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GOE 198 (L.F.G. 5294) AIRFOIL (goe198-il)

GOE 198 (L.F.G. 5294) AIRFOIL - Gottingen 198 (L.F.G. 5294) airfoil


Airfoil goe198-il
Details Dat file Parser  
(goe198-il) GOE 198 (L.F.G. 5294) AIRFOIL
Gottingen 198 (L.F.G. 5294) airfoil
Max thickness 7.8% at 19.9% chord.
Max camber 6.5% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 198 (L.F.G. 5294) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122900 0.0223200
 0.0246900 0.0329300
 0.0495700 0.0458700
 0.0744500 0.0582000
 0.0993600 0.0682400
 0.1492200 0.0827100
 0.1991200 0.0926800
 0.2990500 0.1010300
 0.3990300 0.1028700
 0.4990800 0.0970200
 0.5991700 0.0874600
 0.6993100 0.0726100
 0.7995099 0.0518600
 0.8997400 0.0275000
 0.9498500 0.0163800
 1.0000000 0.0042500

 0.0000000 0.0000000
 0.0126300 -.0135800
 0.0251300 -.0134600
 0.0500900 -.0095300
 0.0750300 -.0034900
 0.0999900 0.0012400
 0.1499200 0.0088200
 0.1998600 0.0150900
 0.2997700 0.0245300
 0.3997400 0.0275800
 0.4997400 0.0274200
 0.5997800 0.0236700
 0.6998300 0.0179100
 0.7999000 0.0107600
 0.8999600 0.0038000
 0.9500000 0.0002800
 1.0000000 -.0042500
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Lednicer format dat file
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Polars for GOE 198 (L.F.G. 5294) AIRFOIL (goe198-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe198-il50,000936.2 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe198-il50,000543.2 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe198-il100,000964.5 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe198-il100,000564 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe198-il200,000988.3 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe198-il200,000580.4 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe198-il500,0009112.3 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe198-il500,000592.9 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe198-il1,000,0009117 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe198-il1,000,000592.9 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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