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GOE 234 (MVA CA5) AIRFOIL (goe234-il)

GOE 234 (MVA CA5) AIRFOIL - Gottingen 234 (MVA CA5) airfoil


Airfoil goe234-il
Details Dat file Parser  
(goe234-il) GOE 234 (MVA CA5) AIRFOIL
Gottingen 234 (MVA CA5) airfoil
Max thickness 14.2% at 19.7% chord.
Max camber 9.2% at 49.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 234 (MVA CA5) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0117500 0.0292000
 0.0239500 0.0407200
 0.0484400 0.0606400
 0.0730500 0.0759800
 0.0977300 0.0884100
 0.1472200 0.1080800
 0.1969100 0.1200600
 0.2965700 0.1333200
 0.3964900 0.1365900
 0.4966500 0.1303600
 0.5970100 0.1164400
 0.6975300 0.0962300
 0.7982200 0.0692100
 0.8990100 0.0386000
 0.9494700 0.0207000
 1.0000000 0.0037000

 0.0000000 0.0000000
 0.0128500 -.0135700
 0.0254600 -.0180500
 0.0505600 -.0217000
 0.0756100 -.0237600
 0.1006700 -.0260100
 0.1506600 -.0255300
 0.2005700 -.0221500
 0.3000200 -.0008900
 0.3992000 0.0311600
 0.4986300 0.0532100
 0.5984200 0.0613800
 0.6985600 0.0560500
 0.7988500 0.0446300
 0.8994300 0.0220200
 0.9497700 0.0089100
 1.0000000 -.0037000
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Lednicer format dat file
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Polars for GOE 234 (MVA CA5) AIRFOIL (goe234-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe234-il50,000910.9 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe234-il50,000527.7 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe234-il100,000954.7 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe234-il100,000556.6 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe234-il200,000977 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe234-il200,000579.4 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe234-il500,0009110.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe234-il500,0005108.4 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe234-il1,000,0009137.7 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe234-il1,000,0005127.1 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
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