Centrally cracked specimens of JIS SM58Q and I-IT80 steels were fatigued. The fatigue crack growth rates, da/dn, and the stress intensity threshold levels, AK,, were measured over the range of stress ratio, R, from -1 to 0.8 by the use of an automatic method of continuously decreasing stress intensi
On crack opening stress level in fatigue by Eddy current technique
โ Scribed by K.M. Lal
- Publisher
- Elsevier Science
- Year
- 1979
- Tongue
- English
- Weight
- 272 KB
- Volume
- 12
- Category
- Article
- ISSN
- 0013-7944
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โฆ Synopsis
Linear elastic fracture mechanics relates fatigue crack growth with the stress intensity factor at the crack tip. Presence of residual deformations at the tip of a fatigue crack reduces the crack tip stress intensification such that effective stress intensity range AK~ = U-AK. In this paper use of eddy current technique is exhibited to find the values of test value of effective stress range factor Ut, st. A reasonable comparison between computed and experimental results of UI and Utc~t on two AI alloys 6061-T6 and 6063-T6 has recommended the Eddy Current Technology for finding out the values of crack opening stress level under given loading conditions.
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