机译:在环形级联中的跨音质涡轮叶片的轮廓端部上的上游薄膜冷却
Turbine Heat Transfer Laboratory Department of Mechanical Engineering Texas A&M University College Station TX 77843;
Turbine Heat Transfer Laboratory Department of Mechanical Engineering Texas A&M University College Station TX 77843;
Turbine Heat Transfer Laboratory Department of Mechanical Engineering Texas A&M University College Station TX 77843;
Turbine Heat Transfer Laboratory Department of Mechanical Engineering Texas A&M University College Station TX 77843;
Honeywell Aerospace Phoenix AZ 85034;
Honeywell Aerospace Phoenix AZ 85034;
Honeywell Aerospace Phoenix AZ 85034;
film cooling; contoured endwall; turbine heat transfer; heat transfer and film cooling;
机译:涡轮叶片端壁薄膜冷却用Barchan-Dune形斜坡在单通道延长风隧道中
机译:使用压敏涂料测量技术的延长型涡轮叶片端部薄膜冷却
机译:涡轮叶片端壁薄膜冷却比较五个膜孔设计图案和三个上游注射角度
机译:在环形级联中的跨音质涡轮叶片的轮廓端部上的上游薄膜冷却
机译:燃气轮机第一级喷嘴导流叶片中的测量随着薄膜冷却和端壁轮廓而级联。
机译:湍流强度对燃气轮机叶片通道的阶梯形或光滑端壁处的交叉喷射薄膜冷却的影响
机译:在跨音级级联的高自由流湍流下涡轮叶片的淋浴喷头薄膜冷却性能