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Experimental study of torsional column failure / by Alfred S. Niles.

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Format:
Book
Government document
Author/Creator:
Niles, Alfred S. (Alfred Salem), 1894-1975, author.
Contributor:
United States. National Advisory Committee for Aeronautics, issuing body.
Series:
Technical note (United States. National Advisory Committee for Aeronautics) ; 733.
Technical note / National Advisory Committee for Aeronautics ; No. 733
Language:
English
Subjects (All):
Aluminum alloys.
Columns.
Strains and stresses.
Torsion.
Materials--Fatigue.
Materials.
aluminum alloy.
strain.
stress.
torsional stress.
Physical Description:
1 online resource (47 pages, 12 unnumbered pages) : illustrations.
Place of Publication:
Washington, [D.C.] : National Advisory Committee for Aeronautics, 1939.
Summary:
Thirty-three 24ST aluminum alloy 2- by 2- by 0.10-inch channels, with lengths ranging from 10 to 90 inches were tested at Stanford University in compression to obtain an experimental verification of the theoretical formulas for torsional failure. The observed critical loads and twist-axis locations were sufficiently close to the values obtained from the formulas to establish the substantial validity of the latter. The differences between observed and computed results were small enough to be accounted for by small and mostly unavoidable differences between actual test conditions and those assumed in deriving the formulas. Some data were obtained from the shorter specimens regarding the growth of the buckles that resulted in local buckling failure.
Notes:
Description based on online resource, title from title screen (viewed May 29, 2020).
"October 1939."
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical references (page 40).
Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.
Other Format:
Print version: Niles, Alfred S. Experimental study of torsional column failure
OCLC:
1156323831

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