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A Unified theory of plastic buckling of columns and plates /
On the basis of modern plasticity considerations, a unified theory of plastic buckling applicable to both columns and plates has been developed. For uniform compression, the theory shows shows that long columns which bend without appreciable twisting require the tangent modulus and that long flanges...
| 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. 1556. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 049 | |a UAMI | ||
| 100 | 1 | |a Stowell, Elbridge Z. | |
| 245 | 1 | 2 | |a A Unified theory of plastic buckling of columns and plates / |c Elbridge Z. Stowell. |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1948. | ||
| 300 | |a 1 online resource (31 pages) : |b illustrations | ||
| 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 no. 1556 | |
| 500 | |a "April 1948." | ||
| 500 | |a NACA TN No. 1556. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a On the basis of modern plasticity considerations, a unified theory of plastic buckling applicable to both columns and plates has been developed. For uniform compression, the theory shows shows that long columns which bend without appreciable twisting require the tangent modulus and that long flanges which twist without appreciable bending require the secant modulus. Structures that both bend and twist when they buckle require a modulus which is a combination of the secant modulus and the tangent modulus. | |
| 588 | 0 | |a Print version record. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Columns. | |
| 650 | 0 | |a Plates (Engineering) | |
| 650 | 0 | |a Buckling (Mechanics) | |
| 650 | 0 | |a Mathematical analysis. | |
| 650 | 6 | |a Plaques (Ingénierie) | |
| 650 | 6 | |a Flambage (Résistance des matériaux) | |
| 650 | 6 | |a Analyse mathématique. | |
| 650 | 7 | |a warping. |2 aat | |
| 650 | 7 | |a buckling. |2 aat | |
| 650 | 7 | |a Buckling (Mechanics) |2 fast | |
| 650 | 7 | |a Columns |2 fast | |
| 650 | 7 | |a Mathematical analysis |2 fast | |
| 650 | 7 | |a Plates (Engineering) |2 fast | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 776 | 0 | 8 | |i Print version: |a Stowell, Elbridge Z. |t Unified theory of plastic buckling of columns and plates. |d Washington, D.C. : National Advisory Committee for Aeronautics, 1948 |w (OCoLC)657328900 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 1556. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpUTPBCPN3/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||