Normal and oblique penetration of woven CFRP laminates by a high velocity steel sphere

被引:68
作者
Hazell, P. J. [1 ]
Kister, G. [1 ]
Stennett, C. [1 ]
Bourque, P. [1 ]
Cooper, G. [1 ]
机构
[1] Cranfield Univ, DCMT, Swindon SN6 8LA, Wilts, England
基金
英国工程与自然科学研究理事会;
关键词
carbon fibre; impact behaviour; delamination; damage mechanics;
D O I
10.1016/j.compositesa.2008.01.007
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In this research, two thicknesses of a woven CFRP laminate have been subjected to impact by a steel sphere in a velocity regime ranging from 170 to 374 m/s. Impact and penetration of targets at normal and oblique incidence were studied using high speed video. For the normal incidence targets at the higher velocities of impact, a conical mass of laminate was ejected ahead of the projectile. Furthermore, despite the energy transferred to the plate increasing with impact energy, the degree of delamination in the thicker targets decreased indicating a change in projectile penetration mechanism. Eventually, the degree of delamination in the thicker targets appeared to approach an asymptotic level whereas for the thinner targets the degree of delamination appeared constant regardless of impact energy. For oblique targets, more of the kinetic energy was transferred from the projectile when compared to the same thickness of target that had been subjected to a normal incidence impact. However, this was merely due to a geometrical effect. Further, thicker panels appeared to behave more efficiently by absorbing more kinetic energy per effective linear thickness at the lower impact energies where petalling is a dominant factor in the penetration. This advantage appeared to disappear as the impact energy was increased. (C) 2008 Elsevier Ltd. All rights reserved.
引用
收藏
页码:866 / 874
页数:9
相关论文
共 16 条
[1]  
*AIR FORC MAT LAB, 1970, CRYOG MAT DAT HDB, V1
[2]  
*ASTM, 2006, 317106 ASTM
[3]   COMPARISON OF THE LOW AND HIGH-VELOCITY IMPACT RESPONSE OF CFRP [J].
CANTWELL, WJ ;
MORTON, J .
COMPOSITES, 1989, 20 (06) :545-551
[4]   IMPACT PERFORATION OF CARBON-FIBER REINFORCED PLASTIC [J].
CANTWELL, WJ ;
MORTON, J .
COMPOSITES SCIENCE AND TECHNOLOGY, 1990, 38 (02) :119-141
[5]   THE IMPACT RESISTANCE OF COMPOSITE-MATERIALS - A REVIEW [J].
CANTWELL, WJ ;
MORTON, J .
COMPOSITES, 1991, 22 (05) :347-362
[6]   AN ASSESSMENT OF THE IMPACT PERFORMANCE OF CFRP REINFORCED WITH HIGH-STRAIN CARBON-FIBERS [J].
CANTWELL, WJ ;
CURTIS, PT ;
MORTON, J .
COMPOSITES SCIENCE AND TECHNOLOGY, 1986, 25 (02) :133-148
[7]   AN ASSESSMENT OF THE POTENTIAL OF WOVEN CARBON FIBER-REINFORCED PLASTICS FOR HIGH-PERFORMANCE APPLICATIONS [J].
CURTIS, PT ;
BISHOP, SM .
COMPOSITES, 1984, 15 (04) :259-265
[8]   High-resolution optical study of the impact of carbon-fibre reinforced polymers with different lay-ups [J].
Hammond, RI ;
Proud, WG ;
Goldrein, HT ;
Field, JE .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2004, 30 (01) :69-86
[9]   DYNAMIC PENETRATION OF GRAPHITE-EPOXY LAMINATES IMPACTED BY A BLUNT-ENDED PROJECTILE [J].
LEE, SWR ;
SUN, CT .
COMPOSITES SCIENCE AND TECHNOLOGY, 1993, 49 (04) :369-380
[10]   The effect of low temperatures on the intermediate and high velocity impact response of CFRPs [J].
López-Puente, J ;
Zaera, R ;
Navarro, C .
COMPOSITES PART B-ENGINEERING, 2002, 33 (08) :559-566