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NASA-TN-D-6896
The effects of configuration changes on the aerodynamic characteristics of a full-scale mockup of a light twin engine airplane
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:15:44Z | |
| date available | 2017-09-04T18:15:44Z | |
| date copyright | 01/01/1972 | |
| date issued | 1972 | |
| identifier other | HKYKAEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/198607 | |
| description abstract | Wind tunnel tests of a full-scale model of a light twin engine aircraft were conducted. The angle of attack was varied from minus 4 degrees to plus 20 degrees. The sideslip range was plus or minus 8 degrees. Thrust coefficients were 0, 0.20, and 0.44. Tests were made with various nacelle configurations, modes of propeller rotation, orientation of the thrust axis, and airfoil section at Reynolds numbers of 2.96 times one million amd 2.05 times one million. | |
| language | English | |
| title | NASA-TN-D-6896 | num |
| title | The effects of configuration changes on the aerodynamic characteristics of a full-scale mockup of a light twin engine airplane | en |
| type | standard | |
| page | 223 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1972 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | AIRCRAFT | |
| subject keywords | ANGLE | |
| subject keywords | ATTACK | |
| subject keywords | CHARACTERISTICS | |
| subject keywords | COEFFICIENTS | |
| subject keywords | CONFIGURATIONS | |
| subject keywords | LIGHT | |
| subject keywords | PERFORMANCE | |
| subject keywords | STABILITY | |
| subject keywords | TESTS | |
| subject keywords | TUNNEL | |
| subject keywords | WIND |
