Deflection

The deflection that belongs to the support

A beam calculation answers a question about a beam sitting on things that do not move. Real ones sit on bearings, on other beams and on columns that shorten, and every one of those is a spring in series with the member — so a deflection is the sum of two things and only one of them is a property of the beam.

Assumes Stiffness is not strength, and usually it is the one that governs, One support too many, and what it costs to know and The beam that sits on the ground.

A deflection calculation begins by drawing a beam with a triangle under each end. The triangle means the point does not move, and every result that follows is a statement about a beam whose ends are where they were.

Almost nothing is supported like that. A secondary beam sits on a primary beam, which bends. A primary beam sits on a column, which shortens. A column sits on a pad, which settles. A precast unit sits on a bearing, which compresses. Each of those is a spring, each is in series with the member above it, and a series combination is dominated by whichever is softer.

How much of a deflection belongs to the beam. The share of the total deflection that is the beam's own bending, against the stiffness of what it sits on. A 8 m beam on two supports under a uniform load: on rigid supports every millimetre is the beam's, and the share falls away as the supports soften until almost none of it is. The beam drawn beside this figure sits at 51% — so 49% of what it does is happening somewhere a beam calculation never looks. The two flexibilities are in series, which means the softer one governs and stiffening the other buys nothing.
Fig. 1 The fraction of a beam’s total deflection that is its own bending, against the stiffness of what it sits on. On rigid supports every millimetre is the beam’s; the share falls away as the supports soften; and the 8 m beam marked on the curve, sitting on supports of 7,875 kN/m, is at 51% — so 49% of what it does is happening somewhere a beam calculation never looks. The curve is the same shape for any beam. Only where a particular beam sits on it changes.

The arithmetic, on a floor

Take an 8 m secondary beam of EI=84,000EI = 84{,}000 kNm², carrying 20 kN/m. On rigid supports it deflects

δ=5wL4384EI=12.7  mm\delta = \frac{5wL^4}{384EI} = 12.7\;\text{mm}

which is span over 630 and comfortable.

Now put it on primary beams of the same section, spanning 8 m, receiving it at their mid-spans. A simply supported beam’s stiffness at mid-span is 48EI/L3=7,87548EI/L^3 = 7{,}875 kN/m. The secondary delivers 80 kN to each, so each primary goes down by

807,875=10.2  mm\frac{80}{7{,}875} = 10.2\;\text{mm}

and the secondary’s mid-span, which sits on top of that, ends up at 12.7+10.2=22.912.7 + 10.2 = 22.9 mm — span over 350, which is not comfortable and would fail most deflection limits for a floor supporting brittle finishes.

Forty-four per cent of that movement is not the secondary beam’s. It is the primary beam beneath it, doing exactly what it was designed to do.

The two halves of that number obey different laws, which is the first sign they are different quantities. The 12.7 mm follows span to the fourth: double the secondary’s span and its own deflection is multiplied by sixteen. The 10.2 mm does not follow it at all — it is a reaction divided by a stiffness, linear in the load, and the span it contains is the primary’s rather than the secondary’s. Lengthening the beam whose deflection is being checked changes one term by a factor of sixteen and the other by a factor of two.

Which free body produced the number

The two contributions come from different free bodies, and keeping them apart is the whole method.

Cut the beam free of its supports and apply the reactions. The relative deflection of mid-span with respect to a straight line joining the two support points is 5wL4/384EI5wL^4/384EI, and it is a property of the beam and its load alone.

Now take the support, with the reaction applied to it. It moves by R/kR/k, and kk is a property of whatever is underneath — a beam, a column, a bearing pad, a pile.

The absolute deflection of any point on the beam is the sum: the movement of the line joining the supports, plus the beam’s own departure from it. The two do not interact, provided the structure is determinate — which is why the calculation is an addition rather than a solve.

The first of those two free bodies is what every standard method computes. One deflection without solving everything evaluates it as the integral of Mmˉ/EIM\bar{m}/EI along the member, and extending that integral to include the supports needs one extra term per support, RˉR/k\bar{R}R/k — the same virtual-work statement with springs added to the list of things storing energy. Nothing about the method resists the extension; it is simply that nobody writes the extra term down, because the support does not appear on the sheet the beam is being sized on.

How much of a deflection belongs to the beam. The share of the total deflection that is the beam's own bending, against the stiffness of what it sits on. A 8 m beam on two supports under a uniform load: on rigid supports every millimetre is the beam's, and the share falls away as the supports soften until almost none of it is. The beam drawn beside this figure sits at 84% — so 16% of what it does is happening somewhere a beam calculation never looks. The two flexibilities are in series, which means the softer one governs and stiffening the other buys nothing.
Fig. 2 The same curve with the marker moved to a support five times stiffer, 40,000 kN/m instead of 7,875. The share belonging to the beam rises to 84%, which is the state a standard beam calculation silently assumes it is in — near enough to the rigid end that the second free body can be ignored. The assumption is not wrong here; it is simply a claim about a support stiffness, made by a sheet that never names one.

Two flexibilities in series

Write the two contributions as flexibilities — deflection per unit load — and the shape of the answer is fixed:

δtotal=(fbeam+fsupport)W\delta_{total} = \left(f_{beam} + f_{support}\right) W

Flexibilities add. Stiffnesses do not; they combine as 1/k=1/k1+1/k21/k = 1/k_1 + 1/k_2, which is the harmonic sum this collection meets whenever two mechanisms act one after the other along a load path.

A joint is springs in series. The five components of an end-plate joint, with each bar the flexibility it contributes. The column flange in bending is 39.62% of the total on its own, and doubling its stiffness raises the joint's by a factor of 1.25 — while doubling the stiffest component buys 1.05. The joint's rotational stiffness is 25227.71 kN·m per radian.
Fig. 3 A joint made of springs in series, where the same arithmetic is the whole design method: a connection’s rotational stiffness is the harmonic sum of its components’, and the softest component decides it. A beam on a support is that method with two components instead of five.

Three consequences follow, and each answers a question a designer actually asks.

The softer flexibility governs, and improving the other one is nearly wasted. Doubling the secondary beam’s second moment halves its own 12.7 mm to 6.4 and leaves the 10.2 alone: 22.9 becomes 16.5, a 28% improvement for twice the steel.

There is no point making either much stiffer than the other. The table below is the whole design guidance on the subject:

support stiffness total deflection the beam’s share
1,000 kN/m 92.7 mm 14%
2,000 52.7 24%
4,000 32.7 39%
7,875 22.9 56%
16,000 17.7 72%
40,000 14.7 86%
rigid 12.7 100%
How much of a deflection belongs to the beam. The share of the total deflection that is the beam's own bending, against the stiffness of what it sits on. A 8 m beam on two supports under a uniform load: on rigid supports every millimetre is the beam's, and the share falls away as the supports soften until almost none of it is. The beam drawn beside this figure sits at 12% — so 88% of what it does is happening somewhere a beam calculation never looks. The two flexibilities are in series, which means the softer one governs and stiffening the other buys nothing.
Fig. 4 And the other end of the table, at a support stiffness of 1,000 kN/m. The share belonging to the beam is 12%, so 88% of the movement is the support going down and the beam is very nearly a passenger. Deepening it here is the classic wasted effort: halving its own contribution takes 12% to 6% of a total that barely moves. The three markers on this one curve — 12%, 51%, 84% — are the whole design question, and which of the three a floor is at is decided by something that is not on its calculation sheet.

The two can be swapped for one another at a fixed rate. A support twice as stiff is worth exactly as much as a beam twice as stiff, when the two are equal — and worth twice as much when the support is the softer half. That exchange rate is the only design information a series combination contains, and it is available before either member has been sized.

And the limit has to be applied to the total. A deflection limit of span over 360 is about what a finish can tolerate, and the finish does not know which part of the movement belonged to which member. Checking the secondary beam alone against its own limit and the primary alone against its own is a check that both pass and the floor fails — a mistake that is easy to make because each member has its own calculation sheet.

What the limit is measured between

The section above ended by saying the limit has to be applied to the total, because the finish does not know which member the movement belonged to. That is right for some finishes and wrong for others, and separating the two is worth doing because it decides which of the two numbers a designer should be worrying about.

A deflection limit is a proxy for damage, and damage is caused by relative movement between the two points something spans between. A movement that carries a finish and both its ends down together does nothing to it at all. So the question is never “how far did the floor drop” but “how far did these two points move relative to each other”, and the answer depends on where the two points are.

Work through the same bay.

A partition running along the secondary beam, from one primary to the other, sees the secondary’s own 12.7 mm and none of the primary’s. Its two ends sit on the primaries and go down 10.2 mm with them; the partition is translated bodily and its sag relative to its own ends is the beam’s contribution alone.

A partition running across the bay, from a column to a point above the middle of a primary, sees the primary’s 10.2 mm and none of the secondary’s — because it is spanning between a point that does not move and a point that moves by the primary’s deflection.

A ceiling or a screed spanning the full bay diagonally, from column to column, sees the whole 22.9 mm, which is the case the earlier section described.

And perimeter cladding sees only the movement of the edge beam it is fixed to, which may be neither.

So there is no single deflection of a floor. There is a field of vertical movement over the plan, and a serviceability limit is a statement about the second difference of that field along one particular line — with a different answer for every direction a finish might run.

Two consequences follow and they cut in opposite directions, which is why the member-by-member habit survives at all.

The member check under-estimates. A secondary beam passing its own L/360L/360 at 12.7 mm is carrying a ceiling that is actually experiencing 22.9. That is the failure the earlier section warned about and it is real.

And the member check over-estimates. Applying the 22.9 mm total to a partition that runs along the beam is charging it for a rigid-body movement it never experienced. A floor condemned on a total that no finish in it actually sees has been condemned by an arithmetic convenience.

The specification that avoids both is one that states a relative deflection between named points — the drop of the middle of the bay relative to its corners, say — rather than a limit on any member. That is how the more careful cladding and partition specifications are written, and it is why a facade contractor asks for movements at fixing points rather than for a span-over-something.

There is a third case that belongs with the other two and is the one most often missed. A finish fixed to two different structures — a partition running from a floor slab up to the underside of the floor above, a stair landing spanning between a core and a floor plate, a lift door frame fixed to both the shaft and the slab — sees the difference between two independent movement fields, and neither member’s own check contains it. That is the same incompatibility a core and its columns produce at building scale, arriving one bay at a time.

The honest reason member limits persist is that they are cheap, they are checkable by the person who sized the member, and a floor that passes all of them is usually acceptable. The failures that do occur cluster exactly where this section predicts: at a finish whose span crosses the contributions of two different members, fixed to points that were checked separately by two people who each got the right answer to their own question.

In a continuous beam it moves the forces too

Everything above is determinate, so the support flexibility changes deflections and nothing else. Make the beam continuous and it changes the forces as well.

3 continuous spans against 3 simple ones. The bending moment in a continuous beam whose support 1 has settled by 0.01. Three curves: the moment the load causes, the moment the settlement causes on its own — dashed, peaking at 73.5, and in equilibrium with no applied load at all — and their sum, which is what the beam carries, peaking at 73.5 against 24.5 without the settlement. The settlement field is proportional to EI: a stiffer beam is punished harder for the same movement, which is the opposite of every intuition load-carrying gives.
Fig. 5 The support that moved: a continuous beam with one support 10 mm lower than the others, and the moment diagram it produces with no change to the load at all. A flexible support is a settlement whose size is decided by the reaction it attracts.

That last sentence is the whole difference between the two problems. A settlement is a known movement, imposed. A flexible support is a movement proportional to the reaction, and the reaction is proportional to the stiffness — so the two are coupled and the answer requires solving them together.

Three equally stiff supports under a uniform load, with the middle one attracting the most reaction:

supports end / middle / end share peak moment
rigid 18.8% / 62.5% / 18.8% 45.0
soft, equal 32.1% / 35.9% / 32.1% 73.9

The middle support is relieved from 62.5% of the load to 35.9%, and the span moments rise by 64% to compensate. Which is exactly the redistribution nobody chose, arriving through the supports instead of through the joints.

How much of a deflection belongs to the beam. The share of the total deflection that is the beam's own bending, against the stiffness of what it sits on. A 8 m beam on three supports under a uniform load: on rigid supports every millimetre is the beam's, and the share falls away as the supports soften until almost none of it is. The beam drawn beside this figure sits at 3% — so 97% of what it does is happening somewhere a beam calculation never looks. The two flexibilities are in series, which means the softer one governs and stiffening the other buys nothing.
Fig. 6 The same beam, the same load and the same supports, with a third support added under the middle. Continuity has taken almost all of the beam’s own bending away — its share falls from 51% to 3% — so 97% of what the beam does is now the supports moving. Making a beam continuous is one of the standard answers to a deflection problem, and this is what it does to the split: it removes the half of the movement the designer controls and leaves the half nobody measured.

There is a cousin of all this at the ends of the member rather than under them. A joint of finite rotational stiffness delivers only part of the fixed-end moment, and support flexibility and joint flexibility are the same phenomenon in two different freedoms — one a translation, one a rotation, and both springs the analysis usually replaces with a certainty.

The continuous version of the same idea

The ground pushes back hardest where the beam has gone down furthest. A strip 16.4 m long and 1 m wide on ground of subgrade modulus 50 × 10³ kN/m³, carrying 1000 kN at its centre. The beam settles 3.90 mm under the load and the ground pushes back in proportion — the arrows are k times the settlement above them, peaking at 195 kN per metre — so the pressure diagram is the settlement bowl and not an assumed distribution. The characteristic length 1/β is 2.56 m: the bowl crosses zero at 6.04 m, which is 3π/4 of it, and beyond that the arrows reverse because the beam has lifted off. By 8.05 m — one π/β — the disturbance is 4.3% of what it was, which is why the moment 641 kNm and the peak pressure 195 kN/m contain no length at all. The settlement is drawn 217 times full size — the real bowl is 3.90 mm deep over 16.4 m, about 1 in 4207 — and at true scale the beam would be a straight line.
Fig. 7 A beam sitting on the ground, where the springs are continuous rather than discrete and the same equation governs. Everything on this page is that problem with the foundation lumped at a few points, and the characteristic length that decides how far a load spreads has the same role as the stiffness ratio here.

The two problems are the same one at two densities. A Winkler beam has a modulus of subgrade reaction kk per unit length and a characteristic length 4EI/k4\sqrt[4]{4EI/k} that decides how far a load reaches. A beam on discrete springs has a stiffness kk at each support and a dimensionless ratio that decides how the load is shared. In both, the answer is a ratio of two stiffnesses and neither absolute value matters.

Everything a beam on the ground does is a function of βx. Deflection, moment and shear along a beam on an elastic foundation, each divided by its own value immediately under the load and drawn against βx. Contact pressure is k times deflection, so it is the same curve as the first. The stations are exact and none of them depends on the load or on the beam: the moment crosses zero at βx = π/4, which is 2.01 m here; hogging peaks at βx = π/2 at 20.8% of the sagging moment; the deflection crosses zero at 3π/4, or 6.04 m, past which the beam lifts; and by βx = π the uplift is 4.32% of the settlement. One characteristic length along, the deflection is already down to 51% of its peak, and by three it is 4.2%. That is what it means for a raft to stop being a beam: past two or three of these lengths, nothing knows the load happened.
Fig. 8 And the ratio drawn as the only variable there is. Deflection, moment and shear along a beam on the ground, each divided by its own value directly under the load and plotted against βx\beta x — so no load and no beam appears anywhere on the axes. The moment crosses zero at βx=π/4\beta x = \pi/4, the deflection at 3π/43\pi/4, and by βx=π\beta x = \pi the uplift is 4.32% of the settlement. One characteristic length away the deflection is already 51% of its peak and by three it is 4.2%. A beam on discrete springs has the same property in coarser form: past two or three supports, nothing knows the load happened.

Where else it decides something

Sideways. The floor plate distributing a lateral load to its walls is this problem turned on its side: the plate is the beam, the walls are the springs, and the ratio of the two flexibilities decides whether the load is shared by stiffness or by tributary span. Every conclusion on this page transfers to it with the word “deflection” replaced by “drift”.

Bearings. An elastomeric bearing under a bridge girder compresses by a millimetre or two under load and is deliberately soft in shear. Its vertical stiffness is part of the girder’s deflection and its rotational flexibility is part of the girder’s end restraint.

Piles and pads. A column on a pile group settles, and a frame on piles of different lengths settles differentially. In a rigid frame that is a redistribution, and it is one of the few cases where a geotechnical stiffness ends up in a bending moment.

Transfer structures. A column landing on a transfer beam has a support whose stiffness is the beam’s, which is orders of magnitude softer than the ground. Every column above it is on a spring, and the loads redistribute up the building — a column that would have taken its share by area takes it by stiffness instead, and the one over the middle of the transfer beam takes least of all.

And a column that shortens. In a tall building the column beneath a floor is getting shorter under everything built above it, which is a support movement arriving on a schedule rather than under a load. It is the same term in the same sum, with a creep coefficient in place of a stiffness.

Which of the two limits it threatens depends on the determinacy. Support flexibility is almost entirely a serviceability matter in a determinate structure and a strength matter in an indeterminate one, so whether it can be ignored is a question about the frame rather than about the member — and stiffness is not strength is the distinction it is trading on.

The rule that comes out of it

Two flexibilities in series produce a design rule short enough to carry, and it is the opposite of the one intuition supplies.

Never improve the stiffer half. If the beam is contributing 56% of the deflection and its support 44%, the two are already well matched and neither improvement is efficient — every 1% of improvement to either buys about half a per cent overall. If the beam is contributing 14% and the support 86%, work on the support and leave the beam alone entirely; doubling the beam’s stiffness in that state improves the floor by seven per cent.

And the matched case is the expensive one to improve. That is the awkward corollary. A series combination whose two terms are equal is at its worst for marginal effort — there is no soft term to fix — and the only route left is to change the arrangement: shorten the primary’s span, add a column, or turn the two-way grid into a one-way system so that there is no primary beam under the secondary at all.

Which is why the answer to a floor at span over 350 is so often a layout change rather than a section change. The section change is available and is being asked to fix less than half the problem.

Where the model stops

A support is not a linear spring. A bearing pad stiffens as it compresses; soil stiffness depends on the stress level and on the loading history; a bolted connection has slack before it has stiffness. A single number kk is a linearisation about an operating point.

The support’s stiffness depends on what else is on it. The 7,875 kN/m used above is the primary beam’s stiffness at mid-span with nothing else applied. Load the primary elsewhere and the secondary’s support moves for reasons that have nothing to do with the secondary — which is why a floor grid is really one structure and its members are analysed as though they were several.

Torsional and rotational flexibility have been ignored. A support that rotates as well as translating changes the beam’s end conditions, and for a continuous beam that is a larger effect than the translation.

And the two contributions have been added. That is exact for a determinate beam and approximate for anything else: in a continuous beam the support movements change the reactions, which change the support movements, and the sum is the result of a solve rather than an addition.

Where the number comes from, and why nobody has it

The whole of this page is a ratio of two flexibilities, and one of the two is routinely unknown to within a factor of two.

A beam’s own flexibility is L3/48EIL^3/48EI or thereabouts, and every term in it is on a drawing. A support’s is not. It depends on what the support is made of, on what else is bearing on it, on whether a bolt has taken up its clearance, on how a pad was bedded and on whether a pile has been loaded before.

The consequence is that support flexibility is very often handled by assuming one of the two limits — rigid, or a nominal spring — and checking whether the answer changes. That is a reasonable procedure and it has a specific failure: the two limits give the same forces in a determinate structure and very different ones in an indeterminate one, so the sensitivity check passes on the member and fails on the frame.

The honest position is that a beam’s own deflection is a calculation and its support’s is an estimate, and adding a calculation to an estimate produces an estimate. Which is an argument for stating the split — 12.7 mm of beam plus 10.2 mm of support — rather than quoting a total of 22.9 that reads as though it were known to three figures.

One thing does survive the uncertainty. Maxwell’s reciprocal theorem holds for the whole assembly, springs included: the deflection at the beam’s mid-span due to a load on the support equals the deflection at the support due to the same load at mid-span. Neither number is known to better than a factor of two, and the equality between them is exact anyway — a relationship between two unknown quantities is still a relationship, and it is the one check available on a model whose inputs cannot be verified.

What the pictures cannot show

Every deflected shape here is drawn at an exaggeration of two or three orders of magnitude. The 22.9 mm this page is about, on an 8 m beam, is a slope of about one in 700, and a figure drawn to scale would show a straight line.

The sharing curve is drawn against a support stiffness with no units on the axis worth reading, because the quantity that matters is a ratio. A support stiffness of 7,875 kN/m means nothing without the beam it carries.

And nothing here shows what the occupant experiences, which is not a deflection but a change in one — a floor that moves when somebody walks across it, a door that binds when the bay next to it is loaded. Those are differences between two states, and every figure on this page shows one state.

The ladder from here

Later rungs on this anchor: the grillage, where primary and secondary beams are solved together and the distinction between beam and support disappears. Rotational support flexibility, and the end restraint a real bearing supplies. Bearing design as a stiffness problem rather than a strength one. Piled foundations as springs, and the interaction between a raft, its piles and the frame above. Support stiffness in dynamics, where a soft support lowers the natural frequency of everything on it — which is how a floor becomes strong and unusable. And the measurement question: support stiffnesses are the least well known numbers in any model, and every result on this page is a ratio of two of them.

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

The 8 essays that link to this one and share the most of its objects, of 9 that link here.

The objects this essay names

Each one links to every other essay that touches it.

Axial shorteningBearingDeflectionDifferential shorteningElastic foundationIndeterminacyLoad-sharingRedistributionSeries combinationSeries stiffnessServiceabilityStiffnessSupport flexibilitySupport settlementUnit load method