Prediction of Cyclic Growth of Cracks and Debonds in Aluminum Sheets Reinforced With Boron/Epoxy

Author:

Roderick G. L.

Publisher

Springer US

Reference7 articles.

1. G. L. Roderick, “Crack Propagation in Aluminum Sheets Reinforced with Boron-Epoxy,” Ph.D. Dissertation, Old Dominion University, Norfolk, VA, 1978.

2. M. M. Ratwani, “Characterization of Crack Growth in Bcnded Structures,” AFFDL-TR-77-31, Vols. I and II, 1977.

3. F. Erdogan and K. Arin, “A Sandwich Plate with a Part-Through and Debonding Crack,” Engineering Fracture Mech. J., Vol. 4, 1972.

4. R. G. Forman, V. E. Kearney, and R. M. Engle, “Numerical Analysis of Crack Propagation in Cyclic-Loaded Structures,” Trans. American Society of Mechanical Engineers, Ser. D.: J. Basic Eng., Vol. 89, No. 3, pp. 459–464, 1967.

5. C.M. Hudson, “Effect of Stress Ratio on Fatigue Crack Growth in 7075-T6 and 2024-T3 Aluminum Alloy Specimens,” National Aeronautics and Space Administration TN D-5390, 196l.

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