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NASA-TM-X-3160
Experimental and theoretical low speed aerodynamic characteristics of the NACA 65 sub 1-213, alpha equals 0.50, airfoil
Year: 1975
Abstract: Low-speed wind-tunnel tests have been conducted to determine the two-dimensional aerodynamic characteristics of the NACA 65 sub 1-213, a = 0.05, airfoil. The results were compared with data from another low-speed wind tunnel and also with theoretical predictions obtained by using a viscous subsonic method. The tests were conducted over a Mach number range from 0.10 to 0.36. Reynolds numbers based on the airfoil chord varied from about 3 million to 23 million.
Subject: AERODYNAMIC
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:28:34Z | |
| date available | 2017-09-04T15:28:34Z | |
| date copyright | 01/01/1975 | |
| date issued | 1975 | |
| identifier other | NUTKAEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/29650 | |
| description abstract | Low-speed wind-tunnel tests have been conducted to determine the two-dimensional aerodynamic characteristics of the NACA 65 sub 1-213, a = 0.05, airfoil. The results were compared with data from another low-speed wind tunnel and also with theoretical predictions obtained by using a viscous subsonic method. The tests were conducted over a Mach number range from 0.10 to 0.36. Reynolds numbers based on the airfoil chord varied from about 3 million to 23 million. | |
| language | English | |
| title | NASA-TM-X-3160 | num |
| title | Experimental and theoretical low speed aerodynamic characteristics of the NACA 65 sub 1-213, alpha equals 0.50, airfoil | en |
| type | standard | |
| page | 76 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1975 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | AIRFOIL | |
| subject keywords | CHARACTERISTICS | |
| subject keywords | COEFFICIENTS | |
| subject keywords | DATA | |
| subject keywords | DIMENSIONAL | |
| subject keywords | FLOW | |
| subject keywords | GEOMETRY | |
| subject keywords | LOW | |
| subject keywords | PROCESSING | |
| subject keywords | PROFILES | |
| subject keywords | SPEED | |
| subject keywords | TESTS | |
| subject keywords | TUNNEL | |
| subject keywords | TWO | |
| subject keywords | VISCOUS | |
| subject keywords | WIND |