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KC-135 BL52.44 AIRFOIL (kc135a-il)

KC-135 BL52.44 AIRFOIL - Boeing KC-135 transonic airfoils


Airfoil kc135a-il
Details Dat file Parser  
(kc135a-il) KC-135 BL52.44 AIRFOIL
Boeing KC-135 transonic airfoils
Max thickness 15.5% at 35% chord.
Max camber 1.3% at 20% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
KC-135 BL52.44 AIRFOIL
      26.0      26.0

 0.0000000 0.0074000
 0.0050000 0.0175000
 0.0075000 0.0205500
 0.0125000 0.0253900
 0.0250000 0.0347000
 0.0500000 0.0483000
 0.0750000 0.0581300
 0.1000000 0.0657200
 0.1500000 0.0766100
 0.2000000 0.0838000
 0.2500000 0.0886000
 0.3000000 0.0913700
 0.3500000 0.0921800
 0.4000000 0.0910500
 0.4500000 0.0876600
 0.5000000 0.0825800
 0.5500000 0.0762000
 0.6000000 0.0687000
 0.6500000 0.0602900
 0.7000000 0.0516800
 0.7500000 0.0430000
 0.8000000 0.0344500
 0.8500000 0.0258400
 0.9000000 0.0172300
 0.9500000 0.0086100
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0050000 -.0087200
 0.0075000 -.0107600
 0.0125000 -.0139000
 0.0250000 -.0191500
 0.0500000 -.0261300
 0.0750000 -.0317800
 0.1000000 -.0366500
 0.1500000 -.0451000
 0.2000000 -.0522800
 0.2500000 -.0575700
 0.3000000 -.0610400
 0.3500000 -.0627500
 0.4000000 -.0625000
 0.4500000 -.0604400
 0.5000000 -.0567800
 0.5500000 -.0518500
 0.6000000 -.0461800
 0.6500000 -.0404100
 0.7000000 -.0346400
 0.7500000 -.0288600
 0.8000000 -.0230900
 0.8500000 -.0173200
 0.9000000 -.0115500
 0.9500000 -.0057700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for KC-135 BL52.44 AIRFOIL (kc135a-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   kc135a-il50,000924.9 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   kc135a-il50,000527.7 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   kc135a-il100,000947.3 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   kc135a-il100,000547.5 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   kc135a-il200,000968.9 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   kc135a-il200,000562.1 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   kc135a-il500,000988.7 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   kc135a-il500,000573.2 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   kc135a-il1,000,000997.8 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   kc135a-il1,000,000582.5 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
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