机译:带有不同配置的Pin Fin-Dimple组合阵列的通道内流动和传热的实验和数值研究
Institute of Turbomachinery, Department Mechanical and Power Engineering, Shanghai Jiaotong University, Dongchuan Road 800, Shanghai 200240, P.R. China;
Institute of Turbomachinery, Department Mechanical and Power Engineering, Shanghai Jiaotong University, Dongchuan Road 800, Shanghai 200240, P.R. China;
Institute of Turbomachinery, Department Mechanical and Power Engineering, Shanghai Jiaotong University, Dongchuan Road 800, Shanghai 200240, P.R. China;
gas turbine cooling; pin fin; dimple; flow; heat transfer enhancement;
机译:针鳍-凹窝和针鳍阵列的通道内流动和传热的实验和数值研究
机译:不同凹坑深度的销鳍-凹坑通道内流动和传热的数值研究
机译:不同凹痕深度的针状鳍状凹痕通道中压力损失和传热的实验研究
机译:双边缘带鳍片的翅片翅片通道内传热和流体流动的数值研究
机译:涡轮机翼型冷却通道传热的组合数值和实验研究,具有成角度肋和180度U型弯曲转动
机译:乙醇/聚α-烯烃纳米乳液流经圆形微通道的流动和传热特性的实验研究
机译:用销翅片和销翅片阵列冷却通道流动和传热的实验和数值研究
机译:矩形通道幂律非牛顿流体流动与传热特性的数值研究