Relation of engine turbine-blade life to stress-rupture properties of the alloys, Stellite 21, Hastelloy B, Cast S-816, Forged S-816, X-40, Nimonic 80, Refractory 26, N-155, and Iconel X Page: 4 of 61

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Garrett, F. B. & Yaker, C. Relation of engine turbine-blade life to stress-rupture properties of the alloys, Stellite 21, Hastelloy B, Cast S-816, Forged S-816, X-40, Nimonic 80, Refractory 26, N-155, and Iconel X, report, August 23, 1951; (https://digital.library.unt.edu/ark:/67531/metadc64863/m1/4/: accessed April 16, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

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