机译:新型异形孔增强薄膜冷却性能的数值评估
Institute of Turbomachinery, School of Energy and Power Engineering, Xi'an Jiaotong University, Xi'an, Shaanxi 710049, China;
Institute of Turbomachinery, School of Energy and Power Engineering, Xi'an Jiaotong University, Xi'an, Shaanxi 710049, China;
Institute of Turbomachinery, School of Energy and Power Engineering, Xi'an Jiaotong University, Xi'an, Shaanxi 710049, China;
gas turbine endwall; novel film cooling hole; numerical simulation; film cooling effectiveness; heat transfer coefficients; discharge coefficients;
机译:具有圆孔影响的圆形出口形孔冷却性能的数值评估
机译:用形状唇形横挖孔膜冷却性能的数值评价
机译:使用复合角注入的异型薄膜冷却孔增强薄膜冷却性能
机译:Laidbach扇形孔中薄膜冷却性能对表面粗糙度影响的数值评价
机译:孔粗糙度和高自由流湍流对成形孔的薄膜冷却影响
机译:CuO /水纳米流体对半导体冷却性能的数值评估
机译:平板表面上圆柱形孔膜冷却几何孔孔薄膜冷却效果的实验研究
机译:薄膜冷却的轮廓孔:肾形涡旋的影响