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10:30 | 11:00 | 1.1.1 |
STREAMLINING CROSS-ORGANIZATIONAL AIRCRAFT DEVELOPMENT PROCESSES: AN OVERVIEW OF THE AGILE PROJECT P.D. Ciampa¹, B. Nagel¹; ¹DLR, Germany | ||||
11:00 | 11:30 | 1.1.2 |
MULTIDISCIPLINARY DESIGN ANALYSIS OF BLENDED WING BODY THROUGH COLLABORATIVE DESIGN APPROACH: AGILE EU PROJECT P.S. Prakasha¹, P.D. Ciampa¹, P. Della Vecchia ², D. Ciliberti ², M. Voskuijl , TU Delft, Netherlands; D. Charbonnier³, A. Jungo³, M. Fioriti, Politecnico di Torino, Italy; K. Anisimov, TsAGI, Russia; A. Mirzoyan, CIAM, Russia; ¹German Aerospace Center DLR, Germany ;²University of Naples, Italy ;³CFSE, Switzerland | ||||
11:30 | 12:00 | 1.1.3 |
AERO-STRUCTURAL OPTIMIZATION OF A MALE CONFIGURATION IN THE AGILE MDO FRAMEWORK R. Maierl¹, A.A. Gastaldi¹, F. Daoud¹, J.N. Walther², P.D. Ciampa², A. Jungo, CFSE, Switzerland; M. Zhang, AIRINNOVA, Sweden; ¹Airbus DS, Germany ;²DLR, Germany |
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10:30 | 11:00 | 2.1.1 |
MULTIDISCIPLINARY OPTIMIZATION OF UNMANNED AIRCRAFT IN A SYSTEM OF SYSTEMS CONTEXT A. Papageorgiou¹, K. Amadori², C. Jouannet², J. Ölvander¹; ¹Linköping University, Sweden ;²SAAB Aeronautics, Sweden | ||||
11:00 | 11:30 | 2.1.2 |
DEVELOPMENT OF A COMPREHENSIVE ANALYSIS AND OPTIMIZED DESIGN FRAMEWORK FOR THE MULTIROTOR UAV H. Kim¹, D. Lim¹, K. Yee¹; ¹Seoul National University, South Korea | ||||
11:30 | 12:00 | 2.1.3 |
DEVELOPMENT AND PERFORMANCE COMPARISON OF OPTIMIZED ELECTRIC FIXED-WING VTOL UAV CONFIGURATIONS P. Stahl¹, T. Seren¹, C. Rößler¹, M. Hornung¹; ¹Technical University of Munich, Germany |
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10:30 | 11:00 | 3.1.1 |
A HOLISTIC ENGINEERING APPROACH FOR AERONAUTICAL PRODUCT DEVELOPMENT I. Staack, Linköping University, Sweden; K. Amadori¹, C. Jouannet¹; ¹Saab Aeronautics, Sweden | ||||
11:00 | 11:30 | 3.1.2 |
CONTINUOUS MODELING IN AIRCRAFT TOP-LEVEL DEMONSTRATION J. Zang¹, Q. Wang¹, J.-Q Zhu¹; ¹Aviation Industry Development Research Center of China, China | ||||
11:30 | 12:00 | 3.1.3 |
FORMULATION AND IMPLEMENTATION OF A METHOD FOR TECHNOLOGY EVALUATION OF SYSTEM OF SYSTEMS D.N. Mavris¹, A. Sudol¹; ¹Georgia Institute of Technology, United States |
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10:30 | 11:00 | 4.1.1 |
INVISCID AND VISCOUS FLOW MODELING FOR FAST TRANSONIC FLUTTER CALCULATIONS H. Güner¹, G. Dimitriadis¹, V.E. Terrapon¹; ¹University of Liège, Belgium | ||||
11:00 | 11:30 | 4.1.2 |
FEASIBILITY OF THE NAVIER-STOKES HARMONIC BALANCE METHOD FOR MODELLING AIRCRAFT UNSTEADY AERODYNAMICS J. Drofelnik¹, A. Da Ronch¹, M.S. Campobasso, University of Lancaster, United Kingdom; ¹University of Southampton, United Kingdom | ||||
11:30 | 12:00 | 4.1.3 |
AERODYNAMIC AND AEROACOUSTIC INVESTIGATION OF SWIRL RECOVERY VANES FOR PROPELLER PROPULSION SYSTEMS L.E. van den Ende¹, Q. Li¹, F. Avallone¹, D. Casalino¹, G. Eitelberg¹, L.L.M. Veldhuis¹; ¹Delft University of Technology, Netherlands |
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10:30 | 11:00 | 5.1.1 |
EXPERIMENTAL INVESTIGATION OF WING LOAD CONTROL USING FLUIDIC DEVICES A. Krzysiak, Institute of Aviation, Poland | ||||
11:00 | 11:30 | 5.1.2 |
LARGE EDDY SIMULATION OF A TRANSIENT SPOILER DEPLOYMENT IN A NACA0012 PROFILE IN SUBSONIC AND TRANSONIC SPEEDS R.V. Linn¹, A.M. Awruch¹; ¹Federal University of Rio Grande do Sul, Brazil | ||||
11:30 | 12:00 | 5.1.3 |
Lecture canceled |
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10:30 | 11:00 | 6.1.1 |
DESTABILIZING EFFECT OF LONGITUDINAL WALL OSCILLATION ON OBLIQUE WAVES IN 2D CHANNEL FLOW T. Atobe, JAXA, Japan | ||||
11:00 | 11:30 | 6.1.2 |
EXPERIMENTAL INVESTIGATION, MATHEMATICAL AND NUMERICAL SIMULATION OF AIRCRAFT ICING PHENOMENA I.A. Amelyushkin, Russia; A.L. Stasenko, Russia; V.A. Zhbanov, Russia | ||||
11:30 | 12:00 | 6.1.3 |
IONIZATION AND DISSOCIATION EFFECTS ON HYPERSONIC BOUNDARY-LAYER STABILITY F. Miró Miró¹, E.-S. Beyak², D. Mullen², F. Pinna¹, H.L. Reed²; ¹von Kármán Institute for Fluid Dynamics, Belgium ;²Texas A&M University, United States |
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10:30 | 11:00 | 7.1.1 |
WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTING V. Ciobaca¹, B. Stefes², A. de Bruin³, M. Bauer, NAVASTO GmbH, Germany; P. Schlösser, Airbus Defence and Space GmbH, Germany; A. de Blécourt³, N. Bier¹, J. Zhai, DNW-KKK, Germany; M. Meyer², J. Wild¹; ¹Deutsches Zentrum für Luft und Raumfahrt, DLR, Germany ;²Airbus Operations GmbH, Germany ;³NLR-Netherlands Aerospace Center, Netherlands | ||||
11:00 | 11:30 | 7.1.2 |
PASSIVE VENTILATION FLOW CONTROL FOR AIRCRAFT GUST LOAD ALLEVIATION Y. Tani¹, S. Seki¹, S. Aso¹; ¹Kyushu University, Japan | ||||
11:30 | 12:00 | 7.1.3 |
INVESTIGATION ON THE POSSIBILITY OF FLOW CONTROL AROUND CAVITY USING TANGENTIAL JET Y. Lee, Agency for Defense Development, South Korea |
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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 |
Lecture canceled | ||||
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 |
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10:30 | 11:00 | 9.1.1 |
MULTI-DISCIPLINARY OPTIMISATION OF MEDIUM ALTITUDE LONG ENDURANCE UAVS D. Verstraete, University of Sydney, Australia | ||||
11:00 | 11:30 | 9.1.2 |
DYNAMIC MODEL FOR PLANETARY GEAR SETS OF GEARED TURBOFAN JET ENGINES D. Kalinin¹, V. Golovanov¹, J. Temis, BMSTU, Russia; L. Magerramova¹; ¹CIAM, Russia |
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10:30 | 11:00 | 10.1.1 |
FAULT TOLERANT CONTROL SYSTEM OF AIRCRAFT BY FEEDBACK ERROR LEARNING WITH SYSTEM ESTIMATION N. Yoshikawa, The university of Tokyo, Japan | ||||
11:00 | 11:30 | 10.1.2 |
FAULT-TOLERANT FLIGHT CONTROL SYSTEM WITH SIMPLE ADAPTIVE CONTROL CONSIDERING PILOT INPUT R. Takase¹, J.O. Entzinger¹, S. Suzuki¹; ¹The University of Tokyo, Japan | ||||
11:30 | 12:00 | 10.1.3 |
DATA-DRIVEN FAILURE IDENTIFICATION USING A MOTION-BASED SIMULATOR A.D. Kraemer¹, E. Villani¹; ¹Instituto Tecnológico de Aeronáutica (ITA), Brazil |
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10:30 | 11:00 | 11.1.1 |
FIXED-WING UAV ROBUST GUIDANCE STRATEGY BASED ON COMPOUND FLIGHT MISSION OF ON-GROUND TARGETS J.L. Gomes Olavo¹, L.A. Borges Tôrres¹, T. Argolo Jesus, CEFET/MG, Brazil; ¹UFMG, Brazil | ||||
11:00 | 11:30 | 11.1.2 |
ROBUST TRAJECTORY OPTIMIZATION OF VTOL TRANSITION MANEUVER USING BI-LEVEL OPTIMAL CONTROL P. Piprek¹, F. Holzapfel¹; ¹Technical University of Munich, Germany | ||||
11:30 | 12:00 | 11.1.3 |
Lecture canceled |
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10:30 | 11:00 | 12.1.1 |
A METHOD FOR ESTIMATING THE PROBABILITY OF RARE ACCIDENTS IN COMPLEX SYSTEMS I. Romani de Oliveira¹, J.D. Musiak¹, G.C. Balvedi¹; ¹Boeing Research & Technology, Brazil | ||||
11:00 | 11:30 | 12.1.2 |
PROBABILISTIC FORECASTING IN AIRCRAFT EMERGENCY EVACUATION SIMULATION D.B. Ferrari¹, R. Giarola¹, L.C.de C. Santos, EMBRAER, Brazil; ¹Instituto Tecnológico de Aeronáutica, Brazil | ||||
11:30 | 12:00 | 12.1.3 |
STUDY ON AIRCRAFT EVACUATION MODELING AND MODEL PARAMETERS BASED ON SOCIAL FORCE K. Chen¹, Y. Wu¹, T. Zou¹; ¹Laboratory of Civil Aircraft Airworthiness Technology, CAUC, China |
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13:00 | 13:30 | 1.2.1 |
DESIGN OF THE STRUT BRACED WING AIRCRAFT IN THE AGILE COLLABORATIVE MDO FRAMEWORK F. Torrigiani¹, J. Bussemaker¹, P.D. Ciampa¹, M. Fioriti², F. Tomasella², B. Aigner, RWTH Aachen, Germany; D. Rajpal, Delft University of Technology, Netherlands; H. Timmermans, Netherlands Aerospace Center (NLR), Netherlands; A. Savelyev, Central Aerohydrodynamic Institute (TsAGI), Russia; D. Charbonnier, CFS Engineering, Switzerland; ¹German Aerospace Center, DLR, Germany ;²Politecnico di Torino, Italy | ||||
13:30 | 14:00 | 1.2.2 |
MDO APPLICATIONS TO CONVENTIONAL AND NOVEL TURBOPROP AIRCRAFT WITHIN AGILE EUROPEAN PROJECT L. Stingo¹, P. Della Vecchia¹, G. Cerino, Leonardo Company, Italy; F. Nicolosi¹, A. De Marco¹; ¹University of Naples, Italy | ||||
14:00 | 14:30 | 1.2.3 |
INCLUDING AEROELASTIC TAILORING IN THE CONCEPTUAL DESIGN PROCESS OF A COMPOSITE STRUT BASED WING D. Rajpal¹, R. De Breuker¹, H. Timmermans², W.F. Lammen², F. Torrigiani, German Aerospace Center, Germany; ¹Delft University of Technology, Netherlands ;²Netherlands Aerospace Centre, Netherlands |
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13:00 | 13:30 | 2.2.1 |
A VTOL SMALL UNMANNED AIRCRAFT SYSTEM TO EXPAND PAYLOAD CAPABILITIES S. Geuther¹, F. Capristan¹, J. Kirk, Georgia Institute of Technology, United States; R. Erhard, University of Denver, United States; ¹NASA Langley Research Center, United States | ||||
13:30 | 14:00 | 2.2.2 |
LIFECYCLE COSTS AND FEASIBILITY ANALYSIS OF THE DESIGNS OF UAV'S FOR HUMANITARIAN RELIEF MISSIONS O. Hektor¹, T. Melin¹; ¹Swedish Aeronautical Institute, Sweden | ||||
14:00 | 14:30 | 2.2.3 |
SOLAR-POWERED UAV PLATFORM SYSTEM: A CASE STUDY FOR GROUND CHANGE DETECTION A.C.B. Ramos¹, M.S. Santiago¹, E.H. Shiguemori, IEAV, Brazil; S. Serokhvostov, MIPT, Russia; P.K. Gupta, JUIT, India; L. Zhong, CAUC, China; ¹UNIFEI, Brazil |
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13:00 | 13:30 | 3.2.1 |
ENABLING THE DIGITAL FACTORY THROUGH THE INTEGRATION OF DATA-DRIVEN AND SIMULATION MODELS O.L. Pinon¹, D.J.L. Siedlak¹, D. Mavris¹; ¹Georgia Institute of Technology, United States | ||||
13:30 | 14:00 | 3.2.2 |
ON-DEMAND SMALL UAS ARCHITECTURE SELECTION AND RAPID MANUFACTURING USING A MODEL-BASED SYSTEMS ENGINEERING APPROACH C. Justin¹, A. Ramamurthy¹, N. Beals², E. Spero², D. Mavris¹; ¹GEORGIA INSTITUTE OF TECHNOLOGY, United States ;²U.S. ARMY RESEARCH LABORATORY, United States | ||||
14:00 | 14:30 | 3.2.3 |
IDENTIFICATION METHOD OF THE SIMULATION MODEL "VIRTUAL ENGINE" BUILT INTO THE DIGITAL ENGINE CONTROL SYSTEM F.D. Golberg¹, O.S. Gurevich¹, A.A. Petukhov¹; ¹CIAM, Russia |
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13:00 | 13:30 | 4.2.1 |
NUMERICAL DEVELOPMENT OF UNSTEADY VORTEX-LATTICE METHOD EXPANSION FOR LEADING-EDGE SHEDDING PREDICTION WITH EXPERIMENTAL VALIDATION T.P. Monteiro¹, K. Ramesh, Glasgow University, United Kingdom; F. Silvestre¹; ¹Instituto Tecnologico de Aeronautica, Brazil | ||||
13:30 | 14:00 | 4.2.2 |
NUMERICAL ANALYSIS OF THE FLOW AROUND A BACKWARD-FACING RAMP P. Catalano¹, A. Mastellone¹, M. Invigorito¹, F. Capuano, Università di Napoli Federico II, Italy; ¹CIRA, Italy | ||||
14:00 | 14:30 | 4.2.3 |
RECTANGULAR CAVITY FLOWFIELD EFFECTS ON STORES IN THE SHEAR LAYER A. Cenko, AIWS, United States; G. Akroyd, Akroyd Aeronautics, Australia |
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13:00 | 13:30 | 5.2.1 |
THE AERODYNAMIC PERFORMANCE MEASUREMENT OF COAXIAL ROTOR IN HOVER X. Zhao¹, N.-Z. Huang¹, X. Liang¹, P. Zhou¹, W.-P. Song¹, Y.-F. Lin, China Helicopter Research and Development Institute, China; ¹Northwestern Polytechnical University, China | ||||
13:30 | 14:00 | 5.2.2 |
ADAPTIVE WING HIGH-LIFT SYSTEM A.V. Petrov¹, A.V. Potapchik¹, J.G. Stepanov¹, V.V. Gubskiy¹; ¹TsAGI, Russia | ||||
14:00 | 14:30 | 5.2.3 |
NUMERICAL INVESTIGATION AERODYNAMICS NACELLE-STRAKE EFFECT J.J. Broekhuijsen¹, G. Vidjaja², J.W. van der Burg², H.W.M. Hoeijmakers¹; ¹University of Twente, Netherlands ;²Airbus Operations GMBH, Germany |
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13:00 | 13:30 | 6.2.1 |
ACOUSTIC MODES AND GLOBAL INSTABILITIES IN WAKES AND JETS E. Martini, ITA, Brazil; A. Cavalieri, ITA, Brazil; P. Jordan, Universite de Poitiers, France | ||||
13:30 | 14:00 | 6.2.2 |
Lecture canceled | ||||
14:00 | 14:30 | 6.2.3 |
ON THE EXISTENCE OF MULTIPLE SELF-EXCITATION FREQUENCIES IN THE INSTABILITY OF INTERACTING PLANAR MIXING LAYER AND WAKE H.R. De Aguiar Quintanilha Jr., University of Liverpool, United Kingdom; L. Santos de Brito Alves, Universidade Federal Fluminense, Brazil |
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13:00 | 13:30 | 7.2.1 |
Lecture canceled | ||||
13:30 | 14:00 | 7.2.2 |
Lecture canceled | ||||
14:00 | 14:30 | 7.2.3 |
Lecture canceled |
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13:00 | 13:30 | 8.2.1 |
Lecture canceled | ||||
13:30 | 14:00 | 8.2.2 |
APPLICATION RESEARCH OF ZIMMERMAN-WEISSENBURGER-YANG METHOD FOR PREDICTING FLUTTER BOUNDARY Y. FEI, Shang Hai Aircraft Design and Research Institute of COMAC, China | ||||
14:00 | 14:30 | 8.2.3 |
A RESEARCH OF MULTIDISCIPLINARY DESIGN OPTIMIZATION ALGORITHM FOR FIGHT VEHICLE DESIGN X. Yan¹, Z. Liu¹, Y. Yang¹; ¹CARDC, China |
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13:00 | 13:30 | 9.2.1 |
ENGINE TEST RESULTS OF FUEL-WATER MICROEMULSION M. Kowalski¹, A. Jankowski¹; ¹AFIT, Poland | ||||
13:30 | 14:00 | 9.2.2 |
PRECISE MEASUREMENT OF PROPAGATING FLAME IN 2-STROKE GASOLINE ENGINE BY MULTIPLE ION-PROBES T. Yatsufusa¹, K. Kii¹, K. Takatani¹; ¹Hiroshima Institute of Technology, Japan | ||||
14:00 | 14:30 | 9.2.3 |
OPTIMIZATION OF THE FUEL INJECTOR TO AN INTERNAL COMBUSTION ENGINE BY MEANS OF LASER EQUIPMENT M. Kowalski¹, A. Jankowski¹, R. Szczepanik, Polish Air Force Academy Deblin, Poland; ¹AFIT, Poland |
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13:00 | 13:30 | 10.2.1 |
BEYOND BEDFORD; DEVELOPMENT OF A TWO-DIMENSIONAL PILOT WORKLOAD RATING SCALE G.R. Ridgway¹, H.R. Shattock¹, A.C.R. Hare¹; ¹QinetiQ, United Kingdom | ||||
13:30 | 14:00 | 10.2.2 |
THE INFLUENCE OF BIODYNAMIC FEEDTHROUGH ON HANDLING QUALITIES D. Drewiacki, Embraer, Brazil; F.J. Silvestre¹, A.B. Guimarães Neto¹; ¹Instituto Tecnológico de Aeronáutica, Brazil | ||||
14:00 | 14:30 | 10.2.3 |
HANDLING QUALITIES OF ONERA’S SMALL BUSINESS CONCEPT PLANE WITH DISTRIBUTED ELECTRIC PROPULSION E. Dillinger, ISAE-SUPAERO/ONERA, France; C. Döll¹, R. Liaboeuf¹, C. Toussaint¹, J. Hermetz¹, C. Verbeke¹, M. Ridel¹; ¹ONERA, France |
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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 |
Lecture canceled |
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13:00 | 13:30 | 12.2.1 |
3D PERSPECTIVE VIEWS ON IMMERSIVE HEAD-WORN DISPLAYS - CAN EXOCENTRIC VIEWS INCREASE PILOT SITUATIONAL AWARENESS? J.M. Ernst, DLR, Germany | ||||
13:30 | 14:00 | 12.2.2 |
HUMAN RELIABILITY ANALYSIS IN AN AIRCRAFT DECOMPRESSION EVENT C. Reiser¹, A. Bayma¹, D.A. Fonseca¹; ¹Embraer S/A, Brazil | ||||
14:00 | 14:30 | 12.2.3 |
IMPACT STUDY ON CYBER THREATS TO GNSS AND FMS SYSTEMS R. Geister¹, J.-P. Buch¹, D. Niedermeier¹, G. Gamba², L. Canzian², O. Pozzobon²; ¹German Aerospace Center, Germany ;²Qascom S.r.l., Italy |
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15:00 | 15:30 | 1.3.1 |
COLLABORATIVE OPEN SOURCE AIRCRAFT DESIGN FRAMEWORK FOR EDUCATION - AGILE ACADEMY INITIATIVES AND RESULTS P. Della Vecchia, University of Naples, Italy; B. Aigner, RWTH Aachen University, Germany; I. van Gent , TU Delft, Netherlands; P.D. Ciampa¹, P.S. Prakasha¹; ¹German Aerospace Center DLR , Germany | ||||
15:30 | 16:00 | 1.3.2 |
MDO AS A SOCIO-TECHNICAL SYSTEM - A SMALL CONTRIBUTION TO COLLABORATIVE ENGINEERING M. Spieck, Thelsys GmbH, Germany; B. Aigner, RWTH Aachen, Germany; P.S. Prakasha¹, P.D. Ciampa¹; ¹German Aerospace Center, Germany | ||||
16:00 | 16:30 | 1.3.3 |
EXPERIENCE WITH INTERNATIONAL COLLABORATIVE AIRCRAFT DESIGN EDUCATION: AREND UAV L. Smith, University of Pretoria, South Africa; J.N. Koster, University of Colorado, United States; J. Schneider, University of Stuttgart, Germany |
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15:00 | 15:30 | 2.3.1 |
RESEARCH ON DESIGN METHOD OF PETROL-ELECTRIC HYBRID DRIVE SYSTEM BASED ON MDO FOR A NOVEL VTOVL UAV Z.X. Yao, Shenyang Aircraft Design and Research Institute, China | ||||
15:30 | 16:00 | 2.3.2 |
DESIGN AND OPTIMIZATION OF A VERSATILE UAV FOR OBSERVATION AND RESEARCH USING THERMAL COLUMNS FOR EXTENDED ENDURANCE U. Golyska¹, M. Nowowiejski¹, P. Pacuszka¹; ¹Warsaw University of Technology, Poland | ||||
16:00 | 16:30 | 2.3.3 |
UAV INITIAL PARAMETER ESTIMATION G.G. Silva¹, L.C. Carmona¹, E. Bauzer Medeiros¹; ¹UFMG, Brazil |
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15:00 | 15:30 | 3.3.1 |
AIRCRAFT STRUCTURE TECHNOLOGY OF ADDITIVE MANUFACTURING X. Wang¹, H. Cui¹, P. Xu¹, S. Bi¹; ¹Shenyang Aircraft Design and Resesarch Institute, China | ||||
15:30 | 16:00 | 3.3.2 |
INVESTIGATION OF CRACK PROPAGATION PROPERTIES OF ADDITIVE MANUFACTURING PRODUCTS H. Abramovich¹, N. Broitman¹, A. Shirizly¹; ¹Technion, I.I.T., Israel | ||||
16:00 | 16:30 | 3.3.3 |
EVALUATION OF MECHANICAL PROPERTIES OF TI-6AL-4V FABRICATED BY SELECTIVE LASER MELTING (SLM) M.Q. Chu¹, X.W. Zhou¹, X.F. Sun¹, L. Wang¹; ¹COMAC, China |
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15:00 | 15:30 | 4.3.1 |
EFFECTS OF NUMERICAL MODELING CHOICES FOR HEATED JETS IN CROSS FLOW K.C. Morais¹, D.F. Abreu¹, R. Papa¹, L. Tobaldini Neto¹, L.C.C. Santos¹; ¹EMBRAER S. A., Brazil | ||||
15:30 | 16:00 | 4.3.2 |
VISCOUS FLUID SIMULATION WITH THE VORTEX ELEMENT METHOD O.S. Kotsur¹, G.A. Shcheglov¹; ¹Bauman Moscow State Technical University, Russia | ||||
16:00 | 16:30 | 4.3.3 |
LAUNCHER AERODYNAMIC ANALYSIS WITH PLUME EFFECTS A. Viviani, University of Campania, Italy; G. Pezzella, Italian Aerospace Research Centre, Italy |
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15:00 | 15:30 | 5.3.1 |
ADAPTIVE DESIGN OF EXPERIMENT BASED ON GAUSSIAN PROCESS MODELS WITH NONSTATIONARY KERNEL APPLIED TO WIND TUNNEL TESTING U.H. Choi¹, J.H. Kim¹, Y.B. Lee, Agency for Defense Development, South Korea; J.M. Ahn¹; ¹KAIST, South Korea | ||||
15:30 | 16:00 | 5.3.2 |
RLG BASED REAL-TIME MODEL ATTITUDE DETERMINATION SYSTEM DEVELOPMENT FOR LARGE LOW SPEED FACILITY OF CARDC F. Litao¹, H. Zhiyuan¹, W. Zhigang¹; ¹CARDC, China | ||||
16:00 | 16:30 | 5.3.3 |
THE INFLUENCE OF HIGH-SPEED SPIV DATA PROCESSING PARAMETERS ON AIRCRAFT WING VORTEX WAKE ASSESSMENT K. Garry¹, D. Di Pasquale¹, S. Prince¹, N.J. Lawson¹; ¹Cranfield University, United Kingdom |
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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 |
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15:00 | 15:30 | 7.3.1 |
THE STUDIES ON LOW-NOISE LAMINAR WING REGIONAL AIRCRAFT N.A. Pushchin, TsAGI, Russia | ||||
15:30 | 16:00 | 7.3.2 |
Lecture canceled | ||||
16:00 | 16:30 | 7.3.3 |
WING TWIST OPTIMISATION USING AERODYNAMIC SOLVERS OF DIFFERENT FIDELITY G. Yang¹, A. Da Ronch¹, D. Kharlamov¹, J. Drofelnik¹; ¹University of Southampton, United Kingdom |
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15:00 | 15:30 | 8.3.1 |
MODELLING OF FLUTTER CHARACTERISTICS OF AIRCRAFT WING WITH PYLON-MOUNTED ENGINE NACELLE Q. Yu¹, S. Lee¹, M. Damodaran¹, B.C. Khoo¹; ¹National University of Singapore, Singapore | ||||
15:30 | 16:00 | 8.3.2 |
AEROELASTIC PROPERTIES OF ACTIVE WINGLETS G.A. Amiryants¹, S.E. Paryshev¹, A.V. Grigoriev¹; ¹TsAGI, Russia | ||||
16:00 | 16:30 | 8.3.3 |
FLUTTER ANALYSIS OF TWIN TURBOPROP AIRCRAFT WITH TIP-TANKS J. Cecrdle¹, O. Vich¹; ¹Aeronautical Research and Test Institute (VZLU) , Czech Republic |
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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 |
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15:00 | 15:30 | 10.3.1 |
A HYBRID DIGITAL-PROPORTIONAL HYDRAULIC ACTUATION SYSTEM FOR AIRCRAFT FLIGHT CONTROL A. Dell’Amico¹, D. Simon¹, S. Ward¹, L.P.G. Pinto², B. Lantto¹, V. De Negri², P. Krus, Linköping University, Sweden; ¹Saab AB, Sweden ;²Federal University of Santa Catarina, Brazil | ||||
15:30 | 16:00 | 10.3.2 |
SELF-INDUCED FAULT OF A HYDRAULIC SERVO VALVE T. Seung, Program Management Office Aeronautics Research / DLR del. iABG, Germany |
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15:00 | 15:30 | 11.3.1 |
FLIGHT DYNAMICS MODELING AND TRIM CURVES OF A CONCEPTUAL SEMI-TANDEM WING VTOL UAV A.C. Daud Filho¹, E.M. Belo¹; ¹EESC-USP, Brazil | ||||
15:30 | 16:00 | 11.3.2 |
SCALABLE DESIGN APPROACH TO ANALYZE FLIGHT MECHANICAL PERFORMANCE OF TILT-WING UAVS M. Schütt¹, T. Islam¹, P. Hartmann¹, D. Moormann¹; ¹Institute of Flight System Dynamics, RWTH Aachen University , Germany | ||||
16:00 | 16:30 | 11.3.3 |
POTENTIAL BENEFITS ASSESSMENT ON HOME DELIVERY SERVICE USING MULTIPLE DRONES H. Omagari, Department of Aeronautics and Astronautics, Kyushu University, Japan |
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15:00 | 15:30 | 12.3.1 |
HUMAN-MACHINE INTERFACES AND INTERACTIONS FOR MULTI UAS OPERATIONS Y. Lim¹, K. Ranasinghe¹, A. Gardi¹, N. Ezer, Northrop Grumman Corporation, United States; R. Sabatini¹; ¹RMIT University, Australia | ||||
15:30 | 16:00 | 12.3.2 |
LOW LEVEL TRAFFIC MONITORING: RPAS CONCEPT OF OPERATION AND DEVELOPEMENT OF A GROUND BASED SYSTEM P. Le Blaye¹, C. Le Tallec¹; ¹ONERA - The French aerospace lab, France | ||||
16:00 | 16:30 | 12.3.3 |
HUMAN FACTOR IN UNMANNED AIRCRAFT SYSTEM FLIGHT TEST F. Wang¹, S.-J. Qi¹, X.-L. Wu¹; ¹Chinese Flight Test Establishment, China |
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10:00 | 10:30 | 1.4.1 |
CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATION A. Seitz¹, F. Peter¹, J. Bijewitz¹, A. Habermann¹, Z. Goraj², M. Kowalski², A. Castillo Pardo³, C.A. Hall³, F. Meller, Airbus Innovations, Germany; R. Merkler, MTU Aero Engines, Germany; O. Petit*, S. Samuelsson*, B. Della Corteº, M. van Sluisº, G. Wortmann, Siemens AG, Germany; M. Dietz, ARTTIC, Germany; ¹Bauhaus Luftfahrt e.V., Germany ;²Warsaw University of Technology, Poland ;³University of Cambridge, United Kingdom ;*Chalmers University of Technology, Sweden ;ºTechnical University of Delft, Netherlands | ||||
10:30 | 11:00 | 1.4.2 |
SYSTEM-LEVEL ASSESSMENT OF TAIL-MOUNTED PROPELLERS FOR REGIONAL AIRCRAFT R. Vos¹, M.F.M. Hoogreef¹; ¹Delft University of Technology, Netherlands | ||||
11:00 | 11:30 | 1.4.3 |
EXPLORATION OF THE AIRBUS "NAUTILIUS" ENGINE INTEGRATION CONCEPT L. Wiart, ONERA, France; C. Negulescu, AIRBUS, France | ||||
11:30 | 12:00 | 1.4.4 |
FLEXFLOIL SHAPE ADAPTIVE CONTROL SURFACES-FLIGHT TEST AND NUMERICAL RESULTS S. Kota, FlexSys Inc, United States; J.R.R.A. Martins, University of Michigan, United States |
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10:00 | 10:30 | 2.4.1 |
BLENDED WING BODY TRANSPORT AIRCRAFT RESEARCH & DEVELOPMENT J.T. Bonet, Boeing Research & Technology, United States | ||||
10:30 | 11:00 | 2.4.2 |
SINGLE-AISLE AIRLINER DISRUPTION WITH A SINGLE-DECK BLENDED-WING-BODY M.A. Page¹, E.J. Smetak¹, S.L. Yang¹; ¹DZYNE Technologies Incorporated, United States | ||||
11:00 | 11:30 | 2.4.3 |
SUBSONIC ULTRA-GREEN AIRCRAFT RESEARCH: TRANSONIC TRUSS-BRACED WING TECHNICAL MATURATION C.K. Droney¹, N.A. Harrison¹, G.M. Gatlin, NASA Langley Research Center, United States; ¹The Boeing Company, United States | ||||
11:30 | 12:00 | 2.4.4 |
DESIGN AND DEVELOPMENT OF THE D8 COMMERCIAL TRANSPORT CONCEPT B. Yutko¹, N. Titchener¹, C. Courtin¹, W. Lieu¹, L. Wirsing¹, D. Hall¹, J. Tylko¹, J. Chambers¹, T. Roberts¹, C. Church¹; ¹Aurora Flight Sciences, United States |
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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 |
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10:00 | 10:30 | 4.4.1 |
"FAST" CFD METHODS IN AIRCRAFT SYSTEM DESIGN. APPLICATION TO C295W MODIFICATIONS. C. González Biedma, Airbus D&S, Spain | ||||
10:30 | 11:00 | 4.4.2 |
MORPHING WING WITH SURFACE DISCONTINUITY - COMPARATIVE TESTS A. Tarnowski¹, T. Goetzendorf-Grabowski¹, J. Mieloszyk¹; ¹Warsaw University of Technology, Poland | ||||
11:00 | 11:30 | 4.4.3 |
HIGHER FIDELITY TRANSONIC AERODYNAMIC MODELING IN PRELIMINARY AIRCRAFT DESIGN A. Crovato¹, G. Dimitriadis¹, V.E. Terrapon¹; ¹University of Liege, Belgium |
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10:00 | 10:30 | 5.4.1 |
UNSTEADY AERODYNAMIC CHARACTERISTICS OF THE OSCILLATING AIRFOIL USING MSBS Y.H. Sung¹, J.S. Han¹, J.H. Han¹; ¹KAIST, South Korea | ||||
10:30 | 11:00 | 5.4.2 |
DESIGN OF AN INSTRUMENTED STATOR VANE FOR UNSTEADY PRESSURE MEASUREMENTS USING MEMS MICROPHONES B. Martinez R. Jr.¹, L.C. Caldas¹, R.G. Cuenca, Federal University of Santa Catarina, Brazil; R. Lauterjung Q., Embraer S/A, Brazil; P.C. Greco Jr.¹; ¹University of Sao Paulo, Brazil | ||||
11:00 | 11:30 | 5.4.3 |
EVALUATION OF TRANSONIC BUFFETING ONSET BOUNDARY ESTIMATED BY TRAILING EDGE PRESSURE DIVERGENCE AND RMS DATA OF WING VIBRATION R.S. Sousa, EMBRAER, Brazil; R.G.A. da Silva¹, R.d.M. Girardi¹; ¹ITA, Brazil | ||||
11:30 | 12:00 | 5.4.4 |
TIME-RESOLVED PRESSURE MEASUREMENTS FOR AN AIRFOIL WITH SELF-SUSTAINED SHOCK OSCILATIONS H.F. Leite¹, R.G.A. da Silva¹, A.C. Avelar, IAE, Brazil; ¹ITA, Brazil |
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10:00 | 10:30 | 6.4.1 |
PREDICTIVE ANALYSIS OF STITCHED AEROSPACE STRUCTURES FOR ADVANCED AIRCRAFT B. Horton¹, Y. Song¹, D. Jegley², F. Collier², J. Bayandor¹; ¹CRashworthiness for Aerospace Structures and Hybrids (CRASH) Lab, United States ;²NASA Langley Research Center, United States | ||||
10:30 | 11:00 | 6.4.2 |
DESIGNING PRIMARY STRUCTURES WITH STITCHED COMPOSITES A. Velicki, The Boeing Company, United States | ||||
11:00 | 11:30 | 6.4.3 |
MULTIFUNCTIONAL COMPOSITE PROCESSED USING EMBROIDERY TECHNOLOGY T. Ikeda, Chubu University, Japan; M. Ishigami¹, T. Nishihara¹; ¹Nagoya University, Japan | ||||
11:30 | 12:00 | 6.4.4 |
MODIFIED WHITNEY-NUISMER CRITERIA FOR PREDICTION OF NOTCHED STRENGTH OF COMPOSITE LAMINATES C. Wallner, USP/Embraer, Brazil; S.F.M. Almeida, Universidade de Sao Paulo, Brazil; C. Kassapoglou, TU Delft, Netherlands |
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10:00 | 10:30 | 7.4.1 |
EXHAUST PLUME EFFECT OF WINGED TWO-STAGE-TO-ORBIT SEPARATION AT ASCENT USING AERODYNAMIC-FLIGHT DYNAMICS TECHNIQUE H. Iwafuji, Tokyo Metropolitan University, Japan | ||||
10:30 | 11:00 | 7.4.2 |
NUMERICAL SIMULATION OF THE AERIAL DROP OF WATER FOR FIXED-WING AIRTANKERS X. Zhao¹, P. Zhou¹, X. Yan, No. 38 Research Institute of CETC, China; Y. Weng, Xi’an Jiaotong University, China; X.-L. Yang, Chinese Flight Test Establishment, China; ¹Northwestern Polytechnical University, China | ||||
11:00 | 11:30 | 7.4.3 |
GRID-MODE TRANSONIC STORE SEPARATION ANALYSES USING MODERN DESIGN OF EXPERIMENTS K.A. Jamison, Council of Scientific and Industrial Research (CSIR), South Africa | ||||
11:30 | 12:00 | 7.4.4 |
STORE SEPARATION TRAJECTORY PREDICTIONS AT LOW SPEEDS A. Cenko, AIWS, United States; N. Stathopoulos, L3-MAS, Canada; R. Hobbins, Bombardier, Canada; G. Akroyd, Akroyd Aeronautics, Australia |
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10:00 | 10:30 | 8.4.1 |
AEROELASTIC TAILORING OF COMPOSITE WING BY USING MULTIDISCIPLINARY DESIGN ENVIRONMENT K.A. Balunov¹, V.V. Chedrik¹, F.Z. Ishmuratov¹; ¹TsAGI, Russia | ||||
10:30 | 11:00 | 8.4.2 |
VIRTUAL AIRCRAFT MODEL FOR AEROELASTIC SIMULATION AND LOAD PREDICTION OF A HIGH ASPECT RATIO COMPOSITE SWEPT WING A. Hermanutz¹, M. Hornung¹; ¹Technical University of Munich, Germany | ||||
11:00 | 11:30 | 8.4.3 |
THERMAL-MECHNICAL COUPLING ANALYSIS AND OPTIMIZATION DESIGN ON TPS WITH GAP S. Huo¹, Q. Yan¹, W. Xie, Harbin Institute of Technology , China; ¹Aircraft Strength Research Institute, China | ||||
11:30 | 12:00 | 8.4.4 |
Lecture canceled |
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10:00 | 10:30 | 9.4.1 |
Lecture canceled | ||||
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 |
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10:00 | 10:30 | 10.4.1 |
WIND TUNNEL VIRTUAL FLIGHT TEST FOR A TRANSPORT AIRCRAFT WITH SIMULATED ICE SHAPE L. Guo¹, M. Zhu¹, J. Guan¹, B. Nie¹; ¹China Aerodynamics Research and Development Centre, China | ||||
10:30 | 11:00 | 10.4.2 |
DEVELOPMENT OF A GENERIC FLIGHT TEST MANEUVER INJECTION MODULE C. Krause¹, C. Göttlicher¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, Germany | ||||
11:00 | 11:30 | 10.4.3 |
CHARACTERISTIC HELICOPTER FLIGHT MECHANICS AND MOTION CUEING INTEGRATION INTO THE SIVOR ROBOTIC FLIGHT SIMULATOR: AN OBJECTIVE APPROACH D.F. Hidalgo, Universidad pontificia bolivariana, Colombia; G.B. Rodamilans¹, W.R. de Oliveira¹; ¹CCM-Instituto Tecnologico de Aeronautica, Brazil | ||||
11:30 | 12:00 | 10.4.4 |
KNOWLEDGE ENGINEERING BASED FLIGHT TEST TECHNOLOGY FOR CIVIL AIRCRAFT AIRWORTHINESS CONFORMITY L. Zhaohui¹, L. Gang¹; ¹Chinese Flight Test Establishment, China |
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10:00 | 10:30 | 11.4.1 |
Lecture canceled | ||||
10:30 | 11:00 | 11.4.2 |
GROUND AND FLIGHT TESTING OF A MULTI-SENSOR OBSTACLE DETECTION AND TRACKING SYSTEM FOR RPAS SITUATION AWARENESS J. Gauci¹, K. Theuma¹, R. Archer, Hawk Aerospace, Malta; R. Grech, Idox Health, Malta; D. Zammit-Mangion¹; ¹University of Malta, Malta | ||||
11:00 | 11:30 | 11.4.3 |
POWER LINE COMMUNICATION APPLIED TO FLIGHT TEST INSTRUMENTATION M.V. Ribeiro¹, F.P.V. de Campos¹, S.A. Souza, Smarti9 Ltd., Brazil; A. 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 |
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10:00 | 10:30 | 12.4.1 |
ALGORITHMS AND SYSTEM FOR CURVED AND CONTINUOUS DESCENT TRAJECTORIES IMPROVING FUEL EFFICIENCY IN TMA A. Errico¹, V. Di Vito¹; ¹CIRA – Italian Aerospace Research Center, Italy | ||||
10:30 | 11:00 | 12.4.2 |
PERFORMANCE COMPARISON OF A320 AND 737NG REGARDING THE VERTICAL AND AND SPEED PROFILES IN ADVANCED RNP TO XLS ARRIVALS T. Dautermann¹, T. Ludwig¹, L. Altenscheidt¹, M. Altenscheidt, NavArt, Germany; R. Geister¹, M. Braschczok¹; ¹DLR, Germany | ||||
11:00 | 11:30 | 12.4.3 |
OPERATIONAL CONCEPT AND VALIDATION OF A NEW AIRPORT LOW-LEVEL WIND INFORMATION SYSTEM T. Iijima¹, N. Matayoshi¹, S. Ueda¹; ¹JAXA, Japan | ||||
11:30 | 12:00 | 12.4.4 |
SEMANTICS-BASED SUMMARIZATION OF ATM DATA TO MANAGE INFORMATION OVERLOAD IN PILOT BRIEFINGS C.G. Schuetz¹, B. Neumayr¹, M. Schrefl¹, E. Gringinger, Frequentis AG, Austria; S. Wilson, EUROCONTROL, Belgium; ¹Johannes Kepler University Linz, Austria |
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14:00 | 14:30 | 1.5.1 |
DEVELOPING THE UNMANNED UNCONVENTIONAL CARGO AIRPLANES WITH HYBRID PROPULSION SYSTEM I. Gál¹, D. Rohács¹, J. Rohács¹; ¹Budapest University of Technology and Economics, Hungary | ||||
14:30 | 15:00 | 1.5.2 |
OPTIMIZATION OF MOTOR FOR THE MAXIMIZATION OF SOLAR-POWERED AIRCRAFT PERFORMANCE S. Serokhvostov, MIPT, Russia; T. Churkina, MAI, Russia | ||||
15:00 | 15:30 | 1.5.3 |
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF COOLING CONCEPT FOR AN ELECTRIC PROPULSION SYSTEM FOR AEROBATIC AIRCRAFTS X. Liu¹, F. Ferrari¹, L. Manfriani¹; ¹Zurich University for Applied Science, Switzerland |
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14:00 | 14:30 | 2.5.1 |
A CASE OF SUCESS: MDO APPLIED ON THE DEVELOPMENT OF EMBRAER 175 ENHANCED WINGTIP J. Cavalcanti¹, P. London¹, R. Wallach¹, P. Ciloni¹; ¹Embraer, Brazil | ||||
14:30 | 15:00 | 2.5.2 |
CONTAINERIZED AIR FREIGHT SYSTEM POWERED BY CRYOGENIC FUEL V.I. Chernousov¹, A.A. Krutov¹, E.A. Pigusov¹; ¹TsAGI, Russia | ||||
15:00 | 15:30 | 2.5.3 |
DESIGN FOR COMFORT: AIRCRAFT INTERIORS DESIGN ASSESSMENT THROUGH A HUMAN CENTERED RESPONSE MODEL APPROACH S. Bagassi¹, F. Lucchi¹, F. De Crescenzio¹, S. Piastra¹; ¹University of Bologna, Italy |
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14:00 | 14:30 | 3.5.1 |
COMBINED AIRFRAME AND SUBSYSTEMS EVOLVABILITY EXPLORATION DURING CONCEPTUAL DESIGN A.S.J. van Heerden¹, M.D. Guenov¹, A. Molina-Cristóbal¹, A. Riaz¹, Y. Bile¹; ¹Cranfield University, United Kingdom | ||||
14:30 | 15:00 | 3.5.2 |
A TECHNIQUE FOR CAPTURING STAKEHOLDER PREFERENCES AND KNOWLEDGE IN EARLY DESIGN STUDIES S. Sartorius, United States; M. Hornung, Technical University of Munich Institute of Aircraft Design, Germany | ||||
15:00 | 15:30 | 3.5.3 |
ROBUST DESIGN OPTIMIZATION OF BENCHMARK AERODYNAMIC CASE BASED ON POLYNOMIAL CHAOS EXPANSION Z. Huan¹, G. Zhenghong¹; ¹Northwestern Polytechnical University , China |
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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 |
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14:00 | 14:30 | 6.5.1 |
A FRAMEWORK FOR UNCONVENTIONAL LANDING GEAR CONFIGURATION MODELLING U. Kling¹, T. Brügge¹, F. Peter¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany | ||||
14:30 | 15:00 | 6.5.2 |
GLOBAL-LOCAL STRUCTURAL ANALYSIS OF COMPOSITE WINGS E. Carrera¹, A. Pagani¹, G.H.C. Silva, Embraer S.A., Brazil; ¹Politecnico di Torino, Italy | ||||
15:00 | 15:30 | 6.5.3 |
BUCKLING/POSTBUCKLING OPTIMIZATION OF STIFFENED COMPOSITE PANELS BASED ON SENSITIVITY ANALYSIS L. Dong¹, D. Cui, Science and Technology committee, China; R. Zhang¹; ¹Chinese Aeronautical Establishment, China |
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14:00 | 14:30 | 7.5.1 |
MITIGATING RISK OF PRODUCIBILITY FAILURES IN PLATFORM CONCEPT DEVELOPMENT J. Madrid¹, J. Landahl¹, R. Söderberg¹, H. Johannesson¹, J. Lööf, GKN Aerospace, Sweden; ¹Chalmers University of Technology, Sweden |
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14:00 | 14:30 | 8.5.1 |
HIGH FREQUENCY MODAL TEST AND DYNAMIC PERFORMANCE EVALUATION OF TURBINE ROTOR BLADES J. Qin¹, X. Gao¹, W.C. Huang¹, G. Yao¹; ¹ASRI, China | ||||
14:30 | 15:00 | 8.5.2 |
HIGH PERFORMANCE PNEUMATIC SHOCK-ABSORBERS FOR AERONAUTICAL APPLICATIONS R. Faraj, Institute of Fundamental Technological Research, Poland |
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14:00 | 14:30 | 9.5.1 |
MATCHING BETWEEN METAMODEL AND OPTIMIZATION TOOL APPLIED IN A MULTISTAGE AXIAL-FLOW COMPRESSOR AIMING DESIGN IMPROVEMENT V. Monteiro¹, K. Iha¹, O.F.R. Silva¹, T. Ebel, Concepts Nrec, United States; ¹ITA, Brazil | ||||
14:30 | 15:00 | 9.5.2 |
NUMERICAL AND EXPERIMENTAL STUDY OF THE EFFECT OF CIRCUMFERENTIAL GROOVES ON HPC LAST STAGE PERFORMANCE V.I. Mileshin¹, A.M. Petrovichev¹, S.I. Baeva¹, V.V. Zhdanov¹; ¹Central Institute of Aviation Motors, Russia | ||||
15:00 | 15:30 | 9.5.3 |
ADAPTTIVE GTE SURGE PROTECTION SYSTEM WITH SELECTIVE CONTROL OF ACTUATORS L.G. Bliznyukov¹, M.G. Kesselman¹, V.I. Chernyshov¹, S.A. Smetanin¹; ¹Central Institute of Aviation Motors, Russia |
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14:00 | 14:30 | 10.5.1 |
ON REAL–TIME SIMULATION OF FLEXIBLE AIRCRAFT WITH PHYSICS–DERIVED MODELS J.A. Paulino¹, A. Da Ronch, University of Southampton, United Kingdom; A.B. Guimarães Neto¹, F.J. Silvestre¹, M.A.V. Morales¹; ¹Instituto Tecnológico de Aeronáutica, Brazil | ||||
14:30 | 15:00 | 10.5.2 |
MANEUVERABILITY ASSESSMENT FOR FAULTY AIRPLANE BY IFS WITH SIMULTANEOUS MODEL-MATCHING FOR GUST AND HANDLING RESPONSES M. Sato, Japan Aerospace Exploration Agency, Japan | ||||
15:00 | 15:30 | 10.5.3 |
BAYESIAN APPROACH TO FLIGHT CHARACTERISTICS MODELING WITH REAL FLIGHT DATA M. Naruoka, Japan Aerospace Exploration Agency, Japan |
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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 (HAIC) ICING EVENTS FROM TOTAL AIR TEMPERATURE A. Rodríguez-Sanz¹, R.M. Arnaldo¹, E. Sánchez Ayra, Universidad Politécnica de Madrid (UPM) & IBERIA, Spain; F. Gómez Comendador¹; ¹Universidad Politécnica de Madrid (UPM), Spain | ||||
15:00 | 15:30 | 11.5.3 |
NUMERICAL SIMULATION OF ICE ACCRETION INFLUENCED BY AN ANTI-ICING HEATING SYSTEM K. Szilder, Aerospace, National Research Council, Canada; E. Lozowski, University of Alberta, Canada |
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14:00 | 14:30 | 12.5.1 |
SIMULATION STUDY FOR VFR AIRCRAFT AND SMALL UNMANNED AIRCRAFT SYSTEMS (SUAS) MIXED OPERATIONS IN LOW LEVEL AIRSPACE H. Hirabayashi¹, D. Toratani¹, A. Kohmura¹; ¹ENRI, Japan | ||||
14:30 | 15:00 | 12.5.2 |
URBAN AIR TRANSPORTATION JOURNEY TIME COMPARISON FOR MELBOURNE METROPOLITAN AREA L. Swadesir¹, C. Bil¹; ¹RMIT University, Australia | ||||
15:00 | 15:30 | 12.5.3 |
ADAPTIVE LANDING SEQUENCING USING BIPARTITE GRAPHS AND PERFECT MATCHING M. Hickson¹, C. Bil¹; ¹RMIT University, Australia |
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16:00 | 16:30 | 1.6.1 |
Lecture canceled | ||||
16:30 | 17:00 | 1.6.2 |
FLIGHT TEST OF A FUEL-CELL/BATTERY/SUPERCAPACITOR TRIPLE HYBRID UAV PROPULSION SYSTEM A. Gong¹, J.L. Palmer, Defence Science and Technology Group, Australia; D. Verstraete¹; ¹The University of Sydney, Australia | ||||
17:00 | 17:30 | 1.6.3 |
Lecture canceled | ||||
17:30 | 18:00 | 1.6.4 |
Lecture canceled |
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16:00 | 16:30 | 2.6.1 |
NEURAL NETWORK DRIVEN ADJOINT SOLVER BETWEEN FLIGHT-PATH OPTIMIZATION AND PANEL METHOD FOR AIRCRAFT DESIGN M. Naoto, the University of Tokyo, Japan | ||||
16:30 | 17:00 | 2.6.2 |
LIFE CYCLE COST ESTIMATION METHODOLOGY FOR HYPERSONIC TRANSPORTATION SYSTEMS R. Fusaro¹, D. Ferretto¹, V. Vercella¹, N. Viola¹, V. Fernandez Villace², J. Steelant²; ¹Politecnico di Torino, Italy ;²ESA-ESTEC, Netherlands | ||||
17:00 | 17:30 | 2.6.3 |
ANALYSIS OF THE INFLUENCE OF THE EXTERNAL CONFIGURATION ON THE WAVE DRAG OFSUPERSONIC BUSINESS JETS M.U. Quirino¹, M. Calvo, École de l’air - French Air Force Academy, France; R.C. Munjulury, Linkoping University, Sweden; A.M. Abdalla¹; ¹University of São Paulo - USP - Brazil, Brazil | ||||
17:30 | 18:00 | 2.6.4 |
ANALYSIS OF LOW-BOOM CHARACTERISTICS OF SUPERSONIC WAVERIDER P. Boonjaipetch, Tohoku University, Japan |
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16:00 | 16:30 | 3.6.1 |
MODEL-BASED CONTROL LOGICS DEVELOPMENT OF AIRCRAFT SYSTEMS V.L. Takase¹, H.H. Sano¹; ¹EMBRAER S.A., Brazil | ||||
16:30 | 17:00 | 3.6.2 |
COUPLING OF PREDESIGN AND PERFORMANCE TOOLS FOR TRANSIENT AIRCRAFT ENGINE ANALYSES M. Vieweg¹, C. Klein¹, S. Reitenbach¹, F. Wolters¹, R.-G. Becker¹; ¹German Aerospace Center , Germany | ||||
17:00 | 17:30 | 3.6.3 |
A 7D TRADE D.K. Howarth, MEE Inc., United States | ||||
17:30 | 18:00 | 3.6.4 |
A NOVEL FMI AND TLM-BASED DESKTOP SIMULATOR FOR DETAILED STUDIES OF THERMAL PILOT COMFORT R. Hällqvist¹, J. Schminder², M. Eek¹, R. Braun², R. Gårdhagen², P. Krus²; ¹Saab Aeronautics, Sweden ;²Linköping University, Sweden |
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16:00 | 16:30 | 4.6.1 |
CFD VERIFICATION AND VALIDATION FOR INDUSTRIAL APPLICATIONS M. Mani¹, A. Cary¹; ¹Boeing, United States | ||||
16:30 | 17:00 | 4.6.2 |
SHIP-HELICOPTER OPERATIONAL LIMITATION ENVELOPE DEFINITION WITH CFD RESULTS AND WIND TUNNEL DATA C.F. Rafael¹, G.A.L. da Silva¹, M.J.M. Guedes, Brazilian Navy, Brazil; ¹Aerothermal Solutions and Software Distributor, Brazil | ||||
17:00 | 17:30 | 4.6.3 |
CFD-BASED STUDY OF DAMAGE LOCATION INFLUENCE ON AERODYNAMICS OF WINGS WITH SINGLE AND DOUBLE THROUGH HOLES Z.W. Chen¹, Y. Pei¹, X.W. Yang¹, H. Ma¹; ¹Northwestern Polytechnical University, China | ||||
17:30 | 18:00 | 4.6.4 |
NUMERICAL SIMULATION OF OPERATING PROCESS ELEMENTS FOR COMBUSTION CHAMBERS OF PERSPECTIVE GTE P.A. Semenev, Central Institute of Aviation Motors, Russia |
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16:00 | 16:30 | 5.6.1 |
ALL JAPAN STUDENT'S INDOOR FLYING ROBOT CONTEST T. Tsuchiya, The University of Tokyo, Japan | ||||
16:30 | 17:00 | 5.6.2 |
THE AERONAUTICAL SOCIETY OF SOUTH AFRICA AEROSPACE CHALLENGE J.S. Monk, CSIR, South Africa | ||||
17:00 | 17:30 | 5.6.3 |
Lecture canceled |
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16:00 | 16:30 | 6.6.1 |
A PASSIVE-ADAPTIVE WING FOR DRAG REDUCTION C.B. York, University of Glasgow, United Kingdom; Y.B. Murta, Embraer, Brazil; S.F.M. Almeida, University of Sao Paulo, Brazil | ||||
16:30 | 17:00 | 6.6.2 |
INVESTIGATION OF SYNERGETIC EFFECT INFLUENCE ON STRENGTH CHARACTERISTICS AND WEIGHT EFFICIENCY OF LOAD-BEARING AVIATION STRUCTURES E.A. Dubovikov¹, M.C. Zichenkov¹, I.V. Mareskin¹, A.V. Chernov¹, A.N. Shanygin¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia | ||||
17:00 | 17:30 | 6.6.3 |
A NUMERICAL ANALYSIS OF THE DYNAMICS OF A TENSEGRITY-MEMBRANE STRUCTURE L.H. Teixeira¹, J.H. Izuka, Faculty of Applied Sciences - UNICAMP, Brazil; P. Gonzalez¹, P. Kurka¹; ¹Faculty of Mechanical Engineering - UNICAMP, Brazil | ||||
17:30 | 18:00 | 6.6.4 |
AN XFEM FRAMEWORK FOR ONSET AND CRACK PROPAGATION FOR COMPOSITES BASED ON ACTION PLANE THEORY M.V. Angelo¹, M.L. Ribeiro¹, V. Tita¹; ¹University of Sao Paulo, Brazil |
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16:00 | 16:30 | 7.6.1 |
MULTI-POINT AERODYNAMIC OPTIMIZATION DESIGN OF A DUAL-AISLE AIRPLANE WING R.Z. Li¹, M. Zhang², M.H. Zhang², Y.F. Zhang¹, H.X. Chen¹; ¹Tsinghua University, China ;²Shanghai Aircraft Design and Research Institute, China | ||||
16:30 | 17:00 | 7.6.2 |
MULTILEVEL COLLABORATIVE AERODYNAMIC DESIGN OPTIMIZATION BASED ON SOBOL’ GLOBAL SENSITIVITY ANALYSIS C. Wang¹, Z. Gao¹, P. Liu¹, Y. Na¹, X. Zhu¹; ¹Northwestern Polytechnical University, China | ||||
17:00 | 17:30 | 7.6.3 |
SURROGATE-BASED OPTIMIZATION METHOD APPLIED TO MULTIDISCIPLINARY DESIGN OPTIMIZATION ARCHITECTURES C.-Z. Xu¹, Z.-H. Han¹, K.-S. Zhang¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China | ||||
17:30 | 18:00 | 7.6.4 |
COMBINING ADJOINT-BASED AND SURROGATE-BASED OPTIMIZATIONS FOR BENCHMARK AERODYNAMIC DESIGN PROBLEMS H. Wang¹, Z.-H. Han¹, S.-Q. Han¹, Y. Zhang¹, C.-Z. Xu¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China |
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16:00 | 16:30 | 8.6.1 |
PROPELLER INFLUENCE ON THE STABILITY OF HALE AIRCRAFT P.C. Teixeira¹, C.E.S. Cesnik¹; ¹University of Michigan, United States | ||||
16:30 | 17:00 | 8.6.2 |
NONLINEAR AEROELASTIC REDUCED ORDER MODELS USING MODAL COORDINATES R.R. Medeiros¹, C.E.S. Cesnik¹, E.B. Coetzee, Airbus Operations, United Kingdom; ¹University of Michigan, United States | ||||
17:00 | 17:30 | 8.6.3 |
NONLINEAR STATIC AEROELASTIC AND TRIM ANALYSIS OF HIGHLY FLEXIBLE AIRCRAFT C. Zhang¹, Z. Zhou¹, P. Meng¹; ¹Northwestern Polytechnical University, China | ||||
17:30 | 18:00 | 8.6.4 |
AEROELASTIC WIND TUNNEL EXPERIMENT OF A HIGH-ASPECT-RATIO WING MODEL AGAINST GEOMETRICAL NON-LINEARITY W. Qian¹, Y. Bai¹, H. Zeng, Shenyang Aircraft Design Institute, China; R. Yang¹; ¹Dalian University of Technology, China |
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16:00 | 16:30 | 9.6.1 |
MULTIOBJECTIVE MULTIPARAMETRIC OPTIMIZATION OF PROPULSION SYSTEM FOR ADVANCED CIVIL AIRCRAFT IN DISTRIBUTED ENVIRONMENT OF COLLABORATIVE MDO SYSTEM DEVELOPED IN AGILE PROJECT A. Mirzoyan¹, A. Isyanov¹, D. Fokin¹, R. D´Ippolito², R. Lombardi²; ¹CIAM, Russia ;²Noesis, Belgium | ||||
16:30 | 17:00 | 9.6.2 |
STUDIES ON PROPULSION AND ON-BOARD SYSTEMS MATCHING IN AGILE PROJECT DISTRIBUTED COLLABORATIVE MDO ENVIRONMENT APPLYING FOR ADVANCED REGIONAL AND MEDIUM HAUL JET M. Fioriti, Politecnico di Torino, Italy; L. Boggero, German Aerospace Center (DLR), Germany; A. Mirzoyan¹, A. Isyanov¹; ¹CIAM, Russia | ||||
17:00 | 17:30 | 9.6.3 |
COMMUNICATION BETWEEN PS AND AIRCRAFT SYSTEMS IN COLLECTIVE MDO SYSTEM IN AGILE PROJECT P.D. Toktaliev, Central Institute of Aviation Motors, Russia | ||||
17:30 | 18:00 | 9.6.4 |
PROPULSION SYSTEM - AIRFRAME INTEGRATION AND OPTIMIZATION OF CIVIL AIRCRAFT- AGILE EU PROJECT K.S. Anisimov¹, A.A. Savelyev¹, I.A. Kursakov¹, A.V. Lysenkov¹, A.A. Mirzoyan, CIAM, Russia; P.S. Prakasha, Institute of System Architectures in Aeronautics, DLR, Germany; ¹TSAGI, Russia |
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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 |
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16:00 | 16:30 | 11.6.1 |
FORCE FIGHT COMPENSATION FOR REDUNDANT ELECTRO-MECHANICAL FLIGHT CONTROL ACTUATORS R. Kowalski¹, J. Windelberg¹, R. Ladner², M. Rottach²; ¹German Aerospace Center (DLR e.V.), Germany ;²Liebherr-Aerospace Lindenberg GmbH, Germany | ||||
16:30 | 17:00 | 11.6.2 |
A MORE INTEGRATED DESIGN APPROACH FOR EMBEDDED MECHATRONIC SYSTEMS: APPLICATION TO ELECTRICAL THRUST REVERSER ACTUATION SYSTEMS S. Delbecq¹, M. Budinger, Institut Clément Ader (UMR CNRS 5312), France; J. Piaton¹; ¹Safran Electronics & Defense, France | ||||
17:00 | 17:30 | 11.6.3 |
POSITION SYNCHRONIZATION OF AEROSPACE ELECTROMECHANICAL ACTUATORS FOR DISTRIBUTED ELECTRICAL ACTUATION SYSTEM J. Fu¹, J.-C. Mare, INSA-Toulouse, France; Y. Fu¹; ¹Beihang University, China | ||||
17:30 | 18:00 | 11.6.4 |
PIO SUSCEPTIBILITY IN FLY-BY-WIRE SYSTEMS H.C. Moura¹, G.S.P. Alegre¹, J.H. Bidinotto¹, E.M. Belo¹; ¹University of São Paulo, Engineering School of São Carlos, Brazil |
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16:00 | 16:30 | 12.6.1 |
DECISION-MAKING INFORMATION SYSTEM FOR MULTIMODAL DISRUPTION MANAGEMENT: SYSTEM ARCHITECTURE AND CONCEPT OF OPERATIONS F. Jiménez Serrano, 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 |
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09:30 | 10:00 | 1.7.1 |
MULTI-DISCIPLINARY ANALYSIS AND OPTIMIZATION JAVA TOOL FOR AIRCRAFT DESIGN V. Trifari¹, M. Ruocco¹, V. Cusati¹, F. Nicolosi¹, A. De Marco¹; ¹University of Naples Federico II, Italy | ||||
10:00 | 10:30 | 1.7.2 |
COUPLED ADJOINT AEROSTRUCTURAL OPTIMIZATION FRAMEWORK FOR PRELIMINARY AIRCRAFT DESIGN C.M. Boozer¹, A. Elham¹; ¹Braunschweig University of Technology, Germany | ||||
10:30 | 11:00 | 1.7.3 |
AIRCRAFT LOADS PREDICTION USING ENHANCED SIMULATION Y. Lemmens, Siemens PLM, Belgium; T. Wilson, Airbus Operations Ltd, United Kingdom; J.E. Cooper, University of Bristol, United Kingdom | ||||
11:00 | 11:30 | 1.7.4 |
GENERAL PARAMETERS DESIGN METHOD OF CANARD ROTARY WING AIRPLANE UNDER THE INFLUENCE OF POWER SYSTEM Y. Na, School of Aeronautics Northwestern Polytechnical University, China; Z.-H. Gao¹, Y.-P. Deng¹, L. Tian¹, H.-G. Gao¹; ¹School of Aeronautics Northwestern Polytechnical University, China | ||||
11:30 | 12:00 | 1.7.5 |
RESERCH ON KEY TECHNOLOGY OF INTELLIGENT CIVIL AIRCRAFT Z. Li¹, D. Xie¹, B. Gao¹, Z. Yao¹; ¹Shanghai Aircraft Design and Research Institute, China |
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09:30 | 10:00 | 2.7.1 |
Lecture canceled | ||||
10:00 | 10:30 | 2.7.2 |
UTILIZATION OF SCALING LAWS AND UNCERTAINTY QUANTIFICATION TO INFORM TECHNOLOGY DEVELOPMENT EXPERIMENTATION K.G. Schwartz¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States | ||||
10:30 | 11:00 | 2.7.3 |
A SYSML-BASED APPROACH TO EXPLORING INNOVATIVE SYSTEM IDEAS FOR AERONAUTICAL APPLICATIONS J. Abulawi, HAW Hamburg, Germany | ||||
11:00 | 11:30 | 2.7.4 |
APPLICATION OF AGILE MODEL-BASED SYSTEMS ENGINEERING IN AIRCRAFT CONCEPTUAL DESIGN G.P. Krupa, Federal University of Itajubá, Brazil | ||||
11:30 | 12:00 | 2.7.5 |
A BOND GRAPH-ORIENTED METHOD FOR ASSESSMENT OF FAILURES IN AN AIRCRAFT HYDRAULIC BRAKE SYSTEM M. Maia Neto¹, L.C.S. Goes¹; ¹ITA, Brazil |
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09:30 | 10:00 | 3.7.1 |
FATIGUE AND CRACK PROPAGATION LIFE IMPROVEMENT QUANTIFICATION FOR COLD-WORKED HOLES OUTSIDE NOMINAL CONDITIONS L. Zaplana ¹, I. Rivero¹, B. García-Fogeda ¹, J. Gómez-Escalonilla¹; ¹AIRBUS DS, Spain | ||||
10:00 | 10:30 | 3.7.2 |
USING THE LEAD CRACK CONCEPT TO REDUCE DURABILITY TEST DURATION L. Molent, DST, Australia | ||||
10:30 | 11:00 | 3.7.3 |
Lecture canceled | ||||
11:00 | 11:30 | 3.7.4 |
THE EFFECT OF STRUCTURAL PARAMETERS OF AIRCRAFT PANEL ON VIBRATION FATIGUE LIFE P. Li¹, J. Ma¹; ¹Aircraft strength research institute, China |
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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, United States | ||||
10:00 | 10:30 | 4.7.2 |
TURBULENCE MODEL CONDITIONING FOR VORTEX DOMINATED FLOWS BASED ON EXPERIMENTAL RESULTS M. Moioli¹, C. Breitsamter¹, K.A. Sørensen, Airbus Defence and Space, Germany; ¹Technical University of Munich, Germany | ||||
10:30 | 11:00 | 4.7.3 |
IMPROVED DELAYED DETACHED EDDY SIMULATION OF THE FLOWS AROUND S809 AIRFOIL FOR ANGLES OF ATTACK FROM 0 TO 90 DEGREES W. Yue¹, L. Kang¹, S. Wenping¹, H. Zhonghua¹; ¹Northwestern Polytechnical University, China | ||||
11:00 | 11:30 | 4.7.4 |
AERODYNAMIC EVALUATION OF THE EXTERNAL FLOW OVER PICKUP TRUCKS E.-K. Mascia¹, O. de Almeida¹; ¹Federal University of Uberlandia, Brazil | ||||
11:30 | 12:00 | 4.7.5 |
A HYBRID LENGTH SCALE SIMILARITY SOLUTION FOR SWIRLING TURBULENT JETS G. Andrews, Purdue University, United States |
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09:30 | 10:00 | 5.7.1 |
OVERVIEW OF DYNAMIC TEST TECHNIQUES AT LOW SPEED AERODYNAMICS INSTITUTE, CARDC Z. Liu¹, H. Sun¹, B. Nie¹, L. Guo¹, F. Cen¹; ¹China Aerodynamics Research and Development Center (CARDC), China | ||||
10:00 | 10:30 | 5.7.2 |
APPLICATION OF THE COMBINED BOUNDARIES TO REDUCE WALL INTERFERENCE FOR NACA 0012 AIRFOIL TESTS S.L. Chernyshev¹, A.I. Ivanov¹, E.V. Streltsov¹, A.O. Volkova¹; ¹Central Aerohydrodynamic Institute n.a. prof. N.E. Zhukovsky, Russia | ||||
10:30 | 11:00 | 5.7.3 |
EVALUATION OF WIND TUNNEL WALL BOUNDARY-LAYER CONTROL FOR 2-D HIGH-LIFT AERODYNAMIC AND AEROACOUSTIC TESTING F.M. Catalano, Aeronautical Engineering Dept. University of São Paulo , Brazil; L.T.L. Pereira, University of São Paulo , Brazil | ||||
11:00 | 11:30 | 5.7.4 |
Lecture canceled |
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09:30 | 10:00 | 6.7.1 |
DEVELOPMENT OF SECONDARY CROSSFLOW INSTABILITY NEAR BREAKDOWN INTO TURBULENCE E. van Bokhorst¹, C. Atkin¹; ¹University of London, United Kingdom | ||||
10:00 | 10:30 | 6.7.2 |
EFFECTS OF THE INTRINSIC THREE-DIMENSIONALIZATION OF LAMINAR SEPARATION BUBBLES ON THE AMPLIFICATION OF EXTERNAL DISTURBANCES D. Rodriguez, Universidade Federal Fluminense, Brazil; E.M. Gennaro, Sao Paulo State University, Brazil | ||||
10:30 | 11:00 | 6.7.3 |
WAVEPACKETS IN TURBULENT FLOW OVER A NACA 4412 AIRFOIL L.I. Abreu¹, A.V.G. Cavalieri¹, P. Schlatter², R. Vinuesa², D. Henningson²; ¹ITA, Brazil ;²KTH, Sweden | ||||
11:00 | 11:30 | 6.7.4 |
CONTROL OF STREAKY DISTURBANCES IN THE BOUNDARY LAYER OVER A FLAT PLATE P. Morra¹, K. Sasaki², A. Cavalieri², A. Hanifi¹, D. Henningson¹; ¹KTH Royal Institute of Technology, Sweden ;²Instituto Tecnológico de Aeronáutica, Brazil | ||||
11:30 | 12:00 | 6.7.5 |
LAMINAR-TURBULENT TRANSITION MECHANISMS OVER WIDELY-SPACED SUCTION HOLES B. Crowley¹, C. Atkin¹; ¹City University of London, United Kingdom |
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09:30 | 10:00 | 7.7.1 |
APPLICATION OF HIGH-ROBUSTNESS BEMT FOR SIMULATION OF UAV-VTOL PROPELLER AT LOW/HIGH ADVANCE RATIO Z. Fan¹, Z. Zhou¹, X. Zhu, Science and Technology on UAV Laboratory, NPU, China; ¹School of Aeronautics,Northwestern Polytechnical University, China | ||||
10:00 | 10:30 | 7.7.2 |
AERODYNAMIC DESIGN OF A RIGID COAXIAL ROTOR AIRFOIL IN UNSTEADY FLOW X.-D. Yang¹, M. Huang¹; ¹School of Aeronautics Northwestern Polytechnical University, China | ||||
10:30 | 11:00 | 7.7.3 |
INVESTIGATION ON APPROACH TO CONTROL LIFT DISTRIBUTION OF WING BY DISTRIBUTED PROPELLERS C. Xue¹, Z. Zhou¹, H.-B. Wang¹; ¹Northwestern Polytechnical University, China | ||||
11:00 | 11:30 | 7.7.4 |
ANALYSIS OF XH-59A ROTOR IN FORWARD FIGHT WITH HIGH EFFICIENCY TRIM METHOD P. Zhou¹, X. Zhao¹, L. Deng¹, Y.-F. Lin, China Helicopter Research and Development Institute, China; ¹Northwestern Polytechnical University, China | ||||
11:30 | 12:00 | 7.7.5 |
SIMULATIONS OF UNSTEADY AIRWAKES BEHIND SHIPS IN MOTION W.X. Yuan¹, A. Wall¹, R. Lee¹; ¹National Research Council Canada, Canada |
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09:30 | 10:00 | 8.7.1 |
PRELIMINARY ASSESSMENT OF A WARPING WING CONFIGURATION IN ROLLING CONTROL E. Cestino¹, G. Frulla¹, A. Lanzillotti¹; ¹Politecnico di Torino, Italy | ||||
10:00 | 10:30 | 8.7.2 |
STRUCTURAL DESIGN AND ANALYSIS OF A QUADROTOR FIXED-WING HYBRID UAV WING W. Fang, China; H. Ma, China; H. Zhang, China | ||||
10:30 | 11:00 | 8.7.3 |
STRUCTURAL SIZING OF A ROTORCRAFT FUSELAGE USING AN INTEGRATED DESIGN APPROACH D.B. Schwinn¹, P. Weiand¹, M. Schmid¹, M. Buchwald¹; ¹German Aerospace Center (DLR), Germany | ||||
11:00 | 11:30 | 8.7.4 |
AN ACTIVE-PASSIVE NONLINEAR FINITE ELEMENT MODEL FOR ELECTROMECHANICAL COMPOSITE MORPHING BEAMS R.B. Olympio¹, M.V. Donadon¹, S.G.P Castro, EMBRAER, Brazil; ¹ITA, Brazil | ||||
11:30 | 12:00 | 8.7.5 |
STRUCTURAL OPTIMIZATION AND PROPOSITION OF PRE-SIZING PARAMETERS FOR UAVS WING SPARS F.A. Fenelon¹, G.F.S. Neves¹, R.S. Martins¹; ¹Universidade Federal de Minas Gerais, Brazil |
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09:30 | 10:00 | 9.7.1 |
STUDY ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLERS WITH PROPLETS X. Yang¹, J. Xu¹, B. Wang¹, C. Song¹, S. Zhang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China | ||||
10:00 | 10:30 | 9.7.2 |
NOVEL JET ENGINE ACOUSTIC LINER WITH IMPROVED BROADBAND NOISE ABSORPTION K. Hoeschler, Brandenburg Technische Universität Cottbus-Senftenberg, Germany; E. Sarradj, Technische Universität Berlin, Germany; N. Modler, Technische Universität Dresden, Germany; L. Enghardt, German Aerospace Center, Germany | ||||
10:30 | 11:00 | 9.7.3 |
CERTAIN ASPECTS OF FAN MODEL STAGE DESIGNING FOR ADVANCED TURBOFANS S.V. Pankov¹, V.I. Mileshin¹, I.K. Orekhov¹, V.A. Fateev¹; ¹Central Institute of Aviation Motors, Russia | ||||
11:00 | 11:30 | 9.7.4 |
BIMODAL UNMANNED VEHICLE: PROPULSION SYSTEM INTEGRATION AND WATER/AIR INTERFACE TESTING A. Bacciaglia¹, D. Guo², P. Marzocca², C. Bil², A. Ceruti¹; ¹University of Bologna, Italy ;²RMIT University, Australia | ||||
11:30 | 12:00 | 9.7.5 |
PARAMETRIC INVESTIGATION OF EESC-USP AEROACOUSTIC FAN RIG R.G. Cuenca, UFSC, Brazil; P. Celso Jr.¹, B.M. Rocamora¹; ¹EESC-USP, Brazil |
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09:30 | 10:00 | 10.7.1 |
QUASI-LPV MODELING AND PARAMETER-DEPENDENT OPTIMAL CONTROL OF MORPHING WING AIRCRAFT J. Lee¹, Y. Kim¹; ¹Seoul National University, South Korea | ||||
10:00 | 10:30 | 10.7.2 |
A LOW COST MODEL AIRCRAFT FLIGHT RESEARCH FACILITY IN WIND TUNNEL B.W. Nie, National University of Defense Technology, China; L.L. Guo¹, F. Cen¹, O. Sename², L. Dugard²; ¹China Aerodynamics Research and Development Center, China ;²Univ. Grenoble Alpes, CNRS, Grenoble INP, GIPSA-lab, France | ||||
10:30 | 11:00 | 10.7.3 |
EFFECTS OF TAILORED CONTROL SURFACE COMPLIANCE ON AIRCRAFT STABILITY AND CONTROL P. Krus, Linköping university, Sweden; B. Lantto, Saab AB, Sweden; M.A. Rodriguez¹, E. Villani¹; ¹Instituto Technologico Aeronautica, Italy | ||||
11:00 | 11:30 | 10.7.4 |
DIGITAL HYDRAULICS IN AEROSPACE APPLICATIONS: SLIDING MODE OF QUANTIZED CONTROL AND LMI APPROACH L.P.G. Pinto¹, P. Krus¹, V.J. De Negri, Universidade Federal de Santa Catarina, Brazil; ¹Linköping University, Sweden | ||||
11:30 | 12:00 | 10.7.5 |
AERODYNAMIC ANALYSIS AND CONTROL ALLOCATION FOR ASYMMETRIC VARIABLE SWEEP AIRCRAFT WITH FLEXIBLE TRAILING EDGE H. Ma¹, B.F. Song¹, Y. Pei¹, Z.W. Chen¹; ¹School of Aeronautics, Northwestern Polytechnical University, China |
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09:30 | 10:00 | 11.7.1 |
MULTI-CHANNEL HUMAN-MACHINE INTERACTIVE SYSTEM FOR MULTIPLE UAVS' CONTROL P.-C. Wen¹, Y.-D. Zhang¹, Y.-H. Li¹; ¹AVIC Xi'an Aeronautics Computing Technique Research Institute, China | ||||
10:00 | 10:30 | 11.7.2 |
FLIGHT PERFORMANCE OF STEERABLE CRUCIFORM PARACHUTE SYSTEMS S.M. Herrington¹, T.D. Fields¹, O.A. Yakimenko, Naval Postgraduate School, United States; ¹University of Missouri-Kansas City, United States | ||||
10:30 | 11:00 | 11.7.3 |
A STRATEGY FOR UAV PERFORMANCE ENHANCEMENT THROUGH ATMOSPHERIC ENERGY EXTRACTION USING MPC TECHNIQUES G. Pogorzelski, CENIC Engenharia, Brazil; F.J. Silvestre, ITA - Instituto Tecnológico de Aeronáutica, Brazil | ||||
11:00 | 11:30 | 11.7.4 |
ON WAKE VORTEX SAFETY ANALYSIS AND CONTROL FOR UAV V. Golubev¹, P. Kazarin¹, C. Moreno¹, W. MacKunis¹; ¹ERAU, United States | ||||
11:30 | 12:00 | 11.7.5 |
MODELING, CONTROL AND HARDWARE-IN-THE-LOOP SIMULATION OF A GENERIC TILTING MULTI-ROTOR F. Machini¹, I.O. Tarifa¹, R.M.F. Neto¹, L. Sanches¹; ¹Universidade Federal de Uberlândia, Brazil |
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09:30 | 10:00 | 12.7.1 |
THE USE OF SYNTHETIC VISION TOOLS IN THE CONTROL TOWER ENVIRONMENT: THE RETINA CONCEPT S. Bagassi¹, F. De Crescenzio ¹, S. Piastra¹; ¹University of Bologna, Italy | ||||
10:00 | 10:30 | 12.7.2 |
A NOVEL CONTROL APPROACH TO IMPROVE SPEED COMMANDS AND PILOT WORKLOAD FOR FLIGHT-DECK BASED INTERVAL MANAGEMENT T. Riedel, Keio University / Electronic Navigation Research Institute, Japan | ||||
10:30 | 11:00 | 12.7.3 |
STUDY ON THE ARRIVAL MANAGER MAXIMIZING THE BENEFIT OF FOUR-DIMENSIONAL TRAJECTORY BASED OPERATIONS D. Toratani¹, N.K. Wickramasinghe¹, E. Itoh¹; ¹Electronic Navigation Research Institute, Japan | ||||
11:00 | 11:30 | 12.7.4 |
NONLINEAR MODEL PREDICTIVE CONTROL FOR OPTIMAL AIRCRAFT SEQUENCING B. Grüter¹, J. Diepolder¹, P. Piprek¹, T. Akman¹, F. Holzapfel¹; ¹Technical University of Munich, Germany | ||||
11:30 | 12:00 | 12.7.5 |
A FRAMEWORK TO ASSESS FUTURE AIRPORT NOISE APPLIED TO A TWO-RUNWAY AIRPORT F. Will¹, M. Hornung¹; ¹Technical University of Munich, Germany |
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14:00 | 14:30 | 1.8.1 |
STUDY ON EVALUATION METHODS OF UNDERGRADUATE AIRCRAFT OVERALL DESIGN COURSE BASED ON TEAM DESIGN COMPETITION Z.-K. Chen¹, H. Liu¹, C.-G. Yang¹; ¹School of Aeronautic Science and Engineering, Beihang University, China | ||||
14:30 | 15:00 | 1.8.2 |
ELECTRIC VTOL UAV CONFIGURATION STUDIES AND OPTIMIZATION WITHIN AIRCRAFT DESIGN PRACTICAL COURSE AT TECHNICAL UNIVERSITY OF MUNICH C. Rößler¹, M. Hornung¹; ¹Technical University of Munich, Institute of Aircraft Design, Germany |
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14:00 | 14:30 | 2.8.1 |
Lecture canceled | ||||
14:30 | 15:00 | 2.8.2 |
AIRLINE MAINTENANCE: A PROPOSAL ENVISIONING DIGITAL TRANSFORMATION L.B. Koslosky¹, N. Fisk, Boeing, United States; P. Krus, Linköping University, Sweden; L. Pereira¹; ¹Universidade Federal do ABC, Brazil | ||||
15:00 | 15:30 | 2.8.3 |
OPTIMAL SHAPE OF REPAIR PATCHES IN COMPOSITES L. Echer¹, C.E. de Souza, Federal University of Santa Maria, Brazil; R.J. Marczak¹; ¹Federal University of Rio Grande do Sul, Brazil |
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14:00 | 14:30 | 3.8.1 |
Lecture canceled | ||||
14:30 | 15:00 | 3.8.2 |
DEVELOPMENT OF STRUCTURAL HEALTH MONITORING METHODS THROUGH THE ANALYSIS OF KINETICS OF LOCAL STRESS-STRAIN STATE A.A. Bautin¹, Y.A. Svirskiy¹; ¹TsAGI, Russia | ||||
15:00 | 15:30 | 3.8.3 |
Lecture canceled |
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14:00 | 14:30 | 4.8.1 |
VALIDATION OF INTERMITTENCY MODEL FOR TRANSITION PREDICTION IN A RANS FLOW SOLVER D. de Rosa¹, P. Catalano¹; ¹CIRA - Italian Aerospace Research Centre, Italy | ||||
14:30 | 15:00 | 4.8.2 |
ON THE CALIBRATION OF THE INTERMITTENCY TRANSITION TURBULENCE MODEL FOR WIND TURBINE AIRFOIL BY MACHINE LEARNING ALGORITHM M.A. Abd Bari¹, A. Da Ronch¹, M. Panzeri, Noesis Solutions, Belgium; J. Drofelnik¹; ¹University of Southampton, United Kingdom | ||||
15:00 | 15:30 | 4.8.3 |
EFFECT OF CONTROLLED PERIODIC ROUGHNESS ON GOERTLER VORTICES IN HYPERSONIC COMPRESSION RAMP FLOW P.V. Chuvakhov¹, V.N. Radchenko¹, E.A. Alexandrova¹, V.Y. Borovoy¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia |
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14:00 | 14:30 | 5.8.1 |
INFLUENCE OF AIRFRAME STIFFNESS ON THE AERODYNAMIC COEFFICIENTS OF A HIGH ASPECT RATIO WING L.A.V. Pelegrineli¹, F.F. Liorbano¹, H.O.H. Natori¹, R.A. Angélico¹; ¹ University of São Paulo, São Carlos School of Engineering, Brazil | ||||
14:30 | 15:00 | 5.8.2 |
HORIZONTAL TAIL LOCAL ANGLE-OF-ATTACK AND TOTAL PRESSURE MEASUREMENTS THROUGH STATIC PRESSURE PORTS AND KIEL PITOT R.M. Granzoto¹, L.A. Algodoal¹, G.J. Zambrano¹, G.G. Becker¹; ¹Embraer, Brazil | ||||
15:00 | 15:30 | 5.8.3 |
EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF A UAV FOR SUPERFICIAL VOLCANO SURVEILLANCE P.D. Bravo-Mosquera¹, L. Botero-Bolivar¹, D. Acevedo-Giraldo¹, H.D. Cerón-Muñoz¹, F.M. Catalano¹; ¹EESC-USP, Brazil |
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14:00 | 14:30 | 6.8.1 |
ON THE WAVE-CANCELLING NATURE OF BOUNDARY LAYER TRANSITION CONTROL K. Sasaki¹, P. Morra², A.V.G. Cavalieri¹, A. Hanifi², D.S. Henningson²; ¹ITA, Brazil ;²KTH, Sweden | ||||
14:30 | 15:00 | 6.8.2 |
ACTUATOR AND SENSOR PLACEMENT FOR CLOSED-LOOP CONTROL OF CONVECTIVE INSTABILITIES G.A. Freire¹, A.V.G. Cavalieri¹, F.J. Silvestre¹; ¹ITA, Brazil | ||||
15:00 | 15:30 | 6.8.3 |
RESOLVENT-BASED CONTROL OF STREAKS IN BOUNDARY LAYERS P.A.S. Nogueira¹, A.V.G. Cavalieri¹, A. Hanifi², D.S. Henningson²; ¹Instituto Tecnológico de Aeronáutica, Brazil ;²KTH Royal Institute of Technology, Sweden |
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14:00 | 14:30 | 7.8.1 |
VERIFIED FUSELAGE SECTION WATER IMPACT MODELING Y. Song¹, B. Harton¹, J. Bayandor¹; ¹CRashworthiness for Aerospace Structures and Hybrids (CRASH Lab), United States | ||||
14:30 | 15:00 | 7.8.2 |
PREDICTING LOW-VELOCITY IMPACT DAMAGE IN COMPOSITE USING COHESIVE ELEMENT H. Liu¹, S. Tan¹; ¹fai, China | ||||
15:00 | 15:30 | 7.8.3 |
ENERGY-ABSORBING CHARACTERISTICS ANALYSIS OF COMPOSITE THIN-WALLED C-CHANNELS UNDER LOW SPEED AXIAL COMPRESSION J. Xie¹, Z. Feng¹, S. Song¹, D. Song¹, X. Zhang¹; ¹Civil Aviation University of China, China |
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14:00 | 14:30 | 8.8.1 |
EXPERIMENTAL AND NUMERICAL STUDIES OF FLUTTER CHARACTERISTICS OF AN ALL-MOVING CONTROL SURFACE AGAINST GAP EFFECTS Y. Bai¹, W. Qian¹, X. Chen¹; ¹Dalian University of Technology, China | ||||
14:30 | 15:00 | 8.8.2 |
MULTIDISCIPLINARY METHODS FOR WING FLIGHT SHAPE ANALYSIS - EFFECT OF THE GEOMETRIC NONLINEAR STRUCTURE FOR STATIC PULL-UP A.A. Verri¹, C.T. Jorge¹, A.F. Bizarro¹, F.L.S. Bussamra, ITA, Brazil; H.N.S. Júnior¹, C.E.S. Cesnik, UniMich, United States; ¹Embraer S/A, Brazil | ||||
15:00 | 15:30 | 8.8.3 |
RESULTS AND COMPARISON OF NUMERICAL SIMULATION AND THE TESTING OF LUG MANUFACTURED BY COMPOSITE MATERIAL BY RTM PROCESS G.C. Fonseca, Embraer - Centro de Engenharia e Tecnologia - Minas Gerais, Brazil; S.F.M. Almeida, ITA - Instituto Tecnológico de Aeronáutica, Brazil |
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14:00 | 14:30 | 9.8.1 |
INVESTIGATION ON AERO-PROPULSIVE BALANCE FOR HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECT A.A. Gubanov¹, D.S. Ivanyushkin¹, N.V. Kukshinov², A.N. Prokhorov², V.A. Talyzin¹, N.V. Voevodenko¹; ¹Central Aerohydrodynamic Institute named after Professor N.E. Zh, Russia ;²Central Institute of Aviation Motors named after P.I. Baranov, Russia | ||||
14:30 | 15:00 | 9.8.2 |
COMPLEX NUMERICAL AND EXPERIMENTAL RESEARCH OF HEXAFLY-INT HIGH-SPEED CIVIL AICRAFT MODEL V.Y. Aleksandrov¹, S.N. Batura¹, O.V. Gouskov¹, N.V. Kukshinov¹, A.N. Prokhorov¹, A.V. Rudinsky¹; ¹Central Institute of Aviation Motors named after P.I. Baranov , Russia | ||||
15:00 | 15:30 | 9.8.3 |
Lecture canceled |
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14:00 | 14:30 | 10.8.1 |
CLOSED-LOOP SYSTEM IDENTIFICATION OF A LARGE FLEXIBLE AIRCRAFT USING SUBSPACE METHODS R.C.M.G. Barbosa¹, L.C.S. Góes¹; ¹ITA, Brazil | ||||
14:30 | 15:00 | 10.8.2 |
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 |
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14:00 | 14:30 | 11.8.1 |
SMART FAULT-TOLERANT AIR-DATA SENSOR FOR AIRCRAFT FLOW ANGLES MEASUREMENT G. Di Rito¹, F. Schettini¹; ¹Università di Pisa - Dip. di Ing. Civile ed Industriale, Italy | ||||
14:30 | 15:00 | 11.8.2 |
DESIGN CRITERIA OF A THERMAL MASS FLOW SENSOR FOR AIRCRAFT AIR DATA APPLICATIONS L.C. Ribeiro¹, R.A. Souza¹, M.L. Oliveira¹, S.P.L. Vieira¹, W.O. Avelino, Labinfo Lab UFMG, Brazil; C.F.R. Oliveira¹, D.W. de Lima Monteiro¹, F.S. Torres¹, R.M.O. Hansen, University of Southern Denmark, Denmark; ¹UFMG, Brazil | ||||
15:00 | 15:30 | 11.8.3 |
AN AIRBORNE DATA BUS NETWORK SYSTEM OF INTERFACE ADAPTIVE AND FLEXIBLE CONTROL Z. Dai¹, Z. Qiu, Xi'an Aeronautics Computing Technique Research Institute, China; L. Shi¹; ¹ChengDu Aircraft Design & Research Institute, China |
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14:00 | 14:30 | 12.8.1 |
A SIMULATION MODELING STUDY FOR FREE ROUTING AIRSPACE IN JAPAN K. Kageyama¹, Y. Nakamura¹; ¹ENRI, Japan | ||||
14:30 | 15:00 | 12.8.2 |
EVALUATION OF THE POTENTIAL IMPACTS OF HYBRID-ELECTRIC AIRCRAFT ON THE GLOBAL AIR TRANSPORTATION NETWORK G. Tay¹, S. Gillen¹, R. Rothfeld, Bauhaus Luftfahrt e.V., Germany; M. Hornung¹; ¹Technical University of Munich, Germany | ||||
15:00 | 15:30 | 12.8.3 |
EULERIAN OPTIMAL CONTROL FORMULATION FOR DYNAMIC MORPHING OF AIRSPACE SECTORS Y. Lim¹, N. Premlal¹, A. Gardi¹, R. Sabatini¹; ¹RMIT University, Australia |
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16:00 | 16:30 | 1.9.1 |
FEASIBILITY STUDY OF MODIFYING A BASELINE KEROSENE AIRCRAFT TO A LH2 POWERED VERSION W. Xie¹, Z. Duan¹, H. Smith, Cranfield University, United Kingdom; ¹AVIC The First Aircraft Institute, China | ||||
16:30 | 17:00 | 1.9.2 |
DEVELOPMENT OF THE REGENERATIVE SOARER: THEORETICAL AND PRACTICAL ASPECTS R.C. Carvalho, EMBRAER S.A., Brazil | ||||
17:00 | 17:30 | 1.9.3 |
DEVELOPMENT OF A NOVEL AERIAL PLATFORM WHICH MERGES THE CONCEPT OF AIRSHIPS AND TETHERED AEROSTATS J.S. Santos¹, B.A. de Azevedo¹, L.C.S. Góes¹, R.S. Pant, Indian Institute of Technology Bombay, India; ¹Instituto Tecnológico de Aeronáutica, Brazil | ||||
17:30 | 18:00 | 1.9.4 |
Lecture canceled |
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16:00 | 16:30 | 2.9.1 |
STRUCTURAL DESIGN AND TESTING OF A TAILORED SKIN SINGLE DUCT (TSSD) FIN APPLICATION M. Schneider¹, M. Horn¹, S. Ritt¹, A. Seitz¹; ¹DLR, Germany | ||||
16:30 | 17:00 | 2.9.2 |
STUDIES ON THE APPLICATION OF MOEA/D TO AERODYNAMIC OPTIMIZATION DESIGN X.Q. Zhu¹, Z.H Gao¹, Z.W. Chen¹; ¹Northwestern Polytechnical University, China | ||||
17:00 | 17:30 | 2.9.3 |
COMPARISON AND APPLICATION OF DIFFERENTS TECHNIQUES OF MULTI-OBJECTIVE OPTIMIZATION FOR AERODYNAMIC WING DESIGN N. Gautier¹, N. Manzanares-Filho¹, E.R. Da Silva¹; ¹UNIFEI, Brazil | ||||
17:30 | 18:00 | 2.9.4 |
INTEGRATED SYSTEM FOR UNIFICATION OF AIRCRAFT CONCEPTUAL DESIGN APPLICATIONS E. Vogiatzis¹, R. Chaitanya Munjulury¹, P. Krus¹; ¹Linköping University, Sweden |
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16:00 | 16:30 | 3.9.1 |
ARAMID-FIBER REINFORCED ELASTOMERS AS FUTURE AIRCRAFT ACTUATORS - A PROOF-OF-CONCEPT INVESTIGATION M. Kanerva¹, M. Poikelispää¹, P. Antunes, Aveiro University, Portugal; ¹Tampere University of Technology, Finland | ||||
16:30 | 17:00 | 3.9.2 |
ON EQUIVALENCE OF POLYMER COMPOSITE MATERIALS STRUCTURES LOADING PROGRAMS UNDER FULL-SCALED SERVICE CYCLE TESTING A.V. Pankov¹, V.V. Konovalov¹; ¹TsAGI, Russia | ||||
17:00 | 17:30 | 3.9.3 |
STUDY OF EXTERNAL FACTOR COMBINATIONS EFFECT ON CFRP STRUCTURE UTILYZING ULTRASONIC MICROSCOPY T. Ryzhova¹, A. Shanygin¹, V. Scherbakov¹, Y. Petronyuk², V. Levin², E. Morokov²; ¹Central Aerohydrodynamic Institute, Russia ;²Institute of Biochemical Physics of RAS, Russia | ||||
17:30 | 18:00 | 3.9.4 |
Lecture canceled |
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16:00 | 16:30 | 4.9.1 |
NUMERICAL INVESTIGATION OF FLOW STRUCTURE OF DIFFERENTIAL EJECTOR H.Y. Zhang¹, Y.S. Yu¹, Q. Chen¹; ¹China Aerodynamics Research and Development Centre, China | ||||
16:30 | 17:00 | 4.9.2 |
MULTIPHASE TURBULENCE MODELS FOR SCRAMJETS AND ABLATING WALLS K.E. Son, Russia | ||||
17:00 | 17:30 | 4.9.3 |
Lecture canceled | ||||
17:30 | 18:00 | 4.9.4 |
NUMERICAL COMPARISON OF STEADY DISTURBANCES IN THE WAKE OF PERIODIC BLOW-SUCTION AND ROUGHNESS ELEMENTS P.V. Chuvakhov¹, S.V. Alexandrov¹, E.A. Alexandrova, Central Aerohydrodynamic Institute (TsAGI), Russia; ¹Moscow Institute of Physics and Technology (MIPT), Russia |
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16:00 | 16:30 | 5.9.1 |
Lecture canceled | ||||
16:30 | 17:00 | 5.9.2 |
PARTICLE IMAGE SURFACE FLOW VISUALIZATION AND SKIN-FRICTION MEASUREMENT V.E. Mosharov¹, V.N. Radchenko¹, N.S. Tsipilev¹; ¹TsAGI, Russia | ||||
17:00 | 17:30 | 5.9.3 |
RELEASE OF DYNAMICALLY SCALED OBJECTS FROM A HELICOPTER WIND TUNNEL MODEL K.H. Lammers, NLR, Netherlands; I. Philipsen, DNW, Netherlands; M.H. Ryu, KAI, South Korea | ||||
17:30 | 18:00 | 5.9.4 |
Lecture canceled |
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16:00 | 16:30 | 6.9.1 |
EFFECTIVE PLASMA BUFFET AND DRAG CONTROL FOR LAMINAR TRANSONIC AIROFOIL P.A. Polivanov¹, A.A. Sidorenko¹; ¹ITAM SB RAS, Russia | ||||
16:30 | 17:00 | 6.9.2 |
CONTROL OF STRONG SEPARATION OF FLOW VIA SIMULTANEOUS-BLOWING-SUCTION TECHNIQUE W. Stalewski, INSTITUTE of AVIATION, Poland | ||||
17:00 | 17:30 | 6.9.3 |
NUMERICAL OPTIMIZATION OF FLOW CONTROL BY TANGENTIAL JET BLOWING ON TRANSONIC AIRFOIL K.A. Abramova¹, V.G. Soudakov¹; ¹TsAGI, Russia | ||||
17:30 | 18:00 | 6.9.4 |
OVERVIEW ON THE INFLUENCE OF COANDA BLANKET CURVATURE ON COANDA DEVICE PERFORMANCE H. Djojodihardjo, Insitute for the Advancement of Aerospace Science and Technology, Indonesia |
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16:00 | 16:30 | 7.9.1 |
ENGINE EXHAUST NOZZLE PLUME EFFECTS ON THE SONIC BOOM FOR A TYPE OF HYPERSONIC LONG-RANGE CIVIL VEHICLE Z. Qian¹, Y. Leng¹, Z. Liu¹; ¹AVIC Aerodynamics Research Institute, China | ||||
16:30 | 17:00 | 7.9.2 |
PRELIMINARY STUDY OF THE AERODYNAMIC CHARACTERISTICS OF KRUEGER FLAP ON THE SST CONFIGURATION D. Kwak, JAXA, Japan; K. Ohira, Ryoyu Systems, Japan | ||||
17:00 | 17:30 | 7.9.3 |
HIGH SPEED DRAG REDUCTION OPTIMIZATION FOR PROJECTILES T. Wan¹, H.-C. Chang¹, C.-M. Liu¹; ¹Tamkang University, China | ||||
17:30 | 18:00 | 7.9.4 |
ADVANCED SONIC BOOM ANALYSIS USING FULL-FIELD SIMULATION R. Yamashita, The University of Cambridge, United Kingdom |
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16:00 | 16:30 | 8.9.1 |
GLOBAL SENSITIVITY ANALYSIS OF TRANSONIC FLUTTER USING A COUPLED CFD-CSD SOLVER R. Sandhu, Carleton University, Canada; W.X. Yuan, National Research Council (NRC) Canada, Canada; D. Poirel, Royal Military College (RMC) of Canada, Canada | ||||
16:30 | 17:00 | 8.9.2 |
NUMERICAL AND EXPERIMENTAL VALIDATION OF UNITIZED BEAM MODEL F. Danzi¹, E. Cestino¹, G. Frulla¹, J.-M. Gibert, Purdue University, United States; ¹Politecnico di Torino, Italy | ||||
17:00 | 17:30 | 8.9.3 |
ASSESSMENT OF THE AERODYNAMICS AND AEROELASTICITY OF FLAPPING WING USING LINEARIZED COMPUTATIONAL METHOD H. Djojodihardjo, Insitute for the Advancement of Aerospace Science and Technology, Indonesia; A.K. Joyodiharjo, The Institute for the Advancement of Aerospace Science and Techn, Indonesia | ||||
17:30 | 18:00 | 8.9.4 |
STRAIN GAGES FULL BRIDGE INSIDE COMPOSITE LAYERS TARGETING WING SHAPE FEEDBACK FOR FLIGHT CONTROL LAWS A.A. Verri¹, J. Barros¹, F.L.S. Bussamra², F.J. Silvestre², F.J.O. Moreira¹, A.B. Guimarães Neto², C.E.S. Cesnik, UniMich, United States; J.S. Martins²; ¹Embraer S/A, Brazil ;²ITA, Brazil |
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16:00 | 16:30 | 9.9.1 |
RESEARCH OF PROPULSION ENGINES FOR ADVANCE REUSABLE TSTO AEROSPACE SYSTEM A.I. Lanshin¹, O.V. Sokolova¹, Y.M. Shikhman¹, V.E. Shlyakotin¹; ¹CIAM, Russia | ||||
16:30 | 17:00 | 9.9.2 |
Lecture canceled | ||||
17:00 | 17:30 | 9.9.3 |
SIMULTANEOUS MEASUREMENTS OF TEMPERATURE AND HEAT FLUX IN SUPERSONIC COMBUSTOR BY ITO THIN FILM THERMOCOUPLE X.H. Jin¹, B.H. Ma¹, T. Qiu¹; ¹Northwestern Polytechnical University, China | ||||
17:30 | 18:00 | 9.9.4 |
GROUND FACILITY TESTS OF HIGH SPEED RAMJET DEMONSTRATORS V.Y. Aleksandrov¹, A.N. Prokhorov¹, V.L. Semenov¹; ¹Central Institute of Aviation Motors , Russia |
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16:00 | 16:30 | 10.9.1 |
BIO-DYNAMIC STABILITY ANALYSIS OF A GREBE DURING MIGRATION J. Feaster¹, B. Gater, Virginia Tech, United States; L. Straker², L. Jehl², J. Bayandor¹; ¹CRashworthiness for Aerospace Structures and Hybrids (CRASH Lab), United States ;²U.S. National Museum of Natural Sciences, United States | ||||
16:30 | 17:00 | 10.9.2 |
Lecture canceled | ||||
17:00 | 17:30 | 10.9.3 |
MATHEMATICAL MODEL OF COMMERCIAL AIRPLANE DYNAMICS AT STALL P.V. Kuzmin¹, N.A. Surkov¹, Y.F. Shelyukhin¹; ¹TsAGI, Russia | ||||
17:30 | 18:00 | 10.9.4 |
IDENTIFICATION OF THE LATERAL-DIRECTIONAL MODEL OF THE VECTOR-P, UNMANNED AERIAL VEHICLE C. Fischer, Instituto Tecnológico de Aeronáutica and IFSP, Brazil; L.M. Nepomuceno¹, R.G.A. Silva¹, L.C.S. Góes¹; ¹Instituto Tecnológico de Aeronáutica, Brazil |
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16:00 | 16:30 | 11.9.1 |
WIND SHEAR PARAMETER ESTIMATION FOR DYNAMIC SOARING WITH UNMANNED AERIAL VEHICLES D. Liu, China Aerodynamics Research and Development Center, China; X. Gao, National University of Defense Technology, China | ||||
16:30 | 17:00 | 11.9.2 |
A METHODOLOGY FOR PRELIMINARY SIZING OF A THERMAL AND ENERGY MANAGEMENT SYSTEM FOR A HYPERSONIC VEHICLE R. Fusaro¹, D. Ferretto¹, V. Vercella¹, N. Viola¹, V. Fernandez Villace², J. Steelant ²; ¹Politecnico di Torino, Italy ;²ESA-ESTEC, Netherlands | ||||
17:00 | 17:30 | 11.9.3 |
INTEGRATION OF ON-BOARD SYSTEMS PRELIMINARY DESIGN DISCIPLINE WITHIN A COLLABORATIVE 3RD GENERATION MDO FRAMEWORK L. Boggero¹, M. Fioriti², F. Tomasella², P.D. Ciampa¹; ¹German Aerospace Center, Germany ;²Politecnico di Torino, Italy | ||||
17:30 | 18:00 | 11.9.4 |
FAULT DIAGNOSIS METHOD STUDY FOR COMPLEX SYSTEM BASED ON KALMAN FILTERS W. Niu¹, J. Cheng, Xi’an Institute of Applied Optics, China; W. Niu¹; ¹AVIC Computing Technique Research Institute, China |
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16:00 | 16:30 | 12.9.1 |
3D AUDIO SUPPORT FOR HELICOPTER PILOTS DURING CONFINED AREA LANDINGS C.A. Niermann, German Aerospace Center (DLR), Germany | ||||
16:30 | 17:00 | 12.9.2 |
INDIVIDUALIZING FLIGHT SKILL TRAINING USING SIMULATOR DATA ANALYSIS AND BIOFEEDBACK J.O. Entzinger¹, T. Uemura¹, S. Suzuki¹; ¹The University of Tokyo, Japan | ||||
17:00 | 17:30 | 12.9.3 |
DESIGN OF A DISTRIBUTED HUMAN FACTORS LABORATORY FOR FUTURE AIR SYSTEMS J. Alfredson, Saab, Sweden; B.J.E. Johansson¹, L.G. Trabasso, ITA, Brazil; J. Schminder¹, R. Granlund, RISE, Sweden; R. Gårdhagen¹; ¹Linköping University, Sweden | ||||
17:30 | 18:00 | 12.9.4 |
CREW TRAINING USING ANIMATION P.M. Razaboni, Embraer SA, Brazil |
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10:00 | 10:30 | 1.10.1 |
PRELIMINARY DESIGN OF A LONG RANGE WINDOWLESS AIRCRAFT CONCEPT S. Bagassi¹, F. Lucchi¹, M.C. Moruzzi¹; ¹University of Bologna, Italy | ||||
10:30 | 11:00 | 1.10.2 |
COLLABORATIVE CONCEPTUAL DESIGN OF A MID-RANGE AIRCRAFT UNDER CONSIDERATION OF ADVANCED METHODS FOR TECHNOLOGY ASSESSMEN J. Hartmann¹, T. Pfeiffer¹, B. Breymann¹, D. Silberhorn¹, E. Moerland¹, M. Weiss¹, B. Nagel¹; ¹DLR, Germany | ||||
11:00 | 11:30 | 1.10.3 |
STRATEGY AND IMPLEMENTATION OF A PARAMETRIC CAD MODEL FOR R2035 AIRCRAFT STRUCTURE AND EXTERNAL CONFIGURATION Z.-J. Goraj¹, B. Goliszek¹, M. Kowalski¹, A. Seitz², F. Peter², F. Meller, Airbus Defence and Space GmbH, Germany; ¹Warsaw University of Technology, Poland ;²Bauhaus Luftfahrt e.V., Germany | ||||
11:30 | 12:00 | 1.10.4 |
AN APPROACH TO ASSESS AIRFRAME WEIGHT REDUCTION PERFORMANCE OF STITCHED COMPOSITE TECHNOLOGIES J.A. Corman¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States | ||||
12:00 | 12:30 | 1.10.5 |
NARROW-BODY B737NG PASSENGER CONVERSION TO FREIGHTER I. Berlowitz, Israel Aerospace Industries, Israel |
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10:00 | 10:30 | 2.10.1 |
FUEL-BURN PENALTIES CAUSED BY IRREGULARITIES IN AIRCRAFT SURFACES (ASTEROID PROJECT) D. Philpott¹, K. Hackett¹, A. Shires², B. Hinchliffe²; ¹IHS Markit (ESDU), United Kingdom ;²University of Leeds, United Kingdom | ||||
10:30 | 11:00 | 2.10.2 |
PARAMETRIC APPROACH TO OPERATING COSTS ESTIMATION FOR AN INNOVATIVE REGIONAL AIRCRAFT M. Fioriti¹, N. Viola¹, D. Ferretto¹, V. Vercella¹, S. Cresto Aleina¹, F. Nicolosi², V. Cusati²; ¹Politecnico di Torino, Italy ;²Università di Napoli Federico II, Italy | ||||
11:00 | 11:30 | 2.10.3 |
COST-BENEFIT ASSESSMENT OF CLIMATE AND WEATHER OPTIMIZED TRAJECTORIES FOR DIFFERENT NORTH ATLANTIC WEATHER PATTERNS B. Lührs, TUHH, Germany; M. Niklaß¹, C. Frömming¹, V. Grewe¹, V. Gollnick¹; ¹DLR, Germany | ||||
11:30 | 12:00 | 2.10.4 |
IDENTIFICATION OF OPTIMAL RENDEZVOUS AND SEPARATION AREAS FOR FORMATION FLIGHT UNDER CONSIDERATION OF WIND T. Marks¹, M. Swaid², B. Lührs², V. Gollnick¹; ¹German Aerospace Center, Germany ;²Technical University Hamburg, Germany | ||||
12:00 | 12:30 | 2.10.5 |
AIRCRAFT BOARDING AS PART OF AN EFFICIENT 4D TRAJECTORY M. Schultz, DLR, Germany |
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10:00 | 10:30 | 3.10.1 |
STUDY OF ACCIDENTAL IMPACT SCENARIOS FOR COMPOSITE WING DAMAGE TOLERANCE EVALUATION S. Dubinskii¹, Y. Feygenbaum², V. Senik¹, E. Metelkin²; ¹TsAGI, Russia ;²GosNII GA, Russia | ||||
10:30 | 11:00 | 3.10.2 |
MULTI-SITE DELAMINATION ANALYSIS USING VIRTUAL CRACK CLOSURE TECHNIQUE FOR A COMPOSITE AIRCRAFT WING FLAP J. Jokinen¹, M. Kanerva¹, O. Saarela, Aalto University, Finland; ¹Tampere University of Technology, Finland | ||||
11:00 | 11:30 | 3.10.3 |
INVESTIGATION OF BULGING EFFECTS ON PROPAGATION OF 1-BAY AND 2-BAY LONGITUDINAL CRACKS WITH BROKEN/INTACT STIFFENER A.S. Kim, TsAGI, Russia | ||||
11:30 | 12:00 | 3.10.4 |
BALLISTIC RESISTANT ANALYSIS FOR AIRCRAFT WING STRUCTURE G.R. Zu¹, Y. Pei¹, X.W. Yang¹; ¹Northwestern Polytechnical University, China | ||||
12:00 | 12:30 | 3.10.5 |
PLY THICKNESS INFLUENCE IN COMPRESSION AFTER IMPACT DAMAGE ON CARBON/EPOXY TEST SPECIMENS T.H.L. Pinto, UFVJM, Brazil; C.A. Cimini Jr., UFMG, Brazil; S.K. Ha, Hanyang University, South Korea |
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10:00 | 10:30 | 4.10.1 |
AERODYNAMIC DESIGN AND ANALYSIS OF AN INNOVATIVE REGIONAL TURBOPROP CONFIGURATION F. Nicolosi¹, S. Corcione¹, P. Della Vecchia¹, V. Trifari¹, M. Ruocco¹; ¹University of Study of Naples Federico II, Italy | ||||
10:30 | 11:00 | 4.10.2 |
PERFORMANCE IMPROVEMENT OF A COMPOUND HELICOPTER ROTOR HEAD BY AERODYNAMIC SHAPE OPTIMIZATION P. Pölzlbauer¹, D. Desvigne, Airbus Helicopters, France; C. Breitsamter¹; ¹Technical University of Munich, Germany | ||||
11:00 | 11:30 | 4.10.3 |
A RAPID AERODYNAMIC PREDICTION METHOD FOR UNCONVENTIONAL TRANSONIC AIRCRAFT CONFIGURATIONS S.A. Prince¹, D. Di Pasquale¹, K.P. Garry¹, C. Nuzzo, Politecnico di Torino, Italy; ¹Cranfield University, United Kingdom | ||||
11:30 | 12:00 | 4.10.4 |
EVALUATION OF DELTA WING EFFECTS ON THE STEALTH-AERODYNAMIC FEATURES FOR NON-CONVENTIONAL FIGHTER AIRCRAFT P.D. Bravo-Mosquera¹, A.M. Abdalla¹, F.M. Catalano¹; ¹EESC-USP, Brazil | ||||
12:00 | 12:30 | 4.10.5 |
Lecture canceled |
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10:00 | 10:30 | 5.10.1 |
THE SANTOS-DUMONT LEGACY TO AERONAUTICS M. Pazini Brandão, Technological Institute of Aeronautics, Brazil | ||||
10:30 | 11:00 | 5.10.2 |
BRAZILIAN AVIATION HISTORY: THE UNIVERSITY OF SÃO PAULO CASE F.M. Catalano, University of São Paulo -EESC-USP, Brazil | ||||
11:00 | 11:30 | 5.10.3 |
HISTORY OF AVIATION IN MINAS GERAIS E. Bauzer Medeiros, Brazil | ||||
11:30 | 12:00 | 5.10.4 |
THE STUDY OF TURBORAMJETS IN CIAM M. Tskhovrebov¹, V. Solonin¹, V. Palkin¹, P. Kadjardouzov¹; ¹CIAM, Russia | ||||
12:00 | 12:30 | 5.10.5 |
AN OVERVIEW OF THE FIRST PARAGUAYAN NEAR-SPACE EXPLORATION USING A HIGH ALTITUDE BALLOON A. Jara¹, F. Kanazawa¹, L. Vielman, AEP, Paraguay; J. Kurita¹; ¹FPUNA, Paraguay |
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10:00 | 10:30 | 7.10.1 |
CONCEPT OF MEDIUM TWIN-ENGINE STOL TRANSPORT AIRPLANE O. Pavlenko¹, A. Petrov¹, E. Pigusov¹; ¹TsAGI, Russia | ||||
10:30 | 11:00 | 7.10.2 |
Lecture canceled | ||||
11:00 | 11:30 | 7.10.3 |
A COMPARISON STUDY ON TRANSITION CHARACTERISTICS OF NLF FORWARD-SWEPT-WING AND AFT-SWEPT-WING Z. Zhu¹, W.-P. Song¹, Z.-H. Han¹, J.-H. Xu¹; ¹Northwestern Polytechnical University, China | ||||
11:30 | 12:00 | 7.10.4 |
OUTBOARD SPLIT FLAP AERODYNAMICS OF A FLYING WING CONFIGURATION S. Pfnür¹, C. Breitsamter¹; ¹Technical University of Munich, Germany | ||||
12:00 | 12:30 | 7.10.5 |
PRACTICAL APPLICATIONS OF VISCOUS FULL-POTENTIAL CFD CODES D. Philpott¹, K. Hackett¹; ¹IHS Markit (ESDU), United Kingdom |
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10:00 | 10:30 | 8.10.1 |
DESIGN OF A RECEPTANCE-BASED ACTIVE AEROELASTIC CONTROLLER IN THE PRESENCE OF PARAMETRIC UNCERTAINTIES S. Fichera¹, T.A.M. Guimaraes, Federal University of Uberlandia, Brazil; S. Jiffri, Swansea University, United Kingdom; D.A. Rade, Technological Institute of Aeronautics, Brazil; J.E. Mottershead¹; ¹University of Liverpool, United Kingdom | ||||
10:30 | 11:00 | 8.10.2 |
INCREASED FLUTTER VELOCITY WITH USE OF A PASSIVE CONTROL SYSTEM F.I. Carvalho¹, R.G. Silva¹; ¹ITA, Brazil | ||||
11:00 | 11:30 | 8.10.3 |
EXPERIMENTAL STUDY OF AEROELASTIC RESPONSE OF A FLEXIBLE HIGH ASPECT RATIO WING WITH PASSIVE SMA ACTUATORS O.T. Silva Neto, Federal University of Uberlândia, Brazil; R.N.C. Duarte, Universidade Federal de Campina Grande, Brazil; R.G.A. Silva, Instituto Tecnológico de Aeronáutica, Brazil | ||||
11:30 | 12:00 | 8.10.4 |
EFFECTS OF NONLINEAR ENERGY SINK ON THE AEROELASTIC BEHAVIOR OF AN ELECTROMECHANICALLY COUPLED TYPICAL SECTION G.M. Otsubo¹, T.M.P. Silva¹, D. D'Assunção¹, C. De Marqui Jr.¹; ¹EESC-USP, Brazil | ||||
12:00 | 12:30 | 8.10.5 |
REPLICA 55 PROJECT: AERODYNAMIC AND FEM ANALYSIS OF A WOODEN SEAPLANE F. Favalli¹, M. Ferrara¹, C. Patuelli¹, A. Polla¹, S. Scarso¹, D. Tomasello¹; ¹Polytechnic of Turin, Italy |
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10:00 | 10:30 | 9.10.1 |
DEVELOPMENT OF HYBRID GASOLINE-BATTERY PROPULSION SYSTEM FOR MULTI-COPTER PLATFORM H.R. Gwon¹, W.B. Kim¹, K.W. Lee¹, D.W. Kim¹, H.S. Lee¹; ¹Korean Air, South Korea | ||||
10:30 | 11:00 | 9.10.2 |
PROPELLER OPTIMISATION FOR AN ELECTRICAL-POWERED TACTICAL UAS R. MacNeill, The University of Sydney, Australia | ||||
11:00 | 11:30 | 9.10.3 |
DESIGN AND OFF-DESIGN PERFORMANCE OF ELECTRIC SYSTEM ARCHITECTURES FOR ELECTRIC POWERED AIRCRAFT P.C. Vratny¹, F. Troeltsch¹, J. Bijewitz¹, J. Kaiser¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany | ||||
11:30 | 12:00 | 9.10.4 |
SYSTEM ANALYSIS OF TURBO ELECTRIC AND HYBRID ELECTRIC PROPULSION SYSTEMS ON A REGIONAL AIRCRAFT H. Gesell¹, F. Wolters¹, M. Plohr¹; ¹DLR, Germany | ||||
12:00 | 12:30 | 9.10.5 |
CHARACTERISTICS OF SYSTEMS WITH ELECTRICALLY DRIVEN UNITS - EXPERIMENTAL STUDIES IN A GAS TURBINE ENGINE DEMONSTRATOR O.S. Gurevich¹, A.I. Gulienko¹, M.V. Gordin¹; ¹CIAM, Russia |
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10:00 | 10:30 | 10.10.1 |
EVALUATION OF ALTITUDE CONTROL FOR AN AIRBREATHING HYPERSONIC AIRCRAFT MODEL M. Hiruma, The University of Tokyo, Japan | ||||
10:30 | 11:00 | 10.10.2 |
A COMPARISON BETWEEN UNIVERSAL INTEGRAL REGULATOR AND LINEAR QUADRATIC TECHNIQUE FOR AN AIRCRAFT AUTOPILOT Y.A. Díaz-Méndez¹, M.S. Sousa¹, S.S. Cunha Jr.¹, G.F. Gomes¹; ¹Federal University of Itajubá, Brazil | ||||
11:00 | 11:30 | 10.10.3 |
MULTI-VARIABLE AIRCRAFT DIRECTIONAL CONTROL WITH ANTI-SKID DIFFERENTIAL BRAKES G. Di Rito¹, R. Galatolo¹, F. Schettini¹; ¹Università di Pisa - Dip. Ing. Civile ed Industriale, Italy | ||||
11:30 | 12:00 | 10.10.4 |
PASSIVE CONTROL METHOD IN ATTENUATING SELF-INDUCED ROLL OSCILLATIONS OF LOW-ASPECT-RATIO WINGS USING OBLIQUE SLOT BLEED T. Hou¹, C. Chen¹, T. Hu¹; ¹Lu Shijia Labortory, Beihang University, China | ||||
12:00 | 12:30 | 10.10.5 |
MONTE-CARLO EVALUATION OF CONTROL LAW FOR HIGH ALTITUDE FLIGHT TEST OF MARS AIRPLANE K. Fujita¹, H. Nagai¹, H. Tokutake, Kanazawa University, Japan; A. Oyama, Institute of Space and Astronautical Science, JAXA, Japan; ¹Institute of Fluid Science, Tohoku University, Japan |
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10:00 | 10:30 | 11.10.1 |
METHODS FOR EFFICIENT FLIGHT TESTING AND MODELLING OF REMOTELY PILOTED AIRCRAFT WITHIN VISUAL LINE-OF-SIGHT A. Sobron¹, D. Lundström¹, R. Larsson², P. Krus¹, C. Jouannet²; ¹Linköping University, Sweden ;²Saab Aeronautics, Sweden | ||||
10:30 | 11:00 | 11.10.2 |
VERTICAL LANDING OF A FIXED-WING UAV USING THE FLAT SPIN S. Higashino, Kyushu University, Japan; K. Nakama, Kyushu University, Graduate Student, Japan | ||||
11:00 | 11:30 | 11.10.3 |
PLANNING, IMPLEMENTATION, AND EXECUTION OF AN AUTOMATIC FIRST FLIGHT OF A UAV M.E. Kügler¹, F. Holzapfel¹; ¹Technical University of Munich, Inst. of Flight System Dynamics, Germany | ||||
11:30 | 12:00 | 11.10.4 |
SAFETY FLIGHT TESTING FOR CARGO UAV DEVELOPMENT K. Iwata¹, K. Yamada¹, R. Horiuchi¹, A. Kamimura¹; ¹National Institute of Advanced Industrial Science and Technology, Japan | ||||
12:00 | 12:30 | 11.10.5 |
Lecture canceled |
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10:00 | 10:30 | 12.10.1 |
FLIGHT TECHNICAL ERROR EVALUATIONS FOR GBAS NAVIGATION REQUIREMENT DEFINITION M. Felux, DLR, Germany; J. Lee, KAIST, South Korea; F. Holzapfel, TUM, Germany | ||||
10:30 | 11:00 | 12.10.2 |
LOAD MONITORING FOR OPERATORS’ LOAD MANAGEMENT U. Kale¹, I. Jankovics¹, J. Rohacs¹, D. Rohacs, Budapest University of Technology and Economics, Hungarian Air N, Hungary; ¹Budapest University of Technology and Economics, Hungary | ||||
11:00 | 11:30 | 12.10.3 |
THRUST MODELS BASED ON OPERATIONAL FLIGHT DATA USED IN PARAMETER ESTIMATION FOR SAFETY ANALYSES P. Koppitz¹, J. Kuerten¹, F. Holzapfel¹; ¹Technical University of Munich - Flight System Dynamics, Germany | ||||
11:30 | 12:00 | 12.10.4 |
Lecture canceled | ||||
12:00 | 12:30 | 12.10.5 |
ADAPTING CAPACITY OF AIR NAVIGATION SERVICE PROVISION IN EUROPE - BETWEEN SCYLLA AND CHARYBDIS T. Standfuss, DLR German Aerospace Center, Germany; F. Fichert, University of Applied Sciences, Germany; M. Whittome, DFS, Germany |
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14:00 | 14:30 | 1.11.1 |
REPLICA 55 PROJECT: A WOOD SEAPLANE IN THE ERA OF COMPOSITE MATERIALS E. Cestino¹, G. Frulla¹, V. Sapienza, Aeronautical Consultant, Italy; P. Pinto, 3Data analysis consultant, Italy; F. Rizzi, Replica 55 Project coordinator, Italy; F. Zaramella , BETA CAE Italy, Italy; D. Banfi , CAD Consultant, Italy; ¹Politecnico di Torino, Italy | ||||
14:30 | 15:00 | 1.11.2 |
THE NUMERICAL HISTORY OF AIRPLANE MANUFACTURING IN XX CENTURY Y.V. Kuzmin, TsAGI, Russia | ||||
15:00 | 15:30 | 1.11.3 |
Lecture canceled |
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14:00 | 14:30 | 2.11.1 |
ADDRESSING TECHNICAL AND REGULATORY REQUIREMENTS TO DEPLOY STRUCTURAL HEALTH MONITORING SYSTEMS ON COMMERCIAL AIRCRAFT D. Roach¹, T. Rice¹; ¹Sandia National Laboratories, United States | ||||
14:30 | 15:00 | 2.11.2 |
SHM QUALIFICATION PROCESS AND THE FUTURE OF AIRCRAFT MAINTENANCE F. Dotta¹, R.P. Rulli¹, P.A. da Silva¹, L.C. Vieira¹, A.K.F. Tamba¹, G.O.C. Prado¹, D. Roach², T. Rice²; ¹Embraer S.A., Brazil ;²Sandia National Labs, United States | ||||
15:00 | 15:30 | 2.11.3 |
SHM WITH AUGMENTED REALITY FOR AIRCRAFT MAINTENANCE G.O.C. Prado¹, P.A. Silva¹, F.M. Simomura¹, K.L.O. Pereira¹; ¹Embraer S.A., Brazil |
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14:00 | 14:30 | 3.11.1 |
MODELLING OF MIXED MODE FATIGUE-INDUCED DELAMINATION IN COMPOSITES: A COMPARATIVE STUDY L.A. de Oliveira¹, D.S. Alves¹, M.V. Donadon¹; ¹Instituto Tecnológico de Aeronáutica, Brazil | ||||
14:30 | 15:00 | 3.11.2 |
COMPARISON OF TWO DIFFERENT INDICATORS FOR HOT CRACKING IN WELDED STRUCTURES J. Edberg¹, J. Draxler¹, J. Andersson, University West, Sweden; ¹Luleå University of Technology, Sweden | ||||
15:00 | 15:30 | 3.11.3 |
IMPORTANCE OF SECONDARY BENDING EVALUATION IN STRUCTURAL JOINT W.R.P. Mendonça, EMBRAER S.A., Brazil |
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14:00 | 14:30 | 4.11.1 |
RESEARCH ON EXTERNAL AERODYNAMICS OF THE HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECT A.A. Gubanov¹, N.V. Voevodenko¹, V.A. Talyzin¹, D.S. Ivanyushkin¹, A.O. Podosinnikov¹, V.A. Yakovleva¹; ¹TsAGI, Russia | ||||
14:30 | 15:00 | 4.11.2 |
LONGITUDINAL STABILITY DESIGN CRITERIA FOR HYPERSONIC GLIDERS B.Y. Chen, China Academy of Aerospace Aerodynamics, China | ||||
15:00 | 15:30 | 4.11.3 |
CFD PACKAGE "FLOW VISION" FOR SIMULATIONS AND IMITATION MODELING OF HYPERSONIC VEHICLES E.E. Son¹, V.G. Degtyar², A.A. Aksenov¹, S.V. Zhluktov¹, V.I. Hlybov², S.T. Kalashnikov, Federal State Budgetary Scientific Institute, Russia; K.E. Son¹; ¹Moscow Institute of Physics and Technology, Russia ;²Academician V.P. Makeyev Space Rocket Centre, Russia |
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14:00 | 14:30 | 6.11.1 |
ENTROPY LAYER EFFECT ON ROUGHNESS-INDUCED LAMINAR-TURBULENT TRANSITION IN SUPERSONIC FLAT PLATE FLOW P.V. Chuvakhov, Central Aerohydrodynamic Institute (TsAGI), Russia | ||||
14:30 | 15:00 | 6.11.2 |
THEORETICAL STUDY OF RECEPTIVITY OF HIGH-SPEED BOUNDARY LAYER TO SURFACE PERTURBATIONS Y. Xi¹, S. Fu¹; ¹Tsinghua University, China | ||||
15:00 | 15:30 | 6.11.3 |
DIRECT NUMERICAL SIMULATION OF MACH WAVE INFLUENCE ON LAMINAR-TURBULENT TRANSITION IN SUPERSONIC FLOW OVER A FLAT PLATE I.V. Egorov¹, A.V. Fedorov¹, K.H. Ding, Central Aerohydrodynamic Institute, Russia; ¹TsAGI, Russia |
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14:00 | 14:30 | 7.11.1 |
Lecture canceled | ||||
14:30 | 15:00 | 7.11.2 |
DEVELOPMENT OF STRUCTURE ELEMENTS BASED ON ARCHITECTURED MATERIALS FOR PERSPECTIVE CIVIL AIRCRAFTS I. Kondakov¹, I. Mareskin¹, D. Vedernikov¹, Y. Mirgorodsky¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia | ||||
15:00 | 15:30 | 7.11.3 |
Lecture canceled |
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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 |
Lecture canceled |
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14:00 | 14:30 | 9.11.1 |
SMALL AIRCRAFT CONCEPT FOR REGIONAL ON-DEMAND AIR MOBILITY E. Stumpf¹, M. Kreimeier¹, P. Strathoff¹, J. Lückhof¹, K.-U. Schröder, RWTH Aachen University, Institute of Structural Mechanics and Li, Germany; F. Janser, University of Applied Sciences Aachen, Aerodynamics Group, Germany; ¹RWTH Aachen University, Institute of Aerospace Systems, Germany | ||||
14:30 | 15:00 | 9.11.2 |
INVESTIGATION OF ‘JUMP TAKEOFF’ POSSIBILITY FOR THE NEW CONCEPT OF MODERN AUTOGYRO R. Zurawski¹, D. Ulma¹; ¹Institute of Aviation, Poland | ||||
15:00 | 15:30 | 9.11.3 |
A PERFORMANCE BENCHMARK OF RECENT PERSONAL AIR VEHICLE CONCEPTS FOR URBAN AIR MOBILITY M. Shamiyeh¹, R. Rothfeld¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany |
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14:00 | 14:30 | 10.11.1 |
IMPLEMENTATION AND FLIGHT TESTING OF AN ENHANCED STABILITY SYSTEM FOR A VERY FLEXIBLE AIRCRAFT P.J. Gonzalez¹, C.E.S. Cesnik ¹, F.J. Silvestre, Instituto Tecnologico de Aeronautica, Brazil; ¹University of Michigan, United States | ||||
14:30 | 15:00 | 10.11.2 |
ADAPTIVE OUTPUT-FEEDBACK GAIN SCHEDULING APPLIED TO FLEXIBLE AIRCRAFT R.M. Bertolin¹, A.B. Guimarães Neto¹, G.C. Barbosa¹, F.J. Silvestre¹; ¹Instituto Tecnológico de Aeronáutica, Brazil | ||||
15:00 | 15:30 | 10.11.3 |
CONTROL OF A VERY FLEXIBLE WING WITH SIMULTANEOUS OPTIMIZATION OF THE GAIN MATRIX AND THE SPATIAL DISTRIBUTION OF THE SENSORS M.A.V. Morales¹, F.J. Silvestre¹, A.B. Guimarães Neto¹, G. Tissot, Université Paul Sabatier, France; ¹Instituto Tecnológico de Aeronáutica, Brazil |
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14:00 | 14:30 | 11.11.1 |
MODIFIED COMPOSITE GUIDANCE LAW AGAINST MOVING TARGET CONSIDERING NARROW FIELD-OF-VIEW LIMIT S. Lee¹, S. Ann¹, Y. Kim¹; ¹Seoul National University, South Korea | ||||
14:30 | 15:00 | 11.11.2 |
AUTONOMOUS FLIGHT OF UNMANNED MULTICOPTER USING SUPER WIDE-ANGLE STEREO VISION SYSTEM T. Yamashita¹, Y. Kajiwara¹, C.T. Raabe², T. Tsuchiya², S. Suzuki²; ¹Ricoh Co. Ltd, Japan ;²the University of Tokyo, Japan | ||||
15:00 | 15:30 | 11.11.3 |
Lecture canceled |
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14:00 | 14:30 | 12.11.1 |
DEVELOPMENT AND FLIGHT DEMONSTRATION OF A NEW LIDAR-BASED ONBOARD TURBULENCE INFORMATION SYSTEM N. Matayoshi¹, T. Iijima¹, E. Yoshikawa¹, J.O. Entzinger², T. Uemura², T. Akiyama¹, H. Inokuchi¹; ¹JAXA, Japan ;²Univ. of Tokyo, Japan | ||||
14:30 | 15:00 | 12.11.2 |
Lecture canceled | ||||
15:00 | 15:30 | 12.11.3 |
FLIGHT DEMONSTRATION OF A LONG RANGE ONBOARD DOPPLER LIDAR H. Inokuchi¹, T. Akiyama¹, K. Sasaki¹; ¹Japan Aerospace Exploration Agency, Japan |