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GOE 180 (MVA H.26) AIRFOIL (goe180-il)

GOE 180 (MVA H.26) AIRFOIL - Gottingen 180 (MVA H.26) airfoil


Airfoil goe180-il
Details Dat file Parser  
(goe180-il) GOE 180 (MVA H.26) AIRFOIL
Gottingen 180 (MVA H.26) airfoil
Max thickness 8.7% at 30% chord.
Max camber 4.4% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 180 (MVA H.26) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0199600
 0.0250000 0.0293200
 0.0500000 0.0436500
 0.0750000 0.0544800
 0.1000000 0.0620000
 0.1500000 0.0734500
 0.2000000 0.0801000
 0.3000000 0.0874000
 0.4000000 0.0852000
 0.5000000 0.0778000
 0.6000000 0.0681000
 0.7000000 0.0561000
 0.8000000 0.0412000
 0.9000000 0.0237000
 0.9500000 0.0146500
 1.0000000 0.0025000

 0.0000000 0.0000000
 0.0125000 -.0098400
 0.0250000 -.0112800
 0.0500000 -.0123500
 0.0750000 -.0115300
 0.1000000 -.0102000
 0.1500000 -.0073500
 0.2000000 -.0044000
 0.3000000 0.0007000
 0.4000000 0.0037000
 0.5000000 0.0050000
 0.6000000 0.0058000
 0.7000000 0.0054000
 0.8000000 0.0044000
 0.9000000 0.0029000
 0.9500000 0.0013500
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for GOE 180 (MVA H.26) AIRFOIL (goe180-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe180-il50,000933.2 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   goe180-il50,000540.6 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe180-il100,000955.3 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe180-il100,000559.5 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe180-il200,000978.2 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe180-il200,000577.8 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe180-il500,0009107.4 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe180-il500,000599.2 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe180-il1,000,0009126.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe180-il1,000,0005112 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
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