GOE 654 AIRFOIL (goe654-il)
GOE 654 AIRFOIL - Gottingen 654 airfoil
| Details | Dat file | Parser | |
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(goe654-il) GOE 654 AIRFOIL Gottingen 654 airfoil Max thickness 14.5% at 30% chord. Max camber 5.2% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 654 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0263800
0.0250000 0.0412500
0.0500000 0.0635000
0.0750000 0.0797500
0.1000000 0.0915000
0.1500000 0.1080000
0.2000000 0.1180000
0.3000000 0.1240000
0.4000000 0.1200000
0.5000000 0.1070000
0.6000000 0.0905000
0.7000000 0.0705000
0.8000000 0.0485000
0.9000000 0.0255000
0.9500000 0.0135000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0151300
0.0250000 -.0182500
0.0500000 -.0215000
0.0750000 -.0232500
0.1000000 -.0240000
0.1500000 -.0245000
0.2000000 -.0235000
0.3000000 -.0210000
0.4000000 -.0160000
0.5000000 -.0110000
0.6000000 -.0065000
0.7000000 -.0035000
0.8000000 -.0015000
0.9000000 -.0005000
0.9500000 0.0000000
1.0000000 0.0000000
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Polars for GOE 654 AIRFOIL (goe654-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe654-il | 50,000 | 9 | 10 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe654-il | 50,000 | 5 | 28.4 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe654-il | 100,000 | 9 | 41 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe654-il | 100,000 | 5 | 50 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe654-il | 200,000 | 9 | 67.3 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe654-il | 200,000 | 5 | 67.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe654-il | 500,000 | 9 | 94.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe654-il | 500,000 | 5 | 92.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe654-il | 1,000,000 | 9 | 118.6 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe654-il | 1,000,000 | 5 | 115.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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