GOE 182 (MVA H.27) AIRFOIL (goe182-il)
GOE 182 (MVA H.27) AIRFOIL - Gottingen 182 (MVA H.27) airfoil
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(goe182-il) GOE 182 (MVA H.27) AIRFOIL Gottingen 182 (MVA H.27) airfoil Max thickness 9.5% at 19.9% chord. Max camber 5.3% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 182 (MVA H.27) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0121800 0.0223700
0.0245400 0.0325500
0.0493200 0.0479000
0.0741300 0.0610600
0.0989900 0.0708100
0.1487700 0.0865200
0.1986700 0.0933300
0.2986400 0.0953600
0.3987100 0.0906800
0.4988500 0.0810100
0.5990200 0.0685400
0.6992400 0.0532600
0.7994600 0.0380900
0.8997100 0.0206200
0.9498500 0.0105400
1.0000000 0.0007500
0.0000000 0.0000000
0.0126600 -.0115200
0.0252000 -.0140400
0.0502000 -.0142800
0.0751800 -.0126300
0.1001600 -.0113700
0.1500900 -.0061600
0.2000200 -.0010500
0.2998800 0.0081700
0.3997900 0.0146000
0.4997200 0.0193200
0.5997200 0.0196500
0.6997600 0.0166700
0.7998500 0.0108000
0.8999400 0.0045200
0.9499800 0.0013400
1.0000000 -.0007500
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Polars for GOE 182 (MVA H.27) AIRFOIL (goe182-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe182-il | 50,000 | 9 | 29.2 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe182-il | 50,000 | 5 | 36.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe182-il | 100,000 | 9 | 48.6 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe182-il | 100,000 | 5 | 51.5 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe182-il | 200,000 | 9 | 68.6 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe182-il | 200,000 | 5 | 69.4 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe182-il | 500,000 | 9 | 98 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe182-il | 500,000 | 5 | 97.9 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe182-il | 1,000,000 | 9 | 122.5 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe182-il | 1,000,000 | 5 | 119.8 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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