NASA NTRS · 19870000230
Solidification Effects in MAR-M246(Hf) Alloy
Abstract
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.
Keep this discovery
Explore connections, maps & timelines
Johnston, M. H., Parr, R. A.. 1987-05-01. Solidification Effects in MAR-M246(Hf) Alloy. https://ntrs.nasa.gov/citations/19870000230
Cite the original work for its findings. Save a collection to share your selection of sources.