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GOE 116 (MVA MK.3) AIRFOIL (goe116-il)

GOE 116 (MVA MK.3) AIRFOIL - Gottingen 116 (MVA MK.3) airfoil


Airfoil goe116-il
Details Dat file Parser  
(goe116-il) GOE 116 (MVA MK.3) AIRFOIL
Gottingen 116 (MVA MK.3) airfoil
Max thickness 9.3% at 39.8% chord.
Max camber 4.1% at 39.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 116 (MVA MK.3) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0121900 0.0117200
 0.0245000 0.0188500
 0.0491900 0.0307000
 0.0739500 0.0398500
 0.0987200 0.0484000
 0.1484000 0.0608100
 0.1981600 0.0700200
 0.2978100 0.0832500
 0.3977000 0.0873800
 0.4978000 0.0835200
 0.5981000 0.0721600
 0.6985199 0.0563100
 0.7989800 0.0386500
 0.8994500 0.0209000
 0.9497000 0.0114200
 1.0000000 0.0017500

 0.0000000 0.0000000
 0.0127100 -.0080700
 0.0253500 -.0134300
 0.0505300 -.0202700
 0.0756300 -.0240100
 0.1006700 -.0254500
 0.1505600 -.0213300
 0.2004300 -.0163200
 0.3002600 -.0096900
 0.4001600 -.0057600
 0.5000600 -.0023200
 0.6000100 -.0002900
 0.6999800 0.0008400
 0.7999700 0.0009800
 0.9000000 -.0001800
 0.9500300 -.0010700
 1.0000000 -.0017500
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Polars for GOE 116 (MVA MK.3) AIRFOIL (goe116-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe116-il50,000929.6 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe116-il50,000537.3 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe116-il100,000958 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe116-il100,000556.8 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe116-il200,000978.4 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe116-il200,000576.2 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe116-il500,0009106.8 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe116-il500,000581.4 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   goe116-il1,000,0009100.3 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe116-il1,000,000591.9 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
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