...
机译:冷却剂质量流量比对两入口旋转楔形通道传热的影响
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics and 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 and 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 and 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 and 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;
Gas turbine heat transfer; Rotor blades trailing edge; Wedge-shaped channel; Rotating;
机译:具有侧向流入孔的旋转式两入口冷却楔形通道中的传热性能
机译:具有销翅片的旋转双入口楔形通道中的传热
机译:在第二入口的不同位置的双入口旋转楔形通道中进行热传递
机译:旋转,光滑,高纵横比(4:1)的冷却水通道的热/质量传递,弯曲壁面在90°和45°方向上
机译:填充床费-托反应器的传热和传质增强:被动流动扰动和反应器纵横比的影响研究
机译:两相入口质量质量速度流向和加热周长对矩形通道中流沸腾的影响:第1部分–两相流和传热结果
机译:滑动效应旋转通道中MHD纳米流体流动的热量和传质分析