Cargando…
Flat sheet metal girder with very thin metal web : Part 2 : Sheet metal girders with spars resistant to bending - oblique uprights - stiffness /
Noting that the stiffness of the girder increases very rapidly as Beta increases, the result can be summed up as follows: When the cross stress preponderates in one direction and when the web plate is to be given the dimensions commensurate to its stresses, it is advisable (regardless of any ensuing...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Autor Corporativo: | |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1931]
|
| Colección: | Technical memorandums (United States. National Committee for Aeronautics) ;
no. 605. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
| LEADER | 00000cam a2200000 i 4500 | ||
|---|---|---|---|
| 001 | KNOVEL_ocn914568933 | ||
| 003 | OCoLC | ||
| 005 | 20231027140348.0 | ||
| 006 | m o d f | ||
| 007 | cr ||||||||||| | ||
| 008 | 150728s1931 dcua ot f000 0 eng d | ||
| 040 | |a SINTU |b eng |e pn |c SINTU |d SINTU |d KNOVL |d ZCU |d TJC |d OCLCQ |d UAB |d COO |d DKU |d OCLCQ |d CEF |d RRP |d YOU |d S2H |d OCLCO |d OCLCQ |d OCLCO |d OCLCQ |d TRAAL |d OCLCO | ||
| 019 | |a 951668825 |a 1363847327 | ||
| 020 | |a 9781680156591 |q (electronic bk.) | ||
| 020 | |a 1680156594 |q (electronic bk.) | ||
| 029 | 1 | |a GBVCP |b 856591769 | |
| 035 | |a (OCoLC)914568933 |z (OCoLC)951668825 |z (OCoLC)1363847327 | ||
| 050 | 4 | |a TA460 | |
| 082 | 0 | 4 | |a 620.166 |2 23 |
| 086 | 0 | |a Y 3.N 21/5:8/605 | |
| 088 | |a NACA-TM-605 | ||
| 049 | |a UAMI | ||
| 100 | 1 | |a Wagner, Herbert, |d 1900-1982. | |
| 245 | 1 | 0 | |a Flat sheet metal girder with very thin metal web : |b Part 2 : Sheet metal girders with spars resistant to bending - oblique uprights - stiffness / |c Herbert Wagner. |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1931] | ||
| 300 | |a 1 online resource (38, [6] 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 / National Advisory Committee for Aeronautics ; |v 605 | |
| 500 | |a "February, 1931." | ||
| 500 | |a NACA TM No. 605. | ||
| 500 | |a Translated from Zeitschrift fur Flugtechnik und Motorluftschiffahrt. Vol. 20, No. 9, May 14, No. 10, May 28, and No. 11, June 14, 1929, by the National Advisory Committee for Aeronautics. | ||
| 520 | 3 | |a Noting that the stiffness of the girder increases very rapidly as Beta increases, the result can be summed up as follows: When the cross stress preponderates in one direction and when the web plate is to be given the dimensions commensurate to its stresses, it is advisable (regardless of any ensuing structural difficulties) to set the uprights at about Beta = 120 degrees, thereby lowering the weight of the plate wall 15 percent (in contrast to Beta = 90 degrees), and raising the stiffness 55 percent. But, when the cross stresses alternate and are approximately of the same intensity in both directions, or, if the web plate thickness is determined by other structural reasons, then Beta = 90 degrees should be chosen. | |
| 588 | 0 | |a Print version record. | |
| 538 | |a Master and use copy. Digital master created according to Technical Guidelines for Digitizing Archival Materials for Electronic Access. U.S. National Archives and Records Administration, 2004. |u http://www.archives.gov/preservation/technical/guidelines.html |5 TxDN | ||
| 583 | 1 | |a digitized |c 2011 |h University of North Texas |l committed to preserve |2 pda |5 TXdn. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Sheet-metal. | |
| 650 | 0 | |a Girders. | |
| 650 | 0 | |a Mathematics. | |
| 650 | 0 | |a Struts (Engineering) | |
| 650 | 0 | |a Bending. | |
| 650 | 6 | |a Tôle. | |
| 650 | 6 | |a Poutres. | |
| 650 | 6 | |a Mathématiques. | |
| 650 | 6 | |a Étrésillons. | |
| 650 | 7 | |a sheet metal. |2 aat | |
| 650 | 7 | |a mathematics. |2 aat | |
| 650 | 7 | |a applied mathematics. |2 aat | |
| 650 | 7 | |a Bending |2 fast | |
| 650 | 7 | |a Girders |2 fast | |
| 650 | 7 | |a Mathematics |2 fast | |
| 650 | 7 | |a Sheet-metal |2 fast | |
| 650 | 7 | |a Struts (Engineering) |2 fast | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 776 | 0 | 8 | |i Print version: |a Wagner, Herbert. |t Flat sheet metal girder with very thin metal web. |d Washington, D.C. : National Advisory Committee for Aeronautics ; [1931] |w (OCoLC)695044344 |
| 830 | 0 | |a Technical memorandums (United States. National Committee for Aeronautics) ; |v no. 605. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpFSMGVT07/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||