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RAF-48 AIRFOIL (raf48-il)

RAF-48 AIRFOIL - RAF-48 airfoil


Airfoil raf48-il
Details Dat file Parser  
(raf48-il) RAF-48 AIRFOIL
RAF-48 airfoil
Max thickness 15% at 30% chord.
Max camber 2.9% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
RAF-48 AIRFOIL
       17.       17.

  0.000000  0.000000
  0.012500  0.026000
  0.025000  0.036500
  0.050000  0.052000
  0.075000  0.063900
  0.100000  0.073000
  0.150000  0.086300
  0.200000  0.095300
  0.300000  0.104000
  0.400000  0.102000
  0.500000  0.093800
  0.600000  0.079400
  0.700000  0.060500
  0.800000  0.040200
  0.900000  0.019500
  0.950000  0.010050
  1.000000  0.000000

  0.000000  0.000000
  0.012500 -0.016500
  0.025000 -0.023400
  0.050000 -0.031600
  0.075000 -0.036900
  0.100000 -0.040300
  0.150000 -0.044100
  0.200000 -0.045800
  0.300000 -0.045600
  0.400000 -0.043300
  0.500000 -0.039000
  0.600000 -0.033600
  0.700000 -0.026500
  0.800000 -0.018300
  0.900000 -0.010000
  0.950000 -0.006400
  1.000000  0.000000
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Lednicer format dat file
Selig format dat file

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Polars for RAF-48 AIRFOIL (raf48-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   raf48-il50,00097.4 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   raf48-il50,000525.8 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   raf48-il100,000945.6 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   raf48-il100,000549.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   raf48-il200,000968.5 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   raf48-il200,000567.8 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   raf48-il500,000997.8 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   raf48-il500,000593.7 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   raf48-il1,000,0009121.8 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   raf48-il1,000,0005108.1 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
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