Stability of rectangular plates with longitudinal or transverse stiffeners under uniform compression (1939)
NASA Technical Reports Server (NTRS) · leaf 53
m *4 … m1 A" I Ha I ID Figure 3.- Cross-sections through the possible buckling forms O I, Uodal line at the stiffener IIafBuckling of plate and stiffener (D CO * lib,Knife edge mounting of stiffener I O TIT ? • g - m 1^ to f T Figure 2.- Forces and moments between plate and stiffeners. 03
NASA Technical Reports Server (NTRS)
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