GOE 498 AIRFOIL (goe498-il)
GOE 498 AIRFOIL - Gottingen 498 airfoil
| Details | Dat file | Parser | |
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(goe498-il) GOE 498 AIRFOIL Gottingen 498 airfoil Max thickness 15.9% at 29.4% chord. Max camber 5.5% at 49.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 498 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0106900 0.0365300
0.0225900 0.0486200
0.0467400 0.0658100
0.0710900 0.0790200
0.0955300 0.0902300
0.1448000 0.1051700
0.1942300 0.1166100
0.2936900 0.1275400
0.3936700 0.1279900
0.4940600 0.1199600
0.5947800 0.1054400
0.6957700 0.0854400
0.7969300 0.0619500
0.8983700 0.0329700
0.9491300 0.0174800
1.0000000 0.0000000
0.0000000 0.0000000
0.0134100 -.0183400
0.0262700 -.0257000
0.0516600 -.0334400
0.0768400 -.0372000
0.1019800 -.0399500
0.1520300 -.0409700
0.2019600 -.0395000
0.3015400 -.0310700
0.4010000 -.0201500
0.5004600 -.0092300
0.5999700 0.0007000
0.6996700 0.0066300
0.7995800 0.0085800
0.8996800 0.0065300
0.9498000 0.0041100
1.0000000 0.0000000
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Polars for GOE 498 AIRFOIL (goe498-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe498-il | 50,000 | 9 | 7.3 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe498-il | 50,000 | 5 | 24.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe498-il | 100,000 | 9 | 49.7 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe498-il | 100,000 | 5 | 53.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe498-il | 200,000 | 9 | 75.9 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe498-il | 200,000 | 5 | 73.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe498-il | 500,000 | 9 | 105.8 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe498-il | 500,000 | 5 | 91.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe498-il | 1,000,000 | 9 | 123.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe498-il | 1,000,000 | 5 | 102.3 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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