低アスペクト比翼の後流の可視化(工学部:機械工学科)
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概要
- 論文の詳細を見る
Flow visualization test of wake patterns behind clipped double delta wings was conducted in AIT low speed wind tunnel. Vortices from wing leading edges and tip, which determine the low speed aerodynamic characteristics of the wing, are clearly observed by the LED method of sensing total pressure in the wake.
- 愛知工業大学の論文
- 2004-03-31