临界迎角是液体或气流从表面开始分离,导致流体效率降低的角度。临界迎角是设计空气动力学表面时的重要考虑因素,例如飞机机翼、涡轮叶片等,因为它决定着不会导致升力或推力损失的最大攻角大小。
答案解析
相关知识点:
临界迎角定最大攻角无损失
相关题目
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