机译:涡轮叶片尖端形状对线性涡轮叶栅总压力损失和二次流的影响
School of Aerospace and Mechanical Engineering, Korea Aerospace University, 100 Hanggongdae-gil, Hwajeon-dong, Deogyang-gu, Coyang-city 417-791, Republic of Korea;
School of Aerospace and Mechanical Engineering, Korea Aerospace University, 100 Hanggongdae-gil, Hwajeon-dong, Deogyang-gu, Coyang-city 417-791, Republic of Korea;
School of Aerospace and Mechanical Engineering, Korea Aerospace University, 100 Hanggongdae-gil, Hwajeon-dong, Deogyang-gu, Coyang-city 417-791, Republic of Korea;
School of Aerospace and Mechanical Engineering, Korea Aerospace University, 100 Hanggongdae-gil, Hwajeon-dong, Deogyang-gu, Coyang-city 417-791, Republic of Korea;
tip leakage vortex; total pressure loss coefficient; squealer tip; grooved tip; chamfered tip; dimpled tip;
机译:线性涡轮叶片叶片翼型和端壁传热的实验研究-二次流和表面粗糙度的影响。
机译:具有线性变化的高度沿水流方向的围墙的涡轮机叶栅的二次流损失减少
机译:具有线性变化的高度沿水流方向的围墙的涡轮叶栅的二次流损失减少
机译:减少带有叶片栅栏的低压涡轮机中的二次流损失:第二部分-线性级联上的实验验证
机译:带有低压涡轮叶片的二维线性叶栅中的非稳态流动。
机译:风力涡轮机叶片沿翼展方向的全尺寸疲劳测试并研究裂纹扩展对叶片性能的影响
机译:二级流动,总压力损失和轴向涡轮叶栅中的周向变形的影响