GOE 279 (DAIMLER X) AIRFOIL (goe279-il)
GOE 279 (DAIMLER X) AIRFOIL - Gottingen 279 (DAIMLER X) airfoil
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(goe279-il) GOE 279 (DAIMLER X) AIRFOIL Gottingen 279 (DAIMLER X) airfoil Max thickness 7.4% at 30% chord. Max camber 4.7% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 279 (DAIMLER X) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0124100 0.0235500
0.0248800 0.0320000
0.0498200 0.0454900
0.0747900 0.0555900
0.0997600 0.0624800
0.1497200 0.0730800
0.1996900 0.0795700
0.2996800 0.0841500
0.3996800 0.0837400
0.4997000 0.0786200
0.5997300 0.0702100
0.6997700 0.0593900
0.7998300 0.0433800
0.8999100 0.0242600
0.9499500 0.0135600
1.0000000 0.0018500
0.0000000 0.0000000
0.0125200 -.0056500
0.0250200 -.0051000
0.0500100 -.0015100
0.0750000 0.0006900
0.0999900 0.0026800
0.1499800 0.0052800
0.1999700 0.0075700
0.2999600 0.0098500
0.3999600 0.0108400
0.4999600 0.0099200
0.5999700 0.0086100
0.6999700 0.0069900
0.7999800 0.0051200
0.8999900 0.0021500
0.9500000 0.0004600
1.0000000 -.0018500
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Polars for GOE 279 (DAIMLER X) AIRFOIL (goe279-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe279-il | 50,000 | 9 | 37.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe279-il | 50,000 | 5 | 42.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe279-il | 100,000 | 9 | 58.3 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe279-il | 100,000 | 5 | 59 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe279-il | 200,000 | 9 | 77.4 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe279-il | 200,000 | 5 | 73.5 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe279-il | 500,000 | 9 | 96.9 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe279-il | 500,000 | 5 | 93 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe279-il | 1,000,000 | 9 | 113.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe279-il | 1,000,000 | 5 | 105 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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