旨在建立能够正确预计复合材料圆柱壳的屈曲和后屈曲渐进破坏行为的模拟策略.采用有限元方法和Hashin失效准则进行模拟,基于该失效准则编写了用户材料子程序,然后插入到商用有限元软件ABAQUS中.分析了中心受横向集中载荷作用复合材料圆柱壳板,壳板的2条直边弹性支持,2条曲边自由.为了探讨弹性边界条件和集中载荷作用点应力集中的影响,将有限元分析结果与文献中的试验结果进行了比较,提出了一种合理的弹性边界选取依据.研究结果表明,在建模中考虑了弹性边界和集中载荷作用点处存在的应力集中后,本文中模拟的结果与文献中的试验结果比较接近,模拟精度明显高于文献中报道的结果.这也验证了本文中建立的模拟策略的合理性.
参考文献
[1] | 万志敏,杜星文,谢志民.玻璃/环氧圆柱壳的冲击响应与稳定性分析[J].复合材料学报,2001,18(4);82-86.Wan Zhimin,Du Xingwen,Xie Zhimin.Impact response and stability analysis of glass-epoxy cylindrical shell[J].Acta Materiae Compositae Sinica,2001,18(4):82-86. |
[2] | 徐孝诚,马斌捷.三维四向整体编织复合材料圆筒壳体临界外压计算及试验验证[J].复合材料学报,2002,19(4):92-95.Xu Xiaocheng,Ma Binjie.Critical external pressure calculation and test validation of 3D 4-step braided composite cylindrical shell[J].Acta Materiae Compositae Sinica,2002,19(4):92-95. |
[3] | Engelstad S P,Reddy J N,Knight N F.Postbuckling response and failure prediction of graphite/epoxy plates loaded in compression[J].AIAA,1992,30(8):2106-2113. |
[4] | Kweon J H,Hong C S,Lee I C.Postbuckling compressive strength of graphite/epoxy laminated cylindrical panels loaded in compression[J].AIAA,1995,33(2):217-222. |
[5] | Knight N F,Starnes J H.Postbuckling behavior of selected curved stiffened graphite-epoxy panels loaded in axial compression[J].AIAA,1988,26(3):344-352. |
[6] | Lee I C,Kim C G,Hong C S.Buckling and postbuckling behavior of stiffened composite panels loaded in compression[J].AIAA,1997,35(1):202-204. |
[7] | 束永平,张建武,吴金松.反对称正交铺层剪切圆柱壳在外压下的屈曲和后屈曲[J].复合材料学报,1999,16(4):121-129.Shu Yongping,Zhang Jianwu,Wu Jinsong.Buckling and postbuckling of antisymmetrically laminated cross-play sheardeformable cylindrical shells under external pressure[J].Acta Materiae Compositae Sinica,1999,16(4):121-129. |
[8] | 赵桂平,赵锺斗.基于改进弧长法的层压复合壳后屈曲反应分析[J].工程力学,2003,20(1):106-111.Zhao Guiping,Zhao Zhongdou.Postbuckling analysis of laminated composite shell based on an improved arc-length method[J].Engineering Mechanics,2003,20(1):106-111. |
[9] | Wardle B L,Lagace P A.Behavior of composite shells under transverse impact and quasi-static loading[J].AIAA,1998,36(6):1065-1073. |
[10] | Wardle B L,Lagace P A,Tudela M A.Buckling response of transversely loaded composite shells Ⅰ:Experiments[J].AIAA,2004,42(7):1457-1464. |
[11] | Wardle B L,Lagace P A,Tudela M A.Buckling response of transversely loaded composite shells Ⅱ:Numerical analysis[J].AIAA,2004,42(7):1465-1473. |
[12] | Spottswood S M,Palazotto A N.Progressive failure analysis of a composite shell[J].Composite Structures,2001,53(1):117-131. |
[13] | 陈伟,许希武.复合材料双曲率壳屈曲和后屈曲的非线性有限元研究[J].复合材料学报,2008,25(2):178-187.Chen Wei,Xu Xiwu.Buckling and postbuckling response analysis of the doubly-curved composite shell by nonlinear FEM[J].Acta Materiae Compositae Sinica,2008,25(2):178-187. |
[14] | Reddy Y S N,Reddy J N.Linear and non-linear failure analysis of composite laminates with transverse shear[J].Composite Science and Technology,1992,44(3):227-255. |
[15] | Hibbit D,Karlsson B,Sorenson P.ABAQUS reference manual 6.7[M].Pawtucket:ABAQUS Inc,2005. |
[16] | 王爱军,王鑫伟,陆浦.圆柱壳板非线性屈曲的分叉解[J].南京航空航天大学学报,2008,40(5):637-640.Wang Aijun,Wang Xinwei,Lu Pu.Nonlinear bifurcation buckling solution of circular cylindrical shell panel[J].Journal of NUAA,2008,40(5):637-640. |
上一张
下一张
上一张
下一张
计量
- 下载量()
- 访问量()
文章评分
- 您的评分:
-
10%
-
20%
-
30%
-
40%
-
50%