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GOE 488 AIRFOIL (goe488-il)

GOE 488 AIRFOIL - Gottingen 488 airfoil


Airfoil goe488-il
Details Dat file Parser  
(goe488-il) GOE 488 AIRFOIL
Gottingen 488 airfoil
Max thickness 6.8% at 19.9% chord.
Max camber 3% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 488 AIRFOIL
       16.       16.

 0.0000000 0.0000000
 0.0122900 0.0136900
 0.0246600 0.0218800
 0.0495000 0.0322700
 0.0743700 0.0406500
 0.0992800 0.0465400
 0.1491500 0.0548100
 0.1990700 0.0600900
 0.2990200 0.0631300
 0.3990200 0.0631800
 0.4990600 0.0607400
 0.5991500 0.0547900
 0.6992800 0.0463400
 0.7994800 0.0333900
 0.8997200 0.0179500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0126900 -.0123000
 0.0252300 -.0146100
 0.0502400 -.0152200
 0.0752300 -.0148300
 0.1002200 -.0139500
 0.1501700 -.0111700
 0.2001200 -.0079000
 0.3000400 -.0028500
 0.4000400 -.0023000
 0.5000400 -.0027500
 0.6000500 -.0032000
 0.7000600 -.0036500
 0.8000600 -.0041000
 0.9000300 -.0020500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 488 AIRFOIL (goe488-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe488-il50,000937.2 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe488-il50,000537.7 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe488-il100,000955.2 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe488-il100,000551.3 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe488-il200,000974.6 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe488-il200,000564.8 at α=2°Mach=0 Ncrit=5Xfoil predictionDetails
   goe488-il500,000996.4 at α=1.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe488-il500,000579.7 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe488-il1,000,0009101.4 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe488-il1,000,000589.4 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
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