درباره ما
NACA-TN-1482
A METHOD FOR CALCULATING THE COMPRESSIVE STRENGTH OF Z-STIFFENED PANELS THAT DEVELOP LOCAL INSTABILITY
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:43:37Z | |
| date available | 2017-09-04T17:43:37Z | |
| date copyright | 17481 | |
| date issued | 1947 | |
| identifier other | EDYHUEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/166667 | |
| description abstract | A method, based on the elastic theory for plate buckling and test results for 24S-T aluminum-alloy Z-stiffened panels, is shown for calculating the compressive strength of Z-stiffened panels that develop local instability. This method can be used to calculate the critical compressive stress above, as well as within, the elastic range. For stresses above three-fourths the compressive yield stress the method can be used for the approximate determination of the average compressive stress at maximum load. | |
| language | English | |
| title | NACA-TN-1482 | num |
| title | A METHOD FOR CALCULATING THE COMPRESSIVE STRENGTH OF Z-STIFFENED PANELS THAT DEVELOP LOCAL INSTABILITY | en |
| type | standard | |
| page | 16 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1947 | |
| contenttype | fulltext | |
| subject keywords | ALUMINUM ALLOYS | |
| subject keywords | ALUMINUM-ALLOY - Z-SHAPED | |
| subject keywords | COMPRESSIVE | |
| subject keywords | FLAT - STRENGTH | |
| subject keywords | PLATES | |
| subject keywords | SHEET - ALCOA 24ST - STRENGTH | |
| subject keywords | STIFFENERS | |
| subject keywords | STRESSED SKIN-STIFFENER COMBINATIONS - STRENGTH |
