Volume 38 Issue 7
Jul.  2012
Turn off MathJax
Article Contents
Yang Lei, Yan Ying, Yan Wei, et al. Progressive damage analysis method and experimental investigation of composite end frame structure[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (7): 931-935. (in Chinese)
Citation: Yang Lei, Yan Ying, Yan Wei, et al. Progressive damage analysis method and experimental investigation of composite end frame structure[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (7): 931-935. (in Chinese)

Progressive damage analysis method and experimental investigation of composite end frame structure

  • Received Date: 04 May 2011
  • Publish Date: 30 Jul 2012
  • Aiming at the upper and lower end frames of the grid stiffened composite cylinder, the tensile tests of three kinds of end frame segment models with different sizes and stacking sequence were conducted. Thus the damage forms and ultimate load of the end frames were gained. The progressive damage analysis based on various strength theories was conducted by finite element method, and the results of different theories were compared. Based on Zinoviev strength theory, by expanding its failure criterion and stiffness degradation scheme to three-dimensional format, and introducing Hashin criterion to estimate the damage modes, the modified Zinoviev theory was developed. The proposed method was used to carry out damage evolution analysis and strength prediction of the end frame model. The results of numerical simulation show good agreement with test results.

     

  • loading
  • [1]
    杜善义.先进复合材料与航空航天[J].复合材料学报,2007,24(1):1-11
    Du Shanyi.Advanced composite materials and aerospace engineering [J].Acta Materiae Compositae Sinica,2007,24(1):1-11 (in Chinese)
    [2]
    燕瑛,刘玉佳,廖宝华,等.先进复合材料格栅结构与大型飞机[J].航空制造技术,2009(2):26-29 Yan Ying,Liu Yujia,Liao Baohua,et al.Advanced composite grid structure and large aircraft[J].Aeronautical Manufacturing Technology,2009(2):26-29 (in Chinese)
    [3]
    杜善义,章继峰,张博明.先进复合材料格栅结构(AGS)应用与研究进展[J].航空学报,2007,28(2):419-424
    Du Shanyi,Zhang Jifeng,Zhang Boming.Overview of application and research on advanced composite grid structures[J].Acta Aeronautica et Astronautica Sinica,2007,28(2):419-424 (in Chinese)
    [4]
    Labossiere P,Neal K W.Macroscopic failure criteria for fiber-reinforced composite materials[J].Solid Mech Arch,1987,12(2):65-95
    [5]
    Hashin Z.Failure criteria for unidirectional fiber composites[J].Journal of Applied Mechanics,1980,47(2):329-334
    [6]
    Puck A,Schurmann H.Failure analysis of FRP laminates by means of physically based phenomenological models [J].Comp Sci & Tech,2002,62(12/13):1633-1662
    [7]
    Liu K S,Tsai S W.A progressive quadratic failure criterion of a laminate[J].Comp Sci & Tech,1998,58(7):1023-1032
    [8]
    Schulte K.World wide failure exercise on failure prediction in composites[J].Comp Sci & Tech,2002,62(12/13):1479
    [9]
    Czichon S,Zimmermann K,Middendorf P,et al.Three-dimensional stress and progressive failure analysis of ultra thick laminates and experimental validation [J].Composite Structures,2011,93(5):1394-1403
    [10]
    MSC.Marc 2010 Volume A:theory and user information.MSC Software,2010
    [11]
    黄争鸣,张华山.纤维增强复合材料强度理论的研究现状与发展趋势—"破坏分析奥运会"评估综述[J].力学进展,2007,37(1):80-98
    Huang Zhengming,Zhang Huashan.Current status and future trend of researches on the strength of fiber-reinforced composites—a summary of the results from a "failure olympics" [J].Advances in Mechanics,2007,37(1):80-98 (in Chinese)
    [12]
    Zinoviev P,Grigoriev S V,Labedeva O V,et al.The strength of multilayered composites under plane stress state[J].Comp Sci & Tech,1998,58(7):1209-1223
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views(3161) PDF downloads(593) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return