Numerical Investigation of Aluminum Foam Shield Based on Fractal Theory and Node-separation FEM

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• 作者：Xiaotian ZHANG ^{u_lever@sa.buaa.edu.cn}  ; [Author Vitae] ; Guanghui JIA ; ^{jiaguanghui@buaa.edu.cn}  ; [Author Vitae] ; Hai HUANG
• 关键词：aluminum foam ; simulation ; fractal ; hypervelocity impact ; FEM
• 刊名：Chinese Journal of Aeronautics
• 出版年：2011
• 出版时间：December, 2011
• 年：2011
• 卷：24
• 期：6
• 页码：734-740
• 全文大小：1466 K

文摘

Fractal feature of aluminum foam (Al-foam) section is analyzed with digital image processing technique, and fractal dimension of Al-foam is evaluated with logarithmic linear regression method. Sierpinski carpet can be used to model Al-foam section. Al-foam with different fractal dimensions and relative density can be obtained by adjusting iteration times and division parameters. Sierpinski sponge is extended from Sierpinski carpet and used to model 3D Al-foam bumper. Node-separation Lagrangian finite element method (FEM) is introduced to simulate the hypervelocity impact (HVI) process. The modeling and simulation method is calibrated by the comparison of numerical results and experimental data. Ballistic limit curves of Al-foam and aluminum alloy bumper with the same areal density are obtained by simulations. The results show that the protection performance of Al-foam bumper is much better than aluminum alloy bumper. Al-foam is well suited for spacecraft shield application.