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GOE 388 AIRFOIL (goe388-il)

GOE 388 AIRFOIL - Gottingen 388 airfoil


Airfoil goe388-il
Details Dat file Parser  
(goe388-il) GOE 388 AIRFOIL
Gottingen 388 airfoil
Max thickness 10.2% at 29.9% chord.
Max camber 5.4% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 388 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0121800 0.0226700
 0.0245500 0.0325400
 0.0493300 0.0278900
 0.0741600 0.0600300
 0.0990200 0.0699800
 0.1488200 0.0846800
 0.1986800 0.0949700
 0.2985700 0.1028700
 0.3985600 0.1031600
 0.4986600 0.0959600
 0.5988200 0.0844500
 0.6990700 0.0665500
 0.7993400 0.0470500
 0.8996601 0.0243500
 0.9498200 0.0132500
 1.0000000 0.0010500

 0.0000000 0.0000000
 0.0126800 -.0127200
 0.0252000 -.0146500
 0.0502000 -.0143000
 0.0751900 -.0134500
 0.1001700 -.0125000
 0.1501200 -.0086100
 0.2000700 -.0052100
 0.2999900 0.0009800
 0.3999200 0.0055800
 0.4998900 0.0080700
 0.5998800 0.0083700
 0.6999000 0.0072600
 0.7999200 0.0058600
 0.8999600 0.0029500
 0.9499800 0.0012500
 1.0000000 -.0010500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 388 AIRFOIL (goe388-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe388-il50,000941.4 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe388-il50,000536.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe388-il100,000955.8 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe388-il100,000537.6 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe388-il200,000934.7 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe388-il200,000536.2 at α=2°Mach=0 Ncrit=5Xfoil predictionDetails
   goe388-il500,000940.2 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe388-il500,000541.6 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe388-il1,000,000953.5 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe388-il1,000,000567.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
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