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GOE 478 AIRFOIL (goe478-il)

GOE 478 AIRFOIL - Gottingen 478 airfoil


Airfoil goe478-il
Details Dat file Parser  
(goe478-il) GOE 478 AIRFOIL
Gottingen 478 airfoil
Max thickness 13.4% at 29.6% chord.
Max camber 4.3% at 39.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 478 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0114600 0.0269400
 0.0235000 0.0389000
 0.0479100 0.0543400
 0.0724700 0.0657900
 0.0971200 0.0747400
 0.1466100 0.0881400
 0.1962400 0.0975600
 0.2958500 0.1078900
 0.3958500 0.1077400
 0.4961100 0.1011000
 0.5965200 0.0904700
 0.6972300 0.0718400
 0.7980500 0.0507200
 0.8989601 0.0271100
 0.9494400 0.0145500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0133700 -.0224900
 0.0260600 -.0275000
 0.0512100 -.0315300
 0.0762900 -.0335600
 0.1012900 -.0336000
 0.1512600 -.0326800
 0.2011500 -.0297600
 0.3009800 -.0254100
 0.4008300 -.0215700
 0.5006800 -.0177200
 0.6005300 -.0138800
 0.7003900 -.0100400
 0.8002600 -.0066900
 0.9001300 -.0033500
 0.9500500 -.0014200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 478 AIRFOIL (goe478-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe478-il50,000919.7 at α=12.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe478-il50,000531.2 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe478-il100,000951.6 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe478-il100,000553 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe478-il200,000973.5 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe478-il200,000571 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe478-il500,0009101.3 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe478-il500,000595.4 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe478-il1,000,0009125.5 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe478-il1,000,0005114.8 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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