Compressive strength of 24S-T aluminum-alloy flat panels with longitudinal formed hat-section stiffeners having a ratio of stiffener thickness to skin thickness equal to 1.00

William A. Hickman, Norris F. Dow
naca-tn-1439
Sep 1947


Results are presented for a part of a test program on 24S-T aluminum-alloy flat compression panels with longitudinal formed hat-section stiffeners. This part of the program is concerned with panels in which the thickness of the stiffener material is equal to the thickness of the skin.

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http://naca.central.cranfield.ac.uk/reports/1947/naca-tn-1439.pdf