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
โฆ LIBER โฆ
Crack growth rate in impact fatigue and in programmed variable amplitude loading fatigue
โ Scribed by P Johnson; X.P Zhang; G Pluvinage
- Publisher
- Elsevier Science
- Year
- 1990
- Tongue
- English
- Weight
- 588 KB
- Volume
- 37
- Category
- Article
- ISSN
- 0013-7944
No coin nor oath required. For personal study only.
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