Internal forces

The shear the chords take

Every shear check in this collection has assumed the two chords of a beam are parallel, so that the whole of the shear crosses the web. Taper the member and that stops being true — and the sign of the correction is decided by which end the haunch is at.

Assumes What a cut reveals, and why it was there all along, The section that changes along the span and The beam that becomes a truss.

Every shear calculation on this site so far has begun with a cut and a vertical force. Cut the beam, look at what is left of the applied load on one side, and whatever does not balance has to cross the cut face as shear. The chords carry the moment as a pair of horizontal forces; the web carries the shear.

That division of labour holds for a prismatic member, and it is so nearly universal in the drawings here that it has never needed stating. It stops holding the moment the two chords stop being parallel — and the reason is not subtle once it is drawn. The chord force is M/zM/z, it acts along the chord, and if the chord slopes, part of that force is vertical.

The chords take the shear the web is credited withA cantilever of 6 m tapering from 400 to 1200 mm, under a 120 kN tip load, with the shear divided between the web and the two inclined chords. The chord force is M/z and it is not horizontal, so its vertical component is real: V_web = V − (M/z)·dz/dx, which is Résal's result of 1899. At the root the web is left with 33 per cent of the applied shear — exactly d₀/d₁ for a straight taper, with no length, load or material in it. Turn the same member round and the figure becomes 300 per cent: the chords stop helping and start adding, at the section where the moment is largest as well. And the limit is worth having — a member whose depth is proportional to its moment leaves the web nothing to do at all, which is the triangular cantilever every crane jib is.120 kNroot00.20.40.60.810.20.40.60.811.2along the member, tip to rootshear ÷ the shear appliedthe applied shearthe web's sharethe haunch reversedweb shear at the root 33% · reversed 300%
Fig. 1 A cantilever tapering three to one from tip to root under a tip load, with the shear divided between the web and the two inclined chords. The web is left with a third of what was applied.

Which free body produced the number

Cut a tapered member at some station and take the piece towards the tip. On the cut face there are three things: a compression CC along the top chord, a tension TT along the bottom one, and whatever shear crosses the web.

Horizontal equilibrium makes the two chord forces equal in their horizontal components; call that common value HH. Taking moments about a point on the line of action of one of them gives M=HzM = H z, so H=M/zH = M/z exactly as for a parallel-chord member. The new statement is the vertical one. Each chord carries a vertical component equal to HH times its own slope, and summing them gives

Vweb=VMzdzdxV_{web} = V - \frac{M}{z}\frac{dz}{dx}

with zz the lever arm and xx measured along the member. That is Résal’s result, published in 1899, and it is the whole of this essay in one line.

Three things about it are worth pausing on. It contains the moment, not the shear, which is why the correction is largest where the moment is largest rather than where the shear is. It contains dz/dxdz/dx and not the individual chord slopes, so a beam haunched symmetrically about its centreline and one haunched on the soffit alone behave identically as long as the lever arm changes at the same rate. And the sign is everything: where the depth grows in the same direction as the moment, the chords take work off the web, and where it grows the other way, they add to it.

Load, shear and moment — a cantileverThe applied load, the shear force it produces and the bending moment that follows, drawn one above another to the same horizontal scale. Shear is the integral of the load and moment is the integral of shear.20shear20.0moment-60.0 at x = 0.00the moment peaks exactly where the shear passes through zero
Fig. 2 The applied shear and moment for the same member. Nothing in this pair of diagrams changes when the beam is tapered — which is exactly why the correction is invisible to anyone reading them.

A closed form with nothing in it

Take the simplest case there is: a cantilever of length LL carrying a tip load PP, tapering linearly from depth d0d_0 at the tip to d1d_1 at the root. Then M=PxM = Px, V=PV = P, and z=kdz = k d with dd linear in xx, so dz/dxdz/dx is constant. At the root, x=Lx = L and z=kd1z = k d_1:

Vweb=P(1Lk(d1d0)/Lkd1)=Pd0d1V_{web} = P\left(1 - \frac{L \cdot k(d_1 - d_0)/L}{k d_1}\right) = P\,\frac{d_0}{d_1}

and the answer is a ratio of two depths. No length appears, no load, no material, no lever-arm factor. A three-to-one haunch leaves the web a third of the applied shear at the section where the moment is largest and the shear check would otherwise be hardest.

Turn the same member round — put the deep end at the tip and the shallow end at the root, which is what a fish-bellied cantilever is — and the same derivation gives Pd1/d0P \, d_1/d_0. The web carries three times the applied shear, at the root, where it is thinnest. The two answers are reciprocals of one another, and the whole difference is which way the taper runs.

The chords take the shear the web is credited withA cantilever of 6 m tapering from 400 to 1200 mm, under a 120 kN tip load, with the shear divided between the web and the two inclined chords. The chord force is M/z and it is not horizontal, so its vertical component is real: V_web = V − (M/z)·dz/dx, which is Résal's result of 1899. At the root the web is left with 33 per cent of the applied shear — exactly d₀/d₁ for a straight taper, with no length, load or material in it. Turn the same member round and the figure becomes 300 per cent: the chords stop helping and start adding, at the section where the moment is largest as well. And the limit is worth having — a member whose depth is proportional to its moment leaves the web nothing to do at all, which is the triangular cantilever every crane jib is.120 kNroot00.20.40.60.810.20.40.60.811.2along the member, tip to rootshear ÷ the shear appliedthe applied shearthe web's sharethe haunch reversedweb shear at the root 33% · reversed 300%
Fig. 3 The same member reversed. Everything about the applied loading is identical and the web is asked for three times as much, which is the same factor the right-way-round haunch saves.

The limiting case, which is a truss

Push the taper until the depth is proportional to the moment. For the tip-loaded cantilever that means dxd \propto x — a wedge whose two chords meet at the point where the load is applied — and the arithmetic gives

Vweb=P(1xkckcx)=0V_{web} = P\left(1 - \frac{x \cdot k c}{k c x}\right) = 0

exactly, everywhere along the member. A cantilever whose depth follows its own moment diagram has no web shear at all.

Chord force against truss depthThe force in a truss chord for a fixed bending moment, against the depth of the truss. The relationship is a reciprocal: the chords form a couple whose lever arm is the depth, so a shallow truss pays for it steeply.0.511.52020040060080010001200depth of the truss1000500333250the same moment, resisted by a longer lever arm
Fig. 4 Chord force against depth, which is the same reciprocal relation from the other side. A wedge is the limit in which the two chords do all the work and nothing crosses between them.

That is not a curiosity, it is a whole family of structures. A crane jib is a wedge. A cable-stayed pylon head is a wedge. The tapered brackets under a mill floor, the triangulated cantilever of a Warren bridge, the tapered flange plate on a plate girder support — all of them are the same idea, and all of them have one property in common: they are two force paths and a spacer. The web of a wedge has nothing to do but hold the chords apart, which is exactly what the diagonals of a truss with no diagonals to carry shear do not have the option of doing.

Read the other way round, the result explains something about trusses. A parallel-chord truss puts real force in its diagonals; a triangular one, loaded at its apex, does not. The difference is entirely the same M/zdz/dxM/z \cdot dz/dx term, arrived at from the geometry of the chords rather than from a lever arm.

Where the shear check actually goes

The practical consequence is a migration. In a prismatic cantilever the worst shear is at the root and everyone knows it. In a tapered one it is not.

Under a tip load the applied shear is constant, so the web shear falls monotonically towards the root and the critical section for shear moves to the tip — the shallowest part of the member, which is also where the web is thinnest. That is a genuinely awkward result, because the tip is where nobody looks: it has almost no moment, its flanges are small, and it is drawn as the unimportant end.

Under a uniform load the applied shear rises towards the root and the correction rises with it, so the two effects fight and the worst station lands somewhere in between. Sweeping it is a two-line calculation and guessing it is not, which is the same finding the tapered member’s bending check produces: a member whose capacity moves has to be checked everywhere rather than at the obvious place.

The load does not taper, and neither does the shearAverage shear stress on the web along the same member. The shear is largest at the root under a uniform load, and the web it crosses shrinks toward the free end, so the shear stress is worst where the bending is least: 0.0 N/mm² at the free end against 16.7 at the root. A taper drawn to suit the moment diagram is drawn against the wrong diagram for the end of it.0123456051015distance from the free end (m)average web shear stress (N/mm²)0.0at the free end
Fig. 5 The shear check along a tapered member under a uniform load, where the applied shear and the chords’ share are both rising and the governing station is at neither end.

The corner of a portal, which is the case that matters

The single most common haunch in construction is the one at the eaves of a portal frame, and it is worth looking at because the sign there is not obvious from the drawing.

A pitched portal has its largest moment at the eaves, and the haunch is put there to provide the depth for it. Reading along the rafter from the apex towards the eaves, both the moment and the depth are increasing — so the chords are helping and the web shear falls, which is convenient because the eaves is also where the shear is largest. The haunch does two jobs and the second is free.

The moment does not stop at the end of the beamA portal frame of 12000 m by 4000 m with fixed bases, carrying 20 kN/m on the beam. The bending moment is drawn on the tension side of every member, and it runs round the corner without a break: 168542094.5 kNm arrives at the end of the beam and 168542094.5 kNm leaves down the column, which is the same number, since joint rotational equilibrium is one of the equations the frame solve satisfied. Midspan carries 191457905.5 kNm, and the two add to 360000000.0 — the 360000000.0 kNm of a simply supported span, to 0.0e+0 kNm. The corner takes 70% of the wL²/12 a fully built-in beam would have carried, because the columns are springs rather than walls: the beam-to-column stiffness ratio is 0.85. The beam's moment crosses zero 1624.41 m from the corner and the column's 1333.33 m above its base.w = 20 kN/mcorner 168542094.5 kNmmidspan 191457905.5 kNm191457905.5 + 168542094.5 = 360000000.0 = wL²/8
Fig. 6 A haunched eaves. The depth grows in the same direction as the moment, so the inclined chord takes part of the shear as well as providing the lever arm.

Read along the column from the base upwards, however, and the picture inverts on one common detail. Where a haunch is fabricated as a straight cut off a rolled section and welded on, the inner flange of the haunch is inclined and the outer one is not, so dz/dxdz/dx is set by one chord alone; and if the frame is designed with a pinned base and a stiff rafter, the moment in the column can be falling over part of the haunched length while the depth is still rising. Over that stretch the correction reverses sign and the web is asked for more than the applied shear.

The general rule is not “a haunch helps”. It is: compare the direction the moment is growing in with the direction the depth is growing in, over the specific length being checked. Two identical haunches on two ends of the same member can be doing opposite things.

The web that is not a web

There is a third case, and it is where the effect stops being a correction and becomes the design.

The cut that severs the stirrups is the cut that counts themA cracked web drawn as the truss it has become: a tension chord along the bottom, a compression chord along the top, concrete struts between the cracks and stirrups crossing them. The free body is a cut parallel to the cracks, which over a lever arm of 630 mm severs z·cot θ/s = 8.4 stirrups at cot θ = 2. Every one of them is at yield, so the shear is their number times their strength, and flattening the crack raises the count rather than the strength. The same cut passes through the bottom chord, which is where the chord force the moment diagram does not contain comes from.the cutcompression chordtension chordstirrups in blue, struts dashedz = 630cot θ = 2 · 8.4 stirrups crossed · V = 573 kN from 1047 mm²/mstrut stress 5.95 N/mm² against 10.56 available
Fig. 7 The truss model of a cracked concrete beam. Its bottom chord is horizontal by assumption, and a tapered member’s is not — so the strut angle available to it changes along the span.

In a reinforced concrete beam the truss model assumes a horizontal tension chord and a horizontal compression chord, and computes a strut angle from the shear the web has to carry. Taper the member and the tension chord follows the soffit. The vertical component of the chord force then subtracts from the shear the struts have to carry, and the links needed fall in proportion — often by a third in a haunched transfer beam, which is a substantial saving in a place where congestion is the real constraint.

The trap in that calculation is the one this essay opened with: the shear used for the link design has to be VwebV_{web} and not VV, and every shear diagram a designer is handed plots VV. Nothing on the diagram says that the member under it is not prismatic.

The man it is named after, and the bridge behind it

Jean Résal was an engineer of the French state bridge service, and the reason his name is attached to a one-line correction is that he was designing the Pont Alexandre III when he needed it.

That bridge is a very flat steel arch of 107 metres, and its ribs are deep at the springings and shallow at the crown. Read along a rib from the crown outwards, the moment and the depth grow together — so the inclined chords take a large share of the shear, and the web plate needed is far lighter than a prismatic analysis would ask for. On a structure whose whole design case was to be as thin as possible over the Seine, that was not a refinement. It was the reason the section worked.

The correction reached the German literature as the Résal-Effekt and the English as, mostly, nothing at all: it appears in bridge codes as a clause about inclined flanges and in very few textbooks as a mechanism. The result is that generations of engineers have derived it from scratch at a haunch, usually correctly and occasionally with the sign the wrong way round.

There is a small historical irony in it. The same effect had been in plain sight for a century in the form every engineer already understood — a triangular truss carries no web force — and what Résal did was to notice that a solid tapered web is the same statement with the diagonals smeared out. The truss analogy has run in that direction ever since: a continuum result recognised because somebody drew the discrete version of it first.

The plate girder, where it is worth money

The place the correction earns most is a welded plate girder over a support, and the arithmetic is worth doing because it is not marginal.

Take a two-span continuous girder haunched over its internal pier from 1,200 mm at midspan to 2,400 at the support. At the pier the moment is at its largest and so is the shear, which is the combination that decides the web thickness for every girder of this shape. With parallel chords the web carries the whole reaction’s share of the shear; with the haunch running the right way it carries half.

Halving the web shear does not halve the web plate, because a web is usually sized for buckling rather than for yielding and the buckling stress goes as the square of the thickness over the depth — but the haunch has also made the panel deeper, which pushes the other way. The two effects have to be taken together, and the net is typically a plate one or two millimetres thinner over a length of twenty metres, or one fewer transverse stiffener every panel. On a bridge that is tonnes.

What it never buys is a shallower girder. The lever arm still has to be there, the chords still carry M/zM/z, and the haunch is providing that as its first job. The shear relief is a second-order benefit of a decision already taken for a first-order reason, which is why it so rarely gets designed for deliberately and so often gets discovered afterwards.

Where the model stops

The derivation assumes the chord force acts along the chord. For a genuinely trussed member — a truss, a cable-stayed deck, a haunched girder with distinct flanges — that is exact. For a solid tapered member it is an idealisation, because the compression in a tapered beam is a stress field rather than a chord force, and it does not all act at the same inclination.

A finite-element solution of a tapered beam shows the correction arriving at somewhat less than the simple formula gives, because the extreme fibre is inclined at dz/dxdz/dx and the fibres nearer the middle are inclined at less. The usual reconciliation is to compute dz/dxdz/dx from the centroids of the chords rather than from the extreme fibres, which is what the lever arm zz means anyway. That is right in principle and it depends on knowing where the chord centroids are, which for a solid section with a varying stress distribution is not a fixed fraction of the depth. Nothing here compares the formula against a plane-stress solution of the same wedge.

And the picture cannot show what happens after the web buckles. Everything above is an elastic force division, and a slender tapered web that has gone into a tension field redistributes its shear along the diagonal the buckle sets rather than the one the geometry sets. The Résal correction survives — the chords still resolve — but the panel geometry that decides the tension-field capacity is a trapezium rather than a rectangle, and the standard treatment of it does not exist.

The generalisation

The habit worth carrying away is smaller than the formula and more useful. A force that is not perpendicular to the cut is not entirely in the plane of the cut, and every internal force diagram on this site is drawn as though it were.

The same slip appears elsewhere. A curved beam’s chord forces are inclined by definition and the same term appears as a radial force. An arch’s thrust is the same statement carried to the point where the whole shear has been resolved away. A sloping column carries part of the floor shear as an axial component. In each case the picture that gets drawn — a vertical cut, a shear force, a moment — carries an assumption about direction that nobody wrote down and nothing on the diagram records.

The way to catch it is the free body. Draw the cut face, draw every force actually crossing it in its own direction, and resolve. A diagram that arrives with its shear already separated from its moment has done part of the work already, and it may have done it for a beam whose chords were parallel.

Shear stress across a sectionThe 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 0.08 against a mean of 0.04 — a ratio of 1.71 — and it falls at the neutral axis, where the bending stress is zero.neutral axispeak 0.1stressflow, q = VQ ÷ Imean stress 0.04 — the value a shear divided by an area would givepeak 1.71× that, and in the place bending ignoresthe flow is continuous; the stress jumps wherever the width does
Fig. 8 The shear flow across a section, drawn as though the flanges were horizontal. Incline them and part of this diagram is carried by the flange force instead, without anything in the drawing changing.
The same beam, cut at x = 3A beam separated at one station. On the exposed face a shear force and a bending moment appear, equal and opposite on the two pieces, with values obtained by summing the forces on whichever piece is easier.2012.57.5shear 12.5moment 37.5the cut, at x = 3nothing was applied here — the internal forces are what the left-hand piece needs
Fig. 9 The cut that every result on this site descends from. What crosses it is decided by the geometry of what is being cut, and a diagram of shear and moment has already assumed an answer to that.

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.

Chord forceDiagram relationsEquilibriumFree bodyHaunchInternal forcesLever armLoad pathResal effectSection shapeShear flowSpan to depthTapered memberTruss analogyWeb shear