机译:具有横向流体提取的旋转双入口后边缘通道的传热
National Key Laboratory of Science and Technology on Aero-Engines School of Energy and Power Engineering Beijing University of Aeronautics and Astronautics;
National Key Laboratory of Science and Technology on Aero-Engines School of Energy and Power Engineering Beijing University of Aeronautics and Astronautics;
National Key Laboratory of Science and Technology on Aero-Engines School of Energy and Power Engineering Beijing University of Aeronautics and Astronautics;
National Key Laboratory of Science and Technology on Aero-Engines School of Energy and Power Engineering Beijing University of Aeronautics and Astronautics;
R&
D Center Dept of Discipline Engineering;
National Key Laboratory of Science and Technology on Aero-Engines School of Energy and Power Engineering Beijing University of Aeronautics and Astronautics;
Trailing edge channel; Rotating heat transfer; Two inlets; Mass flow ratio;
机译:具有横向流体提取的旋转双入口后边缘通道的传热
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:传热在旋转,后缘,带有部分长针翅片的会聚通道
机译:带有侧墙流体萃取的两入口旋转销-翅片强化矩形通道中的传热
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:使用新型旋转扩张器护套TightRail™进行铅提取:双中心体验
机译:后缘喷射对涡轮叶片针翅冷却通道局部热(质量)传递的影响