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Handbook of structural stability. Part 3, Buckling of curved plates and shells /
Available theories and test data on buckling of curved plates and shells are reviewed. For torsion and external-pressure loadings, the test data are correlated in terms of linear buckling theories for both the elastic and inelastic ranges.
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Autor Corporativo: | |
| Otros Autores: | |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1957]
|
| Colección: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 3783. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 100 | 1 | |a Gerard, George. | |
| 245 | 1 | 0 | |a Handbook of structural stability. |n Part 3, |p Buckling of curved plates and shells / |c George Gerard and Herbert Becker. |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1957] | ||
| 300 | |a 1 online resource (iii, 154 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 Technical note / National Advisory Committee for Aeronautics ; |v 3783 | |
| 500 | |a NACA TN No. 3783. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a Available theories and test data on buckling of curved plates and shells are reviewed. For torsion and external-pressure loadings, the test data are correlated in terms of linear buckling theories for both the elastic and inelastic ranges. | |
| 520 | 3 | |a The cases which exhibit a marked disagreement between linear theory and test data include those of curved plates and cylinders under axial compression, cylinders under bending, and spherical plates under external pressure. These cases have been analyzed by a unified semiempirical approach for both the elastic and inelastic ranges which is satisfactory for analysis and design purposes. | |
| 520 | 3 | |a The effects of internal pressure on buckling of elements under uniaxial loads are discussed and data on various combined loadings are presented in interaction form. | |
| 588 | 0 | |a Print version record. | |
| 583 | 1 | |a digitized |c 2011 |h University of North Texas |l committed to preserve |2 pda |5 TXdn. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Structural analysis (Engineering) | |
| 650 | 0 | |a Stability. | |
| 650 | 0 | |a Plates (Engineering) |x Curvature. | |
| 650 | 0 | |a Shells (Engineering) |x Curvature. | |
| 650 | 0 | |a Buckling (Mechanics) | |
| 650 | 0 | |a Loads (Mechanics) | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 6 | |a Théorie des constructions. | |
| 650 | 6 | |a Stabilité. | |
| 650 | 6 | |a Flambage (Résistance des matériaux) | |
| 650 | 6 | |a Charges. | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 7 | |a structural analysis. |2 aat | |
| 650 | 7 | |a stability. |2 aat | |
| 650 | 7 | |a Buckling (Mechanics) |2 fast | |
| 650 | 7 | |a Loads (Mechanics) |2 fast | |
| 650 | 7 | |a Stability |2 fast | |
| 650 | 7 | |a Strains and stresses |2 fast | |
| 650 | 7 | |a Structural analysis (Engineering) |2 fast | |
| 700 | 1 | |a Becker, Herbert, |d 1918- | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 776 | 0 | 8 | |i Print version: |a Gerard, George. |t Handbook of structural stability. |d Washington, D.C. : National Advisory Committee for Aeronautics, [1957] |w (OCoLC)682898018 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 3783. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpHSSPIII5/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||