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NACA-TM-856
The lift distribution of wings with end plates
Year: 1938
Abstract: The object of the present report is to ascertain the relationship of the circulation distribution over the wing and of the lift to the height and position of the end plate. The side forces and moments on the end plates were also determined. It is found that moving an end plate of certain length up from the symmetrical position, is followed by a slight increase of the total lift.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:56:03Z | |
| date available | 2017-09-04T16:56:03Z | |
| date copyright | 01/01/1938 | |
| date issued | 1938 | |
| identifier other | XCYIYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/119515 | |
| description abstract | The object of the present report is to ascertain the relationship of the circulation distribution over the wing and of the lift to the height and position of the end plate. The side forces and moments on the end plates were also determined. It is found that moving an end plate of certain length up from the symmetrical position, is followed by a slight increase of the total lift. | |
| language | English | |
| title | NACA-TM-856 | num |
| title | The lift distribution of wings with end plates | en |
| type | standard | |
| page | 21 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1938 | |
| contenttype | fulltext |