Torsion of honeycomb FRP sandwich beams with a sinusoidal core configuration

被引:16
作者
Davalos, Julio F. [2 ]
Qiao, Pizhong [1 ]
Ramayanam, Vinod [2 ]
Shan, Luyang [1 ]
Robinson, Justin [2 ]
机构
[1] Washington State Univ, Dept Civil & Environm Engn, Pullman, WA 99164 USA
[2] W Virginia Univ, Dept Civil & Environm Engn, Morgantown, WV 26506 USA
关键词
Honeycomb FRP sandwich panel; Finite element modeling; Torsion; Effective stiffness; Shear modulus; Sinusoidal core; TRANSVERSE-SHEAR STIFFNESS; COMPOSITES;
D O I
10.1016/j.compstruct.2008.02.005
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A combined analytical, numerical and experimental investigation of honeycomb fiber-reinforced polymer (HFRP) sandwich beam samples subjected to torsion loads is conducted. The sandwich panel considered in this study has unique sinusoidal core geometry in the plane extending vertically between face laminates, and it has been used primarily as decking systems in highway bridges. Using a homogenization process and mechanics of materials approach, the equivalent core material properties for the honeycomb core geometry are found, and the material properties of face sheets are obtained by micro/macromechanics. Equivalent material properties of the core and face sheets are then used to evaluate effective torsional stiffness properties of HFRP panels. The torsional analysis includes the evaluation of core equivalent in-plane and out-of plane shear properties and panel apparent torsional stiffness properties. Finite element models using layered shell elements are used to correlate with the analytical and experimental results for HFRP beams samples in torsion. Two types of models are presented in the finite element simulation: an actual geometry model, where the core and face sheet geometry are defined by layer shell elements, and an equivalent plate model, for which the equivalent material properties of the core and face sheets are utilized. In order to verify the accuracy of the analytical and numerical predictions, several honeycomb sandwich beam samples with sinusoidal core waves oriented along the longitudinal or transverse or vertical directions and with different face sheet configurations are experimentally tested in torsion. The present analysis and characterization procedures can be used in design applications and optimization of honeycomb structures, and they can also be employed to verify or refine in-plane and out-of-plane shear equivalent material properties for the present and other honeycomb FRP panels. (C) 2008 Elsevier Ltd. All rights reserved.
引用
收藏
页码:97 / 111
页数:15
相关论文
共 28 条
[1]  
BROKAW JT, 1992, THESIS W VIRGINIA U
[2]  
Chamis C.C., 1984, TM83696 NASA
[3]   A solution including skin effect for stiffness and stress field of sandwich honeycomb core [J].
Chen, A ;
Davalos, JF .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2005, 42 (9-10) :2711-2739
[4]  
Christensen R.M., 1991, Mechanics of Composite Materials
[5]   Analysis and design of pultruded FRP shapes under bending [J].
Davalos, JF ;
Salim, HA ;
Qiao, PZ ;
LopezAnido, R ;
Barbero, EJ .
COMPOSITES PART B-ENGINEERING, 1996, 27 (3-4) :295-305
[6]  
Davalos JF, 2002, J COMPOS MATER, V36, P1151, DOI 10.1106/002199802023486
[7]   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
[8]  
DAVALOS JF, 2002, P 3 INT C COMP INFR
[9]  
DAVALOS JF, 1991, J MATER CIVIL ENG, V3, P125
[10]  
*HIBB KARLSS SOR I, 1998, ABAQUS STAND US MAN