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GOE 134 (MVA H.12) AIRFOIL (goe134-il)

GOE 134 (MVA H.12) AIRFOIL - Gottingen 134 (MVA H.12) airfoil


Airfoil goe134-il
Details Dat file Parser  
(goe134-il) GOE 134 (MVA H.12) AIRFOIL
Gottingen 134 (MVA H.12) airfoil
Max thickness 9.5% at 30% chord.
Max camber 4% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 134 (MVA H.12) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0207100
 0.0250000 0.0311200
 0.0500000 0.0450400
 0.0750000 0.0552700
 0.1000000 0.0632900
 0.1500000 0.0754300
 0.2000000 0.0826800
 0.3000000 0.0882700
 0.4000000 0.0868600
 0.5000000 0.0805500
 0.6000000 0.0707400
 0.7000000 0.0583300
 0.8000000 0.0452200
 0.9000000 0.0286100
 0.9500000 0.0190600
 1.0000000 0.0090000

 0.0000000 0.0000000
 0.0125000 -.0087900
 0.0250000 -.0086800
 0.0500000 -.0084500
 0.0750000 -.0082300
 0.1000000 -.0080100
 0.1500000 -.0075700
 0.2000000 -.0071200
 0.3000000 -.0062300
 0.4000000 -.0053400
 0.5000000 -.0044500
 0.6000000 -.0035600
 0.7000000 -.0026700
 0.8000000 -.0017800
 0.9000000 -.0008900
 0.9500000 -.0004500
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for GOE 134 (MVA H.12) AIRFOIL (goe134-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe134-il50,000929.4 at α=11°Mach=0 Ncrit=9Xfoil predictionDetails
   goe134-il50,000538.3 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe134-il100,000950.7 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe134-il100,000555.2 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe134-il200,000970.4 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe134-il200,000571.7 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe134-il500,000996.1 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe134-il500,000593.7 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe134-il1,000,0009114.7 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe134-il1,000,0005109.7 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
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