Dynamics

The wind that brings its own frequency

Every other load in this subject arrives at whatever rate it happens to arrive at. Vortex shedding arrives at a rate set by the wind speed — so for any chimney, mast or cable there is always a wind speed at which the shedding matches the structure exactly, and it is a breeze rather than a storm.

Assumes The wind is a spectrum and The only thing that stops it.

A steel chimney 1.2 m across stands on a factory roof. It has been checked for the fifty-year wind, its foundation bolts are sized, and it is entirely adequate.

In a light breeze it swings sideways — across the wind, not along it — by about 180 mm, and does so for hours at a time, several times a month.

Lock-in: the frequency the wind sheds at, and what it does to the chimneyA 1.2 m cylinder at 0.9 Hz. Vortices leave it at St·U/D, so the critical speed at which they match the structure is 6 m/s — a breeze, met many times a year rather than once in fifty. The upper panel shows the shedding frequency locking on to the structure across a band from 5.1 to 7.8 m/s; the lower shows the amplitude that results. At a Scruton number of 11.2 the peak amplitude is 180.94 mm, which is 15% of the diameter. 024681012141618200123shedding frequency (Hz)1.2 m across · St 0.18 · 0.9 Hzlock-in6 m/s02468101214161820050100150200wind speed (m/s)cross-wind amplitude (mm)0.40% damping — Sc = 11.2, peak 180.94 mm
Fig. 1 The mechanism, in two panels. Above: the frequency at which vortices leave the cylinder, which follows St·U/D — a straight line through the origin — so it crosses the structure’s own 0.9 Hz at 6.0 m/s. Inside a band around that speed the line breaks and the shedding locks on to the structure. Below: the resulting cross-wind amplitude, which peaks in that band at 181 mm and is negligible everywhere else.

Nothing about that behaviour is visible in a wind pressure. The load that causes it is small, it is at right angles to the wind, and the speed at which it matters is one that a design calculation never looks at.

Why a shedding frequency exists at all

Flow past a bluff body separates, and behind it the two shear layers roll up into vortices — alternately, one from each side, in a regular street. Each vortex leaves a low pressure behind it as it forms, so the sideways force on the body reverses with every shed vortex, and the body is pushed alternately left and right at the shedding frequency.

That frequency is remarkably orderly across a wide range of conditions:

fs=StUDf_s = \frac{St \cdot U}{D}

with StSt the Strouhal number, about 0.2 for a circular cylinder over several decades of Reynolds number, and about 0.11 to 0.15 for the rectangular shapes buildings are. The number is a property of the shape, not of the fluid or the speed, which is what makes it useful.

Two consequences follow immediately and neither has an analogue anywhere else on this site.

The excitation frequency is proportional to the wind speed. Every other load’s timing is set by something outside the structure — a machine’s speed, a person’s pace, a fault’s rupture. This one is set by a variable that sweeps continuously through every value from zero upwards as the weather changes.

Therefore the coincidence is guaranteed. Setting fs=f0f_s = f_0 gives the critical speed Ucrit=f0D/StU_{\text{crit}} = f_0 D / St, and for this chimney that is 6.0 m/s — a fresh breeze. It is not a question of whether the structure meets its critical speed but of how often, and the answer is measured in hundreds of times a year.

The shedding frequency against wind speed, and where it stops following itVortices leave a 1.2 m cylinder at St·U/D, which is the faint straight line, so there is always a wind speed at which they match the structure's own 0.9 Hz — here 6 m/s, which is a breeze. Inside a band from 5.1 to 7.8 m/s the shedding abandons the line and locks on to the structure, driven by the structure's own motion.024681012141618200123wind speed (m/s)shedding frequency (Hz)1.2 m across · St 0.18 · 0.9 Hzlock-in6 m/s
Fig. 2 The frequency panel alone, showing the step. Outside the band the shedding follows the Strouhal line and knows nothing about the structure; inside it, the shedding frequency is the structure’s own — flat, over a range of wind speeds from 5.1 to 7.8 m/s. The wind speed changed and the excitation frequency did not.

Lock-in, and why it is not resonance

The flat section in that figure is the part that makes vortex shedding a separate subject.

As the wind approaches the critical speed the cylinder begins to move, and a moving cylinder organises its own wake: the vortices shed in step with the motion rather than in step with the flow. Over a band of roughly ±25% around the critical speed the shedding abandons the Strouhal relationship entirely and follows the structure. Wind tunnel measurements show this as a plateau, and full-scale measurements show it as a structure that oscillates steadily while the wind speed wanders.

That is not a resonance in the sense the earlier essays used. In a resonance the excitation is fixed and the structure happens to respond strongly; here the structure changes the excitation. The load is a function of the response, which means:

  • the response cannot be found by multiplying a force by a magnification factor, because there is no force independent of the response to multiply;
  • the amplitude is limited by nonlinearity in the fluid rather than by damping alone, so it does not grow as 1/2ζ1/2\zeta indefinitely;
  • the band is wider than any resonance peak, because the structure drags the excitation along with it rather than waiting for it to arrive.

It is the same disqualification that removes the magnification factor from the crowd on a footbridge, and lock-in is the mildest member of a family whose other members are considerably worse — the essay on self-excitation takes that family as a whole.

The Scruton number, which is the whole design answer

The amplitude that results is inversely proportional to one dimensionless group:

Sc=4πmζρD2Sc = \frac{4\pi m \zeta}{\rho D^2}

with mm the mass per unit length and ρ\rho the air density. It compares how much the structure weighs and dissipates against how much air it is disturbing, and the practical rule is that above about 20 the response is small and below about 10 it is not.

The cross-wind amplitude through the lock-in bandA 1.2 m cylinder at 0.9 Hz. Vortices leave it at St·U/D, so the critical speed at which they match the structure is 6 m/s — a breeze, met many times a year rather than once in fifty. At a Scruton number of 11.2 the peak amplitude is 180.94 mm, which is 15% of the diameter. At 0.80% damping the Scruton number is 22.3 and the peak is 90.47 mm — the amplitude is inversely proportional to it, and mass and damping enter it only as their product.02468101214161820050100150200wind speed (m/s)cross-wind amplitude (mm)0.40% damping — Sc = 11.2, peak 180.94 mm0.80% damping — Sc = 22.3, peak 90.47 mm
Fig. 3 The same chimney at 0.4% and 0.8% damping. The Scruton number goes from 11.2 to 22.3 and the peak amplitude halves, from 181 mm to 90 mm. Nothing else changed — the critical speed is identical, the band is identical, and the whole difference is a factor of two in a quantity that could be supplied by a single damper.

Mass and damping enter only as their product, which is the design statement and is not obvious from the equation of motion. It means a heavy structure needs no damping and a light one cannot be rescued by stiffening:

The cross-wind amplitude through the lock-in bandA 1.2 m cylinder at 0.9 Hz. Vortices leave it at St·U/D, so the critical speed at which they match the structure is 6 m/s — a breeze, met many times a year rather than once in fifty. At a Scruton number of 111.7 the peak amplitude is 18.09 mm, which is 2% of the diameter. 0246810121416182005101520wind speed (m/s)cross-wind amplitude (mm)0.40% damping — Sc = 111.7, peak 18.09 mm
Fig. 4 The same chimney in concrete rather than steel — ten times the mass per metre, the same damping. The Scruton number is 111.7 and the peak amplitude is 18 mm on a 1.2 m cylinder. A masonry or concrete chimney essentially does not do this, which is why the problem arrived with welded steel construction.

Stiffening changes f0f_0, which changes the critical speed and moves the problem to a different wind — it does not remove it. That is a genuinely different design logic from everything else in this collection, where stiffness is the usual lever and depth is the cheapest thing to buy.

There is one exception, and it is worth naming because it is the design decision most often taken. Raising the frequency far enough moves the critical speed above the range the site actually experiences — for a short, stocky mast the critical speed can be pushed to 25 m/s, which occurs rarely and briefly, and the fatigue count collapses. So stiffness does help, not by reducing the response but by making the episodes rare. That is a different argument from the one stiffness usually wins, and it depends entirely on the wind statistics at the site rather than on the structure.

The free body, and where the force comes from

It is worth drawing the free body explicitly, because the load has an unusual origin and the unusual part is easy to lose.

Cut a metre of the chimney and draw it. On it act: the drag, along the wind, roughly steady; the lift, across the wind, alternating at the shedding frequency; the inertia force of the metre of steel; and the shear and moment from the chimney above and below. The sums cancel, as ever.

The alternating lift is the whole subject, and its magnitude is modest — a lateral force coefficient of about 0.7 for a circular cylinder in the subcritical range, which on this chimney at 6 m/s is roughly 20 N per metre. Twenty newtons. What turns twenty newtons per metre into 180 mm of motion is not the force but the multiplier:

How much a harmonic force is magnified, at three damping ratiosDisplacement amplitude divided by the deflection the same force would produce if it were applied slowly, against the ratio of the forcing frequency to the structure's own, at 0%, 0%, 1% of critical damping. At the natural frequency the magnification is 250, 125, 50 respectively — one over twice the damping ratio, and nothing else in the problem enters it.00.20.40.60.811.21.41.61.820510152025forcing frequency ÷ natural frequencyamplitude ÷ static deflection0% damping — 250× at the peak0% damping — 125× at the peak1% damping — 50× at the peak
Fig. 5 The magnification available to a welded steel structure: 250, 125 and 50 at damping ratios of 0.2%, 0.4% and 1%. These are the largest multipliers anywhere in this field, and they belong to exactly the structures vortex shedding attacks — slender, welded, unclad, with nothing rubbing against anything.

So the mechanism is a small force meeting an enormous multiplier, and the multiplier exists because a steel chimney is the most lightly damped structure engineers build. Every other structure on this site has partitions, cladding, bolted joints and finishes rubbing against a frame; a chimney has a weld and a coat of paint.

What is actually done about it

Three remedies, in increasing order of admission that the problem is real.

Accept the motion and check the fatigue. A chimney swinging 180 mm at 0.9 Hz for hours at a time accumulates cycles quickly: three thousand an hour, ten million in a few years. The limit state is not strength but fatigue at the welded details, and the stress range at the base is what has to be checked. This is the commonest outcome and it is why vortex shedding is a fatigue problem more often than a strength one.

Add damping. A tuned mass damper, a chain damper hanging inside the flue, or a viscous device at the top. Because the response goes as 1/Sc1/Sc and ScSc contains ζ\zeta linearly, a small amount of added damping is worth a great deal — which is why an added mass is the standard fix for slender steel structures.

Spoil the shedding. Helical strakes wound around the top third of a chimney break the vortices’ spanwise correlation so that they no longer shed in phase along the length. It is the only remedy that attacks the excitation rather than the response, it costs about 25% more drag, and it is the reason so many industrial chimneys have a spiral fin near the top. It is also the only one of the three that would still work if the structure’s damping turned out to be a tenth of what was assumed — which, given how damping is arrived at, is not a hypothetical.

The cross-wind amplitude through the lock-in bandA 0.5 m cylinder at 2.5 Hz. Vortices leave it at St·U/D, so the critical speed at which they match the structure is 6.94 m/s — a breeze, met many times a year rather than once in fifty. At a Scruton number of 18.1 the peak amplitude is 46.56 mm, which is 9% of the diameter. 0246810121416182001020304050wind speed (m/s)cross-wind amplitude (mm)0.30% damping — Sc = 18.1, peak 46.56 mm
Fig. 6 A different structure entirely — a 500 mm mast at 2.5 Hz. The critical speed is 6.9 m/s, the Scruton number is 18.1, and the peak amplitude is 47 mm, which is a tenth of the diameter. The pattern is the same at every scale because the governing groups are dimensionless, which is why sign gantries, lamp posts, cables and bridge hangers all have the same problem in the same terms.

How often, and for how long

The design question a chimney raises is not “how big” but “how often”, and the wind statistics answer it in a way no other load on this site does.

Wind speed at a site has a distribution, and the middle of it is where structures spend their lives. A speed of 6 m/s is exceeded for a large fraction of the year at almost any exposed location and occurs — in the sense of sitting inside a ±25% band around it — for hundreds of hours annually. Every one of those hours, this chimney is oscillating at 0.9 Hz, which is 3,240 cycles an hour.

Pulled to 180 mm and let go, on a structure of 1.11 s periodDisplacement against time for a single-degree-of-freedom structure of natural period 1.11 s and 0.4% damping, under pulled to 180 mm and let go. The static deflection under the same peak force is 62.42 mm and the peak response is 180 mm — a factor of 2.88.0510152025303540-200-100100200time (s)displacement (mm)pulled to 180 mm and let goeach cycle is 0.975 of the one beforepeak 180 mm at 0.000 s
Fig. 7 And it does not stop promptly when the wind moves off the band. Displaced to its lock-in amplitude and left alone, this chimney is still at 40% of it forty cycles later — three quarters of a minute. A structure with this little damping accumulates cycles from every episode long after the episode ends.

Ten million cycles in a few years is entirely ordinary, and that number is the reason vortex shedding shows up in inspection reports as cracked welds at the base rather than as a chimney lying on the ground. The failure mode is fatigue and the design case is a breeze, which between them make this the least intuitive load case in structural engineering.

Ferrybridge, and the cylinders that were not alone

The most instructive wind failure of a group of bluff bodies happened at Ferrybridge power station in Yorkshire on 1 November 1965, when three of eight cooling towers collapsed in a gale.

The towers had been designed for a wind loading based on a single isolated tower. In a group, the downwind ones stand in the wake of the upwind ones, where the flow is more turbulent and the pressure distribution is different — and the loading they actually received was outside what the design had contemplated. The investigation that followed changed British wind loading practice substantially, and one of its lasting effects was the recognition that a structure’s wind loading is a property of its surroundings and not only of itself.

That is the same lesson the two-cylinder problem teaches at a smaller scale, and it is worth attaching to this essay rather than to the previous one because it is a lesson about shape and arrangement rather than about turbulence statistics. The Davenport apparatus of the last essay handles a building in a boundary layer very well and says nothing at all about what the building next door is doing to it.

What the picture cannot show

The amplitude model is empirical. The Strouhal relation and the Scruton number are solid; the coefficient that converts them into a displacement is fitted to measurements, and different codes give noticeably different answers. The shape of the curve is trustworthy and its height is a correlation.

Turbulence disrupts it. Everything here assumes smooth flow. Real atmospheric turbulence breaks up the spanwise correlation of the shedding on its own, so a structure in a rough urban boundary layer responds less than one in open country — and a wind tunnel test in smooth flow overestimates. The worst conditions are steady, smooth, moderate winds, which is another reason the problem is a fine-weather one.

Two cylinders are a different problem. Adjacent stacks, a pair of cables, a chimney beside a building: the wake of one interferes with the other, and the interference produces its own instabilities at speeds neither has alone.

3 kN at 1.00 times the natural frequency, on a structure of 1.11 s periodDisplacement against time for a single-degree-of-freedom structure of natural period 1.11 s and 0.4% damping, under 3 kN at 1.00 times the natural frequency. The static deflection under the same peak force is 4.68 mm and the peak response is 455.63 mm — a factor of 97.33.0102030405060-400-200200400time (s)displacement (mm)3 kN at 1.00 times the natural frequencysteady amplitude 585.18 mmstatic, 4.68 mmpeak 455.63 mm at 67 s
Fig. 8 Why the response is so large for so small a force. A 3 kN cross-wind force on a chimney of 0.4% damping builds up over about forty cycles to 125 times the deflection it would cause if applied slowly. The force is trivial; the multiplier is not, and the multiplier is the reciprocal of a number the structure was never designed to have.

Why it is a modern problem

Vortex shedding has been going on since the first mast was put up, and it became an engineering problem in the middle of the twentieth century. The reason is entirely in the Scruton number.

A masonry chimney has a mass per metre in the thousands of kilograms and mortar joints that dissipate energy; its Scruton number is in the hundreds and it does not respond. A welded steel chimney of the same diameter has a tenth of the mass and a fortieth of the damping; its Scruton number is around ten and it responds to a breeze. Nothing about the aerodynamics changed — the same vortices leave the same cylinder at the same rate — and the structure stopped being able to ignore them.

The pattern is one this site meets in floor vibration and will meet again: the problems that arrive with better engineering are dynamic ones, because efficiency removes exactly the mass and the accidental friction that used to make dynamics irrelevant. Every kilogram saved is a kilogram not available to the Scruton number.

Where the ladder goes

Two directions, and they diverge sharply.

One is the fatigue calculation the accepted-motion remedy needs — the same accumulation argument as the load that never came near failing anything, with the cycle count supplied by the wind statistics rather than by a machine: how many cycles, at what stress range, against a detail category — a subject this site has already opened from the materials side.

The other is the family this belongs to. Lock-in is the mild case of a load that depends on the response. There are worse ones, where the feedback is positive without limit and the structure supplies its own excitation from a steady wind — the case where nothing bounds the answer at all.

What this makes readable

Essays that name this one as a prerequisite.

Named alongside this one

Essays reaching for the same objects. Nobody chose these; they are what the concept index makes visible.

What links here

Every essay whose body links to this one.

The objects this essay names

Each one links to every other essay that touches it.

AeroelasticityCross wind responseDampingLock inResonanceScruton numberStrouhal numberVortex shedding