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Handbook of structural stability. Part VI, Strength of stiffened curved plates and shells /
A comprehensive review of failure of stiffened curved plates and shells is presented.
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Autor Corporativo: | |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1958]
|
| Colección: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 3786. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 100 | 1 | |a Becker, Herbert, |d 1918- |e author. | |
| 245 | 1 | 0 | |a Handbook of structural stability. |n Part VI, |p Strength of stiffened curved plates and shells / |c Herbert Becker. |
| 264 | 1 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1958] | |
| 300 | |a 1 online resource (iii, 82 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 3786 | |
| 500 | |a NACA TN No. 3786. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a A comprehensive review of failure of stiffened curved plates and shells is presented. | |
| 520 | 3 | |a Panel instability in stiffened curved plates and general instability of stiffened cylinders are discussed. The loadings considered for the plates are axial, shear, and the combination of the two. For the cylinders, bending, external pressure, torsion, transverse shear, and combinations of these loads are considered. | |
| 520 | 3 | |a General instability in stiffened cylinders was investigated. For bending and torsion loads, test data and theory were correlated. For external pressure several existing theories were compared. As a result of this investigation a unified theoretical approach to analysis of general instability in stiffened cylinders was developed. | |
| 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 Strength of materials. | |
| 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 Résistance des matériaux. | |
| 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 strength of materials. |2 aat | |
| 650 | 7 | |a buckling. |2 aat | |
| 650 | 7 | |a warping. |2 aat | |
| 650 | 7 | |a strain. |2 aat | |
| 650 | 7 | |a stress. |2 aat | |
| 650 | 7 | |a Buckling (Mechanics) |2 fast |0 (OCoLC)fst00840001 | |
| 650 | 7 | |a Loads (Mechanics) |2 fast |0 (OCoLC)fst01739107 | |
| 650 | 7 | |a Stability. |2 fast |0 (OCoLC)fst01131203 | |
| 650 | 7 | |a Strains and stresses. |2 fast |0 (OCoLC)fst01134288 | |
| 650 | 7 | |a Strength of materials. |2 fast |0 (OCoLC)fst01134837 | |
| 650 | 7 | |a Structural analysis (Engineering) |2 fast |0 (OCoLC)fst01135602 | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 776 | 0 | 8 | |i Print version: |a Becker, Herbert. |t Handbook of structural stability |w (OCoLC)682898406 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 3786. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpHSSPVIS1/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||