Strength tests on thin-walled duralumin cylinders in torsion / by Eugene E. Lundquist.

Format:

Book

Government document

Author/Creator:

Lundquist, Eugene E., author.

Contributor:

United States. National Advisory Committee for Aeronautics, issuing body.

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 427.

Technical note / National Advisory Committee for Aeronautics ; No. 427

Language:

English

Subjects (All):

Duralumin--Testing.

Duralumin.

Strength of materials--Testing.

Strength of materials.

Torsion.

torsional stress.

Physical Description:

1 online resource (8 pages, 12 unnumbered pages) : illustrations.

Place of Publication:

Washington, [D.C.] : National Advisory Committee for Aeronautics, 1932.

Summary:

This report is the first in a series presenting the results of strength tests on thin-walled cylinders and truncated cones of circular and elliptical section; it comprises the results obtained to date from torsion (pure shear) tests of 65 thin-walled duralumin cylinders of circular section with ends clamped to rigid bulkheads. The effect of variations in the length/radius and radius/thickness ratios on the type of failure is indicated, and a semi-empirical equation for the shearing stress at maximum load is given.

Notes:

Description based on online resource, PDF version; title from title page (TRAIL, viewed January 5, 2021).

"August, 1932."

"Langley Memorial Aeronautical Laboratory."

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: Lundquist, Eugene E. Strength tests on thin-walled duralumin cylinder in torsion

OCLC:

1143006527