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NACA-TM-838
The Strength of Shell Bodies - Theory and Practice
Year: 1937
Abstract: The monocoque form of airplane construction has introduced a number of new problems to the stress calculator and the designer. The problems for the stress calculator fall into two groups: the determination of the stress condition (shell statics) and the determination of the failing strength (shell strength). The present report summarizes the most important theoretical and experimental results on this subject.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:16:13Z | |
| date available | 2017-09-04T15:16:13Z | |
| date copyright | 09/01/1937 | |
| date issued | 1937 | |
| identifier other | MIYHUEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/15416 | |
| description abstract | The monocoque form of airplane construction has introduced a number of new problems to the stress calculator and the designer. The problems for the stress calculator fall into two groups: the determination of the stress condition (shell statics) and the determination of the failing strength (shell strength). The present report summarizes the most important theoretical and experimental results on this subject. | |
| language | English | |
| title | NACA-TM-838 | num |
| title | The Strength of Shell Bodies - Theory and Practice | en |
| type | standard | |
| page | 63 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1937 | |
| contenttype | fulltext |