机译:沟槽形孔对涡轮叶片前缘薄膜冷却的影响
Mechanical Engineering Department, Tabriz University, 29 Bahman Boulevard, Tabriz, Iran;
rnMechanical Engineering Department, Tabriz University, Tabriz, Iran;
rnDepartment of Aerospace Engineering, Ryerson University, Toronto, Ontario, Canada;
rnMechanical Engineering Department, Tabriz University, Tabriz, Iran;
d: diameter of cylindrical part of film hole, m; h: slot height, m; H: vane height, m; k: turbulent kinetic energy, m~2 s~(-2); L: chord length, m; et al;
机译:汽轮机叶片前缘轮廓对成形孔薄膜冷却的影响
机译:异形喷孔对涡轮叶片前缘膜冷却的影响
机译:涡轮叶片前缘附近沟槽中的薄膜冷却的计算研究
机译:涡轮叶片前缘轮廓对异型孔薄膜冷却的影响
机译:涡轮叶片前缘的脉冲薄膜冷却
机译:燃气轮机叶片前缘旋流膜冷却的共轭传热研究
机译:涡轮叶片前缘区域的模拟薄膜冷却(横流中气缸对薄膜效率的影响)
机译:薄膜涡轮叶片的前缘冷却剂管道