Bending of rectangular plates with large deflections /
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| Corporate Authors: | , |
| Format: | Government Document eBook |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1948.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 1462. |
| Subjects: | |
| Online Access: | Connect to the full text of this electronic book |
| Abstract: | 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. |
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| Item Description: | "April 1948." NACA TN Number 1462. |
| Physical Description: | 1 online resource (34 pages) : illustrations, tables. |
| Bibliography: | Includes bibliographical references. |
| ISBN: | 9781680156089 168015608X |