| 1. | It was found that the introduce of tip clearance deteriorate the overall performance of the compressor rotor
数值结果表明叶顶间隙的引入恶化了压气机转子的性能。 |
| 2. | The influence of tip clearance on overall performance and detailed flow structure in tip region of an axial compressor rotor was investigated
研究了顶部间隙对压气机转子总性能及内部流场的影响。 |
| 3. | The flow field in the rotor tip of a compressor was numerical analyzed using the calculation method , the result compare well with experimental data
对某压气机转子项部间隙内的流动进行了详细的数值模拟，计算结果与试验结果吻合良好。 |
| 4. | Abstract : a 3d numerical solution of transonic turbulent flowfield inside a compressor rotor is analyzed with a consideration of blade tip clearance
文摘:借助于考虑叶片顶部间隙的压气机转子内跨音速湍流流场的三维数值解，得到了该转子流场中的复杂涡系与波系结构。 |
| 5. | On the basis of above work , by using of " thin blade approximation " , a 3d viscous code had been developed to calculate flow field in rotor with tip clearance
在以上工作的基础上，采用“薄叶片”假设，发展了一种用于计算考虑顶部间隙的压气机转子内部流场的三维粘性程序。 |
| 6. | The effects of layout of tip gap clearance on axial compressor rotor performance and stability have been investigated experimentally . a single - stage compressor rotor with no inlet guide vanes was tested under subsonic condition
本文用实验的方法对压气机转子尖部间隙沿轴向周向的布局进行了详细的研究。 |
| 7. | 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。 |
| 8. | The effect of leakage flow due to the upstream hub axial gap on the rotor performance and the mechanism of interaction between the hub leakage flow and the rotor blade passage flow were studied based on the numerical simulations of the flow fields of a transonic compressor rotor with upstream hub leakage
摘要为研究压气机转子上游叶根轴向间隙泄漏流对转子性能的影响程度以及泄漏流与转子流场之间的相互作用机制，对带有叶根泄漏流的跨声压气机转子流场进行了数值模拟。 |
