Experimental and numerical failure analysis of bolted joints in CFRP wovenlaminates

Citation
N. Andreasson et al., Experimental and numerical failure analysis of bolted joints in CFRP wovenlaminates, AERONAUT J, 102(1018), 1998, pp. 445-450
Citations number
21
Categorie Soggetti
Aereospace Engineering
Journal title
AERONAUTICAL JOURNAL
ISSN journal
00019240 → ACNP
Volume
102
Issue
1018
Year of publication
1998
Pages
445 - 450
Database
ISI
SICI code
0001-9240(199810/12)102:1018<445:EANFAO>2.0.ZU;2-A
Abstract
The purpose of a joint is to transfer load between the two parts beings joi ned. As a result of this load transfer there will be a stress variation in the components in the joint region, as well as stresses in the joining medi um (fasteners or adhesive). In this work, the stress results of a two-dimen sional finite element (FE) analysis are used to understand failure modes of a bolted joint in low-temperature cure carbon fibre reinforced plastic (CF RP) woven laminates loaded in tension, and to predict the bearing strength. Good agreement with experimentally observed damage modes and strengths is achieved with, in some cases, a difference of less than 10%.