GOE 368 AIRFOIL (goe368-il)
GOE 368 AIRFOIL - Gottingen 368 airfoil
| Details | Dat file | Parser | |
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(goe368-il) GOE 368 AIRFOIL Gottingen 368 airfoil Max thickness 7.7% at 14.9% chord. Max camber 3.8% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 368 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122700 0.0147000
0.0245800 0.0249200
0.0493200 0.0398400
0.0741400 0.0507600
0.0990000 0.0586800
0.1488600 0.0670300
0.1988000 0.0708800
0.2987800 0.0715800
0.3988600 0.0667800
0.4989900 0.0594800
0.5991700 0.0486900
0.6993600 0.0378900
0.7995700 0.0255900
0.8997600 0.0143000
0.9498500 0.0075000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125900 -.0065300
0.0251600 -.0095700
0.0502300 -.0136500
0.0752700 -.0157200
0.1002500 -.0148000
0.1501700 -.0099500
0.2000600 -.0036000
0.2999200 0.0046000
0.3998700 0.0078000
0.4998700 0.0075000
0.5998900 0.0062000
0.6999300 0.0044000
0.7999500 0.0031000
0.8999700 0.0018000
0.9499800 0.0011500
1.0000000 0.0000000
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Polars for GOE 368 AIRFOIL (goe368-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe368-il | 50,000 | 9 | 29.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe368-il | 50,000 | 5 | 36 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe368-il | 100,000 | 9 | 49.8 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe368-il | 100,000 | 5 | 50.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe368-il | 200,000 | 9 | 64.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe368-il | 200,000 | 5 | 63.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe368-il | 500,000 | 9 | 83.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe368-il | 500,000 | 5 | 83.6 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe368-il | 1,000,000 | 9 | 98.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe368-il | 1,000,000 | 5 | 98.1 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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