丸い前縁を有するボルテックス・フラップ付き50°デルタ翼に関する風洞実験
1999 年 47 巻 548 号 p. 364-366
詳細
1999 年 47 巻 548 号 p. 364-366
Low speed wind tunnel measurements were done on a 50° delta wing with rounded leading-edge vortex flaps in order to assess the benefits of the rounded leading-edge vortex flaps. Deflecting the rounded leading-edge vortex flap improves the lift/drag ratio at relatively higher lift coefficients, when compared with the sharp edged vortex flap.
