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GOE 570 AIRFOIL (goe570-il)

GOE 570 AIRFOIL - Gottingen 570 airfoil


Airfoil goe570-il
Details Dat file Parser  
(goe570-il) GOE 570 AIRFOIL
Gottingen 570 airfoil
Max thickness 33.7% at 30% chord.
Max camber 9.7% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 570 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0520000
 0.0250000 0.0800000
 0.0500000 0.1210000
 0.0750000 0.1530000
 0.1000000 0.1785000
 0.1500000 0.2140000
 0.2000000 0.2395000
 0.3000000 0.2635000
 0.4000000 0.2625000
 0.5000000 0.2445000
 0.6000000 0.2140000
 0.7000000 0.1720000
 0.8000000 0.1230000
 0.9000000 0.0670000
 0.9500000 0.0375000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0225000
 0.0250000 -.0365000
 0.0500000 -.0490000
 0.0750000 -.0565000
 0.1000000 -.0618000
 0.1500000 -.0695000
 0.2000000 -.0715000
 0.3000000 -.0735000
 0.4000000 -.0690000
 0.5000000 -.0605000
 0.6000000 -.0510000
 0.7000000 -.0415000
 0.8000000 -.0310000
 0.9000000 -.0200000
 0.9500000 -.0109000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 570 AIRFOIL (goe570-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe570-il50,00090.7 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   goe570-il50,00052.5 at α=-14°Mach=0 Ncrit=5Xfoil predictionDetails
   goe570-il100,00097.1 at α=-12.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe570-il100,00056.3 at α=-14.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe570-il200,00097.8 at α=-14.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe570-il200,000510.4 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe570-il500,000923.7 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe570-il500,000515.8 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe570-il1,000,000920.8 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe570-il1,000,000516.4 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
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