GOE 436 AIRFOIL (goe436-il)
GOE 436 AIRFOIL - Gottingen 436 airfoil
| Details | Dat file | Parser | |
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(goe436-il) GOE 436 AIRFOIL Gottingen 436 airfoil Max thickness 11% at 30% chord. Max camber 3.8% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 436 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0223100
0.0250000 0.0326300
0.0500000 0.0462500
0.0750000 0.0578700
0.1000000 0.0665000
0.1500000 0.0792500
0.2000000 0.0875000
0.3000000 0.0925000
0.4000000 0.0895000
0.5000000 0.0830000
0.6000000 0.0720000
0.7000000 0.0585000
0.8000000 0.0410000
0.9000000 0.0220000
0.9500000 0.0112500
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0146900
0.0250000 -.0198700
0.0500000 -.0227500
0.0750000 -.0228300
0.1000000 -.0225000
0.1500000 -.0212500
0.2000000 -.0200000
0.3000000 -.0175000
0.4000000 -.0150000
0.5000000 -.0125000
0.6000000 -.0100000
0.7000000 -.0075000
0.8000000 -.0050000
0.9000000 -.0025000
0.9500000 -.0012500
1.0000000 0.0000000
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Polars for GOE 436 AIRFOIL (goe436-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe436-il | 50,000 | 9 | 23.5 at α=12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe436-il | 50,000 | 5 | 34.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe436-il | 100,000 | 9 | 47.8 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe436-il | 100,000 | 5 | 51.6 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe436-il | 200,000 | 9 | 68.2 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe436-il | 200,000 | 5 | 69.1 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe436-il | 500,000 | 9 | 96.7 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe436-il | 500,000 | 5 | 92.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe436-il | 1,000,000 | 9 | 118.3 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe436-il | 1,000,000 | 5 | 108.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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