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Experimental investigation of the effects of plastic flow in a tension panel with a circular hole /
Seven uniformly dimensioned 24S-T tension panels with a central circular hole were subjected to various loads in order to study the effects of plastic flow at the point of maximum stress concentration. The results, presented in graphical form, show that, as the amount of plastic flow increases, the...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Autor Corporativo: | |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1948.
|
| Colección: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 1705. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 020 | |a 9781680156140 |q (electronic bk.) | ||
| 020 | |a 1680156144 |q (electronic bk.) | ||
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| 035 | |a (OCoLC)919094518 | ||
| 050 | 4 | |a TA480.A6 | |
| 082 | 0 | 4 | |a 620.186 |2 23 |
| 086 | 0 | |a Y 3.N 21/5:6/1705 | |
| 049 | |a UAMI | ||
| 100 | 1 | |a Griffith, George E., |e author. | |
| 245 | 1 | 0 | |a Experimental investigation of the effects of plastic flow in a tension panel with a circular hole / |c by George E. Griffith. |
| 264 | 1 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1948. | |
| 300 | |a 1 online resource (17 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 note ; |v number 1705 | |
| 500 | |a "September 1948." | ||
| 500 | |a NACA TN No. 1705. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a Seven uniformly dimensioned 24S-T tension panels with a central circular hole were subjected to various loads in order to study the effects of plastic flow at the point of maximum stress concentration. The results, presented in graphical form, show that, as the amount of plastic flow increases, the stress concentration factor is appreciably reduced and the strain concentration factor is appreciably increased. Subjecting the panels to 100 repeated loading cycles caused no change to occur in the maximum values of the stress and strain concentration factors. | |
| 583 | 1 | |a digitized |c 2011 |h University of North Texas |l committed to preserve |2 pda |5 TXdn. | |
| 588 | 0 | |a Print version record. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Aluminum alloys. | |
| 650 | 0 | |a Plates (Engineering) | |
| 650 | 0 | |a Holes. | |
| 650 | 0 | |a Loads (Mechanics) | |
| 650 | 0 | |a Alloys |x Creep. | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 6 | |a Aluminium |x Alliages. | |
| 650 | 6 | |a Plaques (Ingénierie) | |
| 650 | 6 | |a Trous. | |
| 650 | 6 | |a Charges. | |
| 650 | 6 | |a Alliages |x Fluage. | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 7 | |a aluminum alloy. |2 aat | |
| 650 | 7 | |a strain. |2 aat | |
| 650 | 7 | |a stress. |2 aat | |
| 650 | 7 | |a Aluminum alloys. |2 fast |0 (OCoLC)fst00806309 | |
| 650 | 7 | |a Holes. |2 fast |0 (OCoLC)fst00958715 | |
| 650 | 7 | |a Loads (Mechanics) |2 fast |0 (OCoLC)fst01739107 | |
| 650 | 7 | |a Plates (Engineering) |2 fast |0 (OCoLC)fst01066785 | |
| 650 | 7 | |a Strains and stresses. |2 fast |0 (OCoLC)fst01134288 | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 776 | 0 | 8 | |i Print version: |a Griffith, George E. |t Experimental investigation of the effects of plastic flow in a tension panel with a circular hole |w (OCoLC)658230735 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 1705. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpEIEPFTP3/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||