机译:在旋转叶片的前缘进行薄膜抽出流动的冲击传热实验。
National Key Laboratory of Science and Technology on Aero-Engines, School of Jet Propulsion, Beihang University, Beijing 100191, China;
National Key Laboratory of Science and Technology on Aero-Engines, School of Jet Propulsion, Beihang University, Beijing 100191, China;
Institute of Engineering Thermophysics, Chinese Academy of Science, Beijing 100190, China;
National Key Laboratory of Science and Technology on Aero-Engines, School of Jet Propulsion, Beihang University, Beijing 100191, China;
impinging; film; heat transfer; transient experiment; rotation;
机译:薄膜冷却孔位置对涡轮叶片前缘撞击/扩散冷却的流动和传热特性的影响
机译:叶片前缘模型组合撞击和薄膜冷却的共轭传热预测
机译:使用不同方案在薄膜冷却的刀片前缘的不同方案的锥形冷却的共轭热传递
机译:薄膜冷却装置对涡轮叶片前缘撞击传热的影响
机译:在高转数下在燃气涡轮叶片的前缘和后缘冷却通道中的热传递。
机译:燃气轮机叶片前缘旋流膜冷却的共轭传热研究
机译:吹气比对燃气轮机叶片前缘薄膜冷却结构中薄膜冷却效率和传热系数影响的实验和数值研究
机译:薄膜涡轮叶片的前缘冷却剂管道