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KC-135 BL124.32 AIRFOIL (kc135b-il)

KC-135 BL124.32 AIRFOIL - Boeing KC-135 transonic airfoils


Airfoil kc135b-il
Details Dat file Parser  
(kc135b-il) KC-135 BL124.32 AIRFOIL
Boeing KC-135 transonic airfoils
Max thickness 13% at 40% chord.
Max camber 1.4% at 20% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
KC-135 BL124.32 AIRFOIL
      26.0      26.0
 
 0.0000000 0.0053600
 0.0050000 0.0139900
 0.0075000 0.0165400
 0.0125000 0.0206000
 0.0250000 0.0284000
 0.0500000 0.0399800
 0.0750000 0.0485000
 0.1000000 0.0551100
 0.1500000 0.0643600
 0.2000000 0.0707000
 0.2500000 0.0750000
 0.3000000 0.0776000
 0.3500000 0.0792000
 0.4000000 0.0791000
 0.4500000 0.0772500
 0.5000000 0.0738200
 0.5500000 0.0689500
 0.6000000 0.0628400
 0.6500000 0.0557000
 0.7000000 0.0478200
 0.7500000 0.0398500
 0.8000000 0.0318800
 0.8500000 0.0239100
 0.9000000 0.0159400
 0.9500000 0.0079700
 1.0000000 0.0000000
 
 0.0000000 0.0000000
 0.0050000 -.0073300
 0.0075000 -.0089500
 0.0125000 -.0112300
 0.0250000 -.0147500
 0.0500000 -.0191500
 0.0750000 -.0229000
 0.1000000 -.0264600
 0.1500000 -.0331800
 0.2000000 -.0392500
 0.2500000 -.0440100
 0.3000000 -.0474600
 0.3500000 -.0498000
 0.4000000 -.0507000
 0.4500000 -.0500700
 0.5000000 -.0479300
 0.5500000 -.0444800
 0.6000000 -.0399500
 0.6500000 -.0349600
 0.7000000 -.0299600
 0.7500000 -.0249700
 0.8000000 -.0199800
 0.8500000 -.0149800
 0.9000000 -.0099900
 0.9500000 -.0049900
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for KC-135 BL124.32 AIRFOIL (kc135b-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   kc135b-il50,000931.1 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   kc135b-il50,000531.8 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   kc135b-il100,000950.3 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   kc135b-il100,000549.3 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   kc135b-il200,000970.7 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   kc135b-il200,000562.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   kc135b-il500,000989.2 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   kc135b-il500,000571.2 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   kc135b-il1,000,000998.2 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   kc135b-il1,000,000579.8 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
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