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GOE 57 AIRFOIL (goe57-il)

GOE 57 AIRFOIL - Gottingen 57 airfoil


Airfoil goe57-il
Details Dat file Parser  
(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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Lednicer format dat file
Selig format dat file

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Polars for GOE 57 AIRFOIL (goe57-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe57-il50,000941.6 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe57-il50,000543.5 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe57-il100,000963.3 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe57-il100,000559.2 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe57-il200,000982.4 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe57-il200,000570.2 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   goe57-il500,000993 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe57-il500,000586.5 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe57-il1,000,0009105.3 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe57-il1,000,0005102.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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