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UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT (ua79sff-il)

UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT - University of Alberta/Marsden UA 79-SF-187 sailplane airfoil FLAP


Airfoil ua79sff-il
Details Dat file Parser  
(ua79sff-il) UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT
University of Alberta/Marsden UA 79-SF-187 sailplane airfoil FLAP
Max thickness 8.7% at 73.1% chord.
Max camber 3.4% at 78.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT
     20.0      20.0

 0.650000  -.018400
 0.654800  0.007200
 0.665100  0.026400
 0.682300  0.042400
 0.697200  0.050800
 0.716900  0.057800
 0.730700  0.061100
 0.747600  0.063400
 0.766000  0.064400
 0.780800  0.063600
 0.795800  0.061800
 0.811700  0.058400
 0.853500  0.045000
 0.890900  0.033300
 0.923400  0.023000
 0.950500  0.015000
 0.971900  0.008500
 0.987500  0.003700
 0.996900  0.001000
 1.000000  0.000000

 0.650000  -.018400
 0.654800  -.029800
 0.665100  -.034100
 0.682300  -.032900
 0.697200  -.031100
 0.716900  -.028100
 0.730700  -.025700
 0.747600  -.023400
 0.766000  -.020800
 0.780800  -.018300
 0.795800  -.016500
 0.811700  -.013700
 0.853500  -.007900
 0.890900  -.003300
 0.923400  -.000300
 0.950500  0.000600
 0.971900  0.000900
 0.987500  0.000700
 0.996900  0.000300
 1.000000  0.000000
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Lednicer format dat file
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Polars for UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT (ua79sff-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ua79sff-il50,00093.4 at α=19.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ua79sff-il50,00053.5 at α=19.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ua79sff-il100,00093.6 at α=19.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ua79sff-il100,00054.1 at α=18.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ua79sff-il200,00093.8 at α=19.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ua79sff-il200,00055.1 at α=13.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ua79sff-il500,00096.4 at α=13.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ua79sff-il500,000525.9 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ua79sff-il1,000,000960.5 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ua79sff-il1,000,000562 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
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