GOE 499 AIRFOIL (goe499-il)
GOE 499 AIRFOIL - Gottingen 499 airfoil
| Details | Dat file | Parser | |
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(goe499-il) GOE 499 AIRFOIL Gottingen 499 airfoil Max thickness 6.8% at 30% chord. Max camber 5.9% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 499 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0121600
0.0250000 0.0193100
0.0500000 0.0311200
0.0750000 0.0404400
0.1000000 0.0477500
0.1500000 0.0613700
0.2000000 0.0710000
0.3000000 0.0837500
0.4000000 0.0870000
0.5000000 0.0852500
0.6000000 0.0795000
0.7000000 0.0677500
0.8000000 0.0495000
0.9000000 0.0267500
0.9500000 0.0138800
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0103400
0.0250000 -.0116900
0.0500000 -.0118800
0.0750000 -.0110600
0.1000000 -.0087500
0.1500000 -.0031300
0.2000000 0.0035000
0.3000000 0.0157500
0.4000000 0.0245000
0.5000000 0.0317500
0.6000000 0.0355000
0.7000000 0.0342500
0.8000000 0.0275000
0.9000000 0.0157500
0.9500000 0.0083700
1.0000000 0.0000000
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Polars for GOE 499 AIRFOIL (goe499-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe499-il | 50,000 | 9 | 38.8 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe499-il | 50,000 | 5 | 44.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe499-il | 100,000 | 9 | 71.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe499-il | 100,000 | 5 | 69.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe499-il | 200,000 | 9 | 102.2 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe499-il | 200,000 | 5 | 99.1 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe499-il | 500,000 | 9 | 149.4 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe499-il | 500,000 | 5 | 118.3 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe499-il | 1,000,000 | 9 | 157.8 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe499-il | 1,000,000 | 5 | 111.9 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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