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).

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)。

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But Beachy theorized it is needed to make repairs in parts of the body that undergo constant regeneration, as in chronic acid reflux, where Sonic hedgehog works overtime to reline the throat.

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