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SARATOV AIRFOIL (saratov-il)

SARATOV AIRFOIL - Saratov R/C sailplane airfoil


Airfoil saratov-il
Details Dat file Parser  
(saratov-il) SARATOV AIRFOIL
Saratov R/C sailplane airfoil
Max thickness 9.2% at 15% chord.
Max camber 9.8% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
SARATOV AIRFOIL
       15.       15.

 0.0000000 0.0000000
 0.0125000 0.0203100
 0.0250000 0.0306300
 0.0500000 0.0462500
 0.1000000 0.0675000
 0.1500000 0.0827500
 0.2000000 0.0970000
 0.3000000 0.1175000
 0.4000000 0.1250000
 0.5000000 0.1135000
 0.6000000 0.0970000
 0.7000000 0.0775000
 0.8000000 0.0550000
 0.9000000 0.0285000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0146900
 0.0250000 -.0193800
 0.0500000 -.0217500
 0.1000000 -.0205000
 0.1500000 -.0092500
 0.2000000 0.0050000
 0.3000000 0.0355000
 0.4000000 0.0700000
 0.5000000 0.0625000
 0.6000000 0.0500000
 0.7000000 0.0375000
 0.8000000 0.0250000
 0.9000000 0.0125000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for SARATOV AIRFOIL (saratov-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   saratov-il50,000918.8 at α=13.5°Mach=0 Ncrit=9Xfoil predictionDetails
   saratov-il50,000518.9 at α=1.25°Mach=0 Ncrit=5Xfoil predictionDetails
   saratov-il100,000933.7 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   saratov-il100,000548.6 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   saratov-il200,0009161.9 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   saratov-il200,000577.9 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   saratov-il500,0009112.2 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   saratov-il500,0005113.8 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   saratov-il1,000,0009145.9 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   saratov-il1,000,0005136.9 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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