An investigation on the effect of a small mass impact on sandwich composite plates

被引：10

作者：

Christopherson, J ^{[1
]}

Mahinfalah, M ^{[1
]}

Jazar, GN ^{[1
]}

Aagaah, MR ^{[1
]}

机构：

[1] N Dakota State Univ, Dept Mech Engn & Appl Mech, Fargo, ND 58105 USA

来源：

COMPOSITE STRUCTURES | 2005年 / 67卷 / 03期

基金：

美国国家科学基金会; 美国国家航空航天局;

关键词：

sandwich composite; honeycomb structures; small mass impacts; carbon fiber;

D O I：

10.1016/j.compstruct.2004.07.013

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

This paper investigates the high strain rate response of polymer matrix sandwich composites utilizing foam-filled honeycomb cores by means of a small mass impact. The reinforcement fiber chosen for use in this paper is a simple weave carbon fiber. This paper also investigates the effects of utilizing different laminate configurations in Conjunction with investigation of the effectiveness of such laminate during impact loading. In an effort to ascertain more information about the impact situation, compression after impact tests are performed to determine the extent of the damage by observing the degradation of strength associated with the impact event. (C) 2004 Elsevier Ltd. All rights reserved.

引用

页码：299 / 306

页数：8

共 13 条

[1] Delamination criticality in slender compression-loaded composite panels [J].

Asp, LE ;

Nilsson, KF .

EXPERIMENTAL TECHNIQUES AND DESIGN IN COMPOSITE MATERIALS 5, 2002, 221-2 :3-15

[2] Effects of manufacturing techniques on the mechanical properties of composite laminates [J].

Carvelli, V ;

De Angelis, D ;

Poggi, C ;

Puoti, R .

EXPERIMENTAL TECHNIQUES AND DESIGN IN COMPOSITE MATERIALS 5, 2002, 221-2 :109-119

[3]

Fatt MSH, 2001, COMPOS STRUCT, V52, P353

[4]

Fatt MSH, 2001, COMPOS STRUCT, V52, P335

[5]

GUSTIN J, 2003, SEM ANN C EXP EXPT A

[6]

GUSTIN J, 2004, SEM INT C EXP EXPT A

[7] Compressive failure of carbon-foam sandwich composites with holes and/or partial delamination [J].

Kwon, YW ;

Yoon, SH ;

Sistare, PJ .

COMPOSITE STRUCTURES, 1997, 38 (1-4) :573-580

[8] An innovative technique for measuring the high strain rate response of sandwich composites [J].

Mahfuz, H ;

Al Mamun, W ;

Haque, A ;

Turner, S ;

Mohamed, H ;

Jeelani, S .

COMPOSITE STRUCTURES, 2000, 50 (03) :279-285

[9] Closed form prediction of peak load and delamination onset under small mass impact [J].

Olsson, R .

COMPOSITE STRUCTURES, 2003, 59 (03) :341-349

[10] Low velocity impact damage characteristics of Z-fiber reinforced sandwich panels - an experimental study [J].

Palazotto, AN ;

Gummadi, LNB ;

Vaidya, UK ;

Herup, EJ .

COMPOSITE STRUCTURES, 1998, 43 (04) :275-288

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