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RG 14 10% AIRFOIL (rg1410-il)

RG 14 10% AIRFOIL - Rolf Girsberger RG 14 (10%) airfoil


Airfoil rg1410-il
Details Dat file Parser  
(rg1410-il) RG 14 10% AIRFOIL
Rolf Girsberger RG 14 (10%) airfoil
Max thickness 10% at 31% chord.
Max camber 1.6% at 36% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
RG 14 10% AIRFOIL
       30.       30.

 0.0000000 0.0000000
 0.0046500 0.0107200
 0.0144700 0.0194000
 0.0293800 0.0277800
 0.0493100 0.0356000
 0.0741200 0.0427100
 0.1036300 0.0490300
 0.1375600 0.0541900
 0.1755900 0.0588600
 0.2173000 0.0623300
 0.2622700 0.0645600
 0.3099800 0.0655700
 0.3598900 0.0654100
 0.4114400 0.0641200
 0.4640100 0.0618300
 0.5170100 0.0586100
 0.5697900 0.0546500
 0.6217500 0.0500900
 0.6722700 0.0450500
 0.7207300 0.0397200
 0.7668900 0.0342000
 0.8105700 0.0286100
 0.8512100 0.0231200
 0.8881100 0.0179300
 0.9206300 0.0131500
 0.9481700 0.0089300
 0.9702600 0.0051900
 0.9865400 0.0022200
 0.9965900 0.0004900
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0046500 -.0072600
 0.0144700 -.0130200
 0.0293800 -.0181900
 0.0493100 -.0226900
 0.0741200 -.0264300
 0.1036300 -.0294400
 0.1375600 -.0317100
 0.1755900 -.0333100
 0.2173000 -.0342500
 0.2622700 -.0346100
 0.3099800 -.0344300
 0.3598900 -.0337500
 0.4114400 -.0326500
 0.4640100 -.0311900
 0.5170100 -.0293800
 0.5697900 -.0273000
 0.6217500 -.0249400
 0.6722700 -.0223300
 0.7207300 -.0193100
 0.7668900 -.0157500
 0.8105700 -.0119800
 0.8512100 -.0085300
 0.8881100 -.0056200
 0.9206300 -.0033400
 0.9481700 -.0017100
 0.9702600 -.0006200
 0.9865400 -.0000600
 0.9965900 0.0000500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for RG 14 10% AIRFOIL (rg1410-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   rg1410-il50,000932.2 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   rg1410-il50,000533.6 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   rg1410-il100,000948.2 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   rg1410-il100,000546.4 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   rg1410-il200,000963.5 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   rg1410-il200,000558.1 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   rg1410-il500,000982.3 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   rg1410-il500,000571.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   rg1410-il1,000,000989.4 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   rg1410-il1,000,000585.5 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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