GOE 225 (MVA H.35) AIRFOIL (goe225-il)
GOE 225 (MVA H.35) AIRFOIL - Gottingen 225 (MVA H.35) airfoil
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(goe225-il) GOE 225 (MVA H.35) AIRFOIL Gottingen 225 (MVA H.35) airfoil Max thickness 12.8% at 19.7% chord. Max camber 7.6% at 49.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 225 (MVA H.35) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0118900 0.0278600
0.0241300 0.0398300
0.0487300 0.0577700
0.0734000 0.0732100
0.0981300 0.0853500
0.1477500 0.1027400
0.1974900 0.1147300
0.2971900 0.1285100
0.3971400 0.1306000
0.4972800 0.1239900
0.5975300 0.1126900
0.6979200 0.0948800
0.7985200 0.0676900
0.8991900 0.0367900
0.9495500 0.0204000
1.0000000 0.0030000
0.0000000 0.0000000
0.0128400 -.0154200
0.0254200 -.0193400
0.0505000 -.0229900
0.0755100 -.0232500
0.1004800 -.0217000
0.1504000 -.0183100
0.2002900 -.0132100
0.2999700 0.0015700
0.3996500 0.0158500
0.4993700 0.0288400
0.5992000 0.0367200
0.6992000 0.0364100
0.7993700 0.0286100
0.8996800 0.0148000
0.9498600 0.0065000
1.0000000 -.0030000
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Polars for GOE 225 (MVA H.35) AIRFOIL (goe225-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe225-il | 50,000 | 9 | 10.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe225-il | 50,000 | 5 | 33.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe225-il | 100,000 | 9 | 59.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe225-il | 100,000 | 5 | 63.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe225-il | 200,000 | 9 | 87.5 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe225-il | 200,000 | 5 | 83.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe225-il | 500,000 | 9 | 116.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe225-il | 500,000 | 5 | 107.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe225-il | 1,000,000 | 9 | 140.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe225-il | 1,000,000 | 5 | 129 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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