Sections and stress

Two cells, one equation, and a web with nothing in it

Bredt's formula answers a single closed cell because a single closed cell has one unknown and one equation. Put a web down the middle and there are two unknowns and still one equation — and the answer, when the missing statement is supplied, is that the new web carries exactly nothing.

Assumes The slit that costs a factor of six hundred, One support too many, and what it costs to know and The section that will not keep its shape.

A single closed cell under torque is one of the few genuinely easy calculations in this subject. The shear flow qq — force per unit length round the wall — is constant all the way round, because a longitudinal cut anywhere shows it has nowhere to change; taking moments about any point in the plane gives T=2qAT = 2qA, where AA is the area the wall encloses; and that is the whole thing. One unknown, one equation, no stiffness anywhere in it.

One loop, one flow, and Bredt answers it. A 1-cell box 3.0 m wide and 1.5 m deep under 4000 kNm of torque. Statics gives one equation, T = 2 Σ q_i A_i, and there are 1 unknown flows — so the section is torsionally redundant and the missing statements are that every cell twists by the same amount. Solving that system gives 444.4 N/mm in the cells. J is 2.3679e+12 mm⁴ against 2.3679e+12 for the same outline with no internal web at all, a ratio of 1.000000. The same walls slit open would give 7.413e+10, so closure is worth 32 times and the internal web is worth what the ratio says.
Fig. 1 The determinate case. One loop, one flow — 444.4 N/mm under 4,000 kNm on a box enclosing 4.50 m² — and the stress in each wall is that flow divided by the wall’s own thickness, so the thinnest wall works hardest. Nothing here required the material to be named.

Now put a web down the middle. There are two cells, two shear flows, and T=2(q1A1+q2A2)T = 2(q_1A_1 + q_2A_2) is still one equation.

The equation that is missing

The section has become torsionally redundant, to a degree equal to the number of cells less one. What statics cannot supply, compatibility must, and the compatibility statement is the one thing that has to be true of two cells sharing a wall: they twist by the same amount. They are parts of the same cross-section, and a cross-section rotates as a unit.

Writing the rate of twist of cell ii as a circuit integral round its own walls,

2AiGθ  =  iqstds,2A_i\,G\theta' \;=\; \oint_i \frac{q_s}{t}\,ds,

where qsq_s is the flow in each wall as seen going round cell ii. On the outer walls that is qiq_i. On a wall shared with cell jj it is qiqjq_i - q_j, because the two cells’ flows run in opposite directions through the shared wall and what physically exists there is their difference.

That gives one equation per cell, plus the torque equation, and the system closes. It is worth noticing what has entered: the shear modulus, the wall thicknesses and the cell areas are all in the compatibility equations and none of them is in the torque equation. An indeterminate problem is one whose answer depends on stiffness, and a multi-cell box has just become one — which is the price every redundant structure pays for the redundancy, and it is paid here by a cross-section rather than by a frame.

The shear modulus turns out to cancel, because it multiplies every cell’s twist equally and the twists are being set equal. The thicknesses do not.

The web down the middle carries no torsion at all. A 2-cell box 3.0 m wide and 1.5 m deep under 4000 kNm of torque. Statics gives one equation, T = 2 Σ q_i A_i, and there are 2 unknown flows — so the section is torsionally redundant and the missing statements are that every cell twists by the same amount. Solving that system gives 444.4 and 444.4 N/mm in the cells, so the internal web carries 0.00 N/mm — 0.00 per cent of the outer wall's. J is 2.3679e+12 mm⁴ against 2.3679e+12 for the same outline with no internal web at all, a ratio of 1.000000. The same walls slit open would give 7.413e+10, so closure is worth 32 times and the internal web is worth what the ratio says.
Fig. 2 Solved for the symmetric case, and the answer is a number worth stopping on. Both cells carry 444.4 N/mm, so the flow in the wall they share is their difference: zero, to fourteen decimal places. J comes out at 2.36788 × 10¹² mm⁴ against 2.36788 × 10¹² for the same outline with no internal web whatever — a ratio of 1.000000000000.

Why it is zero, without solving anything

The result does not need the linear algebra. The box is symmetric about the internal web; the torque is symmetric about it; so the solution must be. Two identical cells under identical conditions carry identical flows, and q1q2=0q_1 - q_2 = 0 by the symmetry alone.

What is worth checking is the second half of the claim — that JJ is then exactly the single-cell value rather than merely close to it. With the shared wall carrying nothing, cell 1’s circuit integral has no contribution from it, so

2A1Gθ=qcell 1’s outer wallsst,2A_1 G\theta' = q\sum_{\text{cell 1's outer walls}} \frac{s}{t},

and with A1=A/2A_1 = A/2 and cell 1’s outer walls being half the outer perimeter’s s/t\sum s/t, this rearranges to J=4A2/(ds/t)J = 4A^2 / \oint (ds/t) over the outer perimeter. Bredt’s single-cell formula, with the web absent from every term. The web is not merely unhelpful; it is not in the answer.

The consequence for design is direct and slightly startling. The web in the middle of a symmetric box girder — several hundred millimetres of concrete or a full-depth stiffened steel plate, running the length of the span — is doing nothing at all about torsion. Everything it is in the section for is something else.

It is also, stated carefully, not quite the same claim as the web is unstressed. The web carries no shear flow from the torque. It carries plenty from everything else, and the finding is about attribution rather than about the member. That distinction matters because it is the one a design check gets wrong in the safe direction and a section optimisation gets wrong in the other: nobody is going to under-design the web by believing this, and somebody might delete it.

The same shape of finding has appeared on this site before in a truss. A member can carry the full applied panel load and contribute exactly nothing to the deflection being measured, because the zero belongs to the pair — member and question — rather than to the member. The web here is idle with respect to torsion, and to nothing else.

What the web is actually for

Three things, and none of them is on this page’s title.

Shear stress across a section. The distribution of shear stress over an I-section, computed as VQ/It by accumulating the first moment of the area above every height. The peak is 0.41 against a mean of 0.19 — a ratio of 2.15 — and it falls at the neutral axis, where the bending stress is zero.
Fig. 3 The first. Under vertical load the webs carry the bending shear, and here the internal web is a full participant: the shear flow from bending runs down all three webs in proportion to their share of the section, and removing the middle one raises the stress in the other two by half. A box with three webs is a box designed for shear, whatever its torsion does.
An eccentric load is three load cases, and only two of them are checked. A line load of 40 N/mm at 0.8 m from the axis of a 3.0 by 1.5 m box, replaced by the three cases it is equivalent to. Bending is the load on the axis. The torque 30 kNm per metre then splits into a set of edge forces that drives Bredt's shear flow and distorts nothing, and a set with the flange forces reversed — 5.0 kN/m up one web and down the other, 10.0 kN/m across the flanges — which carries no torque at all and squashes the rectangle into the rhombus drawn behind it. Its generalised load is exactly half the torque, so a box girder spends half of an eccentric load's torsion on changing its own shape, and no torsion calculation contains that half.
Fig. 4 The second, and the reason box girders have webs and diaphragms at all. An eccentric load is not one load case but three — bending, torsion, and distortion, in which the rectangle becomes a parallelogram in its own plane. Distortion is neither of the other two, it has its own stresses, and an internal web is a very effective brake on it because the parallelogram cannot form without shearing the web.
A diaphragm spacing is a decay length in disguise. The peak distortional stress, as a share of the bending stress, against the spacing of the diaphragms that hold the section square. The curve is flat at the right — past the decay length of 14.2 m a diaphragm is too far away to help its neighbour — and falls steeply once the spacing comes inside it. At a spacing of one decay length the distortional stress is 20 per cent of the bending stress; halving that spacing again takes it to 5. The number a designer needs is not a rule of thumb about span over five; it is this length.
Fig. 5 The third is the same argument with the members turned across the span. Diaphragms resist distortion at points and their spacing is a decay length rather than a rule of thumb. A longitudinal web resists it continuously, which is why a wide box gets a web and a narrow one gets diaphragms.

Plate buckling is the fourth reason and it is often the governing one: a 3 m wide compression flange with a web under its centre is two 1.5 m plates rather than one 3 m plate, and the buckling stress of a plate goes as the inverse square of its width. Halving the width quadruples the critical stress, which is a very large return for a member the torsion calculation values at nothing.

And there is a fifth that is not structural at all. A wide single-cell box has an internal void several metres across with no support to its soffit formwork during construction; a web under the middle of it is something to prop from. The structure that exists during construction is not the one being designed, and members put in for the first are checked in the second and then quietly credited with helping.

Move it and it starts working

If the flow is the difference between two cells, then making the cells different should make the difference nonzero. It does.

The internal web carries 12.8 per cent of the outer wall's flow. A 2-cell box 3.0 m wide and 1.5 m deep under 4000 kNm of torque. Statics gives one equation, T = 2 Σ q_i A_i, and there are 2 unknown flows — so the section is torsionally redundant and the missing statements are that every cell twists by the same amount. Solving that system gives 403.0 and 462.2 N/mm in the cells, so the internal web carries -59.20 N/mm — 12.81 per cent of the outer wall's. J is 2.3838e+12 mm⁴ against 2.3679e+12 for the same outline with no internal web at all, a ratio of 1.006720. The same walls slit open would give 7.413e+10, so closure is worth 32 times and the internal web is worth what the ratio says.
Fig. 6 The same box with the internal web at 30 per cent of its width. The cells now carry 403.0 and 462.2 N/mm, so the web carries their difference, −59.2 — 12.8 per cent of the outer wall’s flow. J rises to 2.38379 × 10¹² mm⁴, which is 0.67 per cent more than the box without a web at all.

The direction of the difference is worth reading. The smaller cell carries the larger flow, which is the opposite of what an area-based intuition suggests. A cell twists at a rate set by its flow divided by its area, so a small cell needs a large flow to twist as fast as a big one — and the shared wall then carries the surplus, in the direction that runs against the small cell’s circulation.

The web is worth least exactly where anybody would put it. Torsional stiffness, and the flow the internal web carries, against where that web is put across a 3.0 m box. Both are drawn as ratios: stiffness against the same outline with no web at all, and flow against the outer wall's. At the centre both are exactly zero — the two cells are identical, they carry identical flows, and the difference across the shared wall is nothing. Moving the web out to a tenth of the width raises the stiffness by 3.3 per cent and puts 141 N/mm into the web. The whole range is 3.3 per cent, against the 32× that closing the section was worth.
Fig. 7 The whole range, swept. Stiffness against the webless box, and the flow in the web against the outer wall’s, as the web moves across. Both are exactly zero at the centre and both grow monotonically as it moves out — reaching 3.3 per cent of stiffness and 141 N/mm of flow at a tenth of the width, which is the most a single internal web is ever worth in torsion.

Three per cent is the honest size of the whole effect, and it needs a comparison to be read properly.

One slit, and the torsional stiffness falls by a factor of hundreds. A 200 by 200 box of 8 mm wall, drawn closed and then slit along its length. Closed, the torque runs round the wall as a shear flow and the torsion constant is 5.66×10⁷ mm⁴; slit, the loop is broken and only each wall's own thickness resists, giving 1.31×10⁵ mm⁴. The ratio is 432 to one, so the same torque twists the slit section 432 times as far and raises a peak shear stress 36 times as high. Nothing about the material changed.
Fig. 8 The comparison. Slit the same box along one corner and its torsion constant falls by a factor of 32. Whether the section is closed is worth about a thousand times what the internal web’s position is worth, and the two questions are asked in the same design meeting with the same apparent weight.

More cells

Three cells is the first case where symmetry does not save the arithmetic, and it shows what the general answer looks like.

The internal web carries 15.4 per cent of the outer wall's flow. A 3-cell box 3.0 m wide and 1.5 m deep under 4000 kNm of torque. Statics gives one equation, T = 2 Σ q_i A_i, and there are 3 unknown flows — so the section is torsionally redundant and the missing statements are that every cell twists by the same amount. Solving that system gives 419.0 and 495.3 and 419.0 N/mm in the cells, so the internal webs carry -76.27 and 76.27 N/mm — 15.40 per cent of the outer wall's. J is 2.4023e+12 mm⁴ against 2.3679e+12 for the same outline with no internal web at all, a ratio of 1.014542. The same walls slit open would give 7.413e+10, so closure is worth 32 times and the internal web is worth what the ratio says.
Fig. 9 Three cells, symmetric about the centre. The outer cells carry 419.0 N/mm and the middle cell 495.3, so both internal webs carry 76.3 — 15.4 per cent of the largest cell flow. J is 1.45 per cent above the webless box. Symmetry makes the two outer cells equal to each other and does not make any of them equal to the middle one, because the middle cell has two internal walls and the outer cells have one each.

The middle cell’s circuit runs through two thin internal webs rather than one thin and one thick outer web, so its ds/t\oint ds/t is smaller and it needs a larger flow to twist at the same rate. The flows are decided by the wall thicknesses and the cell areas, and by nothing about the materialGG cancels out of the ratios, exactly as it does for a single cell.

That cancellation is worth a sentence of its own, because it is not obvious and it is what makes the calculation usable. The compatibility equations each contain GθG\theta' on one side; setting them equal to one another eliminates it, and the torque equation then fixes the scale. So a multi-cell box’s distribution of flow is a pure geometry problem, and only its twist per unit length needs a modulus — which is the same separation that lets a truss’s forces be found before anything is known about its members, arriving here in a section rather than a structure.

The general result generalises the two-cell one. A web between two cells carries the difference of their flows, and two cells carry equal flows when their circuit integrals divided by their areas are equal. Symmetry is the easy way to arrange that and not the only way: a small cell with thin walls and a large cell with thick ones can be tuned to carry the same flow, and the web between them would then also carry nothing. Nothing about the arrangement has to look symmetric for the result to hold.

The same problem, and one of these can be solved by hand. The flexibility matrices for a 6-span continuous beam, one per choice of redundant, with the magnitude of each entry shaded and the exact zeros left empty. Releasing a moment at a support is felt only in the two spans either side of it, so the matrix is tridiagonal and each equation involves three unknowns — which is the three-moment equation, and is the whole reason continuous beams could be solved on paper for a century. Releasing a support instead is felt everywhere: a unit reaction at any interior support deflects every other point on the beam, so the matrix is full at 100% against 52%. Both give the same bending moment everywhere. The structure did not change; the bookkeeping did, and the bookkeeping was the invention.
Fig. 10 The shape of the calculation, stated generally. A redundant structure needs as many compatibility statements as it has redundancies, and each one is a deformation set equal to another deformation. Choosing which quantity to release is the whole art of the force method — and in a multi-cell box nobody gets to make it, because the cells are the releases and the twists are the compatibility.

The number a designer actually needs

The reason any of this is computed is that a box girder on a curved alignment, or one carrying an eccentric load, has a torque to get to its bearings, and the check is a shear stress in a wall. That stress is the flow divided by the thickness, so the busiest wall is the thinnest one and not the one carrying most.

For the symmetric box under 4,000 kNm the flow is 444.4 N/mm everywhere on the outer loop, and the walls report 1.78 N/mm² in the 250 mm top slab, 2.02 in the 220 mm bottom slab, and 1.27 in the 350 mm webs. The soffit is the critical wall and it is the one nobody thinks of as a shear member. It is also the wall most likely to be thinned in a value-engineering exercise, because it carries no bending reinforcement over most of the span and looks like the cheapest place to save concrete.

Two more consequences follow from the flow being constant round the loop. Any wall can be checked in isolation once the flow is known, which is why a torsion check reduces to a list. And the sum of the wall thicknesses is irrelevant — what matters is the smallest one, exactly as a chain’s strength is its worst link and not its average. Thickening the webs of this box does nothing whatever for its torsional shear stress; thickening the soffit by 15 per cent removes the governing check.

Where the model stops

Every wall is thin and every flow is uniform across it. Bredt’s assumption, and progressively wrong as walls thicken. A concrete box girder’s webs at 350 mm on a 1.5 m depth are not thin by any reasonable standard, and the shear flow across such a wall is not constant.

The section does not distort. The compatibility statement used is that the cells rotate together as a rigid cross-section, which is exactly the assumption distortion violates. For pure torque on a box with adequate diaphragms this is close to true; for an eccentric point load on a long unbraced box it is not, and the flows found here are the torsional part of a three-part answer.

Warping is free. Closed sections warp very little and the warping stresses are usually neglected, which is standard and is not always right — a box with a very wide, very thin cell warps more than the calculation admits, and a box restrained at a diaphragm generates axial stresses this has no term for.

It is elastic throughout. At collapse the flows redistribute: a wall that reaches its shear capacity sheds flow to the others, and the plastic torque of a multi-cell box is a mechanism problem rather than a compatibility one. The centred web that carries nothing elastically may carry a great deal at collapse, which is a good reason not to design it away.

The webs are vertical. A trapezoidal box — which is most of them, because a sloping web sheds rain and looks better — has webs whose length is not the depth, and both the circuit integral and the enclosed area change. The arithmetic is identical and none of the numbers on this page survive it.

And the drawing is of a torque alone. No box girder anywhere is loaded in pure torsion. Every real load case is bending plus torsion plus distortion, the webs carry all three at once, and the picture of a web with nothing in it is a picture of one third of one load case. What the calculation licenses is not removing the web — it is declining to claim credit for it in the torsion check.

The ladder from here

Later rungs on this anchor: the shear-flow superposition properly done, with bending, torsion and distortion resolved on the same webs and the governing wall found from the sum rather than from any part of it. Cells that are not rectangles — a trapezoidal box, an aerofoil, a ship’s hull section — where the areas and perimeters have to be computed before the system can be assembled. Open cells connected to closed ones, where a cantilevering deck slab contributes bt3/3bt^3/3 to a section otherwise dominated by a closed loop and the two contributions differ by three orders of magnitude. The plastic torque of a multi-cell section, from the sand-heap analogy with islands in it. Shear lag across a wide cell, which changes the effective wall a flow is running through. And the same redundancy in a structure rather than a section: a frame with more restraints than equations is solved by the identical move — count the redundancies, write one compatibility statement for each, and let the stiffnesses decide what statics could not.

Named alongside this one

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

The objects this essay names

Each one links to every other essay that touches it.

CompatibilityDiaphragmIndeterminacyLoad pathShear flowStiffnessTorsionTorsional constant