Cargando…
Description of stress-strain curves by three parameters /
A simple formula is suggested for describing the stress-strain curve in terms of three parameters: namely, Young's modulus and two secant yield strengths. Dimensionless charts are derived from this formula for determining the stress-strain curve, the tangent modulus, and the reduced modulus of...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Autor Corporativo: | |
| Otros Autores: | |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington D.C. :
National Advisory Committee for Aeronautics,
1943.
|
| Colección: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 902. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
| LEADER | 00000cam a2200000 i 4500 | ||
|---|---|---|---|
| 001 | KNOVEL_ocn914158502 | ||
| 003 | OCoLC | ||
| 005 | 20231027140348.0 | ||
| 006 | m o d f | ||
| 007 | cr ||||||||||| | ||
| 008 | 150719s1943 dcua obt f000 0 eng d | ||
| 040 | |a SINTU |b eng |e pn |c SINTU |d SINTU |d KNOVL |d ZCU |d OCLCQ |d UAB |d DKU |d OCLCQ |d CEF |d RRP |d WYU |d YOU |d AU@ |d OCL |d TRAAL |d S2H |d OCLCO |d OCLCQ |d OCLCO |d OCLCA |d OCLCQ |d UPM |d OCLCQ | ||
| 019 | |a 951667939 |a 1183431167 | ||
| 020 | |a 9781680156034 |q (electronic bk.) | ||
| 020 | |a 1680156039 |q (electronic bk.) | ||
| 029 | 1 | |a GBVCP |b 856591556 | |
| 035 | |a (OCoLC)914158502 |z (OCoLC)951667939 |z (OCoLC)1183431167 | ||
| 050 | 4 | |a TA404.8 | |
| 082 | 0 | 4 | |a 620.11292 |2 23 |
| 086 | 0 | |a Y 3.N 21/5:6/902 | |
| 088 | |a NACA-TN-902 | ||
| 049 | |a UAMI | ||
| 100 | 1 | |a Ramberg, Walter. | |
| 245 | 1 | 0 | |a Description of stress-strain curves by three parameters / |c Walter Ramberg and William R. Osgood. |
| 260 | |a Washington D.C. : |b National Advisory Committee for Aeronautics, |c 1943. | ||
| 300 | |a 1 online resource (13, [15] 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 no. 902 | |
| 500 | |a "July 1943." | ||
| 500 | |a NACA TN no. 902. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a A simple formula is suggested for describing the stress-strain curve in terms of three parameters: namely, Young's modulus and two secant yield strengths. Dimensionless charts are derived from this formula for determining the stress-strain curve, the tangent modulus, and the reduced modulus of a material for which these three parameters are given. Comparison with the tensile and compressive data on aluminum alloy, stainless-steel, and carbon-steel sheet in NACA Technical Note No. 840 indicates that the formula is adequate for most of these materials. The formula does not describe the behavior of alclade sheet, which shows a marked change in slope at low stress. It seems probable that more than three parameters will be necessary to represent such stress-strain curves adequately. | |
| 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 Strains and stresses. | |
| 650 | 0 | |a Mathematics |v Formulae. | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 6 | |a Mathématiques |v Formules. | |
| 650 | 7 | |a formulas (algorithms) |2 aat | |
| 650 | 7 | |a Mathematics. |2 fast |0 (OCoLC)fst01012163 | |
| 650 | 7 | |a Strains and stresses. |2 fast |0 (OCoLC)fst01134288 | |
| 655 | 7 | |a Mathematical formulae. |2 fast |0 (OCoLC)fst01424053 | |
| 700 | 1 | |a Osgood, William R. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 776 | 0 | 8 | |i Print version: |a Ramberg, Walter. |t Description of stress-strain curves by three parameters. |d Washington D.C. : National Advisory Committee for Aeronautics ; 1943 |w (OCoLC)647792994 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 902. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpDSSCTPN1/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||