According to the boundary layer character in reentry wake of hypersonic blunt cone body, this paper presents a local similar solution for hypersonicwake.
依据钝锥体再入远尾迹流动的边界层特征，从边界层方程出发得到了高超声速远尾迹流动的拟相似性解。
2
In this paper, plasma wake flow of hypersonic reentry vehicle and radar scattering characteristics have been studied.