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BOEING-VERTOL VR-11X AIRFOIL (vr11x-il)

BOEING-VERTOL VR-11X AIRFOIL - Boeing-Vertol/NASA/Dadone VR-11X transonic rotorcraft airfoil


Airfoil vr11x-il
Details Dat file Parser  
(vr11x-il) BOEING-VERTOL VR-11X AIRFOIL
Boeing-Vertol/NASA/Dadone VR-11X transonic rotorcraft airfoil
Max thickness 11% at 40% chord.
Max camber 2.4% at 25% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 
 BOEING-VERTOL VR-11X AIRFOIL
       34.       34.
 
 0.0       0.0
 0.002     0.0105
 0.005     0.0160
 0.0075    0.0193
 0.0125    0.0242
 0.025     0.0345
 0.050     0.0481
 0.075     0.0573
 0.100     0.0636
 0.150     0.07038
 0.200     0.07453
 0.250     0.07718
 0.300     0.07832
 0.350     0.07890
 0.400     0.07861
 0.450     0.07754
 0.500     0.07575
 0.550     0.07303
 0.600     0.07016
 0.650     0.06615
 0.69      0.06257
 0.73      0.05728
 0.77      0.05004
 0.81      0.04081
 0.845     0.03220
 0.88      0.02477
 0.91      0.01800
 0.935     0.01260
 0.955     0.00820
 0.97      0.00500
 0.98      0.00430
 0.99      0.00366
 0.995     0.00333
 1.000     0.00300
 
 0.0       0.0
 0.002    -0.00450
 0.005    -0.00670
 0.0075   -0.00780
 0.0125   -0.00940
 0.025    -0.01230
 0.050    -0.01600
 0.075    -0.01890
 0.100    -0.02110
 0.150    -0.02450
 0.200    -0.02692
 0.250    -0.02885
 0.300    -0.03000
 0.350    -0.03080
 0.400    -0.03110
 0.450    -0.03100
 0.500    -0.03035
 0.550    -0.02920
 0.600    -0.02770
 0.650    -0.02600
 0.69     -0.02450
 0.73     -0.02280
 0.77     -0.02085
 0.81     -0.01890
 0.845    -0.01690
 0.88     -0.01460
 0.91     -0.01210
 0.935    -0.01000
 0.955    -0.00800
 0.97     -0.00610
 0.98     -0.00460
 0.99     -0.00280
 0.995    -0.00160
 1.000     0.000000
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Lednicer format dat file
Selig format dat file

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Polars for BOEING-VERTOL VR-11X AIRFOIL (vr11x-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   vr11x-il50,000930.5 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   vr11x-il50,000529.4 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   vr11x-il100,000941 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   vr11x-il100,000539.5 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   vr11x-il200,000955.4 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   vr11x-il200,000551.6 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   vr11x-il500,000971.7 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   vr11x-il500,000573.2 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   vr11x-il1,000,000992.3 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   vr11x-il1,000,000589.6 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
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