An engineering method for calculating transient surface heat flux and surface temperature of hypersonic vehicle is described in this paper,including stagnation point and out of stagnation point.

• 采用工程算法,包括驻点和非驻点的瞬态表面热流和温度的计算以及完全气体和平衡气体条件下边界层外缘参数的计算。