对某涡喷发动机压气机的气动失稳过程进行了相关积分分析。
The process of loosing compressor aerodynamic stability in a turbojet engine was analyzed using the correlation integral method.
在土体非线性有限元分析的基础上，采用干扰能量法对边坡失稳过程进行了模拟。
On the basis of non linear finite element analysis, the destabilization process of slope was simulated by disturbing energy method in the thesis.
分析表明，非线性的相关积分分析方法是进行压气机气动失稳过程研究的有效手段。
Thus, nonlinear correlation integral method is an effective means in the investigation of the process of loosing compressor aerodynamic stability.
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