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BOEING-VERTOL VR-14 AIRFOIL (vr14-il)

BOEING-VERTOL VR-14 AIRFOIL - Boeing-Vertol/Dadone VR-14 rotorcraft airfoil


Airfoil vr14-il
Details Dat file Parser  
(vr14-il) BOEING-VERTOL VR-14 AIRFOIL
Boeing-Vertol/Dadone VR-14 rotorcraft airfoil
Max thickness 8% at 35% chord.
Max camber 1.7% at 20% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 BOEING-VERTOL VR-14 AIRFOIL
       43.       41.
 
0.00000   0.0000000
0.00012   0.0018100
0.00080   0.0046750
0.00195   0.0072980
0.00340   0.0096370
0.00520   0.0119170
0.00700   0.0138270
0.00900   0.0156780
0.01105   0.0173710
0.01415   0.0196600
0.01860   0.0225390
0.02450   0.0258680
0.03205   0.0295370
0.04160   0.0333330
0.05350   0.0374390
0.06850   0.0416570
0.08800   0.0456500
0.11400   0.0494160
0.15000   0.0527310
0.20000   0.0551410
0.25000   0.0561960
0.30000   0.0565730
0.35000   0.0563840
0.40000   0.0555930
0.45000   0.0540490
0.50000   0.0520530
0.55000   0.0492280
0.60000   0.0456990
0.65000   0.0412430
0.69000   0.0371550
0.73000   0.0326360
0.77000   0.0279500
0.81000   0.0231740
0.84500   0.0186980
0.88000   0.0141260
0.91000   0.0102570
0.93500   0.0070320
0.95500   0.0046490
0.97000   0.0031890
0.98000   0.0023530
0.99000   0.0016290
0.99500   0.0013040
1.00000   0.0011300
 
0.00000   0.0000000
0.00055   -.0018830
0.00200   -.0035400
0.00400   -.0050850
0.00620   -.0063280
0.00860   -.0074050
0.01100   -.0082490
0.01465   -.0092660
0.01955   -.0101690
0.02615   -.0111490
0.03430   -.0120900
0.04449   -.0131070
0.05690   -.0142370
0.07245   -.0154430
0.09240   -.0166480
0.11850   -.0179660
0.15000   -.0192470
0.20000   -.0207910
0.25000   -.0219210
0.30000   -.0226740
0.35000   -.0232020
0.40000   -.0234270
0.45000   -.0233520
0.50000   -.0230890
0.55000   -.0225990
0.60000   -.0218950
0.65000   -.0209040
0.69000   -.0199040
0.73000   -.0187000
0.77000   -.0172530
0.81000   -.0156030
0.84500   -.0139520
0.88000   -.0120920
0.91000   -.0100310
0.93500   -.0081620
0.95500   -.0066080
0.97000   -.0051100
0.98000   -.0039350
0.99000   -.0026840
0.99500   -.0019070
1.00000   -.0011300
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Lednicer format dat file
Selig format dat file

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Polars for BOEING-VERTOL VR-14 AIRFOIL (vr14-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   vr14-il50,000929.4 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   vr14-il50,000529 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   vr14-il100,000940.6 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   vr14-il100,000540.3 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   vr14-il200,000950.7 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   vr14-il200,000554.3 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   vr14-il500,000974.3 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   vr14-il500,000573.4 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   vr14-il1,000,000991.2 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   vr14-il1,000,000587.3 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
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