درباره ما
NACA-ARR-L4H29
CHARTS FOR CALCULATING THE CRITICAL COMPRESSIVE STRESS FOR LOCAL INSTABILITY OF IDEALIZED WEB - AND T-STIFFENED PANELS
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:18:58Z | |
| date available | 2017-09-04T16:18:58Z | |
| date copyright | 08/01/1944 | |
| date issued | 1944 | |
| identifier other | TGYHUEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/82422 | |
| description abstract | Charts are presented for the calculation of the critical compressive stress The stress at which local instability occurs for idealised web- and T-stiffened panels, and examples of the use of the charts are given. | |
| language | English | |
| title | NACA-ARR-L4H29 | num |
| title | CHARTS FOR CALCULATING THE CRITICAL COMPRESSIVE STRESS FOR LOCAL INSTABILITY OF IDEALIZED WEB - AND T-STIFFENED PANELS | en |
| type | standard | |
| page | 16 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1944 | |
| contenttype | fulltext | |
| subject keywords | ALUMINUM ALLOYS - ALCOA 24ST | |
| subject keywords | ALUMINUM ALLOYS - ALCOA XB75ST | |
| subject keywords | CHARTS - STRESSES | |
| subject keywords | STRESSED SKIN - STIFFENER COMBINATIONS | |
| subject keywords | STRESSED SKIN - STIFFENER COMBINATIONS - BUCKLING |
