Residual strength prediction for aircraft panels with Multiple Site Damage, using the ?EPFEAM? for stable crack growth analysis

Author:

Pyo C. R.,Okada H.,Atluri S. N.

Publisher

Springer Science and Business Media LLC

Subject

Applied Mathematics,Computational Mathematics,Computational Theory and Mathematics,Mechanical Engineering,Ocean Engineering,Computational Mechanics

Reference13 articles.

1. Atluri, S. N. 1986: Energetic approaches and path-independent integrals in fracture mechanics. Computational methods in the mechanics of fracture. Ed. by Atluri, S. N. Elsevier Science Publisher. B.V

2. AtluriS. N.; HarrisC. E.; HoggardA.; MillerN. A.; SampathS. G. 1992: Durability of metal air frame structures. Technical Publications. Atlanta, USA

3. AtluriS. N.; SampathS. G.; TongP. 1991: Structural integrity of aging airplanes. Berlin, Heidelberg, New York. Springer

4. Broek, D. 1993: The effects of multi-site-damage on the arrest capability of aircraft fuselage structures. FractuREsearch TR 9302

5. MurakamiY. et al. 1987: Stress intensity handbook. Pergamon Press, Oxford

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