Structural form

The same span, four ways

A beam, a truss, an arch and a cable can all cross the same gap under the same load, and the choice between them is usually described as a matter of judgement or of taste. It is neither. Each carries the load by a different mechanism, each mechanism has a different exponent, and an exponent decides the ordering at every span rather than at some spans.

Assumes The shape that carries itself, and the arch that is its reflection, Depth is the cheapest strength there is and The triangle that cannot fold, and everything built out of it.

Four structures cross the same gap under the same load. A beam bends. A truss turns the bending into a couple of axial forces. An arch turns it into a compression along a line. A cable turns it into a tension along the same line, upside down.

The usual account of the choice between them is a list of considerations, and the list is not wrong. What it hides is that the four differ in exponent, not in coefficient — so there is no span at which they are all within a factor of two, and the ordering changes as spans change rather than the gaps between them narrowing.

Before the four are set against each other, it is worth seeing what an exponent looks like when it is the only thing in an answer. Take one job and one form — a beam carrying a column across a gap — and ask how deep it has to be.

Four times the load is exactly twice the depth. Depth of a 0.6 m wide transfer beam against the load it moves 3 m across its 14 m span. Strength wants √(6M/σb) with M = P·a(L − a)/L, so the depth goes as √P and nothing else: 1.144 m at 2000 kN and 2.289 m at 8000 — a ratio of 2.000, which is 2 to three decimals and is a property of the square root rather than of this beam. The upper curve is the depth the settlement criterion asks for instead, and it is above the strength curve everywhere on this chart: deflection goes as 1/d³ where strength goes as 1/d², so the two converge as the load grows and the stiffness criterion governs every ordinary transfer. At 2000 kN it asks for 1.89 m against 1.14.
Fig. 1 Depth of a transfer beam 0.6 m wide against the load it moves 3 m across a 14 m span, by two criteria. Strength wants √(6M/σb), so the depth goes as the square root of the load and nothing else: 1.144 m at 2000 kN and 2.289 m at 8000, a ratio of 2.000. The upper curve is the depth the settlement criterion asks for instead — 1.89 m against 1.14 at the load drawn — and it is above the strength curve everywhere here, because deflection goes as 1/d³ where strength goes as 1/d².

Four times the load is exactly twice the depth, and no property of this beam appears in that statement: it is the square root and nothing else. The second curve is the same member measured by a different criterion, and because its exponent differs by one it is a different curve with a different answer — 1.89 m rather than 1.14, on the same load. Two criteria applied to one beam already disagree by three quarters of a metre, and neither of them is wrong. Four mechanisms disagree by very much more.

Which free body produced the number

Cut each of the four at midspan and look at what appears on the cut.

A beam shows a bending moment resisted by a stress distribution across its depth, with a lever arm of a fraction of the depth. Capacity is σZ\sigma Z, and ZZ contains the depth squared and the breadth once.

A truss shows the same bending moment resisted by two axial forces at the full depth apart. Capacity is σAd\sigma A d with the whole area available at the extreme fibres, so a truss is a beam whose section modulus has been made as large as its depth permits.

An arch and a cable show no bending moment at all if their shape is right, because the internal force follows a line whose eccentricity from the axis is zero everywhere. Capacity is σA\sigma A with no depth in it, and the depth reappears as the sag, which decides the magnitude of the force rather than its capacity.

Four cuts, four different quantities on the cut face. That is the whole taxonomy, and everything else in this essay follows from it — the exponents, the crossovers, and the fact that the four cannot be compared by any single number.

The first of those cuts can be drawn immediately, because the beam of the previous figure is exactly the bending case: cut it under the column and there is a moment on the cut face and a shear either side of it, and nothing else.

The depth is decided by how far it moves, not by what it can carry. A column carrying 2000 kN landing 3 m into a 14 m transfer member. The free body is the member itself, cut under the column: M = P·a(L − a)/L = 4714 kNm, with 1571 kN of shear on one side of the cut and 429 on the other. At an allowable stress that moment asks for 1.14 m of depth — the dashed outline — and keeping the settlement it causes inside the floors' own bending asks for 1.89 m, which is the member drawn solid. 65% more depth is bought by nothing the strength calculation can see. The depth grows as √(P·a), so four times the load is exactly twice the depth, and depth in a transfer member is a storey nobody occupies.
Fig. 2 A 2000 kN column landing 3 m into a 14 m transfer member, with the member cut under the column. The free body gives M = P·a(L − a)/L = 4714 kNm, with 1571 kN of shear on one side of the cut and 429 on the other. The dashed outline is the 1.14 m of depth that moment asks for; the member drawn solid is the 1.89 m the settlement asks for — 65 per cent more depth, bought by nothing the strength calculation can see.

That moment on that cut face is the quantity every other form in this essay exists to get rid of. A truss keeps it and splits it into two axial forces at the full depth; an arch and a cable arrange for it not to appear.

The exponent, made visible

The clearest demonstration is not a span at all. It is a pressure vessel against a flat plate.

The same span, the same pressure, thirty times the thickness. A 4.4 m diameter carried two ways at 0.8 MPa, both drawn to the same scale across and both allowed 150 MPa. Curved, the wall is in pure tension: the free body is half the cylinder cut along its length, and N_θ = pR = 1760 kN/m needs 11.7 mm of steel. Flat, the same width is a strip in bending: M = p(2R)²/8 = 1936 kNm/m needs 278 mm, a factor of 23.7. That factor is √(3σ/p) = 23.7 and it is not a proportion but a change of exponent: the membrane thickness is linear in the pressure and the bending one is a square root of it, so the advantage grows as the load falls. Both wall thicknesses are drawn 10 times over, because at the scale of the span the curved one is a third of a pixel.
Fig. 3 The same diameter carried two ways at the same pressure and the same allowable stress. Curved, the wall is in pure tension and needs 11.7 mm; flat, the same width is a bending strip and needs 278.

The membrane thickness is t=pR/σt = pR/\sigma — linear in the pressure. The bending thickness is t=3pR2/σt = \sqrt{3p R^2/\sigma} — a square root of it. Their ratio is 3σ/p\sqrt{3\sigma/p}, which for this case is 23.7 and which grows as the pressure falls.

That last clause is what makes it an exponent argument rather than a factor. The advantage of the curved form is not a constant 24 to be traded against buildability; it is unbounded as the load gets lighter, which is why a lightly loaded roof is a shell or a fabric and a heavily loaded floor is a slab. The surface that carries by being curved is the essay about the mechanism; this is what it is worth.

The shape that has to be found

Both the arch and the cable only carry axially if their shape is the funicular of the load, and the funicular is a solved quantity rather than a chosen curve.

Under five point loads it is a polygon with a vertex at each of them and one horizontal component throughout, the end segments carrying the most because they are the steepest. Under a load spread along the horizontal it is a parabola, and under the cable’s own weight it is a catenary — a different curve, close enough to a parabola at ordinary sags that the distinction matters for the geometry and not for the forces. Reflected, every one of those carries the same load in pure compression, which is why the cable and the arch are one family and not two.

The catch is that a funicular is the funicular of one load case. Change the load and the shape is wrong, bending appears, and the form loses precisely the advantage it was chosen for. So an arch that has to carry a variable load is either given a depth to resist the bending — at which point it is a curved truss — or given hinges so the bending cannot develop.

That is why the line that must stay inside is the governing check for a masonry arch and why steel arches are usually stiffened. It is also the honest limit of the whole family: the axial forms are the efficient ones for the load they were shaped for and no other.

What the thrust costs

An arch delivers a horizontal thrust at its springings and a cable delivers a horizontal pull at its anchorages, and both have to go somewhere.

A three-pinned arch settles the question with a single moment equation about the crown hinge, and its thrust line then lands on the axis everywhere, so there is no bending anywhere in it.

The thrust is wL2/8rwL^2/8r — inversely proportional to the rise — so a shallow arch is not merely less efficient, it is expensive at both ends. Halving the rise doubles the thrust and doubles whatever has to resist it, which may be a rock face, a tie across the span, or a very large foundation.

That is the arch’s characteristic trade: it converts a bending problem into an axial one and a foundation problem. Where the foundation cannot take a thrust, the thrust that never reaches the ground is the alternative, and the tie it needs is a member in tension the length of the span.

Stiffness, which is a different ranking

Everything so far has been about strength, and the four forms rank differently on stiffness.

A cable has no stiffness at all until it has tension in it, which is the state a slack tie is in, and the tension it has is a design decision rather than a property. So a cable structure’s stiffness is bought with pretension and with sag, and neither is free — the pretension has to be resisted by the anchorages and the sag has to be accommodated by whatever the cable is holding up. The stiffness that comes from the shape is the essay about the mechanism.

A beam’s stiffness, by contrast, is a property of the section, and it goes as the fourth power of the span.

Doubling the span multiplies the deflection by sixteen and the moment by four.

That fourth power is the reason a beam runs out of usefulness at a span long before it runs out of strength, and it is the single strongest argument for changing form as spans grow: the strength penalty for a beam is a square and the stiffness penalty is a fourth power, so a form that reduces the bending reduces the more expensive of the two.

The two exponents do not merely give different numbers on the same member. They change which check is the one being answered, and a procedure that answers the wrong one returns a member that is right and a building that is not.

At the depth strength asks for, the floors above are bent nearly twice as hard by the settlement. The moment a 10-storey stack of floors picks up from the settlement of the column below them, divided by the moment those floors carry under their own 30 kN/m, against how deep the transfer member is. At the depth strength asks for — 1.14 m — the ratio is 1.89: the settlement is doing more to the floors than the load they were designed for. The curve falls through one at 1.67 m, which is 46% more depth than the moment needed. The criterion solved in closed form asks for 1.89 m and lands at 0.769 rather than exactly one, and the gap is not an error: that calculation lets the transfer member take the whole 2000 kN, while the floors it is bending hold the column up in return. They shed 57% of the load, and the settlement with that coupling is 60.6 mm against 140.4 free.
Fig. 4 The moment a ten-storey stack of floors picks up from the settlement of the column beneath them, divided by the moment those floors carry under their own 30 kN/m, against how deep the transfer member is. At the 1.14 m depth strength asks for, the ratio is 1.89: the settlement is doing more to the floors than the load they were designed for. The curve falls through one at 1.67 m, which is 46 per cent more depth than the moment needed.

Nothing in the strength calculation can see that curve, because the quantity it plots is not on the transfer member at all — it is on ten floors above it, and it arrives through a displacement rather than through a force. The exponent is what makes it so: at 1/d³ the stiffness demand outruns the strength demand at every depth that matters here.

Three ways to do one job

The abstraction is easiest to check on a problem with only one answer required.

Three ways to move the same column, and they are not close. The same 2000 kN moved 3 m across 14 m, built three ways and drawn to one scale. The deep beam is 1.14 m of concrete, 24.1 tonnes, and settles 60.6 mm in the long term. The storey-deep truss takes the same moment as a couple at 3.6 m centres, so its chords carry M/h and it weighs 2.6 tonnes — a fifth of the beam — while settling 15.8 mm, and it does not creep. The wall is 72.8 tonnes and hardly moves at all, 1.71 mm, of which 36% is shear rather than bending — which is what a member as deep as it is long always does, and is why beam theory does not describe one. A wall as a deep beam is the stiffest of the three by a factor of 35.4.
Fig. 5 The same 2000 kN column moved 3 m across 14 m, built three ways to one scale. The deep beam weighs 24.1 tonnes and settles 60.6 mm; the storey-deep truss weighs 2.6 and settles 15.8; the wall weighs 72.8 and settles 1.71.

The truss is a ninth of the beam’s weight and four times as stiff, because it has the whole storey depth as a lever arm rather than a metre of concrete. The wall is three times the beam’s weight and thirty-five times as stiff — and 36% of its deflection is shear rather than bending, which is what a member as deep as it is long always does and is why beam theory does not describe one.

No consideration of taste separates those three. They are the three mechanisms of this essay applied to one job, and the numbers are as far apart as the mechanisms are.

The material question rides on top

Having chosen a mechanism, the ranking of materials for it is decided by an exponent too, and it is not the same exponent for each.

Three lines through one point, and three different winners. Modulus against density on logarithmic axes, with a guide line for each of three indices drawn through mild steel. A performance index E^(1/n)/ρ is a straight line of slope n on these axes, so ranking materials by it means sliding the line up and to the left and seeing what it leaves behind. The three lines have three different orders, which is why a table of properties cannot answer the question on its own: for a tie the answer is carbon fibre, for a beam it is timber at 8.56 times steel, and for a plate timber wins by more still. The construction is Ashby's; the arithmetic on it is this site's.
Fig. 6 Modulus against density on logarithmic axes, with a guide line for each of three indices through mild steel. Each index is a straight line of slope n, so ranking by it means sliding a line and seeing what it leaves behind.

For a tie, where the shape is fixed and only the area is free, the index is E/ρE/\rho. For a beam of free depth it is E1/2/ρE^{1/2}/\rho; for a plate of free thickness, E1/3/ρE^{1/3}/\rho. Three lines through the same point with three slopes, and three different winners — which is the ranking belonging to the load case rather than to the material.

So form and material cannot be chosen separately. Timber beats steel eight to one as a beam and loses to it as a tie, so a decision to use a truss rather than a beam is partly a decision about which materials are in the running.

And a third exponent again governs every compression member in the family, because a strut’s capacity falls as the inverse square of its length rather than staying put. That is why the struts of a long-span form are the members that decide it, and why the same section at four lengths is four quite different members.

The truss, which is a beam with the middle taken out

The truss deserves a closer look than the exponent argument gives it, because it is the one form in the family whose advantage is a pure geometric ratio.

A beam of depth dd has a section modulus Z=αAdZ = \alpha A d with α\alpha about 0.4 for a rolled shape and a sixth for a rectangle. A truss of the same depth has an effective α\alpha of a half, because all of the material is at the extreme fibres. That alone is a factor of between one and three — worth having and not decisive.

What makes the truss decisive is that its depth is not limited by the same things. A beam’s depth is limited by what can be rolled, cast or transported; a truss’s is limited by the storey height, which is an order of magnitude larger. So the truss’s advantage is not its better α\alpha but the depth its openness allows, and the reciprocal between chord force and depth is what turns that depth into a force.

It buys the depth with connections. A truss has two or three joints per panel, each of which is a place where the idealisation fails — the joints are not pins, the members are eccentric to their working points, and the whole thing is a set of compression members whose effective lengths are decided by out-of-plane bracing nobody has drawn yet. Its efficiency in a calculation and its efficiency in a fabrication shop are quite different numbers.

The Vierendeel is the same trade taken to its end: remove the diagonals for the sake of the opening they block, and the panel has to carry its shear in bending — which puts the mechanism back where it started and costs, on a typical geometry, a factor of several in material.

Where the crossovers actually are

It is tempting to want a table of spans at which each form takes over. The exponents make it possible in principle and the answer is disappointingly wide, for a reason worth stating.

The crossover between a beam and a truss depends on the depth available, which is a client’s decision about floor-to-floor height. The crossover between a truss and an arch depends on whether the ground can take a thrust. The crossover between an arch and a cable depends on whether the load can reverse, because a cable cannot take compression and an arch under an uplift is an arch in the wrong direction.

Every one of those is a boundary condition rather than a structural quantity, which is why the same span is crossed by different forms in different places, and why the four have coexisted for two centuries rather than one of them winning.

One crossover in the family can be drawn, because both of its terms are structural quantities rather than somebody’s decision.

The case for hanging a building gets worse as the building gets taller. What hanging the floors saves, against how many floors there are, with the movement of the worst floor on the same axes. The saving is the average buckling reduction over the height and nothing else, so it falls from 38.4 per cent at 2 storeys to 4.3 at 40 — because a tall building's columns are heavily loaded and therefore stocky, and a stocky column has almost no reduction to give away. The movement runs the other way, growing straight with the height because every hanger is at the same full stress: 277 mm at the tallest drawn. The two curves cross, and everything to the right of where they do is a building that would be hung for a reason other than material.
Fig. 7 What hanging a building’s floors saves, against how many floors there are, with the movement of the worst floor on the same axes. The saving is the average buckling reduction over the height and nothing else, so it falls from 38.4 per cent at two storeys to 4.3 at forty. The movement runs the other way, growing straight with the height and reaching 277 mm at the tallest drawn. The two curves cross, and everything to the right of the crossing is a building that would be hung for a reason other than material.

Even that one does not end where it crosses, because to the right of the crossing the form is still available and gets chosen for the clear ground floor it leaves rather than for the steel it saves. A crossover between two structural quantities turns out to be the start of the argument rather than the end of it, which is the general case.

What the exponents do settle is the direction: as spans grow, forms move from bending toward axial action, and never the other way. That trend is not a fashion. It is the observation that a bending capacity contains a depth that cannot grow with the span and an axial capacity does not.

Each form has a span at which it can carry only itself

The exponents have been compared at a fixed applied load. Their final currency is what happens when the load is the structure, because that is where each form meets a span it cannot exceed at any size.

The asymmetry that decides it is visible one storey at a time, before any span is involved.

A tie is worth all of itself and a strut is not, which is worth nine per cent. The same 20 floors carried two ways, with every member drawn at the width its own force requires. Hung, the loads accumulate upward, so the largest hanger is at the top: 18.0 MN at 355 N/mm² with no buckling reduction of any kind. On columns they accumulate downward and the largest column is at the bottom, at the same force — but every column above it is understressed by its own slenderness, worst at the top where a 900 kN column still has to be 4.8 × 10³ mm² to reach χ = 0.529. Over the height the hangers total 0.002 m³ of steel against 0.002: a saving of 9.0 per cent, which is the average χ and nothing else.
Fig. 8 Twenty floors carried two ways, with every member drawn at the width its own force requires. Hung, the load accumulates upward and the largest hanger is at the top, working at 355 N/mm² with no buckling reduction of any kind. On columns it accumulates downward, and every column above the bottom one is understressed by its own slenderness — worst at the top, where a 900 kN column still has to be 4.8 × 10³ mm² to reach χ = 0.529. Over the height the hangers save 9.0 per cent of the steel, which is the average χ and nothing else.

A tie is worth all of itself and a strut is worth χ of itself, and χ is a function of a length somebody else decided. Every comparison below is that asymmetry again, at the scale of a span rather than a storey.

The quantity both answers are built from is the breaking length σ/ρg\sigma/\rho g — how far a member of any area can hang from its own end. For structural steel at 355 N/mm² it is 4.6 km; for bridge strand at 1,600 it is 20.5 km.

A cable at a sag ratio nn has a horizontal pull wL/8nwL/8n and a support tension 1+16n2\sqrt{1+16n^2} times it, so carrying only itself it reaches

Lmax=8n1+16n2⋅σρg=0.74×20,500=15,200 mL_{max} = \frac{8n}{\sqrt{1+16n^2}}\cdot\frac{\sigma}{\rho g} = 0.74 \times 20{,}500 = 15{,}200\ \text{m}

at n=0.1n = 0.1. Linear in the breaking length, and the area cancels out entirely — a thicker cable carries more of itself and gets no further.

A beam is limited by σαAd≥ρgAL2/8\sigma\alpha A d \ge \rho g A L^2/8, and the area cancels here too. What does not cancel is the depth, and a beam’s depth is capped by what can be rolled, cast or driven under a bridge. At d=3d = 3 m and α=0.4\alpha = 0.4:

Lmax=8αd σρg=8×0.4×3×4,551=209 mL_{max} = \sqrt{\frac{8\alpha d\,\sigma}{\rho g}} = \sqrt{8 \times 0.4 \times 3 \times 4{,}551} = 209\ \text{m}

A square root of the breaking length times a depth. That is the exponent argument in its sharpest form: not a coefficient of two or ten between the forms, but a linear law against a square-root one, so the ratio is 73 here and grows with every improvement in the material. Doubling σ\sigma moves the beam by 41 per cent and the cable by 100.

It also says exactly what the beam is short of. Its limit is finite only because dd is capped; let the depth grow with the span and the beam becomes a truss and the limit becomes linear again. The bending forms are the ones with a depth somebody else decides.

The cable is not what limits a suspension bridge

The 15 km is a bare cable, and no bridge is a bare cable. Put a deck on it, at qq per metre per cable, and the required area is no longer indeterminate:

A=qk−ρg,k=8n σ1+16n2  LA = \frac{q}{k - \rho g}, \qquad k = \frac{8n\,\sigma}{\sqrt{1+16n^2}\;L}

The asymptote is unchanged — AA runs away exactly at the 15,200 m the bare cable reaches — but the approach to it is what a designer meets. At q=100q = 100 N/mm, which is one cable’s share of a substantial deck:

span cable area
2,000 m 0.194 m²
5,000 m 0.626 m²

Two and a half times the span for 3.2 times the cable. That is a gentle price, and it is nothing like the reason the longest span built is under two kilometres.

What stops it is everything the exponent argument leaves out. The deck has to be stiff enough not to be a Tacoma, and the aerodynamic stability of a suspended deck falls with span rather than rising. The towers grow with the sag, which grows with the span. The anchorages take a pull proportional to the whole cable force. And a deck 5 km long is 5 km of deck, which is most of the cost whatever holds it up.

So the honest conclusion of the whole comparison is a qualified one. The exponents settle which form can reach a span; they do not settle which one is built there, because past a few hundred metres the structure that carries the load has stopped being the expensive part of the problem.

Where the model stops

Self weight has been left out. Every comparison above is at a fixed applied load, and at long spans the structure’s own weight is most of what it carries — which shifts the ranking further toward the axial forms and introduces a fixed point that none of the arithmetic here contains.

Fabrication is not in the exponents. A truss is a ninth of the weight of a beam and several times its cost per tonne, because it is made of many small pieces with connections at each. Below some span, the beam wins on money while losing on every quantity in this essay — and where that span falls is a property of a labour market rather than of a material.

Buckling has been assumed away. Every capacity quoted above is a stress times an area, and the compression members in three of the four forms are governed by something that falls as the inverse square of a length instead. An arch has the whole of its length in compression and is the form this bites hardest.

A form is not chosen once. A real structure is a hierarchy — a deck on beams on trusses on arches — and each level answers a different span with a different mechanism. The interesting choices are usually about where to put the boundaries between levels rather than about which single form to use.

What the picture cannot show

Every figure here compares forms at one span, and the comparison a designer actually faces is a comparison of systems including their supports, their stability, their erection sequence and their tolerance to a load nobody predicted.

The last of those is the one the exponents are silent about and it decides many real projects. A beam is robust to almost anything: change the load, move it, add a hole, and it goes on being a beam. An arch shaped for a load case is not a structure once the load case changes, a cable cannot be pushed, and a shell is a membrane only while its edges are held.

Efficiency and tolerance run in opposite directions here, and the drawings show only the first.

The generalisation

The habit worth carrying is to ask what exponent a design decision moves.

Choosing a bigger section changes a coefficient. Choosing a deeper truss changes a coefficient. Choosing to carry a load axially rather than in bending changes an exponent, and an exponent beats a coefficient at every scale far enough from where they were compared.

That is the sharpest form of a thread that runs through this whole collection: geometry beats material, and it beats it by more the further the problem is pushed. The reason is always the same — a material property enters a capacity linearly and a geometric one enters it squared, cubed, or as a square root of the load — and the reason it is so often ignored is that the material property is the one on the order and the geometry is the one on the drawing.

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

Every essay whose body links to this one.

The objects this essay names

Each one links to every other essay that touches it.

ArchCableFunicularHorizontal thrustLever armLoad pathMaterial indexMembrane actionSelf-weightSlendernessSpan scalingStiffnessStructural formTransfer structureTruss