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Effect of aging on mechanical properties of aluminum-alloy rivets / by Frederick C. Roop.

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U.S. Government Documents
Format:
Book
Government document
Author/Creator:
Roop, Frederick C., author.
Contributor:
United States. National Advisory Committee for Aeronautics, issuing body.
Series:
Technical note (United States. National Advisory Committee for Aeronautics) ; 805.
Technical note / National Advisory Committee for Aeronautics ; no. 805
Language:
English
Subjects (All):
Rivets and riveting, Aircraft.
Aluminum alloys.
aluminum alloy.
Physical Description:
1 online resource (24 pages, 9 unnumbered pages) : illustrations.
Place of Publication:
Washington, [D.C.] : National Advisory Committee for Aeronautics, 1941.
Summary:
Curves and tabular data present the results of strength tests made during and after 2.5 years of aging on rivets and rivet wire of 3/16-inch nominal diameter. The specimens were of aluminum alloy: 24S, 17S, and A17S of the duralumin type and 53S of the magnesium-silicide type.
Notes:
Description based on online resource, PDF version; title from title page (TRAIL, viewed March 8, 2022).
"April 1941."
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical references (pages 21-24).
Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas
Other Format:
Print version: Roop, Frederick C. Effect of aging on mechanical properties of aluminum-alloy rivets
OCLC:
1158388815

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