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NACA-TN-1928
Critical Combinations of Shear and Direct Axial Stress For Curved Rectangular Panels
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:23:00Z | |
| date available | 2017-09-04T15:23:00Z | |
| date copyright | 08/01/1949 | |
| date issued | 1949 | |
| identifier other | NDYHUEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/23192 | |
| description abstract | A solution is presented for the problem of the buckling of curved rectangular panels subjected to combined shear and direct axial stress. Charts giving theoretical critical combinations of shear and direct axial stress are presented for panels having five different length-width ratios. Because the actual critical compressive stress of rectangular panels having substantial curvature is known to be much lower than the theoretical value, a semiempirical method of analysis of curved panels subjected to combined shear and direct axial stress is presented for use in design. (author) | |
| language | English | |
| title | NACA-TN-1928 | num |
| title | Critical Combinations of Shear and Direct Axial Stress For Curved Rectangular Panels | en |
| type | standard | |
| page | 30 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1949 | |
| contenttype | fulltext | |
| subject keywords | PLATES - BUCKLING CURVED | |
| subject keywords | PLATES - BUCKLING RECTANGULAR | |
| subject keywords | PLATES - COMPRESSION CURVED | |
| subject keywords | PLATES - COMPRESSION RECTANGULAR | |
| subject keywords | PLATES - STRESSES | |
| subject keywords | SHEARING CURVED | |
| subject keywords | PLATES | |
| subject keywords | FLAT - SHEAR RECTANGULAR | |
| subject keywords | STRESSED SKIN - PLATES |
