Internal forces

The stiffest path takes the load

When two members share a force the split can be argued about. When they share a displacement it cannot — stiffness settles it, and nothing about the load or the plan drawing gets a vote. The consequence is that stiffening a lightly loaded member raises its stress, and the way to unload something is to soften it.

Assumes One support too many, and what it costs to know, The load a beam is given is a decision and The material far from the middle does nearly all the work.

Two steel beams of the same span lie side by side, one twice as deep as the other, and a bolt through both of them at midspan ties them together. A hundred kilonewtons is hung off the bolt. The question is how much of it each beam carries, and there is a strong temptation to answer it by looking at the picture.

The picture has nothing to say. The load is at one point, on one bolt, and the bolt is on both beams. No area can be allocated, no half can be taken, no line can be drawn on the plan that divides anything. What settles it is a condition that has not yet been written down anywhere in this collection as an equation in its own right: the two beams are bolted together, so they move the same distance.

Two beams tied together, and the deeper one takes 89% of the loadTwo simply supported beams of 6 m, one twice as deep as the other, tied together at midspan so that they have to move as one. A load of 100 kN stands on the tie. Point stiffness is 48EI/L³, so the deeper beam is 8 times as stiff — depth cubed, nothing else — and the load divides in that ratio: 11.1 kN into the shallow beam and 88.9 kN into the deep one, 11% against 89%. Both midspan points move 5.00 mm, which is the whole of the argument: the geometry of the load never entered it. The deflection is drawn 78 times full size — the real sag is 5.00 mm on a 6 m span, about 1 in 1200.P = 100 kNthe shallow beam takes 11.1 kN11% of it — one part of the stiffness in 9the deep beam takes 88.9 kN89% of it — 8 times the stiffness of its neighbourone load, two beams, one deflection: 5.0 mm each
Fig. 1 Two 6 m simply supported beams tied at midspan, one twice as deep as the other, under 100 kN. Point stiffness is 48EI/L³, so the deep beam is 8 times as stiff and the load divides in that ratio: 11.1 kN and 88.9 kN, 11% against 89%. Both midspan points move 5.00 mm. The deflection is drawn 78 times full size — the real sag is 5.00 mm on 6 m, about 1 in 1200.

Eleven point one against eighty-eight point nine, from two beams that differ in one dimension by a factor of two. That ratio is the whole subject, and everything below is a consequence of it.

Sharing a force is a decision; sharing a displacement is not

Most divisions of load in this collection are decisions. The load a beam is given comes from a tributary rule that somebody chose, and two defensible choices differ by sixty per cent on the same floor. Both are legitimate because equilibrium objects to neither: any division that hands over the whole load and puts it in the right place satisfies statics, so statics declines to arbitrate.

Sharing a displacement is a different category of thing. The moment two members are attached at a point, that point has one position, and whatever each member does it does to the same distance. That is not a modelling choice and not a rule of thumb — it is a geometrical fact about a structure that has not come apart, and it supplies exactly the equation statics is short of.

P=R1+R2(equilibrium: one equation, two unknowns)P = R_1 + R_2 \qquad\text{(equilibrium: one equation, two unknowns)}

δ1=δ2(compatibility: the missing one)\delta_1 = \delta_2 \qquad\text{(compatibility: the missing one)}

With δ=R/k\delta = R/k for each member, the second line becomes R1/k1=R2/k2R_1/k_1 = R_2/k_2, and the two together give

Ri=Pkik.R_i = P\,\frac{k_i}{\sum k}.

That is the whole of load sharing. It is the same shortage of equations that makes a propped cantilever indeterminate, met in its smallest possible form: two members, one point, one degree of redundancy. And the resolution is the same one — a statement about movement, imported into a problem that thought it was about force.

Which free body produced the split

The free body is the bolt. Cut it out of the structure and draw it alone: the applied 100 kN pushes it down, and the two beams push it up with R1R_1 and R2R_2. Vertical equilibrium of that one small body gives R1+R2=100R_1 + R_2 = 100 and nothing else — no moment equation is available, because everything acts through the same point, and no other cut anywhere in the structure produces a second independent equation.

The second equation comes from a different cut. Take each beam on its own, with RiR_i applied upward at midspan, and integrate its curvature twice. The standard result is δ=RL3/48EI\delta = RL^3/48EI, so the point stiffness of a simply supported beam loaded at its centre is

k=48EIL3.k = \frac{48EI}{L^3}.

For the pair drawn above, LL is the same and EE is the same, so the stiffness ratio is the ratio of the second moments — and second moment goes as depth cubed. Twice the depth is eight times the stiffness, and eight times the stiffness is eight times the force: 100×8/9=88.9100 \times 8/9 = 88.9 kN into the deep beam, 100×1/9=11.1100 \times 1/9 = 11.1 kN into the shallow one.

Cutting each beam again at midspan gives the moments that follow, RL/4RL/4: 133.3 kNm in the deep beam and 16.7 kNm in the shallow one. And both midspan points have moved 5.00 mm, which is the check — two independently computed deflections that had to agree, and do.

Nothing about the load entered any of that. The same pair under 40 kN divides it 4.4 and 35.6; under a moving axle it divides every position the same way. The split is a property of the structure, not of the loading.

The case where the drawing has nothing to divide

A pair of beams bolted together is a slightly artificial arrangement. Two beams crossing each other, with a column landing where they cross, is a floor plan, and it is the case where the tributary habit fails hardest.

One load, two beams, and no tributary area to divide it withA plan of a 6 m beam crossing a 9 m beam, with 100 kN standing exactly where they cross. There is no area to allocate, so a tributary drawing can only say half each. Compatibility says otherwise: the point flexibility of a simply supported beam under a central load is L³/48EI, so the 6 m beam is 3.37 times as stiff as the 9 m one and takes 77.1 kN against 22.9 kN — 77.1% against 22.9%, which is 9³/(6³ + 9³) exactly. Both beams settle 34.7 mm at the crossing, agreeing to 2e-16, and the moments that follow are 115.7 kNm and 51.4 kNm. The tributary answer is wrong by 54% on the beam that matters.100 kN, on both beams at once6 m9 mstiffness decides: 77% to the 6 m beam77.1%a tributary area says: 50% each50.0%9³ ÷ (6³ + 9³) = 77.1% — the cube of the span, and nothing elseboth beams deflect 34.7 mm at the crossing, to 2e-16
Fig. 2 A 6 m beam crossing a 9 m beam in plan, with 100 kN standing exactly where they cross. There is no area to allocate. Compatibility of the two deflections gives 77.1 kN to the short beam against 22.9 kN to the long one — 9³/(6³ + 9³) exactly — with both beams settling 34.7 mm and agreeing to 2e-16. The tributary answer of half each is wrong by 54%.

The short beam takes three quarters of a load that a plan drawing splits down the middle. The arithmetic is one line: both beams have the same EIEI, so their point flexibilities are L3/48EIL^3/48EI and the stiffnesses go as 1/L31/L^3, giving

share of the 6 m beam=1/631/63+1/93=9363+93=729945=77.1%.\text{share of the 6 m beam} = \frac{1/6^3}{1/6^3 + 1/9^3} = \frac{9^3}{6^3 + 9^3} = \frac{729}{945} = 77.1\%.

The cube is the entire content of that result. A three-metre difference in span moves three quarters of the load onto one member, and it does so with both beams made of the same steel in the same section. Geometry beats material outright here: changing EE changes nothing at all, because it appears identically in both flexibilities and cancels.

Set beside it what the tributary method would say about the same floor.

Where a beam's load comes fromA 8 × 6 m panel carrying 5 kN/m², divided at 45° from the corners. The long beams take a trapezoid of 15.0 m² each and the short beams a triangle of 9.0 m²; the four areas sum to 48.0 m², which is the panel, so no load has been invented or lost. The line loads quoted are the uniform equivalents; the real distributions peak at 15.00 kN/m at midspan.15.0 m²9.38 kN/m15.0 m²9.38 kN/m9.0 m²7.50 kN/m9.0 m²7.50 kN/m8 m6 m48.0 m² divided, 48.0 m² of panel — the division closes
Fig. 3 The tributary division of an 8 × 6 m panel at 5 kN/m², drawn at 45° from the corners. The long beams take 15.0 m² each and the short beams 9.0 m², the four regions summing to 48.0 m², which is the panel — so nothing has been invented or lost. The division closes exactly and is still a decision about where a slab hands over its load.

That division is honest, closes to the last square metre, and answers a question the crossing-beam case does not pose. The tributary rule works by area, and a point load standing on two members at once has none. Where there is an area the rule is a defensible approximation; where there is not it degenerates into “half each”, the one answer compatibility never gives unless the members are identical.

Pushing the spans further apart makes the plan drawing’s failure absurd.

One load, two beams, and no tributary area to divide it withA plan of a 5 m beam crossing a 12 m beam, with 60 kN standing exactly where they cross. There is no area to allocate, so a tributary drawing can only say half each. Compatibility says otherwise: the point flexibility of a simply supported beam under a central load is L³/48EI, so the 5 m beam is 13.82 times as stiff as the 12 m one and takes 56.0 kN against 4.0 kN — 93.3% against 6.7%, which is 12³/(5³ + 12³) exactly. Both beams settle 14.6 mm at the crossing, agreeing to 2e-15, and the moments that follow are 69.9 kNm and 12.1 kNm. The tributary answer is wrong by 87% on the beam that matters.60 kN, on both beams at once5 m12 mstiffness decides: 93% to the 5 m beam93.3%a tributary area says: 50% each50.0%12³ ÷ (5³ + 12³) = 93.3% — the cube of the span, and nothing elseboth beams deflect 14.6 mm at the crossing, to 2e-15
Fig. 4 The same arrangement with a 5 m beam crossing a 12 m one under 60 kN. The short beam is 13.82 times as stiff and takes 56.0 kN against 4.0 kN — 93.3% against 6.7%, which is 12³/(5³ + 12³). Both beams settle 14.6 mm at the crossing. The tributary answer is wrong by 87%, and the 12 m beam it would have loaded to 30 kN is carrying four.

A designer who sized the long beam for half the load has bought a member that is doing almost nothing, and has under-sized the short one by a factor of nearly two. Both errors come from the same source: a picture that shows where things are and says nothing about how stiff they are.

The whole curve, and the bound it never reaches

One member’s share is r/(1+r)r/(1+r), where rr is its stiffness measured in units of everything it shares with. That function is worth drawing in full, because it has a property that is easy to state and easy to forget.

The share follows the stiffness, and always falls a little short of itThe share of a shared load taken by one member, against its stiffness measured in units of everything it shares with. The curve is r/(1 + r) and the dashed line is r itself, the share a member would take if it were paid in proportion to what it brought: the two meet only in the limit, because a member's own stiffness is part of the total it is being divided by. Three cases are marked. An equal pair splits 50% each. A 6 m beam crossing a 9 m beam is at a ratio of 3.37 and takes 77.1% — a point computed by a different solver, from compatibility of two deflections, and it lands on this curve. A beam twice as deep as its neighbour is at 8 and takes 89%. Softening is the only way down: to halve the shallow member's force its stiffness has to fall to 0.47 of what it was, not to a half.0.111000.20.40.60.81one member's stiffness ÷ the stiffness of everything it shares withthe share of the load it takesthe 6 m beam crossing the 9 m onetwice the depth: 89%an equal pair: half eachproportional to stiffness — the bound
Fig. 5 Share against stiffness ratio over three decades, with the proportional line beside it. The curve is r/(1 + r) and the dashed line is r itself. Three cases are marked: an equal pair at 50%, the 6 m beam crossing the 9 m one at a ratio of 3.37 taking 77.1%, and a beam of twice the depth at a ratio of 8 taking 89%. The crossing point was computed by a different solver, from compatibility of two deflections, and lands on this curve.

The share always falls short of the stiffness ratio, because a member’s own stiffness is part of the total it is being divided by. Doubling a member’s stiffness never doubles its force; it cannot, since half of what it competes against is itself.

Run backwards, that is the useful half. To halve the force in the shallow beam of the hero figure, its stiffness has to fall not to a half but to 0.47 of what it was — and for two equal members the number is a third. Softening sheds load onto the neighbour, the neighbour deflects more, and some of the shed load comes straight back. Every intervention in a shared-displacement system is partly undone by the system’s response to it.

Load sharing does not need two separate members. A slab spanning both ways is the same argument with the members drawn as strips of a continuum.

A two-way slab is a one-way slab as soon as it is not squareThe share of the load carried by the strips spanning the short way, against the ratio of the sides. The two families of strips cross at the centre and must deflect equally there, and a strip's deflection goes as the fourth power of its span — so at a ratio of 1.33 the short strips already take 76% and at 2 they take 94%. The panel drawn here is 6 × 8 m, a ratio of 1.33, and its short strips take 76.0%. Two-way action is worth having at a ratio of one and worth almost nothing by two.11.522.530.40.50.60.70.80.91long span ÷ short spanshare taken by the short strips6 × 8 m: 76.0%by 2 : 1 it is a one-way slab
Fig. 6 The share taken by the strips spanning the short way of a rectangular panel, against the side ratio. The two families of strips cross at the centre and must deflect equally there, so the split follows the fourth power of the span rather than the third — at a ratio of 1.33 the short strips already take 76%, and by 2 they take 94%.

The exponent is four rather than three because a strip carries a distributed load rather than a point one, and 5wL4/384EI5wL^4/384EI replaces PL3/48EIPL^3/48EI. Everything else is identical, including the conclusion: two-way action is worth having at a ratio of one and worth almost nothing by two. No amount of reinforcement in the long direction changes it, because the long strips are not declining the load — they are outvoted by a stiffness they cannot alter without becoming deeper.

The same argument with the load taken away

Compatibility does not need a load to enforce. Impose a movement on the tie instead of a force and every member develops whatever force that movement demands of it.

Two beams tied together, and the deeper one takes 89% of the loadTwo simply supported beams of 6 m, one twice as deep as the other, tied together at midspan so that they have to move as one. A movement of 20.0 mm is imposed on the tie. Point stiffness is 48EI/L³, so the deeper beam is 8 times as stiff — depth cubed, nothing else — and the load divides in that ratio: 44.4 kN into the shallow beam and 355.6 kN into the deep one, 11% against 89%. Both midspan points move 20.00 mm, which is the whole of the argument: the geometry of the load never entered it. The deflection is drawn 19 times full size — the real sag is 20.00 mm on a 6 m span, about 1 in 300.20.0 mm imposedthe shallow beam takes 44.4 kN11% of it — one part of the stiffness in 9the deep beam takes 355.6 kN89% of it — 8 times the stiffness of its neighbourone imposed movement of 20.0 mm, and the force each beam needs to make it
Fig. 7 The same pair with 20.0 mm imposed at the tie rather than a load applied. Each beam supplies the force its own stiffness demands at that displacement: 44.4 kN from the shallow beam and 355.6 kN from the deep one, 400 kN in total. The proportions are unchanged at 11% and 89%, and the total is now an output rather than an input. Drawn 19 times full size — the real movement is 20.00 mm on 6 m, about 1 in 300.

The change is small on the page and large in what it means. Under an applied force the total is fixed and the members argue over it. Under an imposed movement the total is whatever the structure happens to add up to, and making a member stiffer increases the total rather than redistributing it. That is the regime of a support that has settled, of a temperature change nobody applied, and of jacking, shrinkage and construction misfit — every case where the input is a distance.

It is also where the bound of the previous section is reached exactly. Doubling the shallow beam’s second moment under an applied force raised its force by 1.80; under an imposed movement it raises it by exactly 2, because R=kδR = k\delta and δ\delta is not free to change.

Stiffening the member that is not working

Here is the finding, and it inverts the reflex that produced the question in the first place.

Stiffening the lightly loaded member is the one case where it cannot workWhat multiplying one member's second moment of area by 2 does to it, against the share of the load it carried before. Its force rises by 2/(1 + s(2 − 1)), which is largest for the member carrying least: at a share of 11% the force goes up 80%. Its capacity rises by only 1.587, because depth enters stiffness as the cube and section modulus as the square, and that number does not depend on the share at all. The stress is the ratio of the two, and it crosses one at a share of 0.260: every member below that line is more highly stressed for having been stiffened. The pair drawn elsewhere in this family sits at 11%, so doubling the shallow beam's stiffness takes its force up 80%, its capacity up 59% and its stress up 13%. Softening it would have worked; stiffening it made it worse.00.20.40.60.8100.511.52the share of the load this member carried beforemultiplier after its I is multiplied by 2at 11%: stress ×1.13break-even at a share of 0.260its force, ×1.80 hereits capacity, ×1.59 everywhereits stress, ×1.13 here
Fig. 8 What doubling one member’s second moment of area does to it, against the share it carried before. Its force rises by 2/(1 + s), largest for the member carrying least — 80% at a share of 11%. Its capacity rises by only 1.587, the same at every share, because depth enters stiffness as the cube and section modulus as the square. The ratio crosses one at a share of 0.260: below that line, stiffening leaves the member more highly stressed than it was.

The two curves come from the same dimension. Multiplying II by ff means multiplying depth by f1/3f^{1/3} and section modulus by f2/3f^{2/3}, so

force afterforce before=f(k+K)fk+K,capacity aftercapacity before=f2/3,\frac{\text{force after}}{\text{force before}} = \frac{f(k+K)}{fk+K}, \qquad \frac{\text{capacity after}}{\text{capacity before}} = f^{2/3},

and the stress multiplier is the first divided by the second. Setting the two equal and solving for the share s=k/(k+K)s = k/(k+K) gives the break-even line:

s=f1/31f1.s^{*} = \frac{f^{1/3}-1}{f-1}.

For a doubling that is 0.260. For a quadrupling it is 0.196. And in the limit of an infinitesimal stiffening it is exactly one third — so any member carrying less than a third of a shared load is made worse by the first millimetre of extra depth. The number has no material in it, no span in it and no load in it. It is the cube root of two, minus one, and it decides whether a perfectly sensible-looking repair helps or hurts.

The shallow beam of the hero figure sits at 11%, well below the line. Doubling its second moment takes its force up 80%, its capacity up 59%, and its stress up 13%. It has been made deeper, heavier and more expensive, and it is worse off than before.

Stiffening the lightly loaded member is the one case where it cannot workWhat multiplying one member's second moment of area by 4 does to it, against the share of the load it carried before. Its force rises by 4/(1 + s(4 − 1)), which is largest for the member carrying least: at a share of 11% the force goes up 200%. Its capacity rises by only 2.520, because depth enters stiffness as the cube and section modulus as the square, and that number does not depend on the share at all. The stress is the ratio of the two, and it crosses one at a share of 0.196: every member below that line is more highly stressed for having been stiffened. The pair drawn elsewhere in this family sits at 11%, so doubling the shallow beam's stiffness takes its force up 200%, its capacity up 152% and its stress up 19%. Softening it would have worked; stiffening it made it worse.00.20.40.60.8101234the share of the load this member carried beforemultiplier after its I is multiplied by 4at 11%: stress ×1.19break-even at a share of 0.196its force, ×3.00 hereits capacity, ×2.52 everywhereits stress, ×1.19 here
Fig. 9 The same comparison for a fourfold increase in second moment. The force multiplier reaches 3.00 at a share of 11% while the capacity multiplier is 2.520 everywhere, so the stress goes up 19% — more than the doubling did. The break-even share falls to 0.196: a bigger intervention rescues a slightly wider band of members and punishes the lightly loaded ones harder.

Two readings follow. First, the members that respond well to stiffening are the ones already carrying most of the load — a member on 80% of a shared load is nearly alone, and its capacity gain outruns the small extra share it can pick up. Second, the way to relieve an overstressed member sharing a displacement is to soften something, or to stiffen its neighbour; adding material to the victim is the intervention with the worst return in the subject.

That is why a strengthening scheme can fail in the direction nobody planned for. A stiff new element added beside a flexible one takes load out of all proportion to its size, which is the mechanism behind the redistribution nobody chose at a connection.

Springs in parallel, springs in series

The same algebra read from the other end produces the opposite advice, and the pair is worth holding together because confusing them is easy.

A joint is springs in seriesThe five components of an end-plate joint, with each bar the flexibility it contributes. The column flange in bending is 39.62% of the total on its own, and doubling its stiffness raises the joint's by a factor of 1.25 — while doubling the stiffest component buys 1.05. The joint's rotational stiffness is 25227.71 kN·m per radian.flexibility contributed by each componentthey add, so the softest dominates — Sj = 25227.71 kN·m/radwhat doubling it buyscolumn web in shear21.89%×1.12column web in compression11.55%×1.06column flange in bending39.62%×1.25end plate in bending18.09%×1.1bolts in tension8.85%×1.05
Fig. 10 The five components of an end-plate joint, each drawn as the flexibility it contributes. Flexibilities in series add, so the softest component dominates: the column flange in bending is 39.62% of the total on its own, and doubling its stiffness raises the joint’s rotational stiffness of 25227.71 kN·m per radian by a factor of 1.25, while doubling the stiffest component buys 1.05.

Members sharing a displacement are springs in parallel: stiffnesses add, the stiffest one dominates, and the softest is nearly irrelevant. Components carrying the same force through a chain are springs in series: flexibilities add, the softest one dominates, and the stiffest is nearly irrelevant. A joint is the second kind and a floor grillage is the first, and the diagnostic is a single question — do these things share a force, or share a movement?

Answer it wrong and every instinct inverts. In series, stiffening the strongest-looking component buys 5%; in parallel, stiffening the weakest-looking member makes it worse. Both surprises are the same equation with the reciprocal taken.

Where the model stops

Both beams are elastic and stay that way. The share ki/kk_i/\sum k is a statement about a linear system. Once the deep beam yields it stops taking more load and the shallow one starts catching up, so the split at collapse is governed by strength rather than stiffness — which is exactly why plastic analysis is indifferent to the elastic distribution and why a ductile structure is forgiving of the whole of this essay.

The tie is rigid and carries only a vertical force. A real bolt, weld or bearing has its own flexibility in series with the two beams, and if it is soft compared with them it takes over the answer: two very stiff beams joined by a soft link share almost equally, because the link’s flexibility swamps the difference between them. A stiff connection does the opposite — it forces the two rotations to match as well, which adds equations and changes the split. The figures here assume a rigid pin.

Both members have the same modulus. Where they do not — a steel beam sharing with a concrete one, a new member with an old — the ratio is E1I1E_1I_1 against E2I2E_2I_2 and the modulus stops cancelling. That is when a stiffer material attracts load, which is the composite case and a different argument.

Nothing here creeps. A concrete member sharing a displacement with a steel one hands load over slowly as it creeps, so the share drifts for years after the load arrives. The elastic split is the day-one answer and, for a mixed-material system, not the long-term one.

What the pictures cannot show

The figures on this page draw force and stiffness and never draw time, which hides the one thing that makes load sharing hard in practice. Every share plotted here assumes both members were present when the load arrived. A member added afterwards shares only the load applied after it was added, so a stiff member installed late may carry almost nothing while its neighbour carries everything — and the sweep curve says nothing about it, because a structure that was never complete has a different stiffness at every stage of its own building.

The second omission is the tie itself. It is drawn as a line, and its flexibility is set to zero everywhere in this family. That assumption is what makes δ1=δ2\delta_1 = \delta_2 an equality rather than an approximation, and it is the assumption a real detail is least likely to honour.

The generalisation

Once the question is “do these share a force or a movement?”, the same answer keeps arriving from unfamiliar directions.

A rigid corner in a frame is a load-sharing problem: the moment that goes round the corner divides between beam and column in proportion to their stiffnesses, and the beam-to-column stiffness ratio is the rr of the sweep curve wearing different clothes. A raft is a load-sharing problem along its own length: a beam on the ground shares its load with a bed of springs, and the characteristic length is the distance over which that sharing dies out. A truss is one in which the members are axial: which member moved the roof ranks them by FfL/EAFf L/EA, and the ranking is not the ranking of their forces. A cable brings no bending stiffness to the argument at all, so the stiffness that comes from the shape depends on the tension already in it — a member whose share depends on how hard it has already been pulled.

The closing observation is the one stiffness is not strength makes from the other side. Sizing a member by strength and then discovering what it carries is backwards in a shared-displacement system, because what it carries is decided by the property nobody was sizing for.

History, briefly

Bridge decks forced the issue first, because a deck is a grillage and a wheel is a point load standing where two members cross. Before computers, distribution across a deck was handled by charts: Guyon’s work in the 1940s and Massonnet’s in the 1950s produced distribution coefficients for an orthotropic plate, which are tables of exactly the share function drawn above, evaluated by hand for a range of stiffness ratios. Computer grillage analysis arrived in the late 1950s and made the charts unnecessary. They are worth remembering anyway — they are the moment the profession accepted that a wheel does not divide by geometry.

The ladder from here

Later rungs on this anchor. The stiffness matrix, which is this essay’s two equations written for every degree of freedom at once. Shear walls sharing a storey shear, where the split follows II but the twist of the floor plate follows the distance from the centre of rigidity. Piles under a cap, where the group’s stiffness is not the sum of the individual ones because the soil transmits between them. Composite action between a slab and the beam beneath it, and what happens when the shear connection is partial. Load sharing between old and new in a strengthening scheme, where the sequence decides the split. The effect of creep on a share, which drifts for years. Grillage and orthotropic plate models for decks, and what their distribution coefficients actually are. The stiffest path under dynamic load, where the share depends on frequency rather than on stiffness alone. And the design use of deliberate softening — the bearing, the sliding joint, the slotted hole put in to stop a member attracting load it is not there to carry.

Named alongside this one

Essays reaching for the same objects. Nobody chose these; they are what the concept index makes visible.

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Every essay whose body links to this one.

The objects this essay names

Each one links to every other essay that touches it.

CompatibilityCrossing beamsLoad pathLoad sharingSection modulusStiffnessStiffness attracts loadTributary area