Hardened parts are used to minimize abrasion at contact surfaces and to extend the lifetime of machine components. Different risks to failure, and therefore, different fatigue limits result from imperfections, notches and surface properties. Two methods for calculating fatigue limits of surface-hard
β¦ LIBER β¦
Calculation of fatigue limits of case-hardened specimens with consideration of mean stresses and residual stresses
β Scribed by F. Jablonski; R. Kienzler
- Publisher
- Springer
- Year
- 2002
- Tongue
- English
- Weight
- 153 KB
- Volume
- 28
- Category
- Article
- ISSN
- 0178-7675
No coin nor oath required. For personal study only.
π SIMILAR VOLUMES
Prediction of fatigue limits of surface-
β
Frank Jablonski; Johanna Varvarikes
π
Article
π
2008
π
Elsevier Science
π
English
β 187 KB
Influence of residual stresses and mean
β
Thomas Krug; Karl-Heinz Lang; Theo Fett; Detlef LΓΆhe
π
Article
π
2007
π
Elsevier Science
π
English
β 634 KB
Redistribution of residual stresses of t
β
M. F. Lutsiv; B. F. Ryabov; M. G. Khitarishvili; Yu. I. Babei
π
Article
π
1971
π
Springer
π
English
β 308 KB
Fatigue crack growth in consideration of
β
Kang Yong Lee; Gun Young Kim
π
Article
π
1993
π
Elsevier Science
π
English
β 412 KB
A fatigue crack growth rate in consideration of fatigue damage accumulation and the mean stress on fatigue material elements ahead of a crack tip are derived using Both Miner's rule and the Manson-Coffin relationship. The theoretical equation of fatigue crack growth rate is shown in terms of J-integ
Fatigue life estimation of spot welds us
β
S.E. Mirsalehi; A.H. Kokabi
π
Article
π
2010
π
Elsevier Science
π
English
β 323 KB
Formation of residual stresses during fr
β
L. V. Klychnikov; S. P. Davtyan; N. A. Belyaeva; S. I. Khudyaev; N. S. Enikolopy
π
Article
π
1985
π
Springer US
π
English
β 355 KB