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Bending of rectangular plates with large deflections /
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 tha...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Autor Corporativo: | |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1948.
|
| Colección: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 1462. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 049 | |a UAMI | ||
| 100 | 1 | |a Wang, Chi-Teh. | |
| 245 | 1 | 0 | |a Bending of rectangular plates with large deflections / |c Chi-Teh Wang. |
| 264 | 1 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1948. | |
| 300 | |a 1 online resource (34 pages) : |b illustrations, tables | ||
| 336 | |a text |b txt |2 rdacontent | ||
| 337 | |a computer |b c |2 rdamedia | ||
| 338 | |a online resource |b cr |2 rdacarrier | ||
| 490 | 1 | |a National Advisory Committee for Aeronautics technical note ; |v number 1462 | |
| 500 | |a "April 1948." | ||
| 500 | |a NACA TN No. 1462. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a 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. | |
| 588 | 0 | |a Print version record. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Plates (Engineering) | |
| 650 | 0 | |a Bending. | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 6 | |a Plaques (Ingénierie) | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 7 | |a Bending |2 fast | |
| 650 | 7 | |a Plates (Engineering) |2 fast | |
| 650 | 7 | |a Strains and stresses |2 fast | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 730 | 0 | |a Technical Report Archive & Image Library (TRAIL) | |
| 776 | 0 | 8 | |i Print version: |a Wang, Chi-Teh. |t Bending of rectangular plates with large deflections |w (OCoLC)656573574 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 1462. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpBRPLDNA4/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||