Connections

The connection is not a point, and every diagram on this site says it is

Every free body drawn here has joined its members at points. Real structures fail at the joints far more often than in the members, and the reason is that a joint is exactly the region the theory behind every other page explicitly excludes.

Assumes The free body is a choice, and choosing it well is the whole skill and What a cut reveals, and why it was there all along.

Every diagram on this site so far has been a lie of the same kind, told deliberately and told well. A truss is drawn as lines meeting at points. A portal frame is drawn as three lines with two corners. A beam is drawn as a line resting on two triangles. In each case the members have length and the joints do not, and the analysis that follows treats the joint as a coordinate: a place where forces are transferred, occupying no space and having no properties.

That idealisation is what makes structural analysis possible, and nothing here is going to retract it. What this field does is ask what was inside the point.

A bolt group under an eccentric loadA 3 by 2 bolt group carrying 100 kN at 150 mm from its centroid, with the resultant force on each bolt drawn to scale, by the elastic vector method. The load is shared equally and the torque is not, so the worst bolt carries 50.37 kN against 16.67 kN of direct shear alone — 3.02 times as much.100 kNe = 150centroidworst bolt 50.37 kNSix bolts · direct shear 16.67 kN eachelastic vector method
Fig. 1 A bracket bolted to a column, carrying 100 kN. On a frame diagram this is a node, and the answer is 100 kN transferred. Here it is six bolts in a rectangle, and the load’s line of action misses their centroid by 150 mm — so the group carries a force and a torque, the two add differently at every bolt, and the worst bolt carries 50.4 kN against a direct share of 16.7. The picture on the frame diagram is not wrong. It is a different question.

Where structures actually fail

The engineering literature on structural failure is dominated by connections, and by a margin that is not close. Bridge collapses, roof collapses, the progressive failures that make textbooks — the fracture almost always starts where two pieces of steel were joined, or where a beam sat on a wall, or where a bolt passed through a plate.

It is tempting to read that as a statement about workmanship, and there is some of that. But the deeper reason is available from the theory itself, and it is the same reason the analysis had to idealise the joint in the first place.

Everything in the six fields that precede this one descends from one assumption about geometry: that a plane section stays plane. That assumption is what makes strain linear across a cut face, which makes stress linear, which produces the second moment of area, the section modulus, the deflection formulae and every capacity this site has computed.

It is justified by Saint-Venant’s principle, which says that the details of how a load is applied stop mattering at a distance of roughly one section depth from where it is applied. Beyond that distance the stress field settles into the smooth linear one the theory assumes.

Read that principle carefully and it says something else at the same time. Within about one section depth of a load application, a support, a change of section or a joint, the linear field does not hold. The theory does not merely become less accurate there; it is a statement about a region it explicitly excludes.

A connection is nothing but that region.

Two kinds of region, and the names for them

The distinction is old enough to have shorthand. A B-region — B for Bernoulli, or for beam — is one where plane sections stay plane and beam theory applies. A D-region — D for disturbed, or discontinuity — is one where it does not.

The rule of thumb for the extent of a D-region is the same section depth Saint-Venant’s principle uses. A beam 400 mm deep has a D-region roughly 400 mm long at each end, at each point load, and around each hole. The rest is B-region, and the rest is where every formula on this site works.

For a member of ordinary proportions the B-regions are most of it. For a short deep beam they may be none of it, which is the case where beam theory stops applying altogether. And for a connection, the D-region is the connection.

Block shear: the metal between the holesThree bolts in a 10 mm plate end connection. The shaded block tears out along a shear plane 180 mm long and a tension plane 40 mm long. Shear yields first, and the capacity is the sum of two different strengths on two different planes: 421.7 kN, of which the shear plane carries 70.43%.pullshear plane, 180 mmtension plane, 40 mmcapacity 421.7 kN0.6 fu Anv = 322.5 kN · 0.6 fy Agv = 297 kN · fu Ant = 124.7 kNthe yield value governs the shear plane
Fig. 2 What a D-region can do that a B-region cannot: fail by tearing a block of metal out of the plate. There is no section modulus in this, no neutral axis, no bending stress. The capacity is the sum of two different strengths acting on two different planes, and no member formula predicts it because the failure is a shape rather than a stress at a point.

The block above is the clearest possible demonstration that the connection needs its own analysis. Nothing in bending, in shear flow or in buckling can express it. The plate is not bending. It is coming apart along two surfaces, and predicting when requires knowing where the surfaces are.

What the point was hiding

Take the bracket at the top of this page and ask what the frame analysis knew about it.

It knew a force: 100 kN, vertical, applied at a node. It possibly knew a moment, if the frame model included one. What it did not know, and could not have known, is that the connection has a size — and that the size is what produces the answer.

The load arrives at the end of a bracket. The bolts are 150 mm away. That distance is not a modelling choice; it is set by how wide the beam is, how much room the bolts need, how a spanner reaches them. And that distance turns a 100 kN force into a 100 kN force plus a 15 kN·m torque, which the six bolts share in a way that gives one of them three times the average.

The general form is worth stating plainly:

A connection has dimensions, and every dimension is a lever arm for something.

This is the sentence that the whole field elaborates. The distance from a bolt to a web face is the lever arm that makes the flange bend and produces prying. The distance from a bolt to the edge of a plate is the lever arm that decides whether the plate tears out or crushes. The distance from a bolt row to the compression flange is the lever arm that turns bolt tension into moment capacity. The distance from the centroid of an angle to the leg it is bolted through is the lever arm that leaves part of the section not working.

None of those distances exists on a frame diagram. All of them decide the answer.

The three questions a connection has to answer

Once the point becomes a region, the design question splits into three, and they are usually answered by different mechanisms with different failure modes.

Can the force get out of the first member? The force in a member is distributed over its section in the way beam theory says. It has to be collected out of that distribution and into whatever fastens the members together — bolts, welds, bearing. A section connected through only part of itself does not deliver all of its own capacity, which is shear lag, and the loss is geometry.

Can the fastenings carry it? This is the question that gets called “connection design” and it is only a third of the problem. Bolts in shear, bolts in tension, welds along a line, friction across an interface. Each has its own capacity and its own way of sharing between fasteners, and the sharing is rarely equal.

Can the second member take it? The force arrives at a small patch of the second member, which has to distribute it back into a smooth field. Web crippling, column web buckling, plate tear-out, base plate bending: every one of them is a member being asked to accept a load at a point.

A connection fails at whichever of the three is weakest, and there is no reason for that to be the one anybody checked.

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. 3 The same structure in the stiffness question rather than the strength one. A joint’s rotational stiffness is the series combination of the flexibilities of everything the force passes through, so the softest component decides — and stiffening any of the others changes almost nothing. The bar lengths are the flexibilities, and the column flange in bending is 40% of the total on its own.
Prying action in a tee stubA tee stub pulled by its web with 100 kN per bolt. The 20 mm flange is in the one-hinge regime, so the prying force at the flange tip is 50.63 kN and the bolt carries 150.63 kN — 1.51 times what was applied. The flange stops prying entirely at 26.97 mm thick, and collapses on its own at 110 kN.100 kN appliedbolt 150.63 kNprying 50.63 kNm = 45n = 40flange 20 mm · one-hingebolt force is 1.51 times the applied load
Fig. 4 The second of the three questions. A bolt pulled through a flexible plate carries more than was applied to it, because the plate bends and levers its own edge against the support — 150.6 kN of bolt for 100 kN of applied load. Nothing about that is visible in a joint drawn as a point, and both of the lengths that produce it are detailing decisions.
Bearing and tear-out against end distanceA 20 mm bolt in a 10 mm plate. Below 165 mm of end distance the bolt tears a channel out to the end and the capacity is proportional to that distance; above it the plate crushes in front of the bolt and the end distance stops mattering. At 40 mm the capacity is 52.12 kN and the mode is tear-out.020406080100120140160180200050100150200end distance, mmbearing capacity, kN40 mm → 52.12 kNcorner at 165 mmplate crushesbolt tears out
Fig. 5 The third question, which is about the member the force arrives in. One 20 mm bolt at the minimum end distance gives at 34.4 kN in a 10 mm plate, against a bolt shear capacity near 94 — so the plate, not the fastener, is usually the limit. The variable that decides is the distance from the bolt to the edge, which is set by a table of minima.

Why this is a field and not a chapter

There is a reason connections have not appeared until now, and it is not that they are advanced.

Every other field on this site can be entered from the middle. Bending stress can be read without knowing about buckling. Deflection can be read without knowing about plasticity. The results are separable because each concerns one member analysed one way.

Connections are not separable, because the connection is where every other question arrives at once. A moment end plate is simultaneously a bolt problem, a plate bending problem, a weld problem, a column web problem and a stiffness problem, and its answer is the worst of them. That is why this field comes eighth and why it needs the seven before it.

It is also why connection design in practice is so heavily codified. The number of possible failure modes is large, several of them are non-obvious, and the consequences of missing one are worse than for a member — a member that is 10% overstressed usually yields and redistributes, whereas a bolt group that is 10% overstressed may fracture without warning at all.

What replaces the smooth field

If beam theory does not apply in a D-region, something has to.

The oldest answer, and still the most useful, is to abandon stress distributions entirely and go back to equilibrium. Draw a free body that cuts through the connection, sum the forces, and ask what mechanism carries each one. That is what a strut-and-tie model does for concrete and what the block-shear calculation does for steel: it identifies a path the load could take and checks whether every element of the path is adequate.

Its justification is the lower-bound theorem of plasticity, which is one of the most useful results in the subject and appears here in the same form it takes for masonry arches: if any distribution of internal forces can be found that is in equilibrium with the applied load and nowhere exceeds the material’s strength, the structure will carry that load. The right distribution does not have to be found. One does.

That theorem is what makes connection design possible at all. Nobody knows the real stress field in a bolted end plate — it is three-dimensional, involves contact, friction and plasticity, and changes as the joint is loaded. What can be done is to propose a mechanism, check every link in it, and rely on the material’s ductility to redistribute towards whatever mechanism was proposed.

Which is why ductility is a precondition rather than a bonus in this field. The lower-bound theorem requires that the material can deform enough to reach the assumed distribution. A connection whose components are all brittle has no guarantee at all, and this is exactly why the property that appears in none of the equations turns out to be doing the load-bearing work here as well.

Moment against rotation, for three real jointsThree connections on one plot, with the classification boundaries for a beam of EI/L = 14000 drawn as rays through the origin. web cleats is pinned, flush end plate is semi-rigid, extended end plate is semi-rigid. The boundaries are multiples of EI/L, so the same joint is rigid on a short stiff beam and semi-rigid on a long slender one.00.0050.010.0150.020.0250.030.0350.040.0450.05050100150200rotation, radiansmoment, kN·mrigid abovepinned belowweb cleats — pinnedflush end plate — semi-rigidextended end plate — semi-rigid
Fig. 6 Three real connections, and the two boundaries that decide what to call them. The boundaries are multiples of EI/L — the beam’s own stiffness — so the classification is a statement about the joint and the member together. The same end plate is rigid on a short stiff beam and semi-rigid on a long slender one.

Why the idealisation is still right

None of this is an argument for modelling connections in the frame analysis. It is worth being explicit about that, because the obvious reading of everything above is “so the frame model should include the joints”, and for almost all work the answer is no.

The frame analysis exists to answer a question the connection cannot: how the load divides between routes to the ground, which needs the whole structure at once and is a stiffness question rather than an equilibrium one. Adding six bolts and a plate to every node would multiply the model’s size by a large factor, would require knowing details of connections that have not been designed yet, and would answer the same question to no better accuracy — because the quantity the frame model produces is a set of member forces, and those are insensitive to almost everything the connection does except its rotational stiffness.

So the division of labour is deliberate and it is the right one. The frame model produces forces at nodes. The connection design takes those forces and asks how they get across, using a completely different method on a much smaller region. The two are checked against each other at exactly one property — the rotational stiffness, which is the only thing the connection does that the frame can feel — and everything else about the joint is invisible to the analysis by design rather than by omission.

What goes wrong is not the split. It is forgetting that the split happened, and reading the frame’s node force as a complete specification of what the connection has to do.

An angle bolted through one legA 100 × 75 × 10 angle connected through its 100 mm leg with three bolts at 75 mm pitch. The centroid sits 19.77 mm from the connected face over a connection 150 mm long, so U = 1 − 19.77/150 = 0.87 and 13.18% of the net area is not working.x̄ = 19.77connected legoutstanding legLc = 150net areaU = 0.87 of it worksU = 1 − x̄ / Lc = 0.87both halves are geometry — where the centroid sits, and how long the connection is
Fig. 7 The first of the three questions, drawn. An angle bolted through one leg has to collect its force out of the whole section and into one face of it, and over a short connection it never fully does — the centroid sits 19.8 mm from the connected face over a connection 150 mm long, so 13% of the net area is not working. The member’s own capacity is unchanged; what changed is how much of it the connection can reach.

Notice which quantities decided that. Not the steel grade, not the bolt grade, not the thickness of anything: the position of the section’s own centroid, and the length of the bolt line. Both are lengths on a drawing, and neither appears anywhere in the member analysis that produced the force being transferred.

The two idealisations, and the space between them

Frame analysis offers two options for a joint: pinned or rigid. Both are convenient, both are used constantly, and both are false.

A pinned joint is one that transmits no moment. Real “pinned” connections — web cleats, fin plates, flexible end plates — transmit some. A rigid joint is one where the members’ ends rotate together. Real “rigid” connections deform, so they do not.

For most purposes the errors are acceptable and in the safe direction, but not always, and the figure above says why the question cannot be answered by looking at the connection alone. The boundaries are stiffnesses compared with EI/L. A joint is not rigid; a joint is rigid relative to a particular beam. Change the beam and the same connection changes class.

The consequence is a redistribution that nobody designed: a beam analysed as simply supported, with a connection that is actually semi-rigid, has real end moments the analysis never predicted and a smaller mid-span moment than it was designed for. Usually that is safe. It is not always, and it is never intentional.

How a moment crosses a gapA moment end plate with three bolt rows. The moment is carried as a couple: tension in the rows, compression through bearing at the bottom flange. The plastic distribution reaches 172.8 kN·m and the elastic one 142.29 kN·m, a factor of 1.21 — and the compression at the bottom flange is 540 kN either way, which is the check that gets forgotten because it is not a bolt.180 kNrow 1 · 420 mm180 kNrow 2 · 340 mm180 kNrow 3 · 200 mm540 kN compressionPlastic distribution — M = 172.8 kN·mthe other distribution is drawn faintly: 1.21× between them
Fig. 8 And all three at once, which is what a real connection is. A moment end plate has to get the force out of the beam’s flanges, share it between bolt rows that are not equally able to take it, and deliver the compression half of the couple into a column web that no bolt schedule mentions. Its capacity is the worst of those, and there is no reason for it to be the one that was checked.

What this field will do

Fifteen essays, and each one takes a distance on a drawing and shows what it decides.

Some of them are about bolts: how a group shares an eccentric load, how a bolt in tension carries more than it was given, how a plate fails around a hole, and what a preloaded joint does that an ordinary one does not. Some are about welds, where the geometry is a line rather than a set of points, and where the capacity depends on the direction of the load in a way that comes out of the yield criterion rather than out of a test.

Some are about whole connections: the end plate that makes a moment cross a gap, the base plate where a structure meets its foundation, the classification that decides what a frame analysis is allowed to assume.

The thread through all of them is the sentence above. The point had a size, and the size is the answer.

What this makes readable

Essays that name this one as a prerequisite.

Named alongside this one

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

What links here

Every essay whose body links to this one.

The objects this essay names

Each one links to every other essay that touches it.

Bolt groupConnectionDisturbed regionEccentricityFree body diagramJointLoad pathSaint-Venant's principle