机译:涡轮机叶片后边缘冷却引导销翅片在楔形通道中湍流流动和传热的实验和数值研究
Institute of Turbomachinety School of Mechanical Engineering Shanghai Jiao Tong University Dongchuan Road 800 Shanghai 200240 China;
Institute of Turbomachinety School of Mechanical Engineering Shanghai Jiao Tong University Dongchuan Road 800 Shanghai 200240 China;
Institute of Turbomachinety School of Mechanical Engineering Shanghai Jiao Tong University Dongchuan Road 800 Shanghai 200240 China;
Paris Tech Elite Institute of Technology Shanghai Jiao Tong University Dongchuan Road 800 Shanghai 200240 China;
Gas turbine; Trailing edge cooling; Heat transfer; Pin fin; Flow optimization;
机译:涡轮叶片尾缘回缩区的薄膜冷却与对流换热特性的数值研究
机译:汽轮机叶片后缘薄膜冷却与对流传热特性的数值研究
机译:后缘冷却孔堵塞对后缘冷却通道传热影响的实验/数值研究
机译:后缘溢流孔对涡轮叶片后缘内部冷却通道的流动和传热影响的数值研究
机译:L型冷却通道中的流动和热传递,该通道带有肋骨和针状鳍片,用于燃气轮机叶片和叶片的后缘。
机译:后缘不同冷却方式的双通道梯形通道数值结果的验证和分析
机译:后缘喷射对涡轮叶片针翅冷却通道局部热(质量)传递的影响
机译:具有冲击,薄膜和对流冷却的弦向翅片涡轮叶片的实验传热和流动结果