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RAF 30 MOD AIRFOIL (raf30md-il)

RAF 30 MOD AIRFOIL - RAF-30 MOD airfoil


Airfoil raf30md-il
Details Dat file Parser  
(raf30md-il) RAF 30 MOD AIRFOIL
RAF-30 MOD airfoil
Max thickness 7.6% at 30% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
RAF 30 MOD AIRFOIL
       15.       15.

 0.0000000 0.0000000
 0.0125000 0.0108000
 0.0250000 0.0149000
 0.0500000 0.0208000
 0.1000000 0.0281000
 0.1500000 0.0326000
 0.2000000 0.0356000
 0.3000000 0.0380000
 0.4000000 0.0372000
 0.5000000 0.0340000
 0.6000000 0.0287000
 0.7000000 0.0222000
 0.8000000 0.0150000
 0.9000000 0.0078000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0108000
 0.0250000 -.0149000
 0.0500000 -.0208000
 0.1000000 -.0281000
 0.1500000 -.0326000
 0.2000000 -.0356000
 0.3000000 -.0380000
 0.4000000 -.0372000
 0.5000000 -.0340000
 0.6000000 -.0287000
 0.7000000 -.0222000
 0.8000000 -.0150000
 0.9000000 -.0078000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for RAF 30 MOD AIRFOIL (raf30md-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   raf30md-il50,000926.4 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   raf30md-il50,000525.1 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   raf30md-il100,000935.2 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   raf30md-il100,000531 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   raf30md-il200,000942.7 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   raf30md-il200,000536.3 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   raf30md-il500,000947.9 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   raf30md-il500,000552.3 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   raf30md-il1,000,000959.9 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   raf30md-il1,000,000565.4 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
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