机译:带肋排风通道整体降温效果的实验研究
University of Science and Technology of China, Hefei 230027, Anhui, PR China;
University of Science and Technology of China, Hefei 230027, Anhui, PR China;
University of Science and Technology of China, Hefei 230027, Anhui, PR China;
Shenyang Aero-Engine Research Institute, Shenyang i 10015, Liaoning, PR China;
Shenyang Aero-Engine Research Institute, Shenyang i 10015, Liaoning, PR China;
ribbed channel; film holes; high temperature; overall cooling effectiveness; blowing ratio; experimental investigation;
机译:具有类似发动机横截面的带肋双通道内部冷却通道180°弯曲时压力损失和传热的实验研究
机译:带肋三角形冷却通道传热的实验研究
机译:蒸汽作冷却剂的肋状矩形通道传热与摩擦特性试验研究
机译:矩形截面矩形通道内雾/空气冷却的数值研究
机译:具有排气孔的肋粗糙矩形冷却通道的实验传热
机译:空气顺应性对微流道血样力学性能测量的实验研究
机译:薄膜孔萃取在汽轮机叶片内部肋冷却通道中薄膜孔提取的影响的实验研究
机译:带肋和排气的多道内冷模型的实验传热和体积温度测量