Assessment of continuum models for sandwich panel honeycomb cores

被引:112
作者
Burton, WS [1 ]
Noor, AK [1 ]
机构
[1] UNIV VIRGINIA, NASA, LANGLEY RES CTR, CTR ADV COMPUTAT TECHNOL, HAMPTON, VA USA
基金
美国国家航空航天局;
关键词
D O I
10.1016/S0045-7825(96)01196-6
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Detailed finite element models are used for predicting the free-vibration response of infinitely long and rectangular sandwich panels. The panels considered have square-cell honeycomb core and simply supported edges. The sandwich core and face sheets are modeled by using three-dimensional solid elements and two-dimensional plate elements. The predictions of the finite element models are compared with those obtained by using higher-order sandwich theory for panels with the core replaced by an effective (equivalent) continuum. Three different approaches are used for estimating the effective material properties of the equivalent continuum layer.
引用
收藏
页码:341 / 360
页数:20
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