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GOE 422 AIRFOIL (goe422-il)

GOE 422 AIRFOIL - Gottingen 422 airfoil


Airfoil goe422-il
Details Dat file Parser  
(goe422-il) GOE 422 AIRFOIL
Gottingen 422 airfoil
Max thickness 17.1% at 29.5% chord.
Max camber 6.5% at 39.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 422 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0113200 0.0345900
 0.0232700 0.0505000
 0.0475300 0.0722300
 0.0720400 0.0863700
 0.0965900 0.0995100
 0.1458900 0.1200000
 0.1953900 0.1344900
 0.2949500 0.1475000
 0.3949200 0.1483300
 0.4952100 0.1399600
 0.5957500 0.1241000
 0.6965500 0.1008600
 0.7975300 0.0722200
 0.8986300 0.0398800
 0.9493200 0.0197100
 1.0000000 0.0010500

 0.0000000 0.0000000
 0.0132200 -.0209500
 0.0258800 -.0258100
 0.0510200 -.0298500
 0.0760700 -.0310900
 0.1010500 -.0307400
 0.1510300 -.0301300
 0.2009700 -.0284200
 0.3007800 -.0229000
 0.4006100 -.0178800
 0.5004600 -.0133600
 0.6003200 -.0094400
 0.7002100 -.0060200
 0.8000500 -.0015000
 0.9001100 -.0009800
 0.9500400 -.0011600
 1.0000000 -.0010500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 422 AIRFOIL (goe422-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe422-il50,00095.8 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe422-il50,000519.4 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe422-il100,000944.9 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe422-il100,000547.6 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe422-il200,000971 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe422-il200,000566.5 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe422-il500,000997.4 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe422-il500,000585.3 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   goe422-il1,000,0009117.3 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe422-il1,000,000598.8 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
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