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USA 48 AIRFOIL (usa48-il)

USA 48 AIRFOIL - USA-48 airfoil


Airfoil usa48-il
Details Dat file Parser  
(usa48-il) USA 48 AIRFOIL
USA-48 airfoil
Max thickness 14.9% at 30% chord.
Max camber 2.9% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
USA 48 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0220000
 0.0250000 0.0320000
 0.0500000 0.0480000
 0.0750000 0.0610000
 0.1000000 0.0690000
 0.1500000 0.0828000
 0.2000000 0.0922000
 0.3000000 0.1010000
 0.4000000 0.1015000
 0.5000000 0.0948000
 0.6000000 0.0836000
 0.7000000 0.0683000
 0.8000000 0.0507000
 0.9000000 0.0287000
 0.9500000 0.0160000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0140000
 0.0250000 -.0200000
 0.0500000 -.0270000
 0.0750000 -.0343000
 0.1000000 -.0383000
 0.1500000 -.0453000
 0.2000000 -.0480000
 0.3000000 -.0480000
 0.4000000 -.0440000
 0.5000000 -.0390000
 0.6000000 -.0320000
 0.7000000 -.0197000
 0.8000000 -.0110000
 0.9000000 -.0057000
 0.9500000 -.0027000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for USA 48 AIRFOIL (usa48-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   usa48-il50,000924.1 at α=12°Mach=0 Ncrit=9Xfoil predictionDetails
   usa48-il50,000530.6 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   usa48-il100,000949.8 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   usa48-il100,000549.3 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   usa48-il200,000969.1 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   usa48-il200,000563.2 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   usa48-il500,000985.1 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   usa48-il500,000565.1 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   usa48-il1,000,000981.4 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   usa48-il1,000,000573.2 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
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