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本文提供了一个计算轴流式压气机叶列的非设计工况沿径气动参数的方法。用此方法对某台多级轴流式压气机的前两级和另一台单级试验压气机进行了计算。计算结果和试验的某些结果比较是令人满意的。该法对调试轴流式压气机可有一定的指导意义。
This article provides a method of calculating aerodynamic parameters along the aerodynamic diameter for non-designed working conditions of axial flow compressor blades. Using this method, the first two stages of a multi-stage axial-flow compressor and another single-stage test compressor were calculated. Comparing the results with those of the test is satisfactory. The method of debugging axial compressor can have some guidance.