| 1. | Numerical study of vortex structure within turbine cascade with tip clearance
有间隙涡炉叶栅涡系结构的数值模拟 |
| 2. | Blade tip clearance
叶尖与船体的间隙 |
| 3. | Development of rotating linear cascade facility for simulating blade tip clearance flow
模拟叶尖间隙流的转动平面叶栅实验方案 |
| 4. | Experimental and numerical study of wall flow pattern of turbine cascade with tip clearance
有间隙涡轮叶栅壁面流谱实验与数值模拟研究 |
| 5. | 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。 |
| 6. | The stepped location and radial depth of tip clearance are crucial parameters to decide rotor stability and performance
阶梯状间隙的开槽位置及径向的间隙深度是影响转子性能和稳定性的重要参数。 |
| 7. | 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。 |
| 8. | Research findings about the tip clearance of engine in the paper are basal , they can be used as reference of control the tip clearance
本文对发动机的叶尖间隙分析做了一些基础性工作，对于叶尖间隙控制方面的研究有一定的参考价值。 |
| 9. | Research finding about the tip clearance of engine in the paper is basal ; they can be used as reference of aero - engine design and the tip clearance control
这些工作对于发动机初步设计设计和叶尖间隙控制理论研究有一定的参考价值。 |
| 10. | 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。 |
