Effects of Surface Geometry and Blowing Ratio on Film Cooling Performance at Airfoil Trailing Edge Investigated by Using Large Eddy Simulation
Effects of Surface Geometry and Blowing Ratio on Film Cooling Performance at Airfoil Trailing Edge Investigated by Using Large Eddy Simulation
复制标题
大涡模拟研究表面几何形状和吹气比对翼型后缘气膜冷却性能的影响
DOI：
10.1615/ihtc15.gtb.008914
复制
发表时间：
2014
期刊：
影响因子：
--
通讯作者：
K.
中科院分区：
文献类型：
--
作者：
Murata;A.;Mori;E.;and Iwamoto;K.
