Numerical study of the unsteady flow in a plane compressor cascade 平面压气机叶栅非定常流动的数值研究
2.
Investigation of swept and curved compressor cascade performance under different incidences 掠叶片的压气机叶栅变冲角性能研究
3.
Compressor blade row 压气机叶栅
4.
A numerical simulation was performed to analyze the effect of bowed blades on the separation structures in a high - turning compressor cascade 摘要通过数值模拟，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。
5.
Both numerical and experimental investigations were carried out to study the effect of aerodynamic sweeping - curving on the endwall flow field of compressor cascade 摘要利用数值和实验方法对气动弯掠在压气机叶栅中的作用机理进行了研究。
