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Effect of normal pressure on the critical compressive and shear stress of curved sheet /
Results are presented of tests of two sets of 20 curved-sheet specimens to determine the effect of normal pressure on the critical compressive and shear stress of curved sheet. It was found that normal pressure raised the critical compressive and shear stress of curved sheet except when outward bulg...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Autores Corporativos: | , |
| Otros Autores: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1945]
|
| Colección: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L57. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 001 | KNOVEL_ocn914330037 | ||
| 003 | OCoLC | ||
| 005 | 20231027140348.0 | ||
| 006 | m o d f | ||
| 007 | cr ||||||||||| | ||
| 008 | 150724s1945 dcua obt f000 0 eng d | ||
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| 019 | |a 951668476 | ||
| 020 | |a 9781680156355 |q (electronic bk.) | ||
| 020 | |a 1680156357 |q (electronic bk.) | ||
| 029 | 1 | |a GBVCP |b 856591653 | |
| 035 | |a (OCoLC)914330037 |z (OCoLC)951668476 | ||
| 050 | 4 | |a TA660.B4 | |
| 082 | 0 | 4 | |a 624.17723 |2 23 |
| 049 | |a UAMI | ||
| 100 | 1 | |a Rafel, Norman. | |
| 245 | 1 | 0 | |a Effect of normal pressure on the critical compressive and shear stress of curved sheet / |c Norman Rafel and Charles W. Sandlin, Jr. |
| 246 | 3 | |a NACA Wartime Reports. Series L. | |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1945] | ||
| 300 | |a 1 online resource (7, [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. L57 | |
| 500 | |a NACA Wartime Report L-57. | ||
| 500 | |a Originally issued as NACA as Advance Restricted Report L5B10 (March 1945). | ||
| 500 | |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a Results are presented of tests of two sets of 20 curved-sheet specimens to determine the effect of normal pressure on the critical compressive and shear stress of curved sheet. It was found that normal pressure raised the critical compressive and shear stress of curved sheet except when outward bulging occurred in compression, in which case the critical stress was lowered by normal pressure. | |
| 588 | 0 | |a Print version record. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Box beams. | |
| 650 | 0 | |a Aluminum alloys. | |
| 650 | 0 | |a Plates (Engineering) |x Curvature. | |
| 650 | 0 | |a Loads (Mechanics) | |
| 650 | 0 | |a Shear (Mechanics) | |
| 650 | 0 | |a Buckling (Mechanics) | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 0 | |a Charts, diagrams, etc. | |
| 650 | 6 | |a Poutres-caissons. | |
| 650 | 6 | |a Aluminium |x Alliages. | |
| 650 | 6 | |a Charges. | |
| 650 | 6 | |a Cisaillement (Mécanique) | |
| 650 | 6 | |a Flambage (Résistance des matériaux) | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 6 | |a Tableaux, graphiques, etc. | |
| 650 | 7 | |a box beams. |2 aat | |
| 650 | 7 | |a aluminum alloy. |2 aat | |
| 650 | 7 | |a shear stress. |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 | |
| 650 | 7 | |a diagrams. |2 aat | |
| 650 | 7 | |a Aluminum alloys |2 fast | |
| 650 | 7 | |a Box beams |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 Shear (Mechanics) |2 fast | |
| 650 | 7 | |a Strains and stresses |2 fast | |
| 700 | 1 | |a Sandlin, Charles W. | |
| 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 and shear stress of curved sheet. |d Washington, D.C. : National Advisory Committee for Aeronautics, [1945] |w (OCoLC)705351009 |
| 830 | 0 | |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ; |v no. L57. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpENPCCSS3/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||