Transverse shear stiffness of composite honeycomb core with general configuration

被引:49
作者
Xu, XF
Qiao, PZ [1 ]
Davalos, JF
机构
[1] Univ Akron, Dept Civil Engn, Akron, OH 44325 USA
[2] W Virginia Univ, Dept Civil & Environm Engn, Morgantown, WV 26506 USA
来源
JOURNAL OF ENGINEERING MECHANICS-ASCE | 2001年 / 127卷 / 11期
关键词
Boundary conditions - Composite structures - Constraint theory - Elasticity - Optimization - Partial differential equations - Sandwich structures - Shear deformation - Stiffness - Thin walled structures;
D O I
10.1061/(ASCE)0733-9399(2001)127:11(1144)
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Based on the zeroth-order approximation of a two-scale asymptotic expansion, equivalent elastic shear coefficients of periodic structures can be evaluated via the solution of a local function tau (kl)(ij)(y), and the homogenization process reduces to solving the local function tau (kl)(ij)(y) by invoking local periodic boundary conditions. Then, effective transverse shear stiffness properties can be analytically predicted by reducing a local problem of a given unit cell into a 2D problem. In this paper, an analytical approach with a two-scale asymptotic homogenization technique is developed for evaluation of effective transverse shear stiffness of thin-walled honeycomb core structures with general configurations, and the governing 3D partial differential equations are solved with the assumptions of free warping constraints and constant variables through the core wall thickness. The explicit formulas for the effective transverse shear stiffness are presented for a general configuration of honeycomb core. A detailed study is given for three typical honeycomb cores consisting of sinusoidal, tubular, and hexagonal configurations, and their solutions are validated with existing equations and numerical analyses. The developed approach with certain modifications can be extended to other sandwich structures, and a summary of explicit solutions for the transverse shear stiffness of common honeycomb core configurations is provided. The lower bound solution provided in this study is a reliable approximation for engineering design and can be efficiently used for quick evaluation and optimization of general core configurations. The upper bound formula, based on the assumption of uniform shear deformation, is also given for comparison. Further, it is expected that with appropriate construction in the displacement field, the more accurate transverse stiffness can be analytically attained by taking into account the effect due to the face-sheet constraints.
引用
收藏
页码:1144 / 1151
页数:8
相关论文
共 11 条
[1]   Modeling and characterization of fiber-reinforced plastic honeycomb sandwich panels for highway bridge applications [J].
Davalos, JF ;
Qiao, PZ ;
Xu, XF ;
Robinson, J ;
Barth, KE .
COMPOSITE STRUCTURES, 2001, 52 (3-4) :441-452
[2]  
Gibson L., 1989, Advances in Polymer Technology, V9
[3]   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
[4]   Effective elastic properties of hexagonal and quadrilateral grid structures [J].
Hohe, J ;
Beschorner, C ;
Becker, W .
COMPOSITE STRUCTURES, 1999, 46 (01) :73-89
[5]  
Kalamkarov AL., 1992, Composite and Reinforced Elements of Construction
[6]  
Kelsey S., 1958, AIRCRAFT ENG, V30, P294, DOI [10.1108/eb033026, DOI 10.1108/EB033026]
[7]   ASYMPTOTIC HOMOGENIZATION OF ELASTIC COMPOSITE-MATERIALS WITH A REGULAR STRUCTURE [J].
MEGUID, SA ;
KALAMKAROV, AL .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 1994, 31 (03) :303-316
[8]  
Noor A., 1996, Appl. Mech. Rev., V49, P155, DOI [DOI 10.1115/1.3101923, 10.1115/1.3101923]
[9]  
Parton V.Z., 1993, ENG MECH COMPOSITE S
[10]   EFFECTIVE SHEAR MODULUS OF HONEYCOMB CELLULAR STRUCTURE [J].
PENZIEN, J ;
DIDRIKSSON, T .
AIAA JOURNAL, 1964, 2 (03) :531-535