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GOE 534 AIRFOIL (goe534-il)

GOE 534 AIRFOIL - Gottingen 534 airfoil


Airfoil goe534-il
Details Dat file Parser  
(goe534-il) GOE 534 AIRFOIL
Gottingen 534 airfoil
Max thickness 14.1% at 19.6% chord.
Max camber 5.2% at 39.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 534 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0111700 0.0374000
 0.0231100 0.0533200
 0.0474200 0.0726800
 0.0719600 0.0855500
 0.0966300 0.0949300
 0.1462000 0.1071900
 0.1959700 0.1134600
 0.2958800 0.1160000
 0.3961300 0.1090600
 0.4965700 0.0966300
 0.5971200 0.0812000
 0.6978800 0.0620600
 0.7985000 0.0423500
 0.8992000 0.0224200
 0.9495800 0.0117100
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0130700 -.0160400
 0.0257800 -.0220800
 0.0510400 -.0291900
 0.0760900 -.0308000
 0.1011200 -.0314100
 0.1510900 -.0306400
 0.2009700 -.0273700
 0.3006000 -.0168300
 0.4001500 -.0042900
 0.4997600 0.0067400
 0.5995500 0.0127800
 0.6995300 0.0133300
 0.7996700 0.0093900
 0.8998600 0.0039500
 0.9499600 0.0012200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 534 AIRFOIL (goe534-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe534-il50,000920 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe534-il50,000532.5 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe534-il100,000944 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe534-il100,000550.2 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe534-il200,000965.4 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe534-il200,000567.4 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe534-il500,000993.2 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe534-il500,000591 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe534-il1,000,0009114.9 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe534-il1,000,0005110.2 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
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