axial compressor cascade 轴流压气机叶栅
annular compressor cascade 环型扩压叶栅
aspirated compressor cascade 吸附式压气机叶栅
compressor cascade experiment 压气机叶栅实验
oscillating compressor cascade 压气机振荡叶栅
an annular compressor cascade 环形压气机叶栅
Highly-loaded compressor cascade 高负荷扩压叶栅
Under off-design conditions, the mechanism which slot-jet improved boundary layer flow is similar to that under design condition. And the operating range with low loss level is widened in the highly-loaded compressor cascade.
非设计冲角条件下,缝隙射流改善附面层分离流动的机理与设计冲角下类似,有效地增加了高负荷扩压叶栅的低损失冲角范围。
参考来源 - 采用缝隙射流技术的弯曲扩压叶栅气动性能研究·2,447,543篇论文数据，部分数据来源于NoteExpress
An experimental investigation of end wall flow control for pit-array cascade plate in a compressor cascade wind tunnel has been completed.
本文介绍在平面叶栅风洞上进行的“孔窝群”端壁叶栅和原始(光滑)端壁叶栅对比试验研究结果。
A numerical simulation was performed to analyze the effect of bowed blades on the separation structures in a high-turning compressor cascade.
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。
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.
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。
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