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机译:大涡模拟和压敏涂料技术研究变长径比简单复角孔的流动结构和绝热膜效果
Gas Turbine Institute, Department of Thermal Engineering, Tsinghua University, Beijing, China;
Gas Turbine Institute, Department of Thermal Engineering, Tsinghua University, Beijing, China;
Gas Turbine Institute, Department of Thermal Engineering, Tsinghua University, Beijing, China;
Gas Turbine Institute, Department of Thermal Engineering, Tsinghua University, Beijing, China;
Gas Turbine Institute, Department of Thermal Engineering, Tsinghua University, Beijing, China;
机译:高分辨率薄膜冷却性能的高分辨率测量,具有不同孔长度到直径比的简单和复合角圆柱孔 - 第一部分:绝热膜效果
机译:具有孔长度与直径比和内部横流定向效应的复合角孔膜冷却大型涡流模拟
机译:使用压敏涂料技术从两排复合角圆柱孔中冷却薄膜的效果
机译:变径长径比的轴向和复合角孔的大涡模拟
机译:一种使用压敏涂料技术引入新薄膜孔几何的实验膜冷却效果
机译:单排和两排交错的薄膜冷却孔的传热,绝热效果和喷射剂分布的下游,角度简单且复合