本文从化学非平衡粘性激波层控制方程出发，用数值法计算了高超音速钝体绕流头部区流场(包括驻点线和音速线)。
In this paper, the nonequilibrium viscous shock layer equations have been used to calculate the hypersonic flows over blunt bodies in the fore-body region (including stagnation line and sonic line).
在热化学非平衡流情况下，经典的粘性相互作用参数和经验公式具有局限性。
The classical viscous interaction parameter and experiential formulae are limitative in thermochemical nonequilibrium flow.
在热化学非平衡流情况下，经典的粘性相互作用参数和经验公式具有局限性。
The classical viscous interaction parameter and experiential formulae are limitative in thermochemical nonequilibrium flow.
应用推荐