درباره ما
NASA-TN-D-8242
Aerodynamic characteristics of a vane flow angularity sensor system capable of measuring flightpath accelerations for the Mach number range from 0.40 to 2.54
Year: 1976
Abstract: The aerodynamic characteristics of the angle of attack vane and the angle of sideslip vane are summarized. The test conditions ranged in free stream Mach number from 0.40 to 2.54, in angle of attack from -2 deg to 22 deg, in angle of sideslip from -2 deg to 12 deg, and in Reynolds number from 590,000 per meter to 1.8 million per meter. The results of the wind tunnel investigation are compared with results obtained with similar vane configurations. Comparisons with a NACA vane configuration are also made. In addition, wind tunnel-derived upwash for the test installation is compared with analytical predictions.
Subject: AERODYNAMIC
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:00:35Z | |
| date available | 2017-09-04T17:00:35Z | |
| date copyright | 01/01/1976 | |
| date issued | 1976 | |
| identifier other | XOYKAEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/124068 | |
| description abstract | The aerodynamic characteristics of the angle of attack vane and the angle of sideslip vane are summarized. The test conditions ranged in free stream Mach number from 0.40 to 2.54, in angle of attack from -2 deg to 22 deg, in angle of sideslip from -2 deg to 12 deg, and in Reynolds number from 590,000 per meter to 1.8 million per meter. The results of the wind tunnel investigation are compared with results obtained with similar vane configurations. Comparisons with a NACA vane configuration are also made. In addition, wind tunnel-derived upwash for the test installation is compared with analytical predictions. | |
| language | English | |
| title | NASA-TN-D-8242 | num |
| title | Aerodynamic characteristics of a vane flow angularity sensor system capable of measuring flightpath accelerations for the Mach number range from 0.40 to 2.54 | en |
| type | standard | |
| page | 46 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1976 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | ANGLE | |
| subject keywords | ATTACK | |
| subject keywords | CHARACTERISTICS | |
| subject keywords | DIRECTION | |
| subject keywords | FLIGHT | |
| subject keywords | FLOW | |
| subject keywords | INDICATORS | |
| subject keywords | MACH | |
| subject keywords | NUMBER | |
| subject keywords | PATHS | |
| subject keywords | TESTS | |
| subject keywords | TUNNEL | |
| subject keywords | VANES | |
| subject keywords | VELOCITY | |
| subject keywords | WIND |