GOE 308 (MVA H.40) AIRFOIL (goe308-il)
GOE 308 (MVA H.40) AIRFOIL - Gottingen 308 (MVA H.40) airfoil
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(goe308-il) GOE 308 (MVA H.40) AIRFOIL Gottingen 308 (MVA H.40) airfoil Max thickness 8.1% at 29.9% chord. Max camber 5% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 308 (MVA H.40) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0124000 0.0175700
0.0248400 0.0270500
0.0497500 0.0427900
0.0746800 0.0547400
0.0996200 0.0638900
0.1495500 0.0761800
0.1995000 0.0843800
0.2994600 0.0908700
0.3994800 0.0879600
0.4995200 0.0811500
0.5995800 0.0706400
0.6996601 0.0573300
0.7997600 0.0408200
0.8998700 0.0228100
0.9499300 0.0123000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125600 -.0093300
0.0250600 -.0105500
0.0500600 -.0109000
0.0750600 -.0094600
0.1000300 -.0058100
0.1500000 -.0004100
0.1999700 0.0048800
0.2999400 0.0099700
0.3999400 0.0101600
0.4999600 0.0069500
0.5999800 0.0035400
0.7000000 -.0001700
0.8000300 -.0051800
0.9000300 -.0042900
0.9500100 -.0023900
1.0000000 0.0000000
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Polars for GOE 308 (MVA H.40) AIRFOIL (goe308-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe308-il | 50,000 | 9 | 32.2 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe308-il | 50,000 | 5 | 37.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe308-il | 100,000 | 9 | 54.3 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe308-il | 100,000 | 5 | 55.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe308-il | 200,000 | 9 | 74.2 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe308-il | 200,000 | 5 | 74.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe308-il | 500,000 | 9 | 103 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe308-il | 500,000 | 5 | 100.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe308-il | 1,000,000 | 9 | 126.3 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe308-il | 1,000,000 | 5 | 115.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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