The Effect Longitudinal Stiffeners Located on One Side of a Plate on the Compressive Buckling Stress of the Plate-Stiffener Combination

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Report Number: NACA TN 2873
Author(s): Seide, Paul
Corporate Author(s): Langley Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-01
Pages: 71
DoD Task:
PB Number: PB108668
Identifier: AD0002814

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