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GOE 92 AIRFOIL (goe92-il)

GOE 92 AIRFOIL - Gottingen 92 airfoil


Airfoil goe92-il
Details Dat file Parser  
(goe92-il) GOE 92 AIRFOIL
Gottingen 92 airfoil
Max thickness 8.8% at 30% chord.
Max camber 5.5% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 92 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124200 0.0186500
 0.0248700 0.0308000
 0.0498000 0.0495000
 0.0747400 0.0639100
 0.0997000 0.0733100
 0.1496400 0.0872100
 0.1996100 0.0959200
 0.2995900 0.0993300
 0.3996100 0.0953400
 0.4996500 0.0861500
 0.5997000 0.0740600
 0.6997500 0.0598700
 0.7998300 0.0410800
 0.8999200 0.0206900
 0.9499500 0.0114900
 1.0000000 0.0008000

 0.0000000 0.0000000
 0.0125200 -.0048500
 0.0250100 -.0032000
 0.0500000 -.0001900
 0.0749900 0.0020100
 0.0999800 0.0037100
 0.1499700 0.0067100
 0.1999600 0.0086200
 0.2999500 0.0116300
 0.3999500 0.0117400
 0.4999500 0.0119500
 0.5999600 0.0107600
 0.6999700 0.0078700
 0.7999800 0.0049800
 0.8999900 0.0016900
 0.9500000 0.0002900
 1.0000000 -.0008000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 92 AIRFOIL (goe92-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe92-il50,000931.2 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe92-il50,000536.9 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe92-il100,000953.8 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe92-il100,000555 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe92-il200,000973.1 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe92-il200,000572.8 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe92-il500,000999.6 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe92-il500,000597.8 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe92-il1,000,0009120.6 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe92-il1,000,0005116.7 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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