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Fatigue damage mechanics of notched graphite: epoxy laminates

Fatigue damage mechanics of notched graphite: epoxy laminates
Fatigue damage mechanics of notched graphite: epoxy laminates
A modeling approach is presented that recognizes that the residual properties of composite laminates after any form of loading depend on the damage state. Therefore, in the case of cyclic loading, it is necessary to first derive a damage growth law and then relate the residual properties to the accumulated damage
fiber reinforced composite laminates, damage, fatigue (materials) growth law, strain energy release rate, toughness, finite element method, residual strength, weibull statistics, composite materials, fracture
0803114192
596-616
ASTM International
Spearing, S.M.
9e56a7b3-e0e8-47b1-a6b4-db676ed3c17a
Beaumont, P.W.R.
985e59e0-5e69-4091-b7ae-68a4bc7c34ad
Ashby, M.F.
b65c202a-5998-4b80-bb6b-f2ad2d644f58
Spearing, S.M.
9e56a7b3-e0e8-47b1-a6b4-db676ed3c17a
Beaumont, P.W.R.
985e59e0-5e69-4091-b7ae-68a4bc7c34ad
Ashby, M.F.
b65c202a-5998-4b80-bb6b-f2ad2d644f58

Spearing, S.M., Beaumont, P.W.R. and Ashby, M.F. (1991) Fatigue damage mechanics of notched graphite: epoxy laminates. In, Composite Materials: Fatigue and Fracture. Third Symposium on Composite Materials: Fatigue and Fracture (06/11/89 - 07/11/89) Ann Arbor, USA. ASTM International, pp. 596-616. (doi:10.1520/STP17739S).

Record type: Book Section

Abstract

A modeling approach is presented that recognizes that the residual properties of composite laminates after any form of loading depend on the damage state. Therefore, in the case of cyclic loading, it is necessary to first derive a damage growth law and then relate the residual properties to the accumulated damage

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More information

Published date: 1991
Additional Information: STP1110
Venue - Dates: Third Symposium on Composite Materials: Fatigue and Fracture, Florida, USA, 1989-11-06 - 1989-11-07
Keywords: fiber reinforced composite laminates, damage, fatigue (materials) growth law, strain energy release rate, toughness, finite element method, residual strength, weibull statistics, composite materials, fracture

Identifiers

Local EPrints ID: 22851
URI: http://eprints.soton.ac.uk/id/eprint/22851
ISBN: 0803114192
PURE UUID: c64fb269-4ba1-40b4-8e0b-d7c17b642017
ORCID for S.M. Spearing: ORCID iD orcid.org/0000-0002-3059-2014

Catalogue record

Date deposited: 13 Feb 2007
Last modified: 16 Mar 2024 03:37

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Contributors

Author: S.M. Spearing ORCID iD
Author: P.W.R. Beaumont
Author: M.F. Ashby

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