Factors influencing creep properties of alloys for use in aircraft propulsion systems containing 20% cobalt, 20% chromium, 20% nickel and balance iron; tests carried out at temperature of 1200 to 1600 F.
Fundamental effects of cold-work on some cobalt-chromium-nickel-iron base creep-resistant alloys
NACA -- Tech Note
1952
12 pages
Charts.
Article (Journal)
English
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