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BOEING VERTOL V(1.95)3009-1.25 AIRFOIL (v13009-il)

BOEING VERTOL V(1.95)3009-1.25 AIRFOIL - Boeing-Vertol V(1.9)3006-1.25 rotorcraft airfoil


Airfoil v13009-il
Details Dat file Parser  
(v13009-il) BOEING VERTOL V(1.95)3009-1.25 AIRFOIL
Boeing-Vertol V(1.9)3006-1.25 rotorcraft airfoil
Max thickness 9% at 30.1% chord.
Max camber 1.3% at 20.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
  BOEING VERTOL V(1.95)3009-1.25 AIRFOIL
       20.       20.

 0.0000000 0.0000000
 0.0052062 0.0116900
 0.0128420 0.0193966
 0.0254831 0.0274050
 0.0506615 0.0375227
 0.0757772 0.0440809
 0.1008605 0.0488094
 0.1509463 0.0536771
 0.2009960 0.0564952
 0.2510130 0.0574635
 0.3010098 0.0572820
 0.3509895 0.0561307
 0.4009583 0.0543594
 0.5008578 0.0486574
 0.6007263 0.0411955
 0.7005668 0.0321439
 0.8003905 0.0221525
 0.9002098 0.0119011
 0.9501143 0.0064805
 1.0000000 0.0005500

 0.0000000 0.0000000
 0.0048215 -.0101266
 0.0122410 -.0146981
 0.0246672 -.0188878
 0.0495940 -.0230379
 0.0745562 -.0251783
 0.0995272 -.0268288
 0.1494896 -.0289600
 0.1994627 -.0304912
 0.2494391 -.0318225
 0.2994237 -.0327039
 0.3494146 -.0332153
 0.3994148 -.0332068
 0.4994531 -.0310301
 0.5995226 -.0270937
 0.6996199 -.0215676
 0.7997339 -.0151016
 0.8998524 -.0083757
 0.9499168 -.0047178
 1.0000000 -.0005500
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Polars for BOEING VERTOL V(1.95)3009-1.25 AIRFOIL (v13009-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   v13009-il50,000926.2 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   v13009-il50,000528.7 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   v13009-il100,000936.6 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   v13009-il100,000539.7 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   v13009-il200,000949.7 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   v13009-il200,000553.7 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   v13009-il500,000972.9 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   v13009-il500,000571.7 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   v13009-il1,000,000988.4 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   v13009-il1,000,000586.4 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
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