机译:相似理论在旋转内部冷却通道传热研究中的应用
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics & Collaborative Innovation Center of Advanced Aero-Engine, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics & Collaborative Innovation Center of Advanced Aero-Engine, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics & Collaborative Innovation Center of Advanced Aero-Engine, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics & Collaborative Innovation Center of Advanced Aero-Engine, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;
Shenyang Aero-Engine Design and Research Institute, Aviation Industry Corporation of China, Shenyang 110015, China;
Similarity theory; Heat transfer; Rotating channel; Dissimilar radius; Scaled-up channel;
机译:对内部通道中传热增强的冷却喷嘴叶片热态进行研究的结果
机译:肋加粗的两通通道的新型冷却设计对燃气轮机叶片的压力侧和吸力侧内壁上的传热增强具有积极的旋转影响
机译:非正交内部冷却通道中高旋转数和高密度比下科里奥利力和离心力对流动和传热的影响
机译:基于LES的旋转敏感湍流模型评估,以预测涡轮叶片内部冷却通道中的传热
机译:在高转数下在燃气涡轮叶片的前缘和后缘冷却通道中的热传递。
机译:低温振荡热管的传热能力及其在超快冷却速率下的应用研究
机译:非正交内冷通道中科里奥利和离心力对高转速和高密度比下流动和传热的影响
机译:完全开发的湍流通道中连续和离散加热的传热:核废料库漂移的对流冷却应用