GOE 241 (MVA PR.1) AIRFOIL (goe241-il)
GOE 241 (MVA PR.1) AIRFOIL - Gottingen 241 (MVA PR.1) airfoil
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(goe241-il) GOE 241 (MVA PR.1) AIRFOIL Gottingen 241 (MVA PR.1) airfoil Max thickness 18.9% at 29.5% chord. Max camber 8.4% at 49.5% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 241 (MVA PR.1) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0112700 0.0381600
0.0231500 0.0573500
0.0472800 0.0846200
0.0716700 0.1033100
0.0961700 0.1189000
0.1454300 0.1418800
0.1950100 0.1548800
0.2945700 0.1687900
0.3946200 0.1670100
0.4950000 0.1552400
0.5956100 0.1364800
0.6964400 0.1106300
0.7974700 0.0786800
0.8986200 0.0427400
0.9492800 0.0223700
1.0000000 0.0020000
0.0000000 0.0000000
0.0129900 -.0152800
0.0256300 -.0195700
0.0507200 -.0223700
0.0757800 -.0242600
0.1008300 -.0258500
0.1509000 -.0278400
0.2008900 -.0277300
0.3006300 -.0195200
0.4001600 -.0048200
0.4995800 0.0130900
0.5990500 0.0294900
0.6988500 0.0357000
0.7989300 0.0333300
0.8993599 0.0199600
0.9497100 0.0088800
1.0000000 -.0020000
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Polars for GOE 241 (MVA PR.1) AIRFOIL (goe241-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe241-il | 50,000 | 9 | 4.8 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe241-il | 50,000 | 5 | 18.8 at α=0.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe241-il | 100,000 | 9 | 42.4 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe241-il | 100,000 | 5 | 49 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe241-il | 200,000 | 9 | 68.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe241-il | 200,000 | 5 | 67.1 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe241-il | 500,000 | 9 | 94.5 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe241-il | 500,000 | 5 | 91.7 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe241-il | 1,000,000 | 9 | 120.6 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe241-il | 1,000,000 | 5 | 113.2 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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