درباره ما
NASA-CR-1316
A theoretical analysis of the free vibration of discretely stiffened cylindrical shells with arbitrary end conditions
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:30:41Z | |
| date available | 2017-09-04T15:30:41Z | |
| date copyright | 01/01/1969 | |
| date issued | 1969 | |
| identifier other | OBIOEEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/32111 | |
| description abstract | Theoretical analysis of free vibration of discretely stiffened cylindrical shells with arbitrary end conditions | |
| language | English | |
| title | NASA-CR-1316 | num |
| title | A theoretical analysis of the free vibration of discretely stiffened cylindrical shells with arbitrary end conditions | en |
| type | standard | |
| page | 86 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1969 | |
| contenttype | fulltext | |
| subject keywords | COMPUTER PROGRAMS | |
| subject keywords | CYLINDRICAL SHELLS | |
| subject keywords | DIGITAL COMPUTERS | |
| subject keywords | FLEXIBILITY | |
| subject keywords | FREE VIBRATION | |
| subject keywords | RAYLEIGH-RITZ METHOD | |
| subject keywords | STIFFENING | |
| subject keywords | STIFFNESS | |
| subject keywords | VIBRATION EFFECTS |
