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GOE 118 (MVA MK.7) AIRFOIL (goe118-il)

GOE 118 (MVA MK.7) AIRFOIL - Gottingen 118 (MVA MK.7) airfoil


Airfoil goe118-il
Details Dat file Parser  
(goe118-il) GOE 118 (MVA MK.7) AIRFOIL
Gottingen 118 (MVA MK.7) airfoil
Max thickness 8.6% at 29.9% chord.
Max camber 5.7% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 118 (MVA MK.7) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124000 0.0120000
 0.0248500 0.0191000
 0.0497300 0.0334000
 0.0746500 0.0441000
 0.0995600 0.0549000
 0.1494300 0.0706000
 0.1993300 0.0837000
 0.2992200 0.0972100
 0.3992000 0.0994100
 0.4992500 0.0931200
 0.5993500 0.0807200
 0.6994900 0.0639300
 0.7996399 0.0450400
 0.8998100 0.0241400
 0.9498900 0.0130500
 1.0000000 0.0010500

 0.0000000 0.0000000
 0.0125200 -.0045000
 0.0250500 -.0061000
 0.0500700 -.0087000
 0.0750600 -.0075000
 0.1000400 -.0047900
 0.1500000 0.0005100
 0.1999600 0.0045100
 0.2999100 0.0108100
 0.3998800 0.0152200
 0.4998600 0.0174200
 0.5998600 0.0172300
 0.6998800 0.0150300
 0.7999200 0.0103400
 0.8999600 0.0051400
 0.9499800 0.0020500
 1.0000000 -.0010500
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Lednicer format dat file
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Polars for GOE 118 (MVA MK.7) AIRFOIL (goe118-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe118-il50,000924.3 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe118-il50,000540.7 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe118-il100,000962 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe118-il100,000561.7 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe118-il200,000983.1 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe118-il200,000582.7 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe118-il500,0009112.3 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe118-il500,0005108.9 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe118-il1,000,0009134.1 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe118-il1,000,0005120.6 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
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