Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load
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| Main Author | |
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| Corporate Author | |
| Other Authors | |
| Format | Electronic eBook |
| Language | English |
| Published |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1955]
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| Series | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 3462. |
| Subjects | |
| Online Access | Full text |
| ISBN | 9781680156256 168015625X |
| Physical Description | 1 online resource (46 pages) : illustrations |
Cover
| Abstract: | 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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| Item Description: | NACA TN No. 3462. |
| Bibliography: | Includes bibliographical references. |
| ISBN: | 9781680156256 168015625X |
| Access: | Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty |
| Physical Description: | 1 online resource (46 pages) : illustrations |