| 1. | On improving cooling effectiveness of lamilloy with infrared technique
技术的当地流活塞理论 |
| 2. | Investigation of the cooling effectiveness of lamilloy
几何参数对层板冷却性能影响的数值模拟研究 |
| 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. | Numerical investigation on improvement of film cooling effectiveness using delta - shaped tabs
尾迹对气膜冷却影响的三维非定常数值模拟 |
| 6. | 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 |
| 7. | Numerical simulation of the impact of leading - edge gas - film pores on cooling effectiveness in turbine stator blades
前缘气膜孔对涡轮静叶冷却效果影响的数值模拟 |
| 8. | The effects of blow ratio and rows on film cooling effectiveness and heat transfer coefficient was studied
研究了吹风比、孔排等因素对气膜冷却效果和换热系数的影响。 |
| 9. | The experimental results showed that the film cooling effectiveness were mainly determined by blowing ratios
该实验结果对涡轮叶片型面气膜冷却的实际工程设计研究有重要意义。 |
| 10. | The computational results show that to a certain extent the denser of the distribution of the holes , the higher of the cooling effectiveness
计算结果显示：在一定的范围内，孔阵排列的疏密度越大，冷却效果越好。 |
