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 beamThe 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.4020080030002000000.20.40.60.81stiffness of each supportfraction of the deflection that is bendingrigid supportsare over here51%the beam drawn
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 beam drawn here — a floor beam sitting on other floor beams — is at 56%.

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.

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×moment: the squareload: the first powerdeflection: the fourth
Fig. 2 Span to the fourth, which is the law the 12.7 mm obeys and the 10.2 mm does not. Doubling the secondary’s span multiplies its own deflection by sixteen; the support’s contribution is a reaction divided by a stiffness — linear in the load, and containing the primary’s span rather than the secondary’s.

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 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. 3 The shape whose peak is 12.7 mm, at an exaggeration this caption states: the beam’s departure from the chord between its supports. Everything the beam calculation knows is in this figure, and the other 10.2 mm is a rigid-body translation of the whole of it.
The deflection at x = 4, by virtual workThree diagrams: the moment from the real load, the moment from a unit load placed where the answer is wanted, and their product. The area under the third, divided by EI, is the deflection — 1066.67 here. No standard case was consulted, so the method works for any load pattern at all.real Mpeak 160.0a unit load, here and nowhere elseunit mM × marea ÷ EI = 1066.67the unit load is the only place the question 'deflection where?' is asked
Fig. 4 One deflection without solving everything — the unit-load method, which computes the beam’s own contribution as an integral of Mmˉ/EIM\bar{m}/EI. Extending it to include the supports needs one extra term per support, RˉR/k\bar{R}R/k, and it is the same virtual-work statement with springs added to the list of things storing energy.

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 seriesThe 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.flexibility contributed by each componentthey add, so the softest dominates — Sj = 25227.71 kN·m/radwhat doubling it buyscolumn web in shear21.89%×1.12column web in compression11.55%×1.06column flange in bending39.62%×1.25end plate in bending18.09%×1.1bolts in tension8.85%×1.05
Fig. 5 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%

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.

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 onesThe 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.this support 0.01 lowmoment19.6 sagging24.5 hogging30.6 if the spans were simplereactions 14.0 38.5 38.5 14.0 — the inner supports carry far more than a sharethe continuous case needed stiffness; the comparison did not
Fig. 6 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.

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. 7 And its cousin at the ends of the member: how much of the fixed-end moment a joint of a given stiffness actually delivers. Support flexibility and joint flexibility are the same phenomenon at the two ends of the same conversation — one is a translation and the other a rotation, and both are 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 furthestA 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.1000 kN1/β = 2.56 mthe beam lifts off at 6.04 msettlement 3.90 mm · contact pressure 195 kN/m · moment 641 kNm, none of which contains the length of the beam
Fig. 8 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.

Where else it decides something

Whether the floor shares the load out by stiffness or by areaThe share of a uniform storey force taken by each of three equally stiff walls, against the stiffness of the floor plate that spans between them. A plate far stiffer than the walls translates almost rigidly, every wall deflects the same and the share is the ratio of stiffnesses — 60% to the middle wall here, the same as everyone else. A plate far softer than the walls behaves as a continuous beam over them and the middle wall takes 33%. Neither end is the tributary-area answer of 50%, which assumes a plate that is both soft and discontinuous over the wall, and which nothing here ever reaches.0.020.1011025000.20.40.60.8floor-plate stiffness ÷ wall stiffnessshare of the storey forcethe middle wallan end walltributary arearigid plate← soft plate
Fig. 9 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 span.

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 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. 10 Which limit arrives first. 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 depends on which of the two curves the member is near.

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.

Maxwell's reciprocal theoremA load at one point and the deflection it causes at another, against the same load moved to the second point and the deflection read at the first. Both integrals return 63.7501, and neither calculation was told about the other. The two deflected shapes are entirely different; the two readings are identical.10 at 3δ at B = 63.75010 at 6δ at A = 63.750the shapes have nothing in commonand the two readings agree to 1e-14which is why an influence line can be measured by pushing the structure where it is easy to push
Fig. 11 And one thing that 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. A relationship between two unknown quantities is still a relationship.

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.

Named alongside this one

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

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The objects this essay names

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Axial shorteningBearingDeflectionDifferential shorteningElastic foundationIndeterminacyLoad sharingRedistributionSeries combinationSeries stiffnessServiceabilityStiffnessSupport flexibilitySupport settlementUnit load method