GOE 5K AIRFOIL (goe05k-il)
GOE 5K AIRFOIL - Gottingen 5K airfoil
| Details | Dat file | Parser | |
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(goe05k-il) GOE 5K AIRFOIL Gottingen 5K airfoil Max thickness 3.7% at 50% chord. Max camber 1.5% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 5K AIRFOIL
16. 16.
0.0000000 0.0000000
0.0250000 0.0078100
0.0500000 0.0116100
0.0750000 0.0146200
0.1000000 0.0173300
0.1500000 0.0216400
0.2000000 0.0249600
0.3000000 0.0299900
0.4000000 0.0329200
0.5000000 0.0338500
0.6000000 0.0329800
0.7000000 0.0294100
0.8000000 0.0231400
0.9000000 0.0138700
0.9500000 0.0080800
1.0000000 0.0000000
0.0000000 0.0000000
0.0250000 -.0034900
0.0500000 -.0038900
0.0750000 -.0041800
0.1000000 -.0042700
0.1500000 -.0045600
0.2000000 -.0044400
0.3000000 -.0040100
0.4000000 -.0035800
0.5000000 -.0031500
0.6000000 -.0027200
0.7000000 -.0022900
0.8000000 -.0018600
0.9000000 -.0014300
0.9500000 -.0012200
1.0000000 0.0000000
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Polars for GOE 5K AIRFOIL (goe05k-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe05k-il | 50,000 | 9 | 20.5 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe05k-il | 50,000 | 5 | 21.2 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe05k-il | 100,000 | 9 | 25.6 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe05k-il | 100,000 | 5 | 27.6 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe05k-il | 200,000 | 9 | 33.4 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe05k-il | 200,000 | 5 | 39.8 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe05k-il | 500,000 | 9 | 71.3 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe05k-il | 500,000 | 5 | 82.4 at α=1.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe05k-il | 1,000,000 | 9 | 95.1 at α=0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe05k-il | 1,000,000 | 5 | 95.1 at α=0.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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