Cargando…
Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load /
Results are presented of tests to determine the effect of heating at uniform temperature rates from 0.2 degrees to 100 degrees F. per second on the tensile properties of 7075-T6 d(75s-T6) and 2024-T3 (24s-T3) aluminum-alloy sheet under constant-load conditions. Yield and rupture stresses, obtained u...
| 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,
[1955]
|
| Colección: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 3462. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
| LEADER | 00000cam a2200000 i 4500 | ||
|---|---|---|---|
| 001 | KNOVEL_ocn919140856 | ||
| 003 | OCoLC | ||
| 005 | 20231027140348.0 | ||
| 006 | m o d | ||
| 007 | cr cnu---unuuu | ||
| 008 | 150825s1955 dcua obt f000 0 eng d | ||
| 040 | |a KNOVL |b eng |e rda |e pn |c KNOVL |d ZCU |d UAB |d DKU |d OCLCQ |d CEF |d RRP |d YOU |d S2H |d OCLCO |d OCLCQ |d UPM |d OCLCQ |d TRAAL |d GZM |d OCLCO | ||
| 019 | |a 1385367562 | ||
| 020 | |a 9781680156256 |q (electronic bk.) | ||
| 020 | |a 168015625X |q (electronic bk.) | ||
| 029 | 1 | |a GBVCP |b 856592242 | |
| 035 | |a (OCoLC)919140856 |z (OCoLC)1385367562 | ||
| 050 | 4 | |a TA480.A6 | |
| 082 | 0 | 4 | |a 620.186 |2 23 |
| 086 | 0 | |a Y 3.N 21/5:6/3462 | |
| 088 | |a NACA-TN-3462 | ||
| 049 | |a UAMI | ||
| 100 | 1 | |a Heimerl, George J. | |
| 245 | 1 | 0 | |a Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load / |c George J. Heimerl and John E. Inge. |
| 264 | 1 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1955] | |
| 300 | |a 1 online resource (46 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 / National Advisory Committee for Aeronautics ; |v 3462 | |
| 500 | |a NACA TN No. 3462. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a Results are presented of tests to determine the effect of heating at uniform temperature rates from 0.2 degrees to 100 degrees F. per second on the tensile properties of 7075-T6 d(75s-T6) and 2024-T3 (24s-T3) aluminum-alloy sheet under constant-load conditions. Yield and rupture stresses, obtained under rapid-heating conditions, are compared with results of elevated-temperature stress-strain tests for 1/2-hour exposure. Master yield-and-rupture-stress curves based on linear temperature-rate parameter are presented with which yield and rupture stresses or temperatures may be predicted for these materials for temperature rates from 0.2 to 100 degrees F per second. A description of the test equipment is included. | |
| 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 Aluminum alloys. | |
| 650 | 0 | |a Plates (Engineering) | |
| 650 | 0 | |a Loads (Mechanics) | |
| 650 | 0 | |a Temperature. | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 2 | |a Temperature | |
| 650 | 6 | |a Aluminium |x Alliages. | |
| 650 | 6 | |a Plaques (Ingénierie) | |
| 650 | 6 | |a Charges. | |
| 650 | 6 | |a Température. | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 7 | |a aluminum alloy. |2 aat | |
| 650 | 7 | |a temperature. |2 aat | |
| 650 | 7 | |a Aluminum alloys |2 fast | |
| 650 | 7 | |a Loads (Mechanics) |2 fast | |
| 650 | 7 | |a Plates (Engineering) |2 fast | |
| 650 | 7 | |a Strains and stresses |2 fast | |
| 650 | 7 | |a Temperature |2 fast | |
| 700 | 1 | |a Inge, John E. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 776 | 0 | 8 | |i Print version: |a Heimerl, George J. |t Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load |w (OCoLC)680081595 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 3462. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpTPTTAAS1/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||