In the present study attempts are made to give an expression of the fatigue crack initiation life of notched elements with the consideration of overloading effects. This expression may be used to predict the fatigue crack initiation life of notched element under variable amplitude loading. Experimen
Effect of rest time after application of single overload cycle on fatigue life
β Scribed by Raghuvir Kumar; Arbind Kumar; Kamlesh Singh
- Publisher
- Elsevier Science
- Year
- 1996
- Tongue
- English
- Weight
- 281 KB
- Volume
- 54
- Category
- Article
- ISSN
- 0013-7944
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β¦ Synopsis
Experiments on IS-1020 steel for single tensile overload applied at 12 mm crack length with and without rest time were carried out. The observed retardation effects are presented here and suggested that overload retardation is primarily due to residual compressive stress generated in the crack tip region. On the basis of these experimental results some power laws are developed to predict the decreased number of delay cycles (No) with rest time. The life of the specimen decreased by increasing the rest time after overload. As the magnitude of overload increased the decrease in life is larger for same rest time as compared to lesser overload.
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Abstrac+-Crack closure experiments were conducted on 6061-T6 Al-alloy, using COD gauge for various overload ratios (1.67, 1.88 and 2.06) and different prestrains (0, 3 and 6%). On the basis of these experiments some power laws are developed. The delay period after application of single overload is a