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RG 15A-1.8/11.0 AIRFOIL (rg15a111-il)

RG 15A-1.8/11.0 AIRFOIL - Rolf Girsberger RG 15A-1.8/11.0 airfoil


Airfoil rg15a111-il
Details Dat file Parser  
(rg15a111-il) RG 15A-1.8/11.0 AIRFOIL
Rolf Girsberger RG 15A-1.8/11.0 airfoil
Max thickness 11% at 30.2% chord.
Max camber 1.8% at 39.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
RG 15A-1.8/11.0 AIRFOIL
       32.       32.

 0.0000000 0.0000000
 0.0021400 0.0071400
 0.0088800 0.0153300
 0.0202800 0.0237900
 0.0360400 0.0322200
 0.0561900 0.0402300
 0.0805500 0.0476700
 0.1089500 0.0543500
 0.1411700 0.0601200
 0.1769400 0.0648800
 0.2159500 0.0685400
 0.2578900 0.0710500
 0.3023600 0.0724100
 0.3489700 0.0726200
 0.3972800 0.0717300
 0.4468300 0.0697900
 0.4971200 0.0669000
 0.5476300 0.0631300
 0.5978700 0.0585800
 0.6473300 0.0534100
 0.6954800 0.0477900
 0.7417800 0.0418900
 0.7857000 0.0359000
 0.8267400 0.0299600
 0.8644000 0.0242400
 0.8982100 0.0188600
 0.9277400 0.0139500
 0.9525500 0.0095600
 0.9724200 0.0056500
 0.9872800 0.0024900
 0.9967200 0.0005900
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0039600 -.0063900
 0.0132000 -.0121800
 0.0250100 -.0170900
 0.0415600 -.0218300
 0.0617900 -.0258900
 0.0860800 -.0294000
 0.1141100 -.0322700
 0.1457700 -.0345200
 0.1808100 -.0361500
 0.2190200 -.0371800
 0.2601000 -.0376300
 0.3037500 -.0375400
 0.3495900 -.0369200
 0.3972400 -.0358000
 0.4462600 -.0341700
 0.4961900 -.0320500
 0.5466600 -.0293200
 0.5970500 -.0257800
 0.6464601 -.0216300
 0.6944200 -.0173500
 0.7405500 -.0132500
 0.7843699 -.0095400
 0.8253900 -.0063500
 0.8631000 -.0037800
 0.8970600 -.0018500
 0.9267800 -.0005600
 0.9517900 0.0001800
 0.9719100 0.0004800
 0.9870500 0.0004400
 0.9966700 0.0001700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for RG 15A-1.8/11.0 AIRFOIL (rg15a111-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   rg15a111-il50,000932.3 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   rg15a111-il50,000535.1 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   rg15a111-il100,000950 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   rg15a111-il100,000549.5 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   rg15a111-il200,000966.8 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   rg15a111-il200,000562.7 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   rg15a111-il500,000987.9 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   rg15a111-il500,000579.7 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   rg15a111-il1,000,0009101.9 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   rg15a111-il1,000,000590 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
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