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Critical stress for an infinitely long flat plate with elastically restrained edges under combined shear and direct stress /
A simple interaction curve is presented for evaluating the conditions of combined shear and direct stress under which an infinitely long, flat plate with equal elastic restraints against rotation along the edges will become unstable. The theoretical work that led to the interaction curve is presente...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Autores Corporativos: | , |
| Otros Autores: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1943]
|
| Colección: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L340. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 082 | 0 | 4 | |a 624.17765 |2 23 |
| 049 | |a UAMI | ||
| 100 | 1 | |a Stowell, Elbridge Z. | |
| 245 | 1 | 0 | |a Critical stress for an infinitely long flat plate with elastically restrained edges under combined shear and direct stress / |c Elbridge Z. Stowell and Edward B. Schwartz. |
| 246 | 3 | |a NACA Wartime Reports. Series L. | |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1943] | ||
| 300 | |a 1 online resource (16, [3] 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 Wartime Report / National Advisory Committee for Aeronautics ; |v no. L340 | |
| 500 | |a NACA Wartime Report L-340. | ||
| 500 | |a Originally issued as NACA as Advance Restricted Report L3K13 (November 1943). | ||
| 500 | |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a A simple interaction curve is presented for evaluating the conditions of combined shear and direct stress under which an infinitely long, flat plate with equal elastic restraints against rotation along the edges will become unstable. The theoretical work that led to the interaction curve is presented in the form of appendixes. | |
| 588 | 0 | |a Print version record. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Plates (Engineering) | |
| 650 | 0 | |a Shear (Mechanics) | |
| 650 | 0 | |a Buckling (Mechanics) | |
| 650 | 0 | |a Loads (Mechanics) | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 0 | |a Charts, diagrams, etc. | |
| 650 | 6 | |a Plaques (Ingénierie) | |
| 650 | 6 | |a Cisaillement (Mécanique) | |
| 650 | 6 | |a Flambage (Résistance des matériaux) | |
| 650 | 6 | |a Charges. | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 6 | |a Tableaux, graphiques, etc. | |
| 650 | 7 | |a shear stress. |2 aat | |
| 650 | 7 | |a diagrams. |2 aat | |
| 650 | 7 | |a Buckling (Mechanics) |2 fast | |
| 650 | 7 | |a Charts, diagrams, etc. |2 fast | |
| 650 | 7 | |a Loads (Mechanics) |2 fast | |
| 650 | 7 | |a Plates (Engineering) |2 fast | |
| 650 | 7 | |a Shear (Mechanics) |2 fast | |
| 650 | 7 | |a Strains and stresses |2 fast | |
| 700 | 1 | |a Schwartz, Edward B. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 710 | 2 | |a Langley Aeronautical Laboratory. | |
| 776 | 0 | 8 | |i Print version: |a Stowell, Elbridge Z. |t Critical stress for an infinitely long flat plate with elastically restrained edges under combined shear and direct stress. |d Washington, D.C. : National Advisory Committee for Aeronautics, [1943] |w (OCoLC)707629297 |
| 830 | 0 | |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ; |v no. L340. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpCSILFPE1/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||