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BOEING-VERTOL VR-15 AIRFOIL (vr15-il)

BOEING-VERTOL VR-15 AIRFOIL - Boeing-Vertol/Dadone VR-15 transonic rotorcraft airfoil


Airfoil vr15-il
Details Dat file Parser  
(vr15-il) BOEING-VERTOL VR-15 AIRFOIL
Boeing-Vertol/Dadone VR-15 transonic rotorcraft airfoil
Max thickness 8% at 35% chord.
Max camber 1.3% at 20% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 BOEING-VERTOL VR-15 AIRFOIL
       43.       41.
 
0.00000   0.0000000
0.00012   0.0016640
0.00080   0.0042970
0.00195   0.0067080
0.00340   0.0088580
0.00520   0.0109540
0.00700   0.0127100
0.00900   0.0144110
0.01105   0.0159670
0.01415   0.0180710
0.01860   0.0207170
0.02450   0.0237770
0.03205   0.0271490
0.04160   0.0306390
0.05350   0.0344130
0.06850   0.0382900
0.08800   0.0419600
0.11400   0.0454220
0.15000   0.0484690
0.20000   0.0506840
0.25000   0.0516540
0.30000   0.0520000
0.35000   0.0518270
0.40000   0.0511000
0.45000   0.0496800
0.50000   0.0478460
0.55000   0.0452490
0.60000   0.0420060
0.65000   0.0379090
0.69000   0.0341520
0.73000   0.0299980
0.77000   0.0256910
0.81000   0.0213010
0.84500   0.0171870
0.88000   0.0129840
0.91000   0.0094280
0.93500   0.0064640
0.95500   0.0042730
0.97000   0.0029320
0.98000   0.0021630
0.99000   0.0014970
0.99500   0.0011990
1.00000   0.0010390
 
0.00000   0.0000000
0.00055   -.0022510
0.00200   -.0042320
0.00400   -.0060770
0.00620   -.0075630
0.00860   -.0088500
0.01100   -.0098590
0.01465   -.0110740
0.01955   -.0121540
0.02615   -.0133250
0.03430   -.0144500
0.04449   -.0156660
0.05690   -.0170160
0.07245   -.0184570
0.09240   -.0198970
0.11850   -.0214730
0.15000   -.0230030
0.20000   -.0248490
0.25000   -.0261990
0.30000   -.0271000
0.35000   -.0277300
0.40000   -.0280000
0.45000   -.0279100
0.50000   -.0275950
0.55000   -.0270100
0.60000   -.0261690
0.65000   -.0249840
0.69000   -.0237890
0.73000   -.0223500
0.77000   -.0206210
0.81000   -.0186480
0.84500   -.0166750
0.88000   -.0144520
0.91000   -.0119890
0.93500   -.0097550
0.95500   -.0078970
0.97000   -.0061080
0.98000   -.0047030
0.99000   -.0032080
0.99500   -.0022790
1.00000   -.0013500
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Lednicer format dat file
Selig format dat file

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Polars for BOEING-VERTOL VR-15 AIRFOIL (vr15-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   vr15-il50,000928.1 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   vr15-il50,000527.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   vr15-il100,000938.2 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   vr15-il100,000539 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   vr15-il200,000949.3 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   vr15-il200,000552 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   vr15-il500,000970.9 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   vr15-il500,000569.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   vr15-il1,000,000985.6 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   vr15-il1,000,000581.7 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
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