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Compressive buckling of simply supported curved plates and cylinders of sandwich construction /
Theoretical solutions are presented for the buckling in uniform axial compression of two types of simply supported curved sandwich plates: the corrugated-core type and the isotropic type. Results are given in the form of equations and curves.
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Autor Corporativo: | |
| Otros Autores: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1952.
|
| Colección: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 2601. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 008 | 150724s1952 ohua obt f000 0 eng d | ||
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| 020 | |a 9781680156232 |q (electronic bk.) | ||
| 020 | |a 1680156233 |q (electronic bk.) | ||
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| 035 | |a (OCoLC)914328448 |z (OCoLC)951667414 | ||
| 050 | 4 | |a TA660.P6 | |
| 082 | 0 | 4 | |a 624.17765 |2 23 |
| 049 | |a UAMI | ||
| 100 | 1 | |a Stein, Manuel. | |
| 245 | 1 | 0 | |a Compressive buckling of simply supported curved plates and cylinders of sandwich construction / |c Manuel Stein and J. Mayers. |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1952. | ||
| 300 | |a 1 online resource (34 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 no. 2601 | |
| 500 | |a "January 1952." | ||
| 500 | |a NACA TN No. 2601. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a Theoretical solutions are presented for the buckling in uniform axial compression of two types of simply supported curved sandwich plates: the corrugated-core type and the isotropic type. Results are given in the form of equations and curves. | |
| 588 | 0 | |a Print version record. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Plates (Engineering) |x Curvature. | |
| 650 | 0 | |a Cylinders. | |
| 650 | 0 | |a Sandwich construction. | |
| 650 | 0 | |a Buckling (Mechanics) | |
| 650 | 0 | |a Loads (Mechanics) | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 6 | |a Cylindres. | |
| 650 | 6 | |a Construction sandwich. | |
| 650 | 6 | |a Flambage (Résistance des matériaux) | |
| 650 | 6 | |a Charges. | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 7 | |a cylinders (solids) |2 aat | |
| 650 | 7 | |a buckling. |2 aat | |
| 650 | 7 | |a warping. |2 aat | |
| 650 | 7 | |a stress. |2 aat | |
| 650 | 7 | |a strain. |2 aat | |
| 650 | 7 | |a Buckling (Mechanics) |2 fast | |
| 650 | 7 | |a Cylinders |2 fast | |
| 650 | 7 | |a Loads (Mechanics) |2 fast | |
| 650 | 7 | |a Sandwich construction |2 fast | |
| 650 | 7 | |a Strains and stresses |2 fast | |
| 700 | 1 | |a Mayers, J. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 776 | 0 | 8 | |i Print version: |a Stein, Manuel. |t Compressive buckling of simply supported curved plates and cylinders of sandwich construction. |d Washington, D.C. : National Advisory Committee for Aeronautics, 1952 |w (OCoLC)666432975 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 2601. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpCBSSCPC5/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||