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机译:热传递汽轮机级联流动的直接数值模拟
School of Jet Propulsion Beijing University of Aeronautics and Astronautics Beijing 100191 China;
China Gas Turbine Establishment Aviation Key Laboratory of Science and Technology on Aero-Engine Altitude Simulation Sichuan 621703 China;
School of Aerospace engineering Tsinghua University Beijing 100084 China;
School of Jet Propulsion Beijing University of Aeronautics and Astronautics Beijing 100191 China;
Direct numerical simulation; high-order finite difference schemes; turbine cascade flow; heat transfer; turbulence; transition; 47.11.-j;
机译:热传递汽轮机级联流动的直接数值模拟
机译:涡轮叶片叶栅高三维湍流和端壁传热数值模拟的最新进展
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