The internal flow fields in scramjet are very complex, due to the interaction of shock waves, expansion waves, boundary layer and strong reactions.
超燃冲压发动机的内部流场很复杂，存在激波、膨胀波、附面层和剧烈的化学反应等相互作用，给数值模拟带来很大的困难。
The numerical result shows clearly the propagations, diffraction, reflection and interaction with each other of shock waves.
计算结果清楚地给出了激波传播、绕射、反射、及相互干扰的复杂流场结构。
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