Kite in the wind - 2D side view

Lift, drag, weight and line tension balance on a tethered kite as the wind changes.

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The science

Forces on a tethered kite

The wind pushes on the sail with dynamic pressure q = ½ ρ U². Lift is perpendicular to the wind, L = q A CL(α), and drag is along it, D = q A CD(α). Gravity adds the weight W = m g. The line is the only other force, so a steady kite sits where the three forces cancel: horizontally T cosθ = D, vertically T sinθ = L - W. Dividing gives the line elevation tanθ = (L - W) / D and the tension T = √(D² + (L - W)²).

Why a kite needs a minimum wind

The kite can only climb when L > W, which sets Umin = √(2 m g / (ρ A CL)). Because force grows with U², a modest increase in wind raises the tension a lot while the line elevation is limited by the lift-to-drag ratio.

Flat-plate coefficients

The sail is modelled as a flat plate: CL = 1.1 sin 2α and CD = 0.08 + 1.9 sin²α. Beyond about 45° the lift falls and the drag keeps rising, which is the stalled kite that dives.

Honest simplifications: the line is straight, weightless and has no drag (a real long line sags and adds drag, lowering the angle); the kite is a point with a fixed angle of attack set by the bridle; the coefficients are textbook flat-plate fits, not a measured kite; the wind is uniform with height (a real boundary layer is faster aloft). Gusts here move the kite through the same quasi-static balance.

What to try
  • Raise the wind from 2 to 14 m/s and watch the line elevation and tension; below the red U min line the kite cannot rise.
  • Make the kite heavier: the minimum flying wind grows with the square root of the mass.
  • Push the angle of attack past 40 degrees: lift drops and drag soars (stall).
  • Turn up the gust strength and see the tension swing roughly twice as fast as the wind.
Line elevation against wind speed
Lift, drag, weight and tension against wind speed
Lift and drag coefficient against angle of attack