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Induced drag (foil)

B1. Naval Architecture

Definition

Drag due to trailing-vortex circulation.

Induced drag is the drag penalty a finite-span lifting surface pays for producing lift, arising because the trailing vortex sheet shed at the tips induces a downwash that tilts the local lift vector backward. For an elliptically loaded foil the induced drag coefficient is C_Di = C_L^2 / (pi AR), so it scales with the square of lift and inversely with aspect ratio AR = b^2 / S. Low-aspect-ratio rudders and control foils therefore carry heavy induced drag at angle, which is why a deeper, higher-AR rudder or an end plate that raises effective AR cuts the penalty. Induced drag is distinct from the viscous profile drag of the section and vanishes only at zero lift.

Source: Prandtl lifting-line theory (finite-wing induced drag)