Minimum-weight design of simply supported transversely stiffened plates under compression

Alexander Gomza, Paul Seide
naca-tn-1710
Sep 1948


The weight of a simply supported transversely stiffened compression panel subjected to a given buckling load is investigated as a function of the stiffener spacing, plate thickness, and the geometry of the stiffener cross section.

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http://naca.central.cranfield.ac.uk/reports/1948/naca-tn-1710.pdf