Title Effect of normal pressure on the critical compressive stress of curved sheet / Norman Rafel

Published Washington, D.C. : National Advisory Committee for Aeronautics, [1942]

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Description 1 online resource (2, [8] pages) : illustrations Series Wartime Report / National Advisory Committee for Aeronautics ; no. L258 Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L258 Summary Results are presented of tests of two specimens tested to study the effect of normal pressure on the critical compressive stress for thin curved sheets. These specimens are designated by their respective rib spacings of 10 inches and 30 inches. The relationship between compressive stress and normal pressure at which buckles disappeared is independent of whether the buckles were made to disappear by increase of normal pressure or decrease of compressive stress Notes NACA Wartime Report L-258 Originally issued as NACA as a Restricted Bulletin (November 1942) Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia Print version record Subject Atmospheric pressure. Buckling (Mechanics) Strains and stresses. Loads (Mechanics) Charts, diagrams, etc. atmospheric pressure. buckling. warping. stress. strain. diagrams. Atmospheric pressure. Buckling (Mechanics) Charts, diagrams, etc. Loads (Mechanics) Strains and stresses. Form Electronic book Author United States. National Advisory Committee for Aeronautics. Langley Aeronautical Laboratory. ISBN 9781680156348 1680156349

Other Titles NACA Wartime Reports. Series L

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