Computational Model of Progressive Failure in Composite Sandwich Structures
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摘要: 建立了可以预测面内破坏、分层破坏和芯层破坏的复合材料夹层结构逐渐破坏模型.利用能量变分原理和非线性几何方程,以反对称失稳为例导出了考虑剪切效应夹层板的非线性稳定性控制方程组,并利用广义傅氏级数法对此高阶偏微分非线性方程组进行数值求解,在此基础上利用蔡-胡及最大剪应力强度理论及刚度退化规律得到复合材料夹层板的临界载荷、后屈曲路径、破坏过程和强度极限.Abstract: Computational model of progressive failure in composite sandwich structures is built up to predict the face fracture,delamination failure and core failure. Nonlinear geometry equations and energy variational equation is estimated according to overall bulking of composite sandwich plates. The nonlinear stability governing equations of anti-symmetrical buckling of sandwich plate are deduced, considering the transverse shear deformation influence of core. In order to solve the governing equations, the method of generalized double Fourier series is employed. Tsai-Wu failure criteria and Maximum stress criteria are proposed to predict composite face-sheet failure,core failure and interlaminar failure. These failure criteria and stiffness reduction are used to obtain critical load,post-bulking behavior and limit load.
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Key words:
- composite materials /
- mechanism of deterioration /
- ultimate loads /
- sandwich structure
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1. 张志民,刘宏增. 大挠度剪切理论下复合材料夹层扁壳的傅里叶级数解法.复合材料学报,1998,15(2):102~107 2. Minguet P,Dugundji J, Paul A. Lagace,buckling and failing of plates with graphite-epoxy faces and various cores. AIAA-87-0795,1987.394~401 3. 张志民. 复合材料结构力学. 北京:北京航空航天大学出版社,1993 4. 刘宏增.复合材料夹层扁壳在复杂载荷下非线性稳定性剪切理论:[学位论文]. 北京:北京航空航天大学飞行器设计与应用力学系,1997 5. SIH G C,Skudra A M. Failure mechanics of composites.Amsterdam:Elsevier Science Publishers,1991 6. 崔维成. 复合材料结构破坏过程的计算机模拟.复合材料学报, 1996,13(4):102~111
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