A mechanics-of-materials model for predicting Young's modulus of damaged woven fabric composites involving three damage modes

被引:13
作者
Gao, XL
Li, K
Mall, S
机构
[1] Michigan Technol Univ, Dept Mech Engn Engn Mech, Houghton, MI 49931 USA
[2] USAF, Res Lab, Mat & Mfg Directorate, Wright Patterson AFB, OH 45433 USA
关键词
woven fabric composites; damage modeling; effective Young's modulus; energy method; homogenization theory; transverse yarn cracking; interface debonding; sliding with friction;
D O I
10.1016/S0020-7683(02)00603-0
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
An analytical model for damaged woven fabric composites is developed using the theory of advanced mechanics of materials. The analysis is based on Castigliano's second theorem and utilizes a damaged mosaic model laminate. Three damage modes (i.e., transverse yarn cracking, interface debonding, and sliding with friction at the interface) are considered. Only one independent interfacial parameter, the friction coefficient between warp and fill yarns, is introduced in the analysis. A closed-form formula is provided for estimating effective Young's modulus of damaged woven laminates. A parametric study of some 192 sample cases of two different composite systems (i.e., glass fiber/epoxy and ceramic fiber/ceramic) is conducted to illustrate the application and significance of the newly derived analytical model. The numerical values of the effective Young's modulus for the special case involving only transverse yarn cracking (the first damage mode) estimated by the present mechanics-of-materials model agree fairly well with those predicted by an elasticity-based model [Int. J. Solids Struct. 38 (2001) 855]. For the general case involving all three damage modes simultaneously, the present model reveals the complex nature of Young's modulus reduction in a quantitative manner, which differs from existing models. (C) 2002 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:981 / 999
页数:19
相关论文
共 19 条
[1]   CRACK BRIDGING MODELS FOR FIBER COMPOSITES WITH SLIP-DEPENDENT INTERFACES [J].
BAO, G ;
SONG, Y .
JOURNAL OF THE MECHANICS AND PHYSICS OF SOLIDS, 1993, 41 (09) :1425-1444
[2]  
BIRMAN V, 1999, AIAA991331
[3]  
Cook RobertD., 1999, ADV MECH MAT, V2nd
[4]   Damage accumulation in woven-fabric CFRP laminates under tensile loading: Part 1. Observations of damage accumulation [J].
Gao, F ;
Boniface, L ;
Ogin, SL ;
Smith, PA ;
Greaves, RP .
COMPOSITES SCIENCE AND TECHNOLOGY, 1999, 59 (01) :123-136
[5]  
Gao XL, 2000, J COMPOS TECH RES, V22, P60
[6]   Damaged mosaic laminate model of woven fabric composites with transverse yarn cracking and interface debonding [J].
Gao, XL ;
Li, K .
COMPOSITES SCIENCE AND TECHNOLOGY, 2002, 62 (14) :1821-1834
[7]   Variational solution for a cracked mosaic model of woven fabric composites [J].
Gao, XL ;
Mall, S .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2001, 38 (05) :855-874
[8]   FRACTURE OF FIBER-REINFORCED MATERIALS [J].
GAO, YC ;
MAI, YW ;
COTTERELL, B .
ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND PHYSIK, 1988, 39 (04) :550-572
[9]   ANALYSIS OF ORTHOGONALLY CRACKED LAMINATES UNDER TENSION [J].
HASHIN, Z .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1987, 54 (04) :872-879
[10]  
HASHIN Z, 1983, ASME, V50, P481