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GOE 392 AIRFOIL (goe392-il)

GOE 392 AIRFOIL - Gottingen 392 airfoil


Airfoil goe392-il
Details Dat file Parser  
(goe392-il) GOE 392 AIRFOIL
Gottingen 392 airfoil
Max thickness 10.2% at 30% chord.
Max camber 4.8% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 392 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0111700
 0.0250000 0.0188500
 0.0500000 0.0332000
 0.0750000 0.0445500
 0.1000000 0.0544000
 0.1500000 0.0706000
 0.2000000 0.0828000
 0.3000000 0.0947000
 0.4000000 0.0966000
 0.5000000 0.0910000
 0.6000000 0.0804000
 0.7000000 0.0653000
 0.8000000 0.0472000
 0.9000000 0.0271000
 0.9500000 0.0148000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0053300
 0.0250000 -.0066500
 0.0500000 -.0088000
 0.0750000 -.0104500
 0.1000000 -.0111000
 0.1500000 -.0119000
 0.2000000 -.0112000
 0.3000000 -.0068000
 0.4000000 0.0001000
 0.5000000 0.0038000
 0.6000000 0.0059000
 0.7000000 0.0078000
 0.8000000 0.0072000
 0.9000000 0.0051000
 0.9500000 0.0023000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 392 AIRFOIL (goe392-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe392-il50,000937.7 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe392-il50,000538.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe392-il100,000959.3 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe392-il100,000558.1 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe392-il200,000978.8 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe392-il200,000577.5 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe392-il500,0009105.3 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe392-il500,0005102.6 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe392-il1,000,0009125.8 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe392-il1,000,0005120.6 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
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