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NACA-TM-774
Tension fields in originally curved, thin sheets during shearing stresses
Year: 1935
Abstract: The analysis of the stresses in the sheet and stiffeners is predicated upon the direction of the wrinkles, particularly the tensile stresses (principal stresses). This analysis and the calculation of stresses after buckling form the subject of the present article. It includes: 1) metal cylinders with closely spaced longitudinal stiffeners; 2) metal cylinders with closely spaced transverse rings.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:35:30Z | |
| date available | 2017-09-04T18:35:30Z | |
| date copyright | 08/01/1935 | |
| date issued | 1935 | |
| identifier other | JIYHUEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=autho4703177D081D20686159DD6EFDEC014A/handle/yse/217535 | |
| description abstract | The analysis of the stresses in the sheet and stiffeners is predicated upon the direction of the wrinkles, particularly the tensile stresses (principal stresses). This analysis and the calculation of stresses after buckling form the subject of the present article. It includes: 1) metal cylinders with closely spaced longitudinal stiffeners; 2) metal cylinders with closely spaced transverse rings. | |
| language | English | |
| title | NACA-TM-774 | num |
| title | Tension fields in originally curved, thin sheets during shearing stresses | en |
| type | standard | |
| page | 15 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1935 | |
| contenttype | fulltext |