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GOE 797 AIRFOIL (goe797-il)

GOE 797 AIRFOIL - Gottingen 797 airfoil


Airfoil goe797-il
Details Dat file Parser  
(goe797-il) GOE 797 AIRFOIL
Gottingen 797 airfoil
Max thickness 16% at 30% chord.
Max camber 4.9% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 797 AIRFOIL
       14.       14.

 0.0000000 0.0000000
 0.0125000 0.0276000
 0.0250000 0.0412000
 0.0500000 0.0604000
 0.1500000 0.1022000
 0.2000000 0.1146000
 0.3000000 0.1264000
 0.4000000 0.1292000
 0.5000000 0.1240000
 0.6000000 0.1104000
 0.7000000 0.0906000
 0.8000000 0.0674000
 0.9000000 0.0392000
 1.0000000 0.0080000

 0.0000000 0.0000000
 0.0125000 -.0214000
 0.0250000 -.0288000
 0.0500000 -.0360000
 0.1500000 -.0400000
 0.2000000 -.0384000
 0.3000000 -.0336000
 0.4000000 -.0288000
 0.5000000 -.0240000
 0.6000000 -.0192000
 0.7000000 -.0144000
 0.8000000 -.0096000
 0.9000000 -.0048000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 797 AIRFOIL (goe797-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe797-il50,00097.3 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe797-il50,000520.9 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe797-il100,000948.9 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe797-il100,000550.3 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe797-il200,000976 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe797-il200,000573.3 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe797-il500,0009108.2 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe797-il500,000596.7 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe797-il1,000,0009128.7 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe797-il1,000,0005106.6 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
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