Internal forces

The length a structure was never given

A disturbance applied at one place dies out over a distance, and the distance is not something anybody chose. A beam forgets a badly applied load over its own depth. A beam on the ground forgets a point load over the fourth root of its stiffness against the soil's. A shell forgets a held edge over the square root of the radius times the thickness — a geometric mean of two lengths three orders of magnitude apart, which is neither of them and is not near either.

Assumes How far a wrong load reaches, The force that is only a radius and The surface that carries by being curved.

Structures have lengths in them that nobody put there. A beam has a span because somebody drew one, and a depth because somebody chose it; it also has a decay length, which is the distance over which it forgets a disturbance applied at one point, and that is not a design decision at all. It falls out of the differential equation the structure obeys, and the only way to find it is to solve the equation and read it off.

This essay is about three of them, because they are three different arithmetics and the third is the strange one.

The edge, and the length over which it is forgotten. A cylinder of radius 4.00 m and wall 12 mm under 0.6 N/mm² of internal pressure, held at its base. Away from the base the wall carries the pressure as pure hoop tension and bends nowhere, which is why a pressure vessel is a cylinder. At the base the hoop force is zero, because the wall cannot grow there, and the difference is made up by a boundary layer of bending that dies out inward. The length it dies out over is 1/β = 170 mm — 0.778√(Rt), a geometric mean of the radius and the thickness — and the moment is under a twentieth of its edge value by 3.07 of them. Nothing in that length is the load. The base moment is p/2β², and the bending stress it produces is 1.82 times the membrane hoop stress the whole design is about, at every pressure, every radius and every thickness: the ratio is √3/√(1 − ν²) and contains none of them. The hoop force overshoots by 4.3% at 3.2 lengths in, which is the wall springing back past where it was going.
Fig. 1 A cylinder under internal pressure, held at its base. Away from the base it carries the pressure as pure hoop tension and bends nowhere. At the base the hoop force is zero, and the difference is made up by a boundary layer of bending that dies out inward over one characteristic length.

Which free body produced the number

A vertical strip of the shell wall, one unit wide, running up from the base.

That strip bends like a beam — it has a flexural rigidity D=Et3/12(1ν2)D = Et^3/12(1-\nu^2) per unit width, exactly as a plate does. What resists its outward movement is not a foundation underneath it but the hoop rings it crosses: push the strip out by ww and every ring it passes through is stretched by w/Rw/R, which puts a hoop force Etw/REtw/R into each of them, which pushes back on the strip with Etw/R2Etw/R^2 per unit length. That is a Winkler foundation with a spring constant k=Et/R2k = Et/R^2, and it was supplied by the shell’s own geometry rather than by anything under it.

So a shell wall is a beam on an elastic foundation made of itself, and everything about it follows from the one parameter that problem has:

β=[k4D]1/4=[3(1ν2)R2t2]1/4\beta = \left[\frac{k}{4D}\right]^{1/4} = \left[\frac{3(1-\nu^2)}{R^2t^2}\right]^{1/4}

and its reciprocal is the length everything else is measured in:

1β=Rt[3(1ν2)]1/4=0.78Rt\frac{1}{\beta} = \frac{\sqrt{Rt}}{[3(1-\nu^2)]^{1/4}} = 0.78\sqrt{Rt}

at ν=0.3\nu = 0.3. The beam that sits on the ground is the same equation with the springs supplied by soil; here they are supplied by the shell, and the fourth root of a stiffness ratio has collapsed into the square root of a product of two lengths.

Everything a beam on the ground does is a function of βx. Deflection, moment and shear along a beam on an elastic foundation, each divided by its own value immediately under the load and drawn against βx. Contact pressure is k times deflection, so it is the same curve as the first. The stations are exact and none of them depends on the load or on the beam: the moment crosses zero at βx = π/4, which is 843.97 m here; hogging peaks at βx = π/2 at 20.8% of the sagging moment; the deflection crosses zero at 3π/4, or 2531.90 m, past which the beam lifts; and by βx = π the uplift is 4.32% of the settlement. One characteristic length along, the deflection is already down to 51% of its peak, and by three it is 4.2%. That is what it means for a raft to stop being a beam: past two or three of these lengths, nothing knows the load happened.
Fig. 2 The same equation with the springs supplied by soil rather than by hoops. Deflection, moment and shear all die out as e^(−βx) times a trigonometric function, and everything about the answer is a function of βx alone — which is what a characteristic length means.

Two boundary conditions, and the whole of the answer

The membrane solution has the wall growing outward by δ=pR2/Et\delta = pR^2/Et at every height. A base slab says it does not grow here. That is all the information there is, and it is enough.

The decaying solution of the fourth-order equation is w=eβx(C1cosβx+C2sinβx)w = e^{-\beta x}(C_1\cos\beta x + C_2\sin\beta x). A clamped base needs w(0)=δw(0) = -\delta and w(0)=0w'(0) = 0, which gives C1=C2=δC_1 = C_2 = -\delta immediately, and everything after that is differentiation. Two of the results are worth having in front of the reader.

The base moment is M0=p/2β2M_0 = p/2\beta^2. Written out, that is pRt/23(1ν2)pRt/2\sqrt{3(1-\nu^2)} — a moment per unit width that grows with the radius and with the thickness, which is not what most people guess.

The bending stress it produces is 1.82 times the membrane hoop stress. Divide 6M0/t26M_0/t^2 by pR/tpR/t and everything cancels:

σbendingσhoop=31ν2=1.816\frac{\sigma_{bending}}{\sigma_{hoop}} = \frac{\sqrt{3}}{\sqrt{1-\nu^2}} = 1.816

There is no pressure in it, no radius, no thickness. A membrane structure carries eighty per cent more stress in bending at the one line where it is held than the membrane stress the entire design is about, and it does so at every size, every pressure and every wall thickness. That is the number to remember, and it is why a shell’s edges are the whole of its detailing.

The reinforcement a tank wants most is not at the bottom. Hoop force up the wall of a 18 m tank holding 8 m of liquid, with the wall cast into its base slab. The dashed line is the membrane answer — γ(H − x)R, a triangle with its peak at the base — and it is what every hand calculation starts from. The solid line is what the wall actually carries. At the base the hoop force is zero, because a wall held there cannot move outwards and there is no hoop strain to go with a hoop force; the pressure is carried in vertical bending instead, at a fixing moment of 52.6 kNm/m. The membrane solution is recovered about 3.96 m up, and in between the two exchange the load. The peak is 454 kN/m at 35% of the height — 64% of the triangle's peak, and a third of the way up the wall.
Fig. 3 The consequence for a real wall: the hoop force is zero at the base, because the base slab says so, and reaches its peak about a third of the way up. The membrane triangle — the answer with no edge in it — peaks at the bottom, where the real wall carries none.

Three decay lengths, three arithmetics

The reason to put these side by side is that the rule for finding a decay length is the same in all three and the answers have nothing in common.

Saint-Venant’s is the member’s own depth. How far a wrong load reaches works it out: a self-equilibrating load applied at an end, decomposed into components of wavelength λ\lambda, dies out as e2πx/λe^{-2\pi x/\lambda}, and the longest wavelength available is the depth. So a 400 mm beam has forgotten how its end load was applied within about 400 mm, and there is one length in the problem.

A beam on the ground has a fourth root. =(4EI/k)1/4\ell = (4EI/k)^{1/4} is a ratio of two stiffnesses that belong to different objects, raised to a small power — which is why a raft’s characteristic length is stubbornly a few metres for almost any combination of raft and soil, and why a stiffer raft is so poor a way of spreading a load.

A shell has a geometric mean. Rt\sqrt{Rt} takes a radius of, say, 4,000 mm and a thickness of 12 and returns 219 — a number that is not near either of them, and that sits at the logarithmic midpoint of two quantities differing by a factor of 333. That is the property that makes shell edge effects so easy to misjudge: the intuition wants the answer to scale with the big number or with the small one, and it does neither.

The decay length is the load's own wavelength, and nothing else. The stress left from a self-equilibrating end load that varies as a cosine of wavelength λ, against distance in depths. The Airy function (A + Bx)e^(−αx)cos(αy) satisfies both boundary conditions and gives a factor of (1 + αx)e^(−αx) with α = 2π/λ, so the curves are the same curve stretched: at one wavelength in there is 1.4 per cent left, whatever λ was. No modulus, no Poisson's ratio and no thickness appears anywhere. A self-equilibrating load across a depth must change sign at least twice, so its slowest component has a wavelength of about the depth — which is the whole of Saint-Venant's principle, with a number in it.
Fig. 4 Saint-Venant’s version. The stress left from a self-equilibrating end load, against distance in depths — one length in the problem, and it is the depth.

The consequence is a table with a very small spread in it. A water tank wall 8 m in radius and 250 mm thick has a characteristic length of 1.09 m; a steel silo at 4 m and 8 mm has 139 mm; a pipeline at 600 mm and 12 has 66; a concrete chimney at 3 m and 200 mm has 595. Four orders of magnitude of structure, and every one of them forgets its edge in a length within a factor of twenty of the others — and every one of those lengths is 0.77 to 0.78 times the square root of the product.

What the boundary layer does on the way out

The layer is not a simple decay. Two features of it are worth knowing because both have consequences on a drawing.

The moment changes sign at βx=π/4\beta x = \pi/4. A quarter of a characteristic length in, the wall stops hogging and starts sagging, so the reinforcement that the base moment demands on the outside face is unnecessary a few hundred millimetres up, and a different face wants a smaller amount of it a few hundred millimetres further on. A tank wall detailed with one arrangement of bars top to bottom is over-reinforced on one face and under-reinforced on the other for most of its height.

The hoop force overshoots. The wall springs back past where it was going: at about π\pi characteristic lengths in, the radial displacement exceeds the free membrane value by eπ=4.3%e^{-\pi} = 4.3\%, and the hoop force with it. It is a small number and it is exactly eπe^{-\pi} — a constant with no shell in it at all, like the 1.82.

Beyond about three characteristic lengths the moment is under a twentieth of its edge value, and the membrane solution is recovered. That is the honest statement of what “local” means here: three lengths, where the length is the geometric mean, which for the silo above is 42 cm and for the chimney is 1.8 m.

The edge, and the length over which it is forgotten. A cylinder of radius 4.00 m and wall 24 mm under 0.6 N/mm² of internal pressure, held at its base. Away from the base the wall carries the pressure as pure hoop tension and bends nowhere, which is why a pressure vessel is a cylinder. At the base the hoop force is zero, because the wall cannot grow there, and the difference is made up by a boundary layer of bending that dies out inward. The length it dies out over is 1/β = 241 mm — 0.778√(Rt), a geometric mean of the radius and the thickness — and the moment is under a twentieth of its edge value by 3.07 of them. Nothing in that length is the load. The base moment is p/2β², and the bending stress it produces is 1.82 times the membrane hoop stress the whole design is about, at every pressure, every radius and every thickness: the ratio is √3/√(1 − ν²) and contains none of them. The hoop force overshoots by 4.3% at 3.2 lengths in, which is the wall springing back past where it was going.
Fig. 5 The same shell with the wall doubled. The stress ratio is identical to the last digit — it contains no thickness — and the reach has grown by exactly the square root of two, because it contains the thickness once under a square root.

Where the edges are, which is more places than the drawing shows

An edge, for this purpose, is any line at which the membrane solution is contradicted. That includes several things that are not drawn as edges.

A base slab, which says the radius does not change here. A roof or a head, which says the same thing at the top and which is why a flat-ended pressure vessel is a much worse vessel than a domed-ended one. A change of thickness, which is an edge in the middle of the wall: the two halves want to grow by different amounts, and the discontinuity is the same problem with a smaller mismatch. A ring stiffener, which is an edge somebody put in on purpose and which produces a local moment for the same reason a base slab does. And a junction of two shells of different radius, where each side’s membrane solution demands a different displacement and neither can have it.

The dome’s springing is the case where the ring is doing it, and it is the one place in this collection where an edge disturbance is unavoidable rather than a detailing decision. The ring at the base of a dome is in tension, so it stretches; the shell’s own hoop force at that latitude is also tension, but of a different magnitude, so the shell wants to stretch by a different amount. The two are connected, so there is a mismatch, and the mismatch produces bending over 0.78Rt0.78\sqrt{Rt} of the meridian.

The latitude where a dome changes its mind. The two membrane forces in a spherical dome of radius 21.5 m carrying 3 kN/m² over its own surface, against latitude from the crown. The meridional force is compression everywhere and grows toward the base. The hoop force starts as compression, passes through zero at 51.83° and is tension below that. The latitude is the root of cos φ + cos²φ = 1, which is cos φ = 0.6180 — the golden ratio, in a problem about masonry with nothing to do with proportion. It does not move: sweeping the radius over an order of magnitude shifts it by 0e+0 of a degree, because neither the radius nor the load nor the thickness appears in the equation that fixes it. That is where a masonry dome cracks — on meridians, from the springing up to about 52° — and it is why the repair has been the same for three hundred years. The ring at the base takes 400 kN of tension here, which is the only tension member in the structure.
Fig. 6 Why the ring has to be there, and where it goes. The hoop force changes sign at 51.83° — the root of cos φ + cos²φ = 1, which is the golden ratio and does not move with the radius, the thickness or the load. Below it the shell is in tension and a masonry dome cracks; the ring is what closes the thrust, and the ring is an edge.

The junction, where two membrane solutions meet

The severest case is not an edge against a foundation. It is an edge against another shell, because then both sides have an opinion about how much the radius should change and neither of them is zero.

A cylindrical tank with a conical bottom is the standard example. The cylinder under liquid pressure wants to grow by pR2/EtpR^2/Et; the cone under the same pressure wants to grow by a different amount, because its own radius is different at the junction and its meridian runs at an angle. The two are welded together, so the growths must match, and the difference is absorbed by a pair of boundary layers — one running up the cylinder over 0.78Rt0.78\sqrt{R t} and one running down the cone over its own version of the same length.

Two things follow, and both are practical.

The moment is shared in proportion to stiffness. Each side of the junction resists rotation with a stiffness of order 2eta D, so the thicker or tighter-radius side takes more of the discontinuity — which is the stiffest path takes the load at a weld line. Thickening one side of a junction to “strengthen” it drags moment into it, and the moment grows faster than the section does.

The horizontal thrust has to go somewhere. The meridional force in the cone has a radial component at the junction that the cylinder does not, and the difference is a ring load. Somebody has to carry it, and the answer is a ring — which is the same conclusion the force that is only a radius reaches for a dome and for exactly the same reason. Vessels are full of small stiffening rings at changes of shape, and every one of them is there because two membrane solutions disagreed.

The failure this prevents is a specific one and it is not collapse. A boundary layer is a local bending, so it does not reduce the structure’s capacity to carry the pressure at all — the membrane action further along is untouched. What it does is crack the concrete, leak the tank, or start a fatigue crack at the weld toe, which is the detail decides and the steel does not applied to a shell. A shell that fails at an edge nearly always fails by serviceability or by fatigue, and hardly ever by strength.

The design that removes the layer instead of reinforcing it

There is a third response, beside computing the moment and reinforcing for it, and on a large tank it is the usual one: let the edge move.

Cast the wall on a sliding joint — a bearing strip, a membrane, a rubber pad — and the base no longer says the radius may not change. The membrane solution is then correct all the way down, the hoop force is a triangle with its peak at the bottom exactly as the textbook figure shows, and there is no boundary layer to reinforce. The price is that something else has to carry the base shear, and that the joint has to be watertight while sliding, which is a detailing problem rather than a structural one.

That is a general move worth naming. A restraint produces a force proportional to the stiffness of whatever is doing the restraining, so the cheapest way to reduce a restraint force is to remove the restraint, not to strengthen the member carrying it — the movement nobody applied is the same trade for a thermal one, and where the structure is allowed to move is it made into a scheme. A shell’s edge is a restraint like any other, and the design question is always which of the two answers is being bought.

Where the model stops

The shell was long. The solution used only the decaying part of the general solution, which is legitimate when the far edge is several characteristic lengths away. A short cylinder — a ring, a stiffener spacing, a segment between two changes of thickness — has both edges inside each other’s boundary layer, and the two disturbances interact. That is not a small correction: at a spacing of one characteristic length the moments roughly double.

The material was elastic and the geometry linear. A concrete tank wall cracks in the boundary layer before it cracks anywhere else, and cracking softens it, which raises β\beta and shortens the reach. The layer moves as the structure damages, which is one of the few places in this collection where the characteristic length is not a constant.

The edge was perfectly clamped. Nothing is. A base slab has its own flexibility, and a partially restrained edge produces a moment somewhere between the clamped value and zero — which is why the honest calculation is a compatibility one between two flexibilities, a joint made of springs in series applied to a shell.

And the pressure was uniform. A tank holding liquid has a pressure that varies up the wall, so the membrane displacement varies with it and the “mismatch” at the base is against a triangle rather than a rectangle. The arithmetic changes; β\beta does not, because β\beta was never told what the load is.

The generalisation

The idea to carry away is that a structure’s own equations hand it lengths, and those lengths decide what “local” means.

It is a habit worth applying wherever a designer is about to say that something is a local effect and can be ignored away from where it happens. The right question is not whether the effect is local but what its length is, and the length is available: it is whatever appears in the exponent when the governing equation is solved. A beam’s is its depth, a beam on springs has a fourth root of a stiffness ratio, a shell has a geometric mean of radius and thickness, a plate on a grid of supports has the support spacing, and a bar being developed into concrete has a length set by the bond strength and the bar’s own area.

The second idea is narrower and sharper: when a number comes out with none of the problem’s variables in it, it is worth stopping at. The 1.82 has no pressure, radius or thickness in it. The eπe^{-\pi} overshoot has nothing in it at all. The 2+π2+\pi in the ground is a mechanism, the 51.83° in a dome, the 1.5 shear factor of a rectangle — each is a place where the geometry has answered a question the loading was not consulted about, and each is therefore a number that will still be right when everything around it has changed.

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 momentBoundary layerCharacteristic lengthCompatibilityDecay lengthDomeEdge disturbanceElastic foundationGeometric meanHoop tensionMembrane actionRestraintSaint-Venant's principleShellStress concentration