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GOE 325 (PFALZ 54) AIRFOIL (goe325-il)

GOE 325 (PFALZ 54) AIRFOIL - Gottingen 325 (Pfalz 54) airfoil


Airfoil goe325-il
Details Dat file Parser  
(goe325-il) GOE 325 (PFALZ 54) AIRFOIL
Gottingen 325 (Pfalz 54) airfoil
Max thickness 8.2% at 20% chord.
Max camber 4.6% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 325 (PFALZ 54) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0181100
 0.0250000 0.0282200
 0.0500000 0.0424500
 0.0750000 0.0536700
 0.1000000 0.0629000
 0.1500000 0.0763500
 0.2000000 0.0838000
 0.3000000 0.0877000
 0.4000000 0.0846000
 0.5000000 0.0765000
 0.6000000 0.0674000
 0.7000000 0.0553000
 0.8000000 0.0412000
 0.9000000 0.0231000
 0.9500000 0.0125500
 1.0000000 0.0030000

 0.0000000 0.0000000
 0.0125000 -.0088900
 0.0250000 -.0097800
 0.0500000 -.0085500
 0.0750000 -.0063200
 0.1000000 -.0041000
 0.1500000 -.0006500
 0.2000000 0.0018000
 0.3000000 0.0057000
 0.4000000 0.0076000
 0.5000000 0.0080000
 0.6000000 0.0074000
 0.7000000 0.0063000
 0.8000000 0.0047000
 0.9000000 0.0026000
 0.9500000 0.0015500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 325 (PFALZ 54) AIRFOIL (goe325-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe325-il50,000935.1 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   goe325-il50,000537.8 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe325-il100,000953.7 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe325-il100,000555.3 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe325-il200,000972.9 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe325-il200,000573.4 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe325-il500,0009100 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe325-il500,000598.3 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe325-il1,000,0009121.4 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe325-il1,000,0005117.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
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