机译:从人字形喷嘴受到外部冷流和内部热射流撞击的锥形壁前缘上的共轭传热-第1部分:实验分析
College of Energy and Power Engineering, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
College of Energy and Power Engineering, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China,Collaborative Innovation Center of Advanced Aero-Engine, Beijing 100191, China;
College of Energy and Power Engineering, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
College of Energy and Power Engineering, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
Conjugated convective heat transfer; Hot jet impingement; Conical surface; Chevron nozzle;
机译:在人字形喷嘴的外部冷流和内部热射流的作用下,在锥形壁前缘上产生共轭传热;第2部分:数值分析
机译:楔形凹壁前缘的共形传热,由瓦楞孔板的热射流内部撞击
机译:使用中心卫星热喷孔改善锥形壁前缘的共轭传热
机译:射流与壁间距对热硅上湍流射流喷嘴的传热特性和流场的影响
机译:德州大学阿灵顿分校新电弧加热风洞(AWHT-II)的主动冷却多级锥形喷嘴和超音速低雷诺扩散器的共轭传热和热结构分析。
机译:燃气轮机叶片前缘旋流膜冷却的共轭传热研究
机译:机翼前缘凹面上的射流冲击传热:实验研究和相关发展
机译:涡轮叶片外部传热。第1卷。前缘喷头薄膜冷却的表面传热分布的分析和实验评估