FAILURE ENVELOPES FOR NOTCHED CSM LAMINATES UNDER BIAXIAL LOADING

Citation
Ws. Arnold et al., FAILURE ENVELOPES FOR NOTCHED CSM LAMINATES UNDER BIAXIAL LOADING, Composites, 26(11), 1995, pp. 739-747
Citations number
16
Categorie Soggetti
Materials Sciences, Composites
Journal title
ISSN journal
00104361
Volume
26
Issue
11
Year of publication
1995
Pages
739 - 747
Database
ISI
SICI code
0010-4361(1995)26:11<739:FEFNCL>2.0.ZU;2-R
Abstract
The failure strength and characteristics of plain and notched E-glass chopped strand mat (CSM) reinforced polyester laminates, subject to un iaxial and biaxial loading, are investigated. Flat plate square specim ens are tested in a novel, specially designed test rig which enables i ndependent tension/tension, tension/compression and compression/compre ssion testing in all stress quadrants. The influence of altering the l oading history on the failure strength is discussed. Biaxial failure e nvelopes are presented for plain specimens and for notched specimens, i.e. D/W = 0.27, 0.214, 0.178, 0.07. Results for the plain specimens a re compared with the maximum stress, maximum strain, maximum shear str ess and the quadratic interactive stress criterion. A finite element a nalysis is performed to predict the residual strength of the notched s pecimens.