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GOE 451 AIRFOIL (modified line 6) (goe451-il)

GOE 451 AIRFOIL (modified line 6) - Gottingen 451 airfoil


Airfoil goe451-il
Details Dat file Parser  
(goe451-il) GOE 451 AIRFOIL (modified line 6)
Gottingen 451 airfoil
Max thickness 4.4% at 30% chord.
Max camber 5.6% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 451 AIRFOIL (modified line 6)
       17.       17.

 0.0000000 0.0000000
 0.0124600 0.0120400
 0.0249500 0.0192624
 0.0499100 0.0291500
 0.0748900 0.0372200
 0.0998600 0.0453000
 0.1498300 0.0569500
 0.1998000 0.0651000
 0.2997800 0.0744000
 0.3997700 0.0772000
 0.4997800 0.0740000
 0.5998000 0.0658000
 0.6998400 0.0531000
 0.7998800 0.0384000
 0.8999400 0.0212000
 0.9499700 0.0113500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125100 -.0019600
 0.0250000 -.0004200
 0.0499900 0.0031500
 0.0749800 0.0067200
 0.0999700 0.0098000
 0.1499500 0.0174500
 0.1999300 0.0226000
 0.2999100 0.0304000
 0.3999000 0.0342000
 0.4999000 0.0335000
 0.5999100 0.0298000
 0.6999300 0.0241000
 0.7999500 0.0174000
 0.8999700 0.0087000
 0.9499800 0.0058500
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for GOE 451 AIRFOIL (modified line 6) (goe451-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe451-il50,000936.5 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe451-il100,000929.2 at α=1.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe451-il200,000950.7 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe451-il500,000937.3 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
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