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GOE 290 (MVA 290) AIRFOIL (goe290-il)

GOE 290 (MVA 290) AIRFOIL - Gottingen 290 (MVA 290) airfoil


Airfoil goe290-il
Details Dat file Parser  
(goe290-il) GOE 290 (MVA 290) AIRFOIL
Gottingen 290 (MVA 290) airfoil
Max thickness 17.6% at 29.1% chord.
Max camber 3.9% at 39.2% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 290 (MVA 290) AIRFOIL
       17.       17.

 0.0000100 0.0000000
 0.0105800 0.0281200
 0.0223400 0.0390300
 0.0460000 0.0585500
 0.0699500 0.0738800
 0.0941900 0.0850400
 0.1429000 0.1038700
 0.1921800 0.1143400
 0.2914700 0.1247400
 0.3916500 0.1220900
 0.4925700 0.1086900
 0.5937200 0.0918100
 0.6950400 0.0725400
 0.7965100 0.0509800
 0.8980400 0.0287300
 0.9489400 0.0155100
 1.0000000 0.0030000

 0.0000100 0.0000000
 0.0140700 -.0228400
 0.0270700 -.0302500
 0.0526000 -.0380000
 0.0779000 -.0422700
 0.1031400 -.0458500
 0.1534400 -.0502000
 0.2036200 -.0528700
 0.3034700 -.0506400
 0.4030000 -.0438300
 0.5025400 -.0370300
 0.6020700 -.0302200
 0.7016000 -.0234100
 0.8011400 -.0166000
 0.9006700 -.0097900
 0.9504400 -.0063900
 1.0000000 -.0030000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 290 (MVA 290) AIRFOIL (goe290-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe290-il50,00096.6 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe290-il50,000522.4 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe290-il100,000941.7 at α=10.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe290-il100,000546.8 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe290-il200,000969 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe290-il200,000567 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe290-il500,000996.5 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe290-il500,000584 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe290-il1,000,0009112.3 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe290-il1,000,000592.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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