The lift coefficient of the wing calculator

The lift coefficient () of a wing in flight mechanics is a dimensionless aerodynamic parameter that quantifies the lift-generating characteristics of the wing. It is a critical parameter used to understand and analyze an aircraft’s performance, stability, and control.
  • is the lift coefficient of the wing.
  • is the lift curve slope of the wing, representing how lift changes with respect to changes in angle of attack ().
  • is the angle of attack (real part).
  • is the imaginary unit (typically representing oscillatory behavior or phase).
  • represents the frequency or angular frequency (related to oscillations or vibrations).
  • is the angle of attack at which the wing experiences zero lift, also known as the zero-lift angle of attack.

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