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Plastic buckling of simply supported compressed plates /
Tests were made of 14S-T6 aluminum-alloy square tubes to determine the critical compressive stress of simply supported flat plates in the plastic range. Excellent agreement is shown with with Stowell's theory for plastic buckling which is based upon a deformation theory of plasticity, close agr...
| Clasificación: | Libro Electrónico |
|---|---|
| Autores principales: | , |
| Autores Corporativos: | , |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1949.
|
| Colección: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 1817. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 008 | 150824s1949 dcua obt f000 0 eng d | ||
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| 020 | |a 9781680156157 |q (electronic bk.) | ||
| 020 | |a 1680156152 |q (electronic bk.) | ||
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| 035 | |a (OCoLC)919094657 | ||
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| 086 | 0 | |a Y 3.N 21/5:6/1817 | |
| 088 | |a NACA-TN-1817 | ||
| 049 | |a UAMI | ||
| 100 | 1 | |a Pride, Richard A., |e author. | |
| 245 | 1 | 0 | |a Plastic buckling of simply supported compressed plates / |c Richard A. Pride and George J. Heimerl. |
| 264 | 1 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1949. | |
| 300 | |a 1 online resource (22 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 ; |v number 1817 | |
| 500 | |a Date of issue: April 1949. | ||
| 500 | |a Report no. NACA-TN-1817. | ||
| 504 | |a Includes bibliographical references (page 10) | ||
| 520 | 3 | |a Tests were made of 14S-T6 aluminum-alloy square tubes to determine the critical compressive stress of simply supported flat plates in the plastic range. Excellent agreement is shown with with Stowell's theory for plastic buckling which is based upon a deformation theory of plasticity, close agreement with two other deformation-type theories of plastic buckling and withthe secant-modulus method, and marked disagreement with a buckling theory based upon a flow theory of plasticity. | |
| 588 | 0 | |a Print version record. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Aluminum alloys. | |
| 650 | 0 | |a Tubes. | |
| 650 | 0 | |a Deformations (Mechanics) | |
| 650 | 0 | |a Buckling (Mechanics) | |
| 650 | 0 | |a Plasticity. | |
| 650 | 0 | |a Pipe. | |
| 650 | 6 | |a Aluminium |x Alliages. | |
| 650 | 6 | |a Tubes. | |
| 650 | 6 | |a Déformations (Mécanique) | |
| 650 | 6 | |a Flambage (Résistance des matériaux) | |
| 650 | 6 | |a Plasticité. | |
| 650 | 6 | |a Tuyaux. | |
| 650 | 7 | |a aluminum alloy. |2 aat | |
| 650 | 7 | |a pipes (conduits) |2 aat | |
| 650 | 7 | |a deformation. |2 aat | |
| 650 | 7 | |a plasticity. |2 aat | |
| 650 | 7 | |a tubes (object forms) |2 aat | |
| 650 | 7 | |a Aluminum alloys |2 fast | |
| 650 | 7 | |a Buckling (Mechanics) |2 fast | |
| 650 | 7 | |a Deformations (Mechanics) |2 fast | |
| 650 | 7 | |a Plasticity |2 fast | |
| 650 | 7 | |a Tubes |2 fast | |
| 700 | 1 | |a Heimerl, George J., |e author. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 710 | 2 | |a Langley Aeronautical Laboratory. | |
| 730 | 0 | |a Technical Report Archive & Image Library (TRAIL) | |
| 776 | 0 | 8 | |i Print version: |a Pride, Richard A. |t Plastic buckling of simply supported compressed plates |w (OCoLC)659780939 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 1817. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpPBSSCPN8/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||