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Effect of normal pressure on the critical compressive stress of curved sheet /
Results are presented of tests of two specimens tested to study the effect of normal pressure on the critical compressive stress for thin curved sheets. These specimens are designated by their respective rib spacings of 10 inches and 30 inches. The relationship between compressive stress and normal...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Autores Corporativos: | , |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1942]
|
| Colección: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L258. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 001 | KNOVEL_ocn914330185 | ||
| 003 | OCoLC | ||
| 005 | 20231027140348.0 | ||
| 006 | m o d f | ||
| 007 | cr ||||||||||| | ||
| 008 | 150724s1942 dcua ot f000 0 eng d | ||
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| 019 | |a 951667782 | ||
| 020 | |a 9781680156348 |q (electronic bk.) | ||
| 020 | |a 1680156349 |q (electronic bk.) | ||
| 029 | 1 | |a GBVCP |b 856591661 | |
| 035 | |a (OCoLC)914330185 |z (OCoLC)951667782 | ||
| 050 | 4 | |a QC885 | |
| 082 | 0 | 4 | |a 551.54 |2 23 |
| 049 | |a UAMI | ||
| 100 | 1 | |a Rafel, Norman. | |
| 245 | 1 | 0 | |a Effect of normal pressure on the critical compressive stress of curved sheet / |c Norman Rafel. |
| 246 | 3 | |a NACA Wartime Reports. Series L. | |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1942] | ||
| 300 | |a 1 online resource (2, [8] 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. L258 | |
| 500 | |a NACA Wartime Report L-258. | ||
| 500 | |a Originally issued as NACA as a Restricted Bulletin (November 1942). | ||
| 500 | |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. | ||
| 520 | 3 | |a Results are presented of tests of two specimens tested to study the effect of normal pressure on the critical compressive stress for thin curved sheets. These specimens are designated by their respective rib spacings of 10 inches and 30 inches. The relationship between compressive stress and normal pressure at which buckles disappeared is independent of whether the buckles were made to disappear by increase of normal pressure or decrease of compressive stress. | |
| 588 | 0 | |a Print version record. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Atmospheric pressure. | |
| 650 | 0 | |a Buckling (Mechanics) | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 0 | |a Loads (Mechanics) | |
| 650 | 0 | |a Charts, diagrams, etc. | |
| 650 | 6 | |a Pression atmosphérique. | |
| 650 | 6 | |a Flambage (Résistance des matériaux) | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 6 | |a Charges. | |
| 650 | 6 | |a Tableaux, graphiques, etc. | |
| 650 | 7 | |a atmospheric pressure. |2 aat | |
| 650 | 7 | |a buckling. |2 aat | |
| 650 | 7 | |a warping. |2 aat | |
| 650 | 7 | |a stress. |2 aat | |
| 650 | 7 | |a strain. |2 aat | |
| 650 | 7 | |a diagrams. |2 aat | |
| 650 | 7 | |a Atmospheric pressure |2 fast | |
| 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 Strains and stresses |2 fast | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 710 | 2 | |a Langley Aeronautical Laboratory. | |
| 776 | 0 | 8 | |i Print version: |a Rafel, Norman. |t Effect of normal pressure on the critical compressive stress of curved sheet. |d Washington, D.C. : National Advisory Committee for Aeronautics, [1942] |w (OCoLC)707099582 |
| 830 | 0 | |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ; |v no. L258. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpENPCCSC1/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||