GOE 269 AIRFOIL (goe269-il)
GOE 269 AIRFOIL - Gottingen 269 airfoil
| Details | Dat file | Parser | |
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(goe269-il) GOE 269 AIRFOIL Gottingen 269 airfoil Max thickness 6.6% at 29.9% chord. Max camber 5% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 269 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122700 0.0192500
0.0246600 0.0287900
0.0495100 0.0420000
0.0744100 0.0515000
0.0993100 0.0585000
0.1491800 0.0691000
0.1990900 0.0764700
0.2990200 0.0824600
0.3990400 0.0809500
0.4991000 0.0752400
0.5992300 0.0643300
0.6993901 0.0512200
0.7995700 0.0365100
0.8997700 0.0197100
0.9498600 0.0118000
1.0000000 0.0029000
0.0000000 0.0000000
0.0126700 -.0116000
0.0251700 -.0135000
0.0501300 -.0113000
0.0750700 -.0060100
0.1000200 -.0017000
0.1499300 0.0057500
0.1998600 0.0113800
0.2998000 0.0165700
0.3997700 0.0195600
0.4997600 0.0203500
0.5997800 0.0182400
0.6998300 0.0143300
0.7999000 0.0085200
0.8999700 0.0022100
0.9500000 -.0002900
1.0000000 -.0029000
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Polars for GOE 269 AIRFOIL (goe269-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe269-il | 50,000 | 9 | 36.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe269-il | 50,000 | 5 | 43.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe269-il | 100,000 | 9 | 59.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe269-il | 100,000 | 5 | 61.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe269-il | 200,000 | 9 | 80.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe269-il | 200,000 | 5 | 79.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe269-il | 500,000 | 9 | 107.7 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe269-il | 500,000 | 5 | 102.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe269-il | 1,000,000 | 9 | 127.9 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe269-il | 1,000,000 | 5 | 115.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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