Fatigue properties degraded with crystallographic orientations greater than 10 degrees from {001} axis. Influence of solidification and heat-treatment parameters on structure and fatigue properties of nickel-based superalloy MAR-M246(Hf) described in 24-page report. Superalloys have high strength and corrosion resistance at temperatures up to 1,400 degrees C; their uses range from petrochemical equipment to marine, industrial, aircraft, and vehicular gas turbines.
Solidification Effects in MAR-M246(Hf) Alloy
NASA Tech Briefs ; 11 , 5
1987-05-01
Miscellaneous
No indication
English
British Library Conference Proceedings | 1993
|Fundamentals of Alloy Solidification
NTRS | 1986
|Solidification-Rate Effects In MAR-M-246+Hf Alloy
NTRS | 1988
|