Identification of impact damage in CRRP laminates using the NDT approach
Identification of impact damage in CRRP laminates using the NDT approach
The motivation for this work is to identify impact damage in structures made from composite material. The composite material chosen for this research was Carbon Fibre Reinforced Polymer (CFRP) prepreg with a MTM57 epoxy resin system with CF2900 fabric. This material was fabricated to produce laminated plate specimens of 250 mm × 150 mm with 11, 12 and 13 layers of thickness. PZT sensors were placed at three different points on each of the plate specimens to record the responses from impact events. The impact test was performed using an instrumented drop test rig and the impact energies were set to range from 2.61 J to 41.72 J. All the signals captured from the impact test were recorded using a LMS data acquisition system and the impacted plate specimens were later examined using X-rays to evaluate the damage area. The correlation between the damage area in terms of the impact energy and the force detected is presented and discussed.
Sultan, M.T.H.
488c3ab1-e888-4001-97cd-ce2cd9355044
Worden, K.
07522936-fd47-4df2-b75e-c3d297d104b3
Dulieu-Barton, J.M.
9e35bebb-2185-4d16-a1bc-bb8f20e06632
Staszewski, W.J
f459ac15-5bb9-4604-9251-5d5d5af49e4c
Hodzic, A.
709e3105-f949-4c33-a476-a39d00778fe0
Pierce, S.G.
9b618edd-6d5c-42ac-9e0c-f285ba75daa2
2009
Sultan, M.T.H.
488c3ab1-e888-4001-97cd-ce2cd9355044
Worden, K.
07522936-fd47-4df2-b75e-c3d297d104b3
Dulieu-Barton, J.M.
9e35bebb-2185-4d16-a1bc-bb8f20e06632
Staszewski, W.J
f459ac15-5bb9-4604-9251-5d5d5af49e4c
Hodzic, A.
709e3105-f949-4c33-a476-a39d00778fe0
Pierce, S.G.
9b618edd-6d5c-42ac-9e0c-f285ba75daa2
Sultan, M.T.H., Worden, K., Dulieu-Barton, J.M., Staszewski, W.J, Hodzic, A. and Pierce, S.G.
(2009)
Identification of impact damage in CRRP laminates using the NDT approach.
AEROTECH III: Advances in Aerospace Engineering, Kuala Lumpar, Malaysia.
18 - 19 Nov 2009.
6 pp
.
Record type:
Conference or Workshop Item
(Paper)
Abstract
The motivation for this work is to identify impact damage in structures made from composite material. The composite material chosen for this research was Carbon Fibre Reinforced Polymer (CFRP) prepreg with a MTM57 epoxy resin system with CF2900 fabric. This material was fabricated to produce laminated plate specimens of 250 mm × 150 mm with 11, 12 and 13 layers of thickness. PZT sensors were placed at three different points on each of the plate specimens to record the responses from impact events. The impact test was performed using an instrumented drop test rig and the impact energies were set to range from 2.61 J to 41.72 J. All the signals captured from the impact test were recorded using a LMS data acquisition system and the impacted plate specimens were later examined using X-rays to evaluate the damage area. The correlation between the damage area in terms of the impact energy and the force detected is presented and discussed.
Text
Aerotech_III_KW.doc
- Other
More information
Published date: 2009
Venue - Dates:
AEROTECH III: Advances in Aerospace Engineering, Kuala Lumpar, Malaysia, 2009-11-18 - 2009-11-19
Organisations:
Fluid Structure Interactions Group
Identifiers
Local EPrints ID: 71819
URI: http://eprints.soton.ac.uk/id/eprint/71819
PURE UUID: 72493e04-50df-4551-a764-4f373d9b9648
Catalogue record
Date deposited: 05 Jan 2010
Last modified: 13 Mar 2024 20:46
Export record
Contributors
Author:
M.T.H. Sultan
Author:
K. Worden
Author:
W.J Staszewski
Author:
A. Hodzic
Author:
S.G. Pierce
Download statistics
Downloads from ePrints over the past year. Other digital versions may also be available to download e.g. from the publisher's website.
View more statistics