GOE 704 AIRFOIL (goe704-il)
GOE 704 AIRFOIL - Gottingen 704 airfoil
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(goe704-il) GOE 704 AIRFOIL Gottingen 704 airfoil Max thickness 12.9% at 29.9% chord. Max camber 2.1% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 704 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0121600 0.0197100
0.0244800 0.0299200
0.0492300 0.0448500
0.0740600 0.0547800
0.0989100 0.0632100
0.1487200 0.0740700
0.1986100 0.0804300
0.2985200 0.0856500
0.3985400 0.0848700
0.4986400 0.0791000
0.5988300 0.0678300
0.6991000 0.0520600
0.7993900 0.0352900
0.8996800 0.0185200
0.9498200 0.0103800
1.0000000 0.0027500
0.0000000 0.0000000
0.0127700 -.0157800
0.0254000 -.0230600
0.0505500 -.0321300
0.0756500 -.0377000
0.1007000 -.0407600
0.1507500 -.0434000
0.2007700 -.0445400
0.3007600 -.0438100
0.4007300 -.0420900
0.5007000 -.0403600
0.6006700 -.0386400
0.7006300 -.0364100
0.8005300 -.0306900
0.9003299 -.0189700
0.9501899 -.0111100
1.0000000 -.0027500
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Polars for GOE 704 AIRFOIL (goe704-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe704-il | 50,000 | 9 | 26 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe704-il | 50,000 | 5 | 31.6 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe704-il | 100,000 | 9 | 44.9 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe704-il | 100,000 | 5 | 44.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe704-il | 200,000 | 9 | 57.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe704-il | 200,000 | 5 | 57.5 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe704-il | 500,000 | 9 | 78.5 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe704-il | 500,000 | 5 | 72.7 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe704-il | 1,000,000 | 9 | 90.1 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe704-il | 1,000,000 | 5 | 83 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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