Comparison of test configurations for determination of mode II interlaminar fracture toughness results from international collaborative test programme

被引：100

作者：

Davies, P

Sims, GD

Blackman, BRK

Brunner, AJ

Kageyama, K

Hojo, M

Tanaka, K

Murri, G

Rousseau, C

Gieseke, B

Martin, RH

机构：

[1] IFREMER, Ctr Brest, Technopole Brest Iroise, F-29280 Plouzane, France

[2] Natl Phys Lab, Teddington, Middx, England

[3] Univ London Imperial Coll Sci Technol & Med, London, England

[4] Eidgenossische Mat Prufungs & Forschungsanhalt, Dubendorf, Switzerland

[5] Univ Tokyo, Tokyo, Japan

[6] Kyoto Univ, Kyoto, Japan

[7] Toyama Prefectural Univ, Toyama, Japan

[8] NASA, Hampton, VA USA

[9] Bell Helicopters, Ft Worth, TX USA

[10] Cincinnati Testing Labs, Cincinnati, OH USA

[11] Mat Engn Res Lab Ltd, Hertford, England

来源：

PLASTICS RUBBER AND COMPOSITES | 1999年 / 28卷 / 09期

关键词：

D O I：

10.1179/146580199101540600

中图分类号：

TB33 [复合材料];

学科分类号：

摘要：

This paper presents a summary of the tests performed within a Versailles Project on Advanced Materials and Standards collaborative test programme to examine the measurement of mode II interlaminar fracture toughness using four different test methods based on end notched flexure, stabilised end notched flexure, end loaded split, and four point end notched flexure carbon fibre reinforced epoxy specimens. Tests were performed by members of the European Structural Integrity Society, the Japan Industrial Standards group, and the American Society for Testing and Materials. PRC/1546 (C) 1999 IoM Communications Ltd.

引用

页码：432 / 437

页数：6

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