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3.4.2 Vortex cylinder theory

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In the limit of an infinite number of blades and ignoring expansion the tip vortices form a cylinder with surface vorticity that follows a helical path with a helix angle ϕt, which is the same as the flow angle at the outer edge of the disc. The strength of the vorticity is , where Δn is the distance along the tube surface in a direction normal to ΔΓ between two successive tip vortices. g has components gθ in the azimuthal direction and gx in the axial direction. Due to gθ the axial (parallel to the axis of rotor rotation) induced velocity ud at the rotor plane is uniform over the rotor disc and can be determined by means of the Biot–Savart law as

(3.27)

In the far wake the axial induced velocity uw is also uniform within the cylindrical wake and is

(3.28)

The ratio of the two induced velocities corresponds to that of the simple momentum theory and justifies the assumption of a cylindrical vortex sheet.

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