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NACA-TR-715
Lateral control required for satisfactory flying qualities based on flight tests of numerous airplanes
Year: 1941
Abstract: Report presents the results of an analysis made of the aileron control characteristics of numerous airplanes tested in flight by the National Advisory Committee for Aeronautics. By the use of previously developed theory, the observed values of pb/2v for the various wing-aileron arrangements were examined to determine the effective section characteristics of the various aileron types.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:15:23Z | |
| date available | 2017-09-04T16:15:23Z | |
| date copyright | 01/01/1941 | |
| date issued | 1941 | |
| identifier other | SWWUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/78641 | |
| description abstract | Report presents the results of an analysis made of the aileron control characteristics of numerous airplanes tested in flight by the National Advisory Committee for Aeronautics. By the use of previously developed theory, the observed values of pb/2v for the various wing-aileron arrangements were examined to determine the effective section characteristics of the various aileron types. | |
| language | English | |
| title | NACA-TR-715 | num |
| title | Lateral control required for satisfactory flying qualities based on flight tests of numerous airplanes | en |
| type | standard | |
| page | 7 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1941 | |
| contenttype | fulltext |