The experimental studies on two wing body junctions and wakes were carried out in a lowturbulence level windtunnel.
绕两个翼型-平面的角区流动及其尾迹的实验是在低湍流度风洞中完成的。
2
The starting process of windtunnel, involving turbulence, shock wave, low subsonic and high supersonic mixing flows, is a very complex transient process.