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GOE 329 (PFALZ 58) AIRFOIL (goe329-il)

GOE 329 (PFALZ 58) AIRFOIL - Gottingen 329 (Pfalz 58) airfoil


Airfoil goe329-il
Details Dat file Parser  
(goe329-il) GOE 329 (PFALZ 58) AIRFOIL
Gottingen 329 (Pfalz 58) airfoil
Max thickness 10.2% at 29.9% chord.
Max camber 5.5% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 329 (PFALZ 58) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123000 0.0203200
 0.0247000 0.0304400
 0.0495400 0.0466900
 0.0744200 0.0592300
 0.0993100 0.0701700
 0.1491500 0.0870600
 0.1990400 0.0979500
 0.2989600 0.1061300
 0.3989800 0.1039100
 0.4990600 0.0963900
 0.5991700 0.0847700
 0.6993300 0.0685500
 0.7995300 0.0482400
 0.8997400 0.0263200
 0.9498500 0.0151100
 1.0000000 0.0030000

 0.0000000 0.0000000
 0.0126200 -.0126800
 0.0251200 -.0120500
 0.0500900 -.0096100
 0.0750700 -.0072600
 0.1000500 -.0055200
 0.1500200 -.0020300
 0.1999900 0.0011600
 0.2999600 0.0045400
 0.3999400 0.0056200
 0.4999400 0.0058000
 0.5999500 0.0047800
 0.6999700 0.0030600
 0.7999800 0.0019400
 0.9000000 0.0002200
 0.9500100 -.0007900
 1.0000000 -.0030000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 329 (PFALZ 58) AIRFOIL (goe329-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe329-il50,000923.6 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe329-il50,000537.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe329-il100,000953.3 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   goe329-il100,000556.2 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe329-il200,000973.9 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe329-il200,000575.2 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe329-il500,0009104.5 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe329-il500,0005103.3 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe329-il1,000,0009129.7 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe329-il1,000,0005125.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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