Core idea

For a smooth three-dimensional solution of the with constant ν\nu, the satisfies

tω+(u)ω=(ω)u+νΔω+×f.\partial_t\omega+(u\cdot\nabla)\omega =(\omega\cdot\nabla)u+\nu\Delta\omega+\nabla\times f.

The term (ω)u(\omega\cdot\nabla)u is vortex stretching and tilting. For the Euler equations, take ν=0\nu=0.

Derivation

Take curl of the momentum equation. The pressure gradient has zero curl, curl commutes with time derivatives and the Laplacian, and

×((u)u)=(u)ω(ω)u\nabla\times((u\cdot\nabla)u) =(u\cdot\nabla)\omega-(\omega\cdot\nabla)u

when u=0\nabla\cdot u=0. The identity follows by expanding components, or by writing (u)u=(u2/2)u×ω(u\cdot\nabla)u=\nabla(|u|^2/2)-u\times\omega.

Planar flows

For a two-dimensional velocity independent of the third coordinate, the stretching term vanishes. The scalar vorticity then obeys a transport-diffusion equation with the corresponding scalar curl of the force.

References