Lift coefficient for arbitrary spanwise station Calculator

Lift coefficient for the local airfoil section at the spanwise station. It is a dimensionless quantity representing the lift generated by the section normalized by dynamic pressure and reference area. 

  • : Lift coefficient for the local airfoil section at the spanwise station. It is a dimensionless quantity representing the lift generated by the section normalized by dynamic pressure and reference area.
  • : Circulation at the spanwise station , representing the strength of the vortex system generated by the airfoil section. It is often measured in square meters per second ().
  • : Freestream velocity (velocity far away from the airfoil), measured in meters per second ().
  • : Local chord length at the spanwise station , measured in meters ().

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