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Critical combinations of shear and longitudinal direct stress for long plates with transverse curvature /
A theoretical solution is presented for the buckling stresses of long plates with transverse curvature loaded in shear and longitudinal direct stress. The theoretical critical-stress combinations for plates having either simply supported or clamped edges are given in figures and tables and a compari...
| Clasificación: | Libro Electrónico |
|---|---|
| Autores principales: | , , |
| Autor Corporativo: | |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1947.
|
| Colección: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 1347. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 020 | |a 1680156063 |q (electronic bk.) | ||
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| 086 | 0 | |a Y 3.N 21/5:6/1347 | |
| 088 | |a NACA-TN-1347 | ||
| 049 | |a UAMI | ||
| 100 | 1 | |a Batdorf, S. B., |e author. | |
| 245 | 1 | 0 | |a Critical combinations of shear and longitudinal direct stress for long plates with transverse curvature / |c by S.B. Batdort, Murry Schildcrout, and Manuel Stein. |
| 264 | 1 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1947. | |
| 300 | |a 1 online resource (27 pages, 9 unnumbered pages) : |b illustrations, tables | ||
| 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 technical note ; |v number 1347 | |
| 500 | |a "Langley Memorial Aeronautical Laboratory." | ||
| 500 | |a Date of issue: June 1947. | ||
| 500 | |a Report no. NACA TN No. 1347. | ||
| 504 | |a Includes bibliographical references (pages 23-24) | ||
| 520 | 3 | |a A theoretical solution is presented for the buckling stresses of long plates with transverse curvature loaded in shear and longitudinal direct stress. The theoretical critical-stress combinations for plates having either simply supported or clamped edges are given in figures and tables and a comparison is made with a previous theoretical solution for simply supported plates. | |
| 588 | 0 | |a Print version record. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Plates (Engineering) | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 0 | |a Buckling (Mechanics) | |
| 650 | 0 | |a Loads (Mechanics) | |
| 650 | 0 | |a Shear (Mechanics) | |
| 650 | 6 | |a Plaques (Ingénierie) | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 6 | |a Flambage (Résistance des matériaux) | |
| 650 | 6 | |a Charges. | |
| 650 | 6 | |a Cisaillement (Mécanique) | |
| 650 | 7 | |a stress. |2 aat | |
| 650 | 7 | |a strain. |2 aat | |
| 650 | 7 | |a warping. |2 aat | |
| 650 | 7 | |a buckling. |2 aat | |
| 650 | 7 | |a shear stress. |2 aat | |
| 650 | 7 | |a Buckling (Mechanics) |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 Schildcrout, Murry, |e author. | |
| 700 | 1 | |a Stein, Manuel, |e author. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics, |e issuing body. | |
| 710 | 2 | |a Langley Aeronautical Laboratory. | |
| 776 | 0 | 8 | |i Print version: |a Batdorf, S.B. |t Critical combinations of shear and longitudinal direct stress for long plates with transverse curvature |w (OCoLC)652540878 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 1347. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpCCSLDSL1/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||