Flows and fields

Where a vortex stops

Four criteria decide where a vortex ends, and in two dimensions three of them are the same criterion. The fourth is a knob. And the one that is not a knob is not objective: a co-rotating pair of vortices occupies two per cent of a window to one observer and twenty-five to another.

Worth reading first: Spin is not the same as going round · The count a pattern cannot break.

Every essay on this site that says the vortex has been relying on a reader to see one. For a point vortex that is fine, because a point vortex has no size. It stops being fine the moment a figure shades a region and calls it the core, because the shading needs a boundary and the equations do not supply one.

Vorticity is a field. A vortex is an object. Turning the first into the second is a decision, and this essay is about who makes it.

Four criteria, and three of them are one

The literature offers four local tests. Written for the velocity gradient u\nabla\mathbf u decomposed into its symmetric part D\mathsf D and antisymmetric part W\mathsf W:

Q=12(W2D2),Δ=tr24det,λ2 of D2+W2,Q = \tfrac12\big(|\mathsf W|^2 - |\mathsf D|^2\big),\qquad \Delta = \mathrm{tr}^2 - 4\det,\qquad \lambda_2\ \text{of}\ \mathsf D^2 + \mathsf W^2,

with a vortex where Q>0Q > 0, or where Δ<0\Delta < 0, or where λ2<0\lambda_2 < 0. They are introduced as three ideas: rotation beating strain, eigenvalues going complex, a pressure minimum in the plane perpendicular to the vortex.

In two dimensions, incompressibly, they are one idea. For a trace-free gradient [[a,b],[c,a]][[a,b],[c,-a]],

Q=(a2+bc)=detuexactly,Δ=4Q,Q = -(a^2 + bc) = \det\nabla\mathbf u\quad\text{exactly},\qquad \Delta = -4Q,

so all three change sign on one curve — measured at 101610^{-16} over sixty sample points on both sides of it. And that curve is the boundary between the points where the local flow pattern is a focus or a centre and the points where it is a saddle, which is exactly the classification topology applies to stagnation points, applied at every point instead of only at the special ones.

Four names for one curve. In two dimensions, for an incompressible flow, the four local vortex criteria in common use change sign on exactly the same curve — and that curve is the boundary between the points where the local flow pattern is a focus and the points where it is a saddle, which is the classification this collection already applies to stagnation points. Q and the determinant of the velocity gradient agree to one part in ten thousand million million over sixty sample points on both sides of the boundary.
Fig. 1 Four names for one curve, and the measurements that say so. Q and the determinant of the velocity gradient agree to one part in ten thousand million million.

That is worth knowing before choosing between them. A paper comparing QQ and λ2\lambda_2 on two-dimensional data is comparing a quantity with itself.

The one that really is different

The vorticity magnitude is not one of them, and the cleanest demonstration is the flow this collection uses for every stability argument.

A parallel shear layer, u=ΔUtanh(y/h)u = \Delta U\tanh(y/h), has vorticity peaking at the centre and falling away on both sides. It has Q=0Q = 0 at every point, because in a parallel shear the strain and the rotation have exactly equal magnitude — the velocity gradient has one non-zero entry, which splits evenly between the two parts.

So a vorticity threshold calls the entire layer a vortex and QQ calls none of it one.

A shear layer, which one criterion calls a vortex and the other does not. Across a shear layer the vorticity is large — it peaks at the centre and is the whole reason the layer is interesting — and Q is negative everywhere, because the strain is exactly as large as the rotation at every point of a parallel shear. A vorticity threshold calls the entire layer a vortex. Q calls none of it one. Neither answer is wrong; they are answers to different questions, and only one of them is about whether the local flow pattern closes on itself.
Fig. 2 Across a shear layer, the vorticity peaks and Q is negative everywhere. Neither answer is wrong; they answer different questions, and only one of them is about whether the local flow closes on itself.

Neither is a mistake. They are answers to different questions, and the question a reader usually has in mind — is there a swirling structure here? — is the second one. The habit of contouring vorticity and calling the result the vortices is what makes a shear layer look, in a great many published figures, like a row of vortices before it has rolled up into any.

Where one vortex ends

Now the case that has a real answer. A Lamb–Oseen vortex — the one everybody means by a vortex with a core — has a Gaussian vorticity distribution and a swirl that rises linearly, peaks, and falls off as 1/r1/r.

Its vorticity is positive at every radius, so a vorticity threshold puts the edge wherever the threshold is put. Its QQ changes sign exactly once, at

r=1.1209rc,r = 1.1209\,r_c,

and that radius encloses 71.5371.53 per cent of the circulation. It is a property of the flow. Nothing was chosen.

Q and the vorticity along a radius of one vortex. Two candidate measures of where the vortex is, along a radius of a Lamb–Oseen vortex. The vorticity is a Gaussian: positive at every radius, so a threshold on it puts the edge wherever the threshold is put. Q — the excess of rotation over strain — changes sign exactly once, at 1.121 core radii, and that radius is a property of the flow rather than of the person drawing it. Inside it, 71.5 per cent of the circulation.
Fig. 3 Q, the vorticity and the enclosed circulation along a radius. One of these curves has an edge in it.

That is as good as it gets, and it is worth pausing on how good it is: a definite radius, a definite fraction of the circulation, and no free parameter. The rest of this essay is about the two ways it is usually thrown away.

The first way: a level

Almost nobody plots Q>0Q > 0. What gets plotted is Q>cQ > c for some cc, because the Q>0Q > 0 set in a turbulent field is enormous and connected and shows nothing.

The consequence is arithmetic. Sweeping cc from zero to seven-tenths of QQ’s peak takes the radius of the region from 1.121rc1.121\,r_c down to 0.4160.416, and the enclosed circulation from 71.571.5 per cent to 15.915.9.

The size of the vortex, against a number nobody can choose. Left: the region Q > c for six values of c, from zero — the only level with any claim to being the flow's own — up to seven-tenths of Q's peak. Right: the fraction of the vortex's circulation inside each of those rings. It runs from 71.5 per cent down to 15.9. Every published measurement of a vortex's size, its area, or how much circulation it contains has one of these numbers behind it, and the number is a choice.
Fig. 4 The region Q > c at six levels, and the circulation each contains. Every published measurement of a vortex’s size, area or strength has one of these numbers behind it.

There is no principled way to pick cc. It is usually chosen so that the picture looks like what the author expects, and the resulting figures are then compared between papers that chose differently. The honest presentation is to state the level and the fraction of circulation it encloses, and this collection now does.

The second way: a frame

The deeper problem is that QQ is not objective. The velocity gradient’s antisymmetric part shifts by the observer’s own rotation rate, so QQ shifts too, and where the vortices are becomes a question with a camera in it.

Take two Lamb–Oseen vortices side by side. They orbit their common midpoint, so the natural frame in which to look at them is the one that turns with the pair — which is exactly what an analyst does with a rotor, a stirred tank or a vortex pair.

The same pair of vortices, from two observers. Instantaneous streamlines of a co-rotating pair of Lamb–Oseen vortices, drawn in the laboratory and in a frame turning at the rate the pair orbits. The two pictures share the vorticity field exactly and share nothing else: closed orbits appear where there were open streamlines, and the outer flow reverses. This is the same field whose vortex-criterion maps are compared in the next figure, and the difference between those maps is already visible here.
Fig. 5 Instantaneous streamlines of a co-rotating pair, in the laboratory and in the frame that turns with it. The vorticity fields are identical and the pictures share nothing.

In the laboratory the Q>0Q > 0 set is two compact cores, of total area 2.00 in the window drawn. In the co-rotating frame it is those two cores plus everything beyond a certain distance, of total area 24.94 — because fluid that is nearly at rest in the laboratory is going round in a rotating frame, and QQ cannot tell the difference between that and a vortex.

Where the vortices are, according to two observers. The set Q > 0 for a co-rotating pair of Lamb–Oseen vortices, drawn in the laboratory and in the frame that turns with the pair. The laboratory sees two compact cores. The rotating observer sees the same two cores plus everything beyond a certain distance — because fluid that is nearly at rest in the laboratory is going round in a rotating frame, and Q cannot tell the difference. The Q-criterion is not objective, and the twelvefold difference in area between these two panels is what that costs.
Fig. 6 The Q = 0 contour in both frames. A twelvefold difference in area, with the same vorticity field in both panels.

The far field is not a vortex. Every criterion in the list says it is, to an observer who is turning.

Why the collapse happens, and what it means

The identity Q=detuQ = \det\nabla\mathbf u is worth an extra minute, because it explains why the three criteria were ever thought to be different.

In three dimensions the characteristic polynomial of the velocity gradient has three invariants — PP, QQ and RR — and for an incompressible flow PP vanishes, leaving two. QQ is the second of them and detu\det\nabla\mathbf u is the third, so they are genuinely independent quantities and the criteria built from them are genuinely different tests. The whole QQRR plane, with its famous teardrop of turbulence statistics, exists because the two are independent.

In two dimensions there is only one non-trivial invariant, so every scalar built from a trace-free 2×22\times2 matrix that is invariant under rotation must be a function of it. Three tests that differ in three dimensions therefore have no room to differ in two. That is not a coincidence being explained away; it is a statement about how much information a plane velocity gradient contains, which is three numbers after the trace is removed and one number after rotations are quotiented out.

The practical consequence: a two-dimensional study cannot distinguish between the criteria and should not claim to, and a three-dimensional study that finds them agreeing has learned something rather than nothing.

What a reader is usually asking

The criteria answer a question about u\nabla\mathbf u at a point. Almost nobody wants that answer.

What a reader looking at a vortex figure usually wants to know is one of:

Which fluid stays together? That is a question about trajectories over an interval, and the answer is a material region — the objects advection is about. It has no pointwise definition at all: whether two parcels stay together depends on how long is meant by stay.

Where would a tracer accumulate? In an incompressible flow, nowhere — a material region keeps its area — so the question is really about where a tracer appears to accumulate over the time somebody is watching, which again has an interval in it.

What carries the circulation? This one has a good answer and it is the one this essay recommends quoting: the fraction of the total circulation inside a stated contour. It is a conserved quantity, it is frame-independent under a boost, and it is far less sensitive to the level than the area is.

And what will happen next? Which no diagnostic answers, because a diagnostic is a function of the instantaneous field and the future is not.

Q and the vorticity along a radius of one vortex. Two candidate measures of where the vortex is, along a radius of a Lamb–Oseen vortex. The vorticity is a Gaussian: positive at every radius, so a threshold on it puts the edge wherever the threshold is put. Q — the excess of rotation over strain — changes sign exactly once, at 1.121 core radii, and that radius is a property of the flow rather than of the person drawing it. Inside it, 71.5 per cent of the circulation.
Fig. 7 The same profile for a vortex of twice the circulation. Every curve scales and the Q = 0 radius does not move, because it is set by the shape of the vorticity distribution rather than by its strength.

The thing that does not move

There is one quantity in all of this that survives every objection, and it is the one this collection has been using since its second essay.

Circulation. It is an integral of vorticity over an area, it is unchanged by a Galilean boost, it is conserved for a material loop in an inviscid fluid, and it needs no threshold and no criterion — only a loop, which the analyst still chooses but whose choice is visible in the answer rather than hidden in it.

That is why every result in this collection about vortices is stated in terms of circulation and not in terms of a core: the lift on a wing, the speed of a vortex pair, the induced drag of a wake are all Γ\Gamma-statements. The core radius appears in exactly one place — the logarithm in a vortex ring’s self-induced speed — and that essay is careful to assert the slope of the dependence rather than the value, for precisely the reason this one is about.

A worked disagreement

To make the level’s cost concrete, here are two entirely reasonable analysts looking at the same Lamb–Oseen vortex.

The first plots Q>0Q > 0 and reports a vortex of radius 1.121rc1.121\,r_c containing 71.571.5 per cent of the circulation and an area of 3.95rc23.95\,r_c^2.

The second plots QQ greater than a fifth of its peak — a common choice, made because it renders well — and reports a vortex of radius 0.832rc0.832\,r_c containing 50.050.0 per cent of the circulation and an area of 2.17rc22.17\,r_c^2.

Neither has done anything wrong. Their radii differ by thirty-five per cent, their areas by a factor of 1.8, and their circulations by a factor of 1.4. If the two numbers being compared were a measured core size and a theoretical one, the comparison would be reported as a discrepancy and somebody would go looking for the physics in it.

What is not in the velocity field

Three things, and the essay is the list.

A threshold, which nothing supplies and which moves the reported size and strength over most of their range.

A frame, which nothing supplies and which can multiply the reported area by twelve.

And an idea of what a vortex is for. The criteria answer is the local flow pattern closed, which is a question about u\nabla\mathbf u at a point. A reader usually wants to know something else: which fluid stays together, where a tracer accumulates, what a following observer would see as coherent. Those are questions about trajectories over an interval, and no pointwise criterion answers them.

That last is not a complaint about the criteria; it is a statement about what they are. Material lines stop being pulled apart exactly on the Q=0Q = 0 surface — which is the best justification QQ has and is derived rather than asserted — but the derivation is for the rotation of the strain axes relative to the material, and an observer’s own rotation is added to it in every published QQ field.

The criteria that do not have a frame in them

The two objections in this essay — a threshold nobody supplies and a frame nobody states — are not unanswerable. There is a family of definitions built to remove both, and what they cost is exactly the thing the essay has been circling: they are not diagnostics of a snapshot.

The construction begins by noticing why QQ moves with the observer. An observer’s own rotation adds the same rigid amount to the vorticity everywhere, so a quantity built from the deviation of the vorticity from its instantaneous spatial mean cannot see it. Average that deviation along a fluid trajectory over an interval, and the result is a scalar attached to each parcel that is the same for every observer, however they are turning.

A vortex is then defined as a region of large values of that scalar, and the threshold problem is attacked separately: rather than choosing a level, take the outermost level set that is still convex around each local maximum. Convexity is the discriminating condition, because a boundary that has begun to filament — to be drawn out into the surrounding strain — stops being convex, and filamenting is precisely what a coherent vortex boundary is defined as not doing.

What comes out is a boundary that is objective, nearly threshold-free, and material: it is made of the same fluid at the end of the interval as at the beginning. Applied to ocean eddies, boundaries of this kind retain their water for months, where the contours drawn from instantaneous fields leak steadily — which is the practical form of the essay’s complaint, since the whole point of calling an eddy an object is that it carries something along.

And the price is the interval. These definitions need trajectories over a stated span of time, so they are not functions of the velocity field at one instant, and the answer depends on how long “coherent” is taken to mean. That is a free parameter, exactly as the level was — with the difference that it is a physically meaningful one, chosen by the question being asked, and visible in the answer rather than hidden inside a colour scale.

Which is the honest resolution rather than an escape. There is no snapshot diagnostic of a material object, and the criteria in this essay are snapshot diagnostics.

What an honest figure does

Four habits, and this collection now keeps all four.

Name the criterion. A vortex is not a measurement. The region where QQ exceeds five per cent of its peak, in the laboratory frame is.

Name the level and what it encloses. The fraction of circulation inside a contour is a far more stable number than the contour’s area, and it is the one a reader can compare across papers.

Name the frame, and say whether the answer moves if it changes. For an isolated vortex in a stream it does not much; for anything rotating it does.

And prefer Q=0Q = 0 when the flow allows it. For a single core it is a real boundary with a real enclosed circulation, and it is the only level in the family that is a property of the flow rather than of the author.

The Q-criterion for a flow with no rotation in it, against the observer's spin. Pure straining flow has no vorticity anywhere, so the Q-criterion — the excess of rotation over strain — is negative everywhere and no part of it is a vortex. An observer rotating fast enough measures a positive Q at the same point in the same flow, and the crossing is at a rotation rate equal to the strain rate. Whether a region of a flow contains a vortex, on this criterion, is a question with an observer in it.
Fig. 8 Q for a flow with no rotation at all, against the observer’s own rotation rate. This is the objectivity failure that the two-frame comparison above is a picture of.

What the criteria are actually for

None of this makes them useless, and it is worth saying what they are good at.

They are excellent at finding structures in a large data set — as a detector, where the threshold’s arbitrariness costs nothing because the question is where to look rather than how big something is. They are good at counting, provided the count is robust to the threshold, which is a thing that can be checked and rarely is. And they are bad at measuring, because every measurement they produce moves with the level.

That maps onto the same distinction this collection has drawn about what a photograph of a flow shows: a visualisation is evidence that something is there and is very poor evidence about how large it is. The criteria are a numerical visualisation and inherit exactly that property.

The model limit

Two, and the second is the one that matters at scale.

Everything computed here is two-dimensional, and the collapse of three criteria into one is a two-dimensional result. In three dimensions QQ, Δ\Delta and λ2\lambda_2 are genuinely different functions and identify genuinely different sets — usually similar, occasionally not, and the cases where they differ are the interesting ones. The vorticity-threshold objection survives unchanged.

There is also a quiet assumption in the whole framework that the flow is incompressible, and it is doing work. The trace of the velocity gradient is what was set to zero to make QQ equal the determinant, and a compressible flow has a divergence which enters every one of these quantities. In a shock-containing flow the criteria pick out the shock as enthusiastically as they pick out a vortex, and the usual fix is to subtract the dilatational part first — which is the decomposition of the previous essay with all of its own ambiguity attached.

And the Lamb–Oseen vortex used throughout is an isolated, axisymmetric, steady structure, which is the easiest possible case. A vortex in a turbulent flow is none of those things: it is being strained by its neighbours, it is not axisymmetric, and it is changing while it is being measured. The Q=0Q = 0 radius that is a clean property of the flow here is, there, a surface that moves while the measurement is being made — and the level, the frame and the averaging interval all come back.

What links here

Computed from the collection rather than written here: the essays that point at this one.

Reads more easily once this is understood

Essays that name this one as worth reading first.

Shares its objects with

Essays naming at least two of the same things, that neither author linked.

Named objects

A dashed tag is an object no other essay names yet.

CirculationFlow visualisationMeasurementModel limitObjectivityQ-criterionRotating frameShear layerStrain rateVortexVortex coreVorticity