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BOEING-VERTOL VR-5 AIRFOIL (vr5-il)

BOEING-VERTOL VR-5 AIRFOIL - Boeing-Vertol VR-5 rotorcraft airfoil


Airfoil vr5-il
Details Dat file Parser  
(vr5-il) BOEING-VERTOL VR-5 AIRFOIL
Boeing-Vertol VR-5 rotorcraft airfoil
Max thickness 12% at 35% chord.
Max camber 3.4% at 35% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 
 BOEING-VERTOL VR-5 AIRFOIL
28.        28.
 
 0.         0.
  .00350     .01340
  .00700     .01720
  .01100     .02090
  .02250     .02910
  .04000     .03860
  .06000     .04720
  .08500     .05630
  .12000     .06640
  .16000     .07600
  .21000     .08400
  .27000     .09030
  .31000     .09300
  .35000     .09400
  .43000     .09200
  .48000     .08760
  .53000     .08140
  .58000     .07430
  .63000     .06590
  .68000     .05670
  .73000     .04730
  .77000     .03940
  .81000     .03090
  .85000     .02260
  .89000     .01500
  .95000     .00540
  .98000     .00180
 1.0         .00040
 
 0.         0.
  .00350    -.00460
  .00700    -.00680
  .01100    -.00863
  .02250    -.01135
  .04000    -.01340
  .06000    -.01520
  .08500    -.01670
  .12000    -.01810
  .16000    -.01960
  .21000    -.02200
  .27000    -.02440
  .31000    -.02580
  .35000    -.02600
  .43000    -.02620
  .48000    -.02600
  .53000    -.02440
  .58000    -.02200
  .63000    -.01900
  .68000    -.01580
  .73000    -.01260
  .77000    -.00980
  .81000    -.00720
  .85000    -.00500
  .89000    -.00290
  .95000    -.00045
  .98000    -.00040
 1.0        -.00040
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Lednicer format dat file
Selig format dat file

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Polars for BOEING-VERTOL VR-5 AIRFOIL (vr5-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   vr5-il50,000931.7 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   vr5-il50,000529.5 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   vr5-il100,000955.2 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   vr5-il100,000555.4 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   vr5-il200,000979.9 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   vr5-il200,000578 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   vr5-il500,0009112.8 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   vr5-il500,0005105.1 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   vr5-il1,000,0009136.1 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   vr5-il1,000,0005117.3 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
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