GOE 13K AIRFOIL (goe13k-il)
GOE 13K AIRFOIL - Gottingen 13K airfoil
| Details | Dat file | Parser | |
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(goe13k-il) GOE 13K AIRFOIL Gottingen 13K airfoil Max thickness 14.8% at 50% chord. Max camber 5.5% at 60% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 13K AIRFOIL
15. 15.
0.0000000 0.0000000
0.0250000 0.0383500
0.0500000 0.0535900
0.1000000 0.0738900
0.1500000 0.0889900
0.2000000 0.1008800
0.3000000 0.1168700
0.4000000 0.1241600
0.5000000 0.1280500
0.6000000 0.1260400
0.7000000 0.1130300
0.8000000 0.0893200
0.9000000 0.0542100
0.9500000 0.0321100
1.0000000 0.0000000
0.0000000 0.0000000
0.0250000 -.0255500
0.0500000 -.0301000
0.1000000 -.0319100
0.1500000 -.0304200
0.2000000 -.0289200
0.3000000 -.0259300
0.4000000 -.0229400
0.5000000 -.0199500
0.6000000 -.0169600
0.7000000 -.0139700
0.8000000 -.0109800
0.9000000 -.0079900
0.9500000 -.0065000
1.0000000 0.0000000
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Polars for GOE 13K AIRFOIL (goe13k-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe13k-il | 50,000 | 9 | 25.6 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe13k-il | 50,000 | 5 | 20.9 at α=10.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe13k-il | 100,000 | 9 | 34.8 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe13k-il | 100,000 | 5 | 30.3 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe13k-il | 200,000 | 9 | 45.8 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe13k-il | 200,000 | 5 | 42.9 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe13k-il | 500,000 | 9 | 92.9 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe13k-il | 500,000 | 5 | 85.8 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe13k-il | 1,000,000 | 9 | 129 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe13k-il | 1,000,000 | 5 | 93.9 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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