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PROPFAN CRUISE MISSILE WING AIRFOIL (pfcm-il)

PROPFAN CRUISE MISSILE WING AIRFOIL - Propfan Cruise Missile wing airfoil


Airfoil pfcm-il
Details Dat file Parser  
(pfcm-il) PROPFAN CRUISE MISSILE WING AIRFOIL
Propfan Cruise Missile wing airfoil
Max thickness 8.2% at 40% chord.
Max camber 1.3% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
PROPFAN CRUISE MISSILE WING AIRFOIL
       26.       26.

  0.000000  0.000000
  0.005000  0.007560
  0.007500  0.009110
  0.012500  0.011580
  0.025000  0.016230
  0.050000  0.022900
  0.075000  0.028040
  0.100000  0.032340
  0.150000  0.039180
  0.200000  0.044410
  0.250000  0.048330
  0.300000  0.051170
  0.350000  0.052990
  0.400000  0.053750
  0.450000  0.053270
  0.500000  0.051710
  0.550000  0.049250
  0.600000  0.046000
  0.650000  0.042070
  0.700000  0.037510
  0.750000  0.032440
  0.800000  0.026940
  0.850000  0.020750
  0.900000  0.014370
  0.950000  0.007840
  1.000000  0.001310

  0.000000  0.000000
  0.005000 -0.005700
  0.007500 -0.006840
  0.012500 -0.008570
  0.025000 -0.011520
  0.050000 -0.015320
  0.075000 -0.018010
  0.100000 -0.020160
  0.150000 -0.023390
  0.200000 -0.025680
  0.250000 -0.027230
  0.300000 -0.028160
  0.350000 -0.028490
  0.400000 -0.028180
  0.450000 -0.026990
  0.500000 -0.025110
  0.550000 -0.022710
  0.600000 -0.019940
  0.650000 -0.016920
  0.700000 -0.013780
  0.750000 -0.010750
  0.800000 -0.008140
  0.850000 -0.006220
  0.900000 -0.004480
  0.950000 -0.002890
  1.000000 -0.001300
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Lednicer format dat file
Selig format dat file

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Polars for PROPFAN CRUISE MISSILE WING AIRFOIL (pfcm-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   pfcm-il50,000930.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   pfcm-il50,000533 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   pfcm-il100,000947 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   pfcm-il100,000544.9 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   pfcm-il200,000961.6 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   pfcm-il200,000556.3 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   pfcm-il500,000567.3 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   pfcm-il500,000078.7 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   pfcm-il1,000,000988.4 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   pfcm-il1,000,000570.9 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
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