| 1. | 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. | Influences of swept and curved blade on the flow near compressor cascade endwall
掠对压气机端壁流动的影响 |
| 3. | Investigation on ways to control unsteady seperated flow in 2d compressor cascade
二维扩压叶栅非定常分离流控制途径探索 |
| 4. | 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 |
| 5. | The 3 - d flow field is changed completely in a forward - swept compressor cascade , which makes the low energy fluid redistribute in the flow passage
叶片前掠改变了叶栅的三维压力场，使得低能流体重新分配。 |
| 6. | 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。 |
| 7. | 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。 |
