GOE 428 AIRFOIL (goe428-il)
GOE 428 AIRFOIL - Gottingen 428 airfoil
| Details | Dat file | Parser | |
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(goe428-il) GOE 428 AIRFOIL Gottingen 428 airfoil Max thickness 7.9% 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 428 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0171000
0.0250000 0.0262000
0.0500000 0.0414000
0.0750000 0.0516000
0.1000000 0.0608000
0.1500000 0.0742000
0.2000000 0.0836000
0.3000000 0.0904000
0.4000000 0.0892000
0.5000000 0.0830000
0.6000000 0.0718000
0.7000000 0.0576000
0.8000000 0.0404000
0.9000000 0.0222000
0.9500000 0.0116000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0059000
0.0250000 -.0068000
0.0500000 -.0066000
0.0750000 -.0054000
0.1000000 -.0032000
0.1500000 0.0022000
0.2000000 0.0056000
0.3000000 0.0114000
0.4000000 0.0152000
0.5000000 0.0170000
0.6000000 0.0168000
0.7000000 0.0136000
0.8000000 0.0094000
0.9000000 0.0052000
0.9500000 0.0026000
1.0000000 0.0000000
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Polars for GOE 428 AIRFOIL (goe428-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe428-il | 50,000 | 9 | 38.6 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe428-il | 50,000 | 5 | 40.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe428-il | 100,000 | 9 | 58.4 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe428-il | 100,000 | 5 | 60.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe428-il | 200,000 | 9 | 77.3 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe428-il | 200,000 | 5 | 78.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe428-il | 500,000 | 9 | 104.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe428-il | 500,000 | 5 | 102.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe428-il | 1,000,000 | 9 | 125 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe428-il | 1,000,000 | 5 | 121.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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