GOE 366 AIRFOIL (goe366-il)
GOE 366 AIRFOIL - Gottingen 366 airfoil
| Details | Dat file | Parser | |
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(goe366-il) GOE 366 AIRFOIL Gottingen 366 airfoil Max thickness 13.1% at 29.8% chord. Max camber 7.2% at 39.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 366 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0120400 0.0298900
0.0243000 0.0448800
0.0489800 0.0659600
0.0737400 0.0813400
0.0985500 0.0933300
0.1482500 0.1126000
0.1980500 0.1257700
0.2978700 0.1375200
0.3978800 0.1366700
0.4980100 0.1282200
0.5982300 0.1142700
0.6985700 0.0925300
0.7989600 0.0669800
0.8994400 0.0362400
0.9496900 0.0200200
1.0000000 0.0015000
0.0000000 0.0000000
0.0127600 -.0168000
0.0252400 -.0155100
0.0501900 -.0122200
0.0751400 -.0091400
0.1001000 -.0063500
0.1500300 -.0021700
0.1999700 0.0020000
0.2999000 0.0061500
0.3998700 0.0083000
0.4998600 0.0087500
0.5998700 0.0082000
0.6998900 0.0071500
0.7999099 0.0060000
0.8999600 0.0027500
0.9499900 0.0009200
1.0000000 -.0015000
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Polars for GOE 366 AIRFOIL (goe366-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe366-il | 50,000 | 9 | 8.1 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe366-il | 50,000 | 5 | 30.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe366-il | 100,000 | 9 | 51.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe366-il | 100,000 | 5 | 55 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe366-il | 200,000 | 9 | 82.6 at α=-0.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe366-il | 200,000 | 5 | 73.3 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe366-il | 500,000 | 9 | 102.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe366-il | 500,000 | 5 | 97.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe366-il | 1,000,000 | 9 | 128.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe366-il | 1,000,000 | 5 | 121.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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