Title Bending of rectangular plates with large deflections / Chi-Teh Wang

Published Washington, D.C. : National Advisory Committee for Aeronautics, 1948

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Description 1 online resource (34 pages) : illustrations, tables Series National Advisory Committee for Aeronautics technical note ; number 1462 Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1462. Summary This document presents the solution of Von Karman equations for thin plates with large deflections for special cases of rectangular plates of 1.5 and 2.0 length-width ratios under uniform normal pressure. The boundary conditions approximate panels with riveted edges under normal pressure greater than that of the surrounding panels. Center deflections (to twice the plate thickness), membrane stresses, and extreme-fiber bending stresses are given as functions of the pressure. For small deflections, the results are consistent with those given by Timoshenko Notes "April 1948." NACA TN No. 1462 Bibliography Includes bibliographical references Notes Print version record Subject Plates (Engineering) Bending. Strains and stresses. Bending Plates (Engineering) Strains and stresses Form Electronic book Author United States. National Advisory Committee for Aeronautics. ISBN 9781680156089 168015608X

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