Equilibrium

Moving a force, and what it costs

Every free body begins by putting a force somewhere convenient. That move is free along the force's own line, costs a couple across it, and in three dimensions leaves behind something no choice of point can remove.

Assumes The free body is a choice, and choosing it well is the whole skill, Everything adds to nothing, and that is the whole of statics and Six equations, and the drawing shows three.

A force is drawn as an arrow, and an arrow has a tail. Almost every calculation in statics begins by moving that tail somewhere more convenient — to the centroid of a bolt group, to the centreline of a column, to the point about which moments are being taken — and the move is made so automatically that the price of it is rarely written down. There is a price. It is exactly one couple, it is the reason a bracket’s bolts work harder than the load suggests, and in three dimensions it leaves behind a residue that no amount of further moving can get rid of.

A force may be moved anywhere, at the price of a couple. A 60 kN force applied 180 mm off the centreline of a body, and the same force applied ON the centreline together with a couple of 10.8 kNm. The two systems are equivalent: they have the same resultant force and the same moment about every point in space, so no equilibrium equation written about the body can tell them apart. What they are not is the same loading — the stresses inside the body differ, and they differ over a distance of about the body's own depth. The offset is drawn to a scale that keeps the arrow on the body; the number beside it is the real one.
Fig. 1 A 60 kN force applied 180 mm off the centreline of a body, and the same force applied on the centreline together with a couple of 10.8 kNm. The two systems have the same resultant and the same moment about every point in space, so no equilibrium equation written about this body can tell them apart.

The rule is short enough to state in one line and is worth stating carefully, because two of its three clauses are usually dropped. A force may be moved anywhere on its own line of action for nothing; moved off that line by a distance ee, it must be accompanied by a couple of magnitude PePe; and a couple has no point of application at all. The first clause is transmissibility, the second is the whole of connection design, and the third is the one that makes the arithmetic work.

The two systems no equation can tell apart

Two force systems are statically equivalent when they have the same resultant force and the same resultant moment about one point — and if they agree about one point they agree about every point, because changing the reduction point changes both moments by the same c×R\mathbf{c} \times \mathbf{R}.

That is a strong statement and a narrow one. It says that the six equilibrium equations cannot distinguish the two panels of the figure above. It does not say the two panels are the same loading, and the whole of this collection’s business is with the quantity that does distinguish them.

A beam, its loads and its reactions. A free body: the beam cut away from everything it touches, with the forces that were doing the touching drawn on it. The reactions are computed from the loads, so their arrows are to scale relative to each other.
Fig. 2 The free body the substitution is made on. Statics gets at every internal force by cutting a body and insisting the sums cancel, so the loads it needs are the ones acting on whatever has been cut out — and moving a load from one side of a cut to the other changes the answer completely while changing no reaction at all.

So the honest form of the rule is: the reactions do not know, and the interior does. Choosing the free body is the skill, and the reason it is a skill is precisely that a substitution which is invisible from outside the body can be catastrophic inside it.

Which free body produced the number

Take the body of the first figure, cut it on a vertical plane through the centreline, and sum moments about a point on that cut.

In the left-hand panel the applied force sits at e=180e = 180 mm on one side of the cut. If the cut is taken on the other side, the force does not appear on the free body at all: the internal moment on the cut is whatever the support reactions require, and nothing else. In the right-hand panel the force has been moved onto the centreline and a couple of 60×0.180=10.860 \times 0.180 = 10.8 kNm added. Now a cut on either side sees the couple, because a couple is a free vector with no point of application — it belongs to the body, not to a place on it.

That is the substitution’s failure mode, exactly located. It has not changed a reaction; it has moved a moment across a cut. Which is another way of stating Saint-Venant’s principle: the two loadings differ, and the difference dies away over a distance of the order of the body’s own depth, so at a distance the substitution is harmless and near the point of application it is not.

The couple is what the lever arm buys

A couple is two equal and opposite forces a distance apart, and the arithmetic that makes it useful is that its moment is the same about every point — P⋅dP \cdot d, whatever the point, with no lever arm to measure from anywhere.

A moment is a product and nothing more, so doubling an arm doubles it exactly, and every quantity in the rest of this page is one of those products with the arm chosen by geometry rather than by a designer. The only thing that distinguishes a couple from the rest of them is that its two forces cancel, which is what leaves it with no point to be measured from.

There is a temptation to treat the couple as bookkeeping — a term that appears because a force was moved and disappears when it is moved back. It does not disappear. It reappears as a real demand on a real detail, and the clearest place to watch it happen is a bracket.

The eccentricity is a lever arm, and the bolts pay for it. A 100 kN load on a bracket 250 mm from the centroid of four bolts at 150 mm pitch. Moving the load to the centroid costs a couple of 25.0 kNm, and the two halves reach the bolts by different routes: the force shared equally at 25.0 kN each, the couple shared in proportion to distance from the centroid at 58.9 kN. So 70% of the worst bolt's force exists only because the load is not where the bolts are.
Fig. 3 A 100 kN load on a bracket 250 mm from the centroid of four bolts at 150 mm pitch. Moving the load to the centroid costs a couple of 25 kNm, and the two halves reach the bolts by different routes — the force shared equally at 25 kN each, the couple in proportion to distance from the centroid at 58.9 kN. So 70% of the worst bolt’s force exists only because the load is not where the bolts are.

The two halves travel differently and that is the finding. The direct force is shared by counting: four bolts, a quarter each. The couple is shared by lever arm: each bolt’s contribution is proportional to its own distance from the centroid, so the group resists the couple with ∑r2\sum r^2 — 45,003 mm² here — exactly as a section resists bending with its second moment of area.

The two components are added vectorially at each bolt, which is why the worst bolt in a group is not always the furthest one from the centroid. It is the one whose two components point most nearly the same way, and on a group that is longer than it is wide that is not the corner the eye picks first.

Sweeping the eccentricity shows what kind of quantity this is. At e=0e = 0 the couple’s share of the worst bolt is zero and the group is carrying 25 kN a bolt. At 50 mm it is already 32%; at 125 mm, 54%; at 250 mm, 70%; at 500 mm, 82.5%. The share rises fast at first and then saturates, because the direct component is fixed while the torsional one grows without limit — so for any bracket worth calling a bracket, the connection is being designed for the move rather than for the load.

The eccentricity is a lever arm, and the bolts pay for it. A 100 kN load on a bracket 500 mm from the centroid of four bolts at 150 mm pitch. Moving the load to the centroid costs a couple of 50.0 kNm, and the two halves reach the bolts by different routes: the force shared equally at 25.0 kN each, the couple shared in proportion to distance from the centroid at 117.9 kN. So 82% of the worst bolt's force exists only because the load is not where the bolts are.
Fig. 4 The far end of that sweep, on the same group. The load has moved from 250 mm out to 500, so the couple has doubled to 50.0 kNm and the torsional component on each bolt has doubled with it, from 58.9 kN to 117.9. The direct component has not moved at all: it is still 25.0 kN on every bolt, because it is shared by counting. What used to be 70% of the worst bolt is now 82% of a much larger number, and a group sized for the load alone is out by a factor of five.

The one term a designer can actually change

If seventy per cent of the worst bolt’s force exists only because the load is not where the bolts are, the obvious question is what can be done about it, and the arithmetic answers it precisely.

The torsional component on a bolt is Mr/∑r2M r / \sum r^2, with M=PeM = Pe. Three quantities are in that expression and they are not equally available. PP is the load and is given. ee is the eccentricity, and it is usually architecture rather than engineering — a bracket is 250 mm out because something has to sit 250 mm out. What is left is the geometry of the group itself, and it enters twice.

Spread the group and rr grows in proportion to the pitch while ∑r2\sum r^2 grows as its square, so the worst bolt’s torsional force falls in inverse proportion to the pitch. Take the four-bolt group above from a 150 mm pitch to 300 mm: ∑r2\sum r^2 goes from 45,000 to 180,000 mm² and rmaxr_{max} from 106.1 to 212.1 mm, so the torsional component falls from 58.9 kN to exactly 29.5. The direct component does not move at all, staying at 25 kN a bolt, because it is shared by counting.

The eccentricity is a lever arm, and the bolts pay for it. A 100 kN load on a bracket 250 mm from the centroid of four bolts at 300 mm pitch. Moving the load to the centroid costs a couple of 25.0 kNm, and the two halves reach the bolts by different routes: the force shared equally at 25.0 kN each, the couple shared in proportion to distance from the centroid at 29.5 kN. So 54% of the worst bolt's force exists only because the load is not where the bolts are.
Fig. 5 The one term a designer owns, moved. The same 100 kN at the same 250 mm, on a group opened from a 150 mm pitch to 300: the couple is the 25.0 kNm it always was, and the torsional component on the worst bolt has fallen from 58.9 kN to 29.5 — exactly halved, because rr grew with the pitch and ∑r2\sum r^2 grew with its square. The direct component is unchanged at 25.0 kN, so the move’s share of the worst bolt falls from 70% to 54%. Nothing about the load, the bracket or the steel is different between this figure and the one two sections above.

That is an unusually clean lever, and it inverts the intuition the previous section leaves. The eccentricity enters linearly and the group size enters inversely, so a bracket twice as far out with a group twice as wide is no worse than the original — the couple doubles and the resistance doubles with it. What makes a bracket bad is not the distance the load sits at but the ratio of that distance to the size of the group resisting it, which is the same statement as depth being the cheapest strength arriving in a connection instead of a beam.

The second entry is the number of bolts, and it is the weaker of the two. Adding bolts on the same footprint raises ∑r2\sum r^2 roughly in proportion to their number and leaves rmaxr_{max} alone, so eight bolts in the space of four halve the torsional component — the same factor the doubled pitch bought, at twice the drilling. Which is why the first move on an overloaded bracket is to make the group bigger rather than denser, and why a connection whose bolts cannot be spread is the one that ends up welded.

The part that cannot be moved away

Everything so far is planar and everything so far has been a matter of choosing where to put the arrow. Reducing about a different point changes the couple by c×R\mathbf{c} \times \mathbf{R}, and a cross product is perpendicular to R\mathbf{R}. So there is a component of the moment that no choice of point can touch: the component along the resultant.

p=M⋅R∣R∣2,M∥=p Rp = \frac{\mathbf{M}\cdot\mathbf{R}}{|\mathbf{R}|^2}, \qquad \mathbf{M}_\parallel = p\,\mathbf{R}

pp has the units of a length and is called the pitch. It is an invariant of the force system: not of the drawing, not of the reduction point, not of the coordinate axes.

One part of the moment is a property of the system. The moment of the same two forces taken about a run of points along the central axis, split into the component along the resultant and the component across it. Moving the point changes the moment by c × R, and a cross product is perpendicular to R — so the component along R cannot be altered by any choice of point at all. It sits at 13.416 everywhere on this line, which is the resultant times a pitch of 1.2000. The perpendicular part is zero on the axis and grows either side of it.
Fig. 6 The moment of two spatial forces — 10 units pressing down at (2,0,0)(2,0,0) and 5 pushing sideways at (0,3,0)(0,3,0) — taken about a run of points along the central axis and split into the component along the resultant and the component across it. The first sits at 13.416 everywhere on the line, which is the resultant times a pitch of 1.2000, and it is in fact the same number about every point in space rather than only along this one. The second is zero on the axis and grows either side of it, which is what makes the axis the axis.

The perpendicular part can always be driven to zero, and the point at which it vanishes is the central axis:

c=R×M∣R∣2\mathbf{c} = \frac{\mathbf{R} \times \mathbf{M}}{|\mathbf{R}|^2}

which is derived rather than quoted: it is the shift for which M+c×R\mathbf{M} + \mathbf{c}\times\mathbf{R} comes out parallel to R\mathbf{R}. For the two forces of the figure, that axis passes through (1.6, 0.6, 0.8)(1.6,\ 0.6,\ 0.8).

Three systems that always reduce to a single force

Before the general case, the special ones, because they are the reason the general case is so easily missed. A force system reduces to a single force whenever M∥\mathbf{M}_\parallel vanishes, and it vanishes automatically in three common arrangements.

Concurrent. If every force passes through one point, the moment about that point is zero, so the pitch is zero. That is the reduction three-force problems are solved by: with three forces on a body and no couple, the lines of action must meet, because two of them meet somewhere and the third must pass through the same point or the sums cannot cancel.

The concurrency there is not a convenience of the graphical construction. It is the statement that a three-force system carrying no couple has a pitch of zero, which forces its central axis through the intersection of the first two lines and leaves the third with nowhere else to go.

Parallel. If every force points the same way, both R\mathbf{R} and every r×P\mathbf{r}\times\mathbf{P} are constrained: the moment is perpendicular to the common direction, so again p=0p = 0. The single force is at the centroid of the load, and replacing a spread load by its resultant is that reduction used every day.

Coplanar. If every force lies in one plane, every moment is normal to that plane and the resultant lies in it, so M⋅R=0\mathbf{M}\cdot\mathbf{R} = 0 identically. Three arbitrary forces in a plane — (3,−4)(3,-4), (−1,6)(-1,6) and (2,1)(2,1) at three unrelated points — reduce to a resultant of (4,3)(4,3) on a line through (−1.86, 2.48)(-1.86,\ 2.48), and the computed pitch comes out as exactly zero.

Every drawing on this site is coplanar, which is why the general result never appears in it and why it comes as a surprise when it does.

What a general system reduces to

A three-dimensional free body has six equations rather than the three a drawing shows, and six equations mean the resultant of everything acting on it is a force and a couple. Nothing in the six says the couple has to be perpendicular to the force. In a plane it always is, which is why the general case never appears; out of it, there is no reason for it to be, and generally it is not.

Take two forces that are neither concurrent, nor parallel, nor coplanar: 10 units pressing down at (2,0,0)(2,0,0), and 5 units pushing sideways at (0,3,0)(0,3,0). The resultant is (5,0,−10)(5, 0, -10), of magnitude 11.1803. The moment about the origin is (0,20,−15)(0, 20, -15). The pitch is M⋅R/∣R∣2=150/125=1.2\mathbf{M}\cdot\mathbf{R}/|\mathbf{R}|^2 = 150/125 = 1.2, which is not zero, so no point in space reduces this pair to a force alone.

A general force system is a screw, not a force. Two forces that are neither parallel, nor concurrent, nor coplanar. Their resultant is (5, 0, -10) and no point in space reduces them to it alone: the moment left on the central axis is (6.00, 0.00, -12.00), which is parallel to the resultant and has a pitch of 1.2000. The simplest object equivalent to the system is therefore a force and a couple about the same line — a wrench — and a planar drawing can never produce one, because a coplanar system has its moment perpendicular to its resultant by construction.
Fig. 7 Those two forces, their central axis, and what survives on it. The resultant is (5,0,−10)(5,0,-10), of magnitude 11.18; the moment left on the axis is (6.00, 0.00, −12.00)(6.00,\ 0.00,\ -12.00), of magnitude 13.42, and it is parallel to the resultant rather than across it. Their ratio is the pitch, 1.2000, and it is the one number about this system that no choice of reduction point, coordinate frame or drawing can alter.

The simplest object equivalent to a general force system is therefore a force and a collinear couple — a wrench, or in the older language a screw. Poinsot published the result in 1804, and the name is not a metaphor: pushing and twisting about the same line is exactly what a screwdriver does, and the pitch has the units of a length for exactly the reason a screw’s pitch does.

Two consequences worth keeping. A general spatial system has no line of action. Asking “where does the resultant act?” is a question with no answer, and only the accident of coplanarity makes it seem like a reasonable one. And the pitch is a genuine invariant, in the same family as the bimoment and locked-in residual stress: quantities that survive every operation the equilibrium equations can perform and are therefore invisible to them.

The substitution that changes the interior

The rule’s first clause — a force may be slid along its own line for nothing — deserves the sharpest statement of its limits, because it is the one that gets used without thinking.

A triangular load and the force that replaces it. A triangular distributed load with its resultant computed by integration: an area of 24.0 acting at 5.33 from the left. The two moment diagrams below show what the substitution costs — the reactions are identical and the peak moment is not.
Fig. 8 A triangular distributed load and the single force that replaces it: the same area, acting at the centroid of that area. The reactions computed from the two agree exactly. The moment diagrams do not, and the difference is largest at the point the substitution was made about.

Sliding a force along its line is free for a rigid body, which is a body with no interior worth asking about. For every body this collection is interested in, it is a change of loading whose effects are confined to the neighbourhood of the move — and “confined to the neighbourhood” is not “absent”. A column loaded through its centroid and the same column loaded at its face with a compensating moment applied to the beam are statically equivalent and are not the same detail; the first has a uniform stress block and the second has a stress concentration and a length of column over which the two have not yet reconciled.

This is why a moment applied to a beam needs its point named. The couple that pays for a translation is a free vector to the equilibrium equations and it is not free to the material: somewhere, two forces a distance apart are actually being applied, and where they are applied decides the local stress field entirely.

Where the model stops

Rigid bodies do not exist. Every statement about equivalence above is a statement about the six equations, and the six equations are blind to compatibility. Two statically equivalent loadings on a redundant structure can produce genuinely different reactions, because the reactions in a redundant structure depend on stiffness, and stiffness depends on where the load actually is. The wrench and the pitch survive; the reaction distribution does not.

A couple’s “no point of application” is an idealisation of a pair. Any real couple is delivered by forces on an area, and the area matters as soon as the question is local. A moment connection delivers its couple through two flange forces on two identifiable patches of steel, which is the whole reason the connection field exists.

Nothing here is dynamic. A force system on a body that is accelerating is not in equilibrium at all, and the reduction above is a statement about the system of forces, not about what the body does with it. The extra term is the mass times the acceleration, and it is not a load anybody applied.

The pitch is invariant, not conserved. Adding a force to the system changes it. It is a property of a given set of forces, not a quantity that persists as loads come and go.

What the pictures cannot show

The wrench figure draws a ring about the central axis to stand for the couple, and a ring is not what a couple looks like — a couple has no shape, no size and no location, and the ring is a symbol whose radius was chosen to be legible. Any other radius would have been equally correct, which is precisely the property being illustrated and is exactly what the drawing cannot convey.

The bracket figure draws two arrows at each bolt and adds them. Real bolts do not carry two forces; they carry one, and the decomposition into a direct part and a torsional part is a way of computing that one, not a description of anything happening in the steel. The decomposition is also elastic, and the same group analysed by its instantaneous centre gives a different and larger answer, because the elastic method assumes a rotation about the centroid that a group at failure does not have.

And the invariant figure plots a moment against distance along a line that a reader cannot see. The line is not a feature of the structure; it is a locus derived from the force system, and the whole of the figure’s content is that one of the two curves in it is flat.

The ladder from here

Later rungs on this anchor: the reduction of a distributed loading over a surface to a wrench, and why a wind pressure field has a centre of pressure only when it is planar. The null system and the reciprocal screw, which is where this argument meets kinematics — a body free to move along a screw is in equilibrium under any wrench reciprocal to it, and the whole of screw theory is that pairing. Statically equivalent load systems in finite element practice, where a nodal load set is chosen for equivalence in the work sense rather than the resultant sense, and gives different answers for that reason. The centre of gravity as a special case of the parallel reduction, and the conditions under which it exists at all in a non-uniform field. And the moment about an axis rather than a point, which is the operation every torsion calculation on this site quietly performs.

Poinsot’s own route to the wrench came from a question about the composition of rotations, not about statics; he was looking for the object that plays the part of the resultant in the kinematic problem and found that the two questions have the same answer. Statics inherited it, drew everything in a plane for the next two centuries, and mostly forgot it.

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

The 8 essays that link to this one and share the most of its objects, of 9 that link here.

The objects this essay names

Each one links to every other essay that touches it.

Bolt groupEccentricityFree body diagramLever armLine of actionMoment about an axisMoment centreMoment equilibriumResultantRigid bodySaint-Venant's principleSelf-equilibrating