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GOE 514 AIRFOIL (goe514-il)

GOE 514 AIRFOIL - Gottingen 514 airfoil


Airfoil goe514-il
Details Dat file Parser  
(goe514-il) GOE 514 AIRFOIL
Gottingen 514 airfoil
Max thickness 16.6% at 19.7% chord.
Max camber 6.4% at 39.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 514 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0118100 0.0322500
 0.0239600 0.0485200
 0.0484400 0.0725400
 0.0730500 0.0905700
 0.0977700 0.1036000
 0.1473500 0.1231700
 0.1970800 0.1357400
 0.2968900 0.1448800
 0.3969500 0.1420300
 0.4971300 0.1336900
 0.5974400 0.1188500
 0.6976500 0.0987800
 0.7984200 0.0736700
 0.8991400 0.0398300
 0.9495500 0.0209200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0127500 -.0117300
 0.0253900 -.0179500
 0.0505500 -.0254100
 0.0756300 -.0293700
 0.1007000 -.0323400
 0.1506900 -.0322600
 0.2006400 -.0296900
 0.3004200 -.0195400
 0.4002800 -.0128900
 0.5003200 -.0147400
 0.6004400 -.0205900
 0.7004400 -.0204400
 0.8003700 -.0172900
 0.9002301 -.0106500
 0.9501300 -.0060700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 514 AIRFOIL (goe514-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe514-il50,00097.2 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe514-il50,000526.1 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe514-il100,000945.3 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe514-il100,000541.9 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe514-il200,000957.2 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe514-il200,000551.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe514-il500,000969.2 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe514-il500,000564.7 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe514-il1,000,000984.1 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe514-il1,000,000578.1 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
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