Lift-induced drag coefficient calculator

The drag component that results from the generation of lift by an aircraft’s wings. It is a critical parameter used to assess the efficiency of an aircraft’s lift production and its impact on overall aerodynamic performance.

  • lv: This likely represents the lift-induced drag coefficient for an aircraft.
  • L’v: This may be the change in lift with respect to a change in the vertical velocity (sometimes represented as dL/dv), which can be influenced by changes in the angle of attack or other factors.
  • ρ: This represents the air density.
  • u0: This is probably the airspeed or the flight velocity.
  • S: This typically stands for the reference wing area.
  • b: This is likely the wingspan of the aircraft.

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