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GOE 217 (MVA MK.12) AIRFOIL (goe217-il)

GOE 217 (MVA MK.12) AIRFOIL - Gottingen 217 (MVA MK.12) airfoil


Airfoil goe217-il
Details Dat file Parser  
(goe217-il) GOE 217 (MVA MK.12) AIRFOIL
Gottingen 217 (MVA MK.12) airfoil
Max thickness 19% at 29.2% chord.
Max camber 6.3% at 59.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 217 (MVA MK.12) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0100400 0.0440600
 0.0215600 0.0617000
 0.0453700 0.0830300
 0.0694600 0.0993800
 0.0937800 0.1115300
 0.1428600 0.1279700
 0.1922600 0.1387300
 0.2916700 0.1492700
 0.3919300 0.1446700
 0.4927200 0.1304900
 0.5938000 0.1111300
 0.6950901 0.0879900
 0.7965200 0.0624500
 0.8980700 0.0346100
 0.9488600 0.0204500
 1.0000000 0.0037000

 0.0000000 0.0000000
 0.0136000 -.0197400
 0.0263600 -.0243300
 0.0517400 -.0311100
 0.0770700 -.0370000
 0.1023500 -.0419900
 0.1526600 -.0476800
 0.2026500 -.0474900
 0.3022200 -.0398400
 0.4013700 -.0246000
 0.5002200 -.0038900
 0.5990800 0.0164300
 0.6983000 0.0304700
 0.7984900 0.0270600
 0.8992600 0.0131800
 0.9497400 0.0047000
 1.0000000 -.0037000
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Polars for GOE 217 (MVA MK.12) AIRFOIL (goe217-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe217-il50,00095 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe217-il50,000521.1 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe217-il100,000940.2 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe217-il100,000548.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe217-il200,000967 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe217-il200,000570.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe217-il500,0009101.7 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe217-il500,000599.6 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe217-il1,000,0009127.5 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe217-il1,000,0005119.1 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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