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NASA-TP-1786
Low-speed aerodynamic characteristics of a 17-percent-thick medium-speed airfoil designed for general aviation applications
Year: 1980
Abstract: Wind tunnel tests were conducted to determine the low speed two dimensional aerodynamic characteristics of a 17 percent thick medium speed airfoil (MS(1)-0317) designed for general aviation applications. The results were compared with data for the 17 percent thick low speed airfoil (LS(1)-0417) and the 13 percent thick medium speed airfoil (MS(1)-0313). Theoretical predictions of the drag rise characteristics of this airfoil are also provided. The tests were conducted in the Langley low turbulence pressure tunnel over a Mach number range from 0.10 to 0.32, a chord Reynolds number range from 2 million to 12 million, and an angle of attack range from about -8 to 20 deg.
Subject: AERODYNAMIC
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:57:52Z | |
| date available | 2017-09-04T17:57:52Z | |
| date copyright | 01/01/1980 | |
| date issued | 1980 | |
| identifier other | FPWWAEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/180936 | |
| description abstract | Wind tunnel tests were conducted to determine the low speed two dimensional aerodynamic characteristics of a 17 percent thick medium speed airfoil (MS(1)-0317) designed for general aviation applications. The results were compared with data for the 17 percent thick low speed airfoil (LS(1)-0417) and the 13 percent thick medium speed airfoil (MS(1)-0313). Theoretical predictions of the drag rise characteristics of this airfoil are also provided. The tests were conducted in the Langley low turbulence pressure tunnel over a Mach number range from 0.10 to 0.32, a chord Reynolds number range from 2 million to 12 million, and an angle of attack range from about -8 to 20 deg. | |
| language | English | |
| title | NASA-TP-1786 | num |
| title | Low-speed aerodynamic characteristics of a 17-percent-thick medium-speed airfoil designed for general aviation applications | en |
| type | standard | |
| page | 86 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1980 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | AIRCRAFT | |
| subject keywords | AIRFOIL | |
| subject keywords | AIRFOILS | |
| subject keywords | ANGLE | |
| subject keywords | ATTACK | |
| subject keywords | AVIATION | |
| subject keywords | CHARACTERISTICS | |
| subject keywords | COEFFICIENTS | |
| subject keywords | GENERAL | |
| subject keywords | LOW | |
| subject keywords | MACH | |
| subject keywords | MOMENTS | |
| subject keywords | NUMBER | |
| subject keywords | PITCHING | |
| subject keywords | PROFILES | |
| subject keywords | RATIO | |
| subject keywords | SPEED | |
| subject keywords | TESTS | |
| subject keywords | THICKNESS | |
| subject keywords | TUNNEL | |
| subject keywords | WIND |