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Consider an incompressible, axisymmetric jet with surface . Once the axial velocity is specified, continuity determines the radial velocity. Requiring regularity at the axis removes the integration constant, and the surface kinematics then give conservation of cross-sectional area.

We use dimensional coordinates, as in the leading-order derivation. Primes denote . If , the dimensional powers of carry the slender ordering; no additional powers of multiply them.

1. Integrate continuity from the axis

Axisymmetric incompressibility requires

Expand the axial velocity as

where the coefficients depend on and . Substitution into continuity gives

Integrating with respect to ,

A nonzero would give a singular velocity at the axis. Regularity therefore requires , giving

The radial velocity is odd in , as required by axis regularity. In particular, a positive axial strain rate produces an inward radial velocity.

2. Apply the surface kinematics

The surface moves with the liquid, so

At leading order this becomes

Multiplying by and collecting the axial derivative gives

This is the leading continuity equation used in the slender-jet model.

3. Retain the first correction to the flux

Keeping the axial-velocity correction gives

Multiplication by now yields

We can check the coefficient by integrating the axial velocity over a section. The exact volume flux is

so its expansion is

The exact area balance is . Truncating this flux after recovers the second-order equation above. Under the regular slender ordering, the contribution is a relative correction, while the contribution is relative . Consequently, the centreline velocity and the mean velocity agree only at leading order.

The corresponding momentum and traction corrections are given in the second-order derivation.