GOE 167 (V.KARMAN PROP.2) AIRFOIL (goe167-il)
GOE 167 (V.KARMAN PROP.2) AIRFOIL - Gottingen 167 (V.Karman PROP.2) airfoil
| Details | Dat file | Parser | |
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(goe167-il) GOE 167 (V.KARMAN PROP.2) AIRFOIL Gottingen 167 (V.Karman PROP.2) airfoil Max thickness 10.1% at 29.9% chord. Max camber 4.5% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 167 (V.KARMAN PROP.2) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123600 0.0182000
0.0247800 0.0283900
0.0496800 0.0412800
0.0746000 0.0521700
0.0995200 0.0620700
0.1494100 0.0766500
0.1993400 0.0853300
0.2992600 0.0958000
0.3992700 0.0944700
0.4993500 0.0838500
0.5994600 0.0704200
0.6995700 0.0553900
0.7997000 0.0391600
0.8998300 0.0223300
0.9499000 0.0130100
1.0000000 0.0045000
0.0000000 0.0000000
0.0125800 -.0110000
0.0250900 -.0120100
0.0500900 -.0113100
0.0750800 -.0103200
0.1000700 -.0087300
0.1500600 -.0073400
0.2000500 -.0063600
0.3000400 -.0050900
0.4000300 -.0038200
0.5000200 -.0030500
0.6000200 -.0027800
0.7000200 -.0025100
0.8000200 -.0023400
0.9000200 -.0025700
0.9500300 -.0039800
1.0000000 -.0045000
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Polars for GOE 167 (V.KARMAN PROP.2) AIRFOIL (goe167-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe167-il | 50,000 | 9 | 26.6 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe167-il | 50,000 | 5 | 34 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe167-il | 100,000 | 9 | 58 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe167-il | 100,000 | 5 | 58.8 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe167-il | 200,000 | 9 | 80.8 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe167-il | 200,000 | 5 | 78.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe167-il | 500,000 | 9 | 106.9 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe167-il | 500,000 | 5 | 97.9 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe167-il | 1,000,000 | 9 | 124.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe167-il | 1,000,000 | 5 | 108.6 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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