An experimental characterization of the acoustic fatigue endurance of GLARE and comparison with that of CFRP
An experimental characterization of the acoustic fatigue endurance of GLARE and comparison with that of CFRP
GLARE is a new aerospace structural material composed of alternating, bonded layers of aluminium alloy and glass fibre reinforced plastic. The results of an experimental study are presented here concerning mechanical fatigue testing of GLARE structural specimens in conditions relevant to the acoustic fatigue problem.
Endurance testing of 35 GLARE Tee-coupons under simulated random acoustic loading has been carried out and resonance frequency, damping loss factor, and strain response of the specimens have been experimentally determined. CFRP specimens have also been tested to provide a benchmark against which to compare the properties of GLARE. FE analysis of the coupons has also been carried out to support the experimental work and the theoretical results have been compared with the experimental data.
Damage mechanisms have been observed and fatigue data established. Using these experimental data, surface strain versus number of cycles to failure curves have been established. In particular, this work has assessed the behaviour of GLARE in bending and has highlighted the importance of the lay-up sequence for the "fibre bridging effect" on crack propagation to be effective.
fatigue, acoustic fatigue, glare, cfrp, aircraft structures testing, coupon testing
455-470
Xiao, Y.
7ca8d021-0028-49f0-b6df-b2fefe95636b
White, R.G.
d67216d7-2691-4322-9dac-56b96add39e1
Aglietti, G.S.
e44d0dd4-0f71-4399-93d2-b802365cfb9e
2005
Xiao, Y.
7ca8d021-0028-49f0-b6df-b2fefe95636b
White, R.G.
d67216d7-2691-4322-9dac-56b96add39e1
Aglietti, G.S.
e44d0dd4-0f71-4399-93d2-b802365cfb9e
Xiao, Y., White, R.G. and Aglietti, G.S.
(2005)
An experimental characterization of the acoustic fatigue endurance of GLARE and comparison with that of CFRP.
Composite Structures, 68 (4), .
(doi:10.1016/j.compstruct.2004.04.011).
Abstract
GLARE is a new aerospace structural material composed of alternating, bonded layers of aluminium alloy and glass fibre reinforced plastic. The results of an experimental study are presented here concerning mechanical fatigue testing of GLARE structural specimens in conditions relevant to the acoustic fatigue problem.
Endurance testing of 35 GLARE Tee-coupons under simulated random acoustic loading has been carried out and resonance frequency, damping loss factor, and strain response of the specimens have been experimentally determined. CFRP specimens have also been tested to provide a benchmark against which to compare the properties of GLARE. FE analysis of the coupons has also been carried out to support the experimental work and the theoretical results have been compared with the experimental data.
Damage mechanisms have been observed and fatigue data established. Using these experimental data, surface strain versus number of cycles to failure curves have been established. In particular, this work has assessed the behaviour of GLARE in bending and has highlighted the importance of the lay-up sequence for the "fibre bridging effect" on crack propagation to be effective.
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Published date: 2005
Keywords:
fatigue, acoustic fatigue, glare, cfrp, aircraft structures testing, coupon testing
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Local EPrints ID: 23143
URI: http://eprints.soton.ac.uk/id/eprint/23143
ISSN: 0263-8223
PURE UUID: a96005ed-ebca-4b7d-82e4-7f34d3e75e85
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Date deposited: 15 Mar 2006
Last modified: 15 Mar 2024 06:44
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Author:
Y. Xiao
Author:
R.G. White
Author:
G.S. Aglietti
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