| 1. | Effect of geometry of back - step slots on film cooling
几何结构对后台阶缝隙气膜冷却效率的影响 |
| 2. | Numerical investigation of film cooling in an air cooled turbine stator
利用三角形突片改善气膜冷却效率的数值研究 |
| 3. | Numerical investigation of back - step three dimensional slots on film cooling effectiveness
后台阶三维缝隙冷却效率的数值模拟 |
| 4. | A new model for film cooling effectiveness computation on blade surface in a turbine cascade
涡轮叶片型面气膜冷却效率的计算模型 |
| 5. | Effect of aerodynamic parameters of backward - step three dimensional slots on film cooling effectiveness
气动参数对后台阶三维缝隙气膜冷却效率的影响 |
| 6. | The best match between cooling efficiency and power can be obtained by choosing a reasonable flow velocity
合理选择流速可以达到冷却效率与动力的最佳匹配。 |
| 7. | Results show that the influence of mainstream reynolds numbers on discharges coefficients and film effectiveness is little but on the heat transfer coefficients is obvious
实验结果表明，主流雷诺数对气膜孔流量系数和气膜孔下游冷却效率影响较小，而对气膜孔下游换热系数的影响则较明显。 |
| 8. | In the part of cooling characteristics investigation , these four laminate plates were tested in a large scale low speed close - looped wind tunnel and the cooling effectiveness were obtained
在冷却特性实验部分，在大尺寸低速回流式风洞中对上述四块层板进行了冷却特性实验，获得了其综合冷却效率。 |
| 9. | The experimental results showed that very high effectiveness can be achieved by using lamilloy and area ratio of the hole will play the most important role in determination of cooling effectiveness
实验结果表明：层板的具有很高的冷却效率；层板冷却效率主要决定于开孔率，开孔率越大，冷却效率越高。 |
| 10. | The mass flow rate coefficients increase and achieve a constant at last with increasing blowing ratio . the influence of blowing ratio on the heat transfer coefficients and film effectiveness is complex
流量系数随吹风比的增大而增大并最终趋于某个定值，但吹风比对气膜孔下游换热系数和冷却效率则较为复杂。 |
