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介绍了一种纤维曲线铺放的变刚度复合材料层合板有限元建模方法.按照曲线铺放规律定义每一个单元的实常数,并对这种纤维曲线铺放层合板进行建模.在此基础上讨论了在弯曲和压缩失效两种不同边界条件下,采用Tsai-Wu失效准则,对其进行失效分析,验证其面内受力情况,计算最大的Tsai-Wu强度比倒数1/R.当1/R =1时,所施加的载荷为失效的临界载荷.对比两组纤维直线和纤维曲线的铺层算例,弯曲失效条件下临界失效载荷提高16%和21%,压缩失效条件下临界失效载荷提高51%和19%.纤维曲线铺放层合板有效提高了失效性能.

参考文献

[1] Olmedo R;Gürdal Z.Composite laminates with spatially varying fibre orientations:Variable stiffness panel concept[A].AIAA,1992:207-284.
[2] Samuel T. IJsselmuiden;Mostafa M. Abdalla;Zafer Guerdal .THERMOMECHANICAL DESIGN OPTIMIZATION OF VARIABLE STIFFNESS COMPOSITE PANELS FOR BUCKLING[J].Journal of thermal stresses,2010(10):977-992.
[3] Waldhart C .Analysis of tow-placed,variable-stiffness laminates[D].Blacksburg.VA:Vir-ginia Polytechnic Institute and State University,1996.
[4] Lopes CS;Camanho PP;Gurdal Z;Tatting BF .Progressive failure analysis of tow-placed, variable-stiffness composite panels[J].International Journal of Solids and Structures,2007(25/26):8493-8516.
[5] C.S. Lopes;Z. Guerdal;P.P. Camanho .Variable-stiffness composite panels: Buckling and first-ply failure improvements over straight-fibre laminates[J].Computers & structures,2008(9):897-907.
[6] Adriana W. Blom;Patrick B. Stickler;Zafer Guerdal .Optimization of a composite cylinder under bending by tailoring stiffness properties in circumferential direction[J].Composites, Part B. Engineering,2010(2):157.
[7] 马永前,张淑杰,许震宇.纤维曲线铺放的变刚度复合材料层合板的屈曲[J].玻璃钢/复合材料,2009(05):31-35.
[8] 秦永利,祝颖丹,范欣愉,颜春,李晓拓,张笑晴.纤维曲线铺放制备变刚度复合材料层合板的研究进展[J].玻璃钢/复合材料,2012(01):61-66.
[9] Liu K S;Tsai S W .A progressive quadratic failure crierion for a laminate[J].Composites Science and Technology,1998,58(07):1023-1032.
[10] W. Van Paepegem;J. Degrieck .Calculation of damage-dependent directional failure indices from the Tsai-Wu static failure criterion[J].Composites science and technology,2003(2):305-310.
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