机译:蜂窝尖注射对1.5级涡轮机空气动力学性能的影响
Institute of Propulsion Theory and Technology Harbin Institute of Technology Harbin 150001 China;
Institute of Propulsion Theory and Technology Harbin Institute of Technology Harbin 150001 China Aerospace System Engineering Shanghai Shanghai 201108 China;
Institute of Propulsion Theory and Technology Harbin Institute of Technology Harbin 150001 China;
Institute of Propulsion Theory and Technology Harbin Institute of Technology Harbin 150001 China;
aerodynamic performance; honeycomb tip; injection; 1.5-stage turbine; cavity depth; cavity and leaking flows; computational fluid dynamics (CFD); impact on the tip leakage flow;
机译:组合热条和旋流型材对冷却1.5级涡轮机空气动力学的影响:实验与计算研究
机译:后缘喷射的涡轮叶栅气动性能的实验研究
机译:低速1.5级涡轮的薄膜冷却性能:主流雷诺数和湍流的影响
机译:密封条尺寸对汽轮机级气动性能的影响:第一部分-蜂窝密封
机译:用数值法向前和后退喷射膜冷却涡轮叶片的空气动力学损失计算
机译:不同风况下海上漂浮式风力发电机的非定常空气动力学分析
机译:组合热条和旋流型材对冷却1.5级涡轮机空气动力学的影响:实验与计算研究