GOE 54 AIRFOIL (goe54-il)
GOE 54 AIRFOIL - Gottingen 54 airfoil
| Details | Dat file | Parser | |
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(goe54-il) GOE 54 AIRFOIL Gottingen 54 airfoil Max thickness 6.5% at 14.9% chord. Max camber 3.5% at 19.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 54 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123000 0.0246000
0.0247200 0.0337000
0.0496200 0.0461100
0.0745500 0.0551100
0.0995000 0.0605200
0.1494500 0.0665300
0.1994500 0.0669500
0.2994900 0.0621700
0.3995700 0.0518000
0.4996600 0.0416200
0.5997300 0.0325500
0.6998000 0.0236700
0.7998600 0.0168000
0.8999299 0.0089200
0.9499500 0.0055400
1.0000000 0.0017500
0.0000000 0.0000000
0.0125800 -.0099000
0.0250700 -.0083900
0.0500200 -.0025900
0.0750100 -.0009800
0.0999900 0.0006200
0.1499900 0.0017400
0.1999800 0.0026500
0.2999800 0.0029700
0.3999700 0.0033000
0.4999700 0.0032200
0.5999800 0.0029500
0.6999800 0.0027700
0.7999800 0.0029000
0.8999900 0.0009200
0.9500100 -.0007600
1.0000000 -.0017500
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Polars for GOE 54 AIRFOIL (goe54-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe54-il | 50,000 | 9 | 19.8 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe54-il | 50,000 | 5 | 29.3 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe54-il | 100,000 | 9 | 34.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe54-il | 100,000 | 5 | 44.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe54-il | 200,000 | 9 | 58.7 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe54-il | 200,000 | 5 | 64.2 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe54-il | 500,000 | 9 | 87.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe54-il | 500,000 | 5 | 88.1 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe54-il | 1,000,000 | 9 | 106.7 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe54-il | 1,000,000 | 5 | 105.7 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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