Energy absorption in composite laminates under impact loading

被引：89

作者：

Quaresimin, Marino ^{[1
]}

Ricotta, Mauro ^{[2
]}

Martello, Livio ^{[1
]}

Mian, Stefano ^{[1
]}

机构：

[1] Univ Padua, Dept Management & Engn, I-36100 Vicenza, Italy

[2] Univ Padua, Dept Ind Engn, I-35131 Padua, Italy

来源：

COMPOSITES PART B-ENGINEERING | 2013年 / 44卷 / 01期

关键词：

Laminates; Impact behaviour; Damage mechanics; Radiography; Energy absorption; LOW-VELOCITY IMPACT; DELAMINATION; PREDICTION; FAILURE; PLATES; BEHAVIOR; PANELS; INDENTATION; PENETRATION; THICKNESS;

D O I：

10.1016/j.compositesb.2012.06.020

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

The impact behaviour of composite laminates under low velocity impact load is investigated by considering the influence of stacking sequence and laminate thickness in terms of contact loads, absorbed energy and delamination extent. After a detailed analysis of impact induced damage evolution, a new methodology for the assessment of the energy absorption capability of composite laminates is proposed. The new approach allows the definition of an empirical master curve suitable to summarise the impact data independently of material system, laminate thickness and lay-up. (C) 2012 Elsevier Ltd. All rights reserved.

引用

页码：133 / 140

页数：8

共 30 条

[1]

[Anonymous], THEORY PLATES SHELL

[2] Impact behaviour of quasi-isotropic graphite-peek laminates [J].

Aymerich, F ;

Bucchioni, A ;

Priolo, P .

EXPERIMENTAL TECHNIQUES AND DESIGN IN COMPOSITE MATERIALS 3, 1998, 144 :63-73

[3]

Aymerich F, 2004, P ICEM12 12 INT C EX

[4]

Aymerich F, 2002, P EXP TECH DES COMP, P4

[5] Influence of the laminate thickness in low velocity impact behavior of composite material plate [J].

Belingardi, G ;

Vadori, R .

COMPOSITE STRUCTURES, 2003, 61 (1-2) :27-38

[6] Low velocity impact tests of laminate glass-fiber-epoxy matrix composite material plates [J].

Belingardi, G ;

Vadori, R .

INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2002, 27 (02) :213-229

[7] IMPACT PERFORATION OF CARBON-FIBER REINFORCED PLASTIC [J].

CANTWELL, WJ ;

MORTON, J .

COMPOSITES SCIENCE AND TECHNOLOGY, 1990, 38 (02) :119-141

[8] THE INFLUENCE OF VARYING PROJECTILE MASS ON THE IMPACT RESPONSE OF CFRP [J].

CANTWELL, WJ ;

MORTON, J .

COMPOSITE STRUCTURES, 1989, 13 (02) :101-114

[9] 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

[10] The significance of indentation in the inspection of carbon fibre-reinforced plastic panels damaged by low-velocity impact [J].

Caprino, G ;

Lopresto, V .

COMPOSITES SCIENCE AND TECHNOLOGY, 2000, 60 (07) :1003-1012

← 1 2 3 →