摘要
给出了一个端壁边界层的求解计算方法，并将端壁边界层的计算结果与无粘主流进行迭代，最终计算得到的转子叶片出口轴向速度与试验结果相吻合的结论。
A solving method for end wall boundary layer is given,and the computing result for the end wall boundary layer is substituted with that for non-viscous main flow.Finally,a conclusion of rotor blade discharge axial velocity being tallied with the test result is obtained through computation.
出处
《风机技术》
北大核心
1997年第3期21-23,共3页
Chinese Journal of Turbomachinery
