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GOE 382 AIRFOIL (goe382-il)

GOE 382 AIRFOIL - Gottingen 382 airfoil


Airfoil goe382-il
Details Dat file Parser  
(goe382-il) GOE 382 AIRFOIL
Gottingen 382 airfoil
Max thickness 20% at 29% chord.
Max camber 6% at 39% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 382 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0104800 0.0309900
 0.0218800 0.0477300
 0.0451100 0.0747500
 0.0689000 0.0933100
 0.0929600 0.1076800
 0.1415000 0.1299600
 0.1904800 0.1454700
 0.2895400 0.1598500
 0.3896300 0.1585000
 0.4904200 0.1464000
 0.5918200 0.1249300
 0.6935199 0.0990900
 0.7954800 0.0690600
 0.8977200 0.0348600
 0.9488900 0.0169100
 1.0000000 0.0010500

 0.0000000 0.0000000
 0.0138800 -.0210900
 0.0280400 -.0263600
 0.0521100 -.0321900
 0.0772800 -.0348400
 0.1025200 -.0384900
 0.1526600 -.0405100
 0.2027200 -.0415300
 0.3026400 -.0402900
 0.4024500 -.0374600
 0.5022000 -.0336300
 0.6017800 -.0271100
 0.7013500 -.0206000
 0.8009200 -.0140800
 0.9005001 -.0075600
 0.9502800 -.0043000
 1.0000000 -.0010500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 382 AIRFOIL (goe382-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe382-il50,00093.5 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe382-il50,000514 at α=0°Mach=0 Ncrit=5Xfoil predictionDetails
   goe382-il100,000925.5 at α=1.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe382-il100,000539.7 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe382-il200,000960.9 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe382-il200,000559.5 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe382-il500,000987 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe382-il500,000581.9 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe382-il1,000,0009109.6 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe382-il1,000,0005103.9 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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