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BOEING-VERTOL V23010-1.58 AIRFOIL (v23010-il)

BOEING-VERTOL V23010-1.58 AIRFOIL - Boeing-Vertol V23010-1.58 rotorcraft airfoil


Airfoil v23010-il
Details Dat file Parser  
(v23010-il) BOEING-VERTOL V23010-1.58 AIRFOIL
Boeing-Vertol V23010-1.58 rotorcraft airfoil
Max thickness 10.2% at 30% chord.
Max camber 1.8% at 15% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 BOEING-VERTOL V23010-1.58 AIRFOIL
       26.       26.

 0.0       0.0
 0.0099884 0.0192060
 0.0199836 0.0270120
 0.0299799 0.0331180
 0.0499741 0.0428300
 0.0749690 0.0514449
 0.0999656 0.0570598
 0.1249631 0.0612748
 0.1499614 0.0641899
 0.1999602 0.0662197
 0.2499603 0.0659497
 0.2999610 0.0649799
 0.3499621 0.0630098
 0.3999636 0.0605399
 0.4499654 0.0574699
 0.4999677 0.0536999
 0.5499704 0.0493299
 0.5999732 0.0446599
 0.6499763 0.0394899
 0.6999798 0.0337199
 0.7499831 0.0281499
 0.7999862 0.0229800
 0.8499898 0.0170100
 0.8999931 0.0115400
 0.9499966 0.0056700
 1.0000000 0.0

 0.0       0.0
 0.0100089 -.0150940
 0.0200104 -.0175880
 0.0300112 -.0189820
 0.0500122 -.0205700
 0.0750135 -.0226550
 0.1000147 -.0247400
 0.1250160 -.0268250
 0.1500173 -.0291100
 0.2000195 -.0326800
 0.2500211 -.0353500
 0.3000220 -.0368200
 0.3500222 -.0370900
 0.4000220 -.0367600
 0.4500213 -.0355299
 0.5000202 -.0337999
 0.5500188 -.0314699
 0.6000172 -.0287399
 0.6500152 -.0254100
 0.7000133 -.0221800
 0.7500111 -.0185500
 0.8000090 -.0149200
 0.8500068 -.0111900
 0.9000045 -.0075600
 0.9500023 -.0038300
 1.0000000 0.0
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Lednicer format dat file
Selig format dat file

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Polars for BOEING-VERTOL V23010-1.58 AIRFOIL (v23010-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   v23010-il50,000923.8 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   v23010-il50,000527.9 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   v23010-il100,000935.1 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   v23010-il100,000541.2 at α=9.5°Mach=0 Ncrit=5Xfoil predictionDetails
   v23010-il200,000954.2 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   v23010-il200,000557.7 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   v23010-il500,000979.9 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   v23010-il500,000578 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   v23010-il1,000,000997.6 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   v23010-il1,000,000594.1 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
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