Aerodynamic Improvement of Flap Performance Using Delta-shaped Vortex Generator

著录项

• 来源
  《Third Asia-Pacific International Symposium on Aerospace Technology》|2011年|1-7|共7页
• 会议地点 Melbourne(AU)
• 作者

  Dongyoun Kwak; Zhong Lei; Masayoshi Noguchi;

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• 作者单位

  Aviation Program Group, Japan Aerospace Exploration Agency, Mitaka, Tokyo, 181-0015, Japan;

  Department of Mechanical Systems Engineering, Tokyo University of Science, Suwa, Nagano, 391-0292, Japan;

  Aviation Program Group, Japan Aerospace Exploration Agency, Mitaka, Tokyo, 181-0015, Japan;

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• 会议组织
• 原文格式 PDF
• 正文语种 eng
• 中图分类 航空;航天（宇宙航行）;
• 关键词

  Trailing edge flap; Vortex generator; Flow separation; Flow control;

  机译：后缘襟翼;涡流发生器;流量分离;流量控制;