Coefficient of lift where zero-lift drag and the drag due to lift are equal Calculator

The coefficient of lift (CL) is a dimensionless quantity used in aerodynamics to characterize the amount of lift generated by an aerodynamic object, such as an airfoil or wing, relative to the fluid flow around it. 
  • CL: Lift coefficient
  • e: Oswald’s efficiency factor
  • AR: Aspect ratio
  • CD,o: zero lift drag coefficient 

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