Away from forcing, set . For a linear sinusoidal disturbance , the reduced equation gives
Since , the phase velocity is positive for every nonzero wavenumber. The group velocity is
Thus both the linear phase and wave packet travel downstream; the sign of does not introduce an upstream branch.
Now seek a permanent nonlinear wave with , for which the propagation velocity is . Substitution gives . Integration with vanishing far-field data gives
Multiplying by and integrating again, with zero integration constant, gives
Here , because and . A smooth nonzero wave approaching zero requires : for the right-hand side is negative at sufficiently small nonzero . At the allowed positive branch has no nonzero turning point, so it cannot form a smooth localized pulse.
When , the nonzero turning point is . The energy curve is positive between and zero and negative below , giving a homoclinic negative pulse. The positive branch has no turning point and cannot return to zero. Therefore
An explicit solution, also confirming smooth exponential tails, is
This establishes the opposite propagation directions in the annular displacement equation: linear waves move downstream while its localized nonlinear depression waves move upstream.
Let the layer occupy , with a free surface at and rigid base at . Write an SH-wave as . The equation and boundary conditions give
Thus and the guided SH modes between rigid and free planes have
The propagating branch has and . Hence the rigid-base approximation to Love waves predicts
At each threshold and . As frequency rises, the phase velocity decreases towards and the group velocity increases towards . Frequencies below have imaginary horizontal wavenumber and do not give propagating guided modes. The infinite threshold phase speed does not violate causality: the limiting group speed is zero. These quarter-wave thresholds differ from the actual Love-wave cutoff frequencies of an elastic substrate.
Write and , with . For the profiles below take , so agrees with the stated parameter; changing the sign of reverses the balanced meridional velocity but not the height profile. The linearized shallow water equations are
Taking the horizontal curl gives . Hence the signed linear shallow-water potential vorticity anomaly is conserved:
The initial data are independent of , so the solution remains independent of and . Differentiating continuity in time and using the zonal momentum equation gives
For a horizontal Fourier mode with wavenumber , put . The solution splits into a balanced component and inertia-gravity waves:
These waves have frequencies , phase velocity , and group velocity , whose magnitude is less than . They have zero perturbation potential vorticity and carry the unbalanced part away. On the unbounded line, the localized difference between the initial and balanced profiles disperses, leaving a local steady limit. No damping is needed for this local geostrophic adjustment; in a closed periodic domain, undamped waves would persist and a literal pointwise steady limit would generally not exist.
The bounded steady height satisfies the modified Helmholtz equation
Oddness removes the even homogeneous solution in the central region. The exterior solution is bounded and tends to the appropriate plateau. Matching both height and its first derivative at gives the geostrophic adjustment of a finite-width height ramp:
For example, writing the interior solution as , matching its slope to the decaying exterior at gives .
The steady meridional momentum equation gives , and the zonal equation gives the geostrophic balance . Thus
The height is odd and monotone, and the meridional current is even, with maximum for .
For , the initial ramp is narrow compared with the Rossby deformation radius. To leading order,
Near the origin the height rises with slope , rather than ; the current has width and peak . For , the central height remains nearly and the central velocity nearly . Around each end of the ramp there is a matching layer of width , with height correction of order ; the exterior current decays over the same width. At the current is approximately half its central value. In both limits the zonal current is zero. These are the broad rotational adjustment of a narrow disturbance and the weak edge adjustment of a broad disturbance, respectively.
Figure 1.
Balanced height and velocity profiles for narrow and wide initial ramps, with scales shown on each axis
. Details.
Use the energy normalization specified for the height energy: the linear total energy density is . The linear equations imply
For , let the potential energy loss mean the positive difference between the initial and final values, per unit transverse length. Although both absolute potential energies diverge on the infinite line, their difference is finite. The leading step approximation gives
The finite ramp changes this leading expression by a relative correction. The initial kinetic energy is zero and the final gain is
The remainder is energy carried away by the outgoing inertia-gravity waves. This explains why the ratio is less than one without invoking dissipation: conservation of energy includes the waves, not only the final balanced flow.
Let be the eddy momentum flux, the eddy density flux, and . The PDF's hydrostatic equation is ; the converted TeX mistakenly replaces the pressure derivative by a density derivative. With , define
The residual mean circulation is nondivergent because . Substituting in the original mean momentum and density equations gives the transformed Eulerian mean equations
with the unchanged geostrophic and hydrostatic balances. Here the Eliassen–Palm flux components are
The eddy buoyancy flux has been absorbed into the residual transport, while both types of wave forcing enter the momentum equation through the Eliassen–Palm flux divergence.
For geostrophic disturbances, the Taylor identity for quasi-geostrophic flux gives
For example, zonal averaging removes and converts the remaining horizontal and vertical terms in into derivatives of and , giving precisely the displayed fluxes.
Locally, for a basic flow with nonzero meridional PV gradient , the quasi-geostrophic wave pseudomomentum is . Multiplying the linear perturbation PV equation by gives
where is a PV source or sink. In a locally uniform conservative Rossby wave packet, . Thus the flux tracks group velocity rather than the generally different phase velocity, with a signed wave activity if .
The non-acceleration theorem for quasi-geostrophic waves states that statistically steady conservative waves, with no wave-activity sources, sinks or independent boundary forcing, produce no balanced mean acceleration. Their flux divergence vanishes. In the present stable, impermeable mean-flow problem the homogeneous residual-circulation equation then has the zero solution, so and . The Eulerian mean flow can still circulate because its eddy-induced correction need not vanish. Dissipation, absorption at a critical layer, time-dependent wave activity or boundary forcing produces a nonzero flux divergence and invalidates the non-acceleration conclusion.
Use incompressibility, negligible viscosity and surface tension, and an initially irrotational flow. Take the undisturbed free surface at and bed at . The velocity potential satisfies Laplace equation and . For a Fourier mode, write
The linear kinematic boundary condition and linear Bernoulli equation at the free surface are and . Eliminating gives the surface gravity wave dispersion relation
The rightward phase velocity and group velocity are
The phase velocity transports a crest; the group velocity transports a narrow-band envelope and its leading-order energy. For , and : deep-water surface gravity waves are dispersive. For , and , the nondispersive shallow-water dispersion relation. The boundary velocity controls the excited amplitude; it does not change the linear dispersion relation.
For a nonrotating inviscid Boussinesq fluid, start from , and
The resting background has and . Write , and . Keeping first-order terms gives
The PDF has a genuine sign error: its momentum equation uses a minus sign before despite defining . A lighter parcel has and accelerates upward, so the plus sign is necessary. Retaining both printed signs would yield negative squared wave frequency and exponential growth in a supposedly stable fluid; no oscillatory stable-wave dispersion relation follows from that inconsistent system. Alternatively one can define a downward density variable , but then its density equation must have .
For the consistent system, take a plane internal gravity wave proportional to , with . Incompressibility gives . Project the momentum equation perpendicular to the wavevector, eliminating pressure: . Combining with gives
On a smooth signed-frequency branch, the phase velocity and group velocity are
Their scalar product is zero. Equivalently, the dispersion relation is homogeneous of degree zero in , so Euler homogeneous function theorem gives . The phase velocity moves crests normal to their phase lines; the group velocity moves wave packets and energy along those lines. Their perpendicularity explains why following individual crests does not reveal the direction of energy propagation.
Assume , , constant , negligible rotation, dissipation and reflection from infinity, small and , and no wave overturning. The terrain is stationary, so laboratory frequency is zero and intrinsic frequency is . Propagation requires . Put
The kinematic boundary condition at the linearized bed is . The upward radiation condition selects the positive branch because . Thus
The internal-wave polarization and every other perturbation follow from this vertical velocity and the linear equations.
In the frame moving with the fluid, , the phase is , and
The intrinsic energy ray slopes upward and upstream, , along a constant-phase line of an internal gravity wave. At fixed intrinsic frequency the spatial wave equation is hyperbolic, with the two characteristic curve line slopes ; the radiation condition selects the upward ray of the appropriate horizontal propagation branch.
In the terrain frame, phase lines remain fixed and the pattern phase velocity is zero. A transported packet has
Its energy path slopes upward and downstream, , and need not coincide with a stationary phase line. One should not add to the chosen normal intrinsic phase velocity and call that the normal ground-frame phase velocity: tangential motion along a phase line is arbitrary; zero laboratory frequency makes the entire crest pattern stationary. The sketch distinguishes stationary crests, intrinsic characteristics and transported energy.
If , is imaginary and the bounded field is an evanescent wave; at the vertical group velocity vanishes and an ordinary upward radiation interpretation degenerates.
Figure 1.
Phase lines and energy rays of topographic internal waves in fluid and terrain frames, with rigid-lid reflection
. Details.
Use translating coordinates and a profile ; the background condensate remains at rest in the laboratory. Then , and the Gross–Pitaevskii solitary wave equation is
This is a coordinate translation of a traveling solution, rather than an additional phase boost to change the background flow.
Set with small real . Since , the real and imaginary linearized equations are
For a longitudinal sinusoid, choose and . Their coefficients obey
A nonzero solution therefore requires , giving the positive-direction phase velocity
Equivalently the time-dependent linear Bogoliubov spectrum is and . Its long-wavelength sound speed is , which becomes in physical units using . For a general wavevector , the stationary resonance is ; specifying only its magnitude does not determine the velocity unless its direction is also fixed. This sinusoidal dispersion describes linear radiation about the background, not an amplitude-independent dispersion law for every nonlinear solitary wave; localized subsonic waves do not require a real oscillatory far-field wavenumber.
Substitution of gives the dispersion relation . The phase velocity is , whereas the group velocity is . Thus nonzero-wavenumber crests move more slowly than their wave packet; the velocities coincide at zero wavenumber.
Fourier evolution gives , where . For the two nondegenerate stationary points are , . At these points and . Expanding the phase quadratically near each point and evaluating the oscillatory Gaussian integral gives the stationary phase method
For a real initial field, , so the two terms are conjugate. The approximation assumes a sufficiently smooth decaying amplitude; if a leading coefficient vanishes, the next stationary-phase terms determine that contribution.
For , everywhere. There are no real stationary points, so no leading propagating packet reaches such a ray. For a Schwartz amplitude, repeated integration by parts with makes the contribution for every fixed . With weaker data the decay rate depends on their regularity. This agrees with the minimum group velocity being .
The free surface is a material surface. For , the material derivative vanishes on . Since the velocity is , this gives the exact kinematic boundary condition for a free-surface graph
At the surface the pressure equals the constant atmospheric pressure. Absorbing that constant into the time-dependent potential gauge in Unsteady Bernoulli equation yields the exact dynamic boundary condition for an inviscid interface
There is no surface-tension term in this model.
Write and linearize in the small perturbation and the surface displacement. The base value is , and evaluation at the displaced surface can be replaced by evaluation at zero to first order. Thus
Incompressibility requires Laplace's equation . For , the complex perturbation satisfies this equation and decays with depth. Put and . The linear boundary conditions become
They are consistent precisely when
Consequently the two laboratory phase velocities of a deep-water gravity wave are
If propagation of a wave packet is intended, its group velocities are instead .
Take shear-horizontal waves with displacement . This is divergence-free, so the elastic equation reduces to . Rigid boundaries require at , giving modes , . With shear speed , the dispersion relation is
For , the phase velocity is and the group velocity is , with .
The kinetic energy density is . The only strains are and , together with their symmetric counterparts; thus the isotropic linear-elastic energy density is . Average over one temporal period and integrate across the layer. The sine- and cosine-squared transverse integrals are both , giving
The guided shear-horizontal mode has average equipartition after both operations; a time average at a fixed transverse point alone need not give equality.
In the Boussinesq approximation, replace density by a constant reference density in inertia and incompressible flow, retaining the small density departure only in the gravitational force. Write and subtract the resting hydrostatic pressure. The upward buoyancy perturbation acceleration and squared buoyancy frequency are
Thus stable density stratification has . Let henceforth denote the pressure anomaly divided by . The ideal, nonrotating Boussinesq equations are
The buoyancy equation follows by materially conserving the total buoyancy , where ; it does not assume constant .
For an -periodic flow of period , define . An infinite-domain average with vanishing end contributions works as well. The necessary pressure condition is no mean zonal pressure gradient, : periodic pressure satisfies it, whereas a pressure containing a term proportional to does not. Use incompressible flow to write the zonal momentum equation in conservative form,
Averaging its zonal derivative terms yields the exact Reynolds stress relation
For two-dimensional small disturbances about rest, the Linearized Boussinesq equations are , , , and . Differentiate the two momentum equations to eliminate pressure: . Differentiating in and using gives . One further time derivative gives
The equation remains valid for . No vertical derivative of was taken: .
For constant and , a plane internal gravity wave has
Both signs give the prescribed lower-boundary velocity. The radiation condition excludes energy arriving from infinity. At positive frequency, the vertical group velocity is
For a source below the fluid, energy must propagate upward, so the outgoing solution has , even though its vertical phase velocity is downward.
To obtain this selection causally, let and , and replace the constant amplitude by . The method of multiple scales treats as independent during differentiation: the carrier derivatives hold fixed, while holds fixed and holds fixed. Only after differentiating do we restrict to , . Acting on the complex wave, the operators become
With , the wave equation has residual
The zeroth-order term is the dispersion relation; the first-order term vanishes precisely when
If is the switched-on boundary amplitude, with for , the outgoing envelope is for . Its characteristics carry the boundary signal into initially undisturbed fluid. If , characteristics instead arrive from the upper half-space; zero initial disturbances and no incoming signal cannot establish the proposed boundary-forced wavetrain. This is the internal-wave envelope radiation condition.
The leading incompressible flow polarization gives . Hence, to second order in amplitude and leading order in the slow modulation,
There is no meridional transport here. Envelope transport gives , so an initially vanishing mean develops as
These are the leading expressions for internal-wave momentum deposition; higher slow-modulation corrections to the stress are beyond the displayed approximation. In particular, a spatially uniform fully established wavetrain has zero stress divergence, but the front has already produced its mean flow.
The mean wave energy density per unit mass follows from :
Thus . In the original frame the mean kinetic energy is . In a frame translating at , the undisturbed velocity is , and the change in mean kinetic energy is . Indeed at this order behind the front. Mean-flow energy is therefore essential at the same order as wave energy in the translating frame. This follows also from the frame transformation of energy, up to the fixed background constant, and is why conservation of momentum cannot be omitted from the moving-frame conservation of energy budget.
Let denote free-surface height and the water depth. The inviscid rotating shallow water equations with constant Coriolis parameter are
It is , not , that supplies the horizontal pressure gradient. For a fixed bottom, mass conservation equivalently gives .
Write for relative vorticity. Differentiate the second momentum equation in and the first in , then subtract. The pressure terms cancel. Expanding the differentiated advection terms gives
Consequently the absolute vorticity satisfies . Combining this with mass conservation yields exact shallow-water potential vorticity conservation:
A sloping bottom changes the depth and hence the stretching, but contributes no curl to the gravitational pressure force.
For the quasi-geostrophic approximation, choose constant reference depth , speed , and horizontal length . Require Rossby number , slow evolution on the advective time , smooth horizontal scales, and or smaller, where is the Rossby deformation radius. Write , , and . The leading momentum balance is geostrophic balance:
It gives , while we require and slopes on the chosen horizontal scale. Relative vorticity divided by is also . Thus
The derivative of the constant first term vanishes. In advecting the first-order anomaly, the ageostrophic flow contributes only at the next order. Therefore the shallow-water quasi-geostrophic potential vorticity equation is
This retains the balanced vortical branch, including Rossby waves driven here by the topographic potential-vorticity gradient. It filters the freely oscillating inertia–gravity branches of the full shallow water equations, and does not retain independent boundary Kelvin wave dynamics. Small Rossby number alone is insufficient for the reduction: fast waves must be absent at leading order, as in well-prepared balanced initial data.
In the channel take and measure the bottom anomaly from mid-channel: . Define . The resting potential vorticity is , and the linear Rossby wave equation is
For nonzero zonal wavenumber , wall conditions select
The modes are stationary. Write and take real for the following sketch. The total potential vorticity is . For a contour whose undisturbed position is , its small meridional displacement is
Thus potential-vorticity conservation says a northward displacement in a positive background gradient carries a negative anomaly, . Potential-vorticity inversion turns this into positive and anticyclonic motion around the bulge. At a positive cosine crest, is northward on its western flank and southward on its eastern flank. Advection raises the contour on the west and lowers it on the east, so the crest moves west. Algebraically, and give , the same phase velocity as above. For all propagation directions reverse.
Figure 1.
Potential-vorticity contour displacement and westward Rossby-wave propagation for a positive background gradient
. Details.
For a square basin use a nonzero-frequency normal mode , with on all walls. Its equation is
Set and . Substitution cancels the first derivative and gives
The square's Dirichlet Laplacian eigenfunctions are , with positive integers. Consequently the square-basin topographic Rossby mode has
For , the positive-frequency branch therefore tends to as , as required. The negative-frequency solution is its complex-conjugate representation for a real disturbance; the physical frequency magnitude is .
Consider a nonreal phase velocity , so never vanishes. Substitute into the Rayleigh equation for inviscid shear flow. Differentiating cancels the two terms involving , leaving
For , the wall condition on normal velocity gives , hence , at both walls. Multiply by and use integration by parts to obtain the weighted identity for Howard's semicircle theorem:
For a nonzero normal mode, . The imaginary and real parts of this identity give, respectively,
Since , these imply
The first equation says that is a positive weighted mean of , and consequently . The division by is essential: the weighted-mean assertion concerns nonreal modes. A neutral mode may have a critical level where and the substitution for is singular.
Pointwise, . Integrating against the nonnegative weight and substituting both identities yields
Completing the square proves Howard's semicircle theorem:
Thus all nonreal phase velocities lie in the closed disk with the real interval as diameter. For the convention and , exponentially growing normal modes occupy its upper semicircle, while decaying modes occupy its lower semicircle.
Away from the velocity-profile corners, and an unstable normal mode satisfies . On the upper half of the jet write
The exterior solution is selected by decay at infinity. From the given velocity components, the perturbation pressure is
Continuity of normal velocity and pressure therefore gives continuity of and pressure matching at a piecewise-linear shear interface:
At the slope of jumps from to zero. Using yields
The lower interface then follows by parity.
For the even sinuous mode of a planar jet, the derivative can jump at the center: being an even function does not require the one-sided derivative to vanish. The slope jump at is , whereas . Thus
Substitute into the upper-interface relation. With , division by and multiplication by give
Collecting powers of the phase velocity gives the required dispersion relation:
These equations can also be treated as a homogeneous two-by-two system in , avoiding division by any potentially zero amplitude or phase-velocity factor.
For the odd varicose mode of a planar jet, , so ; the central pressure matching at a piecewise-linear shear interface is automatic. The upper-interface equation becomes , and therefore
This phase velocity is real for every , so the discrete varicose mode of a planar jet is neutral and there is no exponentially unstable odd mode.
To determine the unstable even modes, factor the reduced discriminant of the quadratic:
The second factor vanishes at zero and has derivative for , so it is positive there. The first factor starts at , is strictly increasing, and tends to infinity. It therefore has one positive zero . The even phase velocities are
It follows that
For , one member of the complex conjugate pair grows at rate and the other decays. At the speeds merge and there is no exponential growth; for both speeds are real. This is inviscid instability of a triangular jet. The unstable sinuous mode of a planar jet also satisfies Howard's semicircle theorem with and : its speed lies in the upper half-disk centered at with radius .
Figure 1.
Triangular jet profile and unstable sinuous phase velocities inside the Howard semicircle
. Details.