Fatigue and crack-growth analyses of riveted lap-joints in a retired aircraft-Reference-Cited by-同舟云学术

Fatigue and crack-growth analyses of riveted lap-joints in a retired aircraft

Published:2016-01 Issue: Volume:82 Page:342-349
ISSN:0142-1123
Container-title:International Journal of Fatigue
language:en
Short-container-title:International Journal of Fatigue

Author:

Newman J.C.,Ramakrishnan R.

Publisher

Elsevier BV

Subject

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

Reference29 articles.

1. Steadman D, Bakuckas Jr JG. Destructive evaluation and extended fatigue testing of retired transport aircraft: program overview. DOT/FAA/AR-07/22, vol. 1; 2007.

2. Ramakrishnan R, Jury D. Destructive evaluation and extended fatigue testing of retired transport aircraft: damage characterization. DOT/FAA/AR-07/22, vol. 2; 2007.

3. Mosinyi B, Bakuckas Jr JG, Steadman D. Destructive evaluation and extended fatigue testing of retired transport aircraft: extended fatigue testing. DOT/FAA/AR-07/22, vol. 4; 2007.

4. Ramakrishnan R, Steadman D, Carter A. Crack history reconstruction of lap joint fatigue cracks. In: Proc Int Fatigue Congress 2006, Atlanta, GA.

5. Jury D, Ramakrishnan R, Carter A. Rivet installation and faying surface quality studies in a lap joint removed from a retired commercial aircraft. In: Proc Int Fatigue Congress 2006, Atlanta, GA.

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