GOE 180 (MVA H.26) AIRFOIL (goe180-il)
GOE 180 (MVA H.26) AIRFOIL - Gottingen 180 (MVA H.26) airfoil
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(goe180-il) GOE 180 (MVA H.26) AIRFOIL Gottingen 180 (MVA H.26) airfoil Max thickness 8.7% at 30% chord. Max camber 4.4% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 180 (MVA H.26) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0199600
0.0250000 0.0293200
0.0500000 0.0436500
0.0750000 0.0544800
0.1000000 0.0620000
0.1500000 0.0734500
0.2000000 0.0801000
0.3000000 0.0874000
0.4000000 0.0852000
0.5000000 0.0778000
0.6000000 0.0681000
0.7000000 0.0561000
0.8000000 0.0412000
0.9000000 0.0237000
0.9500000 0.0146500
1.0000000 0.0025000
0.0000000 0.0000000
0.0125000 -.0098400
0.0250000 -.0112800
0.0500000 -.0123500
0.0750000 -.0115300
0.1000000 -.0102000
0.1500000 -.0073500
0.2000000 -.0044000
0.3000000 0.0007000
0.4000000 0.0037000
0.5000000 0.0050000
0.6000000 0.0058000
0.7000000 0.0054000
0.8000000 0.0044000
0.9000000 0.0029000
0.9500000 0.0013500
1.0000000 0.0000000
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Polars for GOE 180 (MVA H.26) AIRFOIL (goe180-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe180-il | 50,000 | 9 | 33.2 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe180-il | 50,000 | 5 | 40.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe180-il | 100,000 | 9 | 55.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe180-il | 100,000 | 5 | 59.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe180-il | 200,000 | 9 | 78.2 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe180-il | 200,000 | 5 | 77.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe180-il | 500,000 | 9 | 107.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe180-il | 500,000 | 5 | 99.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe180-il | 1,000,000 | 9 | 126.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe180-il | 1,000,000 | 5 | 112 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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