Symmetrical Facing Wrinkling of Composite Sandwich Panels

被引:18
|
作者
Lopatin, A. V. [2 ]
Morozov, E. V. [1 ]
机构
[1] Univ New S Wales, Univ Coll Australian Def Force Acad, Sch Aerosp Civil & Mech Engn, Canberra, ACT, Australia
[2] Siberian State Aerosp Univ, Dept Aerosp Engn, Krasnoyarsk, Russia
关键词
sandwich panel; wrinkling; composite facings; orthotropic core;
D O I
10.1177/1099636208097196
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The article presents the solution of symmetrical face sheet wrinkling problem for sandwich panel with composite facings and an orthotropic core. The new model is proposed for elastic core that takes into account compressive and shear stiffnesses as well as nonlinear change of transverse displacement over the core thickness at wrinkling. The governing buckling equation is derived using energy method. Analysis of cylindrical face wrinkling is performed for sandwich strips subjected to compressive loads applied to the two opposite simply supported edges. The effects of elastic and geometric parameters on the critical buckling stresses and wrinkling waves' formation are examined.
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页码:475 / 497
页数:23
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