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机译:旋转涡轮叶片模型中薄膜冷却的传热系数-第一部分:吹气比的影响
Department of Engineering Thermophysics, and National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beihang University, Beijing 100083, P. R. China;
Department of Engineering Thermophysics, and National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beihang University, Beijing 100083, P. R. China;
Department of Engineering Thermophysics, and National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beihang University, Beijing 100083, P. R. China;
Department of Engineering Thermophysics, and National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beihang University, Beijing 100083, P. R. China;
Department of Engineering Thermophysics, and National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beihang University, Beijing 100083, P. R. China;
Department of Engineering Thermophysics, and National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beihang University, Beijing 100083, P. R. China;
D: film cooling hole diameter, mm; DR: density ratio; h_(f0): heat transfer coefficient in the presence of filmcooling, W/m~2 K (h_f=q/(T_(aw)-T_w); h_g: heat transfer coefficient in the presence of film cooling, W/m~2 K (h_g=q/(T_8-T_w); h_0: heat transfer coefficient in the absence of film cooling, W/m~2 K (h_0=q/(T_(g0)-T_(w0))); et al;
机译:全覆盖薄膜冷却:稀疏孔阵列在不同的吹塑比和收缩比下的传热系数和膜效率
机译:全覆盖薄膜冷却:在不同的孔角度,收缩率和吹塑率下,致密孔阵列的膜效率和传热系数
机译:燃气轮机叶片尖端的传热系数和薄膜冷却效果
机译:旋转涡轮叶片模型上的薄膜冷却换热系数:第一部分:吹气比的影响
机译:燃气轮机叶片膜冷却和叶片尖端传热。
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