Analysis of crack interactions at adjacent holes and onset of multi-site fatigue damage in aging airframes-Reference-Cited by-同舟云学术

Analysis of crack interactions at adjacent holes and onset of multi-site fatigue damage in aging airframes

Published:2009-04 Issue:2 Volume:156 Page:155-163
ISSN:0376-9429
Container-title:International Journal of Fracture
language:en
Short-container-title:Int J Fract

Author:

Wang X.,Modarres M.,Hoffman P.

Publisher

Springer Science and Business Media LLC

Subject

Mechanics of Materials,Modelling and Simulation,Computational Mechanics

Link

http://link.springer.com/content/pdf/10.1007/s10704-009-9354-3.pdf

Reference28 articles.

1. Anderson TL (2005) Fracture mechanics: fundamentals and applications, 3rd edn. CRC Press, Boca Raton

2. Asada H (1989) Reliability assessment of pressurized fuselages with multiple-site fatigue cracks. 5th international conference on structural safety and reliability, pp 2369–2372

3. Cherry MC, Mall S, Heinimann B, Grandt AF Jr (1997) Residual strength of unstiffened aluminum panels with multiple site damage. Eng Fract Mech 57(6): 701–713. doi: 10.1016/S0013-7944(97)00037-4

4. Dowling NE (1998) Mechanical behavior of materials. Prentice Hall, New Jersey

5. Hijazi AL (2001) Residual strength of thin-sheet aluminum panels with multiple site damage. Ph.D. dissertation, Wichita State University

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