Flexural fatigue of carbon fibre-reinforced PEEK laminates

M. Buggy; G. Dillon

doi:10.1016/0010-4361(91)90318-B

Flexural fatigue of carbon fibre-reinforced PEEK laminates

M. Buggy, G. Dillon

Penn State Erie, The Behrend College

Research output: Contribution to journal › Article › peer-review

19 Scopus citations

Abstract

Stress/number of cycles to failure relations were established for unidirectional, cross-plied and angle-plied laminates of APC-2 using three-point bend flexure tests. Results for constant stress ratio fatigue tests were modelled using both Weibull and fatigue modulus degradation analyses. Behaviour was compared with that of an established carbon/epoxy system.

Original language	English (US)
Pages (from-to)	191-198
Number of pages	8
Journal	Composites
Volume	22
Issue number	3
DOIs	https://doi.org/10.1016/0010-4361(91)90318-B
State	Published - May 1991

All Science Journal Classification (ASJC) codes

General Materials Science

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10.1016/0010-4361(91)90318-B

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title = "Flexural fatigue of carbon fibre-reinforced PEEK laminates",

abstract = "Stress/number of cycles to failure relations were established for unidirectional, cross-plied and angle-plied laminates of APC-2 using three-point bend flexure tests. Results for constant stress ratio fatigue tests were modelled using both Weibull and fatigue modulus degradation analyses. Behaviour was compared with that of an established carbon/epoxy system.",

author = "M. Buggy and G. Dillon",

year = "1991",

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AU - Buggy, M.

AU - Dillon, G.

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AB - Stress/number of cycles to failure relations were established for unidirectional, cross-plied and angle-plied laminates of APC-2 using three-point bend flexure tests. Results for constant stress ratio fatigue tests were modelled using both Weibull and fatigue modulus degradation analyses. Behaviour was compared with that of an established carbon/epoxy system.

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JO - Composites

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Flexural fatigue of carbon fibre-reinforced PEEK laminates

Abstract

All Science Journal Classification (ASJC) codes

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