GOE 14K AIRFOIL (goe14k-il)
GOE 14K AIRFOIL - Gottingen 14K airfoil
| Details | Dat file | Parser | |
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(goe14k-il) GOE 14K AIRFOIL Gottingen 14K airfoil Max thickness 12% at 50% chord. Max camber 2.7% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 14K AIRFOIL
15. 15.
0.0000000 0.0000000
0.0250000 0.0237500
0.0500000 0.0340000
0.1000000 0.0480000
0.1500000 0.0581000
0.2000000 0.0661000
0.3000000 0.0776000
0.4000000 0.0838000
0.5000000 0.0870000
0.6000000 0.0850000
0.7000000 0.0776000
0.8000000 0.0612000
0.9000000 0.0380000
0.9500000 0.0226000
1.0000000 0.0000000
0.0000000 0.0000000
0.0250000 -.0176500
0.0500000 -.0233000
0.1000000 -.0300000
0.1500000 -.0336000
0.2000000 -.0353000
0.3000000 -.0358000
0.4000000 -.0344000
0.5000000 -.0330000
0.6000000 -.0316000
0.7000000 -.0296000
0.8000000 -.0262000
0.9000000 -.0195000
0.9500000 -.0134000
1.0000000 0.0000000
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Polars for GOE 14K AIRFOIL (goe14k-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe14k-il | 50,000 | 9 | 25.3 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe14k-il | 50,000 | 5 | 25.4 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe14k-il | 100,000 | 9 | 36 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe14k-il | 100,000 | 5 | 38.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe14k-il | 200,000 | 9 | 60.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe14k-il | 200,000 | 5 | 59.8 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe14k-il | 500,000 | 9 | 100.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe14k-il | 500,000 | 5 | 76.8 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe14k-il | 1,000,000 | 9 | 98.1 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe14k-il | 1,000,000 | 5 | 86.1 at α=1.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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