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GOE 518 AIRFOIL (goe518-il)

GOE 518 AIRFOIL - Gottingen 518 airfoil


Airfoil goe518-il
Details Dat file Parser  
(goe518-il) GOE 518 AIRFOIL
Gottingen 518 airfoil
Max thickness 18% at 29.8% chord.
Max camber 7.3% at 29.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 518 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0120600 0.0436200
 0.0243700 0.0632400
 0.0491200 0.0884900
 0.0739300 0.1067400
 0.0988000 0.1204900
 0.1485900 0.1414900
 0.1984500 0.1549800
 0.2983700 0.1629800
 0.3984200 0.1584800
 0.4985300 0.1469900
 0.5987100 0.1294900
 0.6989300 0.1074900
 0.7992200 0.0784900
 0.8995700 0.0430000
 0.9497800 0.0220000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0126200 -.0123700
 0.0251500 -.0152500
 0.0501700 -.0175000
 0.0751900 -.0187500
 0.1001800 -.0185000
 0.1501800 -.0180000
 0.2001800 -.0180000
 0.3001700 -.0170000
 0.4001600 -.0160000
 0.5001500 -.0150000
 0.6001400 -.0140000
 0.7001300 -.0130000
 0.8001200 -.0120000
 0.9000800 -.0075000
 0.9500500 -.0045000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 518 AIRFOIL (goe518-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe518-il50,00096.5 at α=-3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe518-il50,000523.7 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe518-il100,000941.4 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe518-il100,000539.1 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe518-il200,000954.1 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe518-il200,000548.3 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe518-il500,000964.5 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe518-il500,000561.8 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe518-il1,000,000981 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe518-il1,000,000579.1 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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