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NACA-TN-427
Strength tests on thin-walled duralumin cylinders in torsion
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:24:47Z | |
| date available | 2017-09-04T17:24:47Z | |
| date copyright | 01/01/1932 | |
| date issued | 1932 | |
| identifier other | CFYIYDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/147943 | |
| description abstract | This report is the first of a series presenting the results of strength tests on thin-walled cylinders and truncated cones of circular and elliptical section; it comprises the results obtained to date from torsion (pure shear) tests on 65 thin-walled duralumin cylinders of circular section with ends clamped to rigid bulkheads. The effect of variations in the length/radius and radius/thickness ratios on the type of failure is indicated, and a semi-empirical equation for the shearing stress at maximum load is given. | |
| language | English | |
| title | NACA-TN-427 | num |
| title | Strength tests on thin-walled duralumin cylinders in torsion | en |
| type | standard | |
| page | 24 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1932 | |
| contenttype | fulltext | |
| subject keywords | ALCOA | |
| subject keywords | ALLOYS | |
| subject keywords | ALUMINUM | |
| subject keywords | CIRCULAR | |
| subject keywords | CYLINDERS | |
| subject keywords | SHEET | |
| subject keywords | SKIN | |
| subject keywords | STRENGTH | |
| subject keywords | STRESSED | |
| subject keywords | TRUNCATED |
