Long fatigue life critical crack lengths
ABSTRACT A model based on surface strain redistribution and crack closure is presented for prediction of the endurance or fatigue limit stress by determining the threshold stress and critical length of short cracks that develop under microstructural control. The threshold stress first decreases with...
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| Published in | Fatigue & fracture of engineering materials & structures Vol. 33; no. 5; pp. 320 - 330 |
|---|---|
| Main Authors | , |
| Format | Journal Article |
| Language | English |
| Published |
Oxford, UK
Blackwell Publishing Ltd
01.05.2010
Blackwell Wiley Subscription Services, Inc |
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| Online Access | Get full text |
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| Abstract | ABSTRACT
A model based on surface strain redistribution and crack closure is presented for prediction of the endurance or fatigue limit stress by determining the threshold stress and critical length of short cracks that develop under microstructural control. The threshold stress first decreases with crack size to a local minimum then increases to a local maximum corresponding to the fatigue limit stress. This occurs at the critical crack length corresponding to about four grain diameters. The model is capable of determining the threshold stress range and depth of propagating and non‐propagating surface cracks as a function of stress ratio, material and grain size. The microstructure is shown to be particularly significant in the very long life regime (Nf ≈ 109 cycles). When the surface cracks become non‐propagating, internally initiated cracks continue growing slowly, eventually reaching the critical crack length with failure occurring after a very high number of cycles (107 < Nf < 109 cycles). |
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| AbstractList | ABSTRACT
A model based on surface strain redistribution and crack closure is presented for prediction of the endurance or fatigue limit stress by determining the threshold stress and critical length of short cracks that develop under microstructural control. The threshold stress first decreases with crack size to a local minimum then increases to a local maximum corresponding to the fatigue limit stress. This occurs at the critical crack length corresponding to about four grain diameters. The model is capable of determining the threshold stress range and depth of propagating and non‐propagating surface cracks as a function of stress ratio, material and grain size. The microstructure is shown to be particularly significant in the very long life regime (
N
f
≈ 10
9
cycles). When the surface cracks become non‐propagating, internally initiated cracks continue growing slowly, eventually reaching the critical crack length with failure occurring after a very high number of cycles (10
7
<
N
f
< 10
9
cycles). A model based on surface strain redistribution and crack closure is presented for prediction of the endurance or fatigue limit stress by determining the threshold stress and critical length of short cracks that develop under microstructural control. The threshold stress first decreases with crack size to a local minimum then increases to a local maximum corresponding to the fatigue limit stress. This occurs at the critical crack length corresponding to about four grain diameters. The model is capable of determining the threshold stress range and depth of propagating and non-propagating surface cracks as a function of stress ratio, material and grain size. The microstructure is shown to be particularly significant in the very long life regime (Nf - 109 cycles). When the surface cracks become non-propagating, internally initiated cracks continue growing slowly, eventually reaching the critical crack length with failure occurring after a very high number of cycles (107 < Nf < 109 cycles). A model based on surface strain redistribution and crack closure is presented for prediction of the endurance or fatigue limit stress by determining the threshold stress and critical length of short cracks that develop under microstructural control. The threshold stress first decreases with crack size to a local minimum then increases to a local maximum corresponding to the fatigue limit stress. This occurs at the critical crack length corresponding to about four grain diameters. The model is capable of determining the threshold stress range and depth of propagating and non-propagating surface cracks as a function of stress ratio, material and grain size. The microstructure is shown to be particularly significant in the very long life regime ( Nf [approximate] 109 cycles). When the surface cracks become non-propagating, internally initiated cracks continue growing slowly, eventually reaching the critical crack length with failure occurring after a very high number of cycles (107 < Nf < 109 cycles). [PUBLICATION ABSTRACT] ABSTRACT A model based on surface strain redistribution and crack closure is presented for prediction of the endurance or fatigue limit stress by determining the threshold stress and critical length of short cracks that develop under microstructural control. The threshold stress first decreases with crack size to a local minimum then increases to a local maximum corresponding to the fatigue limit stress. This occurs at the critical crack length corresponding to about four grain diameters. The model is capable of determining the threshold stress range and depth of propagating and non‐propagating surface cracks as a function of stress ratio, material and grain size. The microstructure is shown to be particularly significant in the very long life regime (Nf ≈ 109 cycles). When the surface cracks become non‐propagating, internally initiated cracks continue growing slowly, eventually reaching the critical crack length with failure occurring after a very high number of cycles (107 < Nf < 109 cycles). |
| Author | UNTERMANN, N. PLUMTREE, A. |
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| Cites_doi | 10.1016/j.ijfatigue.2005.05.018 10.1111/j.1460-2695.1992.tb00065.x 10.1016/0025-5416(78)90174-X 10.1016/j.scriptamat.2008.08.004 10.1007/BF02645485 10.1016/S0921-5093(97)00246-3 10.1111/j.1460-2695.1992.tb00026.x 10.1007/BF02644801 10.1016/S0007-8506(07)60412-0 10.1111/j.1460-2695.1982.tb01220.x 10.1016/S0924-0136(01)00770-1 10.1016/0142-1123(80)90024-9 10.1016/0142-1123(92)90155-6 10.1299/kikaia.50.1077 10.1016/j.ijfatigue.2007.03.010 10.1111/j.1460-2695.1995.tb00868.x |
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| Issue | 5 |
| Keywords | Fatigue life Crack length Mechanical properties critical crack lengths Strain distribution Fatigue Fatigue threshold closure long life fatigue Fatigue crack |
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| Notes | ArticleID:FFE1444 ark:/67375/WNG-WP9213B9-C This manuscript was originally compiled for a Special Issue by Prof. C. Rodopoulos entitled 'Physics of Fatigue Damage'. istex:848B75D0257CD032D463BAFBFAC132F81CD54EE7 This manuscript was originally compiled for a Special Issue by Prof. C. Rodopoulos entitled ‘Physics of Fatigue Damage’. ObjectType-Article-2 SourceType-Scholarly Journals-1 ObjectType-Feature-1 content type line 23 |
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| References_xml | – volume: 18 start-page: 1455 year: 1995 end-page: 1467 article-title: The effect of grain size on the fatigue of commercially pure aluminum publication-title: Fatigue Fract. Engng Mater. Struct. – year: 1981 – volume: 19A start-page: 2575 year: 1988 end-page: 2587 article-title: Near‐threshold fatigue crack growth in copper and alpha‐brass: grain size and environmental effects publication-title: Metall. Trans. A – volume: 5 start-page: 1 year: 1982 end-page: 17 article-title: Mixed‐mode fatigue thresholds publication-title: Fatigue Engng. Mater. Structures – start-page: 387 year: 1986 end-page: 404 – volume: 15 start-page: 895 year: 1992 end-page: 909 article-title: A model for the fatigue limit and short crack behaviour related to surface strain redistribution publication-title: Fatigue Fract. Engng. Mater. 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| Snippet | ABSTRACT
A model based on surface strain redistribution and crack closure is presented for prediction of the endurance or fatigue limit stress by determining... A model based on surface strain redistribution and crack closure is presented for prediction of the endurance or fatigue limit stress by determining the... |
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| SubjectTerms | Applied sciences closure Cracks critical crack lengths Exact sciences and technology Fatigue Fatigue life fatigue threshold long life fatigue Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology Metals. Metallurgy strain distribution Stress analysis |
| Title | Long fatigue life critical crack lengths |
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