Magnesium Alloys - Design, Processing and Properties 2011
DOI: 10.5772/13808
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Evaluation Method for Mean Stress Effect on Fatigue Limit of Non-Combustible Mg Alloy

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Cited by 2 publications
(1 citation statement)
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“…However in this study, the singularity index of the T-shaped structure is treated as λ ¼ 0:500 in consideration of the flexibility of the stress intensity factor. Also, in a magnesium alloy, a fatigue crack propagates in the rectangular direction to a maximum principal stress [22]. That is, the fatigue crack starting from the corner in the T-shaped structure follows the s θmax theory [23], propagating in the direction of the tangential adjusting stress s θ .…”
Section: Evaluation By Stress Intensity Factormentioning
confidence: 98%
“…However in this study, the singularity index of the T-shaped structure is treated as λ ¼ 0:500 in consideration of the flexibility of the stress intensity factor. Also, in a magnesium alloy, a fatigue crack propagates in the rectangular direction to a maximum principal stress [22]. That is, the fatigue crack starting from the corner in the T-shaped structure follows the s θmax theory [23], propagating in the direction of the tangential adjusting stress s θ .…”
Section: Evaluation By Stress Intensity Factormentioning
confidence: 98%