GOE 490 AIRFOIL (goe490-il)
GOE 490 AIRFOIL - Gottingen 490 airfoil
| Details | Dat file | Parser | |
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(goe490-il) GOE 490 AIRFOIL Gottingen 490 airfoil Max thickness 8.8% at 19.9% chord. Max camber 3.8% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 490 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122000 0.0162300
0.0245100 0.0264500
0.0492500 0.0404100
0.0740500 0.0513700
0.0989100 0.0588300
0.1487200 0.0692500
0.1986000 0.0756700
0.2984900 0.0815200
0.3985600 0.0798700
0.4986200 0.0747200
0.5987900 0.0655800
0.6990100 0.0534300
0.7992800 0.0387900
0.8996000 0.0216400
0.9497800 0.0120700
1.0000000 0.0000000
0.0000000 0.0000000
0.0127100 -.0112600
0.0252700 -.0145300
0.0503300 -.0175700
0.0753400 -.0186100
0.1003400 -.0181400
0.1502800 -.0152200
0.2002300 -.0123000
0.3000900 -.0049500
0.4000900 -.0031600
0.5000500 -.0027500
0.6000500 -.0029000
0.7000600 -.0030500
0.8000700 -.0037000
0.9000599 -.0033500
0.9500400 -.0019200
1.0000000 0.0000000
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Polars for GOE 490 AIRFOIL (goe490-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe490-il | 50,000 | 9 | 33.2 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe490-il | 50,000 | 5 | 38.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe490-il | 100,000 | 9 | 54.3 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe490-il | 100,000 | 5 | 54.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe490-il | 200,000 | 9 | 72.5 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe490-il | 200,000 | 5 | 70.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe490-il | 500,000 | 9 | 96.2 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe490-il | 500,000 | 5 | 89.6 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe490-il | 1,000,000 | 9 | 114.1 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe490-il | 1,000,000 | 5 | 98.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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