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NACA-TN-4390
Effects of frequency and amplitude on the yawing derivatives of triangular, swept, and unswept wings and of a triangular-wing-fuselage combination with and without a triangular tail performing sinusoidal yawing oscillations
Year: 1958
Abstract: An investigation has been made to determine the effects of frequency and amplitude on the yawing derivatives of triangular, swept, and uswept wings. Some data were also obtained for a triangular-wing-fuselage combination with and without a triangular tail performing sinusoidal yawing oscillations. The oscillation data were compared with data obtained from steady-state yawing tests and the results of the present investigation and those of a pure sideslip investigation are compared both individually and as an algebraic sum with the combination derivatives obtained from an investigation in which the oscillation was a combination of yawing and sideslipping.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:22:31Z | |
| date available | 2017-09-04T18:22:31Z | |
| date copyright | 01/01/1958 | |
| date issued | 1958 | |
| identifier other | IBOUYDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/204936 | |
| description abstract | An investigation has been made to determine the effects of frequency and amplitude on the yawing derivatives of triangular, swept, and uswept wings. Some data were also obtained for a triangular-wing-fuselage combination with and without a triangular tail performing sinusoidal yawing oscillations. The oscillation data were compared with data obtained from steady-state yawing tests and the results of the present investigation and those of a pure sideslip investigation are compared both individually and as an algebraic sum with the combination derivatives obtained from an investigation in which the oscillation was a combination of yawing and sideslipping. | |
| language | English | |
| title | NACA-TN-4390 | num |
| title | Effects of frequency and amplitude on the yawing derivatives of triangular, swept, and unswept wings and of a triangular-wing-fuselage combination with and without a triangular tail performing sinusoidal yawing oscillations | en |
| type | standard | |
| page | 53 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1958 | |
| contenttype | fulltext |