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GOE 228 (MVA H.38) AIRFOIL (goe228-il)

GOE 228 (MVA H.38) AIRFOIL - Gottingen 228 (MVA H.38) airfoil


Airfoil goe228-il
Details Dat file Parser  
(goe228-il) GOE 228 (MVA H.38) AIRFOIL
Gottingen 228 (MVA H.38) airfoil
Max thickness 17.9% at 29.4% chord.
Max camber 7% at 49.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 228 (MVA H.38) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0112700 0.0304600
 0.0231800 0.0449400
 0.0472500 0.0679100
 0.0715200 0.0859000
 0.0959400 0.1003900
 0.1451700 0.1207300
 0.1944400 0.1373700
 0.2938100 0.1529000
 0.3938300 0.1524500
 0.4942300 0.1425200
 0.5948900 0.1260900
 0.6958200 0.1031800
 0.7970300 0.0732800
 0.8984100 0.0393900
 0.9491700 0.0204400
 1.0000000 0.0015000

 0.0000000 0.0000000
 0.0131100 -.0149700
 0.0258300 -.0204500
 0.0510800 -.0267300
 0.0762100 -.0299100
 0.1013100 -.0324000
 0.1513900 -.0343700
 0.2013700 -.0338400
 0.3010300 -.0253100
 0.4005400 -.0132800
 0.5000700 -.0017500
 0.5995800 0.0102800
 0.6992800 0.0178200
 0.7992600 0.0183700
 0.8995200 0.0119300
 0.9497600 0.0059700
 1.0000000 -.0015000
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Lednicer format dat file
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Polars for GOE 228 (MVA H.38) AIRFOIL (goe228-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe228-il50,00095.6 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe228-il50,000525.9 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   goe228-il100,000945.6 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe228-il100,000551.6 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe228-il200,000970.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe228-il200,000566.7 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe228-il500,000992.9 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe228-il500,000588.2 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe228-il1,000,0009116.2 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe228-il1,000,0005109 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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