欢迎登录材料期刊网

材料期刊网

高级检索

通过选择合适的纤维轨迹,丝束变角度(VAT)层合板相对于直纤维层合板能拥有更好的抗屈曲特性.为研究纤维轨迹特征长度和定向坐标系偏角对VAT层合板屈曲性能的影响,首先对原始的纤维角度线性变化方法进行改进,提出了一种纤维角度分段线性变化方法,拓展了纤维轨迹的设计空间;其次,采用改进后的纤维轨迹定义方法构建了一系列变刚度层合板;最后,基于有限元方法,从内力分布角度对变刚度层合板不同承载情况下的屈曲性能进行研究和探讨.数值结果表明:单向轴压工况下,采用半边长的特征长度和90°偏角的纤维轨迹,能使层合板的稳定性最好;双向轴压工况下,应将特征长度和定向坐标系偏角作为额外的设计变量,并通过优化获得最优的纤维轨迹.

参考文献

[1] Shih-Yao Kuo.Flutter of rectangular composite plates with variable fiber pacing[J].Composite structures,201110(10):2533-2540.
[2] Senthil Murugan;Erick I. Saavedra Flores;Sondipon Adhikari;M.I. Friswell.Optimal design of variable fiber spacing composites for morphing aircraft skins[J].Composite structures,20125(5):1626-1633.
[3] Shanshan Shi;Zhi Sun;Mingfa Ren;Haoran Chen;Xiaozhi Hu.Buckling resistance of grid-stiffened carbon-fiber thin-shell structures[J].Composites, Part B. Engineering,20131(1):888-896.
[4] Janis Sliseris;Karlis Rocens.Optimal design of composite plates with discrete variable stiffness[J].Composite structures,2013Apr.(Apr.):15-23.
[5] Zein, S.;Colson, B.;Grihon, S..A primal-dual backtracking optimization method for blended composite structures[J].Structural and multidisciplinary optimization,20125(5):669-680.
[6] Dianzi Liu;Vassili V. Toropov.A lamination parameter-based strategy for solving an integer-continuous problem arising in composite optimization[J].Computers & structures,2013Nov.(Nov.):170-174.
[7] 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,200725/26(25/26):8493-8516.
[8] 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,20089(9):897-907.
[9] Optimal Design of Tow-Placed Fuselage Panels for Maximum Strength with Buckling Considerations[J].Journal of aircraft,20103(3):775-782.
[10] Wenli Liu;Richard Butler.Buckling Optimization of Variable-Angle-Tow Panels Using the Infinite-Strip Method[J].AIAA journal,20136(6):1442-1449.
[11] Ahmad Alhajahmadl;Mostafa M. Abdalla;Zafer Guerdal.Design Tailoring for Pressure Pillowing Using Tow-Placed Steered Fibers[J].Journal of aircraft,20082(2):630-640.
[12] Zhangming Wu;Paul M. Weaver;Gangadharan Raju;Byung Chul Kim.Buckling analysis and optimisation of variable angle tow composite plates[J].Thin-Walled structures,2012:163-172.
[13] Optimization of course locations in fiber-placed panels for general fiber angle distributions[J].Composites science and technology,20104(4):564.
[14] Z. Gurdal;B.F. Tatting;C.K. Wu.Variable stiffness composite panels: Effects of stiffness variation on the in-plane and buckling response[J].Composites. Part A, Applied science and manufacturing,20085(5):911-922.
[15] Gangadharan Raju;Zhangming Wu;Byung Chul Kim;Paul M. Weaver.Prebuckling and buckling analysis of variable angle tow plates with general boundary conditions[J].Composite structures,20129(9):2961-2970.
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%