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GOE 286 AIRFOIL (goe286-il)

GOE 286 AIRFOIL - Gottingen 286 airfoil


Airfoil goe286-il
Details Dat file Parser  
(goe286-il) GOE 286 AIRFOIL
Gottingen 286 airfoil
Max thickness 9.4% at 29.9% chord.
Max camber 4.1% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 286 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122500 0.0207500
 0.0246200 0.0315000
 0.0494500 0.0447000
 0.0743100 0.0568100
 0.0992200 0.0636100
 0.1490700 0.0759200
 0.1989800 0.0836300
 0.2989300 0.0877500
 0.3989700 0.0842700
 0.4990600 0.0766900
 0.5992100 0.0644100
 0.6993700 0.0520300
 0.7995600 0.0362500
 0.8997600 0.0197800
 0.9498800 0.0101900
 1.0000000 0.0025000

 0.0000000 0.0000000
 0.0126400 -.0116500
 0.0251600 -.0131900
 0.0501700 -.0140900
 0.0751600 -.0132800
 0.1001500 -.0122800
 0.1501200 -.0099700
 0.2001000 -.0081600
 0.3000700 -.0057400
 0.4000400 -.0033200
 0.5000300 -.0027000
 0.6000300 -.0020800
 0.7000300 -.0020600
 0.8000400 -.0031400
 0.9000400 -.0031200
 0.9500400 -.0031100
 1.0000000 -.0025000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 286 AIRFOIL (goe286-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe286-il50,000927.9 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe286-il50,000537.6 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe286-il100,000952.2 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe286-il100,000554.5 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe286-il200,000972.3 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe286-il200,000565.5 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe286-il500,000983.6 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe286-il500,000578.8 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe286-il1,000,000995.3 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe286-il1,000,000589.9 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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