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GOE 227 (MVA H.37) AIRFOIL (goe227-il)

GOE 227 (MVA H.37) AIRFOIL - Gottingen 227 (MVA H.37) airfoil


Airfoil goe227-il
Details Dat file Parser  
(goe227-il) GOE 227 (MVA H.37) AIRFOIL
Gottingen 227 (MVA H.37) airfoil
Max thickness 14.6% at 25% chord.
Max camber 7.8% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 227 (MVA H.37) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0253600
 0.0250000 0.0377300
 0.0500000 0.0584500
 0.0750000 0.0751700
 0.1000000 0.0879000
 0.1500000 0.1083500
 0.2000000 0.1228000
 0.2500000 0.1322500
 0.3000000 0.1377000
 0.4000000 0.1406000
 0.5000000 0.1355000
 0.6000000 0.1184000
 0.7000000 0.0973000
 0.8000000 0.0692000
 0.9000000 0.0381000
 1.0000000 0.0030000

 0.0000000 0.0000000
 0.0125000 -.0166400
 0.0250000 -.0222700
 0.0500000 -.0265500
 0.0750000 -.0268200
 0.1000000 -.0261000
 0.1500000 -.0226500
 0.2000000 -.0192000
 0.2500000 -.0137500
 0.3000000 -.0063000
 0.4000000 0.0086000
 0.5000000 0.0215000
 0.6000000 0.0314000
 0.7000000 0.0343000
 0.8000000 0.0322000
 0.9000000 0.0201000
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for GOE 227 (MVA H.37) AIRFOIL (goe227-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe227-il50,00097.9 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe227-il50,000523.3 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe227-il100,000949.6 at α=10.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe227-il100,000558.6 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe227-il200,000988 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe227-il200,000588.5 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe227-il500,0009131.7 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe227-il500,0005118.3 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe227-il1,000,0009155.3 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe227-il1,000,0005134.8 at α=2°Mach=0 Ncrit=5Xfoil predictionDetails
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