1.
There were better benefits through cooling by slot and wiggle-strip film cooling.
其中缝隙式气膜冷却和波纹板式气膜冷却冷却结构的冷却效果比较好。
2.
Numerical Study on Cooling Deterioration Area Between the Film Cooling Holes of Rotating Blades
旋转叶片气膜冷却孔间冷却死区的数值研究
3.
EFFECT OF CONJUGATE HEAT TRANSFER AND INTERNAL COOLANT FLOW ON FILM COOLING
耦合传热和冷却流通道流动对气膜冷却的影响
4.
Influence of Air-film Hole Shapes on Turbine Blade Air-film Cooling Effectiveness
气膜孔形状对涡轮叶片气膜冷却效果的影响
5.
Numerical Simulation of Characteristics of Flow and Heat Transfer of Film-Cooling;
气膜冷却流动与传热特性的数值模拟
6.
FLUID-THERMAL COUPLING SIMULATION OF FLAT PLATE FILM-COOLING AT HIGH TEMPERATURES
高温平板气膜冷却流热耦合数值模拟
7.
Numerical Simulation in Lengthways Coupled-vortex of Multiple Holes
多孔气膜冷却纵向耦合涡的数值模拟
8.
Numerical simulation of effusion holes on the longitudinal ripple heat shield
发散孔纵向波纹隔热屏气膜冷却特性
9.
The Effect of Internal Cooling Channel on the Heat Transfer of Outer Surface Film Cooling
内冷通道特性对外表面气膜冷却换热影响研究
10.
TLC technique can be successfully applied to reflect film cooling effectual area and cooling effect.
利用液晶测温技术可以很好地反映气膜冷却区域及冷却效果等。
11.
Recent Advances in the Study of Influence of Air-film Hole Geometrical Structures on Turbine Blade Air-film Cooling
气膜孔几何结构对涡轮叶片气膜冷却影响的研究进展
12.
DETACHED EDDY SIMULATION OF CYLINDRICAL HOLE FILM COOLING
应用分离涡模型计算斜圆柱孔气膜冷却
13.
Influence of Various Pin Fin Configurations on Trailing Edge Film Cooling;
不同结构扰流柱对叶片尾缘气膜冷却的影响
14.
Heat Transfer Investigation of Film Cooling on the Leading Edge of Turbine Blade;
涡轮叶片前缘气膜冷却的传热实验研究
15.
Investigation of Trailing Edge Film Cooling by Jets Ejected from a Slot;
涡轮叶片尾缘半劈缝气膜冷却实验研究
16.
Research on the Heat Transfer of the Endwall Film-cooling in Axial Flow Turbine Cascade;
轴流涡轮叶栅端壁气膜冷却的传热研究
17.
Film cooling characteristics of converging-expanding hole with equal exit-entry area
出/入口面积相等的收缩-扩张孔气膜冷却特性
18.
Heat Transfer Measurements on a Rotating Film Cooling Model
旋转状态下气膜冷却换热特性的实验研究