Calculating crack growth from small discontinuities in 7050-T7451 under combat aircraft spectra-Reference-Cited by-同舟云学术

Calculating crack growth from small discontinuities in 7050-T7451 under combat aircraft spectra

Published:2013-10 Issue: Volume:55 Page:178-182
ISSN:0142-1123
Container-title:International Journal of Fatigue
language:en
Short-container-title:International Journal of Fatigue

Author:

Jones R.,Molent L.,Barter S.A.

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,General Materials Science,Modelling and Simulation

Reference25 articles.

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

2. Implications of the lead crack philosophy and the role of short cracks in combat aircraft;Jones;Eng Fail Anal,2013

3. Experimental studies into short crack growth;Jones;Eng Fail Anal,2011

4. Forman RG, Shivakumar V, Cardinal JW, Williams LC, McKeighan PC, Fatigue crack growth data base for damage tolerance analysis; 2005 [DOT/FAA/AR-05/15].

5. Sharp PK, Byrnes R, Clark G, Examination of 7050 fatigue crack growth data and its effect on life prediction. Australia; 1998 [DSTO-TN-0729].

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