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GOE 502 AIRFOIL (goe502-il)

GOE 502 AIRFOIL - Gottingen 502 airfoil


Airfoil goe502-il
Details Dat file Parser  
(goe502-il) GOE 502 AIRFOIL
Gottingen 502 airfoil
Max thickness 15.9% at 29.3% chord.
Max camber 6.1% at 49.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 502 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0110100 0.0295600
 0.0228500 0.0426500
 0.0469300 0.0608700
 0.0712100 0.0751000
 0.0956400 0.0863300
 0.1447800 0.1033100
 0.1941300 0.1163000
 0.2933900 0.1308200
 0.3932900 0.1328600
 0.4936700 0.1254300
 0.5943700 0.1115200
 0.6954200 0.0906200
 0.7966600 0.0662300
 0.8982100 0.0353600
 0.9490400 0.0189300
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0137500 -.0248100
 0.0266000 -.0316600
 0.0518900 -.0373800
 0.0771000 -.0416100
 0.1021900 -.0433400
 0.1521600 -.0428200
 0.2019900 -.0393000
 0.3013800 -.0272800
 0.4007200 -.0142600
 0.5001400 -.0027400
 0.5997600 0.0047900
 0.6995000 0.0098200
 0.7994500 0.0108700
 0.8996000 0.0079300
 0.9496500 0.0043900
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 502 AIRFOIL (goe502-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe502-il50,00095.4 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe502-il50,000518.7 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe502-il100,000942.1 at α=11°Mach=0 Ncrit=9Xfoil predictionDetails
   goe502-il100,000553 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe502-il200,000976 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe502-il200,000575.1 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe502-il500,0009106.7 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe502-il500,0005100.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe502-il1,000,0009132.2 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe502-il1,000,0005112.7 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
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