在激波穿越磁云后，原先被高度压缩的磁云本体在其内禀磁弹性的作用下会逐渐恢复为扁圆的几何形态。
After the shock passage, the previously compressed MC body is gradually restored to an oblate morphology under the action of its inherent magnetic elasticity.
以总压恢复系数最大为目标，采用等激波强度和等激波角设计方法建立进气道模型；
The inlet design calculating model was set up based on the theory of equal shock wave intensity and angle of supersonic airflow to get maximum total pressure coefficient.
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