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Rectangular shell plating under uniformly distributed hydrostatic pressure /
A check of the calculation methods used by Foppl and Henky for investigating the reliability of shell plating under hydrostatic pressure has proved that the formulas yield practical results within the elastic range of the material. Foppl's approximate calculation leaves one on the safe side. It...
| Clasificación: | Libro Electrónico |
|---|---|
| Autores principales: | , |
| Autor Corporativo: | |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Commitee for Aeronautics,
[1940]
|
| Colección: | Technical memorandum (United States. National Advisory Committee for Aeronautics) ;
no. 965. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 100 | 1 | |a Neubert, M., |e author. | |
| 245 | 1 | 0 | |a Rectangular shell plating under uniformly distributed hydrostatic pressure / |c by M. Neubert and A. Sommer. |
| 264 | 1 | |a Washington, D.C. : |b National Advisory Commitee for Aeronautics, |c [1940] | |
| 300 | |a 1 online resource (7 pages, 3 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 National Advisory Committee for Aeronautics technical memorandums ; ‡v 965 | |
| 500 | |a "December 1940." | ||
| 500 | |a NACA TM No. 965. | ||
| 500 | |a Translated from Luftfahrtforschung. Vol. 17, No. 7, pp. 207-210, July 20, 1940, by the National Advisory Commitee for Aeronautics. | ||
| 504 | |a Includes bibliographical references (page 7) | ||
| 520 | 3 | |a A check of the calculation methods used by Foppl and Henky for investigating the reliability of shell plating under hydrostatic pressure has proved that the formulas yield practical results within the elastic range of the material. Foppl's approximate calculation leaves one on the safe side. It further was found on the basis of the marked ductility of the shell plating under tensile stress that the strength is from 50 to 100 percent higher in the elastic range than expected by either method. | |
| 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 2011. |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 2011 |h HathiTrust Digital Library |l committed to preserve |2 pda |5 MiAaHDL | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Shells (Engineering) | |
| 650 | 0 | |a Plates (Engineering) | |
| 650 | 0 | |a Hydrostatic pressure. | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 0 | |a Mathematics. | |
| 650 | 2 | |a Hydrostatic Pressure | |
| 650 | 2 | |a Mathematics | |
| 650 | 6 | |a Coques (Ingénierie) | |
| 650 | 6 | |a Plaques (Ingénierie) | |
| 650 | 6 | |a Pression hydrostatique. | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 6 | |a Mathématiques. | |
| 650 | 7 | |a shell structures. |2 aat | |
| 650 | 7 | |a Hydrostatic pressure |2 fast | |
| 650 | 7 | |a Mathematics |2 fast | |
| 650 | 7 | |a Plates (Engineering) |2 fast | |
| 650 | 7 | |a Shells (Engineering) |2 fast | |
| 650 | 7 | |a Strains and stresses |2 fast | |
| 700 | 1 | |a Sommer, A., |e author. | |
| 710 | 1 | |a United States. |b National Advisory Commitee for Aeronautics. | |
| 730 | 0 | |a Technical Report Archive & Image Library (TRAIL) | |
| 776 | 0 | 8 | |i Print version: |a Neubert, M. |t Rectangular shell plating under uniformly distributed hydrostatic pressure |w (OCoLC)697281935 |
| 830 | 0 | |a Technical memorandum (United States. National Advisory Committee for Aeronautics) ; |v no. 965. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpRSPUDHP1/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||