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GOE 517 AIRFOIL (goe517-il)

GOE 517 AIRFOIL - Gottingen 517 airfoil


Airfoil goe517-il
Details Dat file Parser  
(goe517-il) GOE 517 AIRFOIL
Gottingen 517 airfoil
Max thickness 7% at 30% chord.
Max camber 4.7% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 517 AIRFOIL
       13.       13.

 0.0000000 0.0000000
 0.0250000 0.0246900
 0.0500000 0.0373700
 0.1000000 0.0552500
 0.2000000 0.0745000
 0.3000000 0.0807500
 0.4000000 0.0810000
 0.5000000 0.0747500
 0.6000000 0.0660000
 0.7000000 0.0532500
 0.8000000 0.0370000
 0.9000000 0.0197500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0250000 -.0068100
 0.0500000 -.0071200
 0.1000000 -.0027500
 0.2000000 0.0060000
 0.3000000 0.0107500
 0.4000000 0.0120000
 0.5000000 0.0112500
 0.6000000 0.0090000
 0.7000000 0.0052500
 0.8000000 0.0030000
 0.9000000 0.0007500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 517 AIRFOIL (goe517-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe517-il50,000937.4 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe517-il50,000540.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe517-il100,000955.1 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe517-il100,000560.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe517-il200,000975 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe517-il200,000579.1 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe517-il500,0009103 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe517-il500,0005102 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe517-il1,000,0009121.7 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe517-il1,000,0005117.7 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
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