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GOE 546 AIRFOIL (goe546-il)

GOE 546 AIRFOIL - Gottingen 546 airfoil


Airfoil goe546-il
Details Dat file Parser  
(goe546-il) GOE 546 AIRFOIL
Gottingen 546 airfoil
Max thickness 10.4% at 30% chord.
Max camber 3.6% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 546 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0208600
 0.0250000 0.0282200
 0.0500000 0.0399500
 0.0750000 0.0486700
 0.1000000 0.0559000
 0.1500000 0.0673500
 0.2000000 0.0748000
 0.3000000 0.0837000
 0.4000000 0.0851000
 0.5000000 0.0810000
 0.6000000 0.0717000
 0.7000000 0.0593000
 0.8000000 0.0422000
 0.9000000 0.0226000
 0.9500000 0.0125500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0116400
 0.0250000 -.0152800
 0.0500000 -.0185500
 0.0750000 -.0203300
 0.1000000 -.0216000
 0.1500000 -.0229500
 0.2000000 -.0232000
 0.3000000 -.0203000
 0.4000000 -.0154000
 0.5000000 -.0095000
 0.6000000 -.0046000
 0.7000000 -.0012000
 0.8000000 0.0007000
 0.9000000 0.0016000
 0.9500000 0.0010500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 546 AIRFOIL (goe546-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe546-il50,000938.4 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe546-il50,000538.6 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe546-il100,000959.4 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe546-il100,000558.6 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe546-il200,000980.5 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe546-il200,000576.2 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe546-il500,0009106.7 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe546-il500,000593.5 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   goe546-il1,000,0009124.7 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe546-il1,000,0005101.7 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
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