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RAF 28 AIRFOIL (raf28-il)

RAF 28 AIRFOIL - RAF-28 airfoil


Airfoil raf28-il
Details Dat file Parser  
(raf28-il) RAF 28 AIRFOIL
RAF-28 airfoil
Max thickness 9.8% at 30% chord.
Max camber 1.9% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
RAF 28 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0145000
 0.0250000 0.0210000
 0.0500000 0.0313000
 0.0750000 0.0390000
 0.1000000 0.0446000
 0.1500000 0.0536000
 0.2000000 0.0600000
 0.3000000 0.0670000
 0.4000000 0.0672000
 0.5000000 0.0625000
 0.6000000 0.0540000
 0.7000000 0.0432000
 0.8000000 0.0293000
 0.9000000 0.0163000
 0.9500000 0.0089000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0125000
 0.0250000 -.0165000
 0.0500000 -.0220000
 0.0750000 -.0253000
 0.1000000 -.0275000
 0.1500000 -.0305000
 0.2000000 -.0320000
 0.3000000 -.0312000
 0.4000000 -.0286000
 0.5000000 -.0250000
 0.6000000 -.0210000
 0.7000000 -.0160000
 0.8000000 -.0110000
 0.9000000 -.0063000
 0.9500000 -.0034000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for RAF 28 AIRFOIL (raf28-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   raf28-il50,000935.6 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   raf28-il50,000535.8 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   raf28-il100,000952.6 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   raf28-il100,000550.9 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   raf28-il200,000969.4 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   raf28-il200,000564.4 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   raf28-il500,000990.6 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   raf28-il500,000579.5 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   raf28-il1,000,0009103.9 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   raf28-il1,000,000583.6 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
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