Yield strength considerations for selecting material subjected to spectrum loads
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OpenAlex topics: Transport Systems and Technology · Engineering Structural Analysis Methods · Mechanical Engineering and Vibrations Research
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References (6)
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1. 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).
2. 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).
3. 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).10.21236/AD0787655 ↗
4. Personal communication with W. S. Margolis, F-16 Material Allowables Test Data, General Dynamics (1977).
5. J. W. Hagemeyer, Overload Induced Retardation of Fatigue Cracks in Several Aluminum and Titanium Alloys, General Dynamics ERR-FW-1779 (December 1976).
6. 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) 206–213.10.1115/1.3443287 ↗