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NACA-TM-965
Rectangular Shell Plating under Uniformly Distributed Hydrostatic Pressure
Year: 1940
Abstract: A check of the calculation methods used by Foppl and Henky for investigating the reliability of shell plating under hydrostatic pressure has proved that the formulas yield practical results within the elastic range of the material. Foppl's approximate calculation leaves one on the safe side. It further was found on the basis of the marked ductility of the shell plating under tensile stress that the strength is from 50 to 100 percent higher in the elastic range than expected by either method.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:42:11Z | |
| date available | 2017-09-04T15:42:11Z | |
| date copyright | 14946 | |
| date issued | 1940 | |
| identifier other | PIYHUEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/44530 | |
| description abstract | A check of the calculation methods used by Foppl and Henky for investigating the reliability of shell plating under hydrostatic pressure has proved that the formulas yield practical results within the elastic range of the material. Foppl's approximate calculation leaves one on the safe side. It further was found on the basis of the marked ductility of the shell plating under tensile stress that the strength is from 50 to 100 percent higher in the elastic range than expected by either method. | |
| language | English | |
| title | NACA-TM-965 | num |
| title | Rectangular Shell Plating under Uniformly Distributed Hydrostatic Pressure | en |
| type | standard | |
| page | 12 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1940 | |
| contenttype | fulltext |