Abstract: The traditional BPM semi-empirical prediction airfoil turbulent boundary layer trailing edge noise was improved.

摘要：改进了传统的翼型湍流边界层尾缘噪声bpm半经验预测公式。

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Abstract: The traditional BPM semi-empirical prediction airfoil turbulent boundary layer trailing edge noise was improved.

摘要：改进了传统的翼型湍流边界层尾缘噪声bpm半经验预测公式。

youdao