GOE 432 AIRFOIL (goe432-il)
GOE 432 AIRFOIL - Gottingen 432 airfoil
| Details | Dat file | Parser | |
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(goe432-il) GOE 432 AIRFOIL Gottingen 432 airfoil Max thickness 7.7% at 20% chord. Max camber 4.3% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 432 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0211100
0.0250000 0.0307200
0.0500000 0.0444500
0.0750000 0.0536700
0.1000000 0.0609000
0.1500000 0.0693500
0.2000000 0.0758000
0.3000000 0.0802000
0.4000000 0.0776000
0.5000000 0.0710000
0.6000000 0.0629000
0.7000000 0.0518000
0.8000000 0.0382000
0.9000000 0.0216000
0.9500000 0.0110500
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0068900
0.0250000 -.0087700
0.0500000 -.0085500
0.0750000 -.0078300
0.1000000 -.0066000
0.1500000 -.0041500
0.2000000 -.0012000
0.3000000 0.0052000
0.4000000 0.0091000
0.5000000 0.0110000
0.6000000 0.0109000
0.7000000 0.0088000
0.8000000 0.0062000
0.9000000 0.0023000
0.9500000 0.0010500
1.0000000 0.0000000
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Polars for GOE 432 AIRFOIL (goe432-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe432-il | 50,000 | 9 | 35.4 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe432-il | 50,000 | 5 | 40.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe432-il | 100,000 | 9 | 53.3 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe432-il | 100,000 | 5 | 56.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe432-il | 200,000 | 9 | 72.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe432-il | 200,000 | 5 | 72 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe432-il | 500,000 | 9 | 94.8 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe432-il | 500,000 | 5 | 88.3 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe432-il | 1,000,000 | 9 | 108 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe432-il | 1,000,000 | 5 | 107.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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