This paper presents a numerical study on the performances of a compressor stage under different circumferential positions of the rear blades of tandem stator.
本文采用数值模拟研究串列叶栅后排静叶周向位置对压气机级性能的影响。
This paper presents a numerical study on the performances of a compressor stage under different circumferential positions of the rear blades of tandem stator.
本文采用数值模拟研究串列叶栅后排静叶周向位置对压气机级性能的影响。
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