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GOE 244 (MVA PR.4) AIRFOIL (goe244-il)

GOE 244 (MVA PR.4) AIRFOIL - Gottingen 244 (MVA PR.4) airfoil


Airfoil goe244-il
Details Dat file Parser  
(goe244-il) GOE 244 (MVA PR.4) AIRFOIL
Gottingen 244 (MVA PR.4) airfoil
Max thickness 17.7% at 19.6% chord.
Max camber 10% at 49.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 244 (MVA PR.4) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0116000 0.0407600
 0.0236000 0.0635200
 0.0479600 0.0928600
 0.0725200 0.1126000
 0.0972100 0.1270400
 0.1467400 0.1482300
 0.1964000 0.1635200
 0.2961400 0.1755200
 0.3961800 0.1737200
 0.4963800 0.1644200
 0.5967900 0.1461300
 0.6973600 0.1201400
 0.7981000 0.0865600
 0.8989900 0.0459800
 0.9494900 0.0230900
 1.0000000 0.0010000

 0.0000000 0.0000000
 0.0128700 -.0169200
 0.0254300 -.0194400
 0.0504800 -.0218900
 0.0754700 -.0213400
 0.1004600 -.0207900
 0.1504100 -.0187900
 0.2002800 -.0127900
 0.2999400 0.0026000
 0.3995900 0.0185900
 0.4992100 0.0357800
 0.5989500 0.0476800
 0.6988500 0.0523700
 0.7989600 0.0470800
 0.8993800 0.0282900
 0.9496900 0.0138900
 1.0000000 -.0010000
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Lednicer format dat file
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Polars for GOE 244 (MVA PR.4) AIRFOIL (goe244-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe244-il50,00097.9 at α=0.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe244-il50,000525 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe244-il100,000950.1 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe244-il100,000547.8 at α=0.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe244-il200,000973.3 at α=0.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe244-il200,000564.3 at α=0.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe244-il500,000992.3 at α=-0.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe244-il500,000579.5 at α=1.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe244-il1,000,0009105.6 at α=1.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe244-il1,000,000598.8 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
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