222 地面効果翼の空力特性実験 : 第二報,VG設置性能(S38-1 小型飛翔体(1),S38 生物飛行と小型飛翔体)
詳細
In order to improve the lift capability of the wing-in-ground effect craft, the experimental aerodynamic performances were conducted for the ground effect wings through setting the vortex generators. Its performances have been evaluated the higher lift enhancement by controlling the stall at the higher angles of attack even if falling behind at the lower them.
