A two-stage theory on fatigue damage and life prediction of composites
A two-stage theory on fatigue damage and life prediction of composites
Fatigue tests on unnotched and notched composite laminates under compressive cyclic loading have been carried out. The damage mechanism is discussed, and it is seen that the process of composites fatigue damage under the compression cycles loading appears at two different stages. A dual fatigue cumulative damage rule to predict fatigue damage formation and propagation of notched composites is presented according to the traditional phenomenological fatigue methodology and a modern continuum damage mechanics theory. Then a three-dimensional damage constitutive equation for anisotropic composites is established. A new damage evolution equation and a damage propagation ?a–?m–N* surface is derived based on damage strain energy release rate criterion. Finally, the theoretically predicted results are compared with experimental results.
composites, b. fatigue, c. stress concentration
1331-1343
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)
A two-stage theory on fatigue damage and life prediction of composites.
Composites Science and Technology, 64 (9), .
(doi:10.1016/j.compscitech.2003.10.006).
Abstract
Fatigue tests on unnotched and notched composite laminates under compressive cyclic loading have been carried out. The damage mechanism is discussed, and it is seen that the process of composites fatigue damage under the compression cycles loading appears at two different stages. A dual fatigue cumulative damage rule to predict fatigue damage formation and propagation of notched composites is presented according to the traditional phenomenological fatigue methodology and a modern continuum damage mechanics theory. Then a three-dimensional damage constitutive equation for anisotropic composites is established. A new damage evolution equation and a damage propagation ?a–?m–N* surface is derived based on damage strain energy release rate criterion. Finally, the theoretically predicted results are compared with experimental results.
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Published date: 2004
Keywords:
composites, b. fatigue, c. stress concentration
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Local EPrints ID: 22757
URI: http://eprints.soton.ac.uk/id/eprint/22757
ISSN: 0266-3538
PURE UUID: 08b8c978-3ba2-48c5-b542-2dfa1c413de2
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Date deposited: 16 Mar 2006
Last modified: 15 Mar 2024 06:40
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Author:
J.J. Xiong
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