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GOE 114 (MVA MK.1) AIRFOIL (goe114-il)

GOE 114 (MVA MK.1) AIRFOIL - Gottingen 114 (MVA MK.1) airfoil


Airfoil goe114-il
Details Dat file Parser  
(goe114-il) GOE 114 (MVA MK.1) AIRFOIL
Gottingen 114 (MVA MK.1) airfoil
Max thickness 9.6% at 29.7% chord.
Max camber 3.5% at 49.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 114 (MVA MK.1) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122500 0.0071300
 0.0245400 0.0130700
 0.0491900 0.0229400
 0.0738600 0.0323100
 0.0986200 0.0391800
 0.1481800 0.0516300
 0.1978200 0.0616800
 0.2973800 0.0741000
 0.3972600 0.0776200
 0.4973600 0.0747600
 0.5976400 0.0670000
 0.6980800 0.0543400
 0.7986600 0.0380900
 0.8993000 0.0199500
 0.9496400 0.0102200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0127100 -.0058500
 0.0253400 -.0097100
 0.0505800 -.0165100
 0.0757500 -.0213300
 0.1008700 -.0247400
 0.1509700 -.0274700
 0.2010000 -.0282000
 0.3007500 -.0211800
 0.4003800 -.0106700
 0.5001600 -.0046400
 0.6000200 -.0006200
 0.6999700 0.0009100
 0.7999500 0.0013400
 0.8999800 0.0006700
 0.9499900 0.0003300
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 114 (MVA MK.1) AIRFOIL (goe114-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe114-il50,000935.4 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe114-il50,000532.4 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe114-il100,000949.7 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe114-il100,000544.4 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe114-il200,000960.9 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe114-il200,000550.8 at α=1.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe114-il500,000993.4 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe114-il500,000574.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe114-il1,000,000970.6 at α=1°Mach=0 Ncrit=9Xfoil predictionDetails
   goe114-il1,000,000567.6 at α=1°Mach=0 Ncrit=5Xfoil predictionDetails
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