根据简化的二维流动方程,编写了正问题的计算机程序.对亚声速轴流式压气机级进行了计算,把计算结果与试验结果进行了比较.对这种计算方法作了评价并提出了特性计算中需要解决的问题。 Based on the simplified two-dimensional flow equation, a computer program was developed to solve the problem.The subsonic axial compressor stage was calculated and compared with the experimental results.The method was evaluated and proposed Features to be solved in the calculation of the problem.