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GOE 436 AIRFOIL (goe436-il)

GOE 436 AIRFOIL - Gottingen 436 airfoil


Airfoil goe436-il
Details Dat file Parser  
(goe436-il) GOE 436 AIRFOIL
Gottingen 436 airfoil
Max thickness 11% at 30% chord.
Max camber 3.8% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 436 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0223100
 0.0250000 0.0326300
 0.0500000 0.0462500
 0.0750000 0.0578700
 0.1000000 0.0665000
 0.1500000 0.0792500
 0.2000000 0.0875000
 0.3000000 0.0925000
 0.4000000 0.0895000
 0.5000000 0.0830000
 0.6000000 0.0720000
 0.7000000 0.0585000
 0.8000000 0.0410000
 0.9000000 0.0220000
 0.9500000 0.0112500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0146900
 0.0250000 -.0198700
 0.0500000 -.0227500
 0.0750000 -.0228300
 0.1000000 -.0225000
 0.1500000 -.0212500
 0.2000000 -.0200000
 0.3000000 -.0175000
 0.4000000 -.0150000
 0.5000000 -.0125000
 0.6000000 -.0100000
 0.7000000 -.0075000
 0.8000000 -.0050000
 0.9000000 -.0025000
 0.9500000 -.0012500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 436 AIRFOIL (goe436-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe436-il50,000923.5 at α=12°Mach=0 Ncrit=9Xfoil predictionDetails
   goe436-il50,000534.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe436-il100,000947.8 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe436-il100,000551.6 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe436-il200,000968.2 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe436-il200,000569.1 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe436-il500,000996.7 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe436-il500,000592.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe436-il1,000,0009118.3 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe436-il1,000,0005108.7 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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