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Nonlinear large-deflection boundary-value problems of rectangular plates /
Relaxation and successive approximation methods are used to solve Von Karman's equations as applied to initially flat, rectangular plates with large deflections under either normal pressure or combined normal pressure and side thrust, and several specific cases are analyzed. The general method...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| 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. 1425. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 086 | 0 | |a Y 3.N 21/5:6/1425 | |
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| 049 | |a UAMI | ||
| 100 | 1 | |a Wang, Chi-Teh, |e author. | |
| 245 | 1 | 0 | |a Nonlinear large-deflection boundary-value problems of rectangular plates / |c by Chi-Teh Wang. |
| 264 | 1 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1948. | |
| 300 | |a 1 online resource (113 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 1425 | |
| 500 | |a Date of issue: March 1948. | ||
| 500 | |a Report no. NACA TN No. 1425. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a Relaxation and successive approximation methods are used to solve Von Karman's equations as applied to initially flat, rectangular plates with large deflections under either normal pressure or combined normal pressure and side thrust, and several specific cases are analyzed. The general method developed may be applied to bending and combined bending and buckling problems with practically any boundary conditions to any required degree of accuracy or applied to solve the membrane theory of the plate which applies when the deflection is very large in comparison with the thickness of the plate. | |
| 588 | 0 | |a Print version record. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Plates (Engineering) | |
| 650 | 0 | |a Boundary value problems. | |
| 650 | 0 | |a Relaxation methods (Mathematics) | |
| 650 | 6 | |a Plaques (Ingénierie) | |
| 650 | 6 | |a Problèmes aux limites. | |
| 650 | 6 | |a Méthodes de relaxation (Mathématiques) | |
| 650 | 7 | |a Boundary value problems |2 fast | |
| 650 | 7 | |a Plates (Engineering) |2 fast | |
| 650 | 7 | |a Relaxation methods (Mathematics) |2 fast | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics, |e issuing body. | |
| 776 | 0 | 8 | |i Print version: |a Wang, Chi-Teh. |t Nonlinear large-deflection boundary-value problems of rectangular plates |w (OCoLC)656395082 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 1425. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpNLDBVPR6/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||