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GOE 239 (MVA H.31) AIRFOIL (goe239-il)

GOE 239 (MVA H.31) AIRFOIL - Gottingen 239 (MVA H.31) airfoil


Airfoil goe239-il
Details Dat file Parser  
(goe239-il) GOE 239 (MVA H.31) AIRFOIL
Gottingen 239 (MVA H.31) airfoil
Max thickness 11.2% at 19.8% chord.
Max camber 6% at 39.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 239 (MVA H.31) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0120600 0.0242200
 0.0243600 0.0350400
 0.0490800 0.0503900
 0.0738500 0.0632400
 0.0986700 0.0733000
 0.1483700 0.0895000
 0.1982000 0.0997500
 0.2980000 0.1098200
 0.3980000 0.1098400
 0.4981600 0.1010700
 0.5983700 0.0894900
 0.6986500 0.0740200
 0.7990300 0.0530400
 0.8994700 0.0290700
 0.9496900 0.0167800
 1.0000000 0.0021000

 0.0000000 0.0000000
 0.0127300 -.0123700
 0.0252900 -.0160400
 0.0503400 -.0185000
 0.0753400 -.0189300
 0.1003400 -.0184700
 0.1503100 -.0170600
 0.2002200 -.0122600
 0.3000100 -.0005400
 0.3998100 0.0106800
 0.4997000 0.0162900
 0.5996600 0.0188100
 0.6996700 0.0182300
 0.7997700 0.0126600
 0.8998700 0.0070800
 0.9499500 0.0029900
 1.0000000 -.0021000
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Lednicer format dat file
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Polars for GOE 239 (MVA H.31) AIRFOIL (goe239-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe239-il50,000917.3 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe239-il50,000538.8 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe239-il100,000954.5 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe239-il100,000560.7 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe239-il200,000981.8 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe239-il200,000583.6 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe239-il500,0009118.1 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe239-il500,0005113 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe239-il1,000,0009144.3 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe239-il1,000,0005125.6 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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