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GOE 397 AIRFOIL (goe397-il)

GOE 397 AIRFOIL - Gottingen 397 airfoil


Airfoil goe397-il
Details Dat file Parser  
(goe397-il) GOE 397 AIRFOIL
Gottingen 397 airfoil
Max thickness 5.1% at 30% chord.
Max camber 4% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 397 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0130800
 0.0250000 0.0191600
 0.0500000 0.0273300
 0.0750000 0.0339900
 0.1000000 0.0396500
 0.1500000 0.0489800
 0.2000000 0.0563000
 0.3000000 0.0634500
 0.4000000 0.0646000
 0.5000000 0.0613500
 0.6000000 0.0524000
 0.7000000 0.0415500
 0.8000000 0.0282000
 0.9000000 0.0148500
 0.9500000 0.0076700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0074200
 0.0250000 -.0073400
 0.0500000 -.0051700
 0.0750000 -.0030100
 0.1000000 -.0003500
 0.1500000 0.0044700
 0.2000000 0.0078000
 0.3000000 0.0124500
 0.4000000 0.0146000
 0.5000000 0.0137500
 0.6000000 0.0119000
 0.7000000 0.0085500
 0.8000000 0.0052000
 0.9000000 0.0018500
 0.9500000 0.0001800
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 397 AIRFOIL (goe397-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe397-il50,000942.8 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe397-il50,000543 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe397-il100,000961.4 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe397-il100,000561 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe397-il200,000981.7 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe397-il200,000579.1 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe397-il500,0009110 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe397-il500,0005102.1 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   goe397-il1,000,0009129.9 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe397-il1,000,000597.6 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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