Effect of temperature on low velocity impact damage and post-impact flexural strength of cfrp assessed using ultrasonic c-scan and micro-focus computed tomography
Effect of temperature on low velocity impact damage and post-impact flexural strength of cfrp assessed using ultrasonic c-scan and micro-focus computed tomography
The effect of temperature on the low velocity impact resistance properties and on the post-impact flexural performance of CFRP laminates were studied. With this aim, 150x75 mm cross-ply carbon fibre/epoxy laminates with a [0/90/90/0]2s layup, therefore with a total of sixteen layers, were impacted at ambient temperature (30°C) and at elevated temperatures (55, 75 and 90?C) at a velocity of 2m/s using a drop weight impact tower. This was followed by flexural tests carried out at ambient temperature using a three-point bending rig. Damage assessment of impact and post-impact behaviour were carried out using ultrasonic C-scan and microfocus X-ray computed tomography (?CT). Interrupted flexural tests using ?CT allowed delamination propagation to be observed. In general, lower projected damage was observed at elevated temperatures, which resulted also in a possible hindrance to delamination and shear cracks propagation during impact and in a greater amount of retained flexural strength after impact.
A. carbon fibres, B. impact behaviour, B. fracture, D. non-destructive testing, temperature effect
1- 22
Suvarna, R.
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Arumugam, V.
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Bull, D.J.
3569ba02-89de-4398-a14d-02c3f9b4eab2
Chambers, A.R.
74fa9b7e-6362-478e-a038-15f2828c5446
Santulli, C.
ec0be24d-db9f-46a6-9f41-1b89d7529212
Suvarna, R.
cb5642e1-fb5d-4f12-9d0f-ebe7d6856a18
Arumugam, V.
d42b6b9f-19e6-48b5-adde-8d271dde2eb9
Bull, D.J.
3569ba02-89de-4398-a14d-02c3f9b4eab2
Chambers, A.R.
74fa9b7e-6362-478e-a038-15f2828c5446
Santulli, C.
ec0be24d-db9f-46a6-9f41-1b89d7529212
Suvarna, R., Arumugam, V., Bull, D.J., Chambers, A.R. and Santulli, C.
(2014)
Effect of temperature on low velocity impact damage and post-impact flexural strength of cfrp assessed using ultrasonic c-scan and micro-focus computed tomography.
Composites Part B: Engineering, .
(doi:10.1016/j.compositesb.2014.04.028).
Abstract
The effect of temperature on the low velocity impact resistance properties and on the post-impact flexural performance of CFRP laminates were studied. With this aim, 150x75 mm cross-ply carbon fibre/epoxy laminates with a [0/90/90/0]2s layup, therefore with a total of sixteen layers, were impacted at ambient temperature (30°C) and at elevated temperatures (55, 75 and 90?C) at a velocity of 2m/s using a drop weight impact tower. This was followed by flexural tests carried out at ambient temperature using a three-point bending rig. Damage assessment of impact and post-impact behaviour were carried out using ultrasonic C-scan and microfocus X-ray computed tomography (?CT). Interrupted flexural tests using ?CT allowed delamination propagation to be observed. In general, lower projected damage was observed at elevated temperatures, which resulted also in a possible hindrance to delamination and shear cracks propagation during impact and in a greater amount of retained flexural strength after impact.
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e-pub ahead of print date: 10 May 2014
Keywords:
A. carbon fibres, B. impact behaviour, B. fracture, D. non-destructive testing, temperature effect
Organisations:
Engineering Science Unit
Identifiers
Local EPrints ID: 364957
URI: http://eprints.soton.ac.uk/id/eprint/364957
ISSN: 1359-8368
PURE UUID: 7cbc5052-543a-4f37-9261-3c78b68fd405
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Date deposited: 16 May 2014 13:23
Last modified: 14 Mar 2024 16:44
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Author:
R. Suvarna
Author:
V. Arumugam
Author:
A.R. Chambers
Author:
C. Santulli
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