GOE 602 MOD. AIRFOIL (goe602m-il)
GOE 602 MOD. AIRFOIL - Gottingen 602 MOD airfoil
| Details | Dat file | Parser | |
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(goe602m-il) GOE 602 MOD. AIRFOIL Gottingen 602 MOD airfoil Max thickness 9.6% at 30% chord. Max camber 3.8% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 602 MOD. AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0153100
0.0250000 0.0241200
0.0500000 0.0382500
0.0750000 0.0473800
0.1000000 0.0550000
0.1500000 0.0667500
0.2000000 0.0745000
0.3000000 0.0825000
0.4000000 0.0830000
0.5000000 0.0785000
0.6000000 0.0700000
0.7000000 0.0580000
0.8000000 0.0425000
0.9000000 0.0230000
0.9500000 0.0122500
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0098900
0.0250000 -.0128800
0.0500000 -.0162500
0.0750000 -.0181300
0.1000000 -.0187000
0.1500000 -.0192500
0.2000000 -.0190000
0.3000000 -.0135000
0.4000000 -.0081500
0.5000000 -.0025000
0.6000000 0.0025000
0.7000000 0.0040000
0.8000000 0.0050000
0.9000000 0.0035000
0.9500000 0.0017500
1.0000000 0.0000000
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Polars for GOE 602 MOD. AIRFOIL (goe602m-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe602m-il | 50,000 | 9 | 39.2 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe602m-il | 50,000 | 5 | 40.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe602m-il | 100,000 | 9 | 59.5 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe602m-il | 100,000 | 5 | 59.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe602m-il | 200,000 | 9 | 80 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe602m-il | 200,000 | 5 | 76.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe602m-il | 500,000 | 9 | 105.9 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe602m-il | 500,000 | 5 | 95.8 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe602m-il | 1,000,000 | 9 | 122.7 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe602m-il | 1,000,000 | 5 | 108.9 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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