Volume 41 Issue 3
Mar.  2015
Turn off MathJax
Article Contents
XU Yuanming, LI Songze. Approximate calculation method of buckling load on integral sub-stiffened panel[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(3): 369-374. doi: 10.13700/j.bh.1001-5965.2014.0240(in Chinese)
Citation: XU Yuanming, LI Songze. Approximate calculation method of buckling load on integral sub-stiffened panel[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(3): 369-374. doi: 10.13700/j.bh.1001-5965.2014.0240(in Chinese)

Approximate calculation method of buckling load on integral sub-stiffened panel

doi: 10.13700/j.bh.1001-5965.2014.0240
  • Received Date: 30 Apr 2014
  • Publish Date: 20 Mar 2015
  • To calculate the integral sub-stiffened panel buckling load in the preliminary design stage quickly, a simplifying approximate calculation method based on some reasonable assumptions was proposed. The perfect rectangular sub-stiffened panel simply supported on four sizes was used as investigation object. This structure has 3 instability forms, and the corresponding buckling loads were obtained by using the traditional stiffened plate theory. The minimum buckling load of the 3 instability forms was regarded as the approximate buckling load of the integral sub-stiffened panel. The buckling linear perturbation step method of ABAQUS was used to calculate the two sets of finite element (FE) models respectively: one set was used to validate the accuracies of the theoretical formulas for failure modes, and the other set was integral sub-stiffened panel finite element models which were used to verify the applicability of proposed calculation method of sub-stiffened panel buckling load. Only two load cases were considered in the research above: the longitudinal compression load and the combination of compression and shear load. The results indicate that the theoretical approximate calculation method can calculate the buckling load of sub-stiffened panel, which count for engineering application to some extent.

     

  • loading
  • [1]
    Mulani S B, Slemp W C H,Kapania R K.EBF3PanelOpt:an optimization framework for curvilinear blade-stiffened panels[J].Thin-Walled Structures,2013,63:13-26.
    [2]
    Murphy A, Quinn D,Mawhinney P,et al.Tailoring static strength performance of metallic stiffened panels by selective local sub-stiffening[C]//Proceedings of the Forty Seventh AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference.Reston:AIAA,2006:1-4.
    [3]
    Farley G L. Selective reinforcement to enhance the structural performance of metallic compression panels[C]//45th AIAA/ASME/ASCE/AHS/ASCSDM Conference.Reston:AIAA,2004.
    [4]
    Bushnell D, Rankin C.Optimum design of stiffened panels with substiffeners[C]//46th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference.Reston:AIAA,2005:1-54.
    [5]
    Watson A, Featherston C A,Kennedy D.Optimization of postbuckled stiffened panels with multiple stiffener sizes[C]//Proceedings of the Forty Eighth AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference.Reston: AIAA,2007:23-26.
    [6]
    Quinn D, Murphy A,Mcewan W,et al.Non-prismatic sub-stiffening for stiffened panel plates-stability behaviour and performance gains[J].Thin-Walled Structures,2010,48(6):401-413.
    [7]
    Quinn D, Murphy A,Mcewan W,et al.Stiffened panel stability behaviour and performance gains with plate prismatic sub-stiffening[J].Thin-Walled Structures,2009,47(12):1457-1468.
    [8]
    Özakça M, Murphy A,Van der Veen S.Buckling and post-buckling of sub-stiffened or locally tailored aluminium panels[C]//25th International Congress of the Aeronautical Sciences.Bonn:ICAS,2006:3-8.
    [9]
    Khvyiuzov A, Xu Y M.Initial buckling of compressed rectangular panels with variable stiffener sizes[J].Advanced Materials Research,2014,915:150-164.
    [10]
    王博,田阔, 郝鹏,等.多级加筋板结构承载性能与缺陷敏感度研究[J].固体火箭技术,2014,37(3):408-412. Wang B,Tian K,Hao P,et al.Load-carrying capacity and imperfection-sensitivity analysis of hierarchical stiffened panels[J].Journal of Solid Rocket Technology,2014,37(3):408-412(in Chinese).
    [11]
    肖明心. 板的稳定理论[M].1版.成都:四川科学技术出版社,1993:61-87. Xiao M X.Stability theory of plate[M].1st ed.Chengdu: Sichuan Science and Technology Press,1993:61-87(in Chinese).
    [12]
    Timoshenko S. Theory of elastic stability[M].2nd ed.Dover:Dover Publications Inc,2009:348-356.
    [13]
    Bleich F. Buckling strength of metal structures[M].New York:McGraw-Hill,1952:349-385.
    [14]
    Lynch C, Murphy A,Price M,et al.The computational post buckling analysis of fuselage stiffened panels loaded in compression[J].Thin-Walled Structures,2004,42(10):1445-1464.
    [15]
    Murphy A, Price M,Lynch C,et al.The computational post-buckling analysis of fuselage stiffened panels loaded in shear[J].Thin-Walled Structures,2005,43(9):1455-1474.
  • 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(1308) PDF downloads(55114) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return