Prediction of fatigue crack growth rates in Ti-6Al-4V alloy
Crack initiation under thermo-mechanical fatigue is analyzed with consideration given to oxidation and creep strain accumulation. Transitions and interactions between different mechanisms, crack initiation and crack propagation rates display significant scaling and size effects. The objective of thi...
| Main Authors: | , , |
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| Format: | Journal article |
| Language: | English |
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2008
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| _version_ | 1797082789382717440 |
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| author | Korsunsky, A Dini, D Walsh, M |
| author_facet | Korsunsky, A Dini, D Walsh, M |
| author_sort | Korsunsky, A |
| collection | OXFORD |
| description | Crack initiation under thermo-mechanical fatigue is analyzed with consideration given to oxidation and creep strain accumulation. Transitions and interactions between different mechanisms, crack initiation and crack propagation rates display significant scaling and size effects. The objective of this work is to present experimental data for crack initiation and propagation in aerospace alloys, and to offersome means of describing these data so as to develop improved capabilities for life prediction in aerospace materials and assemblies. © Springer Science+Business Media B.V. 2008. |
| first_indexed | 2024-03-07T01:32:50Z |
| format | Journal article |
| id | oxford-uuid:942b91d9-9e30-43e9-8c4a-6691014a8008 |
| institution | University of Oxford |
| language | English |
| last_indexed | 2024-03-07T01:32:50Z |
| publishDate | 2008 |
| record_format | dspace |
| spelling | oxford-uuid:942b91d9-9e30-43e9-8c4a-6691014a80082022-03-26T23:37:30ZPrediction of fatigue crack growth rates in Ti-6Al-4V alloyJournal articlehttp://purl.org/coar/resource_type/c_dcae04bcuuid:942b91d9-9e30-43e9-8c4a-6691014a8008EnglishSymplectic Elements at Oxford2008Korsunsky, ADini, DWalsh, MCrack initiation under thermo-mechanical fatigue is analyzed with consideration given to oxidation and creep strain accumulation. Transitions and interactions between different mechanisms, crack initiation and crack propagation rates display significant scaling and size effects. The objective of this work is to present experimental data for crack initiation and propagation in aerospace alloys, and to offersome means of describing these data so as to develop improved capabilities for life prediction in aerospace materials and assemblies. © Springer Science+Business Media B.V. 2008. |
| spellingShingle | Korsunsky, A Dini, D Walsh, M Prediction of fatigue crack growth rates in Ti-6Al-4V alloy |
| title | Prediction of fatigue crack growth rates in Ti-6Al-4V alloy |
| title_full | Prediction of fatigue crack growth rates in Ti-6Al-4V alloy |
| title_fullStr | Prediction of fatigue crack growth rates in Ti-6Al-4V alloy |
| title_full_unstemmed | Prediction of fatigue crack growth rates in Ti-6Al-4V alloy |
| title_short | Prediction of fatigue crack growth rates in Ti-6Al-4V alloy |
| title_sort | prediction of fatigue crack growth rates in ti 6al 4v alloy |
| work_keys_str_mv | AT korsunskya predictionoffatiguecrackgrowthratesinti6al4valloy AT dinid predictionoffatiguecrackgrowthratesinti6al4valloy AT walshm predictionoffatiguecrackgrowthratesinti6al4valloy |