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GOE 222 (MVA H.33) AIRFOIL (goe222-il)

GOE 222 (MVA H.33) AIRFOIL - Gottingen 222 (MVA H.33) airfoil


Airfoil goe222-il
Details Dat file Parser  
(goe222-il) GOE 222 (MVA H.33) AIRFOIL
Gottingen 222 (MVA H.33) airfoil
Max thickness 18.5% at 29.2% chord.
Max camber 7.2% at 49.2% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 222 (MVA H.33) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0109700 0.0285900
 0.0226900 0.0432100
 0.0465300 0.0649900
 0.0705200 0.0837700
 0.0947600 0.0980700
 0.1436300 0.1191800
 0.1928800 0.1331200
 0.2919400 0.1506200
 0.3917900 0.1534600
 0.4920900 0.1478300
 0.5928200 0.1342200
 0.6941100 0.1101300
 0.7956401 0.0815700
 0.8975900 0.0450200
 0.9487400 0.0235600
 1.0000000 0.0015000

 0.0000000 0.0000000
 0.0134000 -.0167800
 0.0262100 -.0226000
 0.0515900 -.0297400
 0.0769100 -.0355900
 0.1020900 -.0390400
 0.1522900 -.0428500
 0.2023100 -.0431800
 0.3018100 -.0338500
 0.4009700 -.0180500
 0.5001700 -.0032400
 0.5995200 0.0090700
 0.6992000 0.0149100
 0.7991900 0.0150600
 0.8994300 0.0106200
 0.9496900 0.0058100
 1.0000000 -.0015000
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Lednicer format dat file
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Polars for GOE 222 (MVA H.33) AIRFOIL (goe222-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe222-il50,00095.2 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe222-il50,000514.4 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe222-il100,000942.5 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe222-il100,000547.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe222-il200,000974.9 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe222-il200,000567.2 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe222-il500,000999.2 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   goe222-il500,000584.8 at α=0.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe222-il1,000,0009115.2 at α=0.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe222-il1,000,0005102 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
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