Fracture analysis of multi-site cracking in fuselage lap joints

Author:

Beuth J. L.,Hutchinson J. W.

Publisher

Springer Science and Business Media LLC

Subject

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

Reference7 articles.

1. Cartwright, D. J.; Ratcliffe, G. A. (1972): Strain energy release rate for radial cracks emanating from a pin loaded hole. Int. J. Fract. Mech. 8, 175–181

2. Grandt, A. F. Jr. (1975): Stress intensity factors for some through-cracked fastener holes. Int. J. Fract. 11, 283–294

3. Newman, J. C., Jr. (1971): An improved method of collocation for the stress analysis of cracked plates with various shaped boundaries. NASA Technical Note, NASA TN D-6376

4. Samavedam, G.; Hoadley, D. (1991): Fracture and fatigue strength evaluation of multiple site damaged aircraft fuselages—curved panel testing and analysis. U.S. Department of Transportation Federal Aviation Administration Technical Center Technical Report

5. Swift, T. (1986): Important considerations in commercial aircraft damage tolerance. Int. J. Vehicle Design 7, 264–287

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