Author:
Sankaran K.K.,Perez R.,Jata K.V.
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science
Reference11 articles.
1. The failure of an F/A-18 trailing edge flap hinge
2. Aging of US Air Force Aging Aircraft, Nat. Mat. Adv. Board Pub. NMAB-488-2, National Academy Press, Washington, DC, 1997, pp. 54.
3. Prediction of Fatigue Crack Initiation Life Based on Pit Growth
4. Model for prediction of fatigue lives based upon a pitting corrosion fatigue process;Hoeppner,1979
5. Transition from pitting to fatigue crack growth—modeling of corrosion fatigue crack nucleation in a 2024-T3 aluminum alloy
Cited by
203 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献