机译:具有不同壁温比和通道方向的旋转光滑方形U型管的传热研究
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;
R&D Center, Dept of Discipline Engineering, AVIC Commercial Aircraft Engine Co., Ltd., Shanghai 201108, China;
Heat transfer; Rotating channel; Wall-temperature ratio; Channel orientation; Critical rotation number;
机译:高旋转数下旋转方形U形管道中浮力对传热的影响
机译:高转数下旋转光滑方形U形管中的压降和传热
机译:高旋转数旋转光滑方形U形管中的传热研究
机译:高旋转数下通道定向对旋转光滑方形U形管传热的影响
机译:在具有湍流和光滑表面的固定和旋转蛇形通道中,高纵横比矩形通道的热传递。
机译:解耦性科里奥利力和旋转浮力效应旋转通道的全场传热特性
机译:高旋转数下旋转方形U形管道中浮力对传热的影响
机译:旋转蛇形通道中的传热,具有选定的模型方向,用于平滑或倾斜的跳闸壁