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Handbook of structural stability. Part 4, Failure of plates and composite elements /
Available theories on failure of flat plates are reviewed, and test data on the postbuckling behavior, effective width, and failure of flat curved plates are correlated.
| 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. 3784. |
| 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 4, |p Failure of plates and composite elements / |c George Gerard. |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1957] | ||
| 300 | |a 1 online resource (ii, 93 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 3784 | |
| 500 | |a NACA TN No. 3784. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a Available theories on failure of flat plates are reviewed, and test data on the postbuckling behavior, effective width, and failure of flat curved plates are correlated. | |
| 520 | 3 | |a Test data on the crippling strength of various formed and extruded shapes are reviewed, from which a generalized method of crippling analysis is formulated. The effects upon the crippling strength of alclad coatings and the increased properties in the corners of formed sections are investigated by use of this analysis. | |
| 520 | 3 | |a The generalized crippling analysis was applied to a variety of sections and materials in common use. It was found that the crippling strength of all the sections is governed in a simple manner by the developed length-thickness ratio and number of corners of the section. | |
| 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) | |
| 650 | 0 | |a Columns. | |
| 650 | 0 | |a Cylinders. | |
| 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 Plaques (Ingénierie) | |
| 650 | 6 | |a Cylindres. | |
| 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 cylinders (solids) |2 aat | |
| 650 | 7 | |a warping. |2 aat | |
| 650 | 7 | |a buckling. |2 aat | |
| 650 | 7 | |a stress. |2 aat | |
| 650 | 7 | |a strain. |2 aat | |
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| 650 | 7 | |a Columns. |2 fast |0 (OCoLC)fst00868845 | |
| 650 | 7 | |a Cylinders. |2 fast |0 (OCoLC)fst00886041 | |
| 650 | 7 | |a Loads (Mechanics) |2 fast |0 (OCoLC)fst01739107 | |
| 650 | 7 | |a Plates (Engineering) |2 fast |0 (OCoLC)fst01066785 | |
| 650 | 7 | |a Stability. |2 fast |0 (OCoLC)fst01131203 | |
| 650 | 7 | |a Strains and stresses. |2 fast |0 (OCoLC)fst01134288 | |
| 650 | 7 | |a Structural analysis (Engineering) |2 fast |0 (OCoLC)fst01135602 | |
| 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)682899193 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 3784. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpHSSPIIV5/toc |z Texto completo |
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