Deflection

The beam whose moment is a deflection

A beam's bending moment is the second integral of its load. Its deflection is the second integral of M/EI. They are the same problem, so a deflection can be found by loading a fictitious beam with M/EI and asking a statics question — and the only thing to remember is the supports, which are not remembered but derived, one boundary condition at a time.

Assumes The area of a diagram is a rotation, The diagram is an integral, and that is why it can be drawn by eye and One deflection, without solving everything.

Two facts sit next to each other in every course on structures and are almost never introduced.

The first: a beam’s bending moment is the second integral of the load along it, with the two constants of integration fixed by the supports. The diagram is an integral is that statement, and it is why a moment diagram can be drawn by eye.

The second: a beam’s deflection is the second integral of M/EIM/EI, with the two constants fixed by the same supports.

They are the same problem. So the deflection of a beam can be found by loading a fictitious beam with M/EIM/EI and asking what its bending moment is — which converts an integration into a statics question, and a statics question is the one kind that can be answered by drawing.

The same curve, computed twice and from opposite ends. A cantilever of 6 m, with its deflected shape drawn from a double integration of M/EI and the bending moment of its conjugate beam drawn on top of it. The conjugate is the same span carrying M/EI as a load, with its supports transformed — a real fixed end becomes a free end and a real free end becomes a fixed one, because a fixed end has no slope and no deflection and the conjugate therefore needs no shear and no moment there. The two curves agree to 4.7e-6 of the largest deflection, which is the trapezium rule and not the method. The largest deflection is 36.00 mm against the closed form's 36.00. The reaction of the conjugate beam is -9.000 milliradians, which is the real beam's rotation at that support — so the whole of a slope calculation is one reaction.
Fig. 1 A cantilever’s deflected shape, drawn twice: once by integrating M/EI against boundary conditions, and once as the bending moment of a fictitious beam loaded with M/EI. The two curves are computed by different routines and lie on top of one another.

Which free body produced the number

The conjugate beam, cut at a section, with the M/EIM/EI load to one side of the cut and the transformed supports holding it up.

That is an ordinary free body and the arithmetic on it is ordinary statics: the shear at the cut is the area of the M/EIM/EI diagram to one side, and the moment at the cut is the first moment of that area about the cut. Both are numbers a draughtsman can get from a diagram with a planimeter, which is precisely why the method exists.

What has to be got right is the supports, and the derivation is the whole of the method’s content.

A real simple end has M=0M = 0 and δ=0\delta = 0, and a non-zero rotation. The conjugate’s moment is the deflection and its shear is the rotation, so it needs M=0M = 0 and a non-zero shear — a simple end.

A real fixed end has θ=0\theta = 0 and δ=0\delta = 0. The conjugate needs zero shear and zero moment — a free end.

A real free end has both a rotation and a deflection. The conjugate needs both a shear and a moment — a fixed end.

A real interior support has δ=0\delta = 0 and a kink in the slope. The conjugate needs M=0M = 0 and a jump in shear — an internal hinge.

And a real internal hinge, where the slope jumps and the deflection is continuous, needs a jump in the conjugate’s shear with its moment continuous — an interior support.

Five lines, each one boundary condition read through the correspondence, and not one of them has to be remembered.

The area is the rotation, and its first moment is the movement. A 6 m cantilever under a tip load of 10, with the M/EI diagram beneath it. The shaded area is 180.00, which by the first theorem is the change of slope along the whole member. Its centroid is at 2.000 m, and the first moment about the tip is 720.00 — which by the second theorem is the deviation from the tangent, and for a cantilever that tangent is horizontal, so it is the deflection itself. Integrating the curvature twice instead gives 720.00.
Fig. 2 The two area theorems the correspondence generalises. The area of the M/EI diagram between two points is the change of slope between them, and its first moment about a point is the deflection of that point from a tangent — which are the conjugate beam’s shear and moment before anybody has called them that.

The cantilever, which is the memorable one

A cantilever fixed at the left and free at the right has a conjugate that is free at the left and fixed at the right.

As a structure it is absurd. It is a beam held only at the end that used to be free, loaded along its whole length, with nothing under it anywhere else. Anybody drawing it as a structure would object that it would fall over — and it would, if it were one.

It is not one. A conjugate beam is an integration with supports drawn on it. The “fixed end” at the tip is not a support; it is the statement that the real beam’s slope and deflection are unknown there and therefore that the conjugate’s shear and moment are non-zero. The picture is a piece of bookkeeping, and its absurdity as a structure is the clearest possible sign that it is not being used as one.

Once past that, the arithmetic is a pleasure. For a tip load PP the M/EIM/EI diagram is a triangle of height PL/EIPL/EI at the fixed end. Its area is PL2/2EIPL^2/2EI, which is the tip rotation. Its first moment about the tip is PL2/2EI×2L/3=PL3/3EIPL^2/2EI \times 2L/3 = PL^3/3EI, which is the tip deflection. Two lines and no calculus, and both of the standard cantilever formulae have fallen out of the geometry of a triangle.

Where the method earns its keep

It is fair to ask what a graphical device is for on a site whose figures are generated by solving equations.

It answers a deflection at a point without the whole curve. One deflection, without solving everything is the virtual-work version of the same economy; the conjugate beam gets there by taking a moment about the point rather than by integrating a product, and for a hand calculation the moment is quicker.

It handles a stepped or varying EI without difficulty. The load on the conjugate beam is M/EIM/EI, so a change of section is a step in the load — an ordinary thing to have on a beam — where in the direct integration it is a discontinuity in the differential equation. A haunched beam, a cracked concrete beam with a different II over the supports, a composite beam with a different section in the hogging region: all are conjugate beams with awkward-shaped loads and no awkwardness at all.

It answers a rotation as easily as a deflection, which matters more often than it looks. A bearing has a rotation capacity, a movement joint has a rotation the detail must accommodate, and a cladding panel cracks on a rotation rather than on a deflection — the angle nobody limits is the case for that being the criterion that is left out. The conjugate beam gives the rotation as a shear, which is one step less work than the deflection rather than one step more.

And it gives a check. The conjugate’s reaction is the real beam’s rotation at that support, so a slope and a deflection come out of the same calculation and can be verified against each other. The reaction of the simple-span conjugate is wL3/24EIwL^3/24EI, which is the standard end rotation, and finding it as a by-product is the sort of redundancy a hand method should have.

A beam of two stiffnesses has one diagram with a step in it. A 6 m cantilever whose flexural rigidity is 2 times larger beyond 3 m — a deep root and a shallow tip — under a tip load of 10. The M/EI diagram therefore has a step in it at a station where nothing about the moment changes, and the method adds two areas where an integration would need two cases and two more constants. The shaded area is 157.52, which by the first theorem is the change of slope along the whole member. Its centroid is at 1.714 m, and the first moment about the tip is 675.07 — which by the second theorem is the deviation from the tangent, and for a cantilever that tangent is horizontal, so it is the deflection itself. Integrating the curvature twice instead gives 720.00.
Fig. 3 The case the conjugate beam handles most gracefully. Halving EI over part of the span doubles the load on the conjugate beam there — a step in a load, which is nothing at all — where the direct integration meets a discontinuity in the equation it is integrating.

Two routes, and why agreeing matters

The figure at the top of this essay draws the same curve twice, and it is worth being clear that the two are genuinely different computations rather than the same one printed twice.

The direct route integrates the curvature twice along the beam and fixes the constants from the boundary conditions — for a cantilever, by starting both integrals at zero at the fixed end; for a simple span, by subtracting the chord through the two ends.

The conjugate route computes the transformed beam’s reactions by statics — moments about one end for the far reaction, then vertical equilibrium — and gets the moment at each section from the load to one side of it.

Neither uses any part of the other. They agree here to five parts in a million, which is the trapezium rule at four hundred stations rather than the method, and both agree with PL3/3EIPL^3/3EI to the same order.

That is worth having as a check on the implementation as well as on the mathematics, and it is the habit this site runs on: a claim that two things are the same is worth making only if there is a computation that could have said otherwise.

The same curve, computed twice and from opposite ends. A simply supported beam of 6 m, with its deflected shape drawn from a double integration of M/EI and the bending moment of its conjugate beam drawn on top of it. The conjugate is the same span carrying M/EI as a load, with its supports transformed — a real fixed end becomes a free end and a real free end becomes a fixed one, because a fixed end has no slope and no deflection and the conjugate therefore needs no shear and no moment there. The two curves agree to 1.5e-5 of the largest deflection, which is the trapezium rule and not the method. The largest deflection is 10.12 mm against the closed form's 10.13. The reaction of the conjugate beam is 5.400 milliradians, which is the real beam's rotation at that support — so the whole of a slope calculation is one reaction.
Fig. 4 The same two routes on a simply supported span under a uniform load. The conjugate here has the same supports as the real beam, because a simple end transforms to a simple end — and the reactions of the fictitious beam are the real beam’s end rotations, wL³/24EI.

Reading a real deflection off a diagram

The method is worth one worked case at the scale a designer meets, because the arithmetic is short enough to do standing at a drawing.

A simply supported span of 6 m under 12 kN/m, with EI=20,000EI = 20{,}000 kNm². The free bending moment diagram is a parabola of height wL2/8=54wL^2/8 = 54 kNm. Divide by EIEI and the conjugate load is a parabola of height 2.70×1032.70 \times 10^{-3} per metre.

The area of a parabola is two thirds of base times height: 23×6×2.70×103=10.8×103\tfrac{2}{3}\times 6 \times 2.70\times10^{-3} = 10.8\times10^{-3}. Half of that is each end reaction of the conjugate, 5.40×1035.40\times10^{-3} radians — which is the real beam’s end rotation, and the standard formula wL3/24EIwL^3/24EI gives exactly the same.

The moment at mid-span is the reaction times 3 m less the first moment of half the load about mid-span: 5.40×103×35.40×103×38×6=16.2×10312.15×103=4.05×1035.40\times10^{-3}\times 3 - 5.40\times10^{-3}\times \tfrac{3}{8}\times 6 = 16.2\times10^{-3} - 12.15\times10^{-3} = 4.05\times10^{-3} m, which is 4.05 mm. And 5wL4/384EI5wL^4/384EI is 4.05 mm.

Two standard results from the geometry of a parabola, with no integration performed and no formula recalled. That is what the method was for, and it is still the fastest way to get a deflection on a beam whose EIEI or whose loading is not in anybody’s table.

The shear part is not a curve at all. A 300 × 600 rectangle spanning 2,400 mm, a span-to-depth ratio of 4, with its bending deflection and its total drawn together. Bending gives 0.0254 mm and shear a further 0.0049 mm, so 16.3% of the movement is the term beam theory drops. The shear part is drawn separately beneath: two straight lines meeting under the load, each limb straight to 2e-16 of the peak. It is the shear diagram integrated once where the moment diagram above it is integrated twice, so it carries one degree of curvature less than the bending shape — none at all here. The real movement is 1 in 79,116 of the span; both panels are drawn at about 11,932 times it.
Fig. 5 What is being computed, drawn at an exaggeration the caption has to state: a beam at its serviceability limit has deflected by about a three-hundredth of its span, which is thinner than the line used to draw it. Every deflected shape in this collection is drawn many times its true size.

The duality, and where it stops

The support table has a pattern in it that is more than a mnemonic: the conjugate of a restraint is a release, and the conjugate of a release is a restraint.

Count them. A real beam with rr redundants has rr more restraints than statics needs. Transform every one of them and the conjugate has rr fewer than it needs — it is a mechanism, short by exactly the number of equations the real beam was short of.

So a propped cantilever, one degree indeterminate, has a conjugate that is free at one end and free at the other and loaded: not a structure. A fixed-ended beam, two degrees indeterminate, has a conjugate free at both ends. A two-span continuous beam has a conjugate with a hinge where a support was and one support where there were three.

That is why the method belongs to determinate beams, and it is not a convention that could have been chosen differently. The missing equations in the real problem are the missing restraints in the fictitious one, and no amount of care with the table will produce them. The moment-area theorems have the same limit for the same reason, and the standard workaround is the same: release the real beam until it is determinate, solve it, and put the redundant back as an unknown force — which is choose what to take away, and is the force method.

One support too many. The same uniformly loaded beam with three sets of restraints, and the bending moment in each. Adding restraint moves moment from mid-span to the supports and lowers the peak — but only the first case can be solved by statics.
Fig. 6 The beam whose conjugate does not exist. A propped cantilever is one degree redundant, so its fictitious beam is one restraint short — and the extra equation has to come from compatibility, which is what the force method supplies and what the conjugate beam cannot.

Where it came from, and why it looks like that

Otto Mohr published the two area theorems in 1868 and Christian Otto Mohr’s students turned them into the conjugate beam over the following decades; the elastic-weights version and the column analogy are the same idea pushed further, until it solves indeterminate frames by treating the M/EIM/EI field as a load on a fictitious cross-section.

The reason it exists in that form is worth knowing. Mohr was working on the graphical analysis of structures, where a truss’s displacements come out of a Williot diagram and a force system out of a funicular polygon, and the whole intellectual project was to replace calculation with drawing — because drawing was faster, checkable by eye, and available to people who could not integrate. The polygon that finds the shape is that project’s other great success.

Seen that way, the conjugate beam is not a trick for remembering formulae. It is the last step of a programme: turn an integration into a statics problem, because statics can be drawn. The fact that it survives into a period when nobody draws anything is a statement about how good the reduction was.

Where the model stops

Shear deformation was ignored. The whole correspondence rests on curvature being M/EIM/EI, and for a deep beam it is not — there is an additional curvature from shear which the conjugate load does not contain. The deflection that is not bending is the missing term, and adding it means adding a second load to the conjugate beam proportional to the shear.

The beam was elastic. A cracked concrete beam has an EIEI that varies with the moment, so the conjugate load is not a scaled copy of the moment diagram and has to be computed section by section — which is fine, and is exactly how a hand deflection calculation on a concrete beam is done.

Axial force was absent. A beam-column’s curvature includes a PδP\delta term, which makes the equation non-linear in the unknown, and no fictitious beam loaded with a known distribution can represent it. The load that makes itself worse is that term.

Support settlement was not in it. A support that moves adds a rigid-body component to the deflected shape which the curvature does not contain, so it has to be superposed afterwards rather than found from the conjugate beam. The support that moved is the field it adds, and on an indeterminate beam it also changes the moment diagram the conjugate is loaded with.

And the beam was straight. The correspondence generalises to a curved member only through a different pair of theorems, because the relation between curvature change and displacement is no longer a double integral along a straight axis.

The generalisation

The idea worth carrying is that two problems with the same differential equation and the same kind of boundary conditions are the same problem, and that recognising it converts one into whichever is easier to solve.

That is a much larger idea than a beam. A beam on an elastic foundation and a cylinder’s edge disturbance are the same equation, so a table of one solves the other — the length a structure was never given uses that in both directions. Torsion of a section and the deflection of a soap film over the same outline are the same equation, which is Prandtl’s membrane analogy and is how torsion constants were measured before they were computed. A steady heat flow and a seepage flow are the same equation. The stress function of a plate and the deflection of a membrane are the same equation.

The conjugate beam is the smallest and most domestic member of that family: a beam and a beam. Which is why it is the one to learn the habit on, and why the habit is worth more than the method. When a calculation is awkward, the useful question is not how to do it better but what else obeys the same equation — because somewhere there is a version of it whose answer is already drawn. The conjugate beam’s answer had been drawn for four hundred years before anybody wanted a deflection out of it: it is a bending moment diagram, and bending moment diagrams were the first thing this subject learned to draw.

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.

Boundary conditionsConjugate beamCurvatureDeflectionDeterminacyDualityElastic curveFree bodyGraphic staticsIndeterminacyIntegrationMoment areaMoment diagramSlopeStiffness method