STAGS Developments for Residual Strength Analysis Methods for Metallic Fuselage Structures

Author:

Young Richard D.1,Rose Cheryl1

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Reference57 articles.

1. Potyondy, D. O., Wawrzynek, P. A., and Ingraffea, A. R. ``Discrete Crack Growth Analysis Methodology for Through Cracks in Pressurized Fuselage Structures,'' Proceedings of the FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance, edited by C. E. Harris, NASA Langley Research Center, Hampton, VA, 1994, pp. 581 - 602.

2. Residual Strength Calculations of Stiffened Metal Panels Containing Cracks

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