Marker Loads for Quantitative Fractography of Fatigue Cracks in Aerospace Alloys-Reference-Cited by-同舟云学术

Marker Loads for Quantitative Fractography of Fatigue Cracks in Aerospace Alloys

Published:2009 Issue: Volume: Page:15-54
ISSN:
Container-title:ICAF 2009, Bridging the Gap between Theory and Operational Practice
language:
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Author:

Barter S. A.,Molent L.,Wanhill R. J. H.

Publisher

Springer Netherlands

Link

http://link.springer.com/content/pdf/10.1007/978-90-481-2746-7_2.pdf

Reference55 articles.

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3. GlobalSecurity (2007), http://www.globalsecurity.org/military/systems/aircraft/f-16-life.htm

4. MIL-STD-1530A (11) (1975), Airplane Structural Integrity Program, Airplane Requirements, Military Standard, USAF.

5. Glaessgen, E. H., Saether, E., Yamakov, V. (2008), In: Proceedings of the Eleventh Joint FAA/ DoD/ NASA Conference on Aging Aircraft, Phoenix, Arizona, April 21–24, 2008 (to be published).

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