旋翼迎角
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rotor disk angle of attack 桨盘迎角
rotor angle of attack
以上为机器翻译结果,长、整句建议使用 人工翻译 。
Rotor wake effects are modeled in the form of a correction applied to the angle of attack along the blades. This correction is obtained by computing the local induced downwash with free wake analysis.
旋翼尾流的作用通过自由尾流分析来求解局部的诱导下洗速度以修正翼型攻角。
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