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LeanPool.CIVAxisymmetric.Identities.Vorticity

The vorticity and the circulation of an axisymmetric field #

The Cartesian curl curlComp u i of a field is written with CKN's classical spatial partial derivatives. For a smooth axisymmetric field, on the meridional plane {x₂ = 0} away from the axis, its components are the cylindrical ones of eq:aniso:vorticity, ω_r = -∂_z u_θ, ω_θ = ∂_z u_r - ∂_r u_z, ω_z = ∂_r u_θ + u_θ/r; the middle one is the definition itself, the outer two use the θ-derivative relations of design note R4. The circulation Γ = r u_θ of eq:aniso:vorticity is x₁ u₂ on that plane.

The i-th Cartesian component of the curl, (∇ × u)_i = ∂_{i+1} u_{i+2} - ∂_{i+2} u_{i+1} with the indices read cyclically.

Equations
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Instances For

    The second Cartesian component of the curl is ∂₃u₁ - ∂₁u₃; on the meridional plane this is the azimuthal vorticity ω_θ = ∂_z u_r - ∂_r u_z of eq:aniso:vorticity.

    On the meridional plane, off the axis, the first component of the curl of a smooth axisymmetric field is the radial vorticity ω_r = -∂_z u_θ of eq:aniso:vorticity.

    On the meridional plane, off the axis, the third component of the curl of a smooth axisymmetric field is the vertical vorticity ω_z = ∂_r u_θ + u_θ/r of eq:aniso:vorticity.

    On the meridional plane the circulation Γ = r u_θ of eq:aniso:vorticity is x₁ u₂.