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Airfoil comparison (naca0024-il)
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    (naca0024-il) NACA 0024

NACA 0024 airfoil
Max thickness 24% at 30% chord
Max camber 0% at 0% chord
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Used for printing plan. A4 landscape approx 280mm
Used for printing plan. A4 landscape approx 180mm

Polars for (naca0024-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   naca0024-il50,000915.4 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   naca0024-il50,000521.6 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   naca0024-il100,000934.7 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   naca0024-il100,000530.6 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
   naca0024-il200,000943 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   naca0024-il200,000537 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
   naca0024-il500,000952.1 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   naca0024-il500,000550.8 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   naca0024-il1,000,000968.8 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   naca0024-il1,000,000564.1 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
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