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GOE 418 AIRFOIL (goe418-il)

GOE 418 AIRFOIL - Gottingen 418 airfoil


Airfoil goe418-il
Details Dat file Parser  
(goe418-il) GOE 418 AIRFOIL
Gottingen 418 airfoil
Max thickness 12.7% at 20% chord.
Max camber 5.1% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 418 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0344600
 0.0250000 0.0459300
 0.0500000 0.0628500
 0.0750000 0.0747700
 0.1000000 0.0827000
 0.1500000 0.0955500
 0.2000000 0.1044000
 0.3000000 0.1111000
 0.4000000 0.1088000
 0.5000000 0.0985000
 0.6000000 0.0832000
 0.7000000 0.0659000
 0.8000000 0.0456000
 0.9000000 0.0233000
 0.9500000 0.0121500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0195400
 0.0250000 -.0270700
 0.0500000 -.0331500
 0.0750000 -.0342200
 0.1000000 -.0323000
 0.1500000 -.0274500
 0.2000000 -.0226000
 0.3000000 -.0129000
 0.4000000 -.0072000
 0.5000000 -.0035000
 0.6000000 -.0018000
 0.7000000 -.0011000
 0.8000000 0.0006000
 0.9000000 0.0003000
 0.9500000 0.0001500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 418 AIRFOIL (goe418-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe418-il50,000912.5 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe418-il50,000532.3 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe418-il100,000952.6 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe418-il100,000554 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe418-il200,000975.1 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe418-il200,000571.6 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe418-il500,0009101.6 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe418-il500,000590.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe418-il1,000,0009117.7 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe418-il1,000,000592.9 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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