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NACA-TN-4146
Contribution of the wing panels to the forces and moments of supersonic wing-body combinations at combined angles
Year: 1958
Abstract: A wind-tunnel investigation was conducted at a Mach number of 1.96 and at Reynolds numbers (based on the mean aerodynamic chord of the exposed wing) of 0.36 and 1.03 minion to determine the normal forces pitching moments, and rolling moments contributed by each wing panel of a cruciform-wing and body combination over a wide range of combined angles of pitch and roll. The wings were triangular of aspect ratio 2, and the body was an ogive-cyldnder combination. The effects of forebody length and roughness and of the presence of the adjacent panels on these panel contributions were determined.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:48:16Z | |
| date available | 2017-09-04T15:48:16Z | |
| date copyright | 01/01/1958 | |
| date issued | 1958 | |
| identifier other | QAOUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/51161 | |
| description abstract | A wind-tunnel investigation was conducted at a Mach number of 1.96 and at Reynolds numbers (based on the mean aerodynamic chord of the exposed wing) of 0.36 and 1.03 minion to determine the normal forces pitching moments, and rolling moments contributed by each wing panel of a cruciform-wing and body combination over a wide range of combined angles of pitch and roll. The wings were triangular of aspect ratio 2, and the body was an ogive-cyldnder combination. The effects of forebody length and roughness and of the presence of the adjacent panels on these panel contributions were determined. | |
| language | English | |
| title | NACA-TN-4146 | num |
| title | Contribution of the wing panels to the forces and moments of supersonic wing-body combinations at combined angles | en |
| type | standard | |
| page | 64 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1958 | |
| contenttype | fulltext |