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BOEING VERTOL V43012-1.58 AIRFOIL (v43012-il)

BOEING VERTOL V43012-1.58 AIRFOIL - Boeing-Vertol V43012-1.58 rotorcraft airfoil


Airfoil v43012-il
Details Dat file Parser  
(v43012-il) BOEING VERTOL V43012-1.58 AIRFOIL
Boeing-Vertol V43012-1.58 rotorcraft airfoil
Max thickness 12% at 32% chord.
Max camber 3.7% at 15% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
  BOEING VERTOL V43012-1.58 AIRFOIL
       37.       37.

 0.0000000 0.0000000
 0.0100000 0.0321000
 0.0200000 0.0423000
 0.0300000 0.0503000
 0.0400000 0.0571000
 0.0500000 0.0631000
 0.0750000 0.0745000
 0.0900000 0.0791000
 0.1100000 0.0840000
 0.1250000 0.0869000
 0.1500000 0.0901000
 0.1800000 0.0920000
 0.2100000 0.0929000
 0.2450000 0.0926000
 0.2800000 0.0920000
 0.3200000 0.0905000
 0.3600000 0.0880000
 0.4000000 0.0850000
 0.4400000 0.0820000
 0.4800000 0.0780000
 0.5200000 0.0733000
 0.5600000 0.0685000
 0.6000000 0.0635000
 0.6400000 0.0582000
 0.6800000 0.0527000
 0.7200000 0.0469000
 0.7600000 0.0410000
 0.8000000 0.0350000
 0.8300000 0.0301000
 0.8600000 0.0253000
 0.8900000 0.0203000
 0.9100000 0.0167000
 0.9250000 0.0140000
 0.9400000 0.0113000
 0.9550000 0.0084000
 0.9800000 0.0038000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0100000 -.0077000
 0.0200000 -.0090000
 0.0300000 -.0100000
 0.0400000 -.0108000
 0.0500000 -.0108000
 0.0750000 -.0110000
 0.0900000 -.0115000
 0.1100000 -.0130000
 0.1250000 -.0142000
 0.1500000 -.0167000
 0.1800000 -.0200000
 0.2100000 -.0231000
 0.2450000 -.0260000
 0.2800000 -.0281000
 0.3200000 -.0299000
 0.3600000 -.0310000
 0.4000000 -.0315000
 0.4400000 -.0314000
 0.4800000 -.0310000
 0.5200000 -.0304000
 0.5600000 -.0293000
 0.6000000 -.0279000
 0.6400000 -.0263000
 0.6800000 -.0244000
 0.7200000 -.0222000
 0.7600000 -.0198000
 0.8000000 -.0172000
 0.8300000 -.0149000
 0.8600000 -.0125000
 0.8900000 -.0100000
 0.9100000 -.0084000
 0.9250000 -.0070000
 0.9400000 -.0057000
 0.9550000 -.0043000
 0.9800000 -.0020000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for BOEING VERTOL V43012-1.58 AIRFOIL (v43012-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   v43012-il50,000924 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   v43012-il50,000528.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   v43012-il100,000936.3 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   v43012-il100,000540.6 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   v43012-il200,000950.5 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   v43012-il200,000555.9 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   v43012-il500,000977.7 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   v43012-il500,000581.1 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   v43012-il1,000,0009102.9 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   v43012-il1,000,0005101.3 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
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