Elastic Instability of Members Having Sections Common in Aircraft Construction
Description:
"Two fundamental problems of elastic stability are discussed in this report. In part one formulas are given for calculating the critical stress at which a thin, outstanding flange of a compression member will either wrinkle into several waves or form into a single half wave and twist the member about its longitudinal axis. In part two the lateral buckling of beams is discussed" (p. 373).
Date:
October 15, 1930
Creator:
Trayer, George W. & March, H. W.
Partner:
UNT Libraries Government Documents Department