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GOE 144 (MVA H.21) AIRFOIL (goe144-il)

GOE 144 (MVA H.21) AIRFOIL - Gottingen 144 (MVA H.21) airfoil


Airfoil goe144-il
Details Dat file Parser  
(goe144-il) GOE 144 (MVA H.21) AIRFOIL
Gottingen 144 (MVA H.21) airfoil
Max thickness 7.3% at 19.9% chord.
Max camber 4.7% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 144 (MVA H.21) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122600 0.0157800
 0.0246300 0.0249700
 0.0494000 0.0397400
 0.0742600 0.0491100
 0.0991500 0.0564900
 0.1489800 0.0680300
 0.1988800 0.0748800
 0.2987800 0.0813800
 0.3988000 0.0799800
 0.4989000 0.0732800
 0.5990500 0.0635900
 0.6992199 0.0519900
 0.7994200 0.0387900
 0.8996900 0.0208000
 0.9498200 0.0117500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0126400 -.0092100
 0.0251800 -.0118200
 0.0502100 -.0142500
 0.0751900 -.0128700
 0.1001700 -.0113000
 0.1500700 -.0043500
 0.1999700 0.0019000
 0.2998200 0.0118000
 0.3997800 0.0144000
 0.4997800 0.0148000
 0.5998000 0.0139500
 0.6998200 0.0122000
 0.7998800 0.0080000
 0.8999400 0.0041000
 0.9499700 0.0020500
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for GOE 144 (MVA H.21) AIRFOIL (goe144-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe144-il50,000938.6 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe144-il50,000541.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe144-il100,000959 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe144-il100,000560.3 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe144-il200,000979.3 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe144-il200,000578 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe144-il500,0009106.1 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe144-il500,000598.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe144-il1,000,0009125.3 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe144-il1,000,000595.4 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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