Aircraft design papers presented at the AIAA Aviation Forum 2020 : online, 15-19 June 2020

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Bibliographische Detailangaben
Körperschaften: AIAA Aviation Forum (VerfasserIn), American Institute of Aeronautics and Astronautics (VeranstalterIn)
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Sprache:eng
Veröffentlicht: Red Hook, NY Curran Associates, Inc. 2020
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Titel Jahr Verfasser
DESIGN CASE OF THE E-19 AEOLUS SUPERSONIC BUSINESS JET 2020 Smith, Howard
DESIGN TOOLS FOR CONCEPTUAL ANALYSIS OF FUTURE COMMERCIAL SUPERSONIC AIRCRAFT 2020 Hassan, Mohammed
AIRCRAFT CONCEPTUAL DESIGN OF COMMUTER AIRCRAFT INCLUDING DISTRIBUTED ELECTRIC PROPULSION 2020 Orefice, Francesco
FLIGHT-STATES AND CONTROL INPUTS COMPUTATION USING NONLINEAR PROGRAMMING FOR UNMANNED AIR VEHICLE 2020 Salahudden, Qazi M.
DIFFERENTIAL DYNAMIC PROGRAMMING TO CRITICAL-ENGINE-INOPERATIVE TAKEOFF CERTIFICATION ANALYSIS 2020 Xie, Jiacheng
AN APPROACH FOR FAN STAGE CONCEPTUAL DESIGN WITH NON-AXISYMMETRIC STATORS IN PRESENCE OF DISTORTION 2020 Pokhrel, Manish
CONCEPTUAL DESIGN TOOL TO SUPPORT HIGH-SPEED VEHICLE DESIGN 2020 Ferretto, Davide
MAINSTREAM FLOW PREDICTION FOR THE THERMAL RISK ASSESSMENT OF AIRCRAFT SYSTEMS IN CONCEPTUAL DESIGN 2020 Sanchez, Florian
THE IMPACT OF A NEW MID-RANGE AIRCRAFT WITH ADVANCED TECHNOLOGIES ON AIR TRAFFIC EMISSIONS AND CLIMATE 2020 Linke, Florian
STRUCTURAL WEIGHT PREDICTION FOR AN URBAN AIR MOBILITY CONCEPT 2020 Winter, Tyler F.
SIMULATED SCALABILITY OF DISCRETE LATTICE MATERIALS SUBSTRUCTURES TO COMMERCIAL SCALE AIRCRAFT 2020 Cramer, Nick B.
CRACK PROPAGATION IN AN ALUMINUM PLATE BONDED TO A GLARE PANEL: CASE STUDY 2020 Silva, Guilherme V.
HYDROGEN POWERED LONG HAUL AIRCRAFT WITH MINIMIZED CLIMATE IMPACT 2020 Troeltsch, Florian M.
AEROELASTIC ANALYSIS AND CHARACTERIZA TION OF THREE-DEGREE-OF-FREEDOM SYSTEMS WITH DISCONTINUOUS NONLINEARITY 2020 Vasconcellos, Rui
PERFORMANCE AND COST ADVANTAGES OF AIRCRAFT COMPRISED OF MISSION- OPTIMIZED AEROSHELLS ON UNIVERSAL FUSELAGE CORES 2020 Brandt, Steve A.
THE AIR-VEHICLE AS A COMPLEX SYSTEM OF AIR TRANSPORT ENERGY SYSTEMS 2020 Silberhorn, Daniel
CONTINUED DESIGN AND DEVELOPMENT OF A TORNADO INTERCEPT UNMANNED AERIAL VEHICLE 2020 Ross, Andrew L.
CONFIGURATION-INDEPENDENT INITIAL SIZING METHOD FOR UAM/EVTOL VEHICLE 2020 Hascaryo, Rodra W.
TAIL SIZING CONSIDERATIONS FOR WINGTIP PROPULSOR DRIVEN AIRCRAFT APPLIED TO THE PARALLEL ELECTRIC-GAS ARCHITECTURE WITH SYNERGISTIC UTILIZATION SCHEME (PEGASUS) CONCEPT 2020 Blaesser, Nathaniel J.
MINIMIZING INDUCED DRAG OF RECTANGULAR, ADDITIVELY MANUFACTURED 2020 Valenti, Justin D.
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