GOE 228 (MVA H.38) AIRFOIL (goe228-il)
GOE 228 (MVA H.38) AIRFOIL - Gottingen 228 (MVA H.38) airfoil
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(goe228-il) GOE 228 (MVA H.38) AIRFOIL Gottingen 228 (MVA H.38) airfoil Max thickness 17.9% at 29.4% chord. Max camber 7% at 49.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 228 (MVA H.38) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0112700 0.0304600
0.0231800 0.0449400
0.0472500 0.0679100
0.0715200 0.0859000
0.0959400 0.1003900
0.1451700 0.1207300
0.1944400 0.1373700
0.2938100 0.1529000
0.3938300 0.1524500
0.4942300 0.1425200
0.5948900 0.1260900
0.6958200 0.1031800
0.7970300 0.0732800
0.8984100 0.0393900
0.9491700 0.0204400
1.0000000 0.0015000
0.0000000 0.0000000
0.0131100 -.0149700
0.0258300 -.0204500
0.0510800 -.0267300
0.0762100 -.0299100
0.1013100 -.0324000
0.1513900 -.0343700
0.2013700 -.0338400
0.3010300 -.0253100
0.4005400 -.0132800
0.5000700 -.0017500
0.5995800 0.0102800
0.6992800 0.0178200
0.7992600 0.0183700
0.8995200 0.0119300
0.9497600 0.0059700
1.0000000 -.0015000
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Polars for GOE 228 (MVA H.38) AIRFOIL (goe228-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe228-il | 50,000 | 9 | 5.6 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe228-il | 50,000 | 5 | 25.9 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe228-il | 100,000 | 9 | 45.6 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe228-il | 100,000 | 5 | 51.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe228-il | 200,000 | 9 | 70.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe228-il | 200,000 | 5 | 66.7 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe228-il | 500,000 | 9 | 92.9 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe228-il | 500,000 | 5 | 88.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe228-il | 1,000,000 | 9 | 116.2 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe228-il | 1,000,000 | 5 | 109 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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