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AS5046 (16%) (as5046-il)

AS5046 (16%) - AS5046 airfoil Ashok Gopalarathnam/Selig 16% airfoil


Airfoil as5046-il
Details Dat file Parser  
(as5046-il) AS5046 (16%)
AS5046 airfoil Ashok Gopalarathnam/Selig 16% airfoil
Max thickness 16% at 37.6% chord.
Max camber 0.7% at 77.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
AS5046 (16%)
1.0000 .00134  
.99804 .00200      
.99260 .00372    
.98401 .00594  
.97220 .00866  
.95749 .01168        
.93979 .01474   
.91895 .01797   
.89512 .02146 
.86847 .02532   
.83924 .02960   
.80767 .03441   
.77409 .03982   
.73889 .04596  
.70270 .05277   
.66609 .06004   
.62962 .06733 
.59358 .07375 
.55759 .07896 
.52139 .08307  
.48502 .08610 
.44860 .08824 
.41235 .08957 
.37649 .09013 
.34123 .08996 
.30680 .08908 
.27342 .08752 
.24130 .08527 
.21060 .08233 
.18148 .07874 
.15411 .07456 
.12868 .06983 
.10538 .06454  
.08429 .05863 
.06537 .05215
.04876 .04527 
.03450 .03803 
.02260 .03058
.01322 .02302 
.00632 .01544 
.00193 .00801 
.00003 .00097 
.00071 -.00489
.00510 -.00988 
.01342 -.01505 
.02489 -.02044 
.03925 -.02596 
.05625 -.03155 
.07571 -.03710 
.09745 -.04246 
.12133 -.04752 
.14723 -.05216
.17505 -.05634 
.20462 -.06003
.23577 -.06321
.26829 -.06582 
.30198 -.06783 
.33664 -.06919
.37208 -.06986
.40806 -.06980
.44435 -.06899 
.48068 -.06725 
.51700 -.06445 
.55315 -.06046 
.58935 -.05509
.62582 -.04860 
.66265 -.04132 
.70010 -.03396 
.73735 -.02722 
.77354 -.02135 
.80827 -.01632 
.84111 -.01210
.87165 -.00870 
.89952 -.00605 
.92439 -.00407
.94591 -.00256 
.96421 -.00129 
.97931 -.00050 
.99065 -.00052 
.99763 -.00101 
1.0000 -.00134
http://amber.aae.uiuc.edu/~ashok/kr2/airfoils/tests/
Dat file parser warnings
  • Line 83 - Invalid characters : http://amber.aae.uiuc.edu/~ashok/kr2/airfoils/tests/
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Selig format dat file

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Polars for AS5046 (16%) (as5046-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   as5046-il50,000928.2 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   as5046-il50,000528.1 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   as5046-il100,000942.2 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   as5046-il100,000542.3 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   as5046-il200,000958.1 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   as5046-il200,000555.4 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   as5046-il500,000977.7 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   as5046-il500,000569.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   as5046-il1,000,000990.8 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   as5046-il1,000,000583.5 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
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