Strip yield crack analysis for multiple site damage in infinite and finite panels – A weight function approach

Author:

Wu X.R.,Xu W.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference21 articles.

1. Milestone case histories in aircraft structural integrity;Wanhill,2003

2. Tan PW, Bigelow CA, Bakucks JG. Widespread fatigue damage assessment approach. In: Presented at the RTO AVT specialists’ meeting on “life management techniques for ageing air vehicles”, Manchester, UK, October, 2001.

3. Gruber ML, Wilkins KE, Worden RE. Investigation of fuselage structure subjected to widespread fatigue damage. In: Proceedings of the FAA–NASA symposium on the continued airworthiness of aircraft structures, August, 1997. p. 439–60.

4. Analysis of residual strength of stiffened panels with multiple site damage;Koolloos,2001

5. An experimental and numerical analysis of residual strength of butt-joints panels with multiple site damage;Calatolo;Engng Fract Mech,2001

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