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USA-35B AIRFOIL (usa35b-il)

USA-35B AIRFOIL - USA-35B airfoil


Airfoil usa35b-il
Details Dat file Parser  
(usa35b-il) USA-35B AIRFOIL
USA-35B airfoil
Max thickness 11.6% at 30% chord.
Max camber 4.1% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
USA-35B AIRFOIL
      17.0      17.0

 0.0000000 0.0000000
 0.0125000 0.0239000
 0.0250000 0.0335000
 0.0500000 0.0476000
 0.0750000 0.0589000
 0.1000000 0.0669000
 0.1500000 0.0780000
 0.2000000 0.0852000
 0.3000000 0.0900000
 0.4000000 0.0866000
 0.5000000 0.0757000
 0.6000000 0.0605000
 0.7000000 0.0432000
 0.8000000 0.0226000
 0.9000000 -.0004000
 0.9500000 -.0126000
 1.0000000 -.0251000

 0.0000000 0.0000000
 0.0125000 -.0173000
 0.0250000 -.0213000
 0.0500000 -.0248000
 0.0750000 -.0262000
 0.1000000 -.0269000
 0.1500000 -.0276000
 0.2000000 -.0270000
 0.3000000 -.0261000
 0.4000000 -.0250000
 0.5000000 -.0237000
 0.6000000 -.0231000
 0.7000000 -.0234000
 0.8000000 -.0241000
 0.9000000 -.0256000
 0.9500000 -.0264000
 1.0000000 -.0276000
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Lednicer format dat file
Selig format dat file

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Polars for USA-35B AIRFOIL (usa35b-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   usa35b-il50,000924.6 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   usa35b-il50,000536.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   usa35b-il100,000953.3 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   usa35b-il100,000556.7 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   usa35b-il200,000976.8 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   usa35b-il200,000575.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   usa35b-il500,0009106 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   usa35b-il500,000597 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   usa35b-il1,000,0009125.6 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   usa35b-il1,000,0005113.1 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
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