Low velocity impact of combination Kevlar/carbon fiber sandwich composites

被引:225
作者
Gustin, J [1 ]
Joneson, A [1 ]
Mahinfalah, M [1 ]
Stone, J [1 ]
机构
[1] N Dakota State Univ, Dept Mech Engn & Appl Mech, Fargo, ND 58105 USA
基金
美国国家航空航天局; 美国国家科学基金会;
关键词
sandwich composite; hybrid; carbon fiber; Kevlar; low velocity impact;
D O I
10.1016/j.compstruct.2004.07.020
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Impact, compression after impact, and tensile stiffness properties of carbon fiber and Kevlar combination sandwich composites were investigated in this study. The different samples consisted of impact-side facesheets having different combinations of carbon fiber/Kevlar and carbon fiber/hybrid. The bottom facesheets remained entirely carbon fiber to maintain the high overall flexural stiffness of the sandwich composite. The focus of this research was to determine if any improvement in impact properties existed as a result of replacing the impact-side facesheet layers of carbon fiber with Kevlar or hybrid. Impact tests were conducted on different sample types to obtain information about absorbed energy and maximum impact force. Also, compression after impact tests were conducted to determine the reduction in compressive strength when comparing impacted to non-impacted samples. The elastic moduli of carbon fiber, Kevlar, and hybrid were determined from tensile testing. This data was used to characterize the reduction in stiffness from replacing carbon fiber layers with the Kevlar or hybrid layers. The experimental data in its entirety helps define the benefits and disadvantages of replacing carbon fiber layers with Kevlar or hybrid. (c) 2004 Elsevier Ltd. All rights reserved.
引用
收藏
页码:396 / 406
页数:11
相关论文
共 25 条
[1]  
Abrate S., 1994, APPL MECH REV, V47, P517
[2]   ANALYSIS OF IMPACT BEHAVIOR OF HYBRID COMPOSITE MATERIALS [J].
ADAMS, DF ;
MILLER, AK .
MATERIALS SCIENCE AND ENGINEERING, 1975, 19 (02) :245-260
[3]   Experimental investigation of low-velocity impact characteristics of sandwich composites [J].
Anderson, T ;
Madenci, E .
COMPOSITE STRUCTURES, 2000, 50 (03) :239-247
[4]  
[Anonymous], 1990, ASTM STANDARDS LIT R
[5]  
[Anonymous], P ASME AEROSPACE DIV
[6]  
Bunsell A. R., 1974, Composites, V5, P157, DOI 10.1016/0010-4361(74)90107-4
[7]   Structural analysis of the adhesive bond in a honeycomb core sandwich panel [J].
Burton, WS ;
Noor, AK .
FINITE ELEMENTS IN ANALYSIS AND DESIGN, 1997, 26 (03) :213-227
[8]   CHARACTERIZATION OF FACE SHEET CORE SHEAR FRACTURE OF COMPOSITE SANDWICH BEAMS [J].
CARLSSON, LA ;
SENDLEIN, LS ;
MERRY, SL .
JOURNAL OF COMPOSITE MATERIALS, 1991, 25 (01) :101-116
[9]   Fabrication, testing and analysis of composite sandwich beams [J].
Daniel, IM ;
Abot, JL .
COMPOSITES SCIENCE AND TECHNOLOGY, 2000, 60 (12-13) :2455-2463
[10]   Compression after impact strength of composite sandwich panels [J].
Davies, GAO ;
Hitchings, D ;
Besant, T ;
Clarke, A ;
Morgan, C .
COMPOSITE STRUCTURES, 2004, 63 (01) :1-9