GOE 367 AIRFOIL (goe367-il)
GOE 367 AIRFOIL - Gottingen 367 airfoil
| Details | Dat file | Parser | |
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(goe367-il) GOE 367 AIRFOIL Gottingen 367 airfoil Max thickness 16.3% at 29.7% chord. Max camber 4.6% at 39.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 367 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0118100 0.0268100
0.0240000 0.0387200
0.0485400 0.0562600
0.0732100 0.0691000
0.0978900 0.0813400
0.1474400 0.0990200
0.1970700 0.1130000
0.2967300 0.1261900
0.3967100 0.1271700
0.4969000 0.1197700
0.5972600 0.1059700
0.6977900 0.0852700
0.7984400 0.0601800
0.8991800 0.0317900
0.9495700 0.0165900
1.0000000 0.0016000
0.0000000 0.0000000
0.0130500 -.0213600
0.0257200 -.0279300
0.0508700 -.0335800
0.0759500 -.0366300
0.1009700 -.0375800
0.1509700 -.0373900
0.2009700 -.0372900
0.3009500 -.0366100
0.4009100 -.0351200
0.5008400 -.0325300
0.6007800 -.0299400
0.7006800 -.0262500
0.8005500 -.0212700
0.9003000 -.0115800
0.9501600 -.0060900
1.0000000 -.0016000
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Polars for GOE 367 AIRFOIL (goe367-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe367-il | 50,000 | 9 | 5.3 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe367-il | 50,000 | 5 | 20.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe367-il | 100,000 | 9 | 41.2 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe367-il | 100,000 | 5 | 47.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe367-il | 200,000 | 9 | 68 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe367-il | 200,000 | 5 | 64.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe367-il | 500,000 | 9 | 93.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe367-il | 500,000 | 5 | 83.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe367-il | 1,000,000 | 9 | 111.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe367-il | 1,000,000 | 5 | 98.4 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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