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TSAGI 8% AIRFOIL (tsagi8-il)

TSAGI 8% AIRFOIL - TSAGI 8% airfoil


Airfoil tsagi8-il
Details Dat file Parser  
(tsagi8-il) TSAGI 8% AIRFOIL
TSAGI 8% airfoil
Max thickness 8% at 30% chord.
Max camber 1.3% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
TSAGI 8% AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0111000
 0.0250000 0.0166000
 0.0500000 0.0247000
 0.0750000 0.0308000
 0.1000000 0.0359000
 0.1500000 0.0435000
 0.2000000 0.0486000
 0.3000000 0.0531000
 0.4000000 0.0518000
 0.5000000 0.0467000
 0.6000000 0.0388000
 0.7000000 0.0295000
 0.8000000 0.0196000
 0.9000000 0.0097700
 0.9500000 0.0049000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0085000
 0.0250000 -.0119000
 0.0500000 -.0161000
 0.0750000 -.0187000
 0.1000000 -.0205000
 0.1500000 -.0231000
 0.2000000 -.0247000
 0.3000000 -.0264000
 0.4000000 -.0272000
 0.5000000 -.0268000
 0.6000000 -.0256000
 0.7000000 -.0228000
 0.8000000 -.0183000
 0.9000000 -.0112000
 0.9500000 -.0065000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for TSAGI 8% AIRFOIL (tsagi8-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   tsagi8-il50,000932.8 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   tsagi8-il50,000532.5 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   tsagi8-il100,000945.3 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   tsagi8-il100,000544.4 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   tsagi8-il200,000957.7 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   tsagi8-il200,000555.4 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   tsagi8-il500,000972.2 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   tsagi8-il500,000565.1 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   tsagi8-il1,000,000976.8 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   tsagi8-il1,000,000569.7 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
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