Two new practical models for estimating reliability-based fatigue strength of composites
Two new practical models for estimating reliability-based fatigue strength of composites
This paper outlines two new practical models to evaluate fatigue residual strength and the overall range of life for reliability-based design. A new fatigue-driven residual strength surface model with four parameters is derived based on an expression form of power function product to estimate the parameters more easily and expediently, and logically characterize the physical characteristics and the phenomenological quantitative laws. A more appropriate S-N curve formulation with four parameters is presented to cover overall life range. By means of the likelihood principle and the linear regression, the parameter determination formulae of these two models are respectively established to deal with the test data effectively and easily. The probability distributions for these two models are also given. Finally, the models are applied to two sets of experimental data, demonstrating the practical and effective use of the proposed models. It is shown from these examples that fatigue-driven residual strength and the overall range of life can be obtained realistically according to the small sample test data using the new formulae.
composites fatigue, residual strength, overall life range, probability distribution, reliability design
1187-1209
Xiong, J.J.
785d6bd7-e6a1-472c-ae43-484f28d646eb
Shenoi, R.A.
a37b4e0a-06f1-425f-966d-71e6fa299960
2004
Xiong, J.J.
785d6bd7-e6a1-472c-ae43-484f28d646eb
Shenoi, R.A.
a37b4e0a-06f1-425f-966d-71e6fa299960
Xiong, J.J. and Shenoi, R.A.
(2004)
Two new practical models for estimating reliability-based fatigue strength of composites.
Journal of Composite Materials, 38 (14), .
(doi:10.1177/0021998304042081).
Abstract
This paper outlines two new practical models to evaluate fatigue residual strength and the overall range of life for reliability-based design. A new fatigue-driven residual strength surface model with four parameters is derived based on an expression form of power function product to estimate the parameters more easily and expediently, and logically characterize the physical characteristics and the phenomenological quantitative laws. A more appropriate S-N curve formulation with four parameters is presented to cover overall life range. By means of the likelihood principle and the linear regression, the parameter determination formulae of these two models are respectively established to deal with the test data effectively and easily. The probability distributions for these two models are also given. Finally, the models are applied to two sets of experimental data, demonstrating the practical and effective use of the proposed models. It is shown from these examples that fatigue-driven residual strength and the overall range of life can be obtained realistically according to the small sample test data using the new formulae.
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Published date: 2004
Keywords:
composites fatigue, residual strength, overall life range, probability distribution, reliability design
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Local EPrints ID: 22843
URI: http://eprints.soton.ac.uk/id/eprint/22843
ISSN: 0021-9983
PURE UUID: 2a684982-9c26-4a01-ae75-80d329508356
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Date deposited: 22 Mar 2006
Last modified: 15 Mar 2024 06:41
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Author:
J.J. Xiong
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