References
W. S. Johnson, J. W. Morrow, and C. D. Little, Damage Tolerance Crack Growth Characterization of 7475 Aluminum Material, General Dynamics ERR-FW-1753 (December 1976).
J. W. Morrow, P. J. Noronha, Z. R. Wolanski, and W. S. Johnson, An Experimental and Analytical Investigation on the Effects of F-16 Spectra Truncation on Crack Growth, General Dynamics ERR-FW-1695 (January 1976).
J. P. Gallagher and T. F. Hughes, Influence of Yield Strength on Overload Affected Fatigue Crack Growth Behavior in 4340 Steel, AFFDL-TR-74-27 (July 1974).
Personal communication with W. S. Margolis, F-16 Material Allowables Test Data, General Dynamics (1977).
J. W. Hagemeyer, Overload Induced Retardation of Fatigue Cracks in Several Aluminum and Titanium Alloys, General Dynamics ERR-FW-1779 (December 1976).
G.J. Petrak and J.P. Gallagher, Predictions of the Effect of Yield Strength on Fatigue Crack Growth Retardation in HP-9Ni-4Co-30C Steel, Journal of Engineering Materials and Technology 97H (1975) 206–213.
Author information
Authors and Affiliations
Rights and permissions
About this article
Cite this article
Johnson, W.S., Hagemeyer, J.W. Yield strength considerations for selecting material subjected to spectrum loads. Int J Fract 13, 519–523 (1977). https://doi.org/10.1007/BF00034254
Issue Date:
DOI: https://doi.org/10.1007/BF00034254