FATIGUE CRACK GROWTH OF Al 2024-T3 UNDER LOW AMPLITUDE TWO-STEP LOADING
โ Scribed by H. R. Mayer; S. E. Stanzl; E. K. Tschegg; J. Schijve
- Book ID
- 109013386
- Publisher
- John Wiley and Sons
- Year
- 1992
- Tongue
- English
- Weight
- 729 KB
- Volume
- 15
- Category
- Article
- ISSN
- 8756-758X
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๐ SIMILAR VOLUMES
Effects of plasticity induced crack closure on the calculated fatigue crack-growth behaviour of middle-crack tension specimens made of 2024-T351 alloy subjected to variable amplitude fatigue loading were examined. The specified loadings were four distinct aircraft spectra: (1) ''modified'' center-wi
Abe&&-A technique for &meting fatigue crack prope&on in notched plates subjected to variable amplitude~boutlincdinthirpeper.Ane~~~tic~~ekmcntmodelisusedtodetermiaetbe eht of notch geometry and the rehal plastic deformations. The analytic model for crack growth is based on an eactive StreSl intensity