On the prediction of effective material properties of cellular hexagonal honeycomb core

被引:17
作者
Goswami, S [1 ]
机构
[1] German Aerosp Ctr DLR Stuttgart, Inst Struct & Design, D-70569 Stuttgart, Germany
关键词
honeycomb; hexagonal; unit-cell; effective properties; cellular structure;
D O I
10.1177/0731684405060567
中图分类号
TB33 [复合材料];
学科分类号
摘要
Analytical expressions for the effective elastic properties of cellular hexagonal honeycomb core have been presented in this study. The elemental beam theory has been adopted for each component inside the 'unit-cell' to arrive at the different expressions for effective properties utilizing the strain energy concept. The length of the diagonal struts, vertical struts, and included angle, as well as the thickness of the struts have been kept as variable, so various forms of hexagonal honeycomb cellular structures can be investigated in this approach. Other conventional finite element approaches and numerical homogenization methods are rather time consuming to predict effective properties. Moreover, a change in basic cell configuration (i.e., depth) requires a complete new meshing and analysis. In comparison, the analytical approach presented here is simple and computes the effective properties in a fraction of the time that is required for FE analysis with a minimum change in the input file. The proper implementation of this method embedded in large quasi-static or impact dynamic simulations (where part of the structure could be modeled with detailed finite element mesh for cellular core that may initiate damage, and rest could be modeled with a single solid layer of equivalent material properties) would give high computational advantage, which is essential in large-scale aerospace modeling and simulation environment.
引用
收藏
页码:393 / 405
页数:13
相关论文
共 17 条
[1]  
Albracht F, 1996, COMPUTER AIDED DESIGN IN COMPOSITE MATERIAL TECHNOLOGY V, P81
[2]  
Allen HG, 1969, Analysis and design of structural sandwich panels, V1st
[3]   The in-plane stiffnesses of a honeycomb core including the thickness effect [J].
Becker, W .
ARCHIVE OF APPLIED MECHANICS, 1998, 68 (05) :334-341
[4]  
Bourgeois S, 1998, MECHANICS OF SANDWICH STRUCTURES, P131
[5]   Assessment of continuum models for sandwich panel honeycomb cores [J].
Burton, WS ;
Noor, AK .
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 1997, 145 (3-4) :341-360
[6]  
CHAMIS CC, 1988, J COMPOS TECH RES, V10, P93, DOI 10.1520/CTR10135J
[7]   AEROGELS - HIGHLY TENUOUS SOLIDS WITH FASCINATING PROPERTIES [J].
FRICKE, J .
JOURNAL OF NON-CRYSTALLINE SOLIDS, 1988, 100 (1-3) :169-173
[8]  
Gere J.M., 1991, MECH MATER, V3rd SI, DOI DOI 10.1007/978-1-4899-3124-5
[9]   A FINITE-ELEMENT STUDY OF THE TRANSVERSE-SHEAR IN HONEYCOMB-CORES [J].
GREDIAC, M .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 1993, 30 (13) :1777-1788
[10]  
Jones R., 2018, Mechanics of composite materials