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GOE 287 AIRFOIL (goe287-il)

GOE 287 AIRFOIL - Gottingen 287 airfoil


Airfoil goe287-il
Details Dat file Parser  
(goe287-il) GOE 287 AIRFOIL
Gottingen 287 airfoil
Max thickness 8.9% at 29.9% chord.
Max camber 4.9% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 287 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123600 0.0171000
 0.0247900 0.0261000
 0.0496600 0.0423000
 0.0745600 0.0547000
 0.0994800 0.0637100
 0.1493700 0.0777100
 0.1993100 0.0851100
 0.2992500 0.0923200
 0.3992500 0.0926300
 0.4993300 0.0828400
 0.5994400 0.0689600
 0.6995700 0.0526700
 0.7997200 0.0346800
 0.8998600 0.0178900
 0.9499300 0.0088900
 1.0000000 0.0025000

 0.0000000 0.0000000
 0.0125800 -.0098000
 0.0250800 -.0104000
 0.0500700 -.0089900
 0.0750600 -.0070900
 0.1000400 -.0050900
 0.1500200 -.0022800
 0.2000100 -.0001000
 0.2999700 0.0036300
 0.3999600 0.0050400
 0.4999600 0.0052500
 0.5999700 0.0036600
 0.6999800 0.0018700
 0.8000000 0.0005800
 0.9000100 -.0009100
 0.9500100 -.0017000
 1.0000000 -.0025000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 287 AIRFOIL (goe287-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe287-il50,000936.3 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe287-il50,000538 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe287-il100,000958.3 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe287-il100,000559.5 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe287-il200,000980 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe287-il200,000577.7 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe287-il500,0009106.3 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe287-il500,000594.5 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe287-il1,000,0009123 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe287-il1,000,0005106.6 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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