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GOE 184 (MVA H.29) AIRFOIL (goe184-il)

GOE 184 (MVA H.29) AIRFOIL - Gottingen 184 (MVA H.29) airfoil


Airfoil goe184-il
Details Dat file Parser  
(goe184-il) GOE 184 (MVA H.29) AIRFOIL
Gottingen 184 (MVA H.29) airfoil
Max thickness 8.3% at 19.9% chord.
Max camber 5.3% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 184 (MVA H.29) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122000 0.0202800
 0.0245700 0.0294600
 0.0493400 0.0449200
 0.0741900 0.0553800
 0.0990600 0.0641500
 0.1488900 0.0760700
 0.1987600 0.0852000
 0.2986600 0.0916600
 0.3986900 0.0898200
 0.4988100 0.0814800
 0.5989700 0.0706400
 0.6991900 0.0555100
 0.7994300 0.0390700
 0.8996900 0.0209400
 0.9498400 0.0110700
 1.0000000 0.0011000

 0.0000000 0.0000000
 0.0126400 -.0099200
 0.0251300 -.0117300
 0.0502000 -.0138700
 0.0751600 -.0112000
 0.1001300 -.0086400
 0.1500400 -.0029100
 0.1999700 0.0023200
 0.2998400 0.0110800
 0.3997700 0.0159400
 0.4997600 0.0162000
 0.5997900 0.0143600
 0.6998300 0.0113200
 0.7999000 0.0071800
 0.8999500 0.0036400
 0.9499800 0.0015700
 1.0000000 -.0011000
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Lednicer format dat file
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Polars for GOE 184 (MVA H.29) AIRFOIL (goe184-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe184-il50,000934 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   goe184-il50,000539.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe184-il100,000957.4 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe184-il100,000560.4 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe184-il200,000979.4 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe184-il200,000579.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe184-il500,0009107.5 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe184-il500,0005102.7 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe184-il1,000,0009127.7 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe184-il1,000,0005111.9 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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