玻璃钢/复合材料 ›› 2018, Vol. 0 ›› Issue (7): 97-102.

• 应用研究 • 上一篇    下一篇

基于结构动力学修正法识别蜂窝芯层合板特性参数

王德鑫, 王婷婷, 姜年朝, 李家春   

  1. 总参谋部第六十研究所,南京 210016
  • 收稿日期:2017-12-18 出版日期:2018-07-25 发布日期:2018-07-20
  • 作者简介:王德鑫(1985-),男,硕士,工程师,研究方向为无人机强度及复合材料设计,wangdexin725@163.com。

IDENTIFY CHARACTERISTIC PARAMETERS OF THE HONEYCOMB SANDWICH PANELS BASE ON THE STRUCTURAL DYNAMIC MODEL UPDATING

WANG De-xin, WANG Ting-ting, JIANG Nian-chao, LI Jia-chun   

  1. The 60th Research Institute of General Staff Dept. of P.L.A, Nanjing 210016, China
  • Received:2017-12-18 Online:2018-07-25 Published:2018-07-20

摘要: 以蜂窝芯层合板为研究对象,以模态试验的测试结果为修正目标,采用基于模态参数灵敏度有限元模型修正方法对蜂窝芯层合板的碳纤维板单层厚度、蜂窝芯材参数进行修正,从而解决有限元模型与试验测试误差较大的问题。修正结果表明,修正后的有限元模型分析结果与试验测试值基本一致,说明修正后的有限元模型具有较高的精度,使用修正后的有限元模型不仅可以用于其他动力学问题的分析,对于复杂的工程结构也可基于此方法,通过小规模试验测试来修正有限元输入的设计参数,从而提高整体复杂模型分析的准确性,有一定的工程实用价值。

关键词: 模型修正, 有限元, 蜂窝芯层合板, 模态分析, 灵敏度

Abstract: In order to solve the problem of large difference between the initial finite element analysis and experimental test, the model test data of the honeycomb sandwich panels are used as updated target to identify the cure thickness of laminate panel and the material parameters of honeycomb core based on the structural dynamic model updating. The updated results show that updated FE model has high rationality and could be used for other dynamic problems analysis. Beside, for complicated engineering structures, the simple tests can be adopted to modify the design parameters so as to improve the overall analysis accuracy and have certain engineering practical value.

Key words: model updating, finite element, honeycomb sandwich panels, model analysis, sensitivity

中图分类号: