欢迎登录材料期刊网

材料期刊网

高级检索

基于复合材料各向异性板的大挠度方程,采用Ritz法和最小势能原理推导出了正交各向异性复含材料层合板在面内弯曲载荷作用下临界屈曲弯矩的解析解;给出了面内弯剪复合载荷作用下复合材料层合板屈曲的强度校核方法,并将本文方法所得结果与用有限元法(FEM)所得结果进行了比较.结果表明,本文方法与有限元方法相吻合,并且形式简洁,便于工程应用.

参考文献

[1] 岳珠峰,王富生,王佩艳,等.飞机复合材料结构分析与优化设计[M].北京:科学出版社,2011.Yue Zhufeng,Wang Fusheng,Wang Peiyan,et al.Aircraft composite structure analysis and optimization[M].Beijing:Science Press,2011.
[2] 俸翔,马元春,卢子兴.复合材料夹层板屈曲强度的分散性分析[J].复合材料学报,2011,28(1):132-137.Feng Xiang,Ma Yuanchun,Lu Zixing.Variation analysis for buckling strength of composite sandwich plates[J].Acta Materiae Compositae Sinica,2011,28(1):132-137.
[3] 孔斌,叶强,陈普会,等.复合材料整体加筋板轴压后屈曲的传载机制[J].复合材料学报,2010,27(5):142-149.Kong Bin,Ye Qiang,Chen Puhui,et al.Post-buckling load transfer mechanisms of an integrated composite panel under uniaxial compression[J].Acta Materiae Compositae Sinica,2010,27(5):142-149.
[4] 白瑞祥,王 蔓,陈浩然.冲击后含损伤复合材料格栅加筋板的后屈曲[J].复合材料学报,2006,23(3):141-145.Bai Ruixiang,Wang Man,Chen Haoran.Postbuckling behavior of damaged advanced grid stiffened structure after impact[J].Acta Materiae Compositae Sinica,2006,23(3):141-145.
[5] Tung T K,Surdenas J.Buckling of rectangular orthotropie plates under biaxial loading[J].Journal of Composite Materials,1987,21(2):124-128.
[6] Libove C.Buckle pattern of biaxially compressed simply supported orthotropic rectangular plates[J].Journal of Composite Materials,1983,17(1):45-48.
[7] Kassapoglou C.Simultaneous cost and weight minimization of composite stiffened panels under compression and shear[J].Composites Part A:Applied Science and Manufacturing,1997,28(5):419-435.
[8] Timoshenko S,Gere J.Theory of elastic stability[M].2nd ed.New York:McGraw-Hill Book Company,Inc.,1963.
[9] Featherston C A,Ruiz C.Buckling of flat plates under bending and shear[J].Proceedings of the Institution of Mechanical Engineers Part C:Journal of Mechanical Engineering Science,1998(4):212-249.
[10] Leissa A W,Kang J H.Exact solutions for vibration and buckling of an SS-C-SS-C rectangular plate loaded by linearly varying in-plane stresses[J].International Journal of Mechanical Sciences,2002,44(9):1925-1945.
[11] Leissa A W,Kang J H.Exact solutions for the buckling of rectangular plates having linearly varying in-plane loading on two opposite simply supported edges[J].International Journal of Solids and Structures,2005,42(14):4220-4238.
[12] Lekhnitskii S G.Anisotropic plates[M].2nd ed,Tsai S W,Gordon C T,translated.New York:Gordon & Breach Science Publishers,Inc.,1968.
[13] Lopatin A V,Morozov E V.Buckling of the SSFF rectangular orthotropic plate under in-plane pure bending[J].Composite Structure,2009,90(3):287-294.
[14] Panda S K,Ramachandra L S.Buckling of rectangular plates with various boundary conditions loaded by non-uniform inplane loads[J].International Journal of Mechanical Sciences,2010,52(6):819-828.
[15] Kassapoglou C.Design and analysis of composite structures:With applications to aerospace structures[M].Chicester:John Wiley & Sons,2010.
[16] 吴连元.板壳稳定性理论[M].武汉:华中理工大学出版社,1996.Wu Lianyuan.Stability theory of plate and shell[M].Wuhan:Huazhong University of Science and Technology Press,1996.
[17] 中国航空研究院.复合材料结构稳定性分析指南[M].北京:航空工业出版社,2002.Institute of Aeronautics China.Manual of composite structure stability analysis[M].Beijing:Aviation Industry Press,2002.
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:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%