Saved in:
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Government Document eBook |
| Language: | English |
| Published: |
Washington D.C.
National Advisory Committee for Aeronautics
1943
|
| Series: | National Advisory Committee for Aeronautics technical note
no. 902 |
| Links: | https://app.knovel.com/hotlink/toc/id:kpDSSCTPN1/description-of-stress?kpromoter=marc |
| Abstract: | 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. |
| Item Description: | "July 1943." NACA TN no. 902. |
| Physical Description: | 1 Online-Ressource (13, [15] Seiten) Illustrationen |
| ISBN: | 1680156039 9781680156034 |
Staff View
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| 100 | 1 | |a Ramberg, Walter | |
| 245 | 1 | 0 | |a Description of stress-strain curves by three parameters |c Walter Ramberg and William R. Osgood |
| 264 | 1 | |a Washington D.C. |b National Advisory Committee for Aeronautics |c 1943 | |
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| 490 | 1 | |a National Advisory Committee for Aeronautics technical note |v no. 902 | |
| 500 | |a "July 1943." | ||
| 500 | |a NACA TN no. 902. | ||
| 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. | |
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| id | ZDB-10-ARA-ocn914158502 |
| illustrated | Illustrated |
| indexdate | 2025-05-15T09:13:57Z |
| institution | BVB |
| isbn | 1680156039 9781680156034 |
| language | English |
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| physical | 1 Online-Ressource (13, [15] Seiten) Illustrationen |
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| publishDate | 1943 |
| publishDateSearch | 1943 |
| publishDateSort | 1943 |
| publisher | National Advisory Committee for Aeronautics |
| record_format | marc |
| series2 | National Advisory Committee for Aeronautics technical note |
| spelling | Ramberg, Walter Description of stress-strain curves by three parameters Walter Ramberg and William R. Osgood Washington D.C. National Advisory Committee for Aeronautics 1943 1 Online-Ressource (13, [15] Seiten) Illustrationen txt c cr National Advisory Committee for Aeronautics technical note no. 902 "July 1943." NACA TN no. 902. 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. Osgood, William R. |
| spellingShingle | Ramberg, Walter Description of stress-strain curves by three parameters |
| title | Description of stress-strain curves by three parameters |
| title_auth | Description of stress-strain curves by three parameters |
| title_exact_search | Description of stress-strain curves by three parameters |
| title_full | Description of stress-strain curves by three parameters Walter Ramberg and William R. Osgood |
| title_fullStr | Description of stress-strain curves by three parameters Walter Ramberg and William R. Osgood |
| title_full_unstemmed | Description of stress-strain curves by three parameters Walter Ramberg and William R. Osgood |
| title_short | Description of stress-strain curves by three parameters |
| title_sort | description of stress strain curves by three parameters |
| work_keys_str_mv | AT rambergwalter descriptionofstressstraincurvesbythreeparameters AT osgoodwilliamr descriptionofstressstraincurvesbythreeparameters |