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RAF 32 MOD AIRFOIL (raf32md-il)

RAF 32 MOD AIRFOIL - RAF-32 MOD airfoil


Airfoil raf32md-il
Details Dat file Parser  
(raf32md-il) RAF 32 MOD AIRFOIL
RAF-32 MOD airfoil
Max thickness 10.2% at 30% chord.
Max camber 4% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
RAF 32 MOD AIRFOIL
       15.       15.

 0.0000000 0.0000000
 0.0125000 0.0174300
 0.0250000 0.0254600
 0.0500000 0.0366200
 0.1000000 0.0530400
 0.1500000 0.0645600
 0.2000000 0.0733800
 0.3000000 0.0845200
 0.4000000 0.0881600
 0.5000000 0.0853000
 0.6000000 0.0769400
 0.7000000 0.0638800
 0.8000000 0.0462200
 0.9000000 0.0251600
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0113700
 0.0250000 -.0147400
 0.0500000 -.0190800
 0.1000000 -.0223600
 0.1500000 -.0228400
 0.2000000 -.0221200
 0.3000000 -.0170800
 0.4000000 -.0112400
 0.5000000 -.0062000
 0.6000000 0.0001400
 0.7000000 0.0038800
 0.8000000 0.0054200
 0.9000000 0.0037600
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for RAF 32 MOD AIRFOIL (raf32md-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   raf32md-il50,000938 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   raf32md-il50,000537.5 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   raf32md-il100,000962.1 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   raf32md-il100,000561.3 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   raf32md-il200,000987.2 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   raf32md-il200,000583.8 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   raf32md-il500,0009120.8 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   raf32md-il500,0005110.5 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   raf32md-il1,000,0009144.4 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   raf32md-il1,000,0005124.3 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
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