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GOE 117 (MVA MK.4) AIRFOIL (goe117-il)

GOE 117 (MVA MK.4) AIRFOIL - Gottingen 117 (MVA MK.4) airfoil


Airfoil goe117-il
Details Dat file Parser  
(goe117-il) GOE 117 (MVA MK.4) AIRFOIL
Gottingen 117 (MVA MK.4) airfoil
Max thickness 9% at 29.8% chord.
Max camber 4.6% at 39.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 117 (MVA MK.4) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122300 0.0136400
 0.0246000 0.0201800
 0.0494000 0.0304700
 0.0742300 0.0393500
 0.0990700 0.0473400
 0.1487700 0.0626200
 0.1985500 0.0740900
 0.2983000 0.0866500
 0.3982500 0.0893100
 0.4983800 0.0826700
 0.5986000 0.0716300
 0.6988500 0.0583000
 0.7992200 0.0405600
 0.8996100 0.0214300
 0.9497700 0.0116200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0126900 -.0095500
 0.0252400 -.0121100
 0.0503000 -.0151100
 0.0753300 -.0167200
 0.1003500 -.0176300
 0.1503000 -.0152500
 0.2002400 -.0121800
 0.3000600 -.0032200
 0.3999600 0.0022400
 0.4998900 0.0056000
 0.5998800 0.0061600
 0.6999000 0.0051200
 0.7999200 0.0040800
 0.8999600 0.0022400
 0.9499700 0.0015200
 1.0000000 0.0000000
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Polars for GOE 117 (MVA MK.4) AIRFOIL (goe117-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe117-il50,000932.5 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe117-il50,000538.7 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe117-il100,000958.4 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe117-il100,000558.5 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe117-il200,000978.2 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe117-il200,000577.8 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe117-il500,0009107.8 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe117-il500,0005104.5 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe117-il1,000,0009131.1 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe117-il1,000,0005116.9 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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