Modelling of the fatigue strength degradation due to a semi-elliptical flaw
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Elsevier BV
Reference22 articles.
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4. Analysis of fatigue crack growth in an attachment lug based on the weight function technique and the UniGrow fatigue crack growth model;Mikheevskiy;Int. J. Fatigue,2012
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1. Aircraft Lug Failure Design Under Fatigue Loading;Lecture Notes in Networks and Systems;2024
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