GOE 685 AIRFOIL (goe685-il)
GOE 685 AIRFOIL - Gottingen 685 airfoil
| Details | Dat file | Parser | |
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(goe685-il) GOE 685 AIRFOIL Gottingen 685 airfoil Max thickness 13.1% at 19.6% chord. Max camber 4.2% at 49.5% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 685 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0114000 0.0225600
0.0234300 0.0321500
0.0477300 0.0463400
0.0721800 0.0575400
0.0966600 0.0682400
0.1460000 0.0816500
0.1955100 0.0915800
0.2950500 0.1009600
0.3951300 0.0993600
0.4954800 0.0922800
0.5960700 0.0802100
0.6968600 0.0641500
0.7977700 0.0455900
0.8978900 0.0233500
0.9494400 0.0115200
1.0000000 0.0000000
0.0000000 0.0000000
0.0134500 -.0193400
0.0262600 -.0257100
0.0516400 -.0334700
0.0768700 -.0382300
0.1020100 -.0410000
0.1520400 -.0415500
0.2018900 -.0386100
0.3013100 -.0267400
0.4007500 -.0153600
0.5003900 -.0079800
0.6001500 -.0030900
0.7000100 -.0002000
0.7999400 0.0012000
0.8999700 0.0006000
0.9499700 0.0005500
1.0000000 0.0000000
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Polars for GOE 685 AIRFOIL (goe685-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe685-il | 50,000 | 9 | 25.3 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe685-il | 50,000 | 5 | 33.9 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe685-il | 100,000 | 9 | 52.5 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe685-il | 100,000 | 5 | 54.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe685-il | 200,000 | 9 | 73.4 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe685-il | 200,000 | 5 | 71.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe685-il | 500,000 | 9 | 100.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe685-il | 500,000 | 5 | 87.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe685-il | 1,000,000 | 9 | 119.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe685-il | 1,000,000 | 5 | 96.3 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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