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The 1350°F stress-rupture properties of two wrought alloys and three cast alloys / by E. E. Reynolds, J. W. Freeman, and A. E. White.

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Format:
Book
Government document
Author/Creator:
Reynolds, E. E., author.
Freeman, J. W. (James W.), author.
White, A. E. (Albert Easton), 1884-1956, author.
Contributor:
United States. National Advisory Committee for Aeronautics, issuing body.
Series:
Technical note (United States. National Advisory Committee for Aeronautics) ; 1380.
Technical notes / National Advisory Committee for Aeronautics ; No. 1380
Language:
English
Subjects (All):
Alloys--Effect of temperature on.
Alloys.
Alloys--Fatigue--Testing.
Strains and stresses.
Physical Description:
1 online resource (23 pages) : illustrations.
Other Title:
One thousand three hundred fifty degree fahrenheit stress-rupture properties of two wrought alloys and three cast alloys
Place of Publication:
Washington, [D.C.] : National Advisory Committee for Aeronautics, 1947.
Summary:
The rupture-test characteristics at 1350 degrees F of two wrought alloys in the solution-treated and aged condition, NR-82 (6059 modified-low carbon) and NR-84 (N-155 modified-low carbon), and three precision-cast alloys in aged condition, NR-71 (X-40), NR-87 (Co-Cr-Ni base-9Mo) and NR-90 (Co-Cr-Ni base-5Mo, 5W) are reported. The properties are shown to compare favorably with those of the strongeest similar alloys previously investigated. A correlation of NACA and OSRD data is presented, showing the variation of ruture strengths with temperature for the alloys between 1350 degrees and 2000 degrees F.
Notes:
Title from title screen (viewed May 3, 2019).
"November 1947."
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical references (page 7).
Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.
Other Format:
Print version: Reynolds, E. E. The 1350 degree stress-rupture properties of two wrought alloys and three cast alloys
OCLC:
1099802663

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