GOE 239 (MVA H.31) AIRFOIL (goe239-il)
GOE 239 (MVA H.31) AIRFOIL - Gottingen 239 (MVA H.31) airfoil
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(goe239-il) GOE 239 (MVA H.31) AIRFOIL Gottingen 239 (MVA H.31) airfoil Max thickness 11.2% at 19.8% chord. Max camber 6% at 39.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 239 (MVA H.31) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0120600 0.0242200
0.0243600 0.0350400
0.0490800 0.0503900
0.0738500 0.0632400
0.0986700 0.0733000
0.1483700 0.0895000
0.1982000 0.0997500
0.2980000 0.1098200
0.3980000 0.1098400
0.4981600 0.1010700
0.5983700 0.0894900
0.6986500 0.0740200
0.7990300 0.0530400
0.8994700 0.0290700
0.9496900 0.0167800
1.0000000 0.0021000
0.0000000 0.0000000
0.0127300 -.0123700
0.0252900 -.0160400
0.0503400 -.0185000
0.0753400 -.0189300
0.1003400 -.0184700
0.1503100 -.0170600
0.2002200 -.0122600
0.3000100 -.0005400
0.3998100 0.0106800
0.4997000 0.0162900
0.5996600 0.0188100
0.6996700 0.0182300
0.7997700 0.0126600
0.8998700 0.0070800
0.9499500 0.0029900
1.0000000 -.0021000
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Polars for GOE 239 (MVA H.31) AIRFOIL (goe239-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe239-il | 50,000 | 9 | 17.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe239-il | 50,000 | 5 | 38.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe239-il | 100,000 | 9 | 54.5 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe239-il | 100,000 | 5 | 60.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe239-il | 200,000 | 9 | 81.8 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe239-il | 200,000 | 5 | 83.6 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe239-il | 500,000 | 9 | 118.1 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe239-il | 500,000 | 5 | 113 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe239-il | 1,000,000 | 9 | 144.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe239-il | 1,000,000 | 5 | 125.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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