GOE 602 AIRFOIL (goe602-il)
GOE 602 AIRFOIL - Gottingen 602 airfoil
| Details | Dat file | Parser | |
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(goe602-il) GOE 602 AIRFOIL Gottingen 602 airfoil Max thickness 10% at 30% chord. Max camber 3.5% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 602 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0158100
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 -.0190000
0.1500000 -.0197500
0.2000000 -.0200000
0.3000000 -.0170000
0.4000000 -.0135000
0.5000000 -.0100000
0.6000000 -.0065000
0.7000000 -.0030000
0.8000000 -.0010000
0.9000000 0.0005000
0.9500000 0.0007500
1.0000000 0.0000000
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Polars for GOE 602 AIRFOIL (goe602-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe602-il | 50,000 | 9 | 37.8 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe602-il | 50,000 | 5 | 39.1 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe602-il | 100,000 | 9 | 57.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe602-il | 100,000 | 5 | 57.5 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe602-il | 200,000 | 9 | 77.5 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe602-il | 200,000 | 5 | 74 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe602-il | 500,000 | 9 | 102.2 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe602-il | 500,000 | 5 | 93.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe602-il | 1,000,000 | 9 | 119.1 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe602-il | 1,000,000 | 5 | 104.9 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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