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NACA-TN-2392
Charts giving critical compressive stress of continuous flat sheet divided into parallelogram-shaped panels
Year: 1951
Abstract: Charts giving the compressive-buckling-stress coefficients for sheet panels of a shape occurring in swept-wing plan forms are presented. The panels are assumed to be a part of a continuous flat sheet divided by nondeflecting supports into parallelogram-shaped areas. The stability analysis was performed by the energy method and the results show that, over a wide range of panel aspect ratio, such panels are decidedly more stable than equivalent rectangular panels of the same area.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:40:40Z | |
| date available | 2017-09-04T15:40:40Z | |
| date copyright | 01/01/1951 | |
| date issued | 1951 | |
| identifier other | PEKUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/42860 | |
| description abstract | Charts giving the compressive-buckling-stress coefficients for sheet panels of a shape occurring in swept-wing plan forms are presented. The panels are assumed to be a part of a continuous flat sheet divided by nondeflecting supports into parallelogram-shaped areas. The stability analysis was performed by the energy method and the results show that, over a wide range of panel aspect ratio, such panels are decidedly more stable than equivalent rectangular panels of the same area. | |
| language | English | |
| title | NACA-TN-2392 | num |
| title | Charts giving critical compressive stress of continuous flat sheet divided into parallelogram-shaped panels | en |
| type | standard | |
| page | 32 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1951 | |
| contenttype | fulltext |