Abstract
Gas turbine blade materials having suuperior creep strength and hot corrosion resistance are required. Evaluation of the alloy was made by creep rupture tests and a crucible test using a molten Na//2SO//4 plus 25% NaCl salt mixture.
Cite
CITATION STYLE
APA
Harada, H., & Yamazaki, M. (1979). ALLOY DESIGN FOR gamma prime PRECIPITATION HARDENING NICKEL-BASE SUPERALLOYS CONTAINING Ti, Ta, AND W. Tetsu To Hagane, 65(7), 1059–1068. https://doi.org/10.2355/tetsutohagane1955.65.7_1059
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