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GOE 121 (MVA H.1) AIRFOIL (goe121-il)

GOE 121 (MVA H.1) AIRFOIL - Gottingen 121 (MVA H.1) airfoil


Airfoil goe121-il
Details Dat file Parser  
(goe121-il) GOE 121 (MVA H.1) AIRFOIL
Gottingen 121 (MVA H.1) airfoil
Max thickness 6.7% at 19.9% chord.
Max camber 4.6% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 121 (MVA H.1) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122800 0.0153700
 0.0246700 0.0230500
 0.0494900 0.0359000
 0.0743700 0.0443600
 0.0992500 0.0529100
 0.1491100 0.0628200
 0.1990100 0.0700300
 0.2989300 0.0752400
 0.3989400 0.0744600
 0.4990100 0.0693900
 0.5991200 0.0621100
 0.6993000 0.0498300
 0.7994900 0.0362500
 0.8997200 0.0197800
 0.9498300 0.0118900
 1.0000000 0.0010000

 0.0000000 0.0000000
 0.0126700 -.0123200
 0.0251900 -.0142400
 0.0502100 -.0144900
 0.0751800 -.0125300
 0.1001200 -.0083800
 0.1500300 -.0022700
 0.1999500 0.0036400
 0.2998000 0.0139600
 0.3997500 0.0175800
 0.4997500 0.0179000
 0.5997900 0.0150200
 0.6998300 0.0120400
 0.7998700 0.0091600
 0.8999299 0.0051800
 0.9499500 0.0022800
 1.0000000 -.0010000
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Polars for GOE 121 (MVA H.1) AIRFOIL (goe121-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe121-il50,000940.6 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe121-il50,000543.4 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe121-il100,000960.9 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe121-il100,000559.9 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe121-il200,000979.7 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe121-il200,000574.9 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe121-il500,000999.1 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe121-il500,000587 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe121-il1,000,0009104.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe121-il1,000,000597.7 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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