Low velocity impact response and energy absorption behavior on glass fibre reinforced epoxy composites

被引：0

作者：

SHEN YiOu ^{[1
]}

JIANG Bing ^{[1
]}

LI Yan ^{[1
,2
]}

JIANG Xu ^{[3
]}

机构：

[1] School of Aerospace Engineering and Applied Mechanics,Tongji University

[2] Key Laboratory of Advanced Civil Engineering Materials,Ministry of Education,Tongji University

[3] Department of Bridge Engineering,College of Civil Engineering,Tongji University

来源：

Science China(Technological Sciences) | 2017年 / 60卷 / 09期

关键词：

low velocity impact; geometry influencing factor; stacking sequence energy absorption; GFRP composites;

D O I：

暂无

中图分类号：

TQ327.1 [玻璃钢（玻璃增强塑料）];

学科分类号：

0805 ; 080502 ;

摘要：

A study was undertaken to determine the effects of several key geometry influencing factors on the impact response and energy absorption behavior of the glass fibre reinforced epoxy composites at low and intermediate energies.The energy-balance model was employed for characterising the energy absorption behavior and it depends strongly on the plate diameter and thickness.In addition,the damage vs.energy and force maps is effective in monitoring damage growth within the composite panel.The response of the composite laminate configurations characterized by different stacking sequences subjected to low velocity impacts with different impact energies have also been studied to estimate the damage initiation of composites.

引用

页码：1339 / 1346

页数：8

共 14 条

[1]

Delamination prediction in composite laminates under low-velocity impact[J] . Shuchang Long,Xiaohu Yao,Xiaoqing Zhang.Composite Structures . 2015

[2]

Computationally optimized formulation for the simulation of composite materials and delamination failures[J] . Composites Part B . 2010 (2)

[3]

Low-velocity impact damage on dispersed stacking sequence laminates. Part I: Experiments[J] . C.S. Lopes,O. Seresta,Y. Coquet,Z. Gürdal,P.P. Camanho,B. Thuis.Composites Science and Technology . 2009 (7)

[4]

Geometrical effects in the low velocity impact response of GFRP[J] . W.J. Cantwell.Composites Science and Technology . 2006 (9)

[5]

Prediction of low velocity impact damage in carbon–epoxy laminates[J] . M.F.S.F. de Moura,A.T. Marques.Composites Part A . 2002 (3)

[6]

A comparison of the predictive capabilities of current failure theories for composite laminates, judged against experimental evidence[J] . M.J Hinton,A.S Kaddour,P.D Soden.Composites Science and Technology . 2002 (12)

[7] Delamination threshold loads for low velocity impact on composite laminates [J].

Schoeppner, GA ;

Abrate, S .

COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2000, 31 (09) :903-915

[8] Influence of material thickness on the response of carbon-fabric/epoxy panels to low velocity impact [J].

Caprino, G ;

Lopresto, V ;

Scarponi, C ;

Briotti, G .

COMPOSITES SCIENCE AND TECHNOLOGY, 1999, 59 (15) :2279-2286

[9]

Effects of stacking sequence on the impact resistance in composite laminates. Part 2: prediction method[J] . Edgar Fuoss,Paul V. Straznicky,Cheung Poon.Composite Structures . 1998 (2)

[10]

Effects of stacking sequence on the impact resistance in composite laminates — Part 1: parametric study[J] . Edgar Fuoss,Paul V. Straznicky,Cheung Poon.Composite Structures . 1998 (1)

← 1 2 →