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Analysis of sensitivity and robustness for resonance frequencies and response levels of gas-turbine structures with nonlinear contact interfaces

机译:非线性接触界面燃气涡轮机结构谐振频率和响应水平的灵敏度和鲁棒性分析

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An effective method has been developed to calculate sensitivity and robustness of the resonance peak frequency and forced response level to variation of parameters of nonlinear friction contact interfaces and excitation. The method allows determination of the sensitivities and robustness measure simultaneously with the resonance peak frequency and response level calculated as a function of any parameter of interest and without significant computational expense. Capabilities and high efficiency of the method proposed are demonstrated on examples of analysis of large-scale finite element models of realistic bladed discs with major types of the nonlinear contact interfaces.
机译:已经开发了一种有效的方法来计算共振峰值频率的灵敏度和强制响应水平与非线性摩擦接触界面和激发的参数变化。 该方法允许使用作为任何感兴趣的任何参数的函数,并且没有显着的计算费用来确定灵敏度和鲁棒性测量的敏感度和鲁棒性测量。 提出的方法的能力和高效率在于具有主要类型的非线性接触界面的实际叶片圆盘的大规模有限元模型的分析示例。

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