GOE 572 AIRFOIL (goe572-il)
GOE 572 AIRFOIL - Gottingen 572 airfoil
| Details | Dat file | Parser | |
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(goe572-il) GOE 572 AIRFOIL Gottingen 572 airfoil Max thickness 18.6% at 29.9% chord. Max camber 8.3% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 572 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122700 0.0310900
0.0246300 0.0486800
0.0494300 0.0763700
0.0742600 0.0980600
0.0991300 0.1162400
0.1488900 0.1486200
0.1987900 0.1659900
0.2986800 0.1762400
0.3987400 0.1684900
0.4988800 0.1497400
0.5990600 0.1254900
0.6992600 0.0982400
0.7994800 0.0690000
0.8997600 0.0379800
0.9498400 0.0216200
1.0000000 0.0000000
0.0000000 0.0000000
0.0125700 -.0094100
0.0250900 -.0123100
0.0501100 -.0141200
0.0751100 -.0144400
0.1001100 -.0142500
0.1501000 -.0133700
0.2000900 -.0120000
0.3000700 -.0097500
0.4000600 -.0075000
0.5000500 -.0062500
0.6000500 -.0065000
0.7000600 -.0077500
0.8000700 -.0090000
0.9000599 -.0082500
0.9500600 -.0078700
1.0000000 0.0000000
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Polars for GOE 572 AIRFOIL (goe572-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe572-il | 50,000 | 9 | 3.1 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe572-il | 50,000 | 5 | 14.6 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe572-il | 100,000 | 9 | 29.9 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe572-il | 100,000 | 5 | 38.4 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe572-il | 200,000 | 9 | 55.7 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe572-il | 200,000 | 5 | 54.8 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe572-il | 500,000 | 9 | 79.9 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe572-il | 500,000 | 5 | 77.5 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe572-il | 1,000,000 | 9 | 103.8 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe572-il | 1,000,000 | 5 | 98.6 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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