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...
Gespeichert in:
| 1. Verfasser: | |
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| Format: | Elektronisch E-Book |
| Sprache: | English |
| Veröffentlicht: |
Washington, D.C
National Advisory Committee for Aeronautics
1955
|
| Schriftenreihe: | United States / National Advisory Committee for Aeronautics: Technical note
3462 |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Zusammenfassung: | 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 |
| Beschreibung: | Includes bibliographical references. - NACA TN No. 3462 |
| Beschreibung: | 1 Online-Ressource (46 pages) |
| ISBN: | 9781680156256 |
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| 490 | 1 | |a United States / National Advisory Committee for Aeronautics: Technical note |v 3462 | |
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| 520 | 8 | |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 | |
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| id | DE-604.BV043971856 |
| illustrated | Not Illustrated |
| indexdate | 2024-07-31T01:10:29Z |
| institution | BVB |
| isbn | 9781680156256 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-029380416 |
| oclc_num | 968150711 |
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| physical | 1 Online-Ressource (46 pages) |
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| spelling | Heimerl, George J. Verfasser aut Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load George J. Heimerl and John E. Inge Washington, D.C National Advisory Committee for Aeronautics 1955 1 Online-Ressource (46 pages) txt rdacontent c rdamedia cr rdacarrier United States / National Advisory Committee for Aeronautics: Technical note 3462 Includes bibliographical references. - NACA TN No. 3462 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 Plates (Engineering) Temperature Strains and stresses Aluminum alloys Loads (Mechanics) Inge, John E. Sonstige oth National Advisory Committee for Aeronautics: Technical note United States 3462 (DE-604)BV006652327 3462 http://app.knovel.com/web/toc.v/cid:kpTPTTAAS1/viewerType:toc/root_slug:tensile-properties-7075 Aggregator Volltext |
| spellingShingle | Heimerl, George J. Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load Plates (Engineering) Temperature Strains and stresses Aluminum alloys Loads (Mechanics) |
| title | Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load |
| title_auth | Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load |
| title_exact_search | Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load |
| title_full | Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load George J. Heimerl and John E. Inge |
| title_fullStr | Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load George J. Heimerl and John E. Inge |
| title_full_unstemmed | Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load George J. Heimerl and John E. Inge |
| title_short | Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load |
| title_sort | tensile properties of 7075 t6 and 2024 t3 aluminum alloy sheet heated at uniform temperature rates under constant load |
| topic | Plates (Engineering) Temperature Strains and stresses Aluminum alloys Loads (Mechanics) |
| topic_facet | Plates (Engineering) Temperature Strains and stresses Aluminum alloys Loads (Mechanics) |
| url | http://app.knovel.com/web/toc.v/cid:kpTPTTAAS1/viewerType:toc/root_slug:tensile-properties-7075 |
| volume_link | (DE-604)BV006652327 |
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