当机台上方的热通量越大,其产生的涡漩区范围和回流速度越大。
The designed maneuver reentry trajectory can meet the demands of attitude, heat flux and velocity for the warhead.所设计的再入机动弹道能满足机动弹头对姿态、热流和速度的要求。
The simulation of Space heat flux is a very complicated and important problem in ground thermal testing of spacecraft.在航天器地面热试验中,空间热流的模拟是一个非常复杂而重要的问题。