On obtaining fracture toughness values from the literature
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OpenAlex topics: Material Properties and Failure Mechanisms · Fatigue and fracture mechanics · Engineering Diagnostics and Reliability
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References (29)
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10. R.H. Heyer and D.E. McCabe, in Review of Developments in Plane Strain Fracture Toughness Testing, STP 463, American Society for Testing and Materials, Philadelphia (1970) 22–4110.1520/STP33658S ↗
11. U.H. Lindborg and B.L. Averbach, Acta Metallurgica 14 (1966) 1583–159310.1016/0001-6160(66)90179-9 ↗
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17. D.A. Gerdeman, J.C. Wurst, J.A. Cherry, and W.E. Berner, Report AFML-TR-68-53, Air Force Materials Laboratory, Wright-Patterson AFB, Ohio (1968)
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20. H.P. van Leeuwan et al., NLR Report Nos. TR 72032, TR 72082, TR 72088, Amsterdam, The Netherlands (1972)
21. G.T. Schaeffer and V. Weiss, Interim Technical Report No. SUI MET-1078-664-12, Syracuse University, New York (1964)
22. R.J. Goode, unpublished data (1974)
23. D.W. Hoeppner, in Case Studies in Fracture Mechanics, Report No. AMMRC MS 77–5, Army Materials and Mechanics Research Center, Mass. (1977)3.1.1–3.1.10
24. S.O. Davis, N.G. Tupper, and R.M. Niemi, Report AFML-TR-65-150, Air Force Materials Laboratory, Wright-Patterson AFB, Ohio (1965)
25. W.F. Brown, Jr. and J.E. Srawley, Data presented at Subcommittee III Meeting of ASTM Committee E-24 (1964)
26. W.F. Brown, Jr., “Progress Report on NASA-NRL Cooperative Plane Strain Testing Program‘, ASTM Committee E-24 Meeting (1965)
27. M.V. Hyatt and M.O. Spidel,in Stress-Corrosion Cracking in High Strength Steels and in Titanium and Aluminum Alloys, Naval Research Laboratory, Washington, DC (1972) 147–244
28. R.E. Jones, Report AFML-TR-69-58, Air Force Materials Laboratory, Wright-Patterson AFB, Ohio (1969)
29. F.C. Allen, in Damage Tolerance in Aircraft Structures, STP 486, American Society for Testing and Materials, Philadelphia (1971) 16–3810.1520/STP26671S ↗