GOE 450 AIRFOIL (goe450-il)
GOE 450 AIRFOIL - Gottingen 450 airfoil
| Details | Dat file | Parser | |
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(goe450-il) GOE 450 AIRFOIL Gottingen 450 airfoil Max thickness 8.9% at 29.9% chord. Max camber 5.2% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 450 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122900 0.0200300
0.0247100 0.0280600
0.0495700 0.0414200
0.0744600 0.0512800
0.0993700 0.0600400
0.1492400 0.0727600
0.1991400 0.0826800
0.2990300 0.0932200
0.3990000 0.0952700
0.4990500 0.0911200
0.5991500 0.0811600
0.6993000 0.0673100
0.7994900 0.0492500
0.8997200 0.0267000
0.9498500 0.0141300
1.0000000 0.0010500
0.0000000 0.0000000
0.0126100 -.0103700
0.0251200 -.0112400
0.0501100 -.0109800
0.0751000 -.0097200
0.1000800 -.0078500
0.1500500 -.0047300
0.2000100 -.0010100
0.2999600 0.0042300
0.3999100 0.0083800
0.4998700 0.0122200
0.5998900 0.0104700
0.6999100 0.0084100
0.7999300 0.0067600
0.8999700 0.0031000
0.9499900 0.0010300
1.0000000 -.0010500
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Polars for GOE 450 AIRFOIL (goe450-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe450-il | 50,000 | 9 | 39.6 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe450-il | 50,000 | 5 | 40.1 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe450-il | 100,000 | 9 | 63.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe450-il | 100,000 | 5 | 64.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe450-il | 200,000 | 9 | 88.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe450-il | 200,000 | 5 | 85.6 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe450-il | 500,000 | 9 | 120.7 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe450-il | 500,000 | 5 | 108 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe450-il | 1,000,000 | 9 | 141.4 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe450-il | 1,000,000 | 5 | 118.9 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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