Numerical simulation for flow and heat transfer of a rotating turbine cavity with realistic engine parameters
Dept. of Jet Propulsion, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China;Dept. of Jet Propulsion, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China;Dept. of Jet Propulsion, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China;Dept. of Jet Propulsion, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China