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NACA-TN-2587
Influence of wing and fuselage on the vertical-tail contribution to the low-speed rolling derivatives of midwing airplane models with 45 degree sweptback surfaces
Year: 1951
Abstract: An investigation was made to determine the influence of the wing and fuselage on the vertical-tail contribution to the low-speed rolling derivatives of midwing airplane models with 45° sweptback surfaces.
The results show that the vertical-tail contribution to the rolling derivatives of midwing or near-midwing configurations can be calculated with good accuracy throughout the angle-of-attack range by using available procedures when corrections have been made for the effects of fuselage and wing sidewash at the tail due to roll.
The results show that the vertical-tail contribution to the rolling derivatives of midwing or near-midwing configurations can be calculated with good accuracy throughout the angle-of-attack range by using available procedures when corrections have been made for the effects of fuselage and wing sidewash at the tail due to roll.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:49:59Z | |
| date available | 2017-09-04T15:49:59Z | |
| date copyright | 01/01/1951 | |
| date issued | 1951 | |
| identifier other | QFPTYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/53009 | |
| description abstract | An investigation was made to determine the influence of the wing and fuselage on the vertical-tail contribution to the low-speed rolling derivatives of midwing airplane models with 45° sweptback surfaces. The results show that the vertical-tail contribution to the rolling derivatives of midwing or near-midwing configurations can be calculated with good accuracy throughout the angle-of-attack range by using available procedures when corrections have been made for the effects of fuselage and wing sidewash at the tail due to roll. | |
| language | English | |
| title | NACA-TN-2587 | num |
| title | Influence of wing and fuselage on the vertical-tail contribution to the low-speed rolling derivatives of midwing airplane models with 45 degree sweptback surfaces | en |
| type | standard | |
| page | 56 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1951 | |
| contenttype | fulltext |