Effect of the apex flap on the leading edge vortex breakdownover a 70° delta wing;
尖顶襟翼对70°三角翼前缘涡破裂的影响
Experimental studies on the aerodynamic characteristics of a 70-degree delta wing with apex flap;
尖顶襟翼对70°三角翼气动力影响的实验研究
The effectiveness of the apex flaps to control the vortex breakdown on a 70° sweep angle delta wings was studied experimentally.
为了抑制三角翼前缘涡破裂的发生 ,研究了大攻角下 ( 30°～ 5 0°)尖顶襟翼对 70°三角翼前缘涡破裂的影响 。