درباره ما
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
| 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 |
