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Buckling of thin-walled cylinder under axial compression and internal pressure /
An investigation was made of a thin-walled cylinder under axial compression and various internal pressures to study the effect of the internal pressure on the compressive buckling stress of the cylinder. A theoretical analysis based on a large-deflection theory was also made. The theoretically predi...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Autor Corporativo: | |
| Otros Autores: | , |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1950.
|
| Colección: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 2021. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 086 | 0 | |a Y 3.N 21/5:6/2021 | |
| 049 | |a UAMI | ||
| 100 | 1 | |a Lo, Hsu. | |
| 245 | 1 | 0 | |a Buckling of thin-walled cylinder under axial compression and internal pressure / |c Hsu Lo, Harold Crate, and Edward B. Schwartz. |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1950. | ||
| 300 | |a 1 online resource (29 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 National Advisory Committee for Aeronautics ; |v no. 2021 | |
| 500 | |a "January 1950." | ||
| 500 | |a NACA TN No. 2021. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a An investigation was made of a thin-walled cylinder under axial compression and various internal pressures to study the effect of the internal pressure on the compressive buckling stress of the cylinder. A theoretical analysis based on a large-deflection theory was also made. The theoretically predicted increase of compressive buckling stress due to internal pressure agrees fairly well with the experimental results. | |
| 588 | 0 | |a Print version record. | |
| 506 | |3 Use copy |f Restrictions unspecified |2 star |5 MiAaHDL | ||
| 533 | |a Electronic reproduction. |b [Place of publication not identified] : |c HathiTrust Digital Library, |d 2014. |5 MiAaHDL | ||
| 538 | |a Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002. |u http://purl.oclc.org/DLF/benchrepro0212 |5 MiAaHDL | ||
| 583 | 1 | |a digitized |c 2014 |h HathiTrust Digital Library |l committed to preserve |2 pda |5 MiAaHDL | |
| 506 | |a Access restricted to Ryerson students, faculty and staff. |5 CaOTR | ||
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Thin-walled structures. | |
| 650 | 0 | |a Cylinders. | |
| 650 | 0 | |a Buckling (Mechanics) | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 6 | |a Structures à parois minces. | |
| 650 | 6 | |a Cylindres. | |
| 650 | 6 | |a Flambage (Résistance des matériaux) | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 7 | |a cylinders (solids) |2 aat | |
| 650 | 7 | |a Buckling (Mechanics) |2 fast | |
| 650 | 7 | |a Cylinders |2 fast | |
| 650 | 7 | |a Strains and stresses |2 fast | |
| 650 | 7 | |a Thin-walled structures |2 fast | |
| 700 | 1 | |a Crate, Harold. | |
| 700 | 1 | |a Schwartz, Edward B. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 730 | 0 | |a Technical Report Archive & Image Library (TRAIL) | |
| 776 | 0 | 8 | |i Print version: |w (OCoLC)662520567 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 2021. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpBTWCUACR/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||