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A Method for Calculating the Interaction of a Bow Shock of a Re-Entry Vehicle and a Blast Wave

机译:一种计算再入飞行器的弓形冲击与爆炸波相互作用的方法

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A general technique for computing the transient flow field in the nose region of a blunt body traveling at hypersonic speeds after being intercepted head-on by a shock wave is presented. The method is not limited to the assumption that the density, pressure and velocities are constant in the interaction region which has been the assumption in previous investigations of this problem. The technique can be applied to compute the flow in the entire interaction region, but is discussed here for computing the low near the axis of symmetry. (Author)

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