GOE 382 AIRFOIL (goe382-il)
GOE 382 AIRFOIL - Gottingen 382 airfoil
| Details | Dat file | Parser | |
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(goe382-il) GOE 382 AIRFOIL Gottingen 382 airfoil Max thickness 20% at 29% chord. Max camber 6% at 39% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 382 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0104800 0.0309900
0.0218800 0.0477300
0.0451100 0.0747500
0.0689000 0.0933100
0.0929600 0.1076800
0.1415000 0.1299600
0.1904800 0.1454700
0.2895400 0.1598500
0.3896300 0.1585000
0.4904200 0.1464000
0.5918200 0.1249300
0.6935199 0.0990900
0.7954800 0.0690600
0.8977200 0.0348600
0.9488900 0.0169100
1.0000000 0.0010500
0.0000000 0.0000000
0.0138800 -.0210900
0.0280400 -.0263600
0.0521100 -.0321900
0.0772800 -.0348400
0.1025200 -.0384900
0.1526600 -.0405100
0.2027200 -.0415300
0.3026400 -.0402900
0.4024500 -.0374600
0.5022000 -.0336300
0.6017800 -.0271100
0.7013500 -.0206000
0.8009200 -.0140800
0.9005001 -.0075600
0.9502800 -.0043000
1.0000000 -.0010500
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Polars for GOE 382 AIRFOIL (goe382-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe382-il | 50,000 | 9 | 3.5 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe382-il | 50,000 | 5 | 14 at α=0° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe382-il | 100,000 | 9 | 25.5 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe382-il | 100,000 | 5 | 39.7 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe382-il | 200,000 | 9 | 60.9 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe382-il | 200,000 | 5 | 59.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe382-il | 500,000 | 9 | 87 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe382-il | 500,000 | 5 | 81.9 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe382-il | 1,000,000 | 9 | 109.6 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe382-il | 1,000,000 | 5 | 103.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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