本文给出了压气机叶栅出口截面的损失分布和气流角沿叶高的变化。
The loss distribution and the span-wise variations of flow angle at the outlet section of a linear compressor cascade are presented in this paper.
通过数值模拟，分析了叶片周向弯曲对大折转角压气机叶栅内分离结构的影响。
A numerical simulation was performed to analyze the effect of bowed blades on the separation structures in a high-turning compressor cascade.
对压气机叶栅中采用弯曲叶片后，叶栅气动特性与叶栅稠度的关系进行了实验研究。
The relationship between solidity and the characteristics of compressor cascades with curved blades is investigated.
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