Improving energy dissipation and damage resistance of CFRP laminates using alumina nanoparticles

被引:14
作者
Almitani, K. H. [1 ]
Wagih, A. [2 ]
Melaibari, A. [1 ]
Eltaher, M. A. [1 ,2 ]
机构
[1] King Abdulaziz Univ, Fac Engn, Mech Engn Dept, Jeddah, Saudi Arabia
[2] Zagazig Univ, Fac Engn, Mech Design & Prod Dept, Zagazig, Egypt
关键词
Alumina nanoparticles; toughened composites; quasi-static indentation; C-scan; composite laminate; FILLED EPOXY-RESIN; INTRALAMINAR DAMAGE; CRACK-PROPAGATION; IMPACT RESPONSE; INDENTATION; SEQUENCE; COMPOSITES; FRACTURE;
D O I
10.1080/14658011.2019.1591795
中图分类号
TB33 [复合材料];
学科分类号
摘要
In this paper, the effect of a toughened epoxy matrix on the damage evolution, energy dissipation, and permanent indentation of composite laminates under out-of-plane (transverse) loading is presented experimentally. The epoxy matrix was toughened by 3% alumina nanoparticles with sizes less than 200nm. A quasi-static indentation test was exploited to characterise the damage modes and evaluate the dissipation of energy of the composite laminate. The dissipated energy was evaluated as the enclosed area between the loading and unloading curves, while the damage resistance was expressed as the number of delaminations and their size. The results showed that epoxy toughened by alumina nanoparticles, showed an improvement in the damage threshold load by 27.3% and higher ultimate load under indentation. Regarding the damage resistance, the toughened laminates showed lower number of delaminated interfaces and lower projected delamination area than untoughened laminates. This is due to the localised damage under the indenter, the matrix cracks at low indentation energy and fibre breakages occur at high indentation energy.
引用
收藏
页码:208 / 217
页数:10
相关论文
共 35 条
[1]   Experimental analysis of damage creation and permanent indentation on highly oriented plates [J].
Abdallah, Elias Abi ;
Bouvet, Christophe ;
Rivallant, Samuel ;
Broll, Bernhard ;
Barrau, Jean-Jacques .
COMPOSITES SCIENCE AND TECHNOLOGY, 2009, 69 (7-8) :1238-1245
[2]   Interaction of inter- and intralaminar damage in scaled quasi-static indentation tests: Part 1-Experiments [J].
Abisset, E. ;
Daghia, F. ;
Sun, X. C. ;
Wisnom, M. R. ;
Hallett, S. R. .
COMPOSITE STRUCTURES, 2016, 136 :712-726
[3]  
Abrate S., 1994, APPL MECH REV, V47, P517, DOI [10.1115/1.3111065, DOI 10.1115/1.3111065]
[4]   INTERLAMINAR SHEAR FRACTURE OF INTERLEAVED GRAPHITE EPOXY COMPOSITES [J].
AKSOY, A ;
CARLSSON, LA .
COMPOSITES SCIENCE AND TECHNOLOGY, 1992, 43 (01) :55-69
[5]  
[Anonymous], 2004, D626498 ASTM
[6]   The response of viscoelastic-frictionless bodies under normal impact [J].
Assie, A. E. ;
Eltaher, M. A. ;
Mahmoud, F. F. .
INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2010, 52 (03) :446-454
[7]  
Bailie JA., 1997, NAS119347 NASA NORTH
[8]   The role of reinforcement architecture on impact damage mechanisms and post-impact compression behaviour [J].
Bibo, GA ;
Hogg, PJ .
JOURNAL OF MATERIALS SCIENCE, 1996, 31 (05) :1115-1137
[9]  
Davies G, 1992, AGARD DEBONDING DELA, V28, P7
[10]   NUMERICAL MODELING OF IMPACT DAMAGE [J].
DAVIES, GAO ;
ZHANG, X ;
ZHOU, G ;
WATSON, S .
COMPOSITES, 1994, 25 (05) :342-350