GOE 584 AIRFOIL (goe584-il)
GOE 584 AIRFOIL - Gottingen 584 airfoil
| Details | Dat file | Parser | |
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(goe584-il) GOE 584 AIRFOIL Gottingen 584 airfoil Max thickness 12.7% at 30% chord. Max camber 5% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 584 AIRFOIL
13. 13.
0.0000000 0.0000000
0.0250000 0.0371900
0.0500000 0.0548800
0.1000000 0.0767500
0.2000000 0.1010000
0.3000000 0.1107500
0.4000000 0.1110000
0.5000000 0.1027500
0.6000000 0.0880000
0.7000000 0.0687500
0.8000000 0.0465000
0.9000000 0.0237500
1.0000000 0.0000000
0.0000000 0.0000000
0.0250000 -.0198100
0.0500000 -.0236200
0.1000000 -.0247500
0.2000000 -.0210000
0.3000000 -.0162500
0.4000000 -.0120000
0.5000000 -.0092500
0.6000000 -.0065000
0.7000000 -.0042500
0.8000000 -.0025000
0.9000000 -.0012500
1.0000000 0.0000000
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Polars for GOE 584 AIRFOIL (goe584-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe584-il | 50,000 | 9 | 8.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe584-il | 50,000 | 5 | 26 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe584-il | 100,000 | 9 | 51.6 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe584-il | 100,000 | 5 | 55 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe584-il | 200,000 | 9 | 78.1 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe584-il | 200,000 | 5 | 77.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe584-il | 500,000 | 9 | 112.3 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe584-il | 500,000 | 5 | 106 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe584-il | 1,000,000 | 9 | 137.5 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe584-il | 1,000,000 | 5 | 126.1 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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