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Modal scaling in operational modal analysis using a finite element model

机译:使用有限元模型的操作模态分析中的模态缩放

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Operational modal analysis (OMA) is a technique that has been widely used on civil and mechanical structures in the last 10 years. As the force is unknown, mode shapes cannot be mass normalized from the responses used for modal identification. In the past few years, several formulations have been proposed to scale mode shapes using the mass-change method, which consists of repeating modal testing after changing the mass at different points of the structure where the mode shapes are known. This technique is easy to use in small systems but it has important drawbacks in medium and large structures due to the difficulties of applying masses of sufficient magnitude. In this paper a more simple methodology is proposed based on scaling the experimental mode shapes of a structure using the mass matrix of a finite element model. Two approaches are compared; one approach where the mass matrix is reduced to the set of measurement points using SEREP and a second approach where the experimental mode shapes are expanded to all DOFs in the model using a newly published principle called the local correspondence (LC) principle. The two approaches are compared in two case studies: a numerical example and a real experimental case. In the numerical example a finite element model was assembled in MATLAB, which was considered the experimental model, and then one thousand finite element models were simulated changing the material and the section properties of each element of the model, in order to study the accuracy provided by the different techniques. As regarding the experimental case, the scaling factors of a cantilever beam were estimated by the mass change method and with the equations that consider the mass matrix of the finite element model. The effect of discretization of the finite element model was studied by assembling several finite element models with different numbers of degree of freedoms.
机译:操作模态分析(OMA)是一种在过去10年中广泛用于土木和机械结构的技术。由于作用力未知,因此无法从用于模态识别的响应中对模态形状进行质量归一化。在过去的几年中,已经提出了几种使用质量变化方法来缩放模态形状的公式,该方法包括在已知模态形状的结构的不同点改变质量之后重复模态测试。该技术易于在小型系统中使用,但由于难以施加足够量的质量,因此在中型和大型结构中具有重要的缺点。在本文中,基于使用有限元模型的质量矩阵缩放结构的实验模式形状,提出了一种更简单的方法。比较了两种方法;一种方法是使用SEREP将质量矩阵缩减为一组测量点,第二种方法是使用称为局部对应(LC)原理的新发布原理将实验模式形状扩展到模型中的所有自由度。在两个案例研究中比较了这两种方法:一个数值示例和一个实际的实验案例。在数值示例中,在MATLAB中组装了一个有限元模型,将其视为实验模型,然后通过模拟千个有限元模型来更改模型中每个元素的材料和截面特性,以研究所提供的精度通过不同的技术。对于实验情况,通过质量变化方法和考虑了有限元模型质量矩阵的方程式来估算悬臂梁的比例因子。通过组装几个具有不同自由度数的有限元模型,研究了离散化有限元模型的效果。

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