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BOEING VERTOL V43015-2.48 AIRFOIL (v43015-il)

BOEING VERTOL V43015-2.48 AIRFOIL - Boeing-Vertol V43015-2.48 rotorcraft airfoil


Airfoil v43015-il
Details Dat file Parser  
(v43015-il) BOEING VERTOL V43015-2.48 AIRFOIL
Boeing-Vertol V43015-2.48 rotorcraft airfoil
Max thickness 15% at 30% chord.
Max camber 3.7% at 15% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
  BOEING VERTOL V43015-2.48 AIRFOIL
       21.       21.
 
 0.0000000 0.0000000
 0.0100000 0.0412000
 0.0200000 0.0522000
 0.0300000 0.0608000
 0.0400000 0.0680000
 0.0500000 0.0741000
 0.0750000 0.0861000
 0.1000000 0.0941000
 0.1250000 0.0998000
 0.1500000 0.1036000
 0.2000000 0.1071000
 0.2500000 0.1078000
 0.3000000 0.1062000
 0.4000000 0.0991000
 0.5000000 0.0885000
 0.6000000 0.0750000
 0.7000000 0.0593000
 0.8000000 0.0416000
 0.9000000 0.0217000
 0.9500000 0.0109000
 1.0000000 0.0000000
 
 0.0000000 0.0000000
 0.0100000 -.0096000
 0.0200000 -.0130000
 0.0300000 -.0150000
 0.0400000 -.0166000
 0.0500000 -.0179000
 0.0750000 -.0202000
 0.1000000 -.0230000
 0.1250000 -.0265000
 0.1500000 -.0300000
 0.2000000 -.0365000
 0.2500000 -.0412000
 0.3000000 -.0441000
 0.4000000 -.0460000
 0.5000000 -.0440000
 0.6000000 -.0392000
 0.7000000 -.0320000
 0.8000000 -.0233000
 0.9000000 -.0130000
 0.9500000 -.0068000
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for BOEING VERTOL V43015-2.48 AIRFOIL (v43015-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   v43015-il50,000923.5 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   v43015-il50,000527.1 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   v43015-il100,000936.3 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   v43015-il100,000539.8 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   v43015-il200,000951.4 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   v43015-il200,000553.5 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   v43015-il500,000974.6 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   v43015-il500,000576.7 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   v43015-il1,000,000998.2 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   v43015-il1,000,000595 at α=9.5°Mach=0 Ncrit=5Xfoil predictionDetails
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