The interaction between an oblique blast wave and supersonic bluntcone was discussed.
本文讨论了斜爆炸波与超音速钝锥激波层的相互作用问题。
2
This paper presents experimental results of flap heat transfer and pressure characteristics on a bluntcone in shock tunnel.
本文介绍了一种在激波风洞中取得的,装在钝锥模型上的控制翼热流及压力特性实验结果。
3
According to the boundary layer character in reentry wake of hypersonic bluntcone body, this paper presents a local similar solution for hypersonic wake.