Experimental studies on fracture characterisation and energy absorption of GFRP composite box structures

被引:61
作者
Ghasemnejad, H. [1 ]
Blackman, B. R. K. [2 ]
Hadavinia, H. [1 ]
Sudall, B. [1 ]
机构
[1] Kingston Univ, Fac Engn, London, England
[2] Univ London Imperial Coll Sci Technol & Med, Dept Mech Engn, London, England
关键词
Interlaminar fracture toughness; Specific energy absorption; Fibre orientation; I INTERLAMINAR FRACTURE; MODE-I; CYLINDRICAL-SHELLS; POLYMER COMPOSITES; FIBER ORIENTATION; TUBES; TOUGHNESS; FAILURE;
D O I
10.1016/j.compstruct.2008.04.006
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Interlaminar fracture toughness of composite materials plays an important role in the specific energy absorption (SEA) characteristics of crushing composite materials. In this regard the effect of fibre orientation and stacking sequence on the composite crash box design is sought by studying their effects on the interlaminar fracture toughness. In order to achieve this, glass fibre/epoxy orientations of [+/- 60](10), [0(2)/+/- 45](5), [0/90](10) and [0/90](5s) were studied experimentally. Tensile, shear, double cantilever beam (DCB) and axial crush box specimens from different lay-ups were made and tested under quasi-static conditions to determine the mechanical properties, interlaminar fracture toughness (G(ic)) and SEA. It was shown that the interlaminar fracture toughness of glass fibre/epoxy affects the frond bending resistance due to the main central interwall crack in a progressive crushing failure and consequently SEA. A higher interlaminar fracture toughness between laminates will enhance the SEA in the axial crushing of the composite box. (C) 2008 Elsevier Ltd. All rights reserved.
引用
收藏
页码:253 / 261
页数:9
相关论文
共 31 条
[1]  
[Anonymous], 2002, ANN BOOK ASTM STAND
[2]  
Blackman BRK, 1998, ECF 12: FRACTURE FROM DEFECTS, VOLS. I-III, P1471
[3]  
*BRIT STAND I, 1998, 2747 BS EN ISO BRIT
[4]  
*BRIT STAND I, 1998, 14129 BS EN ISO BRIT
[5]  
*BSI, 2001, 150242001 BS EN ISO
[6]   POST-FAILURE ANALYSIS OF BOLTED COMPOSITE JOINTS IN TENSION OR SHEAR-OUT MODE FAILURE [J].
CHANG, FK ;
CHANG, KY .
JOURNAL OF COMPOSITE MATERIALS, 1987, 21 (09) :809-833
[7]   Delamination fracture of multidirectional carbon-fiber/epoxy composites under Mode I, Mode II and Mixed-Mode I/II loading [J].
Choi, NS ;
Kinloch, AJ ;
Williams, JG .
JOURNAL OF COMPOSITE MATERIALS, 1999, 33 (01) :73-100
[8]   Double cantilever beam testing of multidirectional laminates [J].
de Morais, AB .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2003, 34 (12) :1135-1142
[9]  
FAIRFULL AH, 1989, STRUCTURAL FAILURE, P255
[10]   CRUSHING CHARACTERISTICS OF CONTINUOUS FIBER-REINFORCED COMPOSITE TUBES [J].
FARLEY, GL ;
JONES, RM .
JOURNAL OF COMPOSITE MATERIALS, 1992, 26 (01) :37-50