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The effect of internal pressure on the buckling stress of thin-walled circular cylinders under torsion /
The results of a series of tests to determine the effect of internal pressure on the buckling load of a thin cylinder under an applied torque indicated that internal pressure raises the shear buckling stress. The experimental results were analyzed with the aid of previously developed theory and a si...
| Clasificación: | Libro Electrónico |
|---|---|
| Autores principales: | , , |
| Autores Corporativos: | , |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1944]
|
| Colección: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L67. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 020 | |a 9781680156362 |q (electronic bk.) | ||
| 020 | |a 1680156365 |q (electronic bk.) | ||
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| 035 | |a (OCoLC)919146897 | ||
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| 082 | 0 | 4 | |a 621.4772 |2 23 |
| 086 | 0 | |a Y 3.N 21/5:11/L67 | |
| 088 | |a NACA WR L67 | ||
| 088 | |a NACA ARR L4E27 | ||
| 049 | |a UAMI | ||
| 100 | 1 | |a Crate, Harold, |e author. | |
| 245 | 1 | 4 | |a The effect of internal pressure on the buckling stress of thin-walled circular cylinders under torsion / |c Harold Crate, S.B. Batdorf, and George W. Baab. |
| 246 | 3 | |a NACA Wartime Reports. Series L. | |
| 264 | 1 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1944] | |
| 300 | |a 1 online resource (15 pages, 9 unnumbered 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 number L67 | |
| 500 | |a NACA Wartime Report L-67. | ||
| 500 | |a Originally issued as NACA as Advance Restricted Report L4E27 (May 1944). | ||
| 500 | |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. | ||
| 520 | 3 | |a The results of a series of tests to determine the effect of internal pressure on the buckling load of a thin cylinder under an applied torque indicated that internal pressure raises the shear buckling stress. The experimental results were analyzed with the aid of previously developed theory and a simple interaction formula was derived. | |
| 588 | 0 | |a Print version record. | |
| 504 | |a Includes bibliographical references. | ||
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Cylinders. | |
| 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 Cylindres. | |
| 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 cylinders (solids) |2 aat | |
| 650 | 7 | |a shear stress. |2 aat | |
| 650 | 7 | |a warping. |2 aat | |
| 650 | 7 | |a buckling. |2 aat | |
| 650 | 7 | |a strain. |2 aat | |
| 650 | 7 | |a 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 Cylinders |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 Batdorf, S. B., |e author. | |
| 700 | 1 | |a Baab, George W., |e author. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 710 | 2 | |a Langley Aeronautical Laboratory. | |
| 776 | 0 | 8 | |i Print version: |a Crate, Harold. |t Effect of internal pressure on the buckling stress of thin-walled circular cylinders under torsion |w (OCoLC)705374267 |
| 830 | 0 | |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ; |v no. L67. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpEIPBSTW3/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||