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GOE 383 AIRFOIL (goe383-il)

GOE 383 AIRFOIL - Gottingen 383 airfoil


Airfoil goe383-il
Details Dat file Parser  
(goe383-il) GOE 383 AIRFOIL
Gottingen 383 airfoil
Max thickness 20.2% at 28.7% chord.
Max camber 5% at 38.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 383 AIRFOIL
       17.       17.

 0.0000200 0.0000000
 0.0091300 0.0381100
 0.0204100 0.0518100
 0.0436200 0.0719700
 0.0672100 0.0878700
 0.0909300 0.1022700
 0.1390900 0.1230500
 0.1879000 0.1363800
 0.2866900 0.1499600
 0.3868000 0.1487400
 0.4877500 0.1380100
 0.5895900 0.1172500
 0.6918100 0.0923300
 0.7943100 0.0641300
 0.8970800 0.0328600
 0.9485700 0.0161300
 1.0000000 0.0016000

 0.0000200 0.0000000
 0.0148500 -.0257800
 0.0278600 -.0320300
 0.0534600 -.0388500
 0.0789200 -.0439900
 0.1042000 -.0471500
 0.1544600 -.0505800
 0.2046800 -.0525300
 0.3046000 -.0516500
 0.4043200 -.0486000
 0.5038800 -.0435600
 0.6032800 -.0368300
 0.7024900 -.0280200
 0.8017099 -.0192100
 0.9009200 -.0104000
 0.9505300 -.0059900
 1.0000000 -.0016000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 383 AIRFOIL (goe383-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe383-il50,00093.6 at α=11.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe383-il50,000513.9 at α=0.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe383-il100,000925 at α=1.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe383-il100,000540.5 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe383-il200,000962.2 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe383-il200,000560.4 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe383-il500,000988.4 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe383-il500,000583.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe383-il1,000,0009111.7 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe383-il1,000,0005106.1 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
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