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KC-135 BL351.6 AIRFOIL (kc135d-il)

KC-135 BL351.6 AIRFOIL - Boeing KC-135 transonic airfoils


Airfoil kc135d-il
Details Dat file Parser  
(kc135d-il) KC-135 BL351.6 AIRFOIL
Boeing KC-135 transonic airfoils
Max thickness 9% at 40% chord.
Max camber 1.9% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
KC-135 BL351.6 AIRFOIL
      26.0      26.0
 
 0.0000000 0.0030600
 0.0050000 0.0099700
 0.0075000 0.0119800
 0.0125000 0.0151900
 0.0250000 0.0216000
 0.0500000 0.0313000
 0.0750000 0.0385700
 0.1000000 0.0442300
 0.1500000 0.0521000
 0.2000000 0.0570400
 0.2500000 0.0605000
 0.3000000 0.0628000
 0.3500000 0.0643000
 0.4000000 0.0644900
 0.4500000 0.0637000
 0.5000000 0.0617800
 0.5500000 0.0585000
 0.6000000 0.0541200
 0.6500000 0.0488000
 0.7000000 0.0426700
 0.7500000 0.0360500
 0.8000000 0.0290400
 0.8500000 0.0217800
 0.9000000 0.0145200
 0.9500000 0.0072600
 1.0000000 0.0000000
 
 0.0000000 0.0000000
 0.0050000 -.0046500
 0.0075000 -.0055800
 0.0125000 -.0065700
 0.0250000 -.0075000
 0.0500000 -.0089500
 0.0750000 -.0104100
 0.1000000 -.0118700
 0.1500000 -.0147900
 0.2000000 -.0177000
 0.2500000 -.0205900
 0.3000000 -.0227500
 0.3500000 -.0244500
 0.4000000 -.0254300
 0.4500000 -.0256800
 0.5000000 -.0250100
 0.5500000 -.0233000
 0.6000000 -.0207800
 0.6500000 -.0181800
 0.7000000 -.0155800
 0.7500000 -.0129900
 0.8000000 -.0103900
 0.8500000 -.0077500
 0.9000000 -.0052000
 0.9500000 -.0026000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for KC-135 BL351.6 AIRFOIL (kc135d-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   kc135d-il50,000936.2 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   kc135d-il50,000536.6 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   kc135d-il100,000954.7 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   kc135d-il100,000552.7 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   kc135d-il200,000974.7 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   kc135d-il200,000568.8 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   kc135d-il500,0009100.7 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   kc135d-il500,000584 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   kc135d-il1,000,0009114.9 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   kc135d-il1,000,000586.1 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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