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WORTMANN FX 049-915 AIRFOIL (fx049915-il)

WORTMANN FX 049-915 AIRFOIL - Wortmann FX 049-915 airfoil


Airfoil fx049915-il
Details Dat file Parser  
(fx049915-il) WORTMANN FX 049-915 AIRFOIL
Wortmann FX 049-915 airfoil
Max thickness 14.7% at 37.1% chord.
Max camber 5.8% at 37.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
WORTMANN FX 049-915 AIRFOIL
       13.       13.

  0.000000  0.000000
  0.017040  0.031870
  0.066990  0.068620
  0.146450  0.102880
  0.250000  0.127320
  0.370590  0.131780
  0.500000  0.105870
  0.629410  0.075190
  0.750000  0.048700
  0.853560  0.027510
  0.933020  0.014010
  0.982970  0.004690
  1.000000  0.000000

  0.000000  0.000000
  0.017040 -0.010550
  0.066990 -0.014360
  0.146450 -0.015300
  0.250000 -0.015900
  0.370590 -0.015400
  0.500000 -0.014190
  0.629410 -0.012010
  0.750000 -0.009420
  0.853560 -0.007010
  0.933020 -0.004270
  0.982970 -0.001930
  1.000000  0.000000
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Polars for WORTMANN FX 049-915 AIRFOIL (fx049915-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx049915-il50,00094.9 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx049915-il50,000510.4 at α=0.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx049915-il100,00096.2 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx049915-il100,000524.1 at α=1.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx049915-il200,000925.4 at α=1.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx049915-il200,000549.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx049915-il500,0009113.5 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx049915-il500,0005114.6 at α=9.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx049915-il1,000,0009155 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx049915-il1,000,0005152.6 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
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