GOE 735 AIRFOIL (goe735-il)
GOE 735 AIRFOIL - Gottingen 735 airfoil
| Details | Dat file | Parser | |
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(goe735-il) GOE 735 AIRFOIL Gottingen 735 airfoil Max thickness 20.1% at 30% chord. Max camber 4.4% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 735 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0357200
0.0250000 0.0524400
0.0500000 0.0763700
0.0750000 0.0938100
0.1000000 0.1077500
0.1500000 0.1271200
0.2000000 0.1387000
0.3000000 0.1442500
0.4000000 0.1345000
0.5000000 0.1162500
0.6000000 0.0930000
0.7000000 0.0657500
0.8000000 0.0388000
0.9000000 0.0157500
0.9500000 0.0064200
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0212800
0.0250000 -.0305600
0.0500000 -.0419300
0.0750000 -.0481900
0.1000000 -.0517500
0.1500000 -.0553700
0.2000000 -.0570000
0.3000000 -.0567500
0.4000000 -.0540000
0.5000000 -.0502500
0.6000000 -.0445000
0.7000000 -.0375500
0.8000000 -.0282000
0.9000000 -.0162500
0.9500000 -.0088700
1.0000000 0.0000000
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Polars for GOE 735 AIRFOIL (goe735-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe735-il | 50,000 | 9 | 2.9 at α=13° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe735-il | 50,000 | 5 | 16.4 at α=0.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe735-il | 100,000 | 9 | 23.4 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe735-il | 100,000 | 5 | 35.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe735-il | 200,000 | 9 | 49.6 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe735-il | 200,000 | 5 | 55.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe735-il | 500,000 | 9 | 82.2 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe735-il | 500,000 | 5 | 78.9 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe735-il | 1,000,000 | 9 | 105 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe735-il | 1,000,000 | 5 | 97.3 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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