Structural reliability analysis of an aeroengine 2nd-stage compressor disk is presented.
对某型发动机压气机第2级轮盘进行了结构可靠性分析。
Numerical simulations were carried out to investigate interaction between a single stage compressor and pylons.
采用数值模拟方法，对单级低速轴流压气机与发动机吊架之间的干涉进行了计算分析。
The result indicates that the method of adding zero-stage compressor discussed in this paper is basically successful.
结果表明，本文采取的加零级方法是成功的。
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