NACA-TN-1344
CRITICAL STRESS OF THIN-WALLED CYLINDERS IN TORSION
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:14:20Z | |
| date available | 2017-09-04T15:14:20Z | |
| date copyright | 06/01/1947 | |
| date issued | 1947 | |
| identifier other | MCYHUEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/13135 | |
| description abstract | A theoretical solution is given for the critical stress of thin-walled cylinders loaded in torsion. The results are presented in terms of a few simple formulas and curves which are applicable to a wide range of cylinder dimensions from very short cylinders of large radius to long cylinders of small radius. Theoretical results are found to be in somewhat better agreement with experimental results than previous theoretical work for the same range of cylinder dimensions. | |
| language | English | |
| title | NACA-TN-1344 | num |
| title | CRITICAL STRESS OF THIN-WALLED CYLINDERS IN TORSION | en |
| type | standard | |
| page | 34 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1947 | |
| contenttype | fulltext | |
| subject keywords | CYLINDERS | |
| subject keywords | CYLINDERS - STRESSES | |
| subject keywords | LOADS - CYLINDERS | |
| subject keywords | STRESSED SKIN - CYLINDERS | |
| subject keywords | THEORIES - TORSION & BENDING - DONNELL | |
| subject keywords | THIN - BUCKLING | |
| subject keywords | THIN - TORSION |

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