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《Journal of Vibration and Shock》 2011-07
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RSM-based FEM model updating for a carbon fiber honeycomb sandwich panel

QIN Yu-ling1,KONG Xian-ren 1,LUO Wen-bo2 (1.Research Center of Satellite Technology,Harbin Institute of Technology,Harbin 150001,China;2.China Academy of Space Technology,Beijing 100086,China)  
A honeycomb sandwich panel with high strength and light weight is a special composite material which is widely used in satellite and other spacecrafts.There are no honeycomb material paremeters in FEM software,such as,MSC/NASTRAN and ANSYS,and the simplified equivalent structure parameters of a honeycomb sandwich panel are used,they result in the differences between the test data and the FEM data.The RSM-based model updating method avoids calling FEM program in every iteration,it improves the calculation efficiency.Here,the equivalent parameters of a honeycomb sandwich panel were calculated based on the honeycomb sandwich theory,the FEM of a multi-layer carbon fiber sandwich panel was established using SHELL91 in ANSYS.And the test data under all factors and effects were obtained based on uniform design method,the quadratic polynominal response surface model was established and the PSO with mutation factor was used to update the equivalent paremeters of the honeycomb sandwich panel,the updated paremeters were substituted into the FEM model,the FEM model calculation quality was effectively improved.
【Fund】: 长江学者创新团队发展计划(IRT0520)
【CateGory Index】: V214.6
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