GOE 143 (MVA H.20) AIRFOIL (goe143-il)
GOE 143 (MVA H.20) AIRFOIL - Gottingen 143 (MVA H.20) airfoil
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(goe143-il) GOE 143 (MVA H.20) AIRFOIL Gottingen 143 (MVA H.20) airfoil Max thickness 7.4% at 19.9% chord. Max camber 3.8% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 143 (MVA H.20) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122700 0.0174600
0.0246600 0.0262200
0.0494700 0.0410400
0.0743500 0.0499600
0.0992700 0.0560900
0.1491500 0.0653300
0.1990800 0.0711800
0.2990300 0.0747700
0.3990700 0.0717700
0.4991500 0.0655600
0.5992600 0.0567600
0.6994100 0.0453600
0.8000000 0.0316000
0.8997700 0.0174500
0.9498800 0.0094000
1.0000000 0.0014500
0.0000000 0.0000000
0.0126500 -.0113400
0.0251800 -.0140700
0.0501700 -.0131500
0.0751400 -.0111300
0.1001100 -.0085000
0.1500700 -.0055600
0.2000400 -.0032100
0.2999900 0.0009800
0.3999500 0.0034800
0.4999400 0.0047700
0.5999300 0.0054700
0.6999400 0.0044600
0.7999600 0.0034600
0.8999800 0.0017500
0.9500000 -.0001000
1.0000000 -.0014500
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Polars for GOE 143 (MVA H.20) AIRFOIL (goe143-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe143-il | 50,000 | 9 | 35.3 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe143-il | 50,000 | 5 | 39.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe143-il | 100,000 | 9 | 53.7 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe143-il | 100,000 | 5 | 55.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe143-il | 200,000 | 9 | 72.3 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe143-il | 200,000 | 5 | 70.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe143-il | 500,000 | 9 | 94.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe143-il | 500,000 | 5 | 86.8 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe143-il | 1,000,000 | 9 | 109.9 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe143-il | 1,000,000 | 5 | 98.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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