Sections and stress

Both at once, and neither matters until it does

A section carrying shear has less moment capacity, and the reduction is the web's share of the plastic modulus times one minus the root of one minus the shear ratio squared. On a rolled beam that share is a quarter, so half the shear capacity costs three and a half per cent — and then the last tenth costs more than the first eight.

Assumes Bending is a pair of forces, pushing and pulling, The shear nobody draws and After the first yield, which is not the end.

Every capacity computed so far on this site has been computed alone. A plastic moment with no shear near it; a shear capacity with the flanges ignored. That separation is a convenience, and at the support of a continuous beam it is exactly where the assumption is least defensible: the largest moment and the largest shear are in the same cross-section, a few millimetres apart, in the same steel.

The interaction between them is real, and its shape is unusual enough to be worth the whole page. Nothing happens for the first half of the shear range, and then everything happens at once.

Nothing happens, and then everything happensThe moment capacity left to a section already carrying shear, against the shear as a fraction of what the web can take. The web holds 26.1% of this section's plastic modulus and the flanges hold the rest, and only the web's share is reduced — by the factor √(1 − v²) that von Mises leaves it. So the curve is flat for most of its length: the first per cent of moment is not lost until v = 0.27, half the shear capacity costs 3.5%, and 15% is not reached until v = 0.9. The tangent at v = 1 is vertical, which is why the last tenth of the shear range costs more than the first eight.00.20.40.60.810%20%40%60%80%100%shear, as a fraction of the web's capacitymoment capacity leftthe sectionthe web alone√(1 − v²)96.5%85.3%web 26.1% of the plastic modulus · M_pl 744 kNm · V_pl 959 kN
Fig. 1 The curve. Moment capacity left, against shear as a fraction of what the web can take. The first per cent is not lost until v=0.27v = 0.27; half the shear capacity costs 3.5%; and the tangent at v=1v = 1 is vertical, so the last tenth of the range costs more than the first eight.

Which free body produced the number

The mechanism is von Mises and there is nothing else in it.

Take a fibre in the web. It is carrying a shear stress τ=V/Av\tau = V/A_v and it is being asked for a normal stress as well. The yield condition in two dimensions is

σ2+3τ2=fy2\sigma^2 + 3\tau^2 = f_y^2

so what is left for the normal stress is fy13τ2/fy2f_y\sqrt{1 - 3\tau^2/f_y^2}. Write v=V/Vplv = V/V_{pl} and note that Vpl=Avfy/3V_{pl} = A_v f_y/\sqrt{3} makes τ/τy\tau/\tau_y exactly vv. Then

σleft=fy1v2\sigma_{\text{left}} = f_y\sqrt{1 - v^2}

Now assemble the plastic moment out of the parts. The flanges are outside the web, carry no shear, and reach fyf_y whatever is happening below them. The web reaches σleft\sigma_{\text{left}}. So

Mred=Wffy+Wwfy1v2M_{red} = W_f f_y + W_w f_y \sqrt{1 - v^2}

and dividing by Mpl=(Wf+Ww)fyM_{pl} = (W_f + W_w) f_y,

MredMpl=1ρ(11v2),ρ=WwWf+Ww\frac{M_{red}}{M_{pl}} = 1 - \rho\left(1 - \sqrt{1 - v^2}\right), \qquad \rho = \frac{W_w}{W_f + W_w}

The whole interaction is one number: the web’s share of the plastic modulus.

The web keeps what the shear has not already spentAn I-section carrying 50% of its shear capacity, with the normal stress each part has left. The flanges are outside the web and carry no shear, so they still reach 355 N/mm². The web is at a shear stress of v times its own yield in shear, so von Mises leaves it √(1 − v²) of the yield stress, which is 307 N/mm². The moment that follows is 718 kNm against 744 — the loss is entirely the web's, and the web is 26.1% of the section's plastic modulus.500flanges at full yieldweb reduced by the shear355307 N/mm²stress availablev = 0.50 · M = 718 kNm of 744 · loss 3.5%the elastic worst point is the web–flange junction, which is neither of the two the plastic picture names
Fig. 2 The section at half its shear capacity, with what each part has left. The flanges are still at 355 N/mm²; the web is at 35510.25=307355\sqrt{1 - 0.25} = 307. That is the entire calculation, drawn.

The number, for a real section

For the beam here — 200 mm flanges 16 mm thick, a 468 mm web 10 mm thick, at 355 N/mm² — the two plastic moduli are

Wf=2bftfhw+tf2=1.549×106  mm3Ww=twhw24=0.548×106  mm3W_f = 2 b_f t_f \frac{h_w + t_f}{2} = 1.549 \times 10^6\;\text{mm}^3 \qquad W_w = \frac{t_w h_w^2}{4} = 0.548 \times 10^6\;\text{mm}^3

so ρ=0.261\rho = 0.261. A quarter of the section’s bending strength is in the web and three quarters is in the flanges, which is the whole point of an I-section and is also why the interaction is so weak.

The consequences fall out of the algebra:

shear, vv moment lost
0.27 1%
0.50 3.5%
0.59 5%
0.79 10%
0.90 14.7%
0.99 22.4%

Half the web’s shear capacity costs three and a half per cent of the moment. That is not a small effect that ought to be checked anyway; it is smaller than the difference between one rolled section and the next in the same serial size.

Every strip counts by the square of its distanceA rectangular section divided into equal strips, with each strip's contribution to the second moment of area drawn beside it. The strips are identical in size; only their distance from the neutral axis differs.neutral axiscontribution of each striptotal I = 135.00 × 10⁶the outer strips do almost all of the work
Fig. 3 Where ρ\rho comes from. Material far from the middle is what makes an I-section efficient, and the same arrangement that puts three quarters of the strength into the flanges puts three quarters of it out of reach of the shear. The section’s shape has already decided how much this page matters to it.

Why the far end is so steep

1v2\sqrt{1 - v^2} has an infinite derivative at v=1v = 1. That single fact is the reason the interaction has the shape it does, and it is worth reading physically rather than as calculus.

Near v=1v = 1 the web is very nearly fully committed to shear. The normal stress it has left is falling as the square root of the remaining capacity, so a small further increase in shear takes a large fraction of what is left. Between v=0.9v = 0.9 and v=0.99v = 0.99 the moment loss goes from 14.7% to 22.4% — nearly as much as it lost over the whole range from zero to 0.9.

Which gives the practical rule the curve is really about. There is no need to be careful about the interaction anywhere except very close to the shear limit, and there it is not a correction, it is a cliff.

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. 4 Which failure arrives first, which is the standing question this curve answers for one pair. Two capacities computed separately, a member that has to satisfy both, and a crossing point that is a property of the section rather than of the load.

The one section where it bites

On a simply supported beam the interaction is worth nothing: the moment peaks where the shear is zero and the shear peaks where the moment is zero. It takes continuity, or a cantilever, to put both maxima in the same place.

For a fixed-ended beam under a uniform load, the support carries wL2/12wL^2/12 of moment and wL/2wL/2 of shear at the same section. On the 9 m beam at 60 kN/m drawn in the span view, the support shear is 270 kN against a VplV_{pl} of 959, so v=0.28v = 0.28, and the interaction adds 1% to a utilisation of 54%. Not worth the arithmetic.

Shorten and load it, though: 4.5 m at 340 kN/m gives a support shear of 765 kN, v=0.80v = 0.80, and a utilisation that goes from 77% ignoring the interaction to 86% including it. Nine points of utilisation, on the section that governs, from a term the same beam did not need at twice the span.

The one section where both are largest at onceUtilisation along a 9 m beam under 60 kN/m, computed against the reduced capacity and against the full plastic moment. At midspan the shear is nothing and the two agree exactly. At the support the shear is 270 kN, which is 28% of the web's capacity, and the interaction adds 1.1% to the utilisation there. That is a small number and it is at the only station where it is not zero — which is the shape of this whole subject: an effect that is negligible everywhere except at the one section that governs.0246800.10.20.30.40.50.6distance along the span (m)M ÷ capacitywith interactionM_pl aloneworst at x = 0.00 m: 55.0% against 54.4%
Fig. 5 Utilisation along the span, computed both ways. At midspan the shear is nothing and the two agree exactly; at the support they part. The effect is negligible everywhere except at the one station that decides the beam, which is a shape this subject produces often and which makes it very easy to dismiss.
Load, shear and moment — a simple spanThe 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.4 per unit lengthshear17.8moment39.5 at x = 4.44the moment peaks exactly where the shear passes through zero
Fig. 6 Where the two diagrams peak. Shear is the derivative of moment, so on a simply supported beam a maximum of one is a zero of the other — and continuity is what breaks that coincidence, by putting a large moment at a support where the shear has not yet turned round.

The same shape, one action along

The curve above is not the only interaction on this site, and it is worth putting beside the one it most resembles.

Axial force and moment interact for the same reason: an axial force commits part of the section, and what is left carries the moment. But the arithmetic differs in a way that changes the shape completely. Axial force commits the material nearest the neutral axis, which is the material contributing least to the moment, so the axial–moment curve is also flat near the origin — but it is flat because of where the material is, not because of a square root, and it reaches zero linearly rather than vertically.

So the two curves are flat for opposite halves of their range. The moment–shear one falls off a cliff at the end; the moment–axial one arrives at its end smoothly and leaves the section with nothing.

Two ways to fail, and the curve between themThe exact plastic interaction between axial force and moment for two sections of identical area, both normalised by their own squash load and their own plastic moment. The rectangle stands 25.0% of its plastic moment outside the straight line at an axial ratio of 0.50; The I-section stands 6.0% of its plastic moment outside the straight line at an axial ratio of 0.12. Every section here is symmetric about its centroid, so the equal-area axis and the centroid coincide and it makes no difference which the moments are taken about. The straight line is the rule that says the two capacities share out in proportion, and everything between it and a curve is capacity that rule gives away.00.20.40.60.8100.20.40.60.81moment ÷ plastic momentaxial force ÷ squash loadrectangle: 25.0% of Mp outside the lineI-section: 6.0% of Mp outside the linethe straight-line rule
Fig. 7 Two ways to fail at once, for axial force and moment. Same idea, different mechanism: there the section is divided by position, here it is divided by a yield criterion, and the difference between a geometric argument and a material one is visible in the shape of the two curves.

A hinge at high shear is a worse hinge

The plastic moment above is a strength. Using it in an analysis needs something more: the section has to be able to hold that moment while it rotates, because a collapse mechanism needs several hinges and the first one formed has to survive until the last one does.

A web at high shear is much worse at that than a web at low shear. It is already close to its shear yield, its normal stress capacity is on the steep part of the square root, and small further shear strain takes what is left. Hinges at supports of continuous beams, which is exactly where the shear is largest, are therefore the least reliable hinges in any mechanism — and the redistribution that plastic design depends on is asking most of the section least able to give it.

That is a ductility argument rather than a strength one, and this page’s curve says nothing about it. The curve gives a capacity; whether the section can be relied on to keep delivering it through a rotation is a separate question with a separate answer.

The collapse mechanism of a fixed-ended beamA collapse mechanism, with the hinge position found by searching rather than quoted. Every position gives an upper bound on the collapse load; the lowest is 146.96, at a hinge 50.0 per cent along, which is a coefficient of 16.000 times Mp over the square of the span.sagging hinge at 4.50hinge at the fixed endand herelowest upper bound: 146.96every hinge position gives an upper bound on the collapse loadassumed position of the sagging hingecoefficient 16.00 Mp ÷ L²
Fig. 8 The mechanism the capacity is for: hinges at both supports and one in the span, and the support hinges have to hold while the span one forms. Both support hinges are at the maximum shear, which is where the interaction curve is steepest.

The elastic picture disagrees about where the worst point is

Everything above is plastic: the section is at yield through its depth and the question is how much of it is available for bending. The elastic question is different and its answer is different.

Take the same short beam at working load. At the support, three stations are worth measuring:

station σ\sigma τ\tau von Mises
extreme fibre 312 0 312
web–flange junction 292 129 367
neutral axis 0 174 302

The worst point is the junction, and it is worst by a margin. It has 94% of the bending stress — the flange is thin, so the junction is close to the extreme fibre — and a shear stress that is nearly the largest in the section, because the web is where the shear flow concentrates.

This is the same finding as the one on principal stress, and the two pages are the same observation about different questions. That one asks where the material first yields; this one asks what the section as a whole will carry once it has. The elastic worst point and the plastic reduction are not two answers to one question, and neither replaces the other.

One point, every plane through it, one circleA point carrying 292 N/mm² across one face, 0 across the other and 129 of shear. As the plane is turned, the pair (σ, τ) runs round a circle of radius 194.8 centred at 146.0 — and it goes round at twice the rate the plane does, which is the part always misremembered and the part that makes the picture work. The principal stresses are 340.8 and -48.8, on planes 20.7° from the face the 292 acts on; the largest shear on any plane is 194.8, exactly the radius, and it sits 45° from those — which is 90° round the circle. The von Mises stress that ranks this state against any other is 367.7.στthe x faceσ₁ = 340.8σ₂ = -48.8τ max 194.8the plane turns by 20.7°, the circle by 41.5°von Mises 367.7 N/mm²
Fig. 9 The circle for the junction. Combining a normal stress with a shear stress is a rotation, and the number that comes out is larger than either — which is the whole of why the junction beats the extreme fibre.
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 2.66 against a mean of 0.33 — a ratio of 7.97 — and it falls at the neutral axis, where the bending stress is zero.neutral axispeak 2.7stressflow, q = VQ ÷ Imean stress 0.33 — the value a shear divided by an area would givepeak 7.97× that, and in the place bending ignoresthe flow is continuous; the stress jumps wherever the width does
Fig. 10 And the shear flow that puts it there. The flow jumps as the section narrows at the junction, so the largest shear stress in the flange is small and the smallest in the web is not — the discontinuity in the diagram is exactly the junction the table above is about.

A plate girder has a stronger interaction and a weaker web

Everything scales with ρ\rho, and ρ\rho is a design decision.

A rolled beam puts a quarter of its plastic modulus in the web because rolling wants thick material. A welded plate girder, proportioned to carry shear over a long span, puts far more there: for a 600 by 6 web with 150 by 10 flanges, ρ\rho rises to 0.37, and half the shear now costs 5% of the moment instead of 3.5%.

That is the smaller half of the change. The larger half is that a 600 by 6 web has a slenderness of 100 and does not reach fy/3f_y/\sqrt{3} at all — it buckles in shear first, and the capacity it does have comes from the diagonal tension field that forms afterwards. At that point the interaction on this page has to be rewritten against a different shear capacity and a web whose behaviour is post-buckling rather than plastic.

The section most likely to meet a real moment–shear interaction is the section this model describes least well, which is a shape that recurs in this subject often enough to be worth naming.

A 6 mm plate, and the width it can beThe elastic critical stress of a plate in compression against its width, with the yield stress drawn across it. Below 321 mm the plate reaches yield before it buckles; above it the plate ripples first, and the fraction of the width still carrying load falls away — at 700 mm only 41 per cent of it is still working.1002003004005006007000200400600plate width (mm)slender beyond 321 mmyieldcritical stress — inverse square in the widthwhat the plate actually delivers, over its full width
Fig. 11 The plate that ripples before it yields, which is what a slender web does with the shear this page assumed it could carry plastically. The interaction curve above assumes a web at fy/3f_y/\sqrt{3}, and a web at its critical buckling stress is somewhere else entirely.
A buckled panel is a truss that nobody drewA 1000 × 1000 panel of 6 mm web, at d/t = 167. It buckles in shear at 63.8 N/mm², which is 383 kN — and it then carries 696 kN, 1.82 times as much, because the tension diagonal takes over from the compression one that has gone. The band runs at 22.5° with a membrane stress of 252 N/mm² over a width of 541 mm, and it pulls on the flange at 221.3 N per millimetre of its length. A web that never buckled at all would have reached 953 kN, so the panel ends at 73% of a stocky web's capacity on a fraction of its steel.stiffeners at 1000 mmthe band at 22.5°the truss it has becomestiffener in compression,web in tensionbuckles at 383 kN · carries 696 kN · a stocky web would reach 953 kNσ in the band 252 N/mm² over 541 mm
Fig. 12 And what it does afterwards: a diagonal tension field anchored on the flanges and the stiffeners, carrying more shear than the buckling load, with the flanges now bending as well as carrying axial force. Every term in the interaction changes, and none of them changes in the direction that makes the check easier.

Where the model stops

The shear stress is uniform over the web. It is not — the parabolic distribution has its peak at the neutral axis and is about 10% below it at the junction — and the plastic model does not care, because at collapse the web is fully plastic in shear and the distribution really is uniform. The elastic table above uses the true distribution and the plastic curve does not, and that is deliberate rather than inconsistent.

The web is assumed to reach yield in shear. A slender web buckles first, and then the whole of this page is about a section that does not exist: the shear capacity is set by plate buckling rather than by Avfy/3A_v f_y/\sqrt{3}, and the moment interaction has to be written against that instead.

And the flanges carry no shear at all. They carry a little, and it is genuinely negligible: the shear flow in a flange runs horizontally rather than vertically, so it contributes almost nothing to the vertical force even though it is what makes the flange work.

What the pictures cannot show

The interaction curve is drawn for a section. A beam has a length, and what the curve says about the section at the support says nothing about whether the beam can redistribute — a fixed-ended beam that reaches its reduced capacity at the support forms a hinge there and carries on to a span mechanism, so the reduced capacity is a stage rather than an end.

Nor can the drawing show that ρ\rho is a design variable. A deeper, thinner web puts more of the plastic modulus into the web — for a 600 by 6 web with 150 by 10 flanges ρ\rho rises to 0.37 and half the shear costs 5% instead of 3.5% — so a plate girder proportioned for shear has a stronger interaction than a rolled beam, on top of having a slenderer web.

The assumption the figure rests on

The shear area is the web, full stop: Av=hwtwA_v = h_w t_w, with the root fillets and the part of the flange over the web ignored. That is a convention rather than a measurement, and it is a conservative one — real shear areas are quoted a few per cent larger. Every vv on this page is measured against it, so the curve moves slightly left if a more generous definition is used, and the shape of the curve does not move at all.

The ladder from here

Later rungs on this anchor: the interaction with axial force as well, which is the same fibre argument with three actions and a surface rather than a curve. Slender webs, where the shear capacity is a buckling load and the interaction is written against tension-field action instead. The interaction in a plastic hinge that has to rotate, where a web at high shear has much less rotation capacity than one at low shear — which is the failure mode this page’s ductility assumption quietly needs. Bolted and welded connections at a support, where the same combination has to cross a joint. And the elastic side developed properly: the von Mises contour over the whole section, and why its peak moves from the junction to the neutral axis as the span shortens.

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.

Bending stressContinuous beamFlangeInteractionPlastic hingePlastic modulusPrincipal stressShearShear areaUtilisationVon misesWebYield criterion