Vortex Lift Coefficient Calculator

The Vortex Lift Coefficient () is a parameter used in the analysis of aircraft aerodynamics, particularly in the context of vortex lift generated by leading-edge vortices

 

  • is the vortex lift coefficient.
  • is the circulation around the wing (strength of the vortex).
  • is the air density.
  • is the velocity of the aircraft.
  • is the maximum possible circulation for vortex lift.

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