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GOE 225 (MVA H.35) AIRFOIL (goe225-il)

GOE 225 (MVA H.35) AIRFOIL - Gottingen 225 (MVA H.35) airfoil


Airfoil goe225-il
Details Dat file Parser  
(goe225-il) GOE 225 (MVA H.35) AIRFOIL
Gottingen 225 (MVA H.35) airfoil
Max thickness 12.8% at 19.7% chord.
Max camber 7.6% at 49.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 225 (MVA H.35) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0118900 0.0278600
 0.0241300 0.0398300
 0.0487300 0.0577700
 0.0734000 0.0732100
 0.0981300 0.0853500
 0.1477500 0.1027400
 0.1974900 0.1147300
 0.2971900 0.1285100
 0.3971400 0.1306000
 0.4972800 0.1239900
 0.5975300 0.1126900
 0.6979200 0.0948800
 0.7985200 0.0676900
 0.8991900 0.0367900
 0.9495500 0.0204000
 1.0000000 0.0030000

 0.0000000 0.0000000
 0.0128400 -.0154200
 0.0254200 -.0193400
 0.0505000 -.0229900
 0.0755100 -.0232500
 0.1004800 -.0217000
 0.1504000 -.0183100
 0.2002900 -.0132100
 0.2999700 0.0015700
 0.3996500 0.0158500
 0.4993700 0.0288400
 0.5992000 0.0367200
 0.6992000 0.0364100
 0.7993700 0.0286100
 0.8996800 0.0148000
 0.9498600 0.0065000
 1.0000000 -.0030000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 225 (MVA H.35) AIRFOIL (goe225-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe225-il50,000910.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe225-il50,000533.4 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe225-il100,000959.3 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe225-il100,000563.5 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe225-il200,000987.5 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe225-il200,000583.3 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe225-il500,0009116.6 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe225-il500,0005107.5 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe225-il1,000,0009140.6 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe225-il1,000,0005129 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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