机译:端壁上有开孔的薄膜冷却流场
Creative Power Solutions USA, Inc., 11010 North Saguaro Boulevard, Fountain Hills, AZ 85268;
Department of Mechanical and Nuclear Engineering, Pennsylvania University, University Park, PA 16802;
C: true chord of the stator vane; D: diameter of the film-cooling hole; FC: film-cooling holes; M: blowing ratio based on inlet mainstream veloc- ity M=P_jU_j/p_(in)U_(in); P: vane pitch; hole pitch; et al;
机译:叶片-端壁交界处的薄膜冷却孔的凹凸变形
机译:离散孔布置对涡轮叶片叶栅端壁膜冷却效率的影响
机译:横向沟槽中端壁薄膜冷却孔上多相颗粒沉积的模拟
机译:端壁上带有开孔的薄膜冷却流场
机译:表面条件对端壁薄膜冷却的影响
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:具有扩展出口的薄膜冷却孔的流场测量