Aerodynamic Design of Wing in Ground Effect Vehicle for High Flight Stability

DOI
  • Azuma Daisuke
    Kurume Institute of Technology, Intelligent Mobility Laboratory
  • Yamashita Ryota
    Kurume Institute of Technology, Department of Automotive System Engineering
  • Akashi Nobuyuki
    Kurume Institute of Technology, Department of Automotive System Engineering

Bibliographic Information

Other Title
  • 飛行安定性に優れる地面効果翼機の空力デザイン

Description

In recent years, ground effect vehicles are focused again for solving environmental problems and high-speed maritime transportation. Therefore, we have been researching the design of the small air vehicle with high Lift-Drag ratio in ground effect. In this paper, the effects of the wing section shape and dihedral angle on the aerodynamic performance of the ground effect vehicle are discussed. In addition, the effect of the position of the center of gravity on the pitching stability is discussed.

Journal

Keywords

Details 詳細情報について

  • CRID
    1390282680586028160
  • NII Article ID
    130006966517
  • DOI
    10.11247/jssd.64.0_164
  • Text Lang
    ja
  • Data Source
    • JaLC
    • CiNii Articles
  • Abstract License Flag
    Disallowed

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