Experimental study of torsional column failure /

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...

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Bibliographic Details
Main Author: Niles, Alfred S
Corporate Author: United States National Advisory Committee for Aeronautics
Format: Government Document Book
Language:English
Published: Washington D.C. : National Advisory Committee for Aeronautics, 1939
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 733
Subjects:

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Stanford University

Holdings details from Stanford University
Call Number: ISIL:US-CST
NACA TN 733