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GOE 335 (D.F.W.) AIRFOIL (goe335-il)

GOE 335 (D.F.W.) AIRFOIL - Gottingen 335 (D.F.W.) airfoil


Airfoil goe335-il
Details Dat file Parser  
(goe335-il) GOE 335 (D.F.W.) AIRFOIL
Gottingen 335 (D.F.W.) airfoil
Max thickness 6.9% at 20% chord.
Max camber 4.8% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 335 (D.F.W.) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0160900
 0.0250000 0.0251900
 0.0500000 0.0383800
 0.0750000 0.0480600
 0.1000000 0.0567500
 0.1500000 0.0686300
 0.2000000 0.0765000
 0.3000000 0.0812500
 0.4000000 0.0790000
 0.5000000 0.0737500
 0.6000000 0.0640000
 0.7000000 0.0507500
 0.8000000 0.0355000
 0.9000000 0.0202500
 0.9500000 0.0106300
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0069100
 0.0250000 -.0073100
 0.0500000 -.0056300
 0.0750000 -.0034400
 0.1000000 -.0007500
 0.1500000 0.0041200
 0.2000000 0.0080000
 0.3000000 0.0142500
 0.4000000 0.0170000
 0.5000000 0.0162500
 0.6000000 0.0140000
 0.7000000 0.0107500
 0.8000000 0.0070000
 0.9000000 0.0037500
 0.9500000 0.0021300
 1.0000000 0.0000000
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Polars for GOE 335 (D.F.W.) AIRFOIL (goe335-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe335-il50,000938.6 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe335-il50,000541.1 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe335-il100,000956.6 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe335-il100,000557.9 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe335-il200,000975.4 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe335-il200,000575.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe335-il500,0009102.1 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe335-il500,0005100.1 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe335-il1,000,0009123.5 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe335-il1,000,0005119.1 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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