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Improvement of the fatigue limit – Joints

Posted on September 11, 2013 by Aerospace Engineering

Improvement of joints with rows of bolts or rivets A simple double strap joint with two rows of bolts at … Continue reading →

Posted in Fatigue Analysis | Tagged Clamping, crack, cross, damage, double, expansion, fatigue, fretting, good, hole, Improvement, improvements, joints, k, limit, lug, lugs, mandrel, nosecap, pitch, plastic, rivet, rivets, rows, section, split, strap | Leave a comment

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