GOE 419 AIRFOIL (goe419-il)
GOE 419 AIRFOIL - Gottingen 419 airfoil
| Details | Dat file | Parser | |
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(goe419-il) GOE 419 AIRFOIL Gottingen 419 airfoil Max thickness 5.3% at 30% chord. Max camber 4.1% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 419 AIRFOIL
17. 17.
0.0000000 0.0050000
0.0125000 0.0135000
0.0250000 0.0190000
0.0500000 0.0295000
0.0750000 0.0380000
0.1000000 0.0445000
0.1500000 0.0550000
0.2000000 0.0625000
0.3000000 0.0700000
0.4000000 0.0705000
0.5000000 0.0670000
0.6000000 0.0590000
0.7000000 0.0490000
0.8000000 0.0350000
0.9000000 0.0200000
0.9500000 0.0120000
1.0000000 0.0000000
0.0000000 0.0050000
0.0125000 0.0005000
0.0250000 0.0000000
0.0500000 0.0010000
0.0750000 0.0030000
0.1000000 0.0050000
0.1500000 0.0090000
0.2000000 0.0125000
0.3000000 0.0170000
0.4000000 0.0175000
0.5000000 0.0155000
0.6000000 0.0130000
0.7000000 0.0095000
0.8000000 0.0060000
0.9000000 0.0030000
0.9500000 0.0015000
1.0000000 0.0000000
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Polars for GOE 419 AIRFOIL (goe419-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe419-il | 50,000 | 9 | 42.3 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe419-il | 50,000 | 5 | 40.9 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe419-il | 100,000 | 9 | 60 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe419-il | 100,000 | 5 | 59 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe419-il | 200,000 | 9 | 79.8 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe419-il | 200,000 | 5 | 78.5 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe419-il | 500,000 | 9 | 109.2 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe419-il | 500,000 | 5 | 102 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe419-il | 1,000,000 | 9 | 125 at α=1° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe419-il | 1,000,000 | 5 | 119.3 at α=1.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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