GOE 413 AIRFOIL (goe413-il)
GOE 413 AIRFOIL - Gottingen 413 airfoil
| Details | Dat file | Parser | |
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(goe413-il) GOE 413 AIRFOIL Gottingen 413 airfoil Max thickness 16.4% at 30% chord. Max camber 4.6% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 413 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0303400
0.0250000 0.0445800
0.0500000 0.0611600
0.0750000 0.0742500
0.1000000 0.0857300
0.1500000 0.1026900
0.2000000 0.1137600
0.3000000 0.1237900
0.4000000 0.1226200
0.5000000 0.1118500
0.6000000 0.0947800
0.7000000 0.0744100
0.8000000 0.0492400
0.9000000 0.0245700
0.9500000 0.0129300
1.0000000 0.0016000
0.0000000 0.0000000
0.0125000 -.0262600
0.0250000 -.0346200
0.0500000 -.0407400
0.0750000 -.0453500
0.1000000 -.0484700
0.1500000 -.0495100
0.2000000 -.0474400
0.3000000 -.0397100
0.4000000 -.0296800
0.5000000 -.0199500
0.6000000 -.0103200
0.7000000 -.0037900
0.8000000 0.0015400
0.9000000 0.0034700
0.9500000 0.0029400
1.0000000 0.0000000
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Polars for GOE 413 AIRFOIL (goe413-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe413-il | 50,000 | 9 | 7 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe413-il | 50,000 | 5 | 23.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe413-il | 100,000 | 9 | 47.3 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe413-il | 100,000 | 5 | 52.3 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe413-il | 200,000 | 9 | 75.3 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe413-il | 200,000 | 5 | 74.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe413-il | 500,000 | 9 | 108.3 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe413-il | 500,000 | 5 | 98.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe413-il | 1,000,000 | 9 | 130.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe413-il | 1,000,000 | 5 | 107.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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