GOE 15K AIRFOIL (goe15k-il)
GOE 15K AIRFOIL - Gottingen 15K airfoil
| Details | Dat file | Parser | |
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(goe15k-il) GOE 15K AIRFOIL Gottingen 15K airfoil Max thickness 15% at 50% chord. Max camber 3.4% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 15K AIRFOIL
15. 15.
0.0000000 0.0000000
0.0250000 0.0296400
0.0500000 0.0424700
0.1000000 0.0600500
0.1500000 0.0726200
0.2000000 0.0826000
0.3000000 0.0969500
0.4000000 0.1047000
0.5000000 0.1087500
0.6000000 0.1063000
0.7000000 0.0969500
0.8000000 0.0765000
0.9000000 0.0474500
0.9500000 0.0282200
1.0000000 0.0000000
0.0000000 0.0000000
0.0250000 -.0221600
0.0500000 -.0291200
0.1000000 -.0374500
0.1500000 -.0419800
0.2000000 -.0441000
0.3000000 -.0447500
0.4000000 -.0430000
0.5000000 -.0412500
0.6000000 -.0395000
0.7000000 -.0370500
0.8000000 -.0327000
0.9000000 -.0243500
0.9500000 -.0167800
1.0000000 0.0000000
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Polars for GOE 15K AIRFOIL (goe15k-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe15k-il | 50,000 | 9 | 23.7 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe15k-il | 50,000 | 5 | 20.8 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe15k-il | 100,000 | 9 | 32.5 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe15k-il | 100,000 | 5 | 30.7 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe15k-il | 200,000 | 9 | 49.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe15k-il | 200,000 | 5 | 49.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe15k-il | 500,000 | 9 | 92.8 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe15k-il | 500,000 | 5 | 67.7 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe15k-il | 1,000,000 | 9 | 92.4 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe15k-il | 1,000,000 | 5 | 83.1 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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