GOE 217 (MVA MK.12) AIRFOIL (goe217-il)
GOE 217 (MVA MK.12) AIRFOIL - Gottingen 217 (MVA MK.12) airfoil
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(goe217-il) GOE 217 (MVA MK.12) AIRFOIL Gottingen 217 (MVA MK.12) airfoil Max thickness 19% at 29.2% chord. Max camber 6.3% at 59.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 217 (MVA MK.12) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0100400 0.0440600
0.0215600 0.0617000
0.0453700 0.0830300
0.0694600 0.0993800
0.0937800 0.1115300
0.1428600 0.1279700
0.1922600 0.1387300
0.2916700 0.1492700
0.3919300 0.1446700
0.4927200 0.1304900
0.5938000 0.1111300
0.6950901 0.0879900
0.7965200 0.0624500
0.8980700 0.0346100
0.9488600 0.0204500
1.0000000 0.0037000
0.0000000 0.0000000
0.0136000 -.0197400
0.0263600 -.0243300
0.0517400 -.0311100
0.0770700 -.0370000
0.1023500 -.0419900
0.1526600 -.0476800
0.2026500 -.0474900
0.3022200 -.0398400
0.4013700 -.0246000
0.5002200 -.0038900
0.5990800 0.0164300
0.6983000 0.0304700
0.7984900 0.0270600
0.8992600 0.0131800
0.9497400 0.0047000
1.0000000 -.0037000
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Polars for GOE 217 (MVA MK.12) AIRFOIL (goe217-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe217-il | 50,000 | 9 | 5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe217-il | 50,000 | 5 | 21.1 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe217-il | 100,000 | 9 | 40.2 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe217-il | 100,000 | 5 | 48.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe217-il | 200,000 | 9 | 67 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe217-il | 200,000 | 5 | 70.6 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe217-il | 500,000 | 9 | 101.7 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe217-il | 500,000 | 5 | 99.6 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe217-il | 1,000,000 | 9 | 127.5 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe217-il | 1,000,000 | 5 | 119.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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