This article investigates the flow control technique of forward-swept wing blended body (FBB) taillessconfiguration by means of wind tunnel tests.
通过风洞试验研究了前掠翼融合体无尾气动布局(FBB布局)的流动控制技术。
2
The tailless delta-canard configuration is inherently aerodynamically unstable, which provides a high level of agility, particularly at supersonic speeds.
鸭式无尾翼布局具有高度机动性和优越的超音速性能，但亦具有先天空气动力上之不稳定性。
3
For improving the stealth performance, the configuration of the tailless UAV was ameliorated, and then the aerodynamics and stealth performance was analyzed.