Dynamic wrinkling in sandwich beams

被引:8
作者
Birman, V [1 ]
机构
[1] Univ Missouri, Engn Educ Ctr, St Louis, MO 63121 USA
关键词
sandwich beams and panels;
D O I
10.1016/j.compositesb.2003.08.012
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Facings of sandwich structures employed in typical applications are often subject to parametric periodic loading. Such loading can cause local dynamic instability of the facings, i.e. large-amplitude small wavelength lateral vibrations. This phenomenon, called in the paper dynamic wrinkling, may result in fatigue damage or immediate failure. The problem of dynamic wrinkling of the facings is analyzed in the present paper for sandwich beams and for large aspect ratio wide panels that vibrate forming a cylindrical surface. The solution is obtained for the case of a relatively thick or compliant core where the Winkler elastic foundation model of the core is applicable. In addition, the problem is formulated as an extension of the Plantema core model that may be preferable for thinner and stiffer cores. In addition, a new simplified elasticity model is introduced in the paper that is based on the assumption that both facings experience simultaneous and interactive dynamic wrinkling instability. Numerical results shown for the elastic foundation model include the criterion for the onset of dynamic wrinkling and the critical value of the damping coefficient of the facing that is sufficient to prevent such wrinkling. As follows from these results, dynamic wrinkling is unlikely in most engineering applications, except for the case in which the maximum stresses in the facing approach the static wrinkling value. (C) 2004 Elsevier Ltd. All rights reserved.
引用
收藏
页码:665 / 672
页数:8
相关论文
共 12 条
  • [1] Allen HG, 1969, Analysis and design of structural sandwich panels, V1st
  • [2] Analytical evaluation of damping in composite and sandwich structures
    Birman, V
    Byrd, LW
    [J]. AIAA JOURNAL, 2002, 40 (08) : 1638 - 1643
  • [3] BIRMAN V, 2004, IN PRESS J SANDWICH
  • [4] Bolotin V.V., 1964, DYNAMIC STABILITY EL
  • [5] FAGERBERG L, 2001, 200117 ROYAL I TECHN
  • [6] THE EVALUATION OF THEORETICAL CRITICAL COMPRESSION IN SANDWICH PLATES
    GOODIER, JN
    NEOU, IM
    [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1951, 18 (10): : 649 - &
  • [7] Gough G.S., 1940, J ROYAL AERONAUTICAL, V44, P12, DOI 10.1017/S036839310010495X
  • [8] THE BUCKLING OF SANDWICH-TYPE PANELS
    HOFF, NJ
    MAUTNER, SE
    [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1945, 12 (03): : 285 - 297
  • [9] KARDOMATEAS GA, 2003, P 6 INT C SANDW STRU, P142
  • [10] Plantema FJ, 1966, Sandwich construction: the bending and buckling of sandwich beams, plates, and shells