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KC-135 BL200.76 AIRFOIL (kc135c-il)

KC-135 BL200.76 AIRFOIL - Boeing KC-135 transonic airfoils


Airfoil kc135c-il
Details Dat file Parser  
(kc135c-il) KC-135 BL200.76 AIRFOIL
Boeing KC-135 transonic airfoils
Max thickness 10.6% at 40% chord.
Max camber 1.5% at 25% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
KC-135 BL200.76 AIRFOIL
      26.0      26.0
 
 0.0000000 0.0037400
 0.0050000 0.0112300
 0.0075000 0.0134000
 0.0125000 0.0168700
 0.0250000 0.0235000
 0.0500000 0.0336000
 0.0750000 0.0411400
 0.1000000 0.0469900
 0.1500000 0.0553000
 0.2000000 0.0604700
 0.2500000 0.0642200
 0.3000000 0.0666600
 0.3500000 0.0680500
 0.4000000 0.0682900
 0.4500000 0.0673600
 0.5000000 0.0650900
 0.5500000 0.0613600
 0.6000000 0.0564300
 0.6500000 0.0504900
 0.7000000 0.0438000
 0.7500000 0.0368700
 0.8000000 0.0292900
 0.8500000 0.0219700
 0.9000000 0.0146500
 0.9500000 0.0073200
 1.0000000 0.0000000
 
 0.0000000 0.0000000
 0.0050000 -.0057000
 0.0075000 -.0068400
 0.0125000 -.0083700
 0.0250000 -.0105300
 0.0500000 -.0130700
 0.0750000 -.0154400
 0.1000000 -.0178700
 0.1500000 -.0226500
 0.2000000 -.0273100
 0.2500000 -.0311800
 0.3000000 -.0342500
 0.3500000 -.0364200
 0.4000000 -.0376300
 0.4500000 -.0378200
 0.5000000 -.0369600
 0.5500000 -.0348700
 0.6000000 -.0317400
 0.6500000 -.0278700
 0.7000000 -.0238900
 0.7500000 -.0199100
 0.8000000 -.0159300
 0.8500000 -.0119400
 0.9000000 -.0079600
 0.9500000 -.0039800
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for KC-135 BL200.76 AIRFOIL (kc135c-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   kc135c-il50,000934.1 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   kc135c-il50,000534.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   kc135c-il100,000952 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   kc135c-il100,000550.2 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   kc135c-il200,000971.4 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   kc135c-il200,000566 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   kc135c-il500,000991.7 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   kc135c-il500,000573.1 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   kc135c-il1,000,0009100.6 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   kc135c-il1,000,000578.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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