Cargando…
Some investigations of the general instability of stiffened metal cylinders. VIII, Stiffened metal cylinders subjected to pure torsion /
An experimental investigation of the general instability of reinforced thin-walled metal cylinders was carried out at the California Institute of Technology. The basic parameters involved were the spacing and sectional properties of stiffening elements, the wall thickness, and the diameter of the cy...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington :
National Advisory Committee for Aeronautics,
May 1947.
|
| Colección: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 1197. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
| LEADER | 00000cam a2200000 i 4500 | ||
|---|---|---|---|
| 001 | KNOVEL_ocn914576169 | ||
| 003 | OCoLC | ||
| 005 | 20231027140348.0 | ||
| 006 | m o d f | ||
| 007 | cr ||||||||||| | ||
| 008 | 150728e194705 dcua obt f000 0 eng c | ||
| 040 | |a SINTU |b eng |e rda |e pn |c SINTU |d SINTU |d OCLCO |d KNOVL |d ZCU |d OCLCQ |d UAB |d OCLCF |d OCLCQ |d CEF |d RRP |d UMR |d MERER |d OCLCQ |d YOU |d OCL |d GPO |d S2H |d OCLCO |d TRAAL |d GZM |d OCLCQ |d OCLCO |d OCLCQ | ||
| 019 | |a 951676137 |a 1222909559 | ||
| 020 | |a 9781680156126 |q (electronic bk.) | ||
| 020 | |a 1680156128 |q (electronic bk.) | ||
| 029 | 1 | |a GBVCP |b 856591777 | |
| 035 | |a (OCoLC)914576169 |z (OCoLC)951676137 |z (OCoLC)1222909559 | ||
| 042 | |a pcc | ||
| 050 | 4 | |a TA660.C9 | |
| 082 | 0 | 4 | |a 624.17 |2 23 |
| 086 | 0 | |a Y 3.N 21/5:6/1197 | |
| 088 | |a NACA-TN-1197 | ||
| 049 | |a UAMI | ||
| 100 | 1 | |a Dunn, Louis |q (Louis Gerhardus), |d 1908-1979, |e author. | |
| 245 | 1 | 0 | |a Some investigations of the general instability of stiffened metal cylinders. |n VIII, |p Stiffened metal cylinders subjected to pure torsion / |c by Louis G. Dunn. |
| 264 | 1 | |a Washington : |b National Advisory Committee for Aeronautics, |c May 1947. | |
| 300 | |a 1 online resource (14, 39 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 note ; |v no. 1197 | |
| 588 | 0 | |a Online resource; title from PDF cover (UNT website, viewed August 29, 2019). | |
| 500 | |a Agency is no longer active. No federal Depository Library Program (FDLP) item number has been assigned. | ||
| 500 | |a "May 1947"--Cover | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a An experimental investigation of the general instability of reinforced thin-walled metal cylinders was carried out at the California Institute of Technology. The basic parameters involved were the spacing and sectional properties of stiffening elements, the wall thickness, and the diameter of the cylinder. An analysis of the experimental data led to a suitable parameter for estimating the general-instability stress of reinforced metal cylinders when subjected to pure torsion loading. | |
| 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 Cylinders. | |
| 650 | 0 | |a Thin-walled structures. | |
| 650 | 0 | |a Reinforcing bars. | |
| 650 | 0 | |a Loads (Mechanics) | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 0 | |a Torsion. | |
| 650 | 6 | |a Cylindres. | |
| 650 | 6 | |a Structures à parois minces. | |
| 650 | 6 | |a Barres d'armature. | |
| 650 | 6 | |a Charges. | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 6 | |a Torsion (Mécanique) | |
| 650 | 7 | |a cylinders (solids) |2 aat | |
| 650 | 7 | |a reinforcing bars. |2 aat | |
| 650 | 7 | |a torsional stress. |2 aat | |
| 650 | 7 | |a Thin-walled structures. |2 fast |0 (OCoLC)fst01150059 | |
| 650 | 7 | |a Cylinders. |2 fast |0 (OCoLC)fst00886041 | |
| 650 | 7 | |a Loads (Mechanics) |2 fast |0 (OCoLC)fst01739107 | |
| 650 | 7 | |a Reinforcing bars. |2 fast |0 (OCoLC)fst01093515 | |
| 650 | 7 | |a Strains and stresses. |2 fast |0 (OCoLC)fst01134288 | |
| 650 | 7 | |a Torsion. |2 fast |0 (OCoLC)fst01152860 | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics, |e issuing body. | |
| 776 | 0 | 8 | |i Print version: |a Dunn, Louis (Louis Gerhardus), 1908-1979. |t Some investigations of the general instability of stiffened metal cylinders. VIII, Stiffened metal cylinders subjected to pure torsion |w (OCoLC)650826155 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 1197. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpSIGISMC3/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||