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BOEING VERTOL V13006-.7 AIRFOIL (v13006-il)

BOEING VERTOL V13006-.7 AIRFOIL - Boeing-Vertol V13006-.7 rotorcraft airfoil


Airfoil v13006-il
Details Dat file Parser  
(v13006-il) BOEING VERTOL V13006-.7 AIRFOIL
Boeing-Vertol V13006-.7 rotorcraft airfoil
Max thickness 6% at 30.2% chord.
Max camber 0.9% at 20.2% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
  BOEING VERTOL V13006-.7 AIRFOIL
       21.       21.

 0.0000001 0.0
 0.0020625 0.0055647
 0.0045858 0.0079296
 0.0096073 0.0105647
 0.0146265 0.0129998
 0.0271536 0.0173410
 0.0521836 0.0240278
 0.0771898 0.0287186
 0.1021828 0.0323116
 0.1521293 0.0361047
 0.2020521 0.0380019
 0.2519568 0.0384023
 0.3018544 0.0382037
 0.4016305 0.0361106
 0.5013863 0.0324207
 0.6011277 0.0275328
 0.7008607 0.0218470
 0.8005842 0.0154633
 0.9003004 0.0083806
 0.9501550 0.0045893
 1.0000000 0.0006000

 0.0000001 0.0
 0.0019346 -.0051135
 0.0044066 -.0070393
 0.0093743 -.0088949
 0.0143505 -.0100526
 0.0268045 -.0117988
 0.0517271 -.0140935
 0.0766580 -.0156902
 0.1015960 -.0166869
 0.1514768 -.0183824
 0.2013600 -.0197779
 0.2512469 -.0208744
 0.3011386 -.0215720
 0.4009373 -.0217692
 0.5007529 -.0204695
 0.6005828 -.0179719
 0.7004234 -.0146763
 0.8002711 -.0106828
 0.9001283 -.0059903
 0.9500594 -.0033941
 1.0000000 -.0006000
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Lednicer format dat file
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Polars for BOEING VERTOL V13006-.7 AIRFOIL (v13006-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   v13006-il50,000927.9 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   v13006-il50,000528.1 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   v13006-il100,000937.7 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   v13006-il100,000535.3 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   v13006-il200,000946.3 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   v13006-il200,000541.1 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   v13006-il500,000954.7 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   v13006-il500,000553.7 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   v13006-il1,000,000962.4 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   v13006-il1,000,000564.2 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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