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GOE 442 AIRFOIL (goe442-il)

GOE 442 AIRFOIL - Gottingen 442 airfoil


Airfoil goe442-il
Details Dat file Parser  
(goe442-il) GOE 442 AIRFOIL
Gottingen 442 airfoil
Max thickness 7.7% at 19.9% chord.
Max camber 4.3% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 442 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123100 0.0211100
 0.0247200 0.0307200
 0.0496000 0.0444500
 0.0745200 0.0536700
 0.0994600 0.0599000
 0.1493800 0.0693400
 0.1993200 0.0757900
 0.2992800 0.0801900
 0.3993000 0.0775900
 0.4993600 0.0709900
 0.5994300 0.0628900
 0.6995300 0.0518000
 0.7996600 0.0382000
 0.8998100 0.0212000
 0.9499000 0.0110500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125600 -.0068900
 0.0250800 -.0087700
 0.0500800 -.0085500
 0.0750700 -.0073200
 0.1000600 -.0066000
 0.1500400 -.0041500
 0.2000100 -.0012000
 0.2999500 0.0052000
 0.3999200 0.0091000
 0.4999000 0.0110000
 0.5999000 0.0109000
 0.6999199 0.0088000
 0.7999400 0.0062000
 0.8999800 0.0023000
 0.9499900 0.0010500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 442 AIRFOIL (goe442-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe442-il50,000935.3 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe442-il50,000540.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe442-il100,000954.3 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe442-il100,000557.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe442-il200,000973.4 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe442-il200,000573 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe442-il500,000997.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe442-il500,000593 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe442-il1,000,0009115 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe442-il1,000,0005106.2 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
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