Deflection

The area of a diagram is a rotation

A deflection is the double integral of a bending moment, and the two constants of integration are the whole difficulty. Mohr's theorems replace them with two pictures — an area, and where that area's centre of gravity sits.

Assumes One deflection, without solving everything, The diagram is an integral, and that is why it can be drawn by eye and Stiffness is not strength, and usually it is the one that governs.

A beam’s deflected shape is the second integral of M/EIM/EI, and nobody has ever found the integration hard. The difficulty is entirely in the two constants: one for the slope, one for the position, and both of them fixed by conditions at the ends rather than by anything in the integrand. Set the problem up as algebra and the constants arrive as two simultaneous equations that carry no meaning. Set it up as geometry and they arrive as two statements about a picture that is already drawn.

The area is the rotation, and its first moment is the movementA 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 720.00.10centroid at 2.00 mM/EIarea = 180.00 · first moment = 720.00by double integration: 720.00
Fig. 1 A 6 m cantilever under a tip load of 10, with its M/EI diagram beneath. The shaded area is 180, which is the rotation of the tip relative to the root. Its centroid is at 2.00 m — one third of the span from the root, not two — and the first moment of that area about the tip is 720, which is the deflection.

Two numbers have come out of that picture, and neither of them was integrated for. 180 is PL2/2PL^2/2, and 720 is PL3/3PL^3/3. The first is the tip rotation and the second the tip deflection, and both were obtained by measuring an area and finding where its centre of gravity sits.

The two theorems, and why they are one theorem

Write the elastic curve as v=M/EIv'' = M/EI and integrate once between two stations AA and BB:

θBθA=ABMEIdx\theta_B - \theta_A = \int_A^B \frac{M}{EI}\,dx

That is the first theorem and it is a statement about area. The change in slope of the elastic curve between two points is the area under the M/EIM/EI diagram between them — not proportional to it, not approximately it, but exactly it, because the diagram is the derivative of the slope.

Integrate a second time, and the constant is chosen by measuring the deviation from a tangent rather than a datum:

tB/A=ABMEI(xBx)dxt_{B/A} = \int_A^B \frac{M}{EI}\,(x_B - x)\,dx

which is the second theorem: the vertical distance from BB on the elastic curve to the tangent drawn at AA is the first moment of that same area about BB. One area, taken twice — once plain, once weighted by distance — and the second is the first with a lever arm on it, exactly as a section’s second moment is its area weighted twice.

For a cantilever the second theorem is the whole answer, because the tangent at a built-in end is horizontal by definition and a deviation from a horizontal tangent is a deflection. That is why the hero figure needs no construction at all.

Which free body produced the number

Cut the cantilever at a station xx and take the piece between the cut and the free tip. The only force on it is the tip load PP at a distance (Lx)(L-x), so the moment on the cut is P(Lx)-P(L-x): linear, zero at the tip, PL-PL at the root. That is the diagram in the figure, and it was drawn from the free body rather than recalled.

Its area is 12LPL=PL2/2=180\tfrac{1}{2} \cdot L \cdot PL = PL^2/2 = 180, and the centroid of a triangle sits one third of the way from its wide end — so at L/3=2.00L/3 = 2.00 m from the root. The first moment about the tip is therefore 180×(62)=720180 \times (6 - 2) = 720, and the closed form PL3/3=10×216/3PL^3/3 = 10 \times 216/3 agrees exactly.

The figure prints both routes side by side: 720 from the geometry, 720.000 from integrating the curvature twice and applying the boundary conditions algebraically. The agreement is not a check that the method works; it is the observation that the two are the same operation.

The construction the method is famous for

A simply supported span has no horizontal tangent anywhere, so the second theorem does not hand over a deflection. It hands over a deviation, and the deflection has to be assembled from two of them.

The area is the rotation, and its first moment is the movementA 8 m simply supported span under a central load of 10, with the M/EI diagram beneath it. The shaded area is 426.67, which by the first theorem is the change of slope along the whole member. Its centroid is at 4.000 m, and the first moment about mid-span is 1706.7 — 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 533.33.centroid at 4.00 mM/EIarea = 426.67 · first moment = 1706.7by double integration: 533.33
Fig. 2 An 8 m simply supported span under a uniform load of 10, with its parabolic M/EI diagram. The whole area is 426.67 — which is wL³/12, and is the change of slope from one end of the beam to the other rather than any single rotation.

The construction runs like this. Draw the tangent at AA. The far support BB sits on the beam, so its deflection is zero, and its deviation from that tangent is therefore the whole rise of the tangent over the span: tB/A=1706.67t_{B/A} = 1706.67, and dividing by the span gives the slope at AA, θA=213.33\theta_A = 213.33. The closed form is wL3/24=10×512/24wL^3/24 = 10 \times 512/24, and it agrees.

Now go to mid-span. The tangent at AA has risen 213.33×4=853.33213.33 \times 4 = 853.33 by the time it gets there; the beam has deviated from that tangent by tC/A=320.00t_{C/A} = 320.00; and the deflection is the difference, 533.33533.33. The closed form is 5wL4/384EI=5×10×4096/3845wL^4/384EI = 5 \times 10 \times 4096/384, and it agrees to the twelfth figure.

Neither 853.33 nor 320.00 is a deflection. They are two geometric quantities whose difference happens to be one, and every reader who has found this method slippery has found it slippery here. The compensation is that the whole calculation is a subtraction of two areas’ first moments, done on a diagram that had to be drawn anyway.

The first theorem earns its keep on the same beam in a different way. The total area is 426.67; the two end slopes are 213.33-213.33 and +213.33+213.33; their difference is 426.67. So the area is not “the rotation” of anything — it is the change of rotation, and on a symmetric beam the two rotations are equal and opposite and the area is twice either of them.

The method against the method it replaced

Virtual work asks a different question and gets the same answer.

The deflection at x = 4, by virtual workThree diagrams: the moment from the real load, the moment from a unit load placed where the answer is wanted, and their product. The area under the third, divided by EI, is the deflection — 1066.67 here. No standard case was consulted, so the method works for any load pattern at all.100real Mpeak 200.0a unit load, here and nowhere elseunit mM × marea ÷ EI = 1066.67the unit load is the only place the question 'deflection where?' is asked
Fig. 3 The unit-load construction on a comparable beam: a real load’s moment diagram, a unit load’s, and the product whose area divided by EI is the deflection. It gives a deflection at one point directly, and gives nothing about the shape between points.

The two methods divide the labour differently, and the division is worth naming because it survived a century of being taught side by side. Virtual work is best when one number is wanted at one place — it needs a second analysis for the unit load and then produces the answer with no construction. Moment-area is best when the shape is wanted, or when the beam is not prismatic, because a change of EIEI is a change to the diagram being measured rather than a new case in an integral.

Moment distribution belongs to the same family of methods and answers a third question — the moments in a redundant frame — by iterating rather than integrating. All three date from the same fifty years, and all three exist because the alternative was solving simultaneous equations by hand.

The beam the method was made for

A beam of two stiffnesses has one diagram with a step in itA 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 720.00.10EI ÷ 2 beyond herecentroid at 1.71 mM/EIarea = 157.52 · first moment = 675.07by double integration: 720.00
Fig. 4 The same cantilever with twice the flexural rigidity beyond mid-span — a deep root and a shallow tip. The moment diagram is untouched; the M/EI diagram has a step in it at a station where nothing about the loading changes. The area drops from 180 to 157.5, because half of the outer triangle has gone.

A prismatic beam has closed forms and does not need a method. A stepped one does, and here the geometric formulation costs almost nothing: the diagram acquires a discontinuity, the area is computed in two pieces and added, and the centroid is the weighted mean of two centroids. The arithmetic that replaces it in an algebraic treatment is two integrations with two more constants and two matching conditions at the step.

The area lost is exactly half the tip triangle — 12330=45\tfrac{1}{2}\cdot 3 \cdot 30 = 45, halved by the doubled stiffness, so 18022.5=157.5180 - 22.5 = 157.5. And the centroid moves toward the root, because the stiffened half now contributes less. A haunched beam, a plated beam, a beam with a cover plate that stops short: all of them are this figure, and all of them are why the method outlived the slide rule that made it necessary.

The check that reaches for something else

Three routes to the same curve, one of which is a different questionMid-span deflection of a 8 m simply supported beam under a 10 unit load, against where the load is placed, computed by the two moment-area theorems and by integrating the curvature twice with the boundary conditions applied algebraically. The two disagree by at most 6.7e-13% of the answer, and both sit within 0.000086% of the closed form Pb(3L² − 4b²)/48EI. The dashed curve is not this calculation at all: it is the DEFLECTED SHAPE of the same beam under one load at mid-span, read at the station the moving load occupies — and it lands on the same curve to 0.15%. That is Maxwell's reciprocal theorem, which neither computation was told about.012345678-120-100-80-60-40-20position of the load along the span (m)deflection at mid-spanmoment-areadouble integrationthe mid-span load'sown deflected shapeall three within 0.15%
Fig. 5 Mid-span deflection of an 8 m simply supported span with a point load moved along it, computed twice: by the two theorems, and by integrating the curvature twice with the constants applied algebraically. The largest disagreement anywhere on the sweep is 6.6 × 10⁻¹³ of the answer, which is the trapezium rule and not the method.

The sweep also contains something nobody put in it. The deflection at mid-span under a load at aa traces a curve that is symmetric about mid-span in value while the underlying beam is not symmetric in any other respect — a load at 1 m and a load at 7 m give the same mid-span deflection to the last figure.

That is Maxwell’s reciprocal theorem arriving without being asked for. The deflection at CC from a load at AA equals the deflection at AA from a load at CC, so the mid-span deflection under a load at aa equals the deflection at aa under a load at mid-span — and that function is symmetric because the beam and the load case are. The reciprocity was not built into either route; it fell out of both.

Maxwell's reciprocal theoremA load at one point and the deflection it causes at another, against the same load moved to the second point and the deflection read at the first. Both integrals return 93.3335, and neither calculation was told about the other. The two deflected shapes are entirely different; the two readings are identical.20 at 2δ at B = 93.33320 at 6δ at A = 93.334the shapes have nothing in commonand the two readings agree to 1e-14which is why an influence line can be measured by pushing the structure where it is easy to push
Fig. 6 The theorem stated on its own terms: a load at one station and the deflection it causes at another, then the two swapped. The two numbers agree, and the moment-area construction is one of the few methods in which the reason is visible — both are the first moment of the same product of two diagrams, and a product does not know which of its factors came first.

The agreement figure is worth one further reading. Its two curves are not two approximations to a third thing; they are two evaluations of the same integral by routes with different rounding behaviour. Where they disagree, at the thirteenth figure, the disagreement is the trapezium rule applied to a diagram with a kink in it under the point load — and it shrinks as the fourth power of the sampling interval, which is a statement about the arithmetic and about nothing structural at all.

What the picture is for

There is a temptation to file this as a hand method superseded by arithmetic, and to keep it for the same reason graphic statics is kept: as history. That undersells it in one specific respect.

The answer arrives in instalmentsThe hogging moment at support 1 of a three-span beam, cycle by cycle. It starts at the fixed-end moment of 53.3 kNm — the value with every joint clamped — and settles at 64.0 kNm against an exact 64.0. The error falls by about a factor of four per cycle: 14.00, 3.50, 1.95, 0.59 kNm after one, two, three and four. Two cycles is an engineering answer and nobody had to invert anything.012345678020406080cycles of distributionmoment at the support (kNm)exact: 64.0all joints clamped
Fig. 7 The other hand method of the same era, iterating rather than integrating: joints are locked, released and relocked until the out-of-balance moments die away. It answers a different question — the moments in a redundant frame — and it needs a deflection method to convert them into movement, which is where this page returns.
One support too manyThe 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.simply supportedstatics alonesag 32.0propped at one endneeds stiffnesssag 18.0hog 32.0built in at both endsneeds stiffnesssag 10.7hog 21.3the load never changes; only what is holding the endsthe built-in case peaks at two-thirds of the simple span's moment
Fig. 8 A propped cantilever, which is indeterminate by one and therefore cannot be solved by statics alone. The extra equation is geometric: the deflection at the prop is zero, and any method that produces a deflection produces the redundant.

The second theorem’s output is a geometric compatibility statement, and compatibility is the missing equation in every indeterminate structure. Setting the deviation of the prop from the tangent at the fixed end to zero gives R=3wL/8R = 3wL/8 in one line of geometry, with no integration, no unit load and no simultaneous equations — and the same construction with a non-zero deviation gives the effect of a support that has settled directly, since a settlement is a prescribed deviation and nothing else.

The deflected shape is the moment, integrated twiceA loaded beam with its deflected shape above and its bending-moment diagram below. The shape was obtained by integrating the moment twice and fitting the constants to the supports; the vertical scale is exaggerated enormously.the largest movement, at x = 4.00momentdrawn at roughly three hundred times the real deflection —a beam at its serviceability limit moves about a three-hundredth of its span
Fig. 9 The shape those numbers describe, at an exaggeration the caption has to state. A real 8 m beam at its serviceability limit has moved by about a three-hundredth of its span, which is thinner than the line drawn here.

Where the two constants went

It is worth being explicit about the accounting, because the whole claim of the method is that it does not lose anything.

The double integral of M/EIM/EI produces two constants. Algebraically they are fixed by two boundary conditions, written as equations and solved. Geometrically they are fixed by two choices: which tangent to measure from, and which point’s deviation to measure. Those are the same two pieces of information wearing different clothes, and the reason the geometric version feels like it has fewer steps is that the tangent is chosen before any arithmetic starts, at a place where the answer is already known.

For a cantilever the tangent is at the root and is horizontal, so one of the two choices is free and the method has one step. For a simply supported span neither end has a known slope, so both choices have to be made and the answer is a difference. The number of steps tracks the number of unknown end slopes exactly, which is a property no algebraic treatment makes visible.

Deflection goes as the fourth power of the spanDeflection against span for a constant load intensity and section, with two slower relationships drawn faintly behind it for comparison: the load itself, which grows in proportion to the span, and the bending moment, which grows as its square. Doubling the span multiplies the deflection by sixteen, while the moment only quadruples.11.522.533.54050100150200250300span, relative to the first16×81×256×moment: the squareload: the first powerdeflection: the fourth
Fig. 10 What the second theorem’s lever arm does to the scaling. The area under M/EI goes as the moment times the length, the first moment adds another length, and the moment itself carries two — so the deflection goes as the fourth power of the span, which is the single most consequential number in this field.

The scaling is legible in the construction rather than in the formula. The diagram’s height goes as wL2wL^2; its width as LL; the lever arm in the first moment as LL again. Four factors of length, arrived at by counting rather than by expanding an integral, and the fourth power is why spans are short.

Where the model stops

The diagram must be of M/EIM/EI, not of MM. Every statement above is about the curvature diagram, and using the moment diagram instead is correct only for a prismatic beam of one material. The step in the figure above is the whole reminder: nothing about the moment changed there.

Curvature is M/EIM/EI only while the material is elastic and the section is uncracked. Past first yield the diagram is not proportional to the moment at all, and the curvature has to come from the section rather than from a division. A cracked reinforced concrete member has an EIEI that varies with the moment it is carrying, so the diagram to be measured depends on the answer.

Small deflections throughout. v=M/EIv'' = M/EI is the linearised curvature; the exact expression divides by (1+v2)3/2(1+v'^2)^{3/2}, and everything on this page is the first term of that. For the deflections a beam is allowed the approximation is superb, and for a member that is buckling it is not.

Shear is absent. The double integral of a moment does not contain the racking of the section, and for a deep member that missing term is most of the answer. Moment-area inherits the omission exactly, because it is the same integral.

Sign conventions bite harder here than anywhere. An area is positive or negative according to the sagging convention, a first moment takes its sign from both the area and the lever arm, and a construction that subtracts two of them has four opportunities to be wrong. The generator behind these figures integrates the sampled diagram directly and prints the plain double integral beside the geometric result, so a sign slip has somewhere to show.

What the pictures cannot show

The shaded areas are drawn to a scale chosen so that the diagram fills its panel, and the number printed beside them is in the units of M/EIM/EI — which for EI=1EI = 1 are the moment’s units and for any real beam are not. No area on this page has an area’s dimensions. The first theorem’s output is a rotation, in radians; the second theorem’s is a length. A reader who measures the shaded region with a ruler learns nothing.

The centroid mark is the second distortion. It is drawn as a point on the diagram, which suggests it is a station along the beam where something happens. Nothing happens there: it is a property of a shaded region, and moving the load moves it without any physical event occurring at the old position or the new one.

And the tangent construction, which is the whole method for a simply supported span, appears in none of these drawings — because a tangent to a curve exaggerated ten thousand times is a line whose slope is exaggerated ten thousand times, and drawing it would put it off the page.

The ladder from here

Later rungs on this anchor: the conjugate beam, which turns both theorems into a single fictitious beam whose shear is the real beam’s slope and whose moment is its deflection, and the strange support conditions that fiction requires. Moment-area applied to frames, where the tangent has to be transported round a corner. The method on a beam of continuously varying depth, where the area is an integral again and the geometry buys only the constants. Elastic weights and the column analogy, which is the same idea pushed until it solves indeterminate frames. And the reason Otto Mohr found this at all: he was working on the graphical solution of trusses, where a displacement diagram is a drawing, and the beam theorems are that habit applied to a continuum.

Mohr published in 1868 and Charles Greene arrived at the same construction independently in the 1870s; both were teaching, and both wanted a method a class could carry out on a drawing board. That origin explains the shape of it. It is not an approximation made for speed — it is exact arithmetic reorganised so that the difficult parts are ones a draughtsman is already good at.

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.

CentroidDeflectionFirst moment of areaFlexural rigidityGraphic staticsIntegrationMoment diagramPoint of contraflexureStiffnessSuperpositionVirtual work