Choose tangential to the solid boundary and locally along the outer inviscid streamlines, and let be the inward normal coordinate. Write and for the corresponding tangential and normal velocity field components, for the outer tangential velocity, and for the kinematic viscosity.
For a layer of streamwise scale and thickness , incompressible flow gives
so and . The normal Navier-Stokes equation then gives to leading order, while the outer Euler equations give
In the tangential Navier-Stokes equation, streamwise viscous diffusion is smaller than normal diffusion by . Retaining the leading inertial and normal-diffusion terms produces the Prandtl boundary-layer equation
It is supplemented by at a stationary wall and on matching to the outer flow.
The basic state has velocity field
and buoyancy . For disturbances independent of , the linearized equations are
Substituting a plane wave proportional to and eliminating , , and gives the dispersion relation
Thus the requested coefficients are
An instability exists precisely when some wavenumber pair makes . Since the Brunt–Väisälä frequency satisfies , this is possible exactly when
The basic relative vorticity is , so its absolute vorticity is . Its Ertel potential vorticity is therefore
The instability criterion can consequently be written as : the vertical absolute vorticity has the opposite sign to the planetary vorticity. This is inertial instability, approached most directly by disturbances with .
Stagnation point 2026-09-29
A stagnation point of a fluid flow is a point at which the velocity field vanishes. For a two-dimensional streamfunction, it is a critical point satisfying both first spatial derivatives of the streamfunction equal to zero.