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GOE 326 (PFALZ 55) AIRFOIL (goe326-il)

GOE 326 (PFALZ 55) AIRFOIL - Gottingen 326 (Pfalz 55) airfoil


Airfoil goe326-il
Details Dat file Parser  
(goe326-il) GOE 326 (PFALZ 55) AIRFOIL
Gottingen 326 (Pfalz 55) airfoil
Max thickness 8.2% at 29.9% chord.
Max camber 4.7% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 326 (PFALZ 55) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0132100 0.0197000
 0.0247300 0.0295300
 0.0496100 0.0440000
 0.0745100 0.0538800
 0.0994400 0.0613000
 0.1493300 0.0736600
 0.1992700 0.0815000
 0.2992000 0.0877200
 0.3992200 0.0860300
 0.4992800 0.0789400
 0.5993700 0.0690500
 0.6995100 0.0541700
 0.7996500 0.0380800
 0.8998200 0.0198900
 0.9499000 0.0112400
 1.0000000 0.0015000

 0.0000000 0.0000000
 0.0125900 -.0094000
 0.0250900 -.0106000
 0.0500800 -.0085400
 0.0750600 -.0064200
 0.1000400 -.0046900
 0.1500200 -.0012300
 0.1999800 0.0018200
 0.2999500 0.0059300
 0.3999200 0.0084400
 0.4999200 0.0088500
 0.5999300 0.0073600
 0.6999500 0.0053700
 0.7999800 0.0024800
 0.9000000 0.0000900
 0.9500100 -.0009500
 1.0000000 -.0015000
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Lednicer format dat file
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Polars for GOE 326 (PFALZ 55) AIRFOIL (goe326-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe326-il50,000932.5 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe326-il50,000540 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe326-il100,000956.3 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe326-il100,000559.1 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe326-il200,000977.2 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe326-il200,000577.2 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe326-il500,0009104.6 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe326-il500,0005100.1 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe326-il1,000,0009123.9 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe326-il1,000,0005116.7 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
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