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USA 32 AIRFOIL (usa32-il)

USA 32 AIRFOIL - USA-32 airfoil


Airfoil usa32-il
Details Dat file Parser  
(usa32-il) USA 32 AIRFOIL
USA-32 airfoil
Max thickness 14.7% at 19.8% chord.
Max camber 9.3% at 39.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
USA 32 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0120700 0.0391300
 0.0243700 0.0572700
 0.0491100 0.0805400
 0.0739400 0.0968100
 0.0987900 0.1100900
 0.1485700 0.1296300
 0.1984100 0.1441800
 0.2982600 0.1582800
 0.3982500 0.1593800
 0.4983300 0.1514800
 0.5985200 0.1345800
 0.6987400 0.1146900
 0.7990700 0.0847900
 0.8994800 0.0468900
 0.9497200 0.0254500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0126100 -.0098600
 0.0251300 -.0117200
 0.0501500 -.0134500
 0.0751600 -.0141700
 0.1001500 -.0139000
 0.1501100 -.0103500
 0.2000300 -.0028000
 0.2998400 0.0143000
 0.3997000 0.0274000
 0.4997300 0.0245000
 0.5998100 0.0176000
 0.6999400 0.0057000
 0.8000400 -.0032000
 0.9000599 -.0051000
 0.9500400 -.0035500
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for USA 32 AIRFOIL (usa32-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   usa32-il50,00094.5 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   usa32-il50,000513.5 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   usa32-il100,000939.8 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   usa32-il100,000541 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   usa32-il200,000964.3 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   usa32-il200,000550.5 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   usa32-il500,000968.9 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   usa32-il500,000559.6 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   usa32-il1,000,000976.9 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   usa32-il1,000,000567.9 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
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