The Lateral stability of equal-flanged aluminum-alloy I-beams subjected to pure bending /

Equal-flanged beams of a special extruded i-section of 27ST aluminum alloy were tested in pure bending. Complete and fixity was not attained. Loading was continued until a definite maximum value had been reached. Tensile tests were made on specimens cut from the flanges and the web of each beam. Com...

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Bibliographic Details
Main Author: Dumont, C
Corporate Author: United States National Advisory Committee for Aeronautics
Other Authors: Hill, H. N
Format: Government Document Book
Language:English
Published: Washington D.C. : National Advisory Committee for Aeronautics, 1940
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 770
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Stanford University

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Call Number: ISIL:US-CST
NACA TN 770