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- The lengthways coupled-vortex behind the film cooling holes which is of high vorticity and low vortex heart is helpful to improve the film cooling efficiency on the area covered. 气膜孔后高涡量、低涡心位置的纵向耦合涡的形成有助于提高其覆盖区域的气膜冷却效率；
- Investigation of local heat transfer characteristics near film cooling holes about inner side of turbine blade midchord area with impingement was carried out experimentally. 摘要对叶片弦中区内部“冲击-气膜出流”冷却方式中气膜孔附近壁面的换热特性进行了实验研究。
- Numerical investigation for local heat transfer characteristics of the inner side of turbine blade near film cooling holes, whether there is impingement or no has been carried out with an RSM turbulence model. 摘要用RSM模型对有、无冲击气膜出流冷气侧气膜孔局部换热特性进行了数值研究。
- When there is impingement, the effect of flow and geometrical parameters on the local heat transfer characteristics near film cooling holes is investigated, and the mechanism of local heat transfer characteristics is obtained. 在有冲击射流时，着重研究了流动和几何参数对气膜孔局部换热特性的影响，分析了“冲击－气膜出流”局部换热特性规律。
- When there is no impingement, the investigation about flow extravasation effect form film cooling holes is carried out with different cross flow Reynolds Numbers and different density flow ratios of the film outflow to cross flow. 在无冲击射流时，通过改变来流雷诺数、气膜出流与横流密流比，对气膜孔的“溢流效应”进行了研究。
- Xiang Anding,Zhu Huiren,Liu Songling,et al.Discharge coefficient measurements for film cooling holes on blade surface in a turbine cascade[J].Journal of Propulsion Technology,2003,24(3):216-218. [6]向安定;朱惠人;刘松龄;等.;涡轮导向叶片表面气膜孔流量系数的实验研究[J]
- Effects of Film Cooling Hole Shape on Heat Transfer 气膜孔形状对排孔下游换热的影响
- Study of Turbulent Flow of Film Cooling Holes with Lateral Expanded Exits 带有横向扩展出口的气膜冷却孔的紊流流场研究
- Influence of Momentum Ratio on the Discharge Coefficient of Film Cooling Holes on Blade Surface in a Turbine Cascade 动量比对涡轮叶片气膜孔流量系数的影响
- Influence of density ratio on the discharge coefficient of turbine blade film cooling holes 密度比对涡轮叶片气膜孔流量系数的影响
- Interior local heat transfer characteristics of midchord region due to sparse film cooling holes 稀疏气膜冷气侧局部换热特性实验
- Investigation into Equivalent Stress Analysis Method for Turbine Blades with Densely Distributed Film Cooling Holes 带密布气膜冷却孔的涡轮叶片等效应力分析方法研究
- Discharge Coefficient Measurements of Film Cooling Holes on Blade Surface in a Turbine Cascade 涡轮工作叶片型面气膜孔流量系数的实验研究
- Discharge coefficient measurements for film cooling holes on blade surface in a turbine cascade 涡轮导向叶片表面气膜孔流量系数的实验研究
- The Interior Heat Transfer Characteristics of Gas Turbine Blade Due to Dense Film Cooling Holes 密集型气膜出流内部冷气侧换热特性实验研究
- The Interior Heat Transfer Characteristics of Gas Turbine Blade Due to Sparse Film Cooling Holes 稀疏型气膜出流内部冷气侧换热特性实验研究
- Heat transfer characteristics near a row of film cooling holes in interior of turbine blade 叶片内部气膜孔附近壁面局部换热特性
- Experimental Investigation of the Local Heat Transfer Characteristics at the Inner Side of the Midchord Region near Film Cooling Holes 叶片弦中区内部气膜孔局部换热特性实验
- Influence of geometrical construction of film cooling hole on discharge coefficient 气膜冷却孔几何结构对流量系数的影响
- film cooling holes 气膜冷却孔
