Deflection

Built to the wrong shape on purpose

A cambered beam is fabricated curved upward so that load bends it down to something like straight. Nothing in the analysis changes, no stress anywhere is altered, and almost every mistake made with it is a bookkeeping mistake about which loads count.

Assumes Stiffness is not strength, and usually it is the one that governs, The structure that was never complete and The deflection that arrives three years late.

Nothing on a construction site is straight, and one of the crooked things is crooked deliberately. A cambered beam leaves the fabricator’s shop bent upward by a chosen amount, is bolted into a frame that is nominally level, and is then loaded until it is nearly straight. It is one of the few operations in structural engineering that alters no force, no stress and no capacity, and it is also one of the few that is got wrong routinely — because everything about it is bookkeeping, and the books have four columns nobody agrees on.

Cambered against the wet loadA 12 m composite beam whose flexural rigidity rises from 94 to 260 kN·m² when the slab sets, so the first two loads are carried by the bare steel and the rest by the composite section. Fabricated with 25.3 mm of camber, it moves through -20.7, 0.0, 7.5, 12.7 mm as the four stages arrive — 0.0 mm on the day the slab is poured, and 12.7 mm at the end, which is one part in 947 of the span. The largest curvature it ever has is 25.3 mm of hog, and it has that with nothing on it. Every shape is drawn at the same exaggeration and the drawing is a diagram of a proportion: the vertical scale is 119484 times the horizontal.levelas fabricated: 25.3 mm of camber-20.70.07.512.7self-weight of the steel: 4.6 mm on EI = 94wet concrete: 20.7 mm on EI = 94finishes and services: 7.5 mm on EI = 260imposed load: 5.2 mm on EI = 260
Fig. 1 A 12 m composite beam cambered against the loads it carries as bare steel. The faint curve is the shape it was fabricated to, 25.3 mm of hog; the four solid curves are what a spirit level reads after each stage of loading. It is flat on the day the slab is poured and finishes 12.7 mm in sag, which is one part in 945 of the span.

The first thing to be clear about is what has and has not been done to the steel.

A change of shape is not a change of stress

Bend a beam elastically with a load and it acquires curvature and stress together, in the fixed ratio M=EIκM = EI\kappa. Fabricate a beam already curved — by rolling it, by heating one flange, by cutting the web to a curve before welding — and it acquires curvature with no stress at all, because there is no moment anywhere on it. The shape is its unstressed shape, and every subsequent calculation is made from that shape as the datum.

So a cambered beam and a straight one of the same section carry the same load with the same moments and the same fibre stresses. There is nothing to compute; the generator behind these figures returns exactly zero for the difference, which is worth returning as a number rather than asserting in prose, because it is the property every misunderstanding of camber denies.

What changes is where the beam is. That is a serviceability matter and nothing else, and serviceability is usually what governs — so a member’s whole reason for being the size it is may be a limit that camber addresses without touching the strength calculation at all.

The beam that is two beams

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. 2 The staged construction this collection has already drawn: a member whose section changes while it is being loaded, so that superposition has to be done stage by stage rather than on the total. Camber is the same bookkeeping asked about shape instead of about stress.

The complication that makes camber interesting is that a composite floor beam has two different flexural rigidities during its own construction. Before the slab sets, the steel section is on its own: here EI=94,000EI = 94{,}000 kN·m². Afterwards the slab acts with it, and EI=260,000EI = 260{,}0002.77 times as stiff, from concrete that was already sitting on the beam as a dead weight before it did any structural work at all.

Two beams, or one beam four times as stiffTwo 200 × 150 planks spanning 4 m under 6 per millimetre. Loose, they have 112.5×10⁶ mm⁴ between them and deflect 16.2 mm, with the two faces at the interface sliding past one another. Bonded, the pair has 450.0×10⁶ — exactly 4 times as much, because doubling a depth cubes — and deflects 4.0 mm at half the extreme-fibre stress. Nothing was added but a restraint on slip. With connectors of stiffness 200 the same beam deflects 5.4 mm, which is 89% of the way from one bound to the other.loose: two beams, and the faces slide16.2 mmbonded: one beam, and the faces cannot4.0 mmI × 4with connectors at k = 200: 5.4 mm, 89% composite
Fig. 3 Where that factor comes from: two pieces bending separately against the same two bonded into one section. The shear connectors on a composite beam are the restraint on slip that makes the second picture true, and until the concrete has set there is nothing to restrain.

So the four stages of the beam’s life divide into two by stiffness, not by kind:

Stage Load Carried by Movement
self-weight of the steel 1.6 kN/m bare steel 4.60 mm
wet concrete 7.2 bare steel 20.68
finishes and services 2.4 composite 7.48
imposed load 5.0 composite 5.19

The third row carries a long-term multiplier: it is sustained, the concrete creeps under it, and three years later the deflection is three times what it was on the day. That is the whole of the 7.48 mm — 2.49 mm elastic and 4.99 mm arriving over the following decade.

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 3.00, after five years by 3.29, and it approaches 3.38. 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: ×3.005 years: ×3.29the deflection the calculation gives
Fig. 4 The creep coefficient against time for the concrete in that third row. Most of it arrives in the first year and it is still accruing at ten thousand days, which is why a camber decision made about elastic deflections is a decision about the wrong number.

Which free body produced the number

Each row of the table is a separate analysis of a separate beam. Cut the member at mid-span at the moment the wet concrete is placed: the free body carries 8.8 kN/m over 12 m, the section on the cut is the bare steel one, and 5wL4/384EI5wL^4/384EI with EI=94,000EI = 94{,}000 gives 25.28 mm of cumulative sag. Cut the same member after the finishes are on and the cut face is a different section — a composite one, with the neutral axis up in the slab — and the same formula with EI=260,000EI = 260{,}000 gives 2.49 mm for the 2.4 kN/m.

The two cuts are through the same beam at the same station and they reveal different sections, which is the fact all camber bookkeeping turns on. Superposition still holds, because each increment is elastic; it just cannot be applied to the total load, because there is no single section the total load was ever carried by.

Four rules and what each leaves behind

Four camber rules, and what each leaves on the finished beamThe same 12 m composite beam, cambered against four different things, followed through its own load history. Positive is a sag and negative a hog, and the point at the left of each line is the shape it was fabricated to. Cambering against the wet concrete leaves 12.7 mm of sag at the end and a flat beam on the day the slab is poured; cambering against the total load leaves the beam dead flat when fully loaded and hogged 37.9 mm — one part in 316 of the span — before anything is on it at all.1234403020100-10-20-30-40stage in the beam's lifeshape (mm, sag positive)against noneagainst wetagainst deadagainst total
Fig. 5 The same beam cambered against four different things, followed through its own load history. Positive is a sag and negative a hog; the point at the left of each line is the shape the beam was fabricated to. The four lines never cross, because they differ by a constant — which is the whole content of camber.

Against nothing. The beam finishes 37.9 mm down, which is one part in 317 of the span and outside every deflection limit worth having. Under dead load alone it is at 32.8 mm, so the floor is visibly dished before anybody moves in.

Against the wet concrete, 25.3 mm. This is the common rule and the figure shows why: the beam reads exactly zero at the end of the second stage, so the slab is poured to a level top surface and the concrete thickness is uniform. It finishes at 12.7 mm, one part in 945.

Against the dead load, 32.8 mm. Flat under everything permanent, 5.2 mm of sag under the full load, and 7.5 mm of hog on the day of the pour — which means the slab must be poured thicker in the middle, and the extra concrete is a load nobody counted.

Against the total load, 37.9 mm. Dead flat when fully loaded and hogged at every other moment of its life. Its worst hog is 37.9 mm, with nothing on it.

That last line is the finding, and it generalises: a cambered beam is at its most curved when it is empty. The largest departure from straight that any of these members ever shows is the one it was built with, and it shows it on the day it is erected — when the cladding is being set out against it, when the fit-out contractor is measuring from it, and when nobody is thinking about deflections at all.

The rule that is chosen by what is being measured from

The choice between the four is not a structural question and there is no structurally correct answer. It is a question about which stage somebody is going to lay a straightedge on, and the limit that straightedge is checked against is written about the finished member rather than about any moment in its construction.

Which limit arrives firstUtilisation of the strength limit and of the deflection limit, against span. Strength grows as the square of the span and deflection as the fourth power, so the two cross — and past the crossing a beam is sized by how far it moves rather than by what it can carry.0.60.811.21.41.61.8200.511.5span, relative to the firstthey cross heredeflection runs out at 1.40strength runs out at 1.54the limitstrengthdeflection
Fig. 6 The strength and serviceability limits on the same member, and which of them binds. Camber moves neither line: it changes only the ordinate the serviceability limit is measured from, which is why a beam can be made acceptable by camber without being made stronger in any respect.

Three practical constraints narrow it, and none of them is in the analysis.

Concrete is placed to a level, not to a thickness. If the beam is hogged when the slab is poured, the slab is thin over the beam and thick between them, and the extra concrete in the middle of the bay is real load. Cambering against the wet concrete makes that term vanish, which is the reason the rule is common rather than an argument that it is right.

Fabrication tolerance is a substantial fraction of the number. A camber is a length quoted to a millimetre on a member whose own second moment of area is known to a few per cent, and The camber of 25 mm on this 12 m member is 0.2% of the length, and the tolerance on a rolled and cambered beam is commonly ±5 mm or more. A rule that distinguishes 32.8 mm from 37.9 mm is distinguishing quantities inside the noise.

Camber cannot be removed. It is fabricated in. A beam cambered for a load case that then changes is a beam with a permanent hog, and a structure is rarely finished in the sequence it was designed in.

The one case where the sign matters structurally

The water that will not run offWater depth against sag at the middle of the bay, for a roof bay starting with a reversed construction camber of 0.002. 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 depth at which the bay fills faster than it stiffens, and which the roof bay therefore never attains. The perfect roof bay, drawn for comparison, sits on the vertical axis until it arrives there and then has no answer at all.00.0050.010.0150.020.02500.20.40.60.81sag at the middle of the baywater depth ÷ critical depthλ = 1.00, approached and never reachedreversed construction camber: δ₀ = 0.002
Fig. 7 The ponding instability drawn on the same axes as a column’s imperfection growth, because it is the same equation: sag admits water, water causes sag, and the two feed each other with a multiplier of 1/(1 − λ). A reversed camber — a beam built with a hog on a flat roof — is a negative initial sag, and it moves the whole curve.

Almost everywhere, camber is cosmetic. On a flat roof it is not, because there the deflected shape decides the load.

Water collects in the sag, the extra weight increases the sag, and the loop closes with a gain that depends on how stiff the bay is relative to how fast it fills. The essay on ponding sets that out; what belongs here is the consequence for camber. The amplification is 1/(1λ)1/(1-\lambda) acting on the initial sag, so a bay built with a hog starts with a negative initial sag, and the same multiplier that would have magnified a defect now magnifies a margin.

That is the only argument on this page where camber changes a force, and it changes it by changing the load rather than by changing the member.

Camber, precamber, and the thing that is not camber

Three operations get the same word and only one of them belongs here.

Camber is a fabricated change of unstressed shape. No stress, no force, no capacity.

Prestressing is a fabricated change of stress, usually accompanied by a change of shape. Putting the stress in backwards before the load arrives is a real structural operation with real stresses, and a prestressed member’s hog is a consequence of it rather than the point of it.

Jacking, packing and propping change the load path during construction, and therefore change the forces. Propping a composite beam while the slab sets moves the wet-concrete row of the table from the bare-steel column to the composite one and reduces the total deflection by about 13 mm here — which camber cannot do, because camber does not move a load. The distinction matters most where a member is handing its load to something beneath it, since a transfer structure’s settlement is inherited by everything above and a camber is the cheapest way to give some of it back.

A beam of two stiffnesses has one diagram with a step in itA 6 m cantilever whose flexural rigidity is 2 times larger beyond 3 m — a deep root and a shallow tip — under a tip load of 10. The M/EI diagram therefore has a step in it at a station where nothing about the moment changes, and the method adds two areas where an integration would need two cases and two more constants. The shaded area is 157.52, which by the first theorem is the change of slope along the whole member. Its centroid is at 1.714 m, and the first moment about the tip is 675.07 — which by the second theorem is the deviation from the tangent, and for a cantilever that tangent is horizontal, so it is the deflection itself. Integrating the curvature twice instead gives 720.00.10EI ÷ 2 beyond herecentroid at 1.71 mM/EIarea = 157.52 · first moment = 675.07by double integration: 720.00
Fig. 8 The bookkeeping in its general form: a member whose flexural rigidity is not constant, drawn as a step in the M/EI diagram. A composite beam’s step is in time rather than along the length, and every camber calculation is the same sum of areas evaluated stage by stage.

The number that decides how much it matters

Camber is worth arguing about in proportion to how large the deflections are, and deflections are decided by span before they are decided by anything else.

Deflection goes as the fourth power of the spanDeflection against span for a constant load intensity and section, with two slower relationships drawn faintly behind it for comparison: the load itself, which grows in proportion to the span, and the bending moment, which grows as its square. Doubling the span multiplies the deflection by sixteen, while the moment only quadruples.11.522.533.54050100150200250300span, relative to the first16×81×256×moment: the squareload: the first powerdeflection: the fourth
Fig. 9 Deflection against span at constant section and constant load per metre. Doubling a span multiplies the movement by sixteen, so a rule that is a nicety at 6 m is a fabrication instruction at 12 m and a governing constraint at 18 m.

The 12 m beam above moves 37.9 mm uncambered. The same section and loading at 6 m would move 2.4 mm, at which point every one of the four rules produces a beam nobody could distinguish by eye and the whole question is not worth the fabricator’s time. At 18 m it moves 192 mm, which is a member that cannot be built straight in any useful sense.

So camber is a long-span practice, and the threshold is a length rather than a ratio. The common trigger — camber beyond about 10 m of span, or beyond about 20 mm of dead-load deflection — is the fourth-power law meeting a tolerance, and it moves whenever either does.

The deflected shape is the moment, integrated twiceA loaded beam with its deflected shape above and its bending-moment diagram below. The shape was obtained by integrating the moment twice and fitting the constants to the supports; the vertical scale is exaggerated enormously.the largest movement, at x = 4.00momentdrawn at roughly three hundred times the real deflection —a beam at its serviceability limit moves about a three-hundredth of its span
Fig. 10 The shape being offset, drawn at an exaggeration its own caption states. Every profile on this page is that curve translated vertically by a constant, which is the whole geometric content of camber and the reason the four rules never cross.

Where the model stops

Every deflection above is elastic and small. The camber itself is 0.2% of the span, so the change of geometry it produces alters nothing about the analysis — but a deep-cambered member, a curved girder or an arch is a different object, and its curvature is part of its structural behaviour rather than an offset to it.

The creep multiplier is a single number standing in for a process. The 2.0 used here belongs to a particular concrete, a particular age at loading and a particular humidity, and the honest range is roughly 1.5 to 3.0. The rows of the table move with it, and so does every camber rule that includes the third one.

Nothing here accounts for the slab’s own restraint. A composite beam’s long-term deflection is complicated by shrinkage of the slab, which curves the member downward with no load applied at all — an imposed deformation rather than a load, and one of the same order as the creep term on a lightly loaded floor. A restrained member develops force rather than movement, and a composite slab is restrained by the beam it is cast onto.

Fabrication is not exact and neither is erection. A cambered beam that is bolted into a frame whose columns are not plumb acquires a shape nobody computed. The four rules differ by a few millimetres and the site differs from the drawing by a few millimetres, which is a fact about the usefulness of the fourth decimal place rather than about the method.

And camber does not survive a change of section. A member that is later strengthened, or that cracks, has a different stiffness and therefore a different deflection under the same remaining load, while its fabricated shape is fixed.

What the pictures cannot show

Every profile on this page is drawn at an exaggeration of about a thousand. The 12 m beam moves 37.9 mm at its worst; drawn to scale on the page it would be a straight line with a bump one twentieth of a millimetre high, and every distinction the figure is about would be invisible. The honest reading of the shapes is the ratio in the caption — one part in 945, one part in 317 — and not the curvature.

The stage curves are drawn as parabolas of the computed amplitude, which is what a uniform load gives to within about a per cent. The real profiles differ slightly from each other in shape as well as in size, because a point load and a spread load bend a beam differently, and no drawing at this exaggeration can show the difference.

And the fabricated shape is drawn as a smooth curve. A cambered beam is often not smooth: heat-cambering works in discrete passes, and press-cambering in discrete bites, so the real unstressed shape is a chain of straight segments with kinks between them. The kinks are within tolerance and they are not within the drawing.

The ladder from here

Later rungs on this anchor: camber in composite bridge girders, where the deck pour sequence makes the load history genuinely two-dimensional and the camber diagram is a surface. Precamber of trusses, where the shape has to be built into member lengths rather than into a curve, and where a millimetre on one chord moves the whole profile. The interaction of camber with lateral-torsional stability during erection, since a cambered beam hanging from two points is not a straight member. Camber of concrete members by prestress, which is the same shape obtained by an operation that does change stresses. Setting-out and tolerance, and the survey question of what “level” means on a 60 m floor plate. And the long-term case where the third and fourth stages are separated by decades, so that the beam a reader sees is at a point on a creep curve nobody chose.

The word itself is old and comes from the same root as chamber — a vault, an arched space — by way of the French cambré. Which is the right etymology for the operation: it is the arch made small enough to be invisible, and used for its shape rather than for its structural action.

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.

Composite actionConstruction sequenceCreepDeflectionDeflection limitFlexural rigidityImposed deformationPondingProppingServiceabilitySuperpositionSustained load