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GOE 804 (EA 8) AIRFOIL (goe804-il)

GOE 804 (EA 8) AIRFOIL - Gottingen 804 (EA 8) airfoil


Airfoil goe804-il
Details Dat file Parser  
(goe804-il) GOE 804 (EA 8) AIRFOIL
Gottingen 804 (EA 8) airfoil
Max thickness 6% at 40% chord.
Max camber 6.3% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 804 (EA 8) AIRFOIL
       16.       16.

 0.0000000 0.0000000
 0.0250000 0.0231800
 0.0500000 0.0343500
 0.0750000 0.0435200
 0.1000000 0.0507000
 0.1500000 0.0630500
 0.2000000 0.0714000
 0.3000000 0.0841000
 0.4000000 0.0898000
 0.5000000 0.0915000
 0.6000000 0.0872000
 0.7000000 0.0779000
 0.8000000 0.0616000
 0.9000000 0.0363000
 0.9500000 0.0206500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0250000 -.0058200
 0.0500000 -.0036500
 0.0750000 -.0004700
 0.1000000 0.0037000
 0.1500000 0.0100500
 0.2000000 0.0164000
 0.3000000 0.0241000
 0.4000000 0.0298000
 0.5000000 0.0335000
 0.6000000 0.0342000
 0.7000000 0.0319000
 0.8000000 0.0286000
 0.9000000 0.0223000
 0.9500000 0.0146500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 804 (EA 8) AIRFOIL (goe804-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe804-il50,000943.7 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe804-il50,000541.1 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe804-il100,000970.6 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe804-il100,000567.6 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe804-il200,0009107.1 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe804-il200,0005107 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe804-il500,0009169.1 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe804-il500,0005157.3 at α=1.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe804-il1,000,0009211.4 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe804-il1,000,0005147 at α=0°Mach=0 Ncrit=5Xfoil predictionDetails
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