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NACA-TN-3676
INVESTIGATION OF LATERAL CONTROL NEAR THE STALL FLIGHT TESTS WITH HIGH-WING AND LOW-WING MONOPLANES OF VARIOUS CONFIGURATIONS
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:12:46Z | |
| date available | 2017-09-04T17:12:46Z | |
| date copyright | 01/01/1956 | |
| date issued | 1956 | |
| identifier other | YWNUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/136342 | |
| description abstract | This report, the second in a series dealing with the problem of control near the stall, presents the results of flight tests with several typical light aircraft. It has been found that, for all of the aircraft tested, adequate lateral control is available up to some critical angle of attack that is always within 2º of the angle of attack for maximum lift. The elevator deflection required to trim at this condition has been found, with power off and power on, for each of the aircraft tested, as well as the elevator deflection required to make a three-point landing. | |
| language | English | |
| title | NACA-TN-3676 | num |
| title | INVESTIGATION OF LATERAL CONTROL NEAR THE STALL FLIGHT TESTS WITH HIGH-WING AND LOW-WING MONOPLANES OF VARIOUS CONFIGURATIONS | en |
| type | standard | |
| page | 36 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1956 | |
| contenttype | fulltext |
