| 1. | Experimental study of small perturbation induced rotating stall in axial flow compressor
轴流压气机小扰动诱发旋转失速的试验研究 |
| 2. | Experimental and numerical investigation of stepped tip gap effects on an axial - flow compressor
梯状间隙结构对轴流压气机影响的试验与数值模拟 |
| 3. | Analysis on the aerodynamic behaviors of the swept leading edge shocks in high load axial compressors
轴流压气机掠形前缘激波动力学效应的模型分析 |
| 4. | Experimental research of an axial flow compressor performance with stepped tip gap casing configuration
梯状尖部间隙机匣处理对轴流压气机性能影响的实验研究 |
| 5. | The effect of tip injection on the performance of an axial - flow compressor was performed numerically
采用数值模拟方法研究了顶部喷气对某轴流压气机气动性能的影响。 |
| 6. | Exploring mechanism of stall margin enhancement of subsonic axial - flow compressor through steady micro tip injection
定常微量喷气提高轴流压气机稳定工作裕度机理探讨 |
| 7. | The multi - stage axial compressor performance was measured using a streamline curvature method based on two - dimension ( axisymmetric ) mathematical model
摘要采用二维（轴对称）数学模型，应用流线曲率法求解多级轴流压气机特性。 |
| 8. | By using a reynolds - averaged two - dimensional computation , the effect of upstream wake on unsteady separated flow field of downstream adjacent vanes was investigated in low - speed axial compressor
摘要利用二维数值模拟研究了低速轴流压气机上游尾迹对下游相邻叶排的非定常分离流场的影响。 |
| 9. | The unsteady surface pressures on the rotor blades of a single - stage low - speed axial compressor were measured by means of mounting micro - sensors on the surface the blades
摘要为了研究上游叶片尾迹对轴流压气机转子叶片非定常表面压力的影响，采用在叶片表面埋设微型压力传感器的方法，测量了一个单级低速轴流压气机转子叶片的非定常压力分布。 |
| 10. | By comparing the calculated results and test data for a multi - stage axial compressor , this method demonstrates that it could assist in predicting the characteristics of multistage axial compressor and spanwise parameter distribution under off design working conditions
对一台多级轴流压气机的计算结果与试验数据的对比分析表明，该方法能较好地预测多级轴流压气机的特性和非设计工况下级间参数的分布。 |
