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GOE 147 (MVA H.6) AIRFOIL (goe147-il)

GOE 147 (MVA H.6) AIRFOIL - Gottingen 147 (MVA H.6) airfoil


Airfoil goe147-il
Details Dat file Parser  
(goe147-il) GOE 147 (MVA H.6) AIRFOIL
Gottingen 147 (MVA H.6) airfoil
Max thickness 7.5% at 14.9% chord.
Max camber 3.8% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 147 (MVA H.6) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122200 0.0181900
 0.0245800 0.0271800
 0.0493700 0.0412600
 0.0742000 0.0520400
 0.0991000 0.0584200
 0.1489800 0.0666900
 0.1989200 0.0703500
 0.2989100 0.0707900
 0.3989700 0.0668200
 0.4991100 0.0581600
 0.5992600 0.0480000
 0.6994300 0.0370400
 0.7996100 0.0253700
 0.8997900 0.0138100
 0.9498800 0.0079800
 1.0000000 0.0016500

 0.0000000 0.0000000
 0.0126100 -.0078800
 0.0251700 -.0111100
 0.0502300 -.0151300
 0.0752400 -.0158500
 0.1002000 -.0132600
 0.1501300 -.0087000
 0.2000500 -.0029300
 0.2999300 0.0044000
 0.3999200 0.0072400
 0.4999000 0.0067700
 0.5999200 0.0053100
 0.6999400 0.0036400
 0.7999700 0.0018800
 0.8999800 0.0007000
 0.9499900 -.0003400
 1.0000000 -.0016500
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Lednicer format dat file
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Polars for GOE 147 (MVA H.6) AIRFOIL (goe147-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe147-il50,000929.2 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe147-il50,000536.1 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe147-il100,000948.6 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe147-il100,000549.9 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe147-il200,000964.3 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe147-il200,000566.1 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe147-il500,000986.8 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe147-il500,000586.3 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe147-il1,000,0009102.8 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe147-il1,000,0005101.4 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
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