Title Charts for calculation of the critical compressive stress for local instability of idealized web- and T-stiffened panels / Rolla B. Boughan and George W. Baab

Published Washington, D.C. : National Advisory Committee for Aeronautics, [1944]

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Description 1 online resource (8, [6] pages) : illustrations Series Wartime Report / National Advisory Committee for Aeronautics ; no. L204 Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L204 Summary Charts are presented for the calculation of the critical compressive stress - the stress at which local instability occurs - for idealized web- and T-stiffened panels, and examples of the use of the charts are given Notes NACA Wartime Report L-204 Originally issued as NACA as Advance Restricted Report L4H29 (August 1944) Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia Bibliography Includes bibliographical references Notes Print version record Subject Aluminum alloys. Plates (Engineering) Strains and stresses. Buckling (Mechanics) Airplanes -- Materials. Charts, diagrams, etc. aluminum alloy. stress. strain. buckling. warping. diagrams. Airplanes -- Materials Aluminum alloys Buckling (Mechanics) Charts, diagrams, etc. Plates (Engineering) Strains and stresses Form Electronic book Author Baab, George W United States. National Advisory Committee for Aeronautics. Langley Aeronautical Laboratory. ISBN 9781680156492 1680156497

Other Titles NACA Wartime Reports. Series L

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