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GOE 242 (MVA PR.2) AIRFOIL (goe242-il)

GOE 242 (MVA PR.2) AIRFOIL - Gottingen 242 (MVA PR.2) airfoil


Airfoil goe242-il
Details Dat file Parser  
(goe242-il) GOE 242 (MVA PR.2) AIRFOIL
Gottingen 242 (MVA PR.2) airfoil
Max thickness 16.2% at 29.6% chord.
Max camber 7.5% at 49.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 242 (MVA PR.2) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0117900 0.0278000
 0.0239000 0.0431100
 0.0483700 0.0637300
 0.0729600 0.0800600
 0.0975800 0.0949900
 0.1470200 0.1167500
 0.1966800 0.1300200
 0.2963300 0.1440600
 0.3962600 0.1466000
 0.4965300 0.1359600
 0.5970000 0.1177200
 0.6975700 0.0952900
 0.7983000 0.0668600
 0.8991001 0.0354300
 0.9495201 0.0190100
 1.0000000 0.0020000

 0.0000000 0.0000000
 0.0127600 -.0101700
 0.0253300 -.0128500
 0.0504300 -.0167100
 0.0755000 -.0195700
 0.1005500 -.0214400
 0.1506000 -.0236600
 0.2005700 -.0223900
 0.3004500 -.0175400
 0.4001100 -.0043000
 0.4996200 0.0147400
 0.5992000 0.0314800
 0.6989700 0.0403200
 0.7990300 0.0378800
 0.8994200 0.0229400
 0.9497000 0.0117200
 1.0000000 -.0020000
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Lednicer format dat file
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Polars for GOE 242 (MVA PR.2) AIRFOIL (goe242-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe242-il50,00096 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe242-il50,000520.9 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe242-il100,000946.8 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe242-il100,000554.4 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe242-il200,000978.6 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe242-il200,000580.8 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe242-il500,0009116.8 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe242-il500,0005114.6 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe242-il1,000,0009146.4 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe242-il1,000,0005137.9 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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