Stability

The most dangerous day is before it is finished

A structure is analysed once, complete, with every restraint present. It spends weeks in states nobody drew — a beam landed with no deck on it holds 17% of the moment its section is worth, a frame not yet braced buckles at a third of the load it will, and a bolt not yet tightened is a pin where the analysis assumed a fixity.

Assumes The ends decide the length that matters, The beam that fails sideways and The structure that was never complete.

Every analysis in this collection is of a finished structure. Its bracing is in, its slabs are cast, its joints are made, its bases are grouted, and every restraint that the effective lengths assume is present. Loads are applied to that object and the answers follow.

A real structure spends weeks or months in states that are not that object, carrying real loads, in weather. Nobody draws those states, no analysis model contains them, and the arithmetic that governs them is the arithmetic of this collection with terms removed.

The mistake worth dismantling is the intuition that a partly built structure is safe because it is lightly loaded. The load falls, and the capacity falls faster.

How stiff a brace has to be before the frame stops swayingThe effective length factor of a swaying portal against the stiffness of a horizontal spring at its head. The curve starts at k = 1.317, the unbraced value, and falls to 0.774 — the factor for the same frame with its head held — at a brace stiffness of 23.2 EI/L³. Past that point the frame buckles in the non-sway mode, which the brace does not restrain, and further stiffness buys nothing at all. The threshold is worth stating as 1.41 N꜀ᵣ/L, which is the form the number is memorable in: for a storey carrying a thousand kilonewtons over four metres it is about 0.35 kN per millimetre of sway. Against the frame's own lateral stiffness of 12.0 EI/L³ it is a factor of 1.93.02040608000.20.40.60.811.21.41.6brace stiffness (units of EI/L³)effective length factor k23.2 EI/L³ = 1.41 N꜀ᵣ/L0.77 — held1.32 — freepast the threshold the frame buckles in a mode the brace does not hold
Fig. 1 The whole argument in one curve: the effective length factor of a swaying portal against the stiffness of a brace at its head. Unbraced it is 1.317; braced, 0.774. Since capacity goes as the inverse square, the brace is worth a factor of 2.90 — and it is the thing installed last.

Restraint is worth more than load

A restraint does not add strength; it changes what the member is. Removing it does not reduce a capacity by a percentage, it moves the member to a different point on a curve — and the curves in stability are steep.

The length at which a beam stops being a beamElastic critical moment against the distance between lateral restraints, with the section's plastic capacity drawn across it. The two cross at 3803 — beyond that length the beam buckles sideways before it reaches the strength its cross-section has, and the capacity is set by the restraints rather than by the steel.2000400060008000100001200002004006008001000distance between lateral restraintsthey cross at 3803the plastic capacity of the sectionelastic critical momentSt Venant torsion alone — what is left at long lengthswarping dominates here
Fig. 2 The length at which a beam stops being a beam: elastic critical moment against the distance between lateral restraints, with the section’s plastic capacity drawn across it. At 3 m of restraint spacing the critical moment is 802 kNm against a plastic capacity of 522, so the beam reaches its full strength. Unrestrained over 12 m it is 92 kNm — 17.5%.

That is a factor of 8.8 between the beam as designed and the same beam on the day it was landed, and nothing about the beam has changed. The deck that will restrain its compression flange at 3 m centres has not arrived yet; the beam is carrying its own weight and two people, and its capacity is a sixth of what every calculation about it assumed. It is held and not held in the most literal available sense.

The load side of the comparison moves by nothing like as much. A composite floor beam in service carries its own weight plus the slab plus the imposed load — the self-weight alone is perhaps a fifth of the total. So the load has fallen by a factor of five and the capacity by a factor of nearly nine.

A ratio that improves by five and worsens by nine is a ratio that has got worse. That single comparison is the whole subject.

Which free body produced the number

Take the beam as it is on the day: simply supported at its ends, unrestrained between them, carrying a uniform load equal to its own weight and whatever is on it.

The check is the ordinary lateral-torsional one, with the unbraced length equal to the whole span rather than the deck spacing. McrM_{cr} contains EIzGJ\sqrt{EI_z GJ} and a warping term, and both are divided by the unbraced length — so the answer scales roughly as 1/L1/L for a long member and the loss is not a small correction.

The same argument applies to a column and to a frame, and it applies with the same steepness because every stability capacity goes as an inverse square of a length.

A brace is a stiffness requirement, not a strength oneCritical load against brace stiffness for a pinned column braced at mid-height. The curve climbs from the unbraced Euler load of 9.87EI/L² and flattens at 39.48EI/L², which is the Euler load of the braced segment — past that the column buckles in a shape the brace does not obstruct, and further stiffness buys nothing. A stiffness of 16EI/L³ is marked, reaching 13.09EI/L².010203040506001020304050brace stiffness (units of EI/L³)critical load (units of EI/L²)13.139.5 — braced9.87 — unbraced
Fig. 3 The brace that need not be strong, which is the same statement about a column. A brace at mid-height takes the critical load from 9.87 to 39.48 EI/L² — exactly four times, because the buckling length halves — and the stiffness needed to do it is 159 EI/L³, about three times the column’s own transverse stiffness.

A factor of four, from a member whose job is to be stiff rather than strong, and which is not present until somebody installs it.

Joints that are not yet joints

The second thing missing from a partly erected structure is the fixity every analysis assumed.

A steel frame is erected with bolts in place and not fully tightened, so the connections behave as something much closer to pins than to the semi-rigid joints they will be. A base plate is set on levelling nuts and not grouted, so the base is a pin — or worse, a point support on a plate that can rock.

Moment against rotation, for three real jointsThree connections on one plot, with the classification boundaries for a beam of EI/L = 2333.33 drawn as rays through the origin. web cleats is semi-rigid, flush end plate is semi-rigid, extended end plate is rigid. The boundaries are multiples of EI/L, so the same joint is rigid on a short stiff beam and semi-rigid on a long slender one.00.0050.010.0150.020.0250.030.0350.040.0450.05050100150200rotation, radiansmoment, kN·mrigid abovepinned belowweb cleats — semi-rigidflush end plate — semi-rigidextended end plate — rigid
Fig. 4 Three real joints against the classification boundaries. A connection’s classification is a comparison with the beam it serves, and the same bolts at a fraction of their preload sit somewhere quite different on this plot from where they will sit when the frame is complete.
What the joint does to the beamEnd moment as a fraction of the fixed-end value wL²/12, against the joint's rotational stiffness, for a beam of EI/L = 2333.33. At the rigid boundary of 18666.67 kN·m/rad the joint delivers 80% of it and at the pinned boundary 20%. Everything between the two lines is a redistribution nobody chose and every analysis assumed away.02000040000600008000010000012000014000016000018000020000000.20.40.60.81joint rotational stiffness, kN·m/radend moment ÷ wL²/1227.84%72%90.79%rigid boundarysemi-rigidfixed ended
Fig. 5 And what that does to the member. End moment as a fraction of the fixed-end value, against the joint’s stiffness: a joint that will deliver 80% of wL2/12wL^2/12 when it is finished delivers very much less while it is being made — and the mid-span moment that is its complement is correspondingly larger.

For a beam this is usually benign, since a pinned end is the conservative assumption in bending. For a frame it is not, because a frame’s stability against sway depends on its joints. A moment frame with its joints not yet tightened has no lateral system at all — which is the redistribution nobody chose with the whole structure as its subject.

A portal frame swaying under 20A portal frame pushed sideways, solved by the stiffness method because statics cannot divide the load between two columns. The base shears come out at 10.0 and 10.0 and add to the applied 20; the peak moment is 34.3. The sway is drawn hugely exaggerated, and the moment diagram is plotted on each member's tension face.20H 10.0 M 34.3H 10.0 M 34.3the two base shears add to the applied 20 — the split came from stiffness, not staticsthe sway is exaggerated; a real frame at this load moves a fraction of a millimetre
Fig. 6 A portal frame swaying, solved by the stiffness method because statics cannot divide the load between two columns. Everything that resists that sway — the joint fixity, the base fixity, the beam’s own stiffness — is present in the finished frame and partly absent in the erected one.

Second-order effects arrive early

A structure at a fraction of its buckling load has its deflections amplified, and the amplification is not linear.

The load that makes itself worseThe amplification of a deflection against the ratio of applied load to buckling load. A structure at half its buckling load deflects twice as far as first-order analysis predicts, and the curve runs away well before the load is reached.00.20.40.60.80246810applied load ÷ buckling load1.1×1.3×1.4×first-order analysis says the answer is always 1×one over one minus the ratio
Fig. 7 The load that makes itself worse: the amplification of a deflection against the ratio of applied load to buckling load. At 20% of the buckling load the amplification is 1.25 and manageable. At 60% it is 2.5.

Put the two reductions together. If the erection load is 25% of the design load and the erection capacity is 34% of the design capacity — the sway factor of 2.90 above — then a frame designed to sit at 20% of its buckling load in service sits at

0.20×0.250.34=0.150.20 \times \frac{0.25}{0.34} = 0.15

during erection, which is better. That is the honest arithmetic for gravity load and it is the reason most steelwork is erected without incident.

The trouble is that the other load does not scale. Wind does not know the building is unfinished. The lateral load on a partly erected frame is very nearly what it will be on the finished one — the frame is the same height, the cladding may or may not be on, and the reference wind speed is reduced only by the shorter exposure period. Meanwhile the lateral system is the part that is missing.

So the ratio that matters during erection is not gravity load over gravity capacity. It is full wind over a third of the lateral resistance, and that ratio is several times worse than anything the finished structure ever sees.

Both failures are decided by the same two numbersFactors of safety against overturning and against sliding, for a body 12 m wide weighing 4000 kN under a wind pressure of 1 kN/m², as its height grows. Overturning falls as the square of the height and sliding as the first power, so they cross: below 63.2 m the body overturns at a factor of one, and uplift at one edge has already begun at 36.5 m — a ratio of exactly √3, whatever the numbers are.01020304050600123456height of the body (m)factor of safetyuplift starts at 36.5 moverturningsliding
Fig. 8 And the crudest version of the same problem: overturning and sliding of a body under wind, against its height. Both are resisted by weight, and a bare frame has a fraction of the weight it will have — so the wind case that is comfortable when the floors and cladding are on can be marginal when they are not.

The frame that is stable only when it is complete

There is a class of structures for which the finished load path does not exist until the last member is in, and for those the temporary condition is not a reduced version of the permanent one. It is a different structure.

The count is necessary and not sufficientTwo pin-jointed frames, each satisfying m + r = 2j exactly. One of them folds anyway, because the equations are not independent; the ghosted outline is the motion that costs no member any change of length, drawn at an exaggeration of 0.55 of the span.one panel braced twice, the next not at allm 9 + r 3 = 2j 12 · rank 11a mechanismthe same count, properly arrangedm 9 + r 3 = 2j 12 · rank 12stands up
Fig. 9 The count that does not see it: a frame satisfying m + r = 2j exactly, folding anyway. A partly erected frame is one member short of something by definition, and being one member short is the condition under which this failure lives.

An arch is the standard example: incomplete, it is two cantilevers, and its whole mechanism depends on a closure that happens last. A cable-stayed bridge is another, built out from its towers as a balanced cantilever with the deck carrying moments it will never see again. A space frame assembled on the ground and lifted is a third — the lifting configuration has different supports from the final one, and the member forces during the lift can exceed the in-service ones.

The props decide where the stress ends upBottom-fibre stress in the steel of a 12 m composite beam carrying 12 kN/m of wet concrete and 18 kN/m afterwards. Unpropped, the bare steel takes the first stage alone and reaches 292 MPa; propped, the finished composite section takes everything and reaches 186 MPa — a ratio of 1.57. 62% of the unpropped beam's final stress was locked in before the slab was structural at all. The deflections differ by 1.73 times for the same reason, and no drawing of the finished beam distinguishes the two.292 MPaunpropped49.3 mm at midspansteel alonecomposite186 MPapropped28.6 mm at midspancomposite
Fig. 10 What a structure carries depends on what was present when the load arrived — the propped and unpropped composite beam, where 62% of the final stress in the unpropped one was locked in before the slab was structural. That page is about forces; this one is about stability, and the two failures of the same idea are not related except by their cause.

What redundancy is worth here

Take that one away and the load finds another routeA 6-panel pratt truss under 20 kN at each top node, before and after member 2 is removed. The load redistributes. The worst-affected survivor now carries 2.04 times what it did, and four members that carried nothing before are now working. Whether that is survival depends on how much spare capacity was there, which is a different question from whether the frame was strong enough.intactmember 2 removedworst demand 2.04×
Fig. 11 The structure that survives losing a member: a truss before and after a member is removed, with the load finding another route and the worst survivor at 2.03 times what it carried. A structure under erection is permanently in the left-hand state of this figure and progressively arriving at the right-hand one.

The relationship between redundancy and erection is not the one intuition supplies. A highly redundant finished structure is robust; the sequence that builds it passes through configurations that are less redundant than either end, and the least redundant configuration is not necessarily the earliest one. A frame with half its bracing installed can be less stable than the same frame with none, if the half that is in has attracted load to a path that is not yet complete.

Which is the argument for the erection sequence being designed rather than left to be worked out on site: the sequence is a series of structures, and each of them needs to be a structure.

Four states nobody has a drawing for

It is worth listing the specific configurations, because each is a real check that a permanent-works model cannot produce.

The beam landed and not yet decked. Its compression flange is unrestrained over its whole span. Every composite floor beam in a steel building passes through this state, and the check is a lateral-torsional one at the unbraced length of the span.

The frame erected and not yet braced. The bay containing the vertical bracing is often erected last, because the bracing gets in the way of the crane. Until then the frame’s stability comes from temporary guys or from the crane itself, and its effective lengths are the sway ones rather than the braced ones.

The floor cast and not yet cured. A concrete slab is a diaphragm when it has strength and a load when it does not — so for some days it is the heaviest thing on the frame and contributes nothing to holding the frame together. The diaphragm’s whole distribution argument waits on a cube test.

And the column erected and not yet loaded. A column is stabilised in part by the beams framing into it, and a column standing with two of its four beams connected is restrained about one axis and not the other. Its slenderness in that state is about the axis nobody computed.

What the four have in common is that each is a reduction of restraint, not of load. The load lines on a construction programme go up monotonically; the restraint lines do not, and the gap between them is where the risk is.

Where the model stops

Nothing here computes a temporary works design. Guys, plumbing struts, kentledge, tower cranes tied into the frame and the frame’s own use as a crane base are all real loads and real restraints, and they are outside every figure on this page.

The wind during erection is not the design wind. Codes allow a reduced return period for a short exposure, which reduces the pressure by perhaps 20% for a period of months. That is a real reduction and it is nothing like the factor of three the lateral system has lost.

The lifting condition has been ignored entirely. A member picked at two points is a beam with two overhangs; a member picked at one is a member in bending it was never designed for; and a long slender member picked flat is a lateral-torsional problem in its own right.

And the numbers here are one beam and one frame. The factor of 8.8 is a property of a 457 mm universal beam over 12 m; a shallower section restrained more closely loses less, and a deep plate girder loses more.

The one number to carry away

Stability capacities go as the inverse square of a length. That single fact is why removing a restraint is so much more expensive than removing a load, and it can be turned into a rule of thumb that survives without any of the arithmetic above.

Doubling an unbraced length quarters a capacity. Removing every second restraint from a beam does exactly that. Removing every restraint but the ends, on a beam braced at quarter points, divides the capacity by sixteen — before the warping term, which makes it worse still for a rolled section.

Against that, loads during construction fall by factors of two to five. There is no arrangement of those two numbers in which the temporary state is comfortably better than the permanent one, and there are many in which it is much worse.

The corollary is the useful part. The cheapest erection stability measure is always a restraint, never a strengthening. A temporary tie at mid-span of an unrestrained beam costs almost nothing, needs to be stiff rather than strong, and buys a factor of four. Making the beam heavier to survive being unrestrained buys a factor equal to the weight added. The whole of temporary works design is that comparison, made repeatedly.

What the pictures cannot show

Every figure on this page draws a finished structure with something removed. What actually happens on a site is a structure being added to, with each addition changing the whole, and no static figure has a way to show a load path in the process of being connected.

Nor can they show the thing that makes this subject difficult in practice: the erection condition is decided by a sequence that is chosen after the design is complete, by people who were not part of it, and it is checked — when it is checked — against a model built for a different purpose.

And the ratios quoted are for one moment in the sequence. A partly erected frame passes through hundreds of configurations, and the governing one is not usually the one anybody would have chosen to draw.

The ladder from here

Later rungs on this anchor: temporary bracing design, and how much of the permanent bracing’s job it has to do. The lifting analysis of a long member, including the two-point pick and the effect of sling angle on the compression it induces. Balanced cantilever construction, where the temporary condition governs the whole design of the permanent structure. Formwork and falsework as structures in their own right, which they legally are. Wind on a partially clad frame, where the pressure coefficients are not the finished building’s. And the historical case: the great majority of structural collapses happen during construction rather than in service, and the ones that are remembered — Quebec, Tacoma’s erection, the box girder bridges of 1970 — are remembered because each of them found a state the design had not considered.

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.

BracingConstruction sequenceEffective lengthErection stabilityJoint stiffnessLateral restraintLateral torsional bucklingLoad pathOverturningRobustnessSecond orderSpace frameTemporary worksUtilisation