GOE 137 (MVA H.15) AIRFOIL (goe137-il)
GOE 137 (MVA H.15) AIRFOIL - Gottingen 137 (MVA H.15) airfoil
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(goe137-il) GOE 137 (MVA H.15) AIRFOIL Gottingen 137 (MVA H.15) airfoil Max thickness 8.6% at 29.9% chord. Max camber 4.4% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 137 (MVA H.15) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123200 0.0175300
0.0247100 0.0276600
0.0495600 0.0420200
0.0744500 0.0522900
0.0993600 0.0610500
0.1492400 0.0719700
0.1991500 0.0801000
0.2990800 0.0870600
0.3991100 0.0856100
0.4991700 0.0785700
0.5993000 0.0668200
0.6994400 0.0528800
0.7996000 0.0376400
0.8997900 0.0199900
0.9498900 0.0105200
1.0000000 0.0014500
0.0000000 0.0000000
0.0125900 -.0089700
0.0251100 -.0105400
0.0501200 -.0110700
0.0751200 -.0112100
0.1001000 -.0099400
0.1500700 -.0063200
0.2000400 -.0033900
0.2999900 0.0011600
0.3999700 0.0028200
0.4999600 0.0038700
0.5999500 0.0038300
0.6999600 0.0033800
0.7999800 0.0019400
0.9000000 0.0003900
0.9500100 -.0007800
1.0000000 -.0014500
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Polars for GOE 137 (MVA H.15) AIRFOIL (goe137-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe137-il | 50,000 | 9 | 35.2 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe137-il | 50,000 | 5 | 39.8 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe137-il | 100,000 | 9 | 56.9 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe137-il | 100,000 | 5 | 59.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe137-il | 200,000 | 9 | 78.4 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe137-il | 200,000 | 5 | 77.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe137-il | 500,000 | 9 | 104.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe137-il | 500,000 | 5 | 97.3 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe137-il | 1,000,000 | 9 | 120.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe137-il | 1,000,000 | 5 | 109.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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