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临界马赫数

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机翼穿音速时的流场状态,描述了在临界马赫数附近时的流场变化

飞机飞行时,随著飞行速度增大来到临界马赫数时,上翼面压力最低处的速度恰等于此点上的音速。 或者说,当飞行与某马赫数时,机翼表面(通常是上表面)上流速最大处流速达到音速,此时飞机马赫数即为临界马赫数。

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临界马赫数
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