Development of a fatigue crack growth testing apparatus and its application to thin titanium foil
ABSTRACT A low‐cost experimental apparatus has been developed to investigate the mode I fatigue crack growth behaviour of thin metallic foils and sheets. The apparatus utilizes magnetic coupling between a ceramic magnet and a rotating steel disc to induce cyclic tensile loads in notched rectangular...
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Published in | Fatigue & fracture of engineering materials & structures Vol. 36; no. 11; pp. 1187 - 1198 |
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Main Authors | , , |
Format | Journal Article |
Language | English |
Published |
Oxford
Blackwell Publishing Ltd
01.11.2013
Blackwell Wiley Subscription Services, Inc |
Subjects | |
Online Access | Get full text |
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Summary: | ABSTRACT
A low‐cost experimental apparatus has been developed to investigate the mode I fatigue crack growth behaviour of thin metallic foils and sheets. The apparatus utilizes magnetic coupling between a ceramic magnet and a rotating steel disc to induce cyclic tensile loads in notched rectangular specimens. To illustrate the testing apparatus, mode I fatigue crack growth in 30‐µm‐thick high‐purity titanium foils was studied. Experiments were performed at ambient temperature using a loading frequency of 2 Hz and a nominal stress ratio of 0.1. The cyclic crack growth data could be fit to a Paris relationship between crack growth rate and stress intensity range. The stress intensity factor exponent, m, in the Paris relationship was between 4 and 6, which is comparable with the relatively high values found in the literature for the tension–tension fatigue of other metallic bulk materials. Incomplete self‐similarity analysis was used to explain the observed higher m values for thin metallic foils. |
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Bibliography: | ArticleID:FFE12086 ark:/67375/WNG-WPQL5169-B National Natural Science Foundation of China - No. 11002020 istex:48F9CCFC148CC53DB26F941EF036F319BCAD665D ObjectType-Article-1 SourceType-Scholarly Journals-1 ObjectType-Feature-2 content type line 23 |
ISSN: | 8756-758X 1460-2695 |
DOI: | 10.1111/ffe.12086 |