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

Author: Garrett, F. B.
Year: 1951
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E51G13
Link: https://digital.library.unt.edu/ark:/67531/metadc64863/

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