| 1. | Experimental study on the aerodynamic performance of swept - curved blade
弯掠叶片气动性能的实验研究 |
| 2. | Influence of throat parameters on performance of submerged inlet
喉道参数对埋入式进气道气动性能的影响 |
| 3. | A negative bowed blade increases the flow separation and the flow performance is reduced remarkably
反弯则使得叶栅内分离趋势增加，气动性能明显降低。 |
| 4. | 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。 |
| 5. | The mechnaical structure is beautiful , layout of the whole machine reasonable , operation easy and service life long
本机构简单,外形美观,电气控制可靠,气动性能良好 |
| 6. | 5 . the modification of the aerodynamic force performance on a 2d cylinder by use of microjet was numerically simulated
5 .数值模拟再现了微射流改变绕流圆柱气动性能的情形。 |
| 7. | It is found that the hub leakage flow leads to an increased flow blockage near the hub , resulting in drop of rotor performance
结果表明：叶根泄漏流可使叶根附近流动堵塞增大，造成转子气动性能的恶化。 |
| 8. | Comparisons by means of numerical simulation are made between this inlet and the normal two - dimensional ramp inlet
数值模拟结果表明，设计工况下该进气道能够获得跟常规二维斜楔式进气道大致相当的气动性能。 |
| 9. | In present dissertation , a high performance scheme is employed to simulate the complicated flow field inside centrifugal impeller passages
本文应用一种高性能的数值计算方法求解了离心叶轮内部复杂的三维流场，研究了它们的气动性能。 |
| 10. | The result shows that the pressure distribution on the cylinder and the wake are modified , and the separate flow partially is attached to the surface again
相邻微作动器存在相位差时，圆柱上下表面压力系数的差值发生改变，进而使绕流圆柱的气动性能发生变化。 |
