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GOE 223 (MVA H.34) AIRFOIL (goe223-il)

GOE 223 (MVA H.34) AIRFOIL - Gottingen 223 (MVA H.34) airfoil


Airfoil goe223-il
Details Dat file Parser  
(goe223-il) GOE 223 (MVA H.34) AIRFOIL
Gottingen 223 (MVA H.34) airfoil
Max thickness 18.8% at 29.1% chord.
Max camber 5.7% at 49.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 223 (MVA H.34) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0109000 0.0247100
 0.0224500 0.0392600
 0.0459600 0.0622900
 0.0698000 0.0800400
 0.0940500 0.0916100
 0.1426700 0.1127700
 0.1917000 0.1255100
 0.2908000 0.1416000
 0.3906500 0.1438900
 0.4913300 0.1339400
 0.5922900 0.1187000
 0.6937600 0.0960900
 0.7956401 0.0671200
 0.8977400 0.0348500
 0.9488800 0.0171800
 1.0000000 0.0010000

 0.0000000 0.0000000
 0.0134900 -.0151200
 0.0262900 -.0197900
 0.0518000 -.0276300
 0.0771800 -.0334800
 0.1024300 -.0373400
 0.1528900 -.0443600
 0.2031400 -.0483000
 0.3030100 -.0463000
 0.4022000 -.0338600
 0.5012000 -.0184200
 0.6002800 -.0042800
 0.6995500 0.0069700
 0.7992900 0.0109500
 0.8994800 0.0079700
 0.9497600 0.0037300
 1.0000000 -.0010000
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Lednicer format dat file
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Polars for GOE 223 (MVA H.34) AIRFOIL (goe223-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe223-il50,00095 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe223-il50,000515.8 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe223-il100,000943.4 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe223-il100,000548.9 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe223-il200,000973 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe223-il200,000567 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe223-il500,000995.5 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe223-il500,000580.6 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   goe223-il1,000,0009108.5 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe223-il1,000,000580.4 at α=0.5°Mach=0 Ncrit=5Xfoil predictionDetails
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