestern Polytechnical University, China | ||||
| |||||||
| 14:00 | 14:30 | 2.4.1 |
DYNAMICS MODELLING FOR CONTROL OF AN UNSTEADY HYDRODYNAMIC STINGRAY ROBOT B. Gater, Virginia Tech , United States; J. Bayandor, Virginia Tech, United States | ||||
| 14:30 | 15:00 | 2.4.2 |
COMPUTATIONAL INVESTIGATION FOR FREE-FLIGHT AERODYNAMICS AND FLIGHT DYNAMICS OF SUBSONIC AND SUPERSONIC PROJECTILES Q. Zhang¹, Z. Ye¹, S. Wang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | ||||
| 15:00 | 15:30 | 2.4.3 |
STORE SEPARATION FROM WEAPON BAYS M. Tutty, JAIME Enterprises Australia, Australia; G. Akroyd, Akroyd Aeronautics, Australia; A. Cenko¹, A. Piranian¹; ¹AIWS LLC, United States | ||||
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| 14:00 | 14:30 | 3.4.1 |
HYPERPARAMETERS OPTIMIZATION FOR ADAPTIVE DESIGN OF EXPERIMENTS APPLIED TO WIND TUNNEL TESTING H. Jin¹, D. Lee¹, J. Lee¹, J. Ahn¹; ¹Department of Aerospace Engineering, KAIST, South Korea | ||||
| 14:30 | 15:00 | 3.4.2 |
DESIGN AND TEST OF THE HIGH AERODYNAMIC PERFORMANCE LOW-NOISE FAN FOR 5.5- BY 4-M ACOUSTIC WIND TUNNEL X. Qu¹, Y. Yu¹, D. Liao¹, G. Yang¹, Q. Chen¹, G. Tang¹; ¹CARDC, China | ||||
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| 14:00 | 14:30 | 4.4.1 |
LOW REYNOLDS PROPELLER META-MODEL FOR MULTIDICIPLYNARY OPTIMIZATION V.D. Tavernari¹, F.M. Catalano¹; ¹Aeronautical Engineering Department _EESC-USP, Brazil | ||||
| 14:30 | 15:00 | 4.4.2 |
DISTRIBUTED PROPELLERS SLIPSTREAM EFFECTS ON WING AT LOW REYNOLDS NUMBER K. Wang¹, X.P. Zhu¹, Z. Zhou¹; ¹NWPU University, China | ||||
| 15:00 | 15:30 | 4.4.3 |
NUMERICAL SIMULATION OF THE PROPELLER/WING INTERACTIONS AT LOW REYNOLDS NUMBER H.-B. Wang¹, X.-P. Zhu, UAV Laboratory, Northwestern Polytechnical University, China; Z. Zhou¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | ||||
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| 14:00 | 14:30 | 5.4.1 |
EXPERIMENTAL AND SIMULATION STUDY OF THE DYNAMICS OF AN ELECTRO-MECHANICAL LANDING GEAR ACTUATOR G. Di Rito¹, R. Galatolo¹, F. Schettini¹; ¹Università di Pisa - Dip. Ingegneria Civile ed Industriale, Italy | ||||
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| 14:00 | 14:30 | 6.4.1 |
MULTIDISCIPLINARY DESIGN CHAIN FOR MODEL ROTOR BLADES B. van de Kamp¹, S. Kalow¹, J. Riemenschneider¹, R. Bartels¹, H. Mainz¹; ¹German Aerospace Center (DLR), Germany | ||||
| 14:30 | 15:00 | 6.4.2 |
NUMERICAL INVESTIGATION OF FAN-BLADE OUT USING MESO-SCALE COMPOSITE MODELING B. Horton¹, J. Bayandor¹; ¹Virginia Tech, United States | ||||
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| 14:00 | 14:30 | 7.4.1 |
INTEGRATION OF HYBRID PROPULSION SYSTEM IN A CS23 COMMUTER DESIGN M. Strack¹, T. Zill¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany | ||||
| 14:30 | 15:00 | 7.4.2 |
INVESTIGATION OF CHARACTERISTICS OF THE OIL SYSTEM WITH ELECTRICALLY DRIVEN PUMPS FOR GAS TURBINE ENGINE Y.M. Shchurovskiy, Central Institute of Aviation Motors (CIAM), Russia | ||||
| 15:00 | 15:30 | 7.4.3 |
METHODS FOR IMPROVING THE RELIABILITY OF FUEL SUPPLY SYSTEM OF GAS TURBINE ENGINES WITH USING ELECTRICALLY DRIVEN PUMPS O.S. Gurevich¹, A.I. Gulienko¹; ¹Central Institute of Aviation Motors (CIAM), Russia | ||||
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| 14:00 | 14:30 | 8.4.1 |
FLIGHT DYNAMIC STABILITY ANALYSIS OF A FLEXIBLE FLYING WING L. Wang, China; C. Tang, China | ||||
| 14:30 | 15:00 | 8.4.2 |
BIFURCATION ANALYSIS OF A GENERIC PUSHER TYPE TRANSPORT AIRCRAFT CONFIGURATION IN NEAR-STALL FLIGHT A.K. Khatri¹, V. Kumar¹; ¹CSIR-NAL, India | ||||
| 15:00 | 15:30 | 8.4.3 |
HEURISTIC MODEL OF NON-STEADY LONGITUDINAL AERODYNAMIC CHARACTERISTICS AT HIGH ANGLES OF ATTACK P.V. Kuzmin¹, B.A. Meleshin¹, Y.F. Shelyukhin¹, D.V. Shukhovtsov¹; ¹TsAGI, Russia | ||||
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| 14:00 | 14:30 | 9.4.1 |
OVERVIEW OF THE INVERTED JOINED WING SCALED DEMONSTRATOR PROGRAMME C. Galinski¹, W. Stalewski¹, M. Lis¹, J. Hajduk, Air Force Institute of Technology, Poland; ¹Institute of Aviation, Poland | ||||
| 14:30 | 15:00 | 9.4.2 |
IS TO BE THE MICRODRONE M. Babiak¹, A. Garstka¹, M. Mazur¹, I. Skawinski¹; ¹Warsaw University of Technology, Poland | ||||
| 15:00 | 15:30 | 9.4.3 |
STRATEGIES FOR MANUAL LANDING OF REMOTELY PILOTED AIRPLANES WITH LARGE TIME DELAY T. Fricke¹, F. Holzapfel¹; ¹Technische Universität München, Germany | ||||
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| 14:00 | 14:30 | 10.4.1 |
INFLUENCE OF SURFACE FRACTAL MICROSTRUCTURE ON THE CHARACTERISTICS OF A TURBULENT BOUNDARY LAYER M.A. Brutyan¹, V.P. Budaev, NRCKI, Russia; A.V. Wolkov¹; ¹TsAGI, Russia | ||||
| 14:30 | 15:00 | 10.4.2 |
GEOMETRIC ROUGHNESS EFFECTS ON THE AERODYNAMIC CHARACTERISTICS OF A SPINNING CYLINDER IN CROSSFLOW S. Prince¹, J. Holt¹, P. Episkopou¹; ¹Cranfield University, United Kingdom | ||||
| 15:00 | 15:30 | 10.4.3 |
STAGGERED THREE-DIMENSIONAL CAVITIES AS A POSSIBLE METHOD FOR SKIN FRICTION DRAG REDUCTION E.R. Gowree¹, C.J. Atkin¹; ¹City University London, United Kingdom | ||||
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| 14:00 | 14:30 | 11.4.1 |
CONCEPT OF OPERATIONS OF AN ATC TOOL FOR TRAJECTORY OPTIMISATION A. Spiteri¹, K. Chircop¹, D. Zammit-Mangion¹, A. Muscat², K. Falzon², J. Degiorgio³, F. Bezzina³; ¹University of Malta, Malta ;²Quaero Ltd., Malta ;³Malta Air Traffic Services Ltd., Malta | ||||
| 14:30 | 15:00 | 11.4.2 |
FLEET DEVELOPMENT PLANNING OF AIRLINES: INCORPORATING THE AIRCRAFT OPERATING ECONOMICS FACTOR O. Oguntona, Munich Aerospace e.V., Germany; A. Cui, Technische Universität München, Germany; K. Ploetner¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany | ||||
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| 14:00 | 14:30 | 12.4.1 |
DETERMINATION OF DESIGN ALLOWABLES FOR AIRCRAFT COMPOSITE STRUCTURES J.Y. Choung¹, J.W. Kim¹, I.H. Hwang¹; ¹Korea Aerospace Research Institute, South Korea | ||||
| 14:30 | 15:00 | 12.4.2 |
A STRESS INTENSITY FACTOR SOLUTION INSPIRED BY SOAP BUBBLES FRAMEWORK R. de Moura Pinho¹, D. Soria¹, L. Dimithe Aboumou¹; ¹Safran Aircraft Engines, France | ||||
| 15:00 | 15:30 | 12.4.3 |
ESTIMATION OF TEMPERATURE-DEPENDANT THERMAL CONDUCTIVITY OF MATERIAL WITH GENETIC ALGORITHM Q. Wei-qi¹, Z. Yu¹; ¹CARDC, China | ||||
| |||||||
| 16:00 | 16:30 | 1.5.1 |
USING INTERNATIONAL COLLABORATIVE AIRCRAFT DESIGN PROJECTS TO ENHANCE UNDERGRADUATE DESIGN EDUCATION: LESSONS LEARNED P. Raj, Virginia Polytechnic Institute & State University, United States; J. Abulawi, Hochschule für Angewandte Wissenschaften, Germany | ||||
| 16:30 | 17:00 | 1.5.2 |
STUDENT DESIGN PROCESSES IN INTERDISCIPLINARY COLLABORATION ACTIVITIES IN AERONAUTICS ENGINEERING EDUCATION J. Kimura, The University of Tokyo, Japan | ||||
| 17:00 | 17:30 | 1.5.3 |
AIRCRAFT DESIGN EDUCATION FOR UNDERGRADUATE AND GRADUATE STUDENTS AT THE UNIVERSITY OF TOKYO K. Rinoie, The University of Tokyo, Japan | ||||
| 17:30 | 18:00 | 1.5.4 |
THE COLLABORATIVE ENGINEER: HOW EDUCATION SHOULD BRING FORTH THE NEW GENERATION OF ENGINEERS E. Moerland, German Aerospace Center (DLR), Germany; B. Nagel, German Aerospace Centre (DLR), Germany | ||||
| |||||||
| 16:00 | 16:30 | 2.5.1 |
MODELLING NONLINEAR HIGH-PRECISION UNSTEADY AERODYNAMICS FOR ADVANCED AIRCRAFT AT HIGH ANGLE OF ATTACK B.-G. Mi¹, H. Zhan¹, M.-H. Yang¹; ¹Northwestern Polytechnical University, China | ||||
| 16:30 | 17:00 | 2.5.2 |
EFFECTS OF THE BOUNDARY LAYER TRANSITION ON THE GLOBAL AERODYNAMIC COEFFICIENTS G.L.O. Halila¹, A.P. Antunes¹, R.G. da Silva², J.L.F. Azevedo²; ¹Embraer S.A., Brazil ;²Instituto de Aeronautica e Espaco, Brazil | ||||
| 17:00 | 17:30 | 2.5.3 |
EFFECTS OF SOME NUMERICAL FORMULATION ASPECTS IN HIGH-LIFT CONFIGURATION SIMULATIONS E.D.V. Bigarella¹, P.A.G. Ciloni¹, L.C. Scalabrin¹; ¹Embraer S.A., Brazil | ||||
| 17:30 | 18:00 | 2.5.4 |
CFD OF BLENDED WING BODY UCAV WITH VORTEX GENERATOR S. Park¹, K. Chang¹, d.-J. Sheen¹; ¹Hanseo University, South Korea | ||||
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| 16:00 | 16:30 | 3.5.1 |
NON-INTRUSIVE UNSTEADY PSP TECHNIQUE FOR INVESTIGATION OF TRANSONIC BUFFETING Y. Sugioka¹, K. Nakakita, JAXA, Japan; K. Asai¹; ¹Tohoku Univ., Japan | ||||
| 16:30 | 17:00 | 3.5.2 |
UNSTEADY AERODYNAMIC INFORMATION EXTRACTION USING FFT-BASED UNSTEADY PRESSURE-SENSITIVE PAINT MEASUREMENT K. Nakakita, Japan Aerospace Exploration Agency, Japan | ||||
| 17:00 | 17:30 | 3.5.3 |
EXPERIMENTAL STUDY OF GEOMETRIC VARIATIONS EFFECT ON THE FLOW PATTERNS ON A HAMMERHEAD SATELLITE LAUNCH VEHICLE J.G. Medeiros, Instituto Tecnológico de Aeronáutica, Brazil; A.C. Avelar, Instituto de Aeronautica e Espaço, Brazil; J.B.P. Falcão Filho, Instituto de Aeronáutica e Espaço, Brazil | ||||
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| 16:00 | 16:30 | 4.5.1 |
NUMERICAL SIMULATION OF DROPLET IMPINGEMENT ON A MULTI-ELEMENT HIGH-LIFT AIRFOIL L. Prince Raj¹, R.S. Myong¹; ¹Gyeongsang National University, South Korea | ||||
| 16:30 | 17:00 | 4.5.2 |
STRATEGIES FOR ACHIEVING BACKWARD FLIGHT BY A DRAGONFLY A.T. Bode-Oke¹, S. Zeyghami, Lehigh University, United States; H. Dong¹; ¹University of Virginia, United States | ||||
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| 16:00 | 16:30 | 5.5.1 |
SURROGATE MODELING TECHNIQUE FOR THE CONCEPTUAL AND PRELIMINARY DESIGN OF EMBEDDED ACTUATION SYSTEMS AND COMPONENTS F. Sanchez, Institut Clément Ader/Paul Sabatier University, France; S. Delbecq, Institut Clément Ader/Safran Electronics & Defense, France | ||||
| 16:30 | 17:00 | 5.5.2 |
SELECTION OF AN UAV CONFIGURATION LAYOUT FOR OPTIMISATION OF TELEDETECTION MISSION USING HYPERSPECTRAL SENSORS R. Fusaro¹, Z. Goraj, Warsaw University of Technology, Poland; N. Viola¹; ¹Politecnico di Torino, Italy | ||||
| 17:00 | 17:30 | 5.5.3 |
STATISTICAL MODELING OF AIRCRAFT ENGINE FUEL FLOW RATE Y.S. Chati¹, H. Balakrishnan¹; ¹Massachusetts Institute of Technology, United States | ||||
| 17:30 | 18:00 | 5.5.4 |
METHODS FOR AUTOMATING MODEL VALIDATION: STEADY-STATE IDENTIFICATION APPLIED ON GRIPEN FIGHTER ENVIRONMENTAL CONTROL SYSTEM MEASUREMENTS R. Hällqvist¹, M. Eek¹, R. Braun², P. Krus²; ¹Saab Aeronautics, Sweden ;²Linköping University, Sweden | ||||
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| 16:00 | 16:30 | 6.5.1 |
GENERATIVE DESIGN: ADVANCED DESIGN OPTIMIZATION PROCESSES FOR AERONAUTICAL APPLICATIONS S. Bagassi¹, F. Lucchi¹, F. De Crescenzio¹, F. Persiani¹; ¹University of Bologna, Italy | ||||
| 16:30 | 17:00 | 6.5.2 |
DESIGNING OF AIRFRAMES HAVING MINIMUM MASS UNDER SEVERAL LOADINGS (NOT ONLY FULLY STRESSED) A.I. Danilin, Samara State Aerospace University, Russia | ||||
| 17:00 | 17:30 | 6.5.3 |
APPLICATIONS OF DISPLACEMENT TRANSFER FUNCTIONS TO DEFORMED SHAPE PREDICTIONS OF THE G-III SWEPT-WING STRUCTURE S.-F. Lung, Jacobs, United States; W.L. Ko, NASA, United States | ||||
| 17:30 | 18:00 | 6.5.4 |
FAIRING OPTIMIZATION DESIGN OF WING STRUCTURE R. Zhang, Chinese Aeronautical Establishment, China; D.-G. Cui, Aviation of China, China; G. Song, Beihang University, China | ||||
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| 16:00 | 16:30 | 7.5.1 |
EFFECT OF REYNOLDS NUMBER, OPERATING MODE, TURBULENCE PARAMETERS ON PROFILE AND SECONDARY LOSSES OF LPT A.D. Nepomnyashchiy¹, S.V. Suntsov ¹, S.Y. Danilkin¹, V.P. Maslov¹; ¹Central Institute of Aviation Motors (CIAM), Russia | ||||
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| 16:00 | 16:30 | 8.5.1 |
STOCHASTIC TRANSONIC AERODYNAMICS ANALYSIS X. Wu, China; W. Zhang, China | ||||
| 16:30 | 17:00 | 8.5.2 |
MULTIDISCIPLINARY DESIGN OPTIMIZATION OF STRATOSPHERIC AIRSHIP M.I. Alam, Indian Institute of Technology Bombay, India | ||||
| 17:00 | 17:30 | 8.5.3 |
REDUCED ORDER MODELING OF AVIATION ENVIRONMENTAL DESIGN TOOL WITH PROPER ORTHOGONAL DECOMPOSITION AND KRIGING S. Kim¹, K. Lee¹; ¹Pusan National University, South Korea | ||||
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| 15:30 | 16:00 | 9.5.1 |
PLASTIC DEFORMATION OF POWDER METALLURGY TUNGSTEN ALLOY FOILS FOR SATELLITE ENCLOSURES M. Kanerva¹, E. Sarlin, Tampere University of Technology, Department of Material Science, Finland; A. Hållbro, Plansee SE, Sweden; J. Jokinen¹; ¹Aalto University, Department of Mechanical Engineering, Finland | ||||
| 16:00 | 16:30 | 9.5.2 |
MODERN MATERIALS IN AEROSPACE INDUSTRY - MAGNESIUM ALLOY CONTROL SYSTEM LEVER OF THE UNMANNED ILX - 27 HELICOPTER M. Wojtas¹, A. Sobieszek¹, L. Czajkowski¹, R. Zurawski¹; ¹Institute of Aviation, Poland | ||||
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| 16:00 | 16:30 | 10.5.1 |
EXPERIMENTAL STUDY OF AEROFOIL-WAKE INDUCED TRANSITION IN BOUNDARY LAYERS D. Veerasamy, United Kingdom | ||||
| 16:30 | 17:00 | 10.5.2 |
DISTURBANCES IN AN ACCELERATED BOUNDARY LAYER UNDER INFLUENCE OF MODERATE FREE-STREAM TURBULENCE D.S. Sboev, TsAGI, Russia | ||||
| 17:00 | 17:30 | 10.5.3 |
EFFECT OF A 3D INDENTATION ON BOUNDARY LAYER INSTABILITY H. Xu¹, S. Mughal¹, E.R. Gowree, Centre of Aeronautics,City University London, United Kingdom; S.-J. Sherwin, Department of Aeronautics, Imperial College London, United Kingdom; ¹Department of Mathematics,Imperial College London, United Kingdom | ||||
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| 16:00 | 16:30 | 11.5.1 |
ACOUSTICAL COMPARISON OF CONVENTIONAL TAXIING AND DISPATCH TOWING - TAXIBOT´S CONTRIBUTION TO GROUND NOISE ABATEMENT K. Hein¹, S. Baumann¹; ¹TU Darmstadt, Germany | ||||
| 16:30 | 17:00 | 11.5.2 |
QUANTITATIVE EMISSIONS OF NOX, CO AND CO2 DURING AIRCRAFT OPERATIONS P. Glowacki¹, M. Kawalec¹; ¹Institute of Aviation, Poland | ||||
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| 16:00 | 16:30 | 12.5.1 |
EXTENDED LOCAL SCATTERING THEORY AND THE ROLE OF A SCATTER ON BOUNDARY-LAYER INSTABILITY AND ACOUSTIC RADIATION M. Dong¹, X. Wu¹; ¹Imperial College London, United Kingdom | ||||
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| 09:30 | 10:00 | 1.6.1 |
COMMERCIAL DERIVATIVE AIRCRAFT AND TURBINE ENGINE I. Berlowitz, Israel Aerospace Industries, Israel | ||||
| 10:00 | 10:30 | 1.6.2 |
ENHANCING THE EXPLORATION OF AIRCRAFT CHANGEABILITY DURING CONCEPTUAL DESIGN A.S.J. van Heerden¹, M.D. Guenov¹, A. Molina-Cristobal¹, A. Riaz¹; ¹Cranfield University, United Kingdom | ||||
| 10:30 | 11:00 | 1.6.3 |
ROTORCRAFT SYSTEMS MODELLING FOR TWIN-ENGINE HEAVY HELICOPTER F. Hashim¹, C.P. Lawson¹, D.M. Judt¹; ¹Cranfield University, United Kingdom | ||||
| 11:00 | 11:30 | 1.6.4 |
IDENTIFYING THE BEST DESIGN FOR UNCERTAIN MARKETS A.A. Desai¹, P. Hollingsworth¹, P. Chinchapatnam, Rolls-Royce plc, United Kingdom; ¹University of Manchester, United Kingdom | ||||
| 11:30 | 12:00 | 1.6.5 |
DETAILED AERO-STRUCTURAL DESIGN OF WINGLET FOR BUSINESS JET N.R. El Haddad¹, L. Gonzalez¹; ¹EMBRY RIDDLE AERONAUTICAL UNIVERSITY, United States | ||||
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| 09:30 | 10:00 | 2.6.1 |
DEVELOPMENT OF HIGH-ORDER AND HIGH-RESOLUTION SCHEMES FOR EFFICIENT SHOCK CAPTURING IN HIGH-SPEED FLOWS M.H. Ahn¹, D.J. Lee¹; ¹Korea Advanced Institute of Science and Technolgy, South Korea | ||||
| 10:00 | 10:30 | 2.6.2 |
COMPUTATIONAL EFFICIENCY AND QUALITY OF DIFFERENT VERSIONS OF DISCONTINUOUS GALERKIN METHOD FOR LES/DES APPLICATIONS I. Bosnyakov¹, A.I. Troshin¹, V.V. Vlasenko¹, A.V. Wolkov¹; ¹TsAGI, Russia | ||||
| 10:30 | 11:00 | 2.6.3 |
EXTENDED VALIDATION OF A TRANSONIC LATTICEBOLTZMANN METHOD ON THE EXAMPLE OF THE NASA COMMON RESEARCH MODEL B. Koenig¹, A.F.P. Ribeiro¹, E. Fares¹, R. Zhang², P. Gopalakrishnan², Y. Li²; ¹Exa GmbH, Germany ;²Exa Corp., United States | ||||
| 11:00 | 11:30 | 2.6.4 |
EFFICIENT MULTI-RESOLUTION ANALYSIS FOR IMPLICIT TEMPORAL INTEGRATION S. Chae¹, H. Kang, Dongyang Mirae University, South Korea; S. Oh, Pusan National University, South Korea; K. Yee¹; ¹Seoul National University, South Korea | ||||
| 11:30 | 12:00 | 2.6.5 |
INFLUENCE OF THE RHOMBOID ZONE ON AEROELASTIC EXPERIMENTS OF SUPERSONIC AIRCRAFT Y.-G. Bai¹, W. Qian¹; ¹Dalian University of Technology, China | ||||
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| 09:30 | 10:00 | 3.6.1 |
FLOW CONTROL ON HELICOPTER-ROTOR BLADES VIA ACTIVE GURNEY FLAP W. Stalewski, INSTITUTE of AVIATION, Poland | ||||
| 10:00 | 10:30 | 3.6.2 |
STUDY ON THE SYSTEM INTEGRATION FOR MULTI-ELEMENT AIRFOIL AERODYNAMIC ANALYSIS D. Nam¹, J. Lee¹, B. KIim¹; ¹Chungnam National University, South Korea | ||||
| 10:30 | 11:00 | 3.6.3 |
THE INFLUENCE OF A LOCAL CHANGE IN WING DIHEDRAL ON THE LOW SPEED FLOW CHARACTERISTICS OF RECTANGULAR PLANFORM WINGS K.P. Garry¹, J.C. Holt¹, G. Tanguy¹, S.A. Prince¹; ¹Cranfield University, United Kingdom | ||||
| 11:00 | 11:30 | 3.6.4 |
IMPROVED DESIGN OF A HIGH LIFT SYSTEM FOR GENERAL AVIATION AIRCRAFT D. Florjancic¹, D. Steenhuizen¹, L.L.M. Veldhuis¹; ¹TU Delft, Netherlands | ||||
| 11:30 | 12:00 | 3.6.5 |
BROADBAND TRAILING-EDGE NOISE: A STATUS REPORT ON CURRENT PREDICTION CAPABILITIES M. Herr, German Aerospace Center (DLR), Germany | ||||
| |||||||
| 09:30 | 10:00 | 4.6.1 |
AERODYNAMIC SHAPES DESIGN ON THE BASE OF DIRECT NEWTON TYPE OPTIMIZATION METHOD A.V. Grachev¹, A.N. Kraiko, CIAM, Russia; S.A. Takovitskii¹; ¹TsAGI, Russia | ||||
| 10:00 | 10:30 | 4.6.2 |
CFD-BASED AERODYNAMIC SHAPE OPTIMIZATION OF A MANNED RE-ENTRY VEHICLE M.M. Entezari, Aerospace Research Institute, Iran; M. Mohammadi-Amin, Aerospace Research Institue, Iran | ||||
| 10:30 | 11:00 | 4.6.3 |
AERODYNAMIC SHAPE OPTIMIZATION WITH A NEW PARALLEL EVOLUTIONARY ALGORITHM AND NUMERICAL FLOW MODELLING A. Jahangirian¹, M. Ebrahimi¹; ¹Amirkabir University of Technology, Iran | ||||
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| 09:30 | 10:00 | 5.6.1 |
RESEARCH DEVELOPMENTS IN NONDESTRUCTIVE EVALUATION AND STRUCTURAL HEALTH MONITORING FOR THE SUSTAINMENT OF COMPOSITE AEROSPACE STRUCTURES AT NASA K.E. Cramer, NASA, United States | ||||
| 10:00 | 10:30 | 5.6.2 |
IN-FLIGHT VIBRATION-BASED STRUCTURAL HEALTH MONITORING OF AIRCRAFT WINGS E. Neu¹, F. Janser¹, A.A. Khatibi², A.C. Orifici²; ¹FH Aachen UAS, Germany ;²RMIT University, Australia | ||||
| 10:30 | 11:00 | 5.6.3 |
QUALIFICATION OF KAI KUH-1M ON BOARD ROKN SHIPS USING THE DUTCH APPROACH J. van der Vorst¹, P.J.A. Booij¹, J.F. Hakkaart¹, T.I. Lee, KAI, South Korea; ¹NLR, Netherlands | ||||
| 11:00 | 11:30 | 5.6.4 |
3D IMAGING OF GEOMETRICAL STRUCTURE AND DEFECT LOCATION OF INNER CAVITY IN AVIATION DEVICES BY POSITRON INJECTION H. Xiao, China; M. Zhao, China; M. Yao, China; J. Liu, China; H. Chen, China; M. Li, China; M. Du, China | ||||
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| 09:30 | 10:00 | 6.6.1 |
THE ACTIVE AEROELASTICITY CONCEPT - THE MAIN STAGES AND PROSPECTS OF DEVELOPMENT G.A. Amiryants, Russia; A.V. Grigorev, Russia; Y.A. Nayko, Russia; S.E. Paryshev, Russia | ||||
| 10:00 | 10:30 | 6.6.2 |
DESIGN, MANUFACTURE AND FREQUENCY EXPERIMENT OF A NOVEL FLUTTER MODEL FOR AGARD WING 445.6 WITH STRUCTURE-SIMILARITY W. Qian¹, Y.-G. Bai¹, D. Wang, AVIC Aerodynamics Research Institute, China; ¹Dalian University of Technology, China | ||||
| 10:30 | 11:00 | 6.6.3 |
FLUID-STRUCTURE INTERACTION ANALYSIS REGARDING THE INFLUENCE OF STRUCTURAL BOUNDARY CONDITION ON A FLAPPING WING H. Cho¹, N. Lee², S.J. Shin¹, S. Lee², S.Y. Kim, Agency for Defense Development, South Korea; ¹Seoul National Univ., South Korea ;²Inha Univ., South Korea | ||||
| 11:00 | 11:30 | 6.6.4 |
THE INFLUENCE OF MORPHING PROCESS ON THE AEROELASTIC CHARACTERISTICS OF A FOLDING WING W. Hu¹, Z.C. Yang¹, Y.S. Gu¹; ¹Northwestern Polytechnical University, China | ||||
| 11:30 | 12:00 | 6.6.5 |
UNCERTAINTY QUANTIFICATION AND GLOBAL SENSITIVITY ANALYSIS FOR HYPERSONIC AEROTHERMOELASTIC ANALYSIS K. Ye¹, Z.Y. Ye¹, Z.H. Chen¹, Z. Qu¹; ¹Northwestern Polytechnical University, China | ||||
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| 09:30 | 10:00 | 7.6.1 |
STUDY ON EFFICIENT FULL ANNULUS URANS COMPUTATIONS OF AN INTAKE COMPRESSOR CONFIGURATION T. Kächele¹, T. Schneider, MTU Aero Engines AG, Germany; R. Niehuis¹; ¹Universität der Bundeswehr, Germany | ||||
| 10:00 | 10:30 | 7.6.2 |
DESIGN AND DEVELOPMENT OF A MILITARY ENGINE INLET RESEARCH DUCT R.P.M. Rademakers¹, J.P. Haug¹, R. Niehuis¹, M. Stoeßel, Wehrtechnische Dienststelle für Luftfahrzeuge u Luftfahrtgeräte, Germany; ¹Institute of Jet Propulsion (UniBwM), Germany | ||||
| 10:30 | 11:00 | 7.6.3 |
ANALYSES OF AIRFLOW AROUND DUCTED FAN PROPULSION SYSTEM IN PUSHER CONFIGURATION USING PIV METHOD P. Ruchala¹, K. Bogdanski, Politechnika Warszawska, Poland; W. Stryczniewicz¹; ¹Instytut Lotnictwa, Poland | ||||
| 11:00 | 11:30 | 7.6.4 |
THE INVESTIGATION OF TIP CLEARANCE EFFECTS IN DUCTED ROTOR AERODYNAMIC CHARACTERISTICS USED IN UNMANNED AERIAL VEHICLES X. Li¹, Z. Guo¹, Z. Hou¹; ¹National University of Defense Technology, China | ||||
| 11:30 | 12:00 | 7.6.5 |
CHARACTERIZATION OF DISTORTED FLUID FLOW ALONG ADVANCED HIGH-BYPASS PROPULSION SYSTEM Y.K. Song¹, J. Bayandor¹; ¹Virginia Tech, United States | ||||
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| 09:30 | 10:00 | 8.6.1 |
SAMPLING-BASED MOTION PLANNING FOR COOPERATIVE AERIAL MANIPULATION H.I. Kim¹, H.B. Lee¹, H.J. Kim¹; ¹Seoul National Univ., South Korea | ||||
| 10:00 | 10:30 | 8.6.2 |
A NOVEL FLIGHT CONTORL ALGORITHM FOR MULTICOPTERS O. Tekinalp, Middle East Tecnical University, Turkey; S. Kumbasar, Middle East Technical University, Turkey | ||||
| 10:30 | 11:00 | 8.6.3 |
DESIGN THE GUIDANCE LAW FOR FORMATION FLIGHT OF MULTIPLE UAVS H. Shin¹, H. Kim¹, J. Lee¹, D.H. Shim¹; ¹Korea Advance Institute of Science and Technology, South Korea | ||||
| 11:00 | 11:30 | 8.6.4 |
NON-COOPERATIVE GROUND VEHICLE TRACKING AND INTERCEPTION BY MULTI-RPA COLLABORATION Y. Watanabe¹, A. Manecy¹, A. Amiez¹, C. Lesire¹, C. Grand¹; ¹ONERA, France | ||||
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| 09:30 | 10:00 | 9.6.1 |
APPROXIMATE THREE-DIMENSIONAL PATH GENERATION FOR UAV PATH-FOLLOWING N. Cho, South Korea; Y. Kim, South Korea | ||||
| 10:00 | 10:30 | 9.6.2 |
DEVELOPMENT OF PEST\'S BIOLOGICAL CONTROL TOOL USING VTOL UAV SYSTEMS R.K. Rangel, BRVANT / BRV UAV& Flight Systems, Brazil | ||||
| 10:30 | 11:00 | 9.6.3 |
FLIGHT TESTS OF THE VISION-BASED TARGET SENSING AND APPROACHING S. Cho¹, Y. Jung, Korea Aerospace Research Institute, South Korea; D.H. Shim¹; ¹Korea Advanced Institute of Science and Technology, South Korea | ||||
| 11:00 | 11:30 | 9.6.4 |
OPTICAL FLOW ON A FLAPPING WING-MICRO AIR VEHICLE TO AVOID COLLISIONS AND STEER S.W. Ryu¹, J.G. Lee¹, H.J. Kim¹; ¹Seoul National University, South Korea | ||||
| 11:30 | 12:00 | 9.6.5 |
REAL-TIME GENERATION OF WAYPOINTS ENHANCING UAV SURVIVABILITY S.-H. Park, LIG Nex1., South Korea; K.-K. Park¹, S.-S. Park¹, C.-K. Ryoo¹; ¹Inha Univ., South Korea | ||||
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| 09:30 | 10:00 | 10.6.1 |
HYBRID-ELECTRIC TRANSPORT AIRCRAFT: OPPORTUNITIES AND PERSPECTIVES A.T. Isikveren¹, P.-A. Lambert¹, J. Stuhlberger, Airbus Group, Germany; M.K. Bradley, Boeing Commercial Airplanes, United States; J.H. Stromberger, General Electric, Germany; J. Whurr, Rolls Royce, United Kingdom; F. Anton, Siemens, Germany; ¹SAFRAN S.A., France | ||||
| 10:00 | 10:30 | 10.6.2 |
THE E-FAN ALL ELECTRICAL AIRCRAFT DEMONSTRATOR AND ITS INDUSTRIALIZATION E. Joubert¹, D. Chapuis¹, D. Esteyne¹, J.-C. Lambert¹, O. Siri¹, D. Müller-Wiesner¹; ¹Airbus, France | ||||
| 10:30 | 11:00 | 10.6.3 |
HYBRID TURBO-ELECTRIC DISTRIBUTED PROPULSION APPLIED TO SHORT RANGE AIRCRAFT P. Laskaridis, Cranfield University, United Kingdom | ||||
| 11:00 | 11:30 | 10.6.4 |
THE D8 AIRCRAFT CONCEPT AND ITS BOUNDARY LAYER INGESTION BENEFIT A. Uranga, University of Southern California, United States | ||||
| 11:30 | 12:00 | 10.6.5 |
ELECTRIC PROPULSION FOR AIRCRAFT O. Otto, Siemens AG, Germany | ||||
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| 09:30 | 10:00 | 11.6.1 |
A STUDY ON SAFETY ASSURANCE FOR INCREASINGLY AUTONOMOUS TRAFFIC FLOW MANAGEMENT SYSTEM Y. Wu, University of Missouri St. Louis D of Maths and Computer Science, United States; T.A. Lauderdale, NASA Ames Research Center / Aviation Systems Division, United States; H. Chen, Johnson C. Smith University Computer Science & Engineering Dept., United States | ||||
| 10:00 | 10:30 | 11.6.2 |
MODELLING, GENERATING AND EVALUATING SECTOR CONFIGURATION PLANS - METHODOLOGY REPORT OF THE SESAR VP-755 EXERCISE T. Dubot¹, J. Bedouet¹, S. Degrémont, DSNA, France; ¹ONERA, France | ||||
| 10:30 | 11:00 | 11.6.3 |
TOWARDS A MORE HARMONISED AND WIDER USE OF SHORT-TERM ATFCM MEASURES (STAM) P. Choroba¹, L. van der Hoorn¹; ¹Eurocontrol, France | ||||
| 11:00 | 11:30 | 11.6.4 |
VISUALIZATION OF AIRSPACE COMPLEXITY BASED ON AIR TRAFFIC CONTROL DIFFICULTY H. Hirabayashi¹, M. Brown¹, S. Nagaoka¹; ¹Electronic Navigation Research Institute, Japan | ||||
| 11:30 | 12:00 | 11.6.5 |
DEVELOPMENT OF AN ADVANCED ATCO WORKSTATION D. Rohacs¹, I. Jankovics¹, J. Rohacs¹; ¹Budapest University of Technology and Economics, Hungary | ||||
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| 09:30 | 10:00 | 12.6.1 |
FORMAL VERIFICATION OF AUTOPILOTS IN UMANNED AIRCRAFT SYSTEMS B.J. Yang¹, P. Dutta¹, I. Hwang, Purdue University, United States; ¹Optimal Synthesis Inc., United States | ||||
| 10:00 | 10:30 | 12.6.2 |
DETECT AND AVOID FOR REMOTELY PILOTED AIRCRAFT IN AIR TRAFFIC CONTROL SIMULATIONS J. Alfredson, Saab/LiU, Sweden; P. Hagström, Saab, Sweden | ||||
| 10:30 | 11:00 | 12.6.3 |
THE DRONE AVIATION NAVIGATION SYSTEMS M. Tanaka, Nagoya Univ, Japan; T. Okubo, iisec, Japan; S. Yamada¹, G. Idei¹, M. Takase¹, R. Hosomi¹; ¹Kyoto Institute of Technology, Japan | ||||
| 11:00 | 11:30 | 12.6.4 |
VERTICAL POSITION ERROR BOUNDING FOR INTEGRATED GPS/BAROMETER SENSORS TO SUPPORT UNMANNED AERIAL VEHICLE (UAV) J. Lee¹, E. Hyeon¹, M. Kim¹, J. Lee¹; ¹Korea Advanced Institute of Science and Technology, South Korea | ||||
| 11:30 | 12:00 | 12.6.5 |
SECURE ESTIMATION FOR UNMANNED AERIAL VEHICLES AGAINST ADVERSARIAL ATTACKS Q. Hu¹, Y.H. Chang, Oregon Health and Science University, United States; C.J. Tomlin¹; ¹University of California Berkeley, United States | ||||
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| 14:00 | 14:30 | 1.7.1 |
LINKING TECHNOLOGY READINESS TO UNCERTAINTY REDUCTION K.G. Schwartz¹, D. Mavris¹; ¹Georgia Institute of Technology, United States | ||||
| 14:30 | 15:00 | 1.7.2 |
EXPLORING PROPAGATED UNCERTAINTIES IN A MULTI-DISCIPLINARY AIRCRAFT DESIGN FRAMEWORK T. Pfeiffer¹, E. Moerland¹, J. Gibbs¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany | ||||
| 15:00 | 15:30 | 1.7.3 |
UNCERTAINTY QUANTIFICATION OF AIRFOIL DESIGN FOR ADVANCED PROPELLER MODELS H.D. Schwartz¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States | ||||
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| 14:00 | 14:30 | 2.7.1 |
EXPERIENCE IN AERODYNAMICAL TESTS AND CFD SIMULATIONS OF OVERSIZED WING DEMONSTRATOR IN LARGE LOW-SPEED WIND TUNNEL G.M. Carossa, LEONARDO S.p A., Italy; K. Anisimov¹, A. Chevagin¹, R. Efimov¹, I. Kursakov¹, A. Lysenkov¹, V. Malenko¹, A. Saprykin¹; ¹TsAGI, Russia | ||||
| 14:30 | 15:00 | 2.7.2 |
STUDY OF MODEL DEFORMATION AND STING INTERFERENCE TO THE AERODYNAMIC ESTIMATIONS OF THE CAE-AVM MODEL M. Zhong¹, G.L. Wang¹, J. Hua¹; ¹Chinese Aeronautical Establishment, China | ||||
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| 14:00 | 14:30 | 3.7.1 |
DEFORMATION MEASUREMENT IN THE WIND TUNNEL FOR AN UAV LEADING EDGE WITH A MORPHING MECHANISM M. Radestock¹, J. Riemenschneider¹, H.P. Monner¹, O. Huxdorf¹, N.P.M. Werter², R. De Breuker²; ¹German Aerospace Center, Germany ;²Delft University of Technology, Netherlands | ||||
| 14:30 | 15:00 | 3.7.2 |
SEMI-A VIBRATION SUPPRESSION OF AIRCRAFT PANEL USING PIEZOELECTRIC ACTUATOR WITH SYNCHRONIZED SWITCH DAMPING TECHNIQUE K. Li¹, L. Zhang¹, K. Pan¹, W. Huang¹; ¹Aircraft strength research institute of China, China | ||||
| 15:00 | 15:30 | 3.7.3 |
DESIGN, MANUFACTURING AND VALIDATION OF A GUST GENERATOR FOR WIND TUNNEL TEST OF A LARGE SCALE AEROELASTIC MODEL F. Fonte¹, L. Riccobene¹, S. Ricci¹, S. Adden², M. Martegani²; ¹Politecnico di Milano, Italy ;²IBK Technologie, Germany | ||||
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| 13:30 | 14:00 | 4.7.1 |
AN EXPERIMENTAL STUDY OF MICRO-ELECTROMECHANICAL FLYING INSECT FLAPPING WINGS AERODYNAMIC PERFORMANCE P. Czekalowski, Air Force Institute of Technology, Poland; K.-S. Sibilski, Institute of Aviation, Poland; A. Zyluk, Air Force Academy, Poland | ||||
| 14:00 | 14:30 | 4.7.2 |
THE PROPULSIVE EFFICIENCY OF FLEXIBLE FLAPPING-WING W. Yang¹, B. Song¹, D. Xue¹; ¹Northwestern Polytechnical University, China | ||||
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| 14:00 | 14:30 | 5.7.1 |
RESEARCH ADVANCES ON AIRCRAFT STRUCTURAL INTEGRITY AND SUSTAINMENT AT NRC M. Liao¹, M. Yanishevsky¹, P. Patnaik¹; ¹Aerospace, National Research Council Canada, Canada | ||||
| 14:30 | 15:00 | 5.7.2 |
DESIGN AND PRELIMINARY EVALUATION OF AN INTEGRATED AIRCRAFT OPERATION SYSTEM FOR DISASTER RELIEF A. Andreeva-Mori¹, K. Kobayashi¹, M. Shindo¹, Y. Okuno¹; ¹Japan Aerospace Exploration Agency, Japan | ||||
| 15:00 | 15:30 | 5.7.3 |
BOARDING PROCESS ASSESSMENT OF NOVEL AIRCRAFT CABIN CONCEPTS M. Schmidt, Munich Aerospace e.V., Germany; M. Engelmann¹, R. Rothfeld¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany | ||||
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| 14:00 | 14:30 | 6.7.1 |
FRACTURE BEHAVIOR OF RIVETED LAP JOINTS DUE TO PROJECTILE IMPACTS T. Matsuda¹, K. Mizutani¹, S. Enomoto¹, M. Nishida², T. Moroe², K. Yamada²; ¹CHURYO ENGINEERING CO., LTD., Japan ;²Nagoya Institute of Technology, Japan | ||||
| 14:30 | 15:00 | 6.7.2 |
MODELING AND ANALYSIS METHOD ON CRASHWORTHINESS OF CIVILIAN AIRCRAFT FUSELAGE STRUCTURES H. Huang, China; M. Zhao, China; W. Wang, China | ||||
| 15:00 | 15:30 | 6.7.3 |
AIRFRAME STRUCTURAL SURVIVABILITY STUDY THROUGH HYDRODYNAMIC RAM OF WELDED METALLIC WATER TANKS J. Kim¹, C. Kim, Korea Advanced Institute of Science and Technology, South Korea; S. Jun¹; ¹Agency for Defense Development, South Korea | ||||
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| 14:00 | 14:30 | 7.7.1 |
ANALYSIS OF SWIRL RECOVERY VANES FOR INCREASED PROPULSIVE EFFICIENCY IN TRACTOR PROPELLER AIRCRAFT L. Veldhuis¹, T. Stokkermans¹, T. Sinnige¹, G. Eitelberg, TU Delft / DNW, Netherlands; ¹TU Delft, Netherlands | ||||
| 14:30 | 15:00 | 7.7.2 |
MULTI-OBJECTIVE OPTIMAL DESIGN OF THE PROPELLER FOR HIGH ALTITUDE AIRSHIPS BASED ON HIGH EFFICIENCY AND LIGHT WEIGHT J. Jiao¹, Y.-G. Zhang¹, B.-F. Song¹; ¹Northwestern Polytechnical University, China | ||||
| 15:00 | 15:30 | 7.7.3 |
SMALL HEIGHT DUCT DESIGN FOR MULTICOPTER FAN K. Stremousov¹, M. Arkhipov¹, S. Serokhvostov¹; ¹Moscow Institute of Physics and Technology, Russia | ||||
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| 13:30 | 14:00 | 8.7.1 |
WIND TUNNEL THREE-DEGREE-OF-FREEDOM DYNAMIC RIG FOR CONTROL VALIDATION D.I. Ignatyev ¹, M.E. Sidoryuk¹, K.A. Kolinko¹, A.N. Khrabrov¹; ¹Central Aerohydrodynamic Institute named after N.E. Zhukovsky, Russia | ||||
| 14:00 | 14:30 | 8.7.2 |
WIND TUNNEL FREE-FLIGHT TEST FOR FLIGHT DYNAMICS AND CONTROL SYSTEM EXPERIMENTS F. Cen¹, Q. Li¹, B.-W. Nie², Z.-T. Liu², H.-S. Sun²; ¹Tsinghua University, China ;²China Aerodynamics Research and Development Center, China | ||||
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| 14:00 | 14:30 | 9.7.1 |
DYNAMIC MODELING AND STABILITY ANALYSIS OF A HIGH ALTITUDE AIRSHIP R. Hun¹, N.K. Sinha¹, D. Chakraborti, ADRDE, India; P. Balasubramanian, RIC, India; ¹Indian Institute of Technology,Madras, India | ||||
| 14:30 | 15:00 | 9.7.2 |
PERCH LANDING ASSISTED BY THRUSTER (PLAT): SIX D.O.F. TRAJECTORY OPTIMIZATION S.Y. Han¹, B.Y. Lee¹, J.M. Ahn¹, M.J. Tahk¹; ¹KAIST, South Korea | ||||
| 15:00 | 15:30 | 9.7.3 |
ADAPTIVE SLIDING MODE CONTROLLER DESIGN FOR RECONFIGURATION OF ORGANIC FLIGHT ARRAY J. Jeong¹, S. Kim¹, J. Suk¹; ¹Chungnam National University, South Korea | ||||
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| 14:00 | 14:30 | 10.7.1 |
DIRECT NUMERICAL SIMULATION OF DISTURBANCES IN A THREE-DIMENSIONAL HYPERSONIC NEAR-WALL FLOW OVER FLAT PLATE AND COMPRESSION CORNER A.V. Novikov¹, I.V. Egorov¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia | ||||
| 14:30 | 15:00 | 10.7.2 |
STUDY OF THE UNSTEADY STRUCTURES EVOLUTION IN SHOCK WAVE / BOUNDARY LAYER INTERACTION FOR VARIOUS UPSTREAM CONDITIONS P.A. Polivanov¹, A.A. Sidorenko¹, A.A. Maslov¹; ¹ITAM SB RAS, Russia | ||||
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| 14:00 | 14:30 | 11.7.1 |
AN IN-FLIGHT AID TO NEGOTIATE A MORE EFFICIENT FLIGHT PATH C. Posse, United States; K. Rein-Weston, United States | ||||
| 14:30 | 15:00 | 11.7.2 |
PLANNING AND NEGOTIATION OF OPTIMIZED 4D-TRAJECTORIES IN STRATEGIC AND TACTICAL RE-ROUTING OPERATIONS A. Gardi¹, Y. Lim¹, T. Kistan, THALES Australia, Australia; R. Sabatini¹; ¹RMIT University, Australia | ||||
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| 14:00 | 14:30 | 12.7.1 |
CAN 3D-AUDIO IMPROVE STATE-OF-THE-ART PILOT-ASSISTANCE SYSTEMS? C.A. Niermann, German Aerospace Center (DLR), Institute of Flight Guidance, Germany | ||||
| 14:30 | 15:00 | 12.7.2 |
OBJECTIVE EVALUATION OF HUMAN PILOT OPERATIONS IN WIND SHEAR USING PSYCHOPHYSIOLOGICAL MEASUREMENTS J.O. Entzinger¹, T. Uemura¹, T. Iijima², N. Matayoshi², S. Suzuki¹; ¹The University of Tokyo, Japan ;²JAXA (Japan Aerospace Exploration Agency), Japan | ||||
| 15:00 | 15:30 | 12.7.3 |
EVALUATION METHODS OF AIRCRAFT FLIGHT SAFETY J. Rajchel, Polish Air Force Academy, Poland; J. Zurek¹, R. Kaleta¹; ¹Air Force Institute of Technology, Poland | ||||
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| 16:00 | 16:30 | 1.8.1 |
CONCEPTUAL STUDY OF AN INNOVATIVE HIGH ALTITUDE SOLAR POWERED FLIGHT VEHICLE J. Hanjie¹, D. Zhuoyi¹, P. Hongbin¹, S. Liying¹; ¹AVIC, China | ||||
| 16:30 | 17:00 | 1.8.2 |
TOWARDS A 4D TRAFFIC MANAGEMENT OF SMALL UAS OPERATING AT VERY LOW LEVEL A. Joulia¹, T. Dubot¹, J. Bedouet¹; ¹ONERA - The French Aerospace Lab, France | ||||
| 17:00 | 17:30 | 1.8.3 |
FEASIBILITY ANALYSIS OF SPAN EXTENSION OF MORPHING HALE UAV WING T. Prakash, Indian Institute of Technology Bombay, India | ||||
| 17:30 | 18:00 | 1.8.4 |
CONCEPTUAL AND AERODYNAMIC DESIGN OF A UAV FOR SUPERFICIAL VOLCANO MONITORING P.D. Bravo-Mosquera¹, A. Martins-Abdalla¹, H.D. Cerón-Muñoz¹, F.M. Catalano¹; ¹Aerodynamic Laboratory, São Carlos Engineering School-University, Brazil | ||||
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| 16:00 | 16:30 | 2.8.1 |
NUMERICAL SIMULATION OF MIXING IN AN INLET-FUELED HYPERSONIC AIR-BREATHING PROPULSION J.W. Kim¹, O.J. Kwon¹; ¹Korea Advanced Institute of Science and Technology, South Korea | ||||
| 16:30 | 17:00 | 2.8.2 |
AEROTHERMODYNAMICS CHARACTERISTICS OF A SPACE PROBE IN THE MARTIAN ATMOSPHERE I.V. Egorov¹, N.V. Palchekovskaya¹, M.A. Pugach¹; ¹TsAGI, Russia | ||||
| 17:00 | 17:30 | 2.8.3 |
A MESHLESS METHOD FOR SIMULATION OF HYPERSONIC VISCOUS FLOWS J.Y. Huh¹, J.S. Rhee¹, K.H. Kim¹, S.Y. Jung, Agency for Defense Development, South Korea; ¹Seoul National University, South Korea | ||||
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| 16:00 | 16:30 | 3.8.1 |
PRESSURE ANALYSIS BASED ON PIV MEASUREMENT IN AIRPLANE WAKES K. Matsushima¹, R. Namba¹, H. Kato, JAXA, Japan; ¹Univ. of Toyama, Japan | ||||
| 16:30 | 17:00 | 3.8.2 |
THE RESEARCH AND VALIDATION OF GLOBAL SKIN FRICTION FIELDMEASUREMENT BASED ON FLUORESCENT OIL FILM H.W. Wang¹, Z. Huang¹, L. Li¹, L.F. Wei¹, H.L. Xiong¹; ¹China Academy of Aerospace Aerodynamics, China | ||||
| 17:00 | 17:30 | 3.8.3 |
MATHEMATICAL MODELS AND OPTICAL INVESTIGATION OF TWO PHASE FLOWS IN WIND TUNNELS I.A. Amelyushkin, TsAGI, Russia | ||||
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| 16:00 | 16:30 | 4.8.1 |
LOW-DRAG / LOW-BOOM SHAPE OPTIMIZATION OF A BIPLANE WING / TWIN-BODY FUSELAGE SST CONFIGURATION N. Ban, Nagaoka University of Technology, Japan | ||||
| 16:30 | 17:00 | 4.8.2 |
NUMERICAL STUDY OF ACTIVE SHOCK WAVE-TURBULENT BOUNDARY LAYER INTERACTION CONTROL FOR TRANSONIC AERODYNAMICS Z. Seifollahi Moghadam ¹, A. Jahangirian¹; ¹Amirkabir University of Technology, Iran | ||||
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| 16:00 | 16:30 | 5.8.1 |
DAMAGE TOLERANCE AND REPAIR OF UD-RIBS OF LATTICE COMPOSITE FUSELAGE STRUCTURES E. Dubovikov¹, V. Fomin¹, M. Glebova¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia | ||||
| 16:30 | 17:00 | 5.8.2 |
NUMERICAL ASSESSSMENT OF DAMAGE TOLERANCE ALLOWABLES FOR NEW DESIGN CONCEPTS OF STIFFENED COMPOSITE PANELS T. Bach, German Aerospace Center (DLR), Germany | ||||
| 17:00 | 17:30 | 5.8.3 |
XFEM-BASED FRACTURE MECHANICS ANALYSIS OF AERONAUTICAL STRUCTURES AFFECTED BY RESIDUAL STRESSES I. Rivero Arevalo¹, J. Gomez-Escalonilla Martin¹, V. Ramirez Gonzalez², A. Garcia Martinez-Pardo², D. Garijo Hernandez, IMDEA Materials Institute, Spain; ¹Airbus Defence and Space, Spain ;²Safran Engineering Services, Spain | ||||
| 17:30 | 18:00 | 5.8.4 |
INVESTIGATION OF DEFORMATION FIELDS IN AIRCRAFT PANELS BY NON-CONTACT OPTICAL VIDEOGRAMMETRY METHOD K. Kuruliuk, Central Aerohydrodynamic Institute named after Zhukovsky, Russia | ||||
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| 16:00 | 16:30 | 6.8.1 |
NUMERICAL AND EXPERIMENTAL STRENGTH ANALYSIS OF LATTICE COMPOSITE FUSELAGE STRUCTURES A. Dzuba¹, A. Shanygin¹, I. Kondakov¹, A. Razin², V. Vassiliev²; ¹Central Aerohydrodynamic Institute (TsAGI), Russia ;²Central Research Institute for Special Machinery (CRISM), Russia | ||||
| 16:30 | 17:00 | 6.8.2 |
EXPERIENCE OF USING NONLINEAR NUMERICAL ANALYSIS TO ESTIMATE AIRCRAFT PRIMARY STRUCTURE STRENGTH Y.I. Dudarkov¹, E.A. Levchenko¹, M.V. Limonin¹, A.S. Dzuba¹; ¹TsAGI, Russia | ||||
| 17:00 | 17:30 | 6.8.3 |
APPLICATION OF BUCKLING/POST-BUCKLING ANALYSIS FOR COMPOSITE STIFFENED PANELS L.-J. Dong, Chinese Aeronautical Establishment, China; G. Song, Beijing University of Aeronautics and Astronautics, China; D.-G. Cui, Aircraft Design and Research Institute of Shenyang, China | ||||
| 17:30 | 18:00 | 6.8.4 |
OPTIMIZATION OF COMPOSITE PATCH REPAIR FOR INCLINED CRACK ON ALUMINUM PLATE USING GENETIC ALGORITHM B. Talebi¹, A. Abedian¹, S. Firooz¹; ¹Aerospace Engineering, Sharif University of Technology, Iran | ||||
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| 16:00 | 16:30 | 7.8.1 |
UNMANNED VEHICLE COLLABORATION RESEARCH ENVIRONMENT FOR MARITIME SEARCH AND RESCUE W. Roberts¹, K. Griendling¹, A. Gray¹, D.N. Mavris¹; ¹Georgia Tech, United States | ||||
| 16:30 | 17:00 | 7.8.2 |
EVOLUTIONARY GAME BASED MULTI-OBJECTIVE OPTIMIZATION FOR MULTI-AGENT NETWORK RESILIENCE H.-I. Lee¹, H.-S. Shin¹, A. Tsourdos¹; ¹Cranfield University, United Kingdom | ||||
| 17:00 | 17:30 | 7.8.3 |
SYSTEMS ENGINEERING: AN INTERDISCIPLINARY CHALLENGE P. Krus, Linköping University, Sweden; L. Pereira, Federal University of ABC, Brazil | ||||
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| 16:00 | 16:30 | 8.8.1 |
MULTI-STEP TRAJECTORY OPTIMIZATION FOR ATM BASED ON APPROXIMATED OPTIMAL PATH S. Bae¹, H.-S. Shin¹, A. Tsourdos¹; ¹Cranfield University, United Kingdom | ||||
| 16:30 | 17:00 | 8.8.2 |
BENEFITS ASSESSMENT ON TIME-BASED OCEANIC ARRIVALS TO THE TOKYO METROPOLITAN AREA N.K. Wickramasinghe¹, S. Fukushima¹, H. Hirabayashi¹; ¹Electronic Navigation Research Institute, Japan | ||||
| 17:00 | 17:30 | 8.8.3 |
TRAJECTORY DESIGN WITH PATH PREDICTION FOR TERRAIN FOLLOWING M.K. Kim¹, M.-H. Cho¹, M.-J. Tahk¹; ¹KAIST, South Korea | ||||
| 17:30 | 18:00 | 8.8.4 |
MINIMUM-TIME FORMATION USING OPTIMAL SOLUTIONS OF SINGLE FIXED-WING AIRCRAFT H. Fukumoto¹, S. Ueno¹; ¹Yokohama National University, Japan | ||||
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| 16:00 | 16:30 | 9.8.1 |
HISTORY OF RAPID GROWTH IN KOREAN AERONAUTICAL INDUSTRY D.-M. Ahn, Hanseo University, South Korea; W.-H. Kang, Yanbian University, China; S.-Y. Lee, KM Engineering, Former Head of Aircraft Sys. Int. Div. ADD, South Korea | ||||
| 16:30 | 17:00 | 9.8.2 |
DEVELOPMENT OF SMART TILT-ROTOR UAS AND THE BEGINNINGS OF KOREAN CIVILIAN DRONES C.H. Lim¹, W.G. Kang¹, J.W. Kim¹; ¹KARI, South Korea | ||||
| 17:00 | 17:30 | 9.8.3 |
FROM 500MD TO LAH - CHALLENGE TOWARD VERTICAL LIFT IN KOREA J.B. Yim, Agency for Defense Development, South Korea | ||||
| 17:30 | 18:00 | 9.8.4 |
THE ORIGIN OF WIND TUNNELS IN RUSSIA A.R. Gorbushin, Central Aerohydrodynamic Institute, Russia | ||||
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| 16:00 | 16:30 | 10.8.1 |
INVESTIGATION ON OBLIQUE SHOCK WAVE CONTROL BY SURFACE ARC DISCHARGE PLASMA F. Liu¹, H. Yan¹, J. Xu¹; ¹Northwestern Polytechnical University, China | ||||
| 16:30 | 17:00 | 10.8.2 |
CHARACTERISATION OF NS-DBD PLASMA ACTUATORS FOR SUPERSONIC FLOW CONTROL A. Russell¹, H. Zare-Behtash¹, K. Kontis¹; ¹University of Glasgow, United Kingdom | ||||
| 17:00 | 17:30 | 10.8.3 |
THE DEVELOPMENT OF A SIMPLE METHOD FOR DRAG ESTIMATION FOR WEDGE-LIKE FAIRINGS IN HYPERSONIC FLOW A. Roussel¹, S. Prince¹, M. Viguer¹, A. Kshitij¹, J. Stollery¹, K. Garry¹; ¹Cranfield University, United Kingdom | ||||
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| 16:00 | 16:30 | 11.8.1 |
OPTIMAL SEQUENCING IN ATM COMBINING GENETIC ALGORITHMS AND GRADIENT BASED METHODS TO A BILEVEL APPROACH B. Grüter¹, M. Bittner¹, M. Rieck¹, J. Diepolder¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, TU München, Germany | ||||
| 16:30 | 17:00 | 11.8.2 |
WAKE TURBULENCE RE-CATEGORISATION ON APPROACH AND DEPARTURE FOR SAFE AND MORE EFFICIENT AIR TRAFFIC MANAGEMENT F. Rooseleer¹, V. Treve¹, I. De Visscher, Wake Prediction Technologies (WaPT), Belgium; R. Graham¹; ¹EUROCONTROL, Belgium | ||||
| 17:00 | 17:30 | 11.8.3 |
AIRBORNE COLLISION AVOIDANCE CONSIDERATIONS FOR SIMULTANEOUS PARALLEL APPROACH OPERATIONS S.R. Conway¹, M.B. Lapis¹, J.D. Musiak¹, M.L. Ulrey¹, C. Hanses, German Aerospace Center, Germany; ¹Boeing, United States | ||||
| 17:30 | 18:00 | 11.8.4 |
NONLINEAR OPTIMAL CONFLICT RESOLUTION SOLVED WITH PARTICLE SWARM OPTIMIZATION Y.K. Hong¹, Y.D. Kim¹, K.J. Lee, Korea Aerospace University, South Korea; ¹Seoul National University, South Korea | ||||
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| 16:00 | 16:30 | 12.8.1 |
EULERIAN METHOD FOR IN-ENGINE ICING: WITH APPLICATION TO ICE CRYSTAL TRAJECTORIES AND IMPACT IN A GENERIC TURBOFAN COMPRESSOR E. Norde¹, E.T.A. van der Weide¹, H.W.M. Hoeijmakers¹; ¹University of Twente, Netherlands | ||||
| 16:30 | 17:00 | 12.8.2 |
RESEARCH ON AIRWORTHINESS REQUIREMENTS OF SUPERCOOLED LARGE DROP ICING PROTECTION FOR AIRCRAFT (§25.1420) T. Hu¹, L. Jin¹; ¹China Aero-Polytechnology Establishment, AVIC, China | ||||
| 17:00 | 17:30 | 12.8.3 |
RESTARTING OF A JET ENGINE DURING FLYING AND FLIGHT SAFETY M. Kowalski¹, A. Jankowski¹, J. Rajchel, Polish Air Force Academy, Poland; ¹Air Force Institute of Technology, Poland | ||||
| 17:30 | 18:00 | 12.8.4 |
DISPATCH RELIABILITY ORIENTED MMEL FORMULATION TECHNOLOGY RESEARCH Z. Wang, NEIAS-AVIC, China | ||||
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| 10:00 | 10:30 | 1.9.1 |
ENVIRONMENTALLY RESPONSIBLE AVIATION PROJECT OVERVIEW F. Collier, United States | ||||
| 10:30 | 11:00 | 1.9.2 |
STITCHED, RESIN-INFUSED, HWB AIRCRAFT STRUCTURAL DEVELOPMENTS A. Velicki, United States | ||||
| 11:00 | 11:30 | 1.9.3 |
FUEL-FLEXIBLE, COMBUSTOR AND FAN DEVELOPMENTS FOR UHB ENGINES A. Epstein, United States | ||||
| 11:30 | 12:00 | 1.9.4 |
UHB ENGINE INTEGRATION FOR HYBRID WING BODY AIRCRAFT J.T. Bonet, United States | ||||
| 12:00 | 12:30 | 1.9.5 |
TECHNOLOGY INTEGRATION AND SYSTEM ASSESSMENTS WITH UNCERTAINTY MODELLING D.N. Mavris¹, K.G. Schwartz¹, J. Tai¹; ¹Georgia Institute of Technology, United States | ||||
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| 10:00 | 10:30 | 2.9.1 |
ENGINEERING APPLICATION OF GAO-YONG RATIONAL TURBULENCE MODEL TO AN INTER-COOLED DUCT X. Li¹, W. Zheng¹; ¹AVIC, China | ||||
| 10:30 | 11:00 | 2.9.2 |
NUMERICAL SIMULATIONS OF TURBULENT FLOWS OVER THE ONERA-M6 AND DLR-F6 CONFIGURATIONS R.G. da Silva¹, J.L.F. Azevedo¹; ¹Instituto de Aeronautica e Espaco, Brazil | ||||
| 11:00 | 11:30 | 2.9.3 |
NUMERICAL INVESTIGATION OF SUBSONIC RAREFIED FLOWS USING DSMC-IP METHODS Y.-J. Choi¹, O.-J. Kwon¹; ¹Korea Advanced Institute of Science and Technology, South Korea | ||||
| 11:30 | 12:00 | 2.9.4 |
A MESH-LESS METHOD FOR COMPRESSIBLE FLOW CALCULATIONS AT ALL SPEED CONDITIONS A. Jahangirian¹, S. Sattarzadeh¹; ¹Amirkabir University of Technology, Iran | ||||
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| 10:00 | 10:30 | 4.9.1 |
COLLABORATIVE MULTI-LEVEL MDO PROCESS DEVELOPMENT AND APPLICATION TO LONG-RANGE TRANSPORT AIRCRAFT S. Görtz¹, C. Ilic¹, M. Abu-Zurayk¹, R. Liepelt¹, J. Jepsen¹, T. Führer¹, R. Becker¹, J. Scherer¹, T. Kier¹, M. Siggel¹; ¹German Aerospace Center (DLR), Germany | ||||
| 10:30 | 11:00 | 4.9.2 |
ON MORE EFFECTIVE AERODYNAMIC DATA GENERATION FOR SIMULATION BASED AIRCRAFT CONCEPTUAL DESIGN J. Park¹, S. Choi¹, P. Raj¹; ¹Virginia Tech, United States | ||||
| 11:00 | 11:30 | 4.9.3 |
SURROOPT: A GENERIC SURROGATE-BASED OPTIMIZATION CODE FOR AERODYNAMIC AND MULTIDISCIPLINARY DESIGN Z.-H. Han, Northwestern Polytechnical University, China | ||||
| 11:30 | 12:00 | 4.9.4 |
DEVELOPMENT OF A THREE-DIMENSIONAL TIGHTLY COUPLED EULER/POTENTIAL FLOW SOLVER FOR TRANSONIC FLOW Y.M. Jo ¹, S.H. Park¹, D.J. Lee¹, S. Choi, Virginia Polytechnic Institute and State University, United States; ¹Korea Advanced Institute of Science and Technology, South Korea | ||||
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| 10:00 | 10:30 | 5.9.1 |
VERIFICATION OF CFRP COMPONENTS FATIGUE EVALUATION PROCEDURE UNDER IRREGULAR CYCLING LOADING A.V. Pankov¹, V.V. Konovalov¹; ¹TsAGI, Russia | ||||
| 10:30 | 11:00 | 5.9.2 |
PREDICTION OF WFD OCCURRENCE IN LONGITUDINAL JOINTS OF A FUSELAGE FOR COMMERCIAL AIRPLANE A.A. Sviridov¹, I.G. Khlebnikova¹; ¹TsAGI, Russia | ||||
| 11:00 | 11:30 | 5.9.3 |
LIFE PREDICTION MODEL OF AIRCRAFT STRUCTURE UNDER CORROSION ENVIRONMENT C. Li¹, Y. He¹, T. Zhang¹, X. Li¹, S. Zhang¹; ¹Air Force Engineering University, China | ||||
| 11:30 | 12:00 | 5.9.4 |
PREDICTION OF FRACTURE STRENGTH FOR NOTCHED LAMINATE SUBJECTED TO COMPRESSION LOADING M. Lee, Agency for Defense Development, South Korea; J. Kim, Chungnam National University, South Korea | ||||
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| 10:00 | 10:30 | 6.9.1 |
ELASTO-STATIC AND MODAL MODELING OF FLEXIBLE WINGS CARRYING MULTIPLE EXTERNAL STORES E.M. Amato¹, C. Polsinelli¹, E. Cestino¹, G. Frulla¹, R. Carrese², P. Marzocca²; ¹Politecnico di Torino, Italy ;²RMIT University, Australia | ||||
| 10:30 | 11:00 | 6.9.2 |
CHARACTERIZATION OF THE NONLINEAR AEROELASTIC BEHAVIOR OF AN AIRFOIL WITH FREEPLAY AND AERODYNAMIC NONLINEARITY M. Candon¹, R. Carrese¹, H. Ogawa¹, P. Marzocca¹; ¹RMIT University, Australia | ||||
| 11:00 | 11:30 | 6.9.3 |
SENSITIVITY ANALYSIS OF UNSTEADY AERODYNAMIC REDUCED-ORDER MODELS ROBUST TO FREESTREAM PARAMETER VARIATIONS M. Winter¹, C. Breitsamter¹; ¹Technische Universität München, Germany | ||||
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| 10:00 | 10:30 | 7.9.1 |
A REVIEW OF RECENT AIRCRAFT CONCEPTS EMPLOYING SYNERGISTIC PROPULSION-AIRFRAME INTEGRATION J. Bijewitz¹, A. Seitz¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany | ||||
| 10:30 | 11:00 | 7.9.2 |
COMPARATIVE EFFICIENCY ANALYSIS OF DISTRIBUTED PROPULSION SYSTEMS FOR PROPULSIVE FUSELAGE AND HYBRID WING BODY CONCEPTS IN FP7 PROJECT "DISPURSAL" A. Mirzoyan¹, A. Isyanov¹, A.T. Isikveren, Safran Tech, France; ¹CIAM, Russia | ||||
| 11:00 | 11:30 | 7.9.3 |
AEROPROPULSIVE PERFORMANCE ANALYSIS OF THE NOVA CONFIGURATIONS L. Wiart¹, O. Atinault¹, J.-C. Boniface¹, R. Barrier¹; ¹ONERA, France | ||||
| 11:30 | 12:00 | 7.9.4 |
HYBRID-ELECTRIC MOTIVE POWER SYSTEMS FOR COMMUTER TRANSPORT APPLICATIONS Y. Fefermann¹, C. Maury¹, C. Level¹, K. Zarati¹, J.-P. Salanne¹, C. Pornet¹, B. Thoraval¹, A.T. Isikveren¹; ¹SAFRAN S.A., France | ||||
| 12:00 | 12:30 | 7.9.5 |
DISTRIBUTED ELECTRIC PROPULSION FOR SMALL BUSINESS AIRCRAFT A CONCEPT-PLANE FOR KEY-TECHNOLOGIES INVESTIGATIONS J. Hermetz¹, M. Ridel¹, C. Döll¹; ¹ONERA, The French Aerospace Lab, France | ||||
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| 10:00 | 10:30 | 8.9.1 |
NOVEL PILOT CONTROL MODEL WITH STOCHASTIC AND PERIODICAL MOVEMENT R. Mori, Electronic Navigation Research Institute, Japan | ||||
| 10:30 | 11:00 | 8.9.2 |
THE FLYING QUALITIES IMPROVEMENT FOR THE VEHICLES WITH TIME DELAY IN THEIR DYNAMICS A.V. Efremov ¹, M.S. Tyaglik¹, A.S. Tyaglik¹, V.V. Aleksandrov¹; ¹Moscow aviation institute, Russia | ||||
| 11:00 | 11:30 | 8.9.3 |
PILOT'S CG LOCATION AND ATTITUDE CONTROL FOR LATERAL MANEUVER OF A HANG GLIDER Y. Ochi, National Defense Academy, Japan | ||||
| 11:30 | 12:00 | 8.9.4 |
ADVANCED REFUELING BOOM SYSTEM (ARBS) DEVELOPMENT AND HANDLING QUALITIES EVALUATION A. Anton Diez¹, F. Asensio Nieto¹; ¹AIRBUS DEFENCE & SPACE, Spain | ||||
| 12:00 | 12:30 | 8.9.5 |
EFFECT OF FEEL SYSTEM CHARACTERISTICS ON PILOT MODEL PARAMETERS K. Grinev¹, S. Sorokin¹; ¹The Central Aerohydrodynamic Institute (TsAGI), Russia | ||||
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| 10:00 | 10:30 | 9.9.1 |
ONE-VERSUS-ONE AIR-TO-AIR COMBAT MANEUVER GENERATION BASED ON THE DIFFERENTIAL GAME B.-Y. Lee¹, S. Han¹, H.-J. Park², D.-W. Yoo², M.-J. Tahk¹; ¹Korea Advanced Institute of Science and Technology, South Korea ;²Agency for Defense Development , South Korea | ||||
| 10:30 | 11:00 | 9.9.2 |
CAPTURE REGION ANALYSIS FOR MISSILE GUIDANCE WITH FIELD-OF-VIEW CONSTRAINT AGAINST MOVING TARGET S. Lee¹, Y. Kim¹, T.-Y. Um, Agency for Defense Development, South Korea; ¹Seoul National University, South Korea | ||||
| 11:00 | 11:30 | 9.9.3 |
A NEW SOLUTION METHOD FOR SIX DEGREE OF FREEDOM FLIGHT DYNAMICS SIMULATION OF A HIGH ASPECT RATIO WING VEHICLE Y.B. Been¹, Y.J. Kang¹, S.J. Shin¹; ¹Seoul National Univ., South Korea | ||||
| 11:30 | 12:00 | 9.9.4 |
OPERATION SCENARIOS OF UNMANNED AIRCRAFT SYSTEMS INTEGRATED INTO THE KOREAN NATIONAL AIRSPACE SYSTEM T.M. Shim¹, Y.J. Kim¹, H.C. Bang¹; ¹KAIST, South Korea | ||||
| 12:00 | 12:30 | 9.9.5 |
EFFECT OF YAW-TILTED HINGE AXIS ON DEPLOYMENT ROBUSTNESS OF MARS AIRPLANE K. Fujita¹, H. Nagai, Tohoku University, Japan; A. Oyama¹; ¹ISAS/JAXA, Japan | ||||
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| 10:00 | 10:30 | 10.9.1 |
NEW METHOD OF TRANSONIC BUFFET DECREASING ON SUPERCRITICAL AIRFOIL M.A. Brutyan¹, A.V. Petrov¹, A.V. Potapchik¹; ¹TsAGI, Russia | ||||
| 10:30 | 11:00 | 10.9.2 |
INVESTIGATION OF FLOW CONTROL OVER THE SUPERCRITICAL AIRFOIL BY TANGENTIAL JET BLOWING AT TRANSONIC SPEEDS A.V. Petrov¹, A.V. Potapchik¹, V.G. Soudakov¹; ¹TsAGI, Russia | ||||
| 11:00 | 11:30 | 10.9.3 |
NUMERICAL STUDY ON TRANSONIC BUFFET ACTIVE CONTROL BY OPEN AND CLOSED-LOOP STRATEGIES C.Q. Gao¹, W.W. Zhang¹, Z.Y. Ye¹; ¹Northwestern Polytechnical University , China | ||||
| 11:30 | 12:00 | 10.9.4 |
EFFECTS OF LAMINAR-TURBULENT TRANSITION ON BUFFET ONSET AND TRANSONIC CHARACTERISTICS OF LAMINAR AIRFOIL W. Stalewski¹, K. Surmacz¹, J. Sznajder¹; ¹INSTITUTE of AVIATION, Poland | ||||
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| 10:00 | 10:30 | 11.9.1 |
ADVANCED RNP TO ILS AUTOLAND APPROACHES FOR OPTIMAL BENEFITS FROM PBN: FLIGHT TESTING PROCEDURES WITH AN A320 T. Dautermann¹, T. Ludwig¹, R. Geister¹, T. Blase, MBDA Systems, Germany; ¹DLR Institute of Flight Guidance, Germany | ||||
| 10:30 | 11:00 | 11.9.2 |
IMPACT OF WEATHER UNCERTAINTIES ON NOISE CONTOURS AND NOISE ABATEMENT DESCENT TRAJECTORIES A. Andreeva-Mori¹, H. Ishii¹; ¹Japan Aerospace Exploration Agency (JAXA), Japan | ||||
| 11:00 | 11:30 | 11.9.3 |
OPTIMAL APPROACH TRAJECTORIES FOR MULTIPLE AIRCRAFT CONSIDERING DISTURBANCES AND CONFIGURATION CHANGES M. Bittner¹, M. Rieck¹, B. Grüter¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, TUM, Germany | ||||
| 11:30 | 12:00 | 11.9.4 |
AIR TRAFFIC EFFICIENCY EVALUATION BY TRAJECTORY OPTIMIZATION AND ADS-B DATA A. Harada, Kochi University of Technology, Japan | ||||
| 12:00 | 12:30 | 11.9.5 |
EFFICIENT CONTROL OF ARRIVAL TIME AT A CONGESTED AIRPORT'S TERMINAL AREA Y. Higuchi¹, N. Kitazume¹, T. Kozuka¹, K. Tamura¹, Y. Miyazawa¹, M. Brown, Electronic Navigation Research Institute, Japan; ¹Kyushu University, Japan | ||||
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| 10:00 | 10:30 | 12.9.1 |
THE DESIGN OF AN AUTOMATIC BEACON EJECTING SYSTEM FOR AIRCRAFT L. Peters¹, C. Bil¹; ¹RMIT University, Australia | ||||
| 10:30 | 11:00 | 12.9.2 |
AIRCRAFT SECURITY ENHANCEMENT: ROTATING MACHINERY FAULT DIAGNOSIS AND HEALTH ASSESSMENT USING MANIFOLD LEARNING AND DYNAMIC TIME WARPING Y. Tian¹, C. Lu¹, Z.-L. Wang¹; ¹School of Reliability and Systems Engineering,Beihang University, China | ||||
| 11:00 | 11:30 | 12.9.3 |
INFLUENCE OF ETHNICITY ON PASSENGER STANDARD WEIGHT C. Bil, RMIT University, Australia; G. Hanlon, Five Rings Aerospace, Australia | ||||
| 11:30 | 12:00 | 12.9.4 |
FUEL STARVATION CAUSED BY HUB CLOSURE C. Wang¹, L. Drees¹, F. Holzapfel¹; ¹Technische Universität München, Germany | ||||
| 12:00 | 12:30 | 12.9.5 |
RESEARCH ON LOAD SPECTRUM OF AERO HYDRAULIC PUMP BASED ON ACCELERATED DEGRADATION TESTING J. Chen¹, J. Zhang¹, J. Li, Siemens Industry Software (Beijing), Germany; ¹Beihang University, China | ||||
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| 14:00 | 14:30 | 1.10.1 |
CABIN ESCAPE SYSTEM: A WAY TO ENSURE CREW SAFETY DURING SUBORBITAL FLIGHTS R. Fusaro¹, N. Viola¹, D. Ferretto¹, F. Santoro, Altec S.p.A, Italy; F. Fenoglio, Thales Alenia Space, Italy; ¹Politecnico di Torino, Italy | ||||
| 14:30 | 15:00 | 1.10.2 |
SUPERSONIC BUSINESS JET TECHNOLOGY AND MISSION TRADE STUDIES L. Gonzalez, EMBRY RIDDLE AERONAUTICAL UNIVERSITY, United States | ||||
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| 14:00 | 14:30 | 2.10.1 |
NUMERICAL SIMULATION OF AEROTHERMODYNAMIC CHARACTERISTICS OF FLOW OVER SPACE VEHICLE MODEL I. Egorov¹, N. Palchekovskaya¹; ¹TsAGI, Russia | ||||
| 14:30 | 15:00 | 2.10.2 |
AERODYNAMIC ANALYSIS WITH SEPARATION DYNAMICS OF A LAUNCHER AT STAGING CONDITIONS A. Viviani¹, G. Pezzella, Centro Italiano Ricerche Aerospaziali, Italy; E. D'Amato¹; ¹Seconda Università di Napoli, Italy | ||||
| 15:00 | 15:30 | 2.10.3 |
NUMERICAL SIMULATION OF HYDRODYNAMIC LOADINGS ON REENTRY VEHICLE DURING SPLASHDOWN A.A. Aksenov, TESIS; JIHT RAS, Russia; A.A. Dyadkin ¹, M.K. Mikhailova ², A.E. Schelyaev ², T.V. Simakova ¹, V.V. Zharckova ²; ¹JSV «RSC Energia» , Russia ;²TESIS, Russia | ||||
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| 14:00 | 14:30 | 3.10.1 |
SUBSCALE FLIGHT TESTING OF A GENERIC FIGHTER AIRCRAFT D. Lundström¹, A. Sobron¹, P. Krus¹, C. Jouannet, SAAB AB, Sweden; R.G.A. da Silva, Instituto Tecnológico de Aeronáutica, Brazil; ¹Linköping University, Sweden | ||||
| 14:30 | 15:00 | 3.10.2 |
DESIGN AND TESTING OF A LOW-COST FLIGHT CONTROL AND DATA ACQUISITION SYSTEM FOR UNSTABLE SUBSCALE AIRCRAFT A. Sobron¹, D. Lundström¹, I. Staack¹, P. Krus¹; ¹Linköping University, Sweden | ||||
| 15:00 | 15:30 | 3.10.3 |
DEVELOPMENT OF HALF-MODEL TEST CAPABILITY AT THE NF-3 WIND TUNNEL D. Lei¹, H. Zenghong¹, G. Yongwei¹; ¹Northwestern Polytechnical university, China | ||||
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| 14:00 | 14:30 | 4.10.1 |
NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT J. Steelant¹, V. Villace¹, M. Marini², G. Pezzella², B. Reimann, DLR, Germany; S.L. Chernyshev³, A.A. Gubanov³, V.A. Talyzin³, N.V. Voevodenko³, N.V. Kukshinov*, A.N. Prokhorov*, A.J. Neelyº, C. Kennellº, D. Verstraete, University of Sydney, Australia; D. Buttsworth, Univ. of Southern Queensland, Australia; ¹ESA-ESTEC, Netherlands ;²CIRA, Italy ;³TsAGI, Russia ;*CIAM, Russia ;ºUniv. of New South Wales, Australia | ||||
| 14:30 | 15:00 | 4.10.2 |
BOUNDARY LAYER STATE INFLUENCE ON START OF THE INWARD-TURNING INTAKE N.V. Voevodenko¹, A.A. Gubanov¹, D.Y. Gusev¹, M.A. Ivankin, TsAGi, Russia; D.S. Ivanyushkin¹, V.Y. Lunin¹, P.A. Meshennikov¹, Y.G. Shvalev¹, V.A. Talyzin¹, V.A. Yakovleva¹; ¹TsAGI, Russia | ||||
| 15:00 | 15:30 | 4.10.3 |
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF DIFFERENT INTAKE CONFIGURATIONS OF HEXAFLY-INT FACILITY MODULE V.Y. Aleksandrov¹, M.K. Danilov¹, O.V. Gouskov¹, S.V. Gusev¹, N.V. Kukshinov¹, A.N. Prokhorov¹, V.S. Zakharov¹; ¹CIAM, Russia | ||||
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| 14:00 | 14:30 | 5.10.1 |
COLLABORATIVE SYSTEMS DRIVEN AIRCRAFT CONFIGURATION DESIGN OPTIMIZATION P. Shiva Prakasha¹, P.D. Ciampa¹, B. Nagel¹, L. Boggero², M. Fioriti²; ¹German Aerospace Center, Germany ;²Politecnico di Torino, Italy | ||||
| 14:30 | 15:00 | 5.10.2 |
HIL TEST BENCH FOR ENGINE'S FUEL CONTROL SYSTEMS INVESTIGATION S. Gafurov¹, L. Rodionov¹, A. Kryuchkov¹, H. Handroos, Lappeenranta University of Technology, Finland; ¹Samara National Research University, Russia | ||||
| 15:00 | 15:30 | 5.10.3 |
STRATEGIES TO ENHANCE A CONFIGURATION FOR HIGH-PRECISION MULTI DISCIPLINARY OPTIMIZATION H. Liu, China | ||||
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| 14:00 | 14:30 | 6.10.1 |
THE SUPPORT PROCESS, SIMULATION RESEARCH DESIGN AND STRUCTURE OF THE NEW HELICOPTER'S CONSTRUCTION SCHEMATICS WITH SPECIAL EMPHASIS ON GROUND RESONANCE PHENOMENON G. Kowaleczko¹, T. Gorecki¹; ¹Air Force Institute of Technology , Poland | ||||
| 14:30 | 15:00 | 6.10.2 |
A STUDY OF THE ACCURACY OF GROUND VIBRATION TEST DATA USING A REPLICA OF THE GARTEUR SM-AG19 TESTBED STRUCTURE P. Gustafsson, SAAB AB, Sweden; A. Linderholt, Linnaeus University, Sweden | ||||
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| 14:00 | 14:30 | 7.10.1 |
COMBUSTION INSTABILITY FREQUENCY MODE SHIFT OF H2/CH4 RATIO AND COMBUSTOR LENGTH IN A MODEL GAS TURBINE S. Joo¹, J. Yoon¹, J. Kim¹, S. Kim¹, Y. Yoon¹; ¹seoul national university, South Korea | ||||
| 14:30 | 15:00 | 7.10.2 |
INVESTIGATION OF THE HYDROGEN COMBUSTION CHAMBER PERFORMANCE WITHIN THE HEXAFLY-INT PROJECT M.A. Ivankin¹, A.A. Nikolaev¹, V.A. Talyzin¹, O.V. Voloschenko¹; ¹TsAGI, Russia | ||||
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| 14:00 | 14:30 | 8.10.1 |
A WAVELET BASED FLIGHT DATA PREPROCESSING METHOD FOR FLIGHT CHARACTERISTICS ESTIMATION AND FAULT DETECTION M. Naruoka, Japan Aerospace Exploration Agency, Japan | ||||
| 14:30 | 15:00 | 8.10.2 |
WIND VELOCITY ESTIMATION WITHOUT AN AIR SPEED SENSOR USING KALMAN FILTER UNDER THE COLORED MEASUREMENT NOISE Y.G.J. Park¹, C.G. Park¹; ¹Seoul National University, South Korea | ||||
| 15:00 | 15:30 | 8.10.3 |
INFERENCE OF FLIGHT INTENT BASED ON INVERSE OPTIMAL CONTROL N. Yokoyama, National Defense Academy of Japan, Japan | ||||
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| 14:00 | 14:30 | 9.10.1 |
THE EFFECTS OF BODY AERODYNAMICS ON THE DYNAMIC STABILITY OF INSECT FLIGHT A.-T. Nguyen¹, J.-K. Kim¹, J.-H. Han¹; ¹Korea Advanced Institute of Science and Technology, South Korea | ||||
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| 14:00 | 14:30 | 10.10.1 |
COMPUTATIONS OF SUPERSONIC LATERAL JET J. Huh¹, S. Lee¹; ¹Inha univ., South Korea | ||||
| 14:30 | 15:00 | 10.10.2 |
EXPERIMENTAL INVESTIGATION OF LATERAL PULSE JET INTERACTION FLOWFIELD IN HYPERSONIC FLOW Z.-Y. Ni¹, N. Cao¹, L. Xu¹; ¹CAAA, China | ||||
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| 14:00 | 14:30 | 11.10.1 |
REPORT FROM ICAS WORKSHOP ON COMPLEX SYSTEMS INTEGRATION IN AERONAUTICS S.X. Ying, COMAC, China | ||||
| 14:30 | 15:00 | 11.10.2 |
CO-EVOLUTION OF COMPLEX AERONAUTICAL SYSTEM & COMPLEX SYSTEM ENGINEERING X.G. Zhang, Aviation Industry Corporation of China (AVIC), China | ||||
| 15:00 | 15:30 | 11.10.3 |
VIRTUAL EXPERIMENTATION AND VISUAL ANALYTICS IN SUPPORT OF SYSTEMS ENGINEERING AND SYSTEMS OF SYSTEMS ENGINEERING EFFORTS K. Griendling¹, O.J. Pinon¹, D.N. Mavris¹; ¹Georgia Tech, United States | ||||
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| 14:00 | 14:30 | 12.10.1 |
THE FUTURE JOURNEY OF CIVIL AEROSPACE: WEATHER, ENVIRONMENT AND CLIMATE R. Singh, Emeritus Cranfield University, United Kingdom | ||||
| 14:30 | 15:00 | 12.10.2 |
THE FUTURE OF SUSTAINABLE COMMERCIAL PROPULSION A. Epstein, Pratt & Whitney, United States | ||||