The lead fatigue crack concept for aircraft structural integrity

Author:

Molent L.,Barter S.A.

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference30 articles.

1. Fatigue of structures and materials in the 20th century and the state of the art;Schijve;Fatigue,2003

2. An experimental evaluation of fatigue crack growth;Barter;Engineering Failure Analysis,2005

3. A comparison of crack growth behaviour in several full-scale airframe fatigue tests;Molent;Fatigue,2007

4. Understanding crack growth in fuselage lap joints;Jones;Theoretical and Applied Fracture Mechanics,2008

5. A method for evaluation of in-service fatigue cracks;Molent;Engineering Failure Analysis,2004

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