波纹夹芯板等效有限元建模及其振动特征参数计算与试验验证
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西北工业大学航空学院

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国家自然科学基金项目(面上项目,重点项目,重大项目)


Vibrational Feature Calculation On an Equivalent Finite Element Model of Corrugated Sandwich Plates and Experiment Validations
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    摘要:

    用有限元方法计算波纹夹芯板结构的力学行为时,因数值模型占用的计算资源太大,会引起求解时间过长等问题。为了减少该类结构有限元模型规模,快速有效地对其开展动力分析与计算,本文首先将中间波纹夹芯层简化成均质的正交各向异性板,基于三阶剪切变形理论对层合板剪切性能进行分析,确定波纹夹芯板单元的等效刚度阵。然后基于等效模型计算在悬臂和自由两种边界条件下波纹夹芯板结构的固有频率,并与试验结果进行对比,验证该等效有限元模型的有效性,且计算结果明显优于基于一阶剪切变形模型的结果。表明本文提出的方法不仅可简化波纹夹芯板结构动态特征参数的计算,且具有较高的计算精确性。

    Abstract:

    When the finite element method is employed to calculate the mechanical behaviors of a corrugated sandwich panel structure, the numerical model occupies a large amount of computational resources, which usually causes the problem of long-time solution. In order to reduce the scale of the finite element model and to quickly perform the dynamic analysis of such type structures, in this paper the middle corrugated sandwich layer is simplified into a homogeneous orthotropic plate. Then, based on the third-order shear deformation theory, the equivalent stiffness matrix of the corresponding plate element is formulated from adequate performance analyses of the corrugated sandwich plate. Afterwards, the natural frequencies of two corrugated sandwich plate structures in the cantilevered and free states are obtained respectively through the test and numerical calculation. By comparing with the experimental results, the effectiveness of the equivalent finite element model is verified. It turns out that the obtained results are much better than those based on the first-order shear deformation model. Moreover, the method proposed in this work can be utilized efficiently for modal parameter computations of the corrugated sandwich plates with the high accuracy.

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  • 收稿日期:2023-10-29
  • 最后修改日期:2024-01-21
  • 录用日期:2024-01-22
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