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The strength of shell bodies-- theory and practice /
The monocoque form of airplane construction has introduced a number of new problems to the stress calculator and the designer. The problems for the stress calculator fall into two groups: the determination of the stress condition (shell statics) and the determination of the failing strength (shell s...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Autor Corporativo: | |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Commitee for Aeronautics,
[1937]
|
| Colección: | Technical memorandum (United States. National Advisory Committee for Aeronautics) ;
no. 838. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 088 | |a NACA TM 838 | ||
| 049 | |a UAMI | ||
| 100 | 1 | |a Ebner, H., |e author. | |
| 245 | 1 | 4 | |a The strength of shell bodies-- theory and practice / |c H. Ebner. |
| 264 | 1 | |a Washington, D.C. : |b National Advisory Commitee for Aeronautics, |c [1937] | |
| 300 | |a 1 online resource (51 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 Technical memorandums ; |v number 838 | |
| 500 | |a "September 1937." | ||
| 500 | |a NACA TM No. 838. | ||
| 500 | |a Translated from Luftfahrtforschung. Vol. 14, No. 3, March 20, 1937, by the National Advisory Commitee for Aeronautics. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a The monocoque form of airplane construction has introduced a number of new problems to the stress calculator and the designer. The problems for the stress calculator fall into two groups: the determination of the stress condition (shell statics) and the determination of the failing strength (shell strength). The present report summarizes the most important theoretical and experimental results on this subject. | |
| 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 Monocoque construction. | |
| 650 | 0 | |a Shells (Engineering) | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 0 | |a Mathematics. | |
| 650 | 6 | |a Coques (Ingénierie) | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 6 | |a Mathématiques. | |
| 650 | 7 | |a shell structures. |2 aat | |
| 650 | 7 | |a stress. |2 aat | |
| 650 | 7 | |a strain. |2 aat | |
| 650 | 7 | |a applied mathematics. |2 aat | |
| 650 | 7 | |a mathematics. |2 aat | |
| 650 | 7 | |a Mathematics |2 fast | |
| 650 | 7 | |a Monocoque construction |2 fast | |
| 650 | 7 | |a Shells (Engineering) |2 fast | |
| 650 | 7 | |a Strains and stresses |2 fast | |
| 710 | 1 | |a United States. |b National Advisory Commitee for Aeronautics. | |
| 776 | 0 | 8 | |i Print version: |a Ebner, H. |t Strength of shell bodies - theory and practice |w (OCoLC)696399361 |
| 830 | 0 | |a Technical memorandum (United States. National Advisory Committee for Aeronautics) ; |v no. 838. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpSSBTPNA1/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||