Institute of Engineering Thermophysics China Academy of Sciences Beijing, China;
National Key Lab.of Science and Technology on Aero-Engines Beijing University of Aeronautics and Astronautics Beijing, China;
National Key Lab.of Science and Technology on Aero-Engines Beijing University of Aeronautics and Astronautics Beijing, China;
film cooling; effectiveness; blowing ratio; density ratio;
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:热条纹对带喷淋头薄膜冷却的高压涡轮叶片级联的影响
机译:高压涡轮机带有“经络收缩”和“经络”和悠闲扇形薄膜冷却孔的喷嘴叶片平台薄膜冷却效能研究
机译:环形涡轮级联压力侧的薄膜冷却特性
机译:一级高压燃气轮机的泄漏级数和轮廓对端壁膜冷却的影响的实验级联模拟。
机译:燃气轮机叶片前缘旋流膜冷却的共轭传热研究
机译:热条纹对带喷头薄膜冷却的高压涡轮叶栅的影响