GOE 10K AIRFOIL (goe10k-il)
GOE 10K AIRFOIL - Gottingen 10K airfoil
| Details | Dat file | Parser | |
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(goe10k-il) GOE 10K AIRFOIL Gottingen 10K airfoil Max thickness 3.9% at 50% chord. Max camber 1.4% at 60% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 10K AIRFOIL
15. 15.
0.0000000 0.0000000
0.0250000 0.0100900
0.0500000 0.0139800
0.1000000 0.0192700
0.1500000 0.0232600
0.2000000 0.0263400
0.3000000 0.0305100
0.4000000 0.0323800
0.5000000 0.0333500
0.6000000 0.0328200
0.7000000 0.0293900
0.8000000 0.0232600
0.9000000 0.0141300
0.9500000 0.0084100
1.0000000 0.0000000
0.0000000 0.0000000
0.0250000 -.0066100
0.0500000 -.0078100
0.1000000 -.0082300
0.1500000 -.0078500
0.2000000 -.0074600
0.3000000 -.0066900
0.4000000 -.0059200
0.5000000 -.0051500
0.6000000 -.0043800
0.7000000 -.0036100
0.8000000 -.0028400
0.9000000 -.0020700
0.9500000 -.0016900
1.0000000 0.0000000
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Polars for GOE 10K AIRFOIL (goe10k-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe10k-il | 50,000 | 9 | 20.6 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe10k-il | 50,000 | 5 | 22.7 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe10k-il | 100,000 | 9 | 27.8 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe10k-il | 100,000 | 5 | 33.1 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe10k-il | 200,000 | 9 | 47.1 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe10k-il | 200,000 | 5 | 56.4 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe10k-il | 500,000 | 9 | 88.5 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe10k-il | 500,000 | 5 | 74.8 at α=1° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe10k-il | 1,000,000 | 9 | 111.6 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe10k-il | 1,000,000 | 5 | 61 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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