GOE 140 (MVA H.17) AIRFOIL (goe140-il)
GOE 140 (MVA H.17) AIRFOIL - Gottingen 140 (MVA H.17) airfoil
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(goe140-il) GOE 140 (MVA H.17) AIRFOIL Gottingen 140 (MVA H.17) airfoil Max thickness 8.8% at 29.9% chord. Max camber 5.3% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 140 (MVA H.17) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123500 0.0176100
0.0247400 0.0299200
0.0495900 0.0469300
0.0744900 0.0590500
0.0994100 0.0682600
0.1492700 0.0839000
0.1992000 0.0924300
0.2991600 0.0968000
0.3992000 0.0923700
0.4992700 0.0834400
0.5993800 0.0711100
0.6995100 0.0564900
0.7996500 0.0398600
0.8998001 0.0224300
0.9498900 0.0129600
1.0000000 0.0029000
0.0000000 0.0000000
0.0125900 -.0108900
0.0251000 -.0113800
0.0500800 -.0086600
0.0750300 -.0039500
0.1000100 -.0007300
0.1499600 0.0042000
0.1999400 0.0064400
0.2999200 0.0090100
0.3999100 0.0104800
0.4999100 0.0102500
0.5999100 0.0099200
0.6999300 0.0084900
0.7999500 0.0053600
0.8999800 0.0020300
0.9500000 -.0004300
1.0000000 -.0029000
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Polars for GOE 140 (MVA H.17) AIRFOIL (goe140-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe140-il | 50,000 | 9 | 28.2 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe140-il | 50,000 | 5 | 37.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe140-il | 100,000 | 9 | 54.3 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe140-il | 100,000 | 5 | 56.3 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe140-il | 200,000 | 9 | 74.8 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe140-il | 200,000 | 5 | 74 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe140-il | 500,000 | 9 | 100.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe140-il | 500,000 | 5 | 96.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe140-il | 1,000,000 | 9 | 119.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe140-il | 1,000,000 | 5 | 112 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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