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GOE 182 (MVA H.27) AIRFOIL (goe182-il)

GOE 182 (MVA H.27) AIRFOIL - Gottingen 182 (MVA H.27) airfoil


Airfoil goe182-il
Details Dat file Parser  
(goe182-il) GOE 182 (MVA H.27) AIRFOIL
Gottingen 182 (MVA H.27) airfoil
Max thickness 9.5% at 19.9% chord.
Max camber 5.3% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 182 (MVA H.27) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0121800 0.0223700
 0.0245400 0.0325500
 0.0493200 0.0479000
 0.0741300 0.0610600
 0.0989900 0.0708100
 0.1487700 0.0865200
 0.1986700 0.0933300
 0.2986400 0.0953600
 0.3987100 0.0906800
 0.4988500 0.0810100
 0.5990200 0.0685400
 0.6992400 0.0532600
 0.7994600 0.0380900
 0.8997100 0.0206200
 0.9498500 0.0105400
 1.0000000 0.0007500

 0.0000000 0.0000000
 0.0126600 -.0115200
 0.0252000 -.0140400
 0.0502000 -.0142800
 0.0751800 -.0126300
 0.1001600 -.0113700
 0.1500900 -.0061600
 0.2000200 -.0010500
 0.2998800 0.0081700
 0.3997900 0.0146000
 0.4997200 0.0193200
 0.5997200 0.0196500
 0.6997600 0.0166700
 0.7998500 0.0108000
 0.8999400 0.0045200
 0.9499800 0.0013400
 1.0000000 -.0007500
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Polars for GOE 182 (MVA H.27) AIRFOIL (goe182-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe182-il50,000929.2 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe182-il50,000536.5 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe182-il100,000948.6 at α=11°Mach=0 Ncrit=9Xfoil predictionDetails
   goe182-il100,000551.5 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe182-il200,000968.6 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe182-il200,000569.4 at α=9.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe182-il500,000998 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe182-il500,000597.9 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe182-il1,000,0009122.5 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe182-il1,000,0005119.8 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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