ICAS 2018: TOPICS AND TITLES |
1 - Aircraft Design and Integrated Systems |
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ICAS2018_0003: I. Berlowitz, Israel Aerospace Industries, Israel NARROW-BODY B737NG PASSENGER CONVERSION TO FREIGHTER |
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ICAS2018_0030: 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 ANALYSIS OF THE INFLUENCE OF THE EXTERNAL CONFIGURATION ON THE WAVE DRAG OFSUPERSONIC BUSINESS JETS |
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ICAS2018_0034: J. Cavalcanti¹, P. London¹, R. Wallach¹, P. Ciloni¹; ¹Embraer, Brazil A CASE OF SUCESS: MDO APPLIED ON THE DEVELOPMENT OF EMBRAER 175 ENHANCED WINGTIP |
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ICAS2018_0041: X.Q. Zhu¹, Z.H Gao¹, Z.W. Chen¹; ¹Northwestern Polytechnical University, China STUDIES ON THE APPLICATION OF MOEA/D TO AERODYNAMIC OPTIMIZATION DESIGN |
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ICAS2018_0047: A. Papageorgiou¹, K. Amadori², C. Jouannet², J. Ölvander¹; ¹Linköping University, Sweden; ²SAAB Aeronautics, Sweden MULTIDISCIPLINARY OPTIMIZATION OF UNMANNED AIRCRAFT IN A SYSTEM OF SYSTEMS CONTEXT |
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ICAS2018_0057: 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 GENERAL PARAMETERS DESIGN METHOD OF CANARD ROTARY WING AIRPLANE UNDER THE INFLUENCE OF POWER SYSTEM |
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ICAS2018_0065: R. Vos¹, M.F.M. Hoogreef¹; ¹Delft University of Technology, Netherlands SYSTEM-LEVEL ASSESSMENT OF TAIL-MOUNTED PROPELLERS FOR REGIONAL AIRCRAFT |
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ICAS2018_0066: 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 SOLAR-POWERED UAV PLATFORM SYSTEM: A CASE STUDY FOR GROUND CHANGE DETECTION |
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ICAS2018_0086: X. He, Aviation Industry Development Research Center of China, China STUDY ON RADRA CROSS SECTION FOR FLYING-WING UNMANNED AERIAL VEHICLE WITH CLOSE FORMATION FLIGHT |
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ICAS2018_0088: 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 A VTOL SMALL UNMANNED AIRCRAFT SYSTEM TO EXPAND PAYLOAD CAPABILITIES |
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ICAS2018_0103: V.I. Chernousov¹, A.A. Krutov¹, E.A. Pigusov¹; ¹TsAGI, Russia CONTAINERIZED AIR FREIGHT SYSTEM POWERED BY CRYOGENIC FUEL |
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ICAS2018_0133: Y. Lemmens, Siemens PLM, Belgium; T. Wilson, Airbus Operations Ltd, United Kingdom; J.E. Cooper, University of Bristol, United Kingdom AIRCRAFT LOADS PREDICTION USING ENHANCED SIMULATION |
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ICAS2018_0135: L. Wiart, ONERA, France; C. Negulescu, AIRBUS, France EXPLORATION OF THE AIRBUS "NAUTILIUS" ENGINE INTEGRATION CONCEPT |
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ICAS2018_0136: Z.X. Yao, Shenyang Aircraft Design and Research Institute, China RESEARCH ON DESIGN METHOD OF PETROL-ELECTRIC HYBRID DRIVE SYSTEM BASED ON MDO FOR A NOVEL VTOVL UAV |
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ICAS2018_0167: J. Hartmann¹, T. Pfeiffer¹, B. Breymann¹, D. Silberhorn¹, E. Moerland¹, M. Weiss¹, B. Nagel¹; ¹DLR, Germany COLLABORATIVE CONCEPTUAL DESIGN OF A MID-RANGE AIRCRAFT UNDER CONSIDERATION OF ADVANCED METHODS FOR TECHNOLOGY ASSESSMEN |
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ICAS2018_0169: P. Stahl¹, T. Seren¹, C. Rößler¹, M. Hornung¹; ¹Technical University of Munich, Germany DEVELOPMENT AND PERFORMANCE COMPARISON OF OPTIMIZED ELECTRIC FIXED-WING VTOL UAV CONFIGURATIONS |
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ICAS2018_0216: Y. Hong¹, D. Han¹, K. Yee¹; ¹Seoul National University, South Korea DESIGN PARAMETER STUDY OF DRONE BLADE CONSIDERING AEROACOUSTICS |
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ICAS2018_0217: L. Smith, University of Pretoria, South Africa; J.N. Koster, University of Colorado, United States; J. Schneider, University of Stuttgart, Germany EXPERIENCE WITH INTERNATIONAL COLLABORATIVE AIRCRAFT DESIGN EDUCATION: AREND UAV |
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ICAS2018_0222: H. Zhang¹, B.F. Song¹, H. Ma¹, W. Fang¹; ¹ School of Aeronautics, Northwestern Polytechnical University, China ANALYSIS AND OPTIMIZATION OF ANTI-WIND CAPABILITY OF AN ELECTRIC HYBRID AERIAL VEHICLE |
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ICAS2018_0240: C. Rößler¹, M. Hornung¹; ¹Technical University of Munich, Institute of Aircraft Design, Germany ELECTRIC VTOL UAV CONFIGURATION STUDIES AND OPTIMIZATION WITHIN AIRCRAFT DESIGN PRACTICAL COURSE AT TECHNICAL UNIVERSITY OF MUNICH |
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ICAS2018_0250: Z.-K. Chen¹, H. Liu¹, C.-G. Yang¹; ¹School of Aeronautic Science and Engineering, Beihang University, China STUDY ON EVALUATION METHODS OF UNDERGRADUATE AIRCRAFT OVERALL DESIGN COURSE BASED ON TEAM DESIGN COMPETITION |
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ICAS2018_0272: U. Golyska¹, M. Nowowiejski¹, P. Pacuszka¹; ¹Warsaw University of Technology, Poland DESIGN AND OPTIMIZATION OF A VERSATILE UAV FOR OBSERVATION AND RESEARCH USING THERMAL COLUMNS FOR EXTENDED ENDURANCE |
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ICAS2018_0298: J.T. Bonet, Boeing Research & Technology, United States BLENDED WING BODY TRANSPORT AIRCRAFT RESEARCH & DEVELOPMENT |
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ICAS2018_0342: 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 CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATION |
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ICAS2018_0361: S. Serokhvostov, MIPT, Russia; T. Churkina, MAI, Russia OPTIMIZATION OF MOTOR FOR THE MAXIMIZATION OF SOLAR-POWERED AIRCRAFT PERFORMANCE |
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ICAS2018_0384: S. Kota, FlexSys Inc, United States; J.R.R.A. Martins, University of Michigan, United States FLEXFLOIL SHAPE ADAPTIVE CONTROL SURFACES-FLIGHT TEST AND NUMERICAL RESULTS |
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ICAS2018_0385: S.-M. Hong¹, M.-J. Tahk¹; ¹KAIST, South Korea MULTISTAGE MISSILE TRAJECTORY AND STAGE OPTIMIZATION VIA DELTA-V APPROACH |
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ICAS2018_0390: M.A. Page¹, E.J. Smetak¹, S.L. Yang¹; ¹DZYNE Technologies Incorporated, United States SINGLE-AISLE AIRLINER DISRUPTION WITH A SINGLE-DECK BLENDED-WING-BODY |
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ICAS2018_0424: P. Boonjaipetch, Tohoku University, Japan ANALYSIS OF LOW-BOOM CHARACTERISTICS OF SUPERSONIC WAVERIDER |
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ICAS2018_0425: R. Fusaro¹, D. Ferretto¹, V. Vercella¹, N. Viola¹, V. Fernandez Villace², J. Steelant²; ¹Politecnico di Torino, Italy; ²ESA-ESTEC, Netherlands LIFE CYCLE COST ESTIMATION METHODOLOGY FOR HYPERSONIC TRANSPORTATION SYSTEMS |
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ICAS2018_0426: C.M. Boozer¹, A. Elham¹; ¹Braunschweig University of Technology, Germany COUPLED ADJOINT AEROSTRUCTURAL OPTIMIZATION FRAMEWORK FOR PRELIMINARY AIRCRAFT DESIGN |
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ICAS2018_0437: 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 REPLICA 55 PROJECT: A WOOD SEAPLANE IN THE ERA OF COMPOSITE MATERIALS |
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ICAS2018_0498: O. Hektor¹, T. Melin¹; ¹Swedish Aeronautical Institute, Sweden LIFECYCLE COSTS AND FEASIBILITY ANALYSIS OF THE DESIGNS OF UAV'S FOR HUMANITARIAN RELIEF MISSIONS |
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ICAS2018_0504: V. Trifari¹, M. Ruocco¹, V. Cusati¹, F. Nicolosi¹, A. De Marco¹; ¹University of Naples Federico II, Italy MULTI-DISCIPLINARY ANALYSIS AND OPTIMIZATION JAVA TOOL FOR AIRCRAFT DESIGN |
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ICAS2018_0522: M. Gehlen¹, P. Tadeu de Mello Lourencao¹, L. Gonzaga Trabasso, ITA, Brazil; ¹EMBRAER S.A., Brazil EDUCATING ENGINEERS FOR THE DEVELOPMENT OF PRODUCT SERVICE SYSTEMS (PSS) |
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ICAS2018_0568: G.G. Silva¹, L.C. Carmona¹, E. Bauzer Medeiros¹; ¹UFMG, Brazil UAV INITIAL PARAMETER ESTIMATION |
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ICAS2018_0580: W. Xie¹, Z. Duan¹, H. Smith, Cranfield University, United Kingdom; ¹AVIC The First Aircraft Institute, China FEASIBILITY STUDY OF MODIFYING A BASELINE KEROSENE AIRCRAFT TO A LH2 POWERED VERSION |
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ICAS2018_0582: A. Jara¹, F. Kanazawa¹, L. Vielman, AEP, Paraguay; J. Kurita¹; ¹FPUNA, Paraguay AN OVERVIEW OF THE FIRST PARAGUAYAN NEAR-SPACE EXPLORATION USING A HIGH ALTITUDE BALLOON |
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ICAS2018_0594: H. Kim¹, D. Lim¹, K. Yee¹; ¹Seoul National University, South Korea DEVELOPMENT OF A COMPREHENSIVE ANALYSIS AND OPTIMIZED DESIGN FRAMEWORK FOR THE MULTIROTOR UAV |
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ICAS2018_0597: C.K. Droney¹, N.A. Harrison¹, G.M. Gatlin, NASA Langley Research Center, United States; ¹The Boeing Company, United States SUBSONIC ULTRA-GREEN AIRCRAFT RESEARCH: TRANSONIC TRUSS-BRACED WING TECHNICAL MATURATION |
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ICAS2018_0598: J.M. Souza¹, F.M. Catalano¹; ¹University of São Paulo, Brazil MULTI-DISCIPLINARY DESIGN OPTIMIZATION OF A BLENDED WINGLET |
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ICAS2018_0621: P.D. Ciampa¹, B. Nagel¹; ¹DLR, Germany STREAMLINING CROSS-ORGANIZATIONAL AIRCRAFT DEVELOPMENT PROCESSES: AN OVERVIEW OF THE AGILE PROJECT |
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ICAS2018_0623: Z. Li¹, D. Xie¹, B. Gao¹, Z. Yao¹; ¹Shanghai Aircraft Design and Research Institute, China RESERCH ON KEY TECHNOLOGY OF INTELLIGENT CIVIL AIRCRAFT |
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ICAS2018_0627: C. López Sánchez, Spain; D. Sánchez Franco, Spain; R. Chaitanya Munjulurynjulury, Sweden HURRICANE-CS: CONTROL SURFACES AND HIGH LIFT DEVICES MODELING AND SIZING PROGRAM |
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ICAS2018_0630: R. Zurawski¹, D. Ulma¹; ¹Institute of Aviation, Poland INVESTIGATION OF ‘JUMP TAKEOFF’ POSSIBILITY FOR THE NEW CONCEPT OF MODERN AUTOGYRO |
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ICAS2018_0633: M. Spieck, Thelsys GmbH, Germany; B. Aigner, RWTH Aachen, Germany; P.S. Prakasha¹, P.D. Ciampa¹; ¹German Aerospace Center, Germany MDO AS A SOCIO-TECHNICAL SYSTEM - A SMALL CONTRIBUTION TO COLLABORATIVE ENGINEERING |
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ICAS2018_0648: L. Stingo¹, P. Della Vecchia¹, G. Cerino, Leonardo Company, Italy; F. Nicolosi¹, A. De Marco¹; ¹University of Naples, Italy MDO APPLICATIONS TO CONVENTIONAL AND NOVEL TURBOPROP AIRCRAFT WITHIN AGILE EUROPEAN PROJECT |
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ICAS2018_0674: 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 DESIGN OF THE STRUT BRACED WING AIRCRAFT IN THE AGILE COLLABORATIVE MDO FRAMEWORK |
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ICAS2018_0675: 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 AERO-STRUCTURAL OPTIMIZATION OF A MALE CONFIGURATION IN THE AGILE MDO FRAMEWORK |
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ICAS2018_0697: I. Gál¹, D. Rohács¹, J. Rohács¹; ¹Budapest University of Technology and Economics, Hungary DEVELOPING THE UNMANNED UNCONVENTIONAL CARGO AIRPLANES WITH HYBRID PROPULSION SYSTEM |
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ICAS2018_0705: Y.V. Kuzmin, TsAGI, Russia THE NUMERICAL HISTORY OF AIRPLANE MANUFACTURING IN XX CENTURY |
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ICAS2018_0727: 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 SMALL AIRCRAFT CONCEPT FOR REGIONAL ON-DEMAND AIR MOBILITY |
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ICAS2018_0745: M.M. Entezari¹, M. Mohammadi-Amin¹; ¹ARI, Iran AN EFFICIENT FRAMEWORK FOR AERODYNAMIC CONFIGURATION EVOLUTION OF REENTRY VEHICELES |
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ICAS2018_0746: M. Naoto, the University of Tokyo, Japan NEURAL NETWORK DRIVEN ADJOINT SOLVER BETWEEN FLIGHT-PATH OPTIMIZATION AND PANEL METHOD FOR AIRCRAFT DESIGN |
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ICAS2018_0752: 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 STRATEGY AND IMPLEMENTATION OF A PARAMETRIC CAD MODEL FOR R2035 AIRCRAFT STRUCTURE AND EXTERNAL CONFIGURATION |
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ICAS2018_0777: S. Bagassi¹, F. Lucchi¹, M.C. Moruzzi¹; ¹University of Bologna, Italy PRELIMINARY DESIGN OF A LONG RANGE WINDOWLESS AIRCRAFT CONCEPT |
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ICAS2018_0783: 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 MULTIDISCIPLINARY DESIGN ANALYSIS OF BLENDED WING BODY THROUGH COLLABORATIVE DESIGN APPROACH: AGILE EU PROJECT |
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ICAS2018_0785: 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 COLLABORATIVE OPEN SOURCE AIRCRAFT DESIGN FRAMEWORK FOR EDUCATION - AGILE ACADEMY INITIATIVES AND RESULTS |
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ICAS2018_0786: 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 INCLUDING AEROELASTIC TAILORING IN THE CONCEPTUAL DESIGN PROCESS OF A COMPOSITE STRUT BASED WING |
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ICAS2018_0793: J.A. Corman¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States AN APPROACH TO ASSESS AIRFRAME WEIGHT REDUCTION PERFORMANCE OF STITCHED COMPOSITE TECHNOLOGIES |
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ICAS2018_0794: M. Shamiyeh¹, R. Rothfeld¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany A PERFORMANCE BENCHMARK OF RECENT PERSONAL AIR VEHICLE CONCEPTS FOR URBAN AIR MOBILITY |
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ICAS2018_0807: 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 DEVELOPMENT OF A NOVEL AERIAL PLATFORM WHICH MERGES THE CONCEPT OF AIRSHIPS AND TETHERED AEROSTATS |
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ICAS2018_0814: P.D. Bravo-Mosquera¹, A.M. Abdalla¹, H.D. Cerón-Muñoz¹, F.M. Catalano ¹; ¹EESC-USP, Brazil DESIGN AND PERFORMANCE ASSESSMENT OF AN INVERTED RECTANGULAR DORSAL INTAKE FOR MILITARY AVIATION |
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ICAS2018_0839: R.C. Carvalho, EMBRAER S.A., Brazil DEVELOPMENT OF THE REGENERATIVE SOARER: THEORETICAL AND PRACTICAL ASPECTS |
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ICAS2018_0852: M. Schneider¹, M. Horn¹, S. Ritt¹, A. Seitz¹; ¹DLR, Germany STRUCTURAL DESIGN AND TESTING OF A TAILORED SKIN SINGLE DUCT (TSSD) FIN APPLICATION |
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ICAS2018_0864: A. Gong¹, J.L. Palmer, Defence Science and Technology Group, Australia; D. Verstraete¹; ¹The University of Sydney, Australia FLIGHT TEST OF A FUEL-CELL/BATTERY/SUPERCAPACITOR TRIPLE HYBRID UAV PROPULSION SYSTEM |
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ICAS2018_0873: E. Vogiatzis¹, R. Chaitanya Munjulury¹, P. Krus¹; ¹Linköping University, Sweden INTEGRATED SYSTEM FOR UNIFICATION OF AIRCRAFT CONCEPTUAL DESIGN APPLICATIONS |
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ICAS2018_0874: L. Pan, Shanghai Aircraft Design and Research Institute, China PRELIMINARY DESIGN FOR A LOW REYNOLDS NUMBER BWB UAV DEMONSTRATOR |
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ICAS2018_0875: 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 DESIGN AND DEVELOPMENT OF THE D8 COMMERCIAL TRANSPORT CONCEPT |
2 - Systems Engineering and Integration |
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ICAS2018_0062: D.K. Howarth, MEE Inc., United States A 7D TRADE |
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ICAS2018_0085: J. Zang¹, Q. Wang¹, J.-Q Zhu¹; ¹Aviation Industry Development Research Center of China, China CONTINUOUS MODELING IN AIRCRAFT TOP-LEVEL DEMONSTRATION |
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ICAS2018_0132: M. Guenov¹, A. Molina-Cristóbal¹, A. Riaz¹, S. Sharma², A. Murton², J. Crockford²; ¹Cranfield University, United Kingdom; ²Airbus Operations Ltd, United Kingdom AIRCRAFT SYSTEMS ARCHITECTING: LOGICAL-COMPUTATIONAL DOMAIN INTERFACE |
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ICAS2018_0134: A.S.J. van Heerden¹, M.D. Guenov¹, A. Molina-Cristóbal¹, A. Riaz¹, Y. Bile¹; ¹Cranfield University, United Kingdom COMBINED AIRFRAME AND SUBSYSTEMS EVOLVABILITY EXPLORATION DURING CONCEPTUAL DESIGN |
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ICAS2018_0183: K.G. Schwartz¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States UTILIZATION OF SCALING LAWS AND UNCERTAINTY QUANTIFICATION TO INFORM TECHNOLOGY DEVELOPMENT EXPERIMENTATION |
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ICAS2018_0203: R. Hällqvist¹, J. Schminder², M. Eek¹, R. Braun², R. Gårdhagen², P. Krus²; ¹Saab Aeronautics, Sweden; ²Linköping University, Sweden A NOVEL FMI AND TLM-BASED DESKTOP SIMULATOR FOR DETAILED STUDIES OF THERMAL PILOT COMFORT |
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ICAS2018_0208: S. Sartorius, United States; M. Hornung, Technical University of Munich Institute of Aircraft Design, Germany A TECHNIQUE FOR CAPTURING STAKEHOLDER PREFERENCES AND KNOWLEDGE IN EARLY DESIGN STUDIES |
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ICAS2018_0374: 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 SERVICE-ORIENTED ARCHITECTURE TO INTEGRATE FLIGHT SAFETY AND MISSION MANAGEMENT SUBSYSTEMS INTO UAVS |
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ICAS2018_0405: B. Wu¹, X. Qiu¹, F. Fang¹, Z. Yao¹; ¹COMAC Shanghai Aircraft Design and Research Institute, China CIVIL AIRCRAFT DEVELOPMENT PROJECT IPT TEAM OBS DEVELOPMENT RESEARCH |
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ICAS2018_0479: V.L. Takase¹, H.H. Sano¹; ¹EMBRAER S.A., Brazil MODEL-BASED CONTROL LOGICS DEVELOPMENT OF AIRCRAFT SYSTEMS |
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ICAS2018_0514: F.M.S. Turetta, Embraer, Brazil A PRACTICAL ANALYSIS ON THE COMPLEXITY OF AIRCRAFT SYSTEMS ARCHITECTURE AND REQUIREMENTS DEVELOPMENT |
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ICAS2018_0551: M. Maia Neto¹, L.C.S. Goes¹; ¹ITA, Brazil A BOND GRAPH-ORIENTED METHOD FOR ASSESSMENT OF FAILURES IN AN AIRCRAFT HYDRAULIC BRAKE SYSTEM |
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ICAS2018_0553: L.J. Ribeiro¹, M.S. de Sousa¹; ¹Federal University of Itajubá, Brazil STAMP METHOD APPLICATION ON INDUSTRIAL MANAGEMENT |
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ICAS2018_0570: G.P. Krupa, Federal University of Itajubá, Brazil APPLICATION OF AGILE MODEL-BASED SYSTEMS ENGINEERING IN AIRCRAFT CONCEPTUAL DESIGN |
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ICAS2018_0610: Z. Yao¹, B. Guo, China-Russia Commercial Aircraft International Co., China; D. Xie¹, Z. Li¹; ¹Shanghai Aircraft Design and Research Institute, China RESEARCH ON DESKTOP VIRTUAL INTEGRATION AND VERIFICATION OF CIVIAL AIRCRAFT |
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ICAS2018_0724: I. Staack, Linköping University, Sweden; K. Amadori¹, C. Jouannet¹; ¹Saab Aeronautics, Sweden A HOLISTIC ENGINEERING APPROACH FOR AERONAUTICAL PRODUCT DEVELOPMENT |
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ICAS2018_0821: J. Abulawi, HAW Hamburg, Germany A SYSML-BASED APPROACH TO EXPLORING INNOVATIVE SYSTEM IDEAS FOR AERONAUTICAL APPLICATIONS |
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ICAS2018_0830: M. Vieweg¹, C. Klein¹, S. Reitenbach¹, F. Wolters¹, R.-G. Becker¹; ¹German Aerospace Center , Germany COUPLING OF PREDESIGN AND PERFORMANCE TOOLS FOR TRANSIENT AIRCRAFT ENGINE ANALYSES |
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ICAS2018_0862: D.N. Mavris¹, A. Sudol¹; ¹Georgia Institute of Technology, United States FORMULATION AND IMPLEMENTATION OF A METHOD FOR TECHNOLOGY EVALUATION OF SYSTEM OF SYSTEMS |
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ICAS2018_0867: N. Lakemond, Linköping University, Sweden; G. Holmberg, Saab AB and Linköping University, Sweden DIGITAL INNOVATION IN COMPLEX SYSTEMS-MANAGING CRITICAL APPLICATIONS AND GENERATIVITY |
3.1 - Aerodynamics - CFD Methods and Validation |
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ICAS2018_0001: G. Qian¹, J. Si¹, K. Liu¹; ¹COMAC, China NUMERICAL STUDY OF REYNOLDS NUMBER EFFECT ON SUPERCRITICAL WING AERODYNAMIC LOADS |
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ICAS2018_0025: A. Tarnowski¹, T. Goetzendorf-Grabowski¹, J. Mieloszyk¹; ¹Warsaw University of Technology, Poland MORPHING WING WITH SURFACE DISCONTINUITY - COMPARATIVE TESTS |
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ICAS2018_0045: A. Cenko, AIWS, United States; G. Akroyd, Akroyd Aeronautics, Australia RECTANGULAR CAVITY FLOWFIELD EFFECTS ON STORES IN THE SHEAR LAYER |
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ICAS2018_0070: P. Pölzlbauer¹, D. Desvigne, Airbus Helicopters, France; C. Breitsamter¹; ¹Technical University of Munich, Germany PERFORMANCE IMPROVEMENT OF A COMPOUND HELICOPTER ROTOR HEAD BY AERODYNAMIC SHAPE OPTIMIZATION |
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ICAS2018_0076: 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 CFD INVESTIGATION OF AERODYNAMIC COEFFICIENTS AND STALL CHARACTERISTICS FOR HIGH LIFT CONFIGURATIONS |
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ICAS2018_0112: C. González Biedma, Airbus D&S, Spain "FAST" CFD METHODS IN AIRCRAFT SYSTEM DESIGN. APPLICATION TO C295W MODIFICATIONS. |
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ICAS2018_0126: M. Moioli¹, C. Breitsamter¹, K.A. Sørensen, Airbus Defence and Space, Germany; ¹Technical University of Munich, Germany TURBULENCE MODEL CONDITIONING FOR VORTEX DOMINATED FLOWS BASED ON EXPERIMENTAL RESULTS |
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ICAS2018_0130: A. Viviani, University of Campania, Italy; G. Pezzella, Italian Aerospace Research Centre, Italy LAUNCHER AERODYNAMIC ANALYSIS WITH PLUME EFFECTS |
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ICAS2018_0138: S.A. Prince¹, D. Di Pasquale¹, K.P. Garry¹, C. Nuzzo, Politecnico di Torino, Italy; ¹Cranfield University, United Kingdom A RAPID AERODYNAMIC PREDICTION METHOD FOR UNCONVENTIONAL TRANSONIC AIRCRAFT CONFIGURATIONS |
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ICAS2018_0166: B.Y. Chen, China Academy of Aerospace Aerodynamics, China LONGITUDINAL STABILITY DESIGN CRITERIA FOR HYPERSONIC GLIDERS |
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ICAS2018_0191: F. Nicolosi¹, S. Corcione¹, P. Della Vecchia¹, V. Trifari¹, M. Ruocco¹; ¹University of Study of Naples Federico II, Italy AERODYNAMIC DESIGN AND ANALYSIS OF AN INNOVATIVE REGIONAL TURBOPROP CONFIGURATION |
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ICAS2018_0199: P.D. Bravo-Mosquera¹, A.M. Abdalla¹, F.M. Catalano¹; ¹EESC-USP, Brazil EVALUATION OF DELTA WING EFFECTS ON THE STEALTH-AERODYNAMIC FEATURES FOR NON-CONVENTIONAL FIGHTER AIRCRAFT |
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ICAS2018_0201: E.-K. Mascia¹, O. de Almeida¹; ¹Federal University of Uberlandia, Brazil AERODYNAMIC EVALUATION OF THE EXTERNAL FLOW OVER PICKUP TRUCKS |
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ICAS2018_0205: J.J. Broekhuijsen¹, G. Vidjaja², J.W. van der Burg², H.W.M. Hoeijmakers¹; ¹University of Twente, Netherlands; ²Airbus Operations GMBH, Germany NUMERICAL INVESTIGATION AERODYNAMICS NACELLE-STRAKE EFFECT |
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ICAS2018_0227: K.E. Son, Russia MULTIPHASE TURBULENCE MODELS FOR SCRAMJETS AND ABLATING WALLS |
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ICAS2018_0231: G. Qian¹, D. Wu¹, C. Ma¹; ¹COMAC, China NUMERICAL STUDY OF VARIABLE CAMBER WING EFFECT ON AERODYNAMIC PERFORMANCE FOR LONG RANGE CIVIL AIRCRAFT |
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ICAS2018_0242: 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 CFD PACKAGE "FLOW VISION" FOR SIMULATIONS AND IMITATION MODELING OF HYPERSONIC VEHICLES |
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ICAS2018_0256: A.A. Gubanov¹, N.V. Voevodenko¹, V.A. Talyzin¹, D.S. Ivanyushkin¹, A.O. Podosinnikov¹, V.A. Yakovleva¹; ¹TsAGI, Russia RESEARCH ON EXTERNAL AERODYNAMICS OF THE HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECT |
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ICAS2018_0264: V. Cusati¹, P. Della Vecchia¹, D. Ciliberti¹, S. Corcione¹, F. Nicolosi¹; ¹University of Naples Federico II, Italy NUMERICAL HIGH LIFT PREDICTION ON THE JAXA STANDARD MODEL |
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ICAS2018_0294: Z.W. Chen¹, Y. Pei¹, X.W. Yang¹, H. Ma¹; ¹Northwestern Polytechnical University, China CFD-BASED STUDY OF DAMAGE LOCATION INFLUENCE ON AERODYNAMICS OF WINGS WITH SINGLE AND DOUBLE THROUGH HOLES |
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ICAS2018_0318: B. Koenig¹, D. Singh¹, E. Fares¹; ¹Exa GmbH, Germany LATTICE BOLTZMANN HIGH-LIFT SIMULATIONS - A STEP BEYOND CLASSICAL CFD |
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ICAS2018_0323: W. Yue¹, L. Kang¹, S. Wenping¹, H. Zhonghua¹; ¹Northwestern Polytechnical University, China IMPROVED DELAYED DETACHED EDDY SIMULATION OF THE FLOWS AROUND S809 AIRFOIL FOR ANGLES OF ATTACK FROM 0 TO 90 DEGREES |
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ICAS2018_0326: Z. Tan, China; Y. Chen, China; J. Si, China; Y. Zhong, China NUMERICAL ANALYSIS OF BLEND-WING-BODY AIRFRAME AND ENGINE AERODYNAMIC INTERFERENCE |
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ICAS2018_0328: M.A. Abd Bari¹, A. Da Ronch¹, M. Panzeri, Noesis Solutions, Belgium; J. Drofelnik¹; ¹University of Southampton, United Kingdom ON THE CALIBRATION OF THE INTERMITTENCY TRANSITION TURBULENCE MODEL FOR WIND TURBINE AIRFOIL BY MACHINE LEARNING ALGORITHM |
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ICAS2018_0334: H.Y. Zhang¹, Y.S. Yu¹, Q. Chen¹; ¹China Aerodynamics Research and Development Centre, China NUMERICAL INVESTIGATION OF FLOW STRUCTURE OF DIFFERENTIAL EJECTOR |
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ICAS2018_0345: C.F. Rafael¹, G.A.L. da Silva¹, M.J.M. Guedes, Brazilian Navy, Brazil; ¹Aerothermal Solutions and Software Distributor, Brazil SHIP-HELICOPTER OPERATIONAL LIMITATION ENVELOPE DEFINITION WITH CFD RESULTS AND WIND TUNNEL DATA |
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ICAS2018_0369: K.C. Morais¹, D.F. Abreu¹, R. Papa¹, L. Tobaldini Neto¹, L.C.C. Santos¹; ¹EMBRAER S. A., Brazil EFFECTS OF NUMERICAL MODELING CHOICES FOR HEATED JETS IN CROSS FLOW |
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ICAS2018_0436: H. Güner¹, G. Dimitriadis¹, V.E. Terrapon¹; ¹University of Liège, Belgium INVISCID AND VISCOUS FLOW MODELING FOR FAST TRANSONIC FLUTTER CALCULATIONS |
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ICAS2018_0453: A. Crovato¹, G. Dimitriadis¹, V.E. Terrapon¹; ¹University of Liege, Belgium HIGHER FIDELITY TRANSONIC AERODYNAMIC MODELING IN PRELIMINARY AIRCRAFT DESIGN |
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ICAS2018_0484: D. de Rosa¹, P. Catalano¹; ¹CIRA - Italian Aerospace Research Centre, Italy VALIDATION OF INTERMITTENCY MODEL FOR TRANSITION PREDICTION IN A RANS FLOW SOLVER |
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ICAS2018_0503: R.V. Linn¹, A.M. Awruch¹; ¹Federal University of Rio Grande do Sul, Brazil LARGE EDDY SIMULATION OF A TRANSIENT SPOILER DEPLOYMENT IN A NACA0012 PROFILE IN SUBSONIC AND TRANSONIC SPEEDS |
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ICAS2018_0525: D. Han¹, J.Y. Huh¹, S. Noh¹, K.H. Kim¹; ¹Seoul National University, South Korea ANALYSIS OF CHEMICALLY REACTING HYPERSONIC FLOW USING A MESHLESS METHOD |
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ICAS2018_0527: N. Gautier¹, N. Manzanares-Filho¹, E.R. Da Silva¹; ¹UNIFEI, Brazil COMPARISON AND APPLICATION OF DIFFERENTS TECHNIQUES OF MULTI-OBJECTIVE OPTIMIZATION FOR AERODYNAMIC WING DESIGN |
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ICAS2018_0550: T.P. Monteiro¹, K. Ramesh, Glasgow University, United Kingdom; F. Silvestre¹; ¹Instituto Tecnologico de Aeronautica, Brazil NUMERICAL DEVELOPMENT OF UNSTEADY VORTEX-LATTICE METHOD EXPANSION FOR LEADING-EDGE SHEDDING PREDICTION WITH EXPERIMENTAL VALIDATION |
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ICAS2018_0622: P. Catalano¹, A. Mastellone¹, M. Invigorito¹, F. Capuano, Università di Napoli Federico II, Italy; ¹CIRA, Italy NUMERICAL ANALYSIS OF THE FLOW AROUND A BACKWARD-FACING RAMP |
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ICAS2018_0700: P.V. Chuvakhov¹, S.V. Alexandrov¹, E.A. Alexandrova, Central Aerohydrodynamic Institute (TsAGI), Russia; ¹Moscow Institute of Physics and Technology (MIPT), Russia NUMERICAL COMPARISON OF STEADY DISTURBANCES IN THE WAKE OF PERIODIC BLOW-SUCTION AND ROUGHNESS ELEMENTS |
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ICAS2018_0718: O.S. Kotsur¹, G.A. Shcheglov¹; ¹Bauman Moscow State Technical University, Russia VISCOUS FLUID SIMULATION WITH THE VORTEX ELEMENT METHOD |
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ICAS2018_0737: P.A. Semenev, Central Institute of Aviation Motors, Russia NUMERICAL SIMULATION OF OPERATING PROCESS ELEMENTS FOR COMBUSTION CHAMBERS OF PERSPECTIVE GTE |
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ICAS2018_0791: J. Drofelnik¹, A. Da Ronch¹, M.S. Campobasso, University of Lancaster, United Kingdom; ¹University of Southampton, United Kingdom FEASIBILITY OF THE NAVIER-STOKES HARMONIC BALANCE METHOD FOR MODELLING AIRCRAFT UNSTEADY AERODYNAMICS |
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ICAS2018_0856: Z.J. Wang, United States TOWARDS INDUSTRIAL LARGE EDDY SIMULATION AND AERO-ACOUSTIC NOISE COMPUTATION WITH THE HIGH-ORDER FR/CPR METHOD |
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ICAS2018_0857: M. Mani¹, A. Cary¹; ¹Boeing, United States CFD VERIFICATION AND VALIDATION FOR INDUSTRIAL APPLICATIONS |
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ICAS2018_0872: G. Andrews, Purdue University, United States A HYBRID LENGTH SCALE SIMILARITY SOLUTION FOR SWIRLING TURBULENT JETS |
3.2 - Experimental Aerodynamics |
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ICAS2018_0064: K.H. Lammers, NLR, Netherlands; I. Philipsen, DNW, Netherlands; M.H. Ryu, KAI, South Korea RELEASE OF DYNAMICALLY SCALED OBJECTS FROM A HELICOPTER WIND TUNNEL MODEL |
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ICAS2018_0068: V.E. Mosharov¹, V.N. Radchenko¹, N.S. Tsipilev¹; ¹TsAGI, Russia PARTICLE IMAGE SURFACE FLOW VISUALIZATION AND SKIN-FRICTION MEASUREMENT |
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ICAS2018_0095: A. Krzysiak, Institute of Aviation, Poland EXPERIMENTAL INVESTIGATION OF WING LOAD CONTROL USING FLUIDIC DEVICES |
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ICAS2018_0116: Y. Sun¹, C. Breard¹, X. Li¹, Y. Chen¹; ¹Shanghai Aircraft Design and Research Institute of COMAC, China CHALLENGES OF AERO-ACOUSTIC MEASUREMENTS IN WIND TUNNEL: IDENTIFICATION AND ELIMINATION OF "PARASITE" NOISE |
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ICAS2018_0159: U.H. Choi¹, J.H. Kim¹, Y.B. Lee, Agency for Defense Development, South Korea; J.M. Ahn¹; ¹KAIST, South Korea ADAPTIVE DESIGN OF EXPERIMENT BASED ON GAUSSIAN PROCESS MODELS WITH NONSTATIONARY KERNEL APPLIED TO WIND TUNNEL TESTING |
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ICAS2018_0253: Y.H. Sung¹, J.S. Han¹, J.H. Han¹; ¹KAIST, South Korea UNSTEADY AERODYNAMIC CHARACTERISTICS OF THE OSCILLATING AIRFOIL USING MSBS |
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ICAS2018_0297: K. Garry¹, D. Di Pasquale¹, S. Prince¹, N.J. Lawson¹; ¹Cranfield University, United Kingdom THE INFLUENCE OF HIGH-SPEED SPIV DATA PROCESSING PARAMETERS ON AIRCRAFT WING VORTEX WAKE ASSESSMENT |
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ICAS2018_0317: F. Litao¹, H. Zhiyuan¹, W. Zhigang¹; ¹CARDC, China RLG BASED REAL-TIME MODEL ATTITUDE DETERMINATION SYSTEM DEVELOPMENT FOR LARGE LOW SPEED FACILITY OF CARDC |
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ICAS2018_0321: S.L. Chernyshev¹, A.I. Ivanov¹, E.V. Streltsov¹, A.O. Volkova¹; ¹Central Aerohydrodynamic Institute n.a. prof. N.E. Zhukovsky, Russia APPLICATION OF THE COMBINED BOUNDARIES TO REDUCE WALL INTERFERENCE FOR NACA 0012 AIRFOIL TESTS |
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ICAS2018_0337: R.M. Granzoto¹, L.A. Algodoal¹, G.J. Zambrano¹, G.G. Becker¹; ¹Embraer, Brazil HORIZONTAL TAIL LOCAL ANGLE-OF-ATTACK AND TOTAL PRESSURE MEASUREMENTS THROUGH STATIC PRESSURE PORTS AND KIEL PITOT |
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ICAS2018_0364: D. Vukovic¹, V. Lapcevic¹, D. Marinkovski¹, M. Samardzic¹, L. Petrovic¹; ¹Military technical institute (VTI), Serbia DIGITALIZATION OF INTERNAL WIND TUNNEL BALANCES |
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ICAS2018_0371: A.V. Petrov¹, A.V. Potapchik¹, J.G. Stepanov¹, V.V. Gubskiy¹; ¹TsAGI, Russia ADAPTIVE WING HIGH-LIFT SYSTEM |
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ICAS2018_0382: R.S. Sousa, EMBRAER, Brazil; R.G.A. da Silva¹, R.d.M. Girardi¹; ¹ITA, Brazil EVALUATION OF TRANSONIC BUFFETING ONSET BOUNDARY ESTIMATED BY TRAILING EDGE PRESSURE DIVERGENCE AND RMS DATA OF WING VIBRATION |
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ICAS2018_0400: C.O. Oliveira, UFMG - ALFALAB, Brazil LOW-COST CERAMIC JET TURBINE |
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ICAS2018_0470: 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 THE AERODYNAMIC PERFORMANCE MEASUREMENT OF COAXIAL ROTOR IN HOVER |
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ICAS2018_0591: 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 DESIGN OF AN INSTRUMENTED STATOR VANE FOR UNSTEADY PRESSURE MEASUREMENTS USING MEMS MICROPHONES |
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ICAS2018_0599: H.F. Leite¹, R.G.A. da Silva¹, A.C. Avelar, IAE, Brazil; ¹ITA, Brazil TIME-RESOLVED PRESSURE MEASUREMENTS FOR AN AIRFOIL WITH SELF-SUSTAINED SHOCK OSCILATIONS |
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ICAS2018_0750: Z. Liu¹, H. Sun¹, B. Nie¹, L. Guo¹, F. Cen¹; ¹China Aerodynamics Research and Development Center (CARDC), China OVERVIEW OF DYNAMIC TEST TECHNIQUES AT LOW SPEED AERODYNAMICS INSTITUTE, CARDC |
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ICAS2018_0776: 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 INFLUENCE OF AIRFRAME STIFFNESS ON THE AERODYNAMIC COEFFICIENTS OF A HIGH ASPECT RATIO WING |
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ICAS2018_0780: F.M. Catalano, Aeronautical Engineering Dept. University of São Paulo , Brazil; L.T.L. Pereira, University of São Paulo , Brazil EVALUATION OF WIND TUNNEL WALL BOUNDARY-LAYER CONTROL FOR 2-D HIGH-LIFT AERODYNAMIC AND AEROACOUSTIC TESTING |
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ICAS2018_0815: P.D. Bravo-Mosquera¹, L. Botero-Bolivar¹, D. Acevedo-Giraldo¹, H.D. Cerón-Muñoz¹, F.M. Catalano¹; ¹EESC-USP, Brazil EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF A UAV FOR SUPERFICIAL VOLCANO SURVEILLANCE |
3.3 - Basic Fluid Dynamics and Flow Control |
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ICAS2018_0118: T. Atobe, JAXA, Japan DESTABILIZING EFFECT OF LONGITUDINAL WALL OSCILLATION ON OBLIQUE WAVES IN 2D CHANNEL FLOW |
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ICAS2018_0152: P.A. Polivanov¹, A.A. Sidorenko¹; ¹ITAM SB RAS, Russia EFFECTIVE PLASMA BUFFET AND DRAG CONTROL FOR LAMINAR TRANSONIC AIROFOIL |
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ICAS2018_0195: D. Rodriguez, Universidade Federal Fluminense, Brazil; E.M. Gennaro, Sao Paulo State University, Brazil EFFECTS OF THE INTRINSIC THREE-DIMENSIONALIZATION OF LAMINAR SEPARATION BUBBLES ON THE AMPLIFICATION OF EXTERNAL DISTURBANCES |
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ICAS2018_0196: W. Stalewski, INSTITUTE of AVIATION, Poland CONTROL OF STRONG SEPARATION OF FLOW VIA SIMULTANEOUS-BLOWING-SUCTION TECHNIQUE |
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ICAS2018_0349: K. Sasaki¹, P. Morra², A.V.G. Cavalieri¹, A. Hanifi², D.S. Henningson²; ¹ITA, Brazil; ²KTH, Sweden ON THE WAVE-CANCELLING NATURE OF BOUNDARY LAYER TRANSITION CONTROL |
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ICAS2018_0388: L.I. Abreu¹, A.V.G. Cavalieri¹, P. Schlatter², R. Vinuesa², D. Henningson²; ¹ITA, Brazil; ²KTH, Sweden WAVEPACKETS IN TURBULENT FLOW OVER A NACA 4412 AIRFOIL |
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ICAS2018_0438: G.A. Freire¹, A.V.G. Cavalieri¹, F.J. Silvestre¹; ¹ITA, Brazil ACTUATOR AND SENSOR PLACEMENT FOR CLOSED-LOOP CONTROL OF CONVECTIVE INSTABILITIES |
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ICAS2018_0450: E. Martini, ITA, Brazil; A. Cavalieri, ITA, Brazil; P. Jordan, Universite de Poitiers, France ACOUSTIC MODES AND GLOBAL INSTABILITIES IN WAKES AND JETS |
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ICAS2018_0473: P. Morra¹, K. Sasaki², A. Cavalieri², A. Hanifi¹, D. Henningson¹; ¹KTH Royal Institute of Technology, Sweden; ²Instituto Tecnológico de Aeronáutica, Brazil CONTROL OF STREAKY DISTURBANCES IN THE BOUNDARY LAYER OVER A FLAT PLATE |
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ICAS2018_0477: P.A.S. Nogueira¹, A.V.G. Cavalieri¹, A. Hanifi², D.S. Henningson²; ¹Instituto Tecnológico de Aeronáutica, Brazil; ²KTH Royal Institute of Technology, Sweden RESOLVENT-BASED CONTROL OF STREAKS IN BOUNDARY LAYERS |
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ICAS2018_0524: Y. Xi¹, S. Fu¹; ¹Tsinghua University, China THEORETICAL STUDY OF RECEPTIVITY OF HIGH-SPEED BOUNDARY LAYER TO SURFACE PERTURBATIONS |
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ICAS2018_0690: P.V. Chuvakhov¹, V.N. Radchenko¹, E.A. Alexandrova¹, V.Y. Borovoy¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia EFFECT OF CONTROLLED PERIODIC ROUGHNESS ON GOERTLER VORTICES IN HYPERSONIC COMPRESSION RAMP FLOW |
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ICAS2018_0691: I.V. Egorov¹, A.V. Fedorov¹, K.H. Ding, Central Aerohydrodynamic Institute, Russia; ¹TsAGI, Russia DIRECT NUMERICAL SIMULATION OF MACH WAVE INFLUENCE ON LAMINAR-TURBULENT TRANSITION IN SUPERSONIC FLOW OVER A FLAT PLATE |
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ICAS2018_0701: P.V. Chuvakhov, Central Aerohydrodynamic Institute (TsAGI), Russia ENTROPY LAYER EFFECT ON ROUGHNESS-INDUCED LAMINAR-TURBULENT TRANSITION IN SUPERSONIC FLAT PLATE FLOW |
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ICAS2018_0704: K.A. Abramova¹, V.G. Soudakov¹; ¹TsAGI, Russia NUMERICAL OPTIMIZATION OF FLOW CONTROL BY TANGENTIAL JET BLOWING ON TRANSONIC AIRFOIL |
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ICAS2018_0735: E. van Bokhorst¹, C. Atkin¹; ¹University of London, United Kingdom DEVELOPMENT OF SECONDARY CROSSFLOW INSTABILITY NEAR BREAKDOWN INTO TURBULENCE |
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ICAS2018_0738: H. Djojodihardjo, Insitute for the Advancement of Aerospace Science and Technology, Indonesia OVERVIEW ON THE INFLUENCE OF COANDA BLANKET CURVATURE ON COANDA DEVICE PERFORMANCE |
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ICAS2018_0739: B. Crowley¹, C. Atkin¹; ¹City University of London, United Kingdom LAMINAR-TURBULENT TRANSITION MECHANISMS OVER WIDELY-SPACED SUCTION HOLES |
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ICAS2018_0741: I.A. Amelyushkin, Russia; A.L. Stasenko, Russia; V.A. Zhbanov, Russia EXPERIMENTAL INVESTIGATION, MATHEMATICAL AND NUMERICAL SIMULATION OF AIRCRAFT ICING PHENOMENA |
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ICAS2018_0837: 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 IONIZATION AND DISSOCIATION EFFECTS ON HYPERSONIC BOUNDARY-LAYER STABILITY |
3.4 - Applied Aerodynamics |
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ICAS2018_0038: W.X. Yuan¹, A. Wall¹, R. Lee¹; ¹National Research Council Canada, Canada SIMULATIONS OF UNSTEADY AIRWAKES BEHIND SHIPS IN MOTION |
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ICAS2018_0039: Z. Qian¹, Y. Leng¹, Z. Liu¹; ¹AVIC Aerodynamics Research Institute, China ENGINE EXHAUST NOZZLE PLUME EFFECTS ON THE SONIC BOOM FOR A TYPE OF HYPERSONIC LONG-RANGE CIVIL VEHICLE |
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ICAS2018_0069: S. Pfnür¹, C. Breitsamter¹; ¹Technical University of Munich, Germany OUTBOARD SPLIT FLAP AERODYNAMICS OF A FLYING WING CONFIGURATION |
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ICAS2018_0098: D. Kwak, JAXA, Japan; K. Ohira, Ryoyu Systems, Japan PRELIMINARY STUDY OF THE AERODYNAMIC CHARACTERISTICS OF KRUEGER FLAP ON THE SST CONFIGURATION |
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ICAS2018_0104: O. Pavlenko¹, A. Petrov¹, E. Pigusov¹; ¹TsAGI, Russia CONCEPT OF MEDIUM TWIN-ENGINE STOL TRANSPORT AIRPLANE |
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ICAS2018_0131: Z. Fan¹, Z. Zhou¹, X. Zhu, Science and Technology on UAV Laboratory, NPU, China; ¹School of Aeronautics,Northwestern Polytechnical University, China APPLICATION OF HIGH-ROBUSTNESS BEMT FOR SIMULATION OF UAV-VTOL PROPELLER AT LOW/HIGH ADVANCE RATIO |
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ICAS2018_0151: Y.L. Zheng¹, Q.L. Qu¹, P.Q. Liu¹; ¹Beihang University, China HIGH LIFT MECHANISM OF A 2D FLAPPING WING IN HOVERING FLIGHT |
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ICAS2018_0154: R.Z. Li¹, M. Zhang², M.H. Zhang², Y.F. Zhang¹, H.X. Chen¹; ¹Tsinghua University, China; ²Shanghai Aircraft Design and Research Institute, China MULTI-POINT AERODYNAMIC OPTIMIZATION DESIGN OF A DUAL-AISLE AIRPLANE WING |
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ICAS2018_0172: X.-D. Yang¹, M. Huang¹; ¹School of Aeronautics Northwestern Polytechnical University, China AERODYNAMIC DESIGN OF A RIGID COAXIAL ROTOR AIRFOIL IN UNSTEADY FLOW |
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ICAS2018_0187: Z. Huan¹, G. Zhenghong¹; ¹Northwestern Polytechnical University , China ROBUST DESIGN OPTIMIZATION OF BENCHMARK AERODYNAMIC CASE BASED ON POLYNOMIAL CHAOS EXPANSION |
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ICAS2018_0189: C. Xue¹, Z. Zhou¹, H.-B. Wang¹; ¹Northwestern Polytechnical University, China INVESTIGATION ON APPROACH TO CONTROL LIFT DISTRIBUTION OF WING BY DISTRIBUTED PROPELLERS |
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ICAS2018_0226: C. Wang¹, Z. Gao¹, P. Liu¹, Y. Na¹, X. Zhu¹; ¹Northwestern Polytechnical University, China MULTILEVEL COLLABORATIVE AERODYNAMIC DESIGN OPTIMIZATION BASED ON SOBOL’ GLOBAL SENSITIVITY ANALYSIS |
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ICAS2018_0258: R. Kulhánek¹, Z. Pátek¹, P. Vrchota¹, N. Žižkovský¹, J. Cecrdle¹; ¹VZLÚ, a.s., Czech Republic EXPERIMENTAL AND CFD STUDY OF KRUEGER FLAPS |
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ICAS2018_0270: T. Wan¹, H.-C. Chang¹, C.-M. Liu¹; ¹Tamkang University, China HIGH SPEED DRAG REDUCTION OPTIMIZATION FOR PROJECTILES |
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ICAS2018_0311: Y. Lee, Agency for Defense Development, South Korea INVESTIGATION ON THE POSSIBILITY OF FLOW CONTROL AROUND CAVITY USING TANGENTIAL JET |
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ICAS2018_0338: D. Philpott¹, K. Hackett¹; ¹IHS Markit (ESDU), United Kingdom PRACTICAL APPLICATIONS OF VISCOUS FULL-POTENTIAL CFD CODES |
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ICAS2018_0367: A. Cenko, AIWS, United States; N. Stathopoulos, L3-MAS, Canada; R. Hobbins, Bombardier, Canada; G. Akroyd, Akroyd Aeronautics, Australia STORE SEPARATION TRAJECTORY PREDICTIONS AT LOW SPEEDS |
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ICAS2018_0440: G. Yang¹, A. Da Ronch¹, D. Kharlamov¹, J. Drofelnik¹; ¹University of Southampton, United Kingdom WING TWIST OPTIMISATION USING AERODYNAMIC SOLVERS OF DIFFERENT FIDELITY |
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ICAS2018_0444: H. Iwafuji, Tokyo Metropolitan University, Japan EXHAUST PLUME EFFECT OF WINGED TWO-STAGE-TO-ORBIT SEPARATION AT ASCENT USING AERODYNAMIC-FLIGHT DYNAMICS TECHNIQUE |
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ICAS2018_0469: P. Zhou¹, X. Zhao¹, L. Deng¹, Y.-F. Lin, China Helicopter Research and Development Institute, China; ¹Northwestern Polytechnical University, China ANALYSIS OF XH-59A ROTOR IN FORWARD FIGHT WITH HIGH EFFICIENCY TRIM METHOD |
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ICAS2018_0474: 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 NUMERICAL SIMULATION OF THE AERIAL DROP OF WATER FOR FIXED-WING AIRTANKERS |
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ICAS2018_0496: C.-Z. Xu¹, Z.-H. Han¹, K.-S. Zhang¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China SURROGATE-BASED OPTIMIZATION METHOD APPLIED TO MULTIDISCIPLINARY DESIGN OPTIMIZATION ARCHITECTURES |
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ICAS2018_0497: Z. Zhu¹, W.-P. Song¹, Z.-H. Han¹, J.-H. Xu¹; ¹Northwestern Polytechnical University, China A COMPARISON STUDY ON TRANSITION CHARACTERISTICS OF NLF FORWARD-SWEPT-WING AND AFT-SWEPT-WING |
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ICAS2018_0552: K.A. Jamison, Council of Scientific and Industrial Research (CSIR), South Africa GRID-MODE TRANSONIC STORE SEPARATION ANALYSES USING MODERN DESIGN OF EXPERIMENTS |
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ICAS2018_0646: 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 WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTING |
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ICAS2018_0649: G.B. Campos¹, J.T. Tomita¹, F.P. Costa¹, C. Bringhenti¹, O. Petit², T. Grönstedt², A.C. Patrao², G. Trapp³, C.R.I. Silva³, A. Lundbladh, GKN, Sweden; ¹Instituto Tecnológico de Aeronáutica, Brazil; ²Chalmers, Sweden; ³Embraer, Brazil PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERS |
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ICAS2018_0670: A.A.F. Barbosa¹, F.M. Catalano¹; ¹University of Sao Paulo (EESC-USP), Brazil INFLUENCE OF GULL WING ON LONGITUDINAL AND LATERAL-DIRECTIONAL COEFFICIENTS OF AN AIRPLANE |
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ICAS2018_0685: T. Yoon, South Korea; K. Yee, South Korea DESIGN OPTIMIZATION OF AIRFOIL FOR WIND TURBINE WITH RESPECT TO ICE ACCRETION |
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ICAS2018_0715: H. Wang¹, Z.-H. Han¹, S.-Q. Han¹, Y. Zhang¹, C.-Z. Xu¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China COMBINING ADJOINT-BASED AND SURROGATE-BASED OPTIMIZATIONS FOR BENCHMARK AERODYNAMIC DESIGN PROBLEMS |
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ICAS2018_0736: Y. Tani¹, S. Seki¹, S. Aso¹; ¹Kyushu University, Japan PASSIVE VENTILATION FLOW CONTROL FOR AIRCRAFT GUST LOAD ALLEVIATION |
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ICAS2018_0747: N.A. Pushchin, TsAGI, Russia THE STUDIES ON LOW-NOISE LAMINAR WING REGIONAL AIRCRAFT |
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ICAS2018_0846: T. Melin, Svenska Flygtekniska Institutet, Sweden; A.A. Gastaldi¹, M. Zhang¹; ¹Airinnova, Sweden IMPLEMENTATION OF A VORTEX LATTICE METHOD IN A HETEROGENEOUS PROGRAMMING LANGUAGE ENVIRONMENT |
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ICAS2018_0870: R. Yamashita, The University of Cambridge, United Kingdom ADVANCED SONIC BOOM ANALYSIS USING FULL-FIELD SIMULATION |
4.1 - Material Issues, Fatigue and Damage Tolerance |
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ICAS2018_0013: L. Molent, DST, Australia USING THE LEAD CRACK CONCEPT TO REDUCE DURABILITY TEST DURATION |
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ICAS2018_0017: R.M.V. Campos, Universidade Católica de Minas Gerais, Brazil COMPARATIVE STUDY AND VALIDATION OF MATERIAL WITH BETTER PERFORMANCE IN TERMS OF THERMAL ABSORPTION INSIDE AN AIRCRAFT |
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ICAS2018_0142: J. Edberg¹, J. Draxler¹, J. Andersson, University West, Sweden; ¹Luleå University of Technology, Sweden COMPARISON OF TWO DIFFERENT INDICATORS FOR HOT CRACKING IN WELDED STRUCTURES |
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ICAS2018_0160: A.A. Bautin¹, Y.A. Svirskiy¹; ¹TsAGI, Russia DEVELOPMENT OF STRUCTURAL HEALTH MONITORING METHODS THROUGH THE ANALYSIS OF KINETICS OF LOCAL STRESS-STRAIN STATE |
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ICAS2018_0185: A.V. Pankov¹, V.V. Konovalov¹; ¹TsAGI, Russia ON EQUIVALENCE OF POLYMER COMPOSITE MATERIALS STRUCTURES LOADING PROGRAMS UNDER FULL-SCALED SERVICE CYCLE TESTING |
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ICAS2018_0234: S. Dubinskii¹, Y. Feygenbaum², V. Senik¹, E. Metelkin²; ¹TsAGI, Russia; ²GosNII GA, Russia STUDY OF ACCIDENTAL IMPACT SCENARIOS FOR COMPOSITE WING DAMAGE TOLERANCE EVALUATION |
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ICAS2018_0281: P. Li¹, J. Ma¹; ¹Aircraft strength research institute, China THE EFFECT OF STRUCTURAL PARAMETERS OF AIRCRAFT PANEL ON VIBRATION FATIGUE LIFE |
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ICAS2018_0286: L. Zaplana ¹, I. Rivero¹, B. García-Fogeda ¹, J. Gómez-Escalonilla¹; ¹AIRBUS DS, Spain FATIGUE AND CRACK PROPAGATION LIFE IMPROVEMENT QUANTIFICATION FOR COLD-WORKED HOLES OUTSIDE NOMINAL CONDITIONS |
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ICAS2018_0293: Q. Wang, The Research Institute for Special Structures of Aeronautical Co, China; J. Tian, he Research Institute for Special Structures of Aeronautical Com, China EFFECT OF DIELECTRIC PROPERTIES DUE TO THE CHANGE OF DIELECTRIC AS A RESULT OF ELEVATORY TEMPERATURE |
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ICAS2018_0302: E. Dubovikov¹, V. Fomin¹, D. Fomin¹, V. Notkin¹, N. Perchits¹, G. Vodovozov¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia NUMERICAL INVESTIGATION OF INFLUENCE OF INITIAL DAMAGES ON STRENGTH PARAMETERS OF CFRP |
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ICAS2018_0308: T. Ryzhova¹, A. Shanygin¹, V. Scherbakov¹, Y. Petronyuk², V. Levin², E. Morokov²; ¹Central Aerohydrodynamic Institute, Russia; ²Institute of Biochemical Physics of RAS, Russia STUDY OF EXTERNAL FACTOR COMBINATIONS EFFECT ON CFRP STRUCTURE UTILYZING ULTRASONIC MICROSCOPY |
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ICAS2018_0343: J. Jokinen¹, M. Kanerva¹, O. Saarela, Aalto University, Finland; ¹Tampere University of Technology, Finland MULTI-SITE DELAMINATION ANALYSIS USING VIRTUAL CRACK CLOSURE TECHNIQUE FOR A COMPOSITE AIRCRAFT WING FLAP |
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ICAS2018_0376: A.S. Kim, TsAGI, Russia INVESTIGATION OF BULGING EFFECTS ON PROPAGATION OF 1-BAY AND 2-BAY LONGITUDINAL CRACKS WITH BROKEN/INTACT STIFFENER |
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ICAS2018_0377: M. Kanerva¹, M. Poikelispää¹, P. Antunes, Aveiro University, Portugal; ¹Tampere University of Technology, Finland ARAMID-FIBER REINFORCED ELASTOMERS AS FUTURE AIRCRAFT ACTUATORS - A PROOF-OF-CONCEPT INVESTIGATION |
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ICAS2018_0418: G.R. Zu¹, Y. Pei¹, X.W. Yang¹; ¹Northwestern Polytechnical University, China BALLISTIC RESISTANT ANALYSIS FOR AIRCRAFT WING STRUCTURE |
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ICAS2018_0512: A.T.A. Melo¹, B.L. Nolli¹, C.A. Cimini Jr.¹; ¹Universidade Federal de Minas Gerais, Brazil FINITE ELEMENT MODEL DEVELOPMENT FOR SIMULTANEOUS CRACK PROPAGATION IN TWO COOPERATIVE LUGS |
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ICAS2018_0516: B.L. Nolli¹, A.T.A. Melo¹, C.A. Cimini Jr.¹; ¹UFMG, Brazil CRACK PROPAGATION STARTING AT HOLE’S EDGE GROWING TO PLATE’S MAJOR DIMENSION USING FEM |
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ICAS2018_0519: L.A. de Oliveira¹, D.S. Alves¹, M.V. Donadon¹; ¹Instituto Tecnológico de Aeronáutica, Brazil MODELLING OF MIXED MODE FATIGUE-INDUCED DELAMINATION IN COMPOSITES: A COMPARATIVE STUDY |
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ICAS2018_0583: W.R.P. Mendonça, EMBRAER S.A., Brazil IMPORTANCE OF SECONDARY BENDING EVALUATION IN STRUCTURAL JOINT |
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ICAS2018_0707: T.H.L. Pinto, UFVJM, Brazil; C.A. Cimini Jr., UFMG, Brazil; S.K. Ha, Hanyang University, South Korea PLY THICKNESS INFLUENCE IN COMPRESSION AFTER IMPACT DAMAGE ON CARBON/EPOXY TEST SPECIMENS |
4.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity |
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ICAS2018_0004: J. Cecrdle¹, O. Vich¹; ¹Aeronautical Research and Test Institute (VZLU) , Czech Republic FLUTTER ANALYSIS OF TWIN TURBOPROP AIRCRAFT WITH TIP-TANKS |
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ICAS2018_0007: G.C. Fonseca, Embraer - Centro de Engenharia e Tecnologia - Minas Gerais, Brazil; S.F.M. Almeida, ITA - Instituto Tecnológico de Aeronáutica, Brazil RESULTS AND COMPARISON OF NUMERICAL SIMULATION AND THE TESTING OF LUG MANUFACTURED BY COMPOSITE MATERIAL BY RTM PROCESS |
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ICAS2018_0037: R. Sandhu, Carleton University, Canada; W.X. Yuan, National Research Council (NRC) Canada, Canada; D. Poirel, Royal Military College (RMC) of Canada, Canada GLOBAL SENSITIVITY ANALYSIS OF TRANSONIC FLUTTER USING A COUPLED CFD-CSD SOLVER |
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ICAS2018_0049: H. Liu¹, S. Tan¹; ¹fai, China PREDICTING LOW-VELOCITY IMPACT DAMAGE IN COMPOSITE USING COHESIVE ELEMENT |
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ICAS2018_0060: A. Velicki, The Boeing Company, United States DESIGNING PRIMARY STRUCTURES WITH STITCHED COMPOSITES |
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ICAS2018_0078: Y. FEI, Shang Hai Aircraft Design and Research Institute of COMAC, China APPLICATION RESEARCH OF ZIMMERMAN-WEISSENBURGER-YANG METHOD FOR PREDICTING FLUTTER BOUNDARY |
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ICAS2018_0082: D.B. Schwinn¹, P. Weiand¹, M. Schmid¹, M. Buchwald¹; ¹German Aerospace Center (DLR), Germany STRUCTURAL SIZING OF A ROTORCRAFT FUSELAGE USING AN INTEGRATED DESIGN APPROACH |
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ICAS2018_0108: M.M. Nilton¹, A.V.G. Cavalieri¹, M.V. Donadon¹, W.R. Wolf, Universidade Estadual de Campinas, Brazil; ¹Instituto Tecnológico de Aeronáutica, Brazil STRUCTURAL DAMPING EFFECTS ON THE ACOUSTIC SCATTERING BY ELASTIC PLATES |
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ICAS2018_0173: L.A. Magerramova¹, M.E. Volkov¹, A.I. Afonin¹, M.S. Svinareva¹, D.V. Kalinin¹; ¹CIAM, Russia APPLICATION OF LIGHT LATTICE STRUCTURES FOR GAS TURBINE ENGINE FAN BLADES |
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ICAS2018_0177: P.C. Teixeira¹, C.E.S. Cesnik¹; ¹University of Michigan, United States PROPELLER INFLUENCE ON THE STABILITY OF HALE AIRCRAFT |
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ICAS2018_0179: C.B. York, University of Glasgow, United Kingdom; Y.B. Murta, Embraer, Brazil; S.F.M. Almeida, University of Sao Paulo, Brazil A PASSIVE-ADAPTIVE WING FOR DRAG REDUCTION |
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ICAS2018_0206: L.H. Teixeira¹, J.H. Izuka, Faculty of Applied Sciences - UNICAMP, Brazil; P. Gonzalez¹, P. Kurka¹; ¹Faculty of Mechanical Engineering - UNICAMP, Brazil A NUMERICAL ANALYSIS OF THE DYNAMICS OF A TENSEGRITY-MEMBRANE STRUCTURE |
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ICAS2018_0207: R.B. Olympio¹, M.V. Donadon¹, S.G.P Castro, EMBRAER, Brazil; ¹ITA, Brazil AN ACTIVE-PASSIVE NONLINEAR FINITE ELEMENT MODEL FOR ELECTROMECHANICAL COMPOSITE MORPHING BEAMS |
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ICAS2018_0230: Q. Yu¹, S. Lee¹, M. Damodaran¹, B.C. Khoo¹; ¹National University of Singapore, Singapore MODELLING OF FLUTTER CHARACTERISTICS OF AIRCRAFT WING WITH PYLON-MOUNTED ENGINE NACELLE |
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ICAS2018_0245: E. Carrera¹, A. Pagani¹, G.H.C. Silva, Embraer S.A., Brazil; ¹Politecnico di Torino, Italy GLOBAL-LOCAL STRUCTURAL ANALYSIS OF COMPOSITE WINGS |
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ICAS2018_0248: J. Qin¹, X. Gao¹, W.C. Huang¹, G. Yao¹; ¹ASRI, China HIGH FREQUENCY MODAL TEST AND DYNAMIC PERFORMANCE EVALUATION OF TURBINE ROTOR BLADES |
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ICAS2018_0262: R.R. Medeiros¹, C.E.S. Cesnik¹, E.B. Coetzee, Airbus Operations, United Kingdom; ¹University of Michigan, United States NONLINEAR AEROELASTIC REDUCED ORDER MODELS USING MODAL COORDINATES |
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ICAS2018_0266: S. Huo¹, Q. Yan¹, W. Xie, Harbin Institute of Technology , China; ¹Aircraft Strength Research Institute, China THERMAL-MECHNICAL COUPLING ANALYSIS AND OPTIMIZATION DESIGN ON TPS WITH GAP |
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ICAS2018_0276: G.A. Amiryants¹, S.E. Paryshev¹, A.V. Grigoriev¹; ¹TsAGI, Russia AEROELASTIC PROPERTIES OF ACTIVE WINGLETS |
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ICAS2018_0278: C. Zhang¹, Z. Zhou¹, P. Meng¹; ¹Northwestern Polytechnical University, China NONLINEAR STATIC AEROELASTIC AND TRIM ANALYSIS OF HIGHLY FLEXIBLE AIRCRAFT |
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ICAS2018_0296: A. Hermanutz¹, M. Hornung¹; ¹Technical University of Munich, Germany VIRTUAL AIRCRAFT MODEL FOR AEROELASTIC SIMULATION AND LOAD PREDICTION OF A HIGH ASPECT RATIO COMPOSITE SWEPT WING |
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ICAS2018_0299: E.A. Dubovikov¹, M.C. Zichenkov¹, I.V. Mareskin¹, A.V. Chernov¹, A.N. Shanygin¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia INVESTIGATION OF SYNERGETIC EFFECT INFLUENCE ON STRENGTH CHARACTERISTICS AND WEIGHT EFFICIENCY OF LOAD-BEARING AVIATION STRUCTURES |
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ICAS2018_0304: I. Kondakov¹, I. Mareskin¹, D. Vedernikov¹, Y. Mirgorodsky¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia DEVELOPMENT OF STRUCTURE ELEMENTS BASED ON ARCHITECTURED MATERIALS FOR PERSPECTIVE CIVIL AIRCRAFTS |
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ICAS2018_0316: V.V. Chedrik¹, S.A. Tuktarov¹; ¹Central Aerohydrodynamic Institute, Russia STRESS-BASED TOPOLOGY OPTIMIZATION WITH USING GLOBAL-LOCAL APPROACH |
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ICAS2018_0329: V. Paiva¹, P. Kurka¹, J. Izuka, UNICAMP - FCA, Brazil; ¹UNICAMP - FEM, Brazil KINEMATICS AND DYNAMICS OF A TENSEGRITY STRUCTURE IN EXPANSION |
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ICAS2018_0344: R. Faraj, Institute of Fundamental Technological Research, Poland HIGH PERFORMANCE PNEUMATIC SHOCK-ABSORBERS FOR AERONAUTICAL APPLICATIONS |
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ICAS2018_0356: M. Wojtas¹, T. Szczepanik¹, L. Czajkowski¹; ¹Institute of Aviation, Poland NEW TECHNOLOGY OF LAYERED STRUCTURES IMPLEMENTED IN SELECTED GYROPLANE COMPONENTS |
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ICAS2018_0389: J. Xie¹, Z. Feng¹, S. Song¹, D. Song¹, X. Zhang¹; ¹Civil Aviation University of China, China ENERGY-ABSORBING CHARACTERISTICS ANALYSIS OF COMPOSITE THIN-WALLED C-CHANNELS UNDER LOW SPEED AXIAL COMPRESSION |
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ICAS2018_0391: G.M. Otsubo¹, T.M.P. Silva¹, D. D'Assunção¹, C. De Marqui Jr.¹; ¹EESC-USP, Brazil EFFECTS OF NONLINEAR ENERGY SINK ON THE AEROELASTIC BEHAVIOR OF AN ELECTROMECHANICALLY COUPLED TYPICAL SECTION |
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ICAS2018_0430: E. Cestino¹, G. Frulla¹, A. Lanzillotti¹; ¹Politecnico di Torino, Italy PRELIMINARY ASSESSMENT OF A WARPING WING CONFIGURATION IN ROLLING CONTROL |
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ICAS2018_0432: F. Favalli¹, M. Ferrara¹, C. Patuelli¹, A. Polla¹, S. Scarso¹, D. Tomasello¹; ¹Polytechnic of Turin, Italy REPLICA 55 PROJECT: AERODYNAMIC AND FEM ANALYSIS OF A WOODEN SEAPLANE |
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ICAS2018_0443: X. Yan¹, Z. Liu¹, Y. Yang¹; ¹CARDC, China A RESEARCH OF MULTIDISCIPLINARY DESIGN OPTIMIZATION ALGORITHM FOR FIGHT VEHICLE DESIGN |
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ICAS2018_0458: K.A. Balunov¹, V.V. Chedrik¹, F.Z. Ishmuratov¹; ¹TsAGI, Russia AEROELASTIC TAILORING OF COMPOSITE WING BY USING MULTIDISCIPLINARY DESIGN ENVIRONMENT |
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ICAS2018_0475: T. Ikeda, Chubu University, Japan; M. Ishigami¹, T. Nishihara¹; ¹Nagoya University, Japan MULTIFUNCTIONAL COMPOSITE PROCESSED USING EMBROIDERY TECHNOLOGY |
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ICAS2018_0482: 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 STRAIN GAGES FULL BRIDGE INSIDE COMPOSITE LAYERS TARGETING WING SHAPE FEEDBACK FOR FLIGHT CONTROL LAWS |
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ICAS2018_0493: 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 MULTIDISCIPLINARY METHODS FOR WING FLIGHT SHAPE ANALYSIS - EFFECT OF THE GEOMETRIC NONLINEAR STRUCTURE FOR STATIC PULL-UP |
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ICAS2018_0502: M.V. Angelo¹, M.L. Ribeiro¹, V. Tita¹; ¹University of Sao Paulo, Brazil AN XFEM FRAMEWORK FOR ONSET AND CRACK PROPAGATION FOR COMPOSITES BASED ON ACTION PLANE THEORY |
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ICAS2018_0509: 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 DESIGN OF A RECEPTANCE-BASED ACTIVE AEROELASTIC CONTROLLER IN THE PRESENCE OF PARAMETRIC UNCERTAINTIES |
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ICAS2018_0526: W. Fang, China; H. Ma, China; H. Zhang, China STRUCTURAL DESIGN AND ANALYSIS OF A QUADROTOR FIXED-WING HYBRID UAV WING |
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ICAS2018_0556: F. Danzi¹, E. Cestino¹, G. Frulla¹, J.-M. Gibert, Purdue University, United States; ¹Politecnico di Torino, Italy NUMERICAL AND EXPERIMENTAL VALIDATION OF UNITIZED BEAM MODEL |
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ICAS2018_0573: F.A. Fenelon¹, G.F.S. Neves¹, R.S. Martins¹; ¹Universidade Federal de Minas Gerais, Brazil STRUCTURAL OPTIMIZATION AND PROPOSITION OF PRE-SIZING PARAMETERS FOR UAVS WING SPARS |
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ICAS2018_0579: D. Andrade¹, W. Corbelli¹, R. Martins¹, R. Queiroz¹; ¹Universidade Federal de Minas Gerais, Brazil STRUCTURAL DESIGN OF AN UAV FUSELAGE USING TOPOLOGY OPTIMIZATION METHODS |
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ICAS2018_0605: M. Montel¹, F. Thielecke¹; ¹Hamburg University of Technology, Germany VALIDATION OF A HYBRID OBSERVER METHOD FOR FLIGHT LOADS ESTIMATION |
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ICAS2018_0650: M. Halle¹, F. Thielecke¹; ¹Hamburg University of Technology, Germany LOCAL MODEL NETWORKS APPLIED TO FLIGHT LOADS ESTIMATION |
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ICAS2018_0659: R.S. Martins¹, M.T. Santos, Embraer, Brazil; E.S. Palma¹; ¹UFMG, Brazil FASTENING ANALYSIS USING LOW FIDELITY FINITE ELEMENT MODELS |
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ICAS2018_0677: C. Wallner, USP/Embraer, Brazil; S.F.M. Almeida, Universidade de Sao Paulo, Brazil; C. Kassapoglou, TU Delft, Netherlands MODIFIED WHITNEY-NUISMER CRITERIA FOR PREDICTION OF NOTCHED STRENGTH OF COMPOSITE LAMINATES |
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ICAS2018_0688: U. Kling¹, T. Brügge¹, F. Peter¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany A FRAMEWORK FOR UNCONVENTIONAL LANDING GEAR CONFIGURATION MODELLING |
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ICAS2018_0702: 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 STATIC LOADS EVALUATION IN A FLEXIBLE AIRCRAFT USING HIGH FIDELITY FLUID-STRUCTURE ITERATION TOOL (E2-FSI) |
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ICAS2018_0714: L. Dong¹, D. Cui, Science and Technology committee, China; R. Zhang¹; ¹Chinese Aeronautical Establishment, China BUCKLING/POSTBUCKLING OPTIMIZATION OF STIFFENED COMPOSITE PANELS BASED ON SENSITIVITY ANALYSIS |
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ICAS2018_0720: W. Qian¹, Y. Bai¹, H. Zeng, Shenyang Aircraft Design Institute, China; R. Yang¹; ¹Dalian University of Technology, China AEROELASTIC WIND TUNNEL EXPERIMENT OF A HIGH-ASPECT-RATIO WING MODEL AGAINST GEOMETRICAL NON-LINEARITY |
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ICAS2018_0732: Y. Song¹, B. Harton¹, J. Bayandor¹; ¹CRashworthiness for Aerospace Structures and Hybrids (CRASH Lab), United States VERIFIED FUSELAGE SECTION WATER IMPACT MODELING |
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ICAS2018_0740: 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 ASSESSMENT OF THE AERODYNAMICS AND AEROELASTICITY OF FLAPPING WING USING LINEARIZED COMPUTATIONAL METHOD |
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ICAS2018_0756: V.V. Chedrik, Central Aerohydrodynamic Institute, Russia PROBABILISTIC METHOD OF DETERMINATION OF ALLOWABLE DESIGN PARAMETER SCATTERS ON FLUTTER AND STRENGTH CRITERIA |
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ICAS2018_0784: Y. Bai¹, W. Qian¹, X. Chen¹; ¹Dalian University of Technology, China EXPERIMENTAL AND NUMERICAL STUDIES OF FLUTTER CHARACTERISTICS OF AN ALL-MOVING CONTROL SURFACE AGAINST GAP EFFECTS |
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ICAS2018_0800: F.I. Carvalho¹, R.G. Silva¹; ¹ITA, Brazil INCREASED FLUTTER VELOCITY WITH USE OF A PASSIVE CONTROL SYSTEM |
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ICAS2018_0809: 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 EXPERIMENTAL STUDY OF AEROELASTIC RESPONSE OF A FLEXIBLE HIGH ASPECT RATIO WING WITH PASSIVE SMA ACTUATORS |
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ICAS2018_0826: 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 PREDICTIVE ANALYSIS OF STITCHED AEROSPACE STRUCTURES FOR ADVANCED AIRCRAFT |
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ICAS2018_0836: L.P.S. Ferreira¹, L.V. Donadon¹, P.H. Iscold¹; ¹UFMG, Brazil GROUND VIBRATION TEST USING ACOUSTIC EXCITATION: APPLICATION ON A COMPOSITE WING |
5 - Propulsion |
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ICAS2018_0027: N. Liu, Shanghai Aircraft Design & Research Institute, China A ROBUST STABLE PI CONTROLLER DESIGN IN TIME-FREQUENCY DUAL DOMAINS FOR AIRCRAFT ENGINE |
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ICAS2018_0036: A.I. Lanshin¹, O.V. Sokolova¹, Y.M. Shikhman¹, V.E. Shlyakotin¹; ¹CIAM, Russia RESEARCH OF PROPULSION ENGINES FOR ADVANCE REUSABLE TSTO AEROSPACE SYSTEM |
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ICAS2018_0058: J.-F. Sui, COMAC, China THRUST REVERSER INADVERTENT DEPLOYMENT IMPACT STUDY ON AIRPLANE CONTROLLABILITY |
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ICAS2018_0067: H.R. Gwon¹, W.B. Kim¹, K.W. Lee¹, D.W. Kim¹, H.S. Lee¹; ¹Korean Air, South Korea DEVELOPMENT OF HYBRID GASOLINE-BATTERY PROPULSION SYSTEM FOR MULTI-COPTER PLATFORM |
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ICAS2018_0075: A. Kartashev, Federal State Autonomous Educational Institution of Higher Educa, Russia RESEARCH OF FLOW IN STAGE OF TURBINE AND OPTIMAL MODES OF MICRO GAS TURBINE POWER PLANT |
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ICAS2018_0119: Y. Sun¹, C. Breard¹, X.P. Li¹, Y. Mei², P. Liu², M.B. Pang²; ¹Shanghai Aircraft Design and Research Institute of COMAC, China; ²COMAC Flight Test Center, China IN-FLIGHT ACOUSTIC LOADS MEASUREMENTS ON AN ENGINE FLYING TEST BED |
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ICAS2018_0128: X. Yang¹, J. Xu¹, B. Wang¹, C. Song¹, S. Zhang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China STUDY ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLERS WITH PROPLETS |
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ICAS2018_0147: R.G. Cuenca, UFSC, Brazil; P. Celso Jr.¹, B.M. Rocamora¹; ¹EESC-USP, Brazil PARAMETRIC INVESTIGATION OF EESC-USP AEROACOUSTIC FAN RIG |
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ICAS2018_0149: T. Yatsufusa¹, K. Kii¹, K. Takatani¹; ¹Hiroshima Institute of Technology, Japan PRECISE MEASUREMENT OF PROPAGATING FLAME IN 2-STROKE GASOLINE ENGINE BY MULTIPLE ION-PROBES |
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ICAS2018_0162: X. Liu¹, F. Ferrari¹, L. Manfriani¹; ¹Zurich University for Applied Science, Switzerland NUMERICAL AND EXPERIMENTAL INVESTIGATION OF COOLING CONCEPT FOR AN ELECTRIC PROPULSION SYSTEM FOR AEROBATIC AIRCRAFTS |
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ICAS2018_0243: X.D. Yang, China; Z.B. Liu, China; S.L. Zhang, China; C. Song, China AERODYNAMIC DESIGN OF KEY COMPONENTS OF THE LARGE-DISCHARGE AXIAL FAN AT HIGH ALTITUDE |
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ICAS2018_0306: X.H. Jin¹, B.H. Ma¹, T. Qiu¹; ¹Northwestern Polytechnical University, China SIMULTANEOUS MEASUREMENTS OF TEMPERATURE AND HEAT FLUX IN SUPERSONIC COMBUSTOR BY ITO THIN FILM THERMOCOUPLE |
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ICAS2018_0333: 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 NOVEL JET ENGINE ACOUSTIC LINER WITH IMPROVED BROADBAND NOISE ABSORPTION |
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ICAS2018_0365: V. Monteiro¹, K. Iha¹, O.F.R. Silva¹, T. Ebel, Concepts Nrec, United States; ¹ITA, Brazil MATCHING BETWEEN METAMODEL AND OPTIMIZATION TOOL APPLIED IN A MULTISTAGE AXIAL-FLOW COMPRESSOR AIMING DESIGN IMPROVEMENT |
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ICAS2018_0404: R. MacNeill, The University of Sydney, Australia PROPELLER OPTIMISATION FOR AN ELECTRICAL-POWERED TACTICAL UAS |
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ICAS2018_0416: D. Verstraete, University of Sydney, Australia MULTI-DISCIPLINARY OPTIMISATION OF MEDIUM ALTITUDE LONG ENDURANCE UAVS |
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ICAS2018_0505: L.E. van den Ende¹, Q. Li¹, F. Avallone¹, D. Casalino¹, G. Eitelberg¹, L.L.M. Veldhuis¹; ¹Delft University of Technology, Netherlands AERODYNAMIC AND AEROACOUSTIC INVESTIGATION OF SWIRL RECOVERY VANES FOR PROPELLER PROPULSION SYSTEMS |
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ICAS2018_0508: 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 INVESTIGATION ON AERO-PROPULSIVE BALANCE FOR HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECT |
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ICAS2018_0537: H.R. De Aguiar Quintanilha Jr., University of Liverpool, United Kingdom; L. Santos de Brito Alves, Universidade Federal Fluminense, Brazil ON THE EXISTENCE OF MULTIPLE SELF-EXCITATION FREQUENCIES IN THE INSTABILITY OF INTERACTING PLANAR MIXING LAYER AND WAKE |
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ICAS2018_0624: V.I. Mileshin¹, A.M. Petrovichev¹, S.I. Baeva¹, V.V. Zhdanov¹; ¹Central Institute of Aviation Motors, Russia NUMERICAL AND EXPERIMENTAL STUDY OF THE EFFECT OF CIRCUMFERENTIAL GROOVES ON HPC LAST STAGE PERFORMANCE |
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ICAS2018_0626: S.V. Pankov¹, V.I. Mileshin¹, I.K. Orekhov¹, V.A. Fateev¹; ¹Central Institute of Aviation Motors, Russia CERTAIN ASPECTS OF FAN MODEL STAGE DESIGNING FOR ADVANCED TURBOFANS |
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ICAS2018_0628: V.Y. Aleksandrov¹, A.N. Prokhorov¹, V.L. Semenov¹; ¹Central Institute of Aviation Motors , Russia GROUND FACILITY TESTS OF HIGH SPEED RAMJET DEMONSTRATORS |
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ICAS2018_0629: S.V. Belov¹, G.B. Zhestkov¹, D.V. Muravsky¹, S.V. Kharkovsky¹, E.V. Shcherbakova¹; ¹CIAM, Russia THE INFLUENCE OF THE SHAPE OF THE COOLING CHANNEL AND PRESSURE GRADIENT ON THE EFFICIENCY OF FILM COOLING OF GTE BLADES |
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ICAS2018_0637: O.S. Gurevich¹, A.I. Gulienko¹, M.V. Gordin¹; ¹CIAM, Russia CHARACTERISTICS OF SYSTEMS WITH ELECTRICALLY DRIVEN UNITS - EXPERIMENTAL STUDIES IN A GAS TURBINE ENGINE DEMONSTRATOR |
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ICAS2018_0638: S. Kaiser¹, H. Kellermann¹, M. Nickl¹, A. Seitz¹; ¹Bauhaus Luftfahrt e.V., Germany A COMPOSITE CYCLE ENGINE CONCEPT FOR YEAR 2050 |
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ICAS2018_0639: L.G. Bliznyukov¹, M.G. Kesselman¹, V.I. Chernyshov¹, S.A. Smetanin¹; ¹Central Institute of Aviation Motors, Russia ADAPTTIVE GTE SURGE PROTECTION SYSTEM WITH SELECTIVE CONTROL OF ACTUATORS |
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ICAS2018_0640: O.S. Gurevich¹, F.D. Golberg¹, S.A. Smetanin¹, N.E. Romanenko¹; ¹Central Institute of Aviation Motors, Russia APPLICATION OF "VIRTUAL" CONTROLLERS FOR INTEGRATED PROPULSION AND AIRCRAFT CONTROL |
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ICAS2018_0643: F.D. Golberg¹, O.S. Gurevich¹, A.A. Petukhov¹; ¹CIAM, Russia IDENTIFICATION METHOD OF THE SIMULATION MODEL "VIRTUAL ENGINE" BUILT INTO THE DIGITAL ENGINE CONTROL SYSTEM |
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ICAS2018_0645: V.Y. Aleksandrov¹, M.V. Ananyan, MIPT, Russia; K.Y. Arefyev¹, O.D. Dikova², A.N. Prokhorov¹, K.V. Fedotova², L.S. Yanovskiy¹; ¹CIAM, Russia; ²BMSTU, Russia INVESTIGATION OF THE PROCESS SUBLIMATION FOR SOLID HYDROCARBONS IN PERMANENT SECTION CHANNELS |
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ICAS2018_0652: A.D. Nepomnyashchiy¹, I.V. Tsvetkov¹, S.V. Suntsov¹, S.Y. Danilkin¹; ¹CIAM, Russia PERFORMANCES OF LPT AND LINEAR CASCADES AT LOW REYNOLDS NUMBERS |
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ICAS2018_0654: A. Mirzoyan¹, A. Isyanov¹, D. Fokin¹, R. D´Ippolito², R. Lombardi²; ¹CIAM, Russia; ²Noesis, Belgium MULTIOBJECTIVE MULTIPARAMETRIC OPTIMIZATION OF PROPULSION SYSTEM FOR ADVANCED CIVIL AIRCRAFT IN DISTRIBUTED ENVIRONMENT OF COLLABORATIVE MDO SYSTEM DEVELOPED IN AGILE PROJECT |
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ICAS2018_0655: M. Fioriti, Politecnico di Torino, Italy; L. Boggero, German Aerospace Center (DLR), Germany; A. Mirzoyan¹, A. Isyanov¹; ¹CIAM, Russia STUDIES ON PROPULSION AND ON-BOARD SYSTEMS MATCHING IN AGILE PROJECT DISTRIBUTED COLLABORATIVE MDO ENVIRONMENT APPLYING FOR ADVANCED REGIONAL AND MEDIUM HAUL JET |
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ICAS2018_0660: A. Bacciaglia¹, D. Guo², P. Marzocca², C. Bil², A. Ceruti¹; ¹University of Bologna, Italy; ²RMIT University, Australia BIMODAL UNMANNED VEHICLE: PROPULSION SYSTEM INTEGRATION AND WATER/AIR INTERFACE TESTING |
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ICAS2018_0672: 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 COMPLEX NUMERICAL AND EXPERIMENTAL RESEARCH OF HEXAFLY-INT HIGH-SPEED CIVIL AICRAFT MODEL |
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ICAS2018_0728: P.C. Vratny¹, F. Troeltsch¹, J. Bijewitz¹, J. Kaiser¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany DESIGN AND OFF-DESIGN PERFORMANCE OF ELECTRIC SYSTEM ARCHITECTURES FOR ELECTRIC POWERED AIRCRAFT |
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ICAS2018_0742: P.D. Toktaliev, Central Institute of Aviation Motors, Russia COMMUNICATION BETWEEN PS AND AIRCRAFT SYSTEMS IN COLLECTIVE MDO SYSTEM IN AGILE PROJECT |
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ICAS2018_0769: M. Kowalski¹, A. Jankowski¹; ¹AFIT, Poland ENGINE TEST RESULTS OF FUEL-WATER MICROEMULSION |
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ICAS2018_0788: 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 PROPULSION SYSTEM - AIRFRAME INTEGRATION AND OPTIMIZATION OF CIVIL AIRCRAFT- AGILE EU PROJECT |
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ICAS2018_0820: D. Kalinin¹, V. Golovanov¹, J. Temis, BMSTU, Russia; L. Magerramova¹; ¹CIAM, Russia DYNAMIC MODEL FOR PLANETARY GEAR SETS OF GEARED TURBOFAN JET ENGINES |
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ICAS2018_0825: M. Kowalski¹, A. Jankowski¹, R. Szczepanik, Polish Air Force Academy Deblin, Poland; ¹AFIT, Poland OPTIMIZATION OF THE FUEL INJECTOR TO AN INTERNAL COMBUSTION ENGINE BY MEANS OF LASER EQUIPMENT |
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ICAS2018_0831: H. Gesell¹, F. Wolters¹, M. Plohr¹; ¹DLR, Germany SYSTEM ANALYSIS OF TURBO ELECTRIC AND HYBRID ELECTRIC PROPULSION SYSTEMS ON A REGIONAL AIRCRAFT |
6.1 - Flight Dynamics and Control (Control & Modelling) |
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ICAS2018_0009: L. Zhaohui¹, L. Gang¹; ¹Chinese Flight Test Establishment, China KNOWLEDGE ENGINEERING BASED FLIGHT TEST TECHNOLOGY FOR CIVIL AIRCRAFT AIRWORTHINESS CONFORMITY |
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ICAS2018_0016: P.V. Kuzmin¹, N.A. Surkov¹, Y.F. Shelyukhin¹; ¹TsAGI, Russia MATHEMATICAL MODEL OF COMMERCIAL AIRPLANE DYNAMICS AT STALL |
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ICAS2018_0096: F. Abdelmoula¹, M. Scholz¹; ¹DLR Institute of Flight Systems, Germany LNAS - A PILOT ASSISTANCE SYSTEM FOR LOW-NOISE APPROACHES WITH MINIMAL FUEL CONSUMPTION |
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ICAS2018_0125: L. Guo¹, M. Zhu¹, J. Guan¹, B. Nie¹; ¹China Aerodynamics Research and Development Centre, China WIND TUNNEL VIRTUAL FLIGHT TEST FOR A TRANSPORT AIRCRAFT WITH SIMULATED ICE SHAPE |
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ICAS2018_0200: P. Krus, Linköping university, Sweden; B. Lantto, Saab AB, Sweden; M.A. Rodriguez¹, E. Villani¹; ¹Instituto Technologico Aeronautica, Italy EFFECTS OF TAILORED CONTROL SURFACE COMPLIANCE ON AIRCRAFT STABILITY AND CONTROL |
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ICAS2018_0218: J. Lee¹, Y. Kim¹; ¹Seoul National University, South Korea QUASI-LPV MODELING AND PARAMETER-DEPENDENT OPTIMAL CONTROL OF MORPHING WING AIRCRAFT |
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ICAS2018_0221: P. Piprek¹, F. Holzapfel¹; ¹Technical University of Munich, Germany BI-LEVEL TRAJECTORY OPTIMIZATION BY STOCHASTIC COLLOCATION FOR UNCERTAINTY INTERVAL CALCULATION |
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ICAS2018_0241: M. Sato, Japan Aerospace Exploration Agency, Japan MANEUVERABILITY ASSESSMENT FOR FAULTY AIRPLANE BY IFS WITH SIMULTANEOUS MODEL-MATCHING FOR GUST AND HANDLING RESPONSES |
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ICAS2018_0279: C. Grillo, Università di Palermo, Italy RECURSIVE AERODYNAMIC PARAMETER IDENTIFICATION OF A FIGHTER JET FLYING IN TURBULENT AIR |
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ICAS2018_0406: 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 A LOW COST MODEL AIRCRAFT FLIGHT RESEARCH FACILITY IN WIND TUNNEL |
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ICAS2018_0431: 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 MONTE-CARLO EVALUATION OF CONTROL LAW FOR HIGH ALTITUDE FLIGHT TEST OF MARS AIRPLANE |
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ICAS2018_0434: C. Krause¹, C. Göttlicher¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, Germany DEVELOPMENT OF A GENERIC FLIGHT TEST MANEUVER INJECTION MODULE |
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ICAS2018_0460: D. Drewiacki, Embraer, Brazil; F.J. Silvestre¹, A.B. Guimarães Neto¹; ¹Instituto Tecnológico de Aeronáutica, Brazil THE INFLUENCE OF BIODYNAMIC FEEDTHROUGH ON HANDLING QUALITIES |
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ICAS2018_0468: T. Hou¹, C. Chen¹, T. Hu¹; ¹Lu Shijia Labortory, Beihang University, China PASSIVE CONTROL METHOD IN ATTENUATING SELF-INDUCED ROLL OSCILLATIONS OF LOW-ASPECT-RATIO WINGS USING OBLIQUE SLOT BLEED |
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ICAS2018_0492: E. Dillinger, ISAE-SUPAERO/ONERA, France; C. Döll¹, R. Liaboeuf¹, C. Toussaint¹, J. Hermetz¹, C. Verbeke¹, M. Ridel¹; ¹ONERA, France HANDLING QUALITIES OF ONERA’S SMALL BUSINESS CONCEPT PLANE WITH DISTRIBUTED ELECTRIC PROPULSION |
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ICAS2018_0500: M.A.V. Morales¹, F.J. Silvestre¹, A.B. Guimarães Neto¹, G. Tissot, Université Paul Sabatier, France; ¹Instituto Tecnológico de Aeronáutica, Brazil CONTROL OF A VERY FLEXIBLE WING WITH SIMULTANEOUS OPTIMIZATION OF THE GAIN MATRIX AND THE SPATIAL DISTRIBUTION OF THE SENSORS |
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ICAS2018_0501: 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 ON REAL–TIME SIMULATION OF FLEXIBLE AIRCRAFT WITH PHYSICS–DERIVED MODELS |
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ICAS2018_0506: D.F. Hidalgo, Universidad pontificia bolivariana, Colombia; G.B. Rodamilans¹, W.R. de Oliveira¹; ¹CCM-Instituto Tecnologico de Aeronautica, Brazil CHARACTERISTIC HELICOPTER FLIGHT MECHANICS AND MOTION CUEING INTEGRATION INTO THE SIVOR ROBOTIC FLIGHT SIMULATOR: AN OBJECTIVE APPROACH |
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ICAS2018_0521: L.P.G. Pinto¹, P. Krus¹, V.J. De Negri, Universidade Federal de Santa Catarina, Brazil; ¹Linköping University, Sweden DIGITAL HYDRAULICS IN AEROSPACE APPLICATIONS: SLIDING MODE OF QUANTIZED CONTROL AND LMI APPROACH |
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ICAS2018_0523: A.B. Guimarães Neto¹, F.L. Cardoso-Ribeiro¹, F.J. Silvestre¹; ¹ITA, Brazil APPLICABILITY OF GEOMETRICALLY-LINEAR STRUCTURAL-DYNAMIC MODELS FOR THE FLIGHT DYNAMICS OF ARBITRARILY-FLEXIBLE AIRCRAFT |
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ICAS2018_0529: R.M. Bertolin¹, A.B. Guimarães Neto¹, G.C. Barbosa¹, F.J. Silvestre¹; ¹Instituto Tecnológico de Aeronáutica, Brazil ADAPTIVE OUTPUT-FEEDBACK GAIN SCHEDULING APPLIED TO FLEXIBLE AIRCRAFT |
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ICAS2018_0534: P.J. Gonzalez¹, C.E.S. Cesnik ¹, F.J. Silvestre, Instituto Tecnologico de Aeronautica, Brazil; ¹University of Michigan, United States IMPLEMENTATION AND FLIGHT TESTING OF AN ENHANCED STABILITY SYSTEM FOR A VERY FLEXIBLE AIRCRAFT |
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ICAS2018_0559: Y.A. Díaz-Méndez¹, M.S. Sousa¹, S.S. Cunha Jr.¹, G.F. Gomes¹; ¹Federal University of Itajubá, Brazil A COMPARISON BETWEEN UNIVERSAL INTEGRAL REGULATOR AND LINEAR QUADRATIC TECHNIQUE FOR AN AIRCRAFT AUTOPILOT |
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ICAS2018_0564: T. Akman¹, J. Diepolder¹, B. Grüter¹, F. Holzapfel¹; ¹Technical University of Munich, Germany USING SENSITIVITY PENALTIES TO ROBUSTIFY THE OPTIMAL REENTRY TRAJECTORY OF A HYPERSONIC VEHICLE |
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ICAS2018_0581: A.D. Kraemer¹, E. Villani¹; ¹Instituto Tecnológico de Aeronáutica (ITA), Brazil DATA-DRIVEN FAILURE IDENTIFICATION USING A MOTION-BASED SIMULATOR |
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ICAS2018_0607: G. Di Rito¹, R. Galatolo¹, F. Schettini¹; ¹Università di Pisa - Dip. Ing. Civile ed Industriale, Italy MULTI-VARIABLE AIRCRAFT DIRECTIONAL CONTROL WITH ANTI-SKID DIFFERENTIAL BRAKES |
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ICAS2018_0613: T. Rogalski¹, A. Tomczyk¹; ¹Rzeszów University of Technology, Poland APPLICATION OF THE DISTURBANCE VALUE MEASURED DURING THE REAL FLIGHT TO THE FLIGHT CONTROL SYSTEM SYNTHESIS |
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ICAS2018_0651: R. Takase¹, J.O. Entzinger¹, S. Suzuki¹; ¹The University of Tokyo, Japan FAULT-TOLERANT FLIGHT CONTROL SYSTEM WITH SIMPLE ADAPTIVE CONTROL CONSIDERING PILOT INPUT |
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ICAS2018_0661: 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 BIO-DYNAMIC STABILITY ANALYSIS OF A GREBE DURING MIGRATION |
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ICAS2018_0665: N. Yoshikawa, The university of Tokyo, Japan FAULT TOLERANT CONTROL SYSTEM OF AIRCRAFT BY FEEDBACK ERROR LEARNING WITH SYSTEM ESTIMATION |
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ICAS2018_0683: M. Naruoka, Japan Aerospace Exploration Agency, Japan BAYESIAN APPROACH TO FLIGHT CHARACTERISTICS MODELING WITH REAL FLIGHT DATA |
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ICAS2018_0699: G.R. Ridgway¹, H.R. Shattock¹, A.C.R. Hare¹; ¹QinetiQ, United Kingdom BEYOND BEDFORD; DEVELOPMENT OF A TWO-DIMENSIONAL PILOT WORKLOAD RATING SCALE |
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ICAS2018_0726: A.E. Sagalakov¹, A.S. Filatyev¹; ¹TsAGI, Russia NEW APPROACH FOR INVESTIGATION OF MAXIMUM-RANGE AIRCRAFT TRAJECTORIES |
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ICAS2018_0764: 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 IDENTIFICATION OF THE LATERAL-DIRECTIONAL MODEL OF THE VECTOR-P, UNMANNED AERIAL VEHICLE |
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ICAS2018_0765: L.M. Nepomuceno, Brazil SYSTEM IDENTIFICATION OF A SUBSCALE FIGHTER AIRCRAFT |
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ICAS2018_0796: M. Hiruma, The University of Tokyo, Japan EVALUATION OF ALTITUDE CONTROL FOR AN AIRBREATHING HYPERSONIC AIRCRAFT MODEL |
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ICAS2018_0813: R.C.M.G. Barbosa¹, L.C.S. Góes¹; ¹ITA, Brazil CLOSED-LOOP SYSTEM IDENTIFICATION OF A LARGE FLEXIBLE AIRCRAFT USING SUBSPACE METHODS |
6.2 - Flight Dynamics and Control (UAV related) |
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ICAS2018_0046: S. Lee¹, Y. Kim¹; ¹Seoul National University, South Korea PERFORMANCE ANALYSIS OF UAV PERSISTENT SURVEILLANCE ALGORITHM |
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ICAS2018_0080: S. Lee¹, S. Ann¹, Y. Kim¹; ¹Seoul National University, South Korea MODIFIED COMPOSITE GUIDANCE LAW AGAINST MOVING TARGET CONSIDERING NARROW FIELD-OF-VIEW LIMIT |
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ICAS2018_0161: M. Schütt¹, T. Islam¹, P. Hartmann¹, D. Moormann¹; ¹Institute of Flight System Dynamics, RWTH Aachen University , Germany SCALABLE DESIGN APPROACH TO ANALYZE FLIGHT MECHANICAL PERFORMANCE OF TILT-WING UAVS |
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ICAS2018_0171: A.C. Daud Filho¹, E.M. Belo¹; ¹EESC-USP, Brazil FLIGHT DYNAMICS MODELING AND TRIM CURVES OF A CONCEPTUAL SEMI-TANDEM WING VTOL UAV |
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ICAS2018_0210: H. Ma¹, B.F. Song¹, Y. Pei¹, Z.W. Chen¹; ¹School of Aeronautics, Northwestern Polytechnical University, China AERODYNAMIC ANALYSIS AND CONTROL ALLOCATION FOR ASYMMETRIC VARIABLE SWEEP AIRCRAFT WITH FLEXIBLE TRAILING EDGE |
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ICAS2018_0219: T. Yamashita¹, Y. Kajiwara¹, C.T. Raabe², T. Tsuchiya², S. Suzuki²; ¹Ricoh Co. Ltd, Japan; ²the University of Tokyo, Japan AUTONOMOUS FLIGHT OF UNMANNED MULTICOPTER USING SUPER WIDE-ANGLE STEREO VISION SYSTEM |
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ICAS2018_0224: P. Piprek¹, F. Holzapfel¹; ¹Technical University of Munich, Germany ROBUST TRAJECTORY OPTIMIZATION OF VTOL TRANSITION MANEUVER USING BI-LEVEL OPTIMAL CONTROL |
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ICAS2018_0233: J.-P. Theron¹, L. Dala, Northumbria University Newcastle, United Kingdom; D.N. Wilke¹, P. Barrier, UAS consultant, South Africa; ¹University of Pretoria, South Africa PRACTICAL IMPLEMENTATION OF A TRAJECTORY PLANNING ALGORITHM FOR AN AUTONOMOUS UAV |
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ICAS2018_0254: V. Golubev¹, P. Kazarin¹, C. Moreno¹, W. MacKunis¹; ¹ERAU, United States ON WAKE VORTEX SAFETY ANALYSIS AND CONTROL FOR UAV |
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ICAS2018_0260: J.-W. Lee¹, A.T. Nguyen, Le Quy Don Technical University , Vietnam; J.-H. Han¹; ¹KAIST, South Korea LONGITUDINAL FLIGHT CONTROL OF BIOINSPIRED FLAPPING-WING MICRO AIR VEHICLE WITH EXTENDED UNSTEADY VORTEX-LATTICE METHOD. |
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ICAS2018_0348: P.-C. Wen¹, Y.-D. Zhang¹, Y.-H. Li¹; ¹AVIC Xi'an Aeronautics Computing Technique Research Institute, China MULTI-CHANNEL HUMAN-MACHINE INTERACTIVE SYSTEM FOR MULTIPLE UAVS' CONTROL |
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ICAS2018_0393: S. Balachandran, National Institute of Aerospace, United States; A. Narkawicz¹, C. Munoz¹, M. Consiglio¹; ¹NASA Langley Research Center, United States AN EVALUATION OF VARIOUS GEOFENCE CONFLICT RESOLUTION ALGORITHMS AND THEIR IMPACT ON MISSION PERFORMANCE |
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ICAS2018_0396: J.L. Gomes Olavo¹, L.A. Borges Tôrres¹, T. Argolo Jesus, CEFET/MG, Brazil; ¹UFMG, Brazil FIXED-WING UAV ROBUST GUIDANCE STRATEGY BASED ON COMPOUND FLIGHT MISSION OF ON-GROUND TARGETS |
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ICAS2018_0415: S. Higashino, Kyushu University, Japan; K. Nakama, Kyushu University, Graduate Student, Japan VERTICAL LANDING OF A FIXED-WING UAV USING THE FLAT SPIN |
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ICAS2018_0533: F. Machini¹, I.O. Tarifa¹, R.M.F. Neto¹, L. Sanches¹; ¹Universidade Federal de Uberlândia, Brazil MODELING, CONTROL AND HARDWARE-IN-THE-LOOP SIMULATION OF A GENERIC TILTING MULTI-ROTOR |
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ICAS2018_0586: J.C. Vendrichoski¹, T.L. Costa¹, E.S. El´Youssef¹, E.R. de Pieri¹; ¹UFSC, Brazil MODELLING AND CONTROL OF A BI-TILT-ROTOR UAV WITH DOUBLE GIMBAL AND CAMERA FOR SURVEILLANCE SYSTEMS APPLICATION |
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ICAS2018_0614: S.M. Herrington¹, T.D. Fields¹, O.A. Yakimenko, Naval Postgraduate School, United States; ¹University of Missouri-Kansas City, United States FLIGHT PERFORMANCE OF STEERABLE CRUCIFORM PARACHUTE SYSTEMS |
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ICAS2018_0663: A. Sobron¹, D. Lundström¹, R. Larsson², P. Krus¹, C. Jouannet²; ¹Linköping University, Sweden; ²Saab Aeronautics, Sweden METHODS FOR EFFICIENT FLIGHT TESTING AND MODELLING OF REMOTELY PILOTED AIRCRAFT WITHIN VISUAL LINE-OF-SIGHT |
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ICAS2018_0754: K. Iwata¹, K. Yamada¹, R. Horiuchi¹, A. Kamimura¹; ¹National Institute of Advanced Industrial Science and Technology, Japan SAFETY FLIGHT TESTING FOR CARGO UAV DEVELOPMENT |
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ICAS2018_0792: H. Omagari, Department of Aeronautics and Astronautics, Kyushu University, Japan POTENTIAL BENEFITS ASSESSMENT ON HOME DELIVERY SERVICE USING MULTIPLE DRONES |
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ICAS2018_0840: G. Pogorzelski, CENIC Engenharia, Brazil; F.J. Silvestre, ITA - Instituto Tecnológico de Aeronáutica, Brazil A STRATEGY FOR UAV PERFORMANCE ENHANCEMENT THROUGH ATMOSPHERIC ENERGY EXTRACTION USING MPC TECHNIQUES |
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ICAS2018_0844: M.E. Kügler¹, F. Holzapfel¹; ¹Technical University of Munich, Inst. of Flight System Dynamics, Germany PLANNING, IMPLEMENTATION, AND EXECUTION OF AN AUTOMATIC FIRST FLIGHT OF A UAV |
7 - Systems, Subsystems and Equipment |
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ICAS2018_0015: W. Niu¹, J. Cheng, Xi’an Institute of Applied Optics, China; W. Niu¹; ¹AVIC Computing Technique Research Institute, China FAULT DIAGNOSIS METHOD STUDY FOR COMPLEX SYSTEM BASED ON KALMAN FILTERS |
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ICAS2018_0052: 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 A HYBRID DIGITAL-PROPORTIONAL HYDRAULIC ACTUATION SYSTEM FOR AIRCRAFT FLIGHT CONTROL |
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ICAS2018_0100: M. Zheng¹, T. Wu¹, Z. Guo¹, W. Dong¹; ¹Shanghai Jiao Tong University, China CALCULATION OF WATER FILM FLOW AND HEAT TRANSFER ON THE AIRCRAFT ANTI-ICING SURFACE |
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ICAS2018_0129: Z. Dai¹, Z. Qiu, Xi'an Aeronautics Computing Technique Research Institute, China; L. Shi¹; ¹ChengDu Aircraft Design & Research Institute, China AN AIRBORNE DATA BUS NETWORK SYSTEM OF INTERFACE ADAPTIVE AND FLEXIBLE CONTROL |
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ICAS2018_0170: S. Delbecq¹, M. Budinger, Institut Clément Ader (UMR CNRS 5312), France; J. Piaton¹; ¹Safran Electronics & Defense, France A MORE INTEGRATED DESIGN APPROACH FOR EMBEDDED MECHATRONIC SYSTEMS: APPLICATION TO ELECTRICAL THRUST REVERSER ACTUATION SYSTEMS |
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ICAS2018_0180: V. De Simone¹, R. Scigliano¹, P. Catalano¹; ¹Italian Aerospace Research Centre (CIRA), Italy DE-ICING PHENOMENA MODELLED BY FINITE ELEMENT MODELS |
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ICAS2018_0182: J. Gauci¹, K. Theuma¹, R. Archer, Hawk Aerospace, Malta; R. Grech, Idox Health, Malta; D. Zammit-Mangion¹; ¹University of Malta, Malta GROUND AND FLIGHT TESTING OF A MULTI-SENSOR OBSTACLE DETECTION AND TRACKING SYSTEM FOR RPAS SITUATION AWARENESS |
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ICAS2018_0194: H.C. Moura¹, G.S.P. Alegre¹, J.H. Bidinotto¹, E.M. Belo¹; ¹University of São Paulo, Engineering School of São Carlos, Brazil PIO SUSCEPTIBILITY IN FLY-BY-WIRE SYSTEMS |
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ICAS2018_0214: J.P. Kang¹, G.J. Shim¹, K.J. Yee¹; ¹Seoul national university, South Korea COST-EFFECTIVE TELEMETRY, TRACKING AND COMMAND SYSTEM DEVELOPMENT FOR HIGH-ALTITUDE SCIENTIFIC BALLOON |
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ICAS2018_0271: R. Kowalski¹, J. Windelberg¹, R. Ladner², M. Rottach²; ¹German Aerospace Center (DLR e.V.), Germany; ²Liebherr-Aerospace Lindenberg GmbH, Germany FORCE FIGHT COMPENSATION FOR REDUNDANT ELECTRO-MECHANICAL FLIGHT CONTROL ACTUATORS |
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ICAS2018_0402: D.H. Arjoni¹, E. Villani¹, M. Rodríguez¹, A. Matheus¹, A. Almeida¹, G. Rocha¹, L.G. Trabasso¹, D. Hidalgo, UPB, Colombia; ¹ITA, Brazil EXPERIMENTAL ANALYSIS OF FLIGHT PERFORMANCE UNDER WORKLOAD VARIATIONS |
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ICAS2018_0412: L. Boggero¹, M. Fioriti², F. Tomasella², P.D. Ciampa¹; ¹German Aerospace Center, Germany; ²Politecnico di Torino, Italy INTEGRATION OF ON-BOARD SYSTEMS PRELIMINARY DESIGN DISCIPLINE WITHIN A COLLABORATIVE 3RD GENERATION MDO FRAMEWORK |
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ICAS2018_0429: R. Fusaro¹, D. Ferretto¹, V. Vercella¹, N. Viola¹, V. Fernandez Villace², J. Steelant ²; ¹Politecnico di Torino, Italy; ²ESA-ESTEC, Netherlands A METHODOLOGY FOR PRELIMINARY SIZING OF A THERMAL AND ENERGY MANAGEMENT SYSTEM FOR A HYPERSONIC VEHICLE |
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ICAS2018_0463: J. Schminder¹, R. Hällqvist², M. Eek², R. Gårdhagen¹; ¹Linköping University, Sweden; ²Saab Aeronautics, Sweden PILOT PERFORMANCE AND HEAT STRESS ASSESSMENT SUPPORT USING A COCKPIT THERMOREGULATORY SIMULATION MODEL |
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ICAS2018_0464: D. Liu, China Aerodynamics Research and Development Center, China; X. Gao, National University of Defense Technology, China WIND SHEAR PARAMETER ESTIMATION FOR DYNAMIC SOARING WITH UNMANNED AERIAL VEHICLES |
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ICAS2018_0548: J. Mašek, Brno University of Technology,Institute of Aerospace Engineering, Czech Republic THERMO-VACUUM TEST CHAMBER DEVELOPMENT FOR AIRBORNE AND SPACE EQUIPMENT TESTING IN SIMULATED EXTREME CONDITIONS |
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ICAS2018_0569: A.C. Sanches¹, F.J. Silvestre¹, M.A.V. Morales¹, H. Hesse, University of Glasgow, Singapore; ¹Aeronautics Institute of Technology, Brazil DESIGNING A VISION-BASED SYSTEM TO MEASURE IN-FLIGHT WING DEFORMATION |
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ICAS2018_0609: 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 DESIGN CRITERIA OF A THERMAL MASS FLOW SENSOR FOR AIRCRAFT AIR DATA APPLICATIONS |
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ICAS2018_0611: 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 DETECTING HIGH-ALTITUDE ICE CRYSTAL (HAIC) ICING EVENTS FROM TOTAL AIR TEMPERATURE |
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ICAS2018_0620: K. Szilder, Aerospace, National Research Council, Canada; E. Lozowski, University of Alberta, Canada NUMERICAL SIMULATION OF ICE ACCRETION INFLUENCED BY AN ANTI-ICING HEATING SYSTEM |
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ICAS2018_0625: G. Di Rito¹, F. Schettini¹; ¹Università di Pisa - Dip. di Ing. Civile ed Industriale, Italy SMART FAULT-TOLERANT AIR-DATA SENSOR FOR AIRCRAFT FLOW ANGLES MEASUREMENT |
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ICAS2018_0653: J. Fu¹, J.-C. Mare, INSA-Toulouse, France; Y. Fu¹; ¹Beihang University, China POSITION SYNCHRONIZATION OF AEROSPACE ELECTROMECHANICAL ACTUATORS FOR DISTRIBUTED ELECTRICAL ACTUATION SYSTEM |
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ICAS2018_0684: H. Pham¹, Y. Lim¹, A. Gardi¹, R. Sabatini¹, E. Pang¹; ¹RMIT University, Australia A NOVEL BISTATIC LIDAR SYSTEM FOR EARLY-DETECTION OF PLANT DISEASES FROM UNMANNED AIRCRAFT |
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ICAS2018_0774: S. Bagassi¹, F. Lucchi¹, F. De Crescenzio¹, S. Piastra¹; ¹University of Bologna, Italy DESIGN FOR COMFORT: AIRCRAFT INTERIORS DESIGN ASSESSMENT THROUGH A HUMAN CENTERED RESPONSE MODEL APPROACH |
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ICAS2018_0818: 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 POWER LINE COMMUNICATION APPLIED TO FLIGHT TEST INSTRUMENTATION |
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ICAS2018_0853: T. Seung, Program Management Office Aeronautics Research / DLR del. iABG, Germany SELF-INDUCED FAULT OF A HYDRAULIC SERVO VALVE |
8 - Manufacturing and Supply Chain Management |
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ICAS2018_0012: H. Abramovich¹, N. Broitman¹, A. Shirizly¹; ¹Technion, I.I.T., Israel INVESTIGATION OF CRACK PROPAGATION PROPERTIES OF ADDITIVE MANUFACTURING PRODUCTS |
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ICAS2018_0101: J. Madrid¹, J. Landahl¹, R. Söderberg¹, H. Johannesson¹, J. Lööf, GKN Aerospace, Sweden; ¹Chalmers University of Technology, Sweden MITIGATING RISK OF PRODUCIBILITY FAILURES IN PLATFORM CONCEPT DEVELOPMENT |
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ICAS2018_0319: P. Xu¹, X. Wang¹, S. Bi¹, H. Cui¹; ¹Shenyang Aircraft Design and Resesarch Institute, China APPLICATION RESEARCH OF LARGE-SCALED COMPLICATED FRAME-BEAM INTEGRAL COMPONENT BASED ON ELECTRON BEAM ADDITIVE MANUFACTURING |
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ICAS2018_0723: X. Wang¹, H. Cui¹, P. Xu¹, S. Bi¹; ¹Shenyang Aircraft Design and Resesarch Institute, China AIRCRAFT STRUCTURE TECHNOLOGY OF ADDITIVE MANUFACTURING |
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ICAS2018_0850: O.L. Pinon¹, D.J.L. Siedlak¹, D. Mavris¹; ¹Georgia Institute of Technology, United States ENABLING THE DIGITAL FACTORY THROUGH THE INTEGRATION OF DATA-DRIVEN AND SIMULATION MODELS |
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ICAS2018_0851: C. Justin¹, A. Ramamurthy¹, N. Beals², E. Spero², D. Mavris¹; ¹GEORGIA INSTITUTE OF TECHNOLOGY, United States; ²U.S. ARMY RESEARCH LABORATORY, United States ON-DEMAND SMALL UAS ARCHITECTURE SELECTION AND RAPID MANUFACTURING USING A MODEL-BASED SYSTEMS ENGINEERING APPROACH |
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ICAS2018_0866: M.Q. Chu¹, X.W. Zhou¹, X.F. Sun¹, L. Wang¹; ¹COMAC, China EVALUATION OF MECHANICAL PROPERTIES OF TI-6AL-4V FABRICATED BY SELECTIVE LASER MELTING (SLM) |
9 - Air Transport System Efficiency |
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ICAS2018_0021: F. Linke, German Aerospace Center (DLR), Germany THE GLOBAL FUEL SAVING POTENTIAL OF INTERMEDIATE STOP OPERATIONS CONSIDERING METEOROLOGICAL AND OPERATIONAL INFLUENCES |
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ICAS2018_0050: T. Dautermann¹, T. Ludwig¹, L. Altenscheidt¹, M. Altenscheidt, NavArt, Germany; R. Geister¹, M. Braschczok¹; ¹DLR, Germany PERFORMANCE COMPARISON OF A320 AND 737NG REGARDING THE VERTICAL AND AND SPEED PROFILES IN ADVANCED RNP TO XLS ARRIVALS |
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ICAS2018_0059: D. Jeon¹, Y. Eun¹, H. Kim¹, S. Kim¹, E. Oh¹, M. Jeong¹; ¹Korea Aerospace Research Institute, South Korea INTEGRATED ARRIVAL AND DEPARTURE MANAGEMENT FOR JEJU INTERNATIONAL AIRPORT |
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ICAS2018_0063: A. Errico¹, V. Di Vito¹; ¹CIRA – Italian Aerospace Research Center, Italy ALGORITHMS AND SYSTEM FOR CURVED AND CONTINUOUS DESCENT TRAJECTORIES IMPROVING FUEL EFFICIENCY IN TMA |
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ICAS2018_0158: K. Kageyama¹, Y. Nakamura¹; ¹ENRI, Japan A SIMULATION MODELING STUDY FOR FREE ROUTING AIRSPACE IN JAPAN |
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ICAS2018_0174: T. Riedel, Keio University / Electronic Navigation Research Institute, Japan A NOVEL CONTROL APPROACH TO IMPROVE SPEED COMMANDS AND PILOT WORKLOAD FOR FLIGHT-DECK BASED INTERVAL MANAGEMENT |
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ICAS2018_0178: G. Tay¹, S. Gillen¹, R. Rothfeld, Bauhaus Luftfahrt e.V., Germany; M. Hornung¹; ¹Technical University of Munich, Germany EVALUATION OF THE POTENTIAL IMPACTS OF HYBRID-ELECTRIC AIRCRAFT ON THE GLOBAL AIR TRANSPORTATION NETWORK |
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ICAS2018_0211: Y. Eun¹, D. Jeon¹; ¹Korea Aerospace Research Institute, South Korea AIRPORT SURFACE TRAFFIC SCHEDULING WITH CONSIDERATION OF DE-ICING OPERATIONS |
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ICAS2018_0268: B. Cui¹, L. Meilong¹, R. Curran, Delft University of Technology, Netherlands; ¹Nanjing University of Aeronautics and Astronautics, China CASCADING FAILURE OF NODES AND THEIR LINKS IN A COMPLEX NETWORK |
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ICAS2018_0277: F. Will¹, M. Hornung¹; ¹Technical University of Munich, Germany A FRAMEWORK TO ASSESS FUTURE AIRPORT NOISE APPLIED TO A TWO-RUNWAY AIRPORT |
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ICAS2018_0282: J. Ren¹, L. Wang¹; ¹Civil Aviation University of China, China VISUAL FLIGHT PROCEDURE DESIGN IN CHINA |
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ICAS2018_0315: D. Toratani¹, N.K. Wickramasinghe¹, E. Itoh¹; ¹Electronic Navigation Research Institute, Japan STUDY ON THE ARRIVAL MANAGER MAXIMIZING THE BENEFIT OF FOUR-DIMENSIONAL TRAJECTORY BASED OPERATIONS |
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ICAS2018_0433: A. Spiteri, University of Malta, Malta AN ATC ORIENTED INTERFACE FOR MULTI-AIRCRAFT OPTIMISATION FOR CLIMBS AND DESCENTS |
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ICAS2018_0452: T. Iijima¹, N. Matayoshi¹, S. Ueda¹; ¹JAXA, Japan OPERATIONAL CONCEPT AND VALIDATION OF A NEW AIRPORT LOW-LEVEL WIND INFORMATION SYSTEM |
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ICAS2018_0457: Z. Zhang¹, J. Wang¹; ¹Civil Aviation University of China, China STUDY ON LARGE-SCALE FLIGHT DELAY RECOVERY |
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ICAS2018_0487: M. Schultz, DLR, Germany AIRCRAFT BOARDING AS PART OF AN EFFICIENT 4D TRAJECTORY |
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ICAS2018_0634: M. Hickson¹, C. Bil¹; ¹RMIT University, Australia ADAPTIVE LANDING SEQUENCING USING BIPARTITE GRAPHS AND PERFECT MATCHING |
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ICAS2018_0635: L. Swadesir¹, C. Bil¹; ¹RMIT University, Australia URBAN AIR TRANSPORTATION JOURNEY TIME COMPARISON FOR MELBOURNE METROPOLITAN AREA |
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ICAS2018_0636: H. Hirabayashi¹, D. Toratani¹, A. Kohmura¹; ¹ENRI, Japan SIMULATION STUDY FOR VFR AIRCRAFT AND SMALL UNMANNED AIRCRAFT SYSTEMS (SUAS) MIXED OPERATIONS IN LOW LEVEL AIRSPACE |
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ICAS2018_0644: M. Niklaß¹, B. Lührs, Technische Universität Hamburg (TUHH), Germany; V. Grewe¹, V. Gollnick¹; ¹ Deutsches Zentrum für Luft- und Raumfahrt (DLR), Germany IMPLEMENTATION OF ECO-EFFICIENT PROCEDURES TO MITIGATE THE CLIMATE IMPACT OF NON-CO2 EFFECTS |
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ICAS2018_0671: F. Jiménez Serrano, Qatar DECISION-MAKING INFORMATION SYSTEM FOR MULTIMODAL DISRUPTION MANAGEMENT: SYSTEM ARCHITECTURE AND CONCEPT OF OPERATIONS |
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ICAS2018_0694: Y. Lim¹, N. Premlal¹, A. Gardi¹, R. Sabatini¹; ¹RMIT University, Australia EULERIAN OPTIMAL CONTROL FORMULATION FOR DYNAMIC MORPHING OF AIRSPACE SECTORS |
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ICAS2018_0717: S. Bagassi¹, F. De Crescenzio ¹, S. Piastra¹; ¹University of Bologna, Italy THE USE OF SYNTHETIC VISION TOOLS IN THE CONTROL TOWER ENVIRONMENT: THE RETINA CONCEPT |
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ICAS2018_0755: M. Swaid¹, T. Marks², B. Lührs¹, V. Gollnick²; ¹Hamburg University of Technology, Germany; ²German Aerospace Center, Germany QUANTIFICATION OF FORMATION FLIGHT BENEFITS UNDER CONSIDERATION OF UNCERTAINTIES ON FUEL PLANNING |
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ICAS2018_0763: C.G. Schuetz¹, B. Neumayr¹, M. Schrefl¹, E. Gringinger, Frequentis AG, Austria; S. Wilson, EUROCONTROL, Belgium; ¹Johannes Kepler University Linz, Austria SEMANTICS-BASED SUMMARIZATION OF ATM DATA TO MANAGE INFORMATION OVERLOAD IN PILOT BRIEFINGS |
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ICAS2018_0782: B. Grüter¹, J. Diepolder¹, P. Piprek¹, T. Akman¹, F. Holzapfel¹; ¹Technical University of Munich, Germany NONLINEAR MODEL PREDICTIVE CONTROL FOR OPTIMAL AIRCRAFT SEQUENCING |
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ICAS2018_0810: S.L. Mourão¹, K.A. Oliveira¹; ¹University Center UNA, Brazil THE PRIVATE MANAGEMENT OF BRAZILIAN AIRPORTS - A SHORT ANALYSIS |
10 - Safety and Security |
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ICAS2018_0043: L. Höhndorf¹, C. Wang¹, P. Koppitz¹, S. Weiß¹, S. Olmos, Evelop Airlines, Spain; C. Czado, Technical University of Munich, Mathematical Statistics, Germany; F. Holzapfel¹; ¹Technical University of Munich, Flight System Dynamics, Germany INTEGRATION OF VINE COPULA DEPENDENCE STRUCTURES INTO SUBSET SIMULATION FOR ACCIDENT PROBABILITY QUANTIFICATIONS |
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ICAS2018_0072: F. Wang¹, S.-J. Qi¹, X.-L. Wu¹; ¹Chinese Flight Test Establishment, China HUMAN FACTOR IN UNMANNED AIRCRAFT SYSTEM FLIGHT TEST |
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ICAS2018_0121: H. Inokuchi¹, T. Akiyama¹, K. Sasaki¹; ¹Japan Aerospace Exploration Agency, Japan FLIGHT DEMONSTRATION OF A LONG RANGE ONBOARD DOPPLER LIDAR |
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ICAS2018_0193: P. Le Blaye¹, C. Le Tallec¹; ¹ONERA - The French aerospace lab, France LOW LEVEL TRAFFIC MONITORING: RPAS CONCEPT OF OPERATION AND DEVELOPEMENT OF A GROUND BASED SYSTEM |
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ICAS2018_0202: D.B. Ferrari¹, R. Giarola¹, L.C.de C. Santos, EMBRAER, Brazil; ¹Instituto Tecnológico de Aeronáutica, Brazil PROBABILISTIC FORECASTING IN AIRCRAFT EMERGENCY EVACUATION SIMULATION |
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ICAS2018_0220: J.O. Entzinger¹, T. Uemura¹, S. Suzuki¹; ¹The University of Tokyo, Japan INDIVIDUALIZING FLIGHT SKILL TRAINING USING SIMULATOR DATA ANALYSIS AND BIOFEEDBACK |
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ICAS2018_0232: C. Wang¹, F. Holzapfel¹; ¹Technical University of Munich, Germany EVALUATION OF AIRCRAFT BRAKING PERFORMANCE BASED ON OPERATIONAL FLIGHT DATA |
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ICAS2018_0249: R. Geister¹, J.-P. Buch¹, D. Niedermeier¹, G. Gamba², L. Canzian², O. Pozzobon²; ¹German Aerospace Center, Germany; ²Qascom S.r.l., Italy IMPACT STUDY ON CYBER THREATS TO GNSS AND FMS SYSTEMS |
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ICAS2018_0269: C. Reiser¹, A. Bayma¹, D.A. Fonseca¹; ¹Embraer S/A, Brazil HUMAN RELIABILITY ANALYSIS IN AN AIRCRAFT DECOMPRESSION EVENT |
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ICAS2018_0284: N. Matayoshi¹, T. Iijima¹, E. Yoshikawa¹, J.O. Entzinger², T. Uemura², T. Akiyama¹, H. Inokuchi¹; ¹JAXA, Japan; ²Univ. of Tokyo, Japan DEVELOPMENT AND FLIGHT DEMONSTRATION OF A NEW LIDAR-BASED ONBOARD TURBULENCE INFORMATION SYSTEM |
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ICAS2018_0305: J. Alfredson, Saab, Sweden; B.J.E. Johansson¹, L.G. Trabasso, ITA, Brazil; J. Schminder¹, R. Granlund, RISE, Sweden; R. Gårdhagen¹; ¹Linköping University, Sweden DESIGN OF A DISTRIBUTED HUMAN FACTORS LABORATORY FOR FUTURE AIR SYSTEMS |
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ICAS2018_0309: G.C. Rocha, Konatus, Brazil; J. Alfredson, Saab, Sweden; L.G. Trabasso¹, A.N. Almeida¹, A.C. Matheus¹, D.H. Arjoni¹, M.A.R. Diaz¹; ¹ITA, Brazil A ROADMAP FOR ASSESSING HUMAN FACTORS INFLUENCE ON PILOT PERFORMANCE BASED ON SIMULATED FLIGHTS |
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ICAS2018_0314: P. Koppitz¹, J. Kuerten¹, F. Holzapfel¹; ¹Technical University of Munich - Flight System Dynamics, Germany THRUST MODELS BASED ON OPERATIONAL FLIGHT DATA USED IN PARAMETER ESTIMATION FOR SAFETY ANALYSES |
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ICAS2018_0320: K. Chen¹, Y. Wu¹, T. Zou¹; ¹Laboratory of Civil Aircraft Airworthiness Technology, CAUC, China STUDY ON AIRCRAFT EVACUATION MODELING AND MODEL PARAMETERS BASED ON SOCIAL FORCE |
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ICAS2018_0366: C.A. Niermann, German Aerospace Center (DLR), Germany 3D AUDIO SUPPORT FOR HELICOPTER PILOTS DURING CONFINED AREA LANDINGS |
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ICAS2018_0378: P.M. Razaboni, Embraer SA, Brazil UNIVERSAL DESIGN FOR AIRCRAFT SAFETY |
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ICAS2018_0380: P.M. Razaboni, Embraer SA, Brazil CREW TRAINING USING ANIMATION |
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ICAS2018_0419: Y. Lim¹, K. Ranasinghe¹, A. Gardi¹, N. Ezer, Northrop Grumman Corporation, United States; R. Sabatini¹; ¹RMIT University, Australia HUMAN-MACHINE INTERFACES AND INTERACTIONS FOR MULTI UAS OPERATIONS |
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ICAS2018_0483: T. Standfuss, DLR German Aerospace Center, Germany; F. Fichert, University of Applied Sciences, Germany; M. Whittome, DFS, Germany ADAPTING CAPACITY OF AIR NAVIGATION SERVICE PROVISION IN EUROPE - BETWEEN SCYLLA AND CHARYBDIS |
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ICAS2018_0698: 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 LOAD MONITORING FOR OPERATORS’ LOAD MANAGEMENT |
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ICAS2018_0722: M. Felux, DLR, Germany; J. Lee, KAIST, South Korea; F. Holzapfel, TUM, Germany FLIGHT TECHNICAL ERROR EVALUATIONS FOR GBAS NAVIGATION REQUIREMENT DEFINITION |
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ICAS2018_0751: J.M. Ernst, DLR, Germany 3D PERSPECTIVE VIEWS ON IMMERSIVE HEAD-WORN DISPLAYS - CAN EXOCENTRIC VIEWS INCREASE PILOT SITUATIONAL AWARENESS? |
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ICAS2018_0849: I. Romani de Oliveira¹, J.D. Musiak¹, G.C. Balvedi¹; ¹Boeing Research & Technology, Brazil A METHOD FOR ESTIMATING THE PROBABILITY OF RARE ACCIDENTS IN COMPLEX SYSTEMS |
11 - Operations and Sustainment |
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ICAS2018_0055: G. Lu¹, T.X. Wu¹; ¹Chengdu Aircraft Design & Institute, China THE TECHNIQUE AND MODELLING FOR EQUIPMENT MAINTAINABILITY QUANTIFICATION IN 3D DIGITAL AIRCRAFT DESIGN CONDITION |
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ICAS2018_0109: D. Roach¹, T. Rice¹; ¹Sandia National Laboratories, United States ADDRESSING TECHNICAL AND REGULATORY REQUIREMENTS TO DEPLOY STRUCTURAL HEALTH MONITORING SYSTEMS ON COMMERCIAL AIRCRAFT |
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ICAS2018_0164: 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 PARAMETRIC APPROACH TO OPERATING COSTS ESTIMATION FOR AN INNOVATIVE REGIONAL AIRCRAFT |
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ICAS2018_0184: D. Philpott¹, K. Hackett¹, A. Shires², B. Hinchliffe²; ¹IHS Markit (ESDU), United Kingdom; ²University of Leeds, United Kingdom FUEL-BURN PENALTIES CAUSED BY IRREGULARITIES IN AIRCRAFT SURFACES (ASTEROID PROJECT) |
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ICAS2018_0307: R.B. Parra¹, J. Laguardia¹; ¹FUMEC University, Brazil ERRORS FROM ENGINEERING IN FLIGHT SAFETY |
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ICAS2018_0336: R.B. Parra, Fumec University , Brazil; J.C. Almeida Jr, Fumec University, Brazil PREDICTIVE & DETECTIVE MAINTENANCE: EFFECTIVE TOOLS IN THE MANAGEMENT OF AERONAUTICAL PRODUCTS |
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ICAS2018_0354: 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 SHM QUALIFICATION PROCESS AND THE FUTURE OF AIRCRAFT MAINTENANCE |
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ICAS2018_0355: A.K.F. Tamba¹, L.C. Vieira¹, G.O.C Prado¹, F. Dotta¹, R.P. Rulli¹, P.A. da Silva¹, R.R. Cunha¹, J.P. da Costa¹; ¹Embraer S.A., Brazil CORROSION DETECTION IN AERONAUTICAL STRUCTURES USING LAMB WAVES SYSTEM FOR SHM |
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ICAS2018_0357: G.O.C. Prado¹, P.A. Silva¹, F.M. Simomura¹, K.L.O. Pereira¹; ¹Embraer S.A., Brazil SHM WITH AUGMENTED REALITY FOR AIRCRAFT MAINTENANCE |
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ICAS2018_0471: L. Echer¹, C.E. de Souza, Federal University of Santa Maria, Brazil; R.J. Marczak¹; ¹Federal University of Rio Grande do Sul, Brazil OPTIMAL SHAPE OF REPAIR PATCHES IN COMPOSITES |
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ICAS2018_0619: T. Marks¹, M. Swaid², B. Lührs², V. Gollnick¹; ¹German Aerospace Center, Germany; ²Technical University Hamburg, Germany IDENTIFICATION OF OPTIMAL RENDEZVOUS AND SEPARATION AREAS FOR FORMATION FLIGHT UNDER CONSIDERATION OF WIND |
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ICAS2018_0664: L.B. Koslosky¹, N. Fisk, Boeing, United States; P. Krus, Linköping University, Sweden; L. Pereira¹; ¹Universidade Federal do ABC, Brazil AIRLINE MAINTENANCE: A PROPOSAL ENVISIONING DIGITAL TRANSFORMATION |
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ICAS2018_0708: B. Lührs, TUHH, Germany; M. Niklaß¹, C. Frömming¹, V. Grewe¹, V. Gollnick¹; ¹DLR, Germany COST-BENEFIT ASSESSMENT OF CLIMATE AND WEATHER OPTIMIZED TRAJECTORIES FOR DIFFERENT NORTH ATLANTIC WEATHER PATTERNS |
12 - Host nation |
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ICAS2018_0089: M. Pazini Brandão, Technological Institute of Aeronautics, Brazil THE SANTOS-DUMONT LEGACY TO AERONAUTICS |
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ICAS2018_0301: R.B. Parra, FUMEC University, Brazil LEONARDO DA VINCI INTERDISCIPLINARITY |
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ICAS2018_0601: F.M. Catalano, University of São Paulo -EESC-USP, Brazil BRAZILIAN AVIATION HISTORY: THE UNIVERSITY OF SÃO PAULO CASE |
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ICAS2018_0848: M. Tskhovrebov¹, V. Solonin¹, V. Palkin¹, P. Kadjardouzov¹; ¹CIAM, Russia THE STUDY OF TURBORAMJETS IN CIAM |
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ICAS2018_0871: E. Bauzer Medeiros, Brazil HISTORY OF AVIATION IN MINAS GERAIS |
14 - ECSC |
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ICAS2018_0858: T. Tsuchiya, The University of Tokyo, Japan ALL JAPAN STUDENT'S INDOOR FLYING ROBOT CONTEST |
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ICAS2018_0859: J.S. Monk, CSIR, South Africa THE AERONAUTICAL SOCIETY OF SOUTH AFRICA AEROSPACE CHALLENGE |