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GOE 195 AIRFOIL (goe195-il)

GOE 195 AIRFOIL - Gottingen 195 airfoil


Airfoil goe195-il
Details Dat file Parser  
(goe195-il) GOE 195 AIRFOIL
Gottingen 195 airfoil
Max thickness 8.6% at 20% chord.
Max camber 5.1% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 195 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0202100
 0.0250000 0.0284200
 0.0500000 0.0418500
 0.0750000 0.0512800
 0.1000000 0.0587000
 0.1500000 0.0705500
 0.2000000 0.0784000
 0.3000000 0.0871000
 0.4000000 0.0878000
 0.5000000 0.0815000
 0.6000000 0.0732000
 0.7000000 0.0599000
 0.8000000 0.0446000
 0.9000000 0.0253000
 0.9500000 0.0141500
 1.0000000 0.0020000

 0.0000000 0.0000000
 0.0125000 -.0117900
 0.0250000 -.0135700
 0.0500000 -.0151500
 0.0750000 -.0157200
 0.1000000 -.0153000
 0.1500000 -.0124500
 0.2000000 -.0076000
 0.3000000 0.0051000
 0.4000000 0.0138000
 0.5000000 0.0205000
 0.6000000 0.0242000
 0.7000000 0.0229000
 0.8000000 0.0166000
 0.9000000 0.0083000
 0.9500000 0.0041500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 195 AIRFOIL (goe195-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe195-il50,000940.7 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe195-il50,000544 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe195-il100,000963.3 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe195-il100,000564.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe195-il200,000986 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe195-il200,000584 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe195-il500,0009116.7 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe195-il500,0005109.1 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe195-il1,000,0009139 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe195-il1,000,0005106.1 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
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