Stability

The column that fails years later

A concrete column under sustained load goes on straining at constant stress, so its deflection grows — and because the second-order moment is the load times that deflection, the demand grows with it. There is a load below which the two settle and one above which they never do.

Assumes The load that makes itself worse, The deflection that arrives three years late and Strong enough and still falls over.

Two facts about concrete are taught in different courses and are almost never put together.

The first is that concrete creeps: hold a stress on it and the strain goes on growing for years, reaching two or three times its instantaneous value. The second is that a compression member’s deflection is amplified by 1/(1N/Ncr)1/(1 - N/N_{cr}), because the axial load acts on the deflection it has already produced.

Put them together and the amplifier has a denominator that closes with time.

The deflection goes on growing, and sometimes it does not stopSecond-order deflection of a sustained-loaded concrete column against age, on a log time axis. Creep takes the effective modulus down, which takes the buckling load down with it — from 11580 kN on the day to 3309 in the long term, 29 per cent of it — so the amplifier 1/(1 − N/N_cr) grows even though nothing was added to the load. At 2200 kN the column settles: 25 mm of eccentricity on the day and 60 mm at the end, a factor of 2.4 for a load that never changed. At 5294 kN — still only 46 per cent of the day-one critical load — it does not settle, and the divergence arrives at 55 days for no new reason at all.3210031610003162100000102030405060age (days, logarithmic)eccentricity including P-delta (mm)settles at 60 mmand this one does notfirst order 20 mmlong-term critical load 29% of the day-one one
Fig. 1 Second-order eccentricity of a sustained-loaded column against age, on a logarithmic time axis. At 2,200 kN the column settles: 25 mm of eccentricity on the day and 60 mm at the end, a factor of 2.4 for a load that never changed. At 5,294 kN — still under half the day-one critical load — it does not settle, and the divergence arrives after 55 days.

Which free body produced the number

Cut the column at mid-height and take the lower half. The moment there is the axial force times the total eccentricity, and the total eccentricity is the first-order one plus whatever the column has already bent.

For a pin-ended column with a sinusoidal imperfection or a sinusoidal first-order moment, that closes into the standard amplifier

e=e01N/Ncre = \frac{e_0}{1 - N/N_{cr}}

which is exact for the sine shape and near enough for everything else. The only quantity in it that time can touch is NcrN_{cr}, and NcrN_{cr} is π2EI/L2\pi^2 EI/L^2.

Creep touches EE. The effective-modulus method is the simplest honest way to say how: a stress held constant produces a strain that grows by the factor (1+φ)(1 + \varphi), so the member behaves as though its modulus were E/(1+φ)E/(1+\varphi), and

Ncr,=Ncr,01+φN_{cr,\infty} = \frac{N_{cr,0}}{1 + \varphi_\infty}

For an ordinary creep coefficient of 2.5, that is 29 per cent of the day-one value. A column checked at a comfortable third of its buckling load on the day it is propped is above its long-term buckling load.

The deflection that arrives years lateThe multiplier on a concrete member's deflection under a sustained load, against time. The elastic deflection arrives on the day the load does and is the 1.0 at the left. After a year it has been multiplied by 3.09, after five years by 3.39, and it approaches 3.48. Nothing has been added to the load and nothing about the strength has changed: this is a serviceability failure arriving on a structure that passed every strength check on the day it was built.1 d10 d100 d2.7 yr27 yr0123time under loaddeflection ÷ the deflection on day one1 year: ×3.095 years: ×3.39the deflection the calculation gives
Fig. 2 The coefficient the whole argument runs on. It is not a small correction and it is not fast: half of it arrives in the first year and the rest over the following decade, so the structure this essay describes is doing its most dangerous work long after everybody has gone home.

Two regimes, and a boundary that is a fraction

The consequence is a clean division.

Below Ncr,0/(1+φ)N_{cr,0}/(1+\varphi_\infty) the column settles. Its deflection grows — by a factor of 2.4 on the column drawn, from 25 mm to 60 — and stops, because φ\varphi approaches a limit and so does the amplifier. That is a serviceability outcome: a column visibly bent, its moment larger than the design one, and stable.

Above it there is nothing to settle to. φ\varphi passes the value at which N=Ncr(t)N = N_{cr}(t), the amplifier passes through infinity, and the column fails at a moment fixed by a material property rather than by an event.

The date is not found by watching a number run away. It is found by inverting the creep law: the divergence happens when

φ(t)=Ncr,0N1\varphi(t) = \frac{N_{cr,0}}{N} - 1

and the creep law is a known function of time, so the answer comes back directly. At 46 per cent of the day-one critical load it is 55 days. At 38 per cent it is 123 days. At 57 per cent it is 34.

Below a line it settles, above it there is a dateWhen a sustained-loaded column stops moving, or does not, against how much of its day-one buckling load it is carrying. Creep takes the effective modulus to E/(1 + φ), so the long-term critical load is 29 per cent of the short-term one for a creep coefficient of 2.5. Below that fraction the second-order deflection converges to a finite value, and the column is safe with a deflection several times what a day-one calculation gave. Above it there is no equilibrium to converge to, and the curve is the age at which the amplifier diverges — found by inverting the creep law rather than by watching a number run away. At 0.95 of the day-one critical load it arrives after 28 days, with nothing having been added to the load and nothing having changed on site.0.00.20.40.60.81.032100316100031621000031623sustained load ÷ day-one critical loadage at divergence (days)settles, and goes on moving29% — the long-term critical loadthe date it failsφ∞ = 2.5, so E_eff is E over 3.5 and N_cr goes with it
Fig. 3 When the column stops moving, or does not, against how much of its day-one buckling load it carries. The shaded region settles; the curve is the age at which the amplifier diverges, and it is steep — a column ten per cent above the boundary lasts a third of a year and one fifty per cent above it lasts a month.

Which is why the check is written the way it is

The design rules for slender concrete columns look arbitrary until this is in view.

They ask for a creep-adjusted stiffness, computed with an effective creep ratio that is not the material’s φ\varphi_\infty but φ\varphi_\infty scaled by the fraction of the load that is permanent — because a column carrying half its load as imposed floor loading only creeps under the half that stays. They ask for an imperfection, because the amplifier has no answer for a perfectly straight column and every real column is not. And they ask for a nominal stiffness or a nominal curvature rather than a section analysis, which is a way of admitting that the stiffness in the denominator is not a property anyone can compute exactly.

Every one of those is a response to the same structure: an amplification whose denominator depends on a stiffness that is falling.

The column curveFailure load against slenderness, as a fraction of the squash load. A stocky column crushes; a slender one buckles at the Euler load; the crossover is where the two curves meet, and real columns fall below both near it.2040608010012014016000.20.40.60.811.2slenderness (effective length ÷ radius of gyration)they cross at λ = 104squashingEuler bucklingreal columns, which are neither
Fig. 4 The load the whole thing is measured against. Euler’s is a stiffness divided by a length squared, and the argument here is entirely about what happens when the stiffness in the numerator is a function of time.

The same shape in three materials

The structure of this argument is not about concrete. It is about a compression member whose stiffness falls while it is loaded, and there are at least three of those in this collection.

Timber has a duration-of-load factor — a strength reduction for permanent loading — and a creep factor that does exactly what φ\varphi does here, with the added difficulty that both depend on moisture content. A timber column’s long-term buckling load is a smaller fraction of its short-term one than concrete’s.

Steel at temperature is the same equation with the clock running much faster. The hour that is really a temperature is the strength side of it; the stiffness side is that steel’s modulus falls faster than its strength does above about 400 °C, so a steel column in a fire loses buckling capacity before it loses squash capacity, and a slender one fails in minutes at a load a stub column would carry.

And any structure with a soil under it. A footing on clay is a spring whose stiffness falls as consolidation proceeds, and a frame whose sway stiffness depends on that spring is a frame whose NcrN_{cr} falls with time — the same divergence, with the creep in the ground rather than in the member.

The hour that is really a temperatureThe retention factors for carbon steel against temperature: the yield stress and the elastic modulus. The modulus falls away first — at 500°C the steel has kept 78% of its strength and 60% of its stiffness — so a member's failure mode can change during a fire. A member working at 50% of its cold capacity runs out of strength at 590°C, and out of the stiffness for the same ratio at 534°C, 56 degrees earlier. There is nothing about time in any of it: a fire rating is a temperature the member must not reach, converted into the minutes a particular fire takes to get it there.20040060080000.20.40.60.81temperature, °Cfraction of the cold valuestrength runs out at 590°Cstiffness at 534°Cyield stresselastic modulusworking at 50% of cold capacity
Fig. 5 The same collapse of stiffness, in an hour rather than a decade. What makes fire and creep the same problem is that both are a member’s modulus falling under a load that is not changing, and what makes them different is only how long a designer has to notice.

The load that is permanent, and the load that is not

The strongest simplification in the analysis above is that all of the load creeps, and correcting it is where the design rule earns its complexity.

Creep responds to the stress that is held. A column carrying 2,200 kN of which 1,400 is dead load and 800 is a floor loading that comes and goes creeps under something much closer to 1,400 — so its effective creep ratio is the material’s coefficient scaled by the ratio of permanent to total.

That scaling has a consequence worth stating plainly: two columns carrying the same total load can have long-term buckling loads a factor of two apart, according to which of them is holding a warehouse and which is holding a car park. The load case that governs the day-one check is the full one; the load case that governs the long-term check is the permanent part; and the two are different structures asked different questions.

It also means the mode is worst in exactly the buildings where it is least expected. A heavily loaded transfer column under a residential tower is nearly all permanent load, creeping at nearly the full coefficient, for the whole life of the structure.

Two differences up the same building, peaking in different placesDifferential shortening between a perimeter column and the core of a 40-storey building, plotted up the height. The part driven by load peaks at level 20 — exactly half way up, because a floor near the top has almost nothing built above it to shorten what is beneath, and a floor near the bottom has almost nothing beneath it to shorten. The part driven by shrinkage does not care what is above it at all and accumulates all the way to the roof. Their sum is worst at level 40, at 43 mm, which across a 9 m bay is a floor out of level by one in 208.-40-30-20-10010020406080100120140column shorter than core (mm)height (m)from loadfrom shrinkagethe sumworst 43 mmat level 40one in 208
Fig. 6 What a permanent load does to a structure over time. The same creep that shortens a column differentially against its neighbours is the creep that softens it against its own buckling load, and the two calculations are usually done by different people.

The failure has no cause and no warning

The most useful thing to say about this mode is what it looks like from outside.

Nothing happens. The load has not changed, no new load has been applied, no material has been substituted, and the weather is the same as it was. A column bends slowly for months and then bends quickly, and the interval between “visibly out of plumb” and “gone” is short because the amplifier’s growth is not linear — it is a reciprocal approaching a zero.

There is therefore no event to investigate. A collapse of this kind produces an inquiry that finds no cause, because the cause was the absence of a check performed twenty years earlier at a moment when the structure was demonstrably safe.

That is the argument for the check being about a fraction rather than about a stress. A stress-based check on the column drawn passes comfortably at every age; the load is a fifth of the day-one buckling load and the concrete is nowhere near its strength. What fails is a comparison between a load and a stiffness, and stiffness is the quantity structural checks are least often written in.

A column that was never straightLoad against lateral deflection at mid-height, for a column starting with an initial bow of 0.004. There is no critical value to reach: the deflection grows from the first increment, slowly at first and then without bound as the ratio approaches 1.00 — which is the Euler load, and which the column therefore never attains. The perfect column, drawn for comparison, sits on the vertical axis until it arrives there and then has no answer at all.00.010.020.030.040.0500.20.40.60.81lateral deflection at mid-heightload ÷ P꜀ᵣP ÷ P꜀ᵣ = 1.00, approached and never reachedinitial bow: δ₀ = 0.004
Fig. 7 Why a perfectly straight column is not the useful idealisation. The amplifier needs something to amplify, and the something is an imperfection — so the whole of this essay is about how a small initial crookedness is turned into a large one by a load that is well below the critical.

The number a designer can actually move

There are four quantities in Ncr,=π2EI/(1+φ)L2N_{cr,\infty} = \pi^2 EI/(1+\varphi)L^2, and they are not equally available.

φ\varphi belongs to the concrete and the environment, and the range a designer controls is narrow — a lower water-cement ratio, a later age at loading, a larger member. EE moves with the aggregate and hardly at all with the grade. LL is the storey height, which is architecture.

What is left is II, and it is the one that responds quadratically. Taking the 400 mm column drawn to 500 mm multiplies its second moment by 2.4 and its long-term critical load with it, and costs a hundred millimetres of plan.

That is why the practical response to a slender concrete column is almost never a stronger concrete. A grade increase buys a little modulus — EE goes roughly as the cube root of the strength — and buys nothing at all in the quantity that is falling. A creep problem is solved with geometry. It is the same conclusion the section-shape comparison reaches by a completely different route, and it holds here more strongly, because the property being lost is stiffness rather than strength.

The one length a section carries into a columnFour profiles of equal area, with the radius of gyration r = √(I/A) drawn as the distance it is — a pair of lines either side of the centroid, at the depth the whole area would have to sit at to give the section the second moment it has. As a 4 m pin-ended column the same 5200 mm² of material carries between 9 and 16782 kN, in the ratio of the squares of those radii and of nothing else.the same, laid flatr = 3.8 mmλ = 10669 kNsquarer = 20.8 mmλ = 192292 kNtall rectangler = 115.5 mmλ = 358981 kNI-sectionr = 157.8 mmλ = 2516782 kNthe dashed pair is ±r about the centroidthe bar is the Euler load at 4 m, to scale
Fig. 8 The one length a section takes into a column. Creep leaves the radius of gyration alone and takes the modulus down, so the response has to be on the axis the modulus is not on — which is the section’s own geometry.

The reason no test finds it

A structural test is a load applied over minutes. Creep buckling is a load applied over years, and that difference is why the mode is known from theory and from collapses rather than from laboratories.

The obvious response — hold a column at a load for a decade and watch — has been done a handful of times and is not a routine. What is done instead is to accelerate: load at a high stress ratio, where the creep coefficient is reached in months rather than decades, and extrapolate. That works for the arithmetic and imports its own assumption, because concrete’s creep is not linear in stress above about forty per cent of its strength, and the accelerated test is run in exactly that region.

So the design rule for slender concrete columns rests on a chain: a creep model fitted to short-term specimens, an effective modulus that assumes a constant stress, and an amplification derived for an elastic member. Each link is defensible and the chain has never been tested end to end at the timescale it is written for. That is worth knowing when reading a code clause that looks as settled as a strength check.

Three details, and no material anywhere on the plotStress range against cycles to failure for three detail categorys — 160, 90, 36 N/mm² at two million cycles. The lines are parallel because they share a slope of three, and the spread between them is a factor of 4.4 in stress and therefore 88 in life. Nothing on this plot depends on the strength of the steel: the same detail in a grade twice as strong lies on the same line. At a stress range of 60 N/mm² the lives are 160: unlimited, 90: 8.2e+6, 36: 4.3e+5 cycles. The knee in each line is the constant-amplitude limit, past which the slope becomes five.10⁴10⁵10⁶10⁷10⁸2050100200500cycles to failurestress range, N/mm²category 160category 90category 368.2e+64.3e+5working range 60 N/mm² — the lives are marked
Fig. 9 The other design curve built from accelerated tests. Both extrapolate from an experiment shorter than the life of the structure, and both are honest about it only in the small print.

Where the model stops

The effective-modulus method is the crudest of the creep formulations. It is exact for a stress held constant from a single instant and approximate for anything else; a load applied in stages, or partly removed, needs a superposition method or an age-adjusted modulus, and both give a slower loss of stiffness than the number here.

Cracking is a fixed factor. The 0.6 applied to EIEI stands in for a section that is partly cracked, and a real column’s cracked stiffness depends on the moment it is carrying — which is the moment this calculation is trying to find. The honest version is iterative and the answer moves in the unhelpful direction: more moment, more cracking, less stiffness, more moment.

The creep coefficient is treated as a property. It depends on the humidity, the member’s surface-to-volume ratio, the age at loading and the mix, and a factor of two either way across those is ordinary. Since it appears as 1/(1+φ)1/(1+\varphi), that factor of two is a factor of nearly two in the long-term critical load.

The creep law is a curve fitted to tests. The expression used here reaches its final value asymptotically with a time constant of a few hundred days, which is the ordinary shape, and the date it returns for a divergence is only as good as that shape near the value of φ\varphi that matters. Two creep models that agree about the thirty-year answer can disagree by months about when a particular coefficient is reached, and it is the second that this calculation asks for.

And the column is pin-ended and prismatic. A real column is in a frame, and its effective length depends on members whose own stiffness is creeping — so the buckling length is also a function of time, and not necessarily in the safe direction.

What the pictures cannot show

The time axis is logarithmic, which is the only way to draw a process that is half over in a year and continues for thirty. It makes the divergence look like an event at a date; on a linear axis it would look like a curve that becomes vertical, which is closer to the truth and impossible to plot next to the first month.

Nor can any figure show the thing that decides whether this failure mode ever arrives, which is what else is holding the structure up. A column in a braced frame that fails in creep buckling sheds its load to its neighbours; a column that is the only thing under a transfer beam does not. The mode is a property of a member and the consequence is a property of the structure, and nothing on this page is about the second.

The assumption the figure rests on

The load is assumed to be constant from the day it is applied.

Almost no load is. A building is loaded in stages as it is built, its imposed load comes and goes, its prestress relaxes, and the concrete’s own creep redistributes force from the members that creep most to the members that creep least. Each of those makes the effective creep coefficient smaller than the material’s, which is why the check in practice uses a ratio of permanent to total load rather than the coefficient itself.

The one case where the assumption is exactly right is the one that matters most. A prop, a temporary column, a falsework leg under wet concrete: loaded at once, at an age when the concrete is young and creeps fastest, at a load fraction chosen for a short-term check, and left in place for as long as the programme requires. That is where creep buckling has actually happened, and it is not a category of structure anybody designs with a long-term stiffness in mind.

Length costs more than it looksThe same column section at four lengths, with the buckling capacity of each drawn as a bar. Capacity falls as the inverse square of the length, so a column three times as long carries a ninth as much.1× the length100% of the capacity2× the length25% of the capacity3× the length11% of the capacity4× the length6% of the capacityidentical section, identical material, identical end conditions
Fig. 10 What slenderness costs at any age. Creep does not change the shape of this curve; it moves a column along it, from wherever it was on the day to a position corresponding to a modulus a third of the size — which is the same as making it 3.5\sqrt{3.5} times more slender overnight.

Named alongside this one

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

The objects this essay names

Each one links to every other essay that touches it.

AmplificationBucklingCreepCreep bucklingDivergenceDuration of loadEccentricityEffective modulusFireImperfectionSecond orderServiceabilitySlendernessStiffnessSustained load