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Träfflista för sökning "WFRF:(Raymer D.) "

Sökning: WFRF:(Raymer D.)

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  • Raymer, D., et al. (författare)
  • Sparky flapjack : Electric aircraft design inspirations from the vought V-173
  • 2017
  • Ingår i: AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting. - Reston, Virginia : American Institute of Aeronautics and Astronautics Inc.. - 9781624104473
  • Konferensbidrag (refereegranskat)abstract
    • This paper presents a design study of electric personal aircraft concepts inspired by the Vought V-173, the famous “Flying Pancake” of late WWII. With its incredible slow flight and short field capability, this innovative design concept may point towards an aircraft suitable for the emerging “Pocket Airport” concept. The paper presents four modern concepts that could offer remarkable capabilities. All use electric propulsion, novel aerodynamics, and integrated composite construction. Four-seater and two-seater concepts have a separate crew cabin underneath the wing allowing for normal entry, unlike the V-173. Another two-seater version was designed with the cabin integrated with the wing root as in the V-173. A recreational one-person “mini” version was also designed with a prone pilot position on top of the wing. 
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  • Mengmeng, Zhang, 1985-, et al. (författare)
  • Enhancement of CEASIOM with Rapid-Meshing Tool for Aircraft Conceptual Design
  • 2012
  • Ingår i: Aerotecnica Missili & Spazio, The journal of Aerospace Science, Technology and Systems. - : Associazione italiana di Aeronautica e Astronautica. - 2524-6968. ; 91:3/4, s. 79-85
  • Tidskriftsartikel (refereegranskat)abstract
    • This paper details the development and application of the RDS-SUMO-CEASIOM-EDGE rapid-CFD tool. It uses theRDS CAD model as geometry for automated meshing and CFD analysis to produce an aero-data base for control andstability analysis. It is applied to two non-conventional design proposals, an asymmetric twin-prop aircraft and anairliner with rear Open Rotor propulsion, retractable canard, and a “chin-rudder” instead of vertical tail. For bothconfigurations,yaw control is problematic, and the stability and control analysis is used to assess control surface sizing and stabilityaugmentation system.
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