The most dangerous day is before it is finished
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.
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.
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. contains and a warping term, and both are divided by the unbraced length — so the answer scales roughly as 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. That inverse square is the whole reason restraint is expensive to remove, and it is visible without any beam at all.
A column loses its way along that row one restraint at a time, and a partly erected structure is a column somewhere to the right of where its calculation put it.
A brace makes the same point at a smaller scale: one at mid-height takes a column’s critical load from 9.87 to 39.48 EI/L², exactly four times, because the buckling length halves. It needs a stiffness of about 159 EI/L³ to do it, which is three times the column’s own transverse stiffness and still nothing at all in strength terms — a brace need not be strong, and it 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.
A connection’s classification is a comparison with the beam it serves rather than a property it carries on its own — a joint is neither pinned nor rigid until the member is named — and the same bolts at a fraction of their preload sit somewhere quite different in that comparison from where they will sit when the frame is finished. The effective length reads the comparison directly.
Every point on both curves is the lowest eigenvalue of the assembled frame. Nothing is read off a nomogram, which matters here because the right-hand end of the sway curve is where a partly erected frame lives and is exactly where the published charts stop.
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.
The difference between the two pictures is one horizontal restraint. It is also, on most sites, the last thing installed.
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 amplification is 1/(1 − P/P_cr), so at 20 per cent of the buckling load a deflection is multiplied by 1.25 and is manageable, and at 60 per cent by 2.5 — a load that makes itself worse as soon as the buckling load it is measured against has fallen. Both terms of that ratio move during erection, and they move the same way.
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
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.
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.
A frame can satisfy m + r = 2j exactly and fold anyway, which is a count that does not see the fold; and a partly erected frame is one member short of something by definition, which is the condition that failure lives under.
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.
There is a subtler version of the same trap, and it is the one that makes a half-finished sequence worse than an unstarted one. Effective length is not a property of a column. It is a property of the storey the column stands in.
The factor rises as the square root of the load ratio, exactly. At the storey drawn — three leaning columns carrying 70 per cent of the gravity load — it is 3.61, which is off the end of every published alignment chart, and the leaning columns themselves, which a designer would take at 1.0 for pinned ends, are at 2.60. An erection sequence that stands the leaners before it braces the stiff bay has built this figure without meaning to.
What a structure carries also depends on what was present when the load arrived, which is the structure that was never complete — the propped and unpropped composite beam, where 62 per cent of the final stress in the unpropped one was locked in before the slab was structural. That argument is about forces and this one is about stability, and the two share a cause and nothing else.
What redundancy is worth here
A structure that survives losing a member does so because the load finds another route, and the worst survivor there picks up 2.03 times what it had been carrying. A structure under erection is permanently in the before state of that comparison and is progressively arriving at the after 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.
The load that does not go away
The comfort in “the loads are lower during construction” comes from the imposed load, the finishes and the services all being absent. The self-weight is not, and it is at its full value from the moment a member is placed.
So the reduction depends entirely on how much of the design load was dead, and it varies in exactly the wrong direction.
The shape of that force is the only thing in this subject that works in the erector’s favour. A column carries its own weight 3.18 times better than it carries the same total as a tip load, because most of the weight is near the base, where the buckle is not. The height at which a section falls over unaided is then a cube root and rises slowly: 52 m at a radius of gyration of 80 mm, and only 82 m at twice that.
An ordinary floor beam might be 40 per cent permanent and 60 per cent imposed, so during erection it carries 40 per cent of its design load — a factor of 2.5 in hand.
A long-span roof beam is 80 per cent or more permanent, because there is very little imposed load on a roof and a great deal of steel. Its reduction is a factor of 1.25.
And the long-span roof beam is the one that is deep, slender, unrestrained until the purlins arrive, and losing a factor of eight or more in stability capacity. The load reduction is smallest exactly where the restraint loss is largest, and the two do not merely fail to cancel — they are correlated the wrong way, because both follow from the member being long.
The same reasoning picks out the other members at risk without any calculation: precast units, whose only load during handling is their own weight; arch and cantilever segments, likewise; and any transfer member large enough that its own steel is most of what it carries. In each case the phrase “the loads are lower” is nearly empty.
The wall that is a sail before it is a wall
The concrete version of the same argument has different numbers and a sharper edge, because a freshly cast element has almost no capacity of its own to fall back on.
Take a wall panel 3 m high and 6 m long, 200 mm thick, cast or placed and not yet connected to a floor. Its weight is kN, and standing on its base it has a restoring moment of that weight times half its thickness:
Now put a modest wind on it — 0.6 kN/m², which is an ordinary breezy day rather than a design storm. The force is kN at mid-height, and the overturning moment about the base is
Nearly twice the restoring moment. The wall falls over, in a wind nobody would remark on, and nothing about the concrete’s strength enters the arithmetic anywhere — it is an overturning check, and weight is the only thing resisting it.
Two features of that make it the characteristic hazard of concrete construction rather than a curiosity. The wall is at its most vulnerable when it is complete as an element and not yet part of a structure, which is a state that lasts hours to days and has no drawing. And the remedy is a prop, not a thickness: doubling the wall’s thickness doubles both the weight and the lever arm and quadruples the restoring moment, which would work and costs a wall; a raking prop costs a strut and a fixing.
Which is the same conclusion the steel argument reached, from a completely different failure mode. The temporary condition is fixed by restraint, and the permanent one by strength, and a designer who has only checked the second has checked the easier of the two.
There is a third member of the family worth naming because it is the one that is never drawn at all: the stack. Precast units stored on end, formwork panels leaned against a wall, reinforcement cages standing before they are placed, a row of columns laid out ready for lifting. Each is an object whose stability depends on a prop, a chain or a neighbour, whose weight is fully present, and which appears on no drawing produced by anybody. The arithmetic above applies to every one of them unchanged, and the only reason it is not done is that nothing in the design process asks for it.
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.
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.
- Counted, not checked bracing · effective length · second-order
- Held everywhere, and it forgets its length bracing · effective length · lateral-torsional buckling
- Hung from the top, and nine per cent lighter construction sequence · load path · robustness
- The brace on the wrong flange bracing · effective length · lateral-torsional buckling
- The cable that is a spring construction sequence · load path · second-order
- The columns that lean bracing · load path · robustness
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