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Tension fields in originally curved, thin sheets during shearing stresses /
The analysis of the stresses in the sheet and stiffeners is predicated upon the direction of the wrinkles, particularly the tensile stresses (principal stresses). This analysis and the calculation of stresses after buckling form the subject of the present article. It includes: 1) metal cylinders wit...
| Clasificación: | Libro Electrónico |
|---|---|
| Autores principales: | , |
| Autor Corporativo: | |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Commitee for Aeronautics,
[1935]
|
| Colección: | Technical memorandum (United States. National Advisory Committee for Aeronautics) ;
no. 774. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 100 | 1 | |a Wagner, H., |e author. | |
| 245 | 1 | 0 | |a Tension fields in originally curved, thin sheets during shearing stresses / |c H. Wagner and W. Ballerstedt. |
| 264 | 1 | |a Washington, D.C. : |b National Advisory Commitee for Aeronautics, |c [1935] | |
| 300 | |a 1 online resource (11 pages, 2 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 774 | |
| 500 | |a "August 1935." | ||
| 500 | |a NACA TM No. 774. | ||
| 500 | |a Translated from Luftfahrtforschung. Vol. 12, No. 2, pp. 70-74, May 16, 1935, by the National Advisory Commitee for Aeronautics. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a The analysis of the stresses in the sheet and stiffeners is predicated upon the direction of the wrinkles, particularly the tensile stresses (principal stresses). This analysis and the calculation of stresses after buckling form the subject of the present article. It includes: 1) metal cylinders with closely spaced longitudinal stiffeners; 2) metal cylinders with closely spaced transverse rings. | |
| 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 2010. |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 2010 |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 Shells (Engineering) | |
| 650 | 0 | |a Thin-walled structures. | |
| 650 | 0 | |a Curvature. | |
| 650 | 0 | |a Shear (Mechanics) | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 6 | |a Coques (Ingénierie) | |
| 650 | 6 | |a Structures à parois minces. | |
| 650 | 6 | |a Courbure. | |
| 650 | 6 | |a Cisaillement (Mécanique) | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 7 | |a shell structures. |2 aat | |
| 650 | 7 | |a shear stress. |2 aat | |
| 650 | 7 | |a strain. |2 aat | |
| 650 | 7 | |a stress. |2 aat | |
| 650 | 7 | |a Curvature. |2 fast |0 (OCoLC)fst00885436 | |
| 650 | 7 | |a Shear (Mechanics) |2 fast |0 (OCoLC)fst01115422 | |
| 650 | 7 | |a Shells (Engineering) |2 fast |0 (OCoLC)fst01115734 | |
| 650 | 7 | |a Strains and stresses. |2 fast |0 (OCoLC)fst01134288 | |
| 650 | 7 | |a Thin-walled structures. |2 fast |0 (OCoLC)fst01150059 | |
| 700 | 1 | |a Ballerstedt, W., |e author. | |
| 710 | 1 | |a United States. |b National Advisory Commitee for Aeronautics. | |
| 776 | 0 | 8 | |i Print version: |a Wagner, H. |t Tension fields in originally curved, thin sheets during shearing stresses |w (OCoLC)696180837 |
| 830 | 0 | |a Technical memorandum (United States. National Advisory Committee for Aeronautics) ; |v no. 774. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpTFOCTSS1/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||