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NASA-TP-1889
Wing-alone aerodynamic characteristics for high angles of attack of supersonic speeds
Year: 1981
Abstract: An experiment was conducted to determine wing-alone supersonic aerodynamic characteristics at high angles of attack. The wings tested varied in aspect ratio from 0.5 to 4.0 and in taper ratio from 0 to 1.0. The wings were tested at angles of attack ranging rom -5 deg to 60 deg and at Mach number from 1.60 to 4.60. The aerodynamic characteristics were obtained by integrating local pressures measured over the wing surfaces. Presented and discussed are results showing the effects of aspect ratio, taper ratio, Mach number, and angle of attack on force and moment coefficients and center of pressure locations. Also included are tabulations of the pressure measurements.
Subject: AERODYNAMIC
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:35:32Z | |
| date available | 2017-09-04T15:35:32Z | |
| date copyright | 01/01/1981 | |
| date issued | 1981 | |
| identifier other | OPWWAEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/37465 | |
| description abstract | An experiment was conducted to determine wing-alone supersonic aerodynamic characteristics at high angles of attack. The wings tested varied in aspect ratio from 0.5 to 4.0 and in taper ratio from 0 to 1.0. The wings were tested at angles of attack ranging rom -5 deg to 60 deg and at Mach number from 1.60 to 4.60. The aerodynamic characteristics were obtained by integrating local pressures measured over the wing surfaces. Presented and discussed are results showing the effects of aspect ratio, taper ratio, Mach number, and angle of attack on force and moment coefficients and center of pressure locations. Also included are tabulations of the pressure measurements. | |
| language | English | |
| title | NASA-TP-1889 | num |
| title | Wing-alone aerodynamic characteristics for high angles of attack of supersonic speeds | en |
| type | standard | |
| page | 191 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1981 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | ANGLE | |
| subject keywords | ASPECT | |
| subject keywords | ATTACK | |
| subject keywords | CHARACTERISTICS | |
| subject keywords | DATA | |
| subject keywords | DISTRIBUTION | |
| subject keywords | MACH | |
| subject keywords | NUMBER | |
| subject keywords | PRESSURE | |
| subject keywords | RATIO | |
| subject keywords | SPEED | |
| subject keywords | SUPERSONIC | |
| subject keywords | TABLES | |
| subject keywords | WINGS |