GOE 57 AIRFOIL (goe57-il)
GOE 57 AIRFOIL - Gottingen 57 airfoil
| Details | Dat file | Parser | |
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(goe57-il) GOE 57 AIRFOIL Gottingen 57 airfoil Max thickness 6.3% at 19.9% chord. Max camber 5.1% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 57 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123300 0.0151400
0.0247200 0.0253800
0.0495500 0.0399500
0.0744400 0.0505300
0.0993300 0.0601100
0.1492200 0.0696600
0.1991500 0.0759200
0.2990900 0.0815300
0.3991000 0.0810500
0.4991500 0.0764700
0.5992500 0.0675800
0.6993800 0.0558000
0.7995600 0.0398200
0.8997500 0.0220300
0.9498600 0.0125900
1.0000000 0.0008500
0.0000000 0.0000000
0.0126200 -.0107600
0.0251300 -.0117200
0.0500900 -.0080400
0.0750400 -.0037600
0.0999900 0.0005100
0.1499200 0.0073700
0.1998500 0.0131300
0.2997800 0.0193400
0.3997700 0.0213400
0.4997500 0.0221700
0.5997700 0.0203900
0.6998200 0.0161000
0.7998800 0.0112200
0.8999400 0.0050300
0.9499800 0.0020900
1.0000000 -.0008500
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Polars for GOE 57 AIRFOIL (goe57-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe57-il | 50,000 | 9 | 41.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe57-il | 50,000 | 5 | 43.5 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe57-il | 100,000 | 9 | 63.3 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe57-il | 100,000 | 5 | 59.2 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe57-il | 200,000 | 9 | 82.4 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe57-il | 200,000 | 5 | 70.2 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe57-il | 500,000 | 9 | 93 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe57-il | 500,000 | 5 | 86.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe57-il | 1,000,000 | 9 | 105.3 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe57-il | 1,000,000 | 5 | 102.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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