Implications of the lead crack philosophy and the role of short cracks in combat aircraft

Author:

Jones R.,Tamboli D.

Publisher

Elsevier BV

Subject

General Engineering,General Materials Science

Reference63 articles.

1. The lead crack fatigue lifing framework;Molent;Int J Fatigue,2011

2. Schijve J. Fatigue life until small cracks in aircraft structures: durability and damage tolerance. Advanced structural integrity methods for airframe durability and damage tolerance. In: Harris CE, editors. Proceedings FAA/NASA international symposium, Hampton, 1994, NASA Conference Publication 3274; 1994. p. 665–81.

3. Closure mechanisms in Al–Si–Mg cast alloys and long-crack to small-crack corrections;Lados;Int J Fatigue,2005

4. Crack growth from small flaws;Jones;Int J Fatigue,2007

5. Molent L, Sun Q, Green AJ. The F/A-18 fatigue crack growth data compendium, DSTO-TR-1677, Melbourne, Australia; 2005.

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