Force Is Not Enough: the Moment of a Force

You know what changes the translational state of a body: a force. So what changes its rotational state?

The honest way to find out is to look at a door.

A door is a rigid body hinged on a fixed vertical line. Push it and ask what actually makes it swing:

  • Push at the hinge line and it does not turn at all, however hard you push.
  • Push along the door, straight towards the hinge, and again nothing turns.
  • Push at the outer edge, at right angles to the door, and it swings easily.
  • Push at the same outer edge but at a slant, and it swings, but less readily.

Torque as r cross F, and three ways of pushing a door from above

So the force alone settles nothing. Where you apply it and which way it points matter just as much. The quantity that combines all three — how big, where, and which way — is called the moment of force, or the torque.

The definition

Key Point — torque: If a force F\vec{F} acts on a particle whose position vector with respect to a chosen origin OO is r\vec{r}, the moment of the force about OO, or the torque, is τ=r×F\vec{\tau} = \vec{r} \times \vec{F} It is a vector, perpendicular to the plane containing r\vec{r} and F\vec{F}, with its sense given by the right-hand rule. The symbol is the Greek letter tau.

Everything about it follows from the cross product you set up in Section 4 — anticommutativity, the determinant form, the right-hand rule. Nothing new is needed here; we are simply feeding physics into machinery that already works.

Units and dimensions, and a warning

[τ]=[r][F]=LMLT2=ML2T2[\vec{\tau}] = [\vec{r}][\vec{F}] = \mathrm{L} \cdot \mathrm{M L T^{-2}} = \mathrm{M L^2 T^{-2}}

The SI unit is the newton metre (N m).

Key Point: Torque has the same dimensions as work and energy, but it is a completely different physical quantity. Work is a scalar, formed from a dot product; torque is a vector, formed from a cross product. Never write the unit of torque as a joule. Write N m.

[Board Important] "Torque and work have the same dimensions — are they the same quantity?" is a standard two-mark question. The answer is the sentence above: same dimensions, different nature, one scalar and one vector, and the units are deliberately written differently to keep them apart.

Reading the door again, now with symbols

Where you push r\vec{r} Angle between r\vec{r} and F\vec{F} τ=rFsinθ\tau = rF\sin\theta
at the hinge r=0r = 0 undefined 0
along the door, towards the hinge along the door 180°180° 0
at the edge, at right angles full width 90°90° rFrF, the largest possible
at the edge, at a slant full width θ\theta rFsinθrF\sin\theta, less

Key Point — when the torque vanishes: τ=0\vec{\tau} = 0 if the force is zero, or if r=0\vec{r} = 0, or if θ=0°\theta = 0° or 180°180° — that is, whenever the line of action of the force passes through the chosen point. Remember it as: a force aimed at the pivot cannot turn anything about it.

Three Readings of the Same Number

The magnitude of the torque,

τ=rFsinθ\tau = rF\sin\theta

can be grouped in three ways, and each grouping tells a different story about the same situation. In an exam you should be able to slide between them without thinking.

Spanner drawn three times showing rFsin theta, moment arm, and perpendicular force

Reading 1: τ=rFsinθ\tau = r\,F\sin\theta

Take the full distance, the full force, and pay a penalty sinθ\sin\theta for the misalignment. Use this when the question hands you a distance, a force and an angle.

Reading 2: τ=rF\tau = r_\perp F, the moment arm

Regroup as τ=(rsinθ)F\tau = (r\sin\theta)\,F. Now r=rsinθr_\perp = r\sin\theta is the perpendicular distance from the point OO to the line of action of the force — extend the force's line both ways and drop a perpendicular on to it from OO. That distance is the moment arm (or lever arm).

τ=rF=(moment arm)×(force)\tau = r_\perp F = (\text{moment arm}) \times (\text{force})

This is the reading engineers and lever problems use, and it makes the vanishing case obvious: if the line of action passes through OO, the moment arm is zero, so the torque is zero.

Reading 3: τ=rF\tau = r\,F_\perp, the useful component

Regroup the other way as τ=r(Fsinθ)\tau = r\,(F\sin\theta). Split F\vec{F} at the point of application into a piece along r\vec{r} and a piece across it:

  • FcosθF\cos\theta, along r\vec{r} — this piece pulls or pushes towards or away from OO and produces no turning at all;
  • F=FsinθF_\perp = F\sin\theta, at right angles to r\vec{r} — this piece is the whole of the turning effect.

τ=rF\tau = r\,F_\perp

Key Point — the three readings: τ=rFsinθ=rF=rF\tau = rF\sin\theta = r_\perp F = r F_\perp One number, three routes. Pick the route the data hands you.

[JEE Tip] When several forces act at different points and different angles, Reading 2 is nearly always fastest: draw each line of action, read off each moment arm by geometry, multiply, and add with signs. You never have to resolve a single force.

The sign, for coplanar problems

Almost every problem you meet has all the forces in one plane. Then all the torques point along the one perpendicular axis, and you can treat them as signed numbers:

  • torque tending to turn the body anticlockwise in your diagram: positive;
  • torque tending to turn it clockwise: negative.

Add them algebraically. That is legitimate only because they are all parallel vectors, which is exactly what makes coplanar problems easy.

What reversing things does

Because τ=r×F\vec{\tau} = \vec{r} \times \vec{F} is linear in each factor:

Change Effect on τ\vec{\tau}
reverse F\vec{F} τ\vec{\tau} reverses
reverse r\vec{r} (move to the diametrically opposite point) τ\vec{\tau} reverses
reverse both τ\vec{\tau} is unchanged
double FF, halve rr_\perp τ\vec{\tau} unchanged

[NEET Important] That last row is the whole idea of a spanner, a lever and a steering wheel: to get the same turning effect with less force, increase the moment arm.

Torque Is Always Reckoned About a Point — and the Point Matters

A force has a magnitude and a direction and that is the end of it. A torque is not fully specified until you say what it is about. This is the single most-missed idea in the topic.

The same force, two different torques

Let a force F=20j^\vec{F} = 20\hat{j} N act at the point PP with position vector 3i^3\hat{i} m.

About the origin OO: τO=(3i^)×(20j^)=60(i^×j^)=60k^ N m\vec{\tau}_O = (3\hat{i}) \times (20\hat{j}) = 60\,(\hat{i} \times \hat{j}) = 60\hat{k} \text{ N m}

About the point AA at 5i^5\hat{i} m, the position vector of PP relative to AA is 3i^5i^=2i^3\hat{i} - 5\hat{i} = -2\hat{i}, so τA=(2i^)×(20j^)=40k^ N m\vec{\tau}_A = (-2\hat{i}) \times (20\hat{j}) = -40\hat{k} \text{ N m}

Same force, same point of application — different size and opposite sense. Neither answer is wrong; they answer different questions.

The shifting rule

Suppose you know the torque about OO and want it about a new point O1O_1 whose position vector is d\vec{d}. The new position vector of the particle is rd\vec{r} - \vec{d}, so

τ1=(rd)×F=r×Fd×F\vec{\tau}_1 = (\vec{r} - \vec{d}) \times \vec{F} = \vec{r} \times \vec{F} - \vec{d} \times \vec{F}

Key Point — moving the reference point: τ1=τOd×F\vec{\tau}_1 = \vec{\tau}_O - \vec{d} \times \vec{F} The torque of a single force changes when you move the point, unless d\vec{d} happens to be parallel to F\vec{F} — that is, unless you move the point along the line of action.

Check it on the numbers above: d=5i^\vec{d} = 5\hat{i}, d×F=100k^\vec{d} \times \vec{F} = 100\hat{k}, and 60k^100k^=40k^60\hat{k} - 100\hat{k} = -40\hat{k}. It works.

Notice also that there is always one whole line of points about which a given force has zero torque — namely its own line of action. Here that is the vertical line through x=3x = 3 m.

[JEE Tip] In any problem involving torque, the first line of your solution should name the point: "torques about the hinge", "torques about the centre of mass". An unlabelled torque is not an answer.

Torque about an axis, rather than a point

Sometimes what you want is not the whole vector but its effect about a particular line — the hinge line of a door, the shaft of a wheel. That is the component of τ\vec{\tau} along that line:

τaxis=τn^\tau_{\text{axis}} = \vec{\tau} \cdot \hat{n}

where n^\hat{n} is a unit vector along the axis and the torques are taken about any point on the axis. Only this component can change the body's rotation about that axis; the perpendicular components are taken up by the bearings that hold the axis in place.

For rotation about a fixed zz-axis this reduces to the familiar τz\tau_z, and Sections 8 to 10 build the fixed-axis dynamics on top of it.

Key Point: A force with a large torque about a point may have zero torque about a chosen axis through that point — if its torque vector happens to be perpendicular to the axis. This is why pushing sideways on a door frame does not open the door.

Angular Momentum of a Particle: l=r×p\vec{l} = \vec{r} \times \vec{p}

Torque is the rotational partner of force. What, then, is the rotational partner of momentum?

Build it the same way. Torque was the moment of a force: position vector crossed into force. So define the moment of momentum, and give it a name of its own.

Key Point — angular momentum of a particle: For a particle of mass mm with linear momentum p=mv\vec{p} = m\vec{v} at position r\vec{r} relative to a chosen origin OO, l=r×p=m(r×v)\vec{l} = \vec{r} \times \vec{p} = m\,(\vec{r} \times \vec{v}) It is a vector perpendicular to the plane of r\vec{r} and p\vec{p}. Its SI unit is kg m2^2/s, equivalently J s, and its dimensional formula is [ML2T1][\mathrm{M L^2 T^{-1}}].

We write l\vec{l}, lower case, for a single particle, and reserve capital L\vec{L} for a whole system. Like torque, angular momentum is defined about a point and changes if you move that point.

Angular momentum geometry and a free particle keeping constant l

The same three readings

Everything said about the magnitude of τ\vec{\tau} transfers word for word, with F\vec{F} replaced by p\vec{p}:

l=rpsinθ=rp=rpl = r\,p \sin\theta = r_\perp\, p = r\, p_\perp

  • r=rsinθr_\perp = r\sin\theta is the perpendicular distance from OO to the line along which the particle is moving;
  • p=psinθp_\perp = p\sin\theta is the component of momentum at right angles to r\vec{r}.

Key Point — when l\vec{l} vanishes: l=0\vec{l} = 0 if the particle is at rest (p=0p = 0), or sits at the origin (r=0r = 0), or is moving directly towards or away from the origin (θ=0°\theta = 0° or 180°180°), so that the line of its motion passes through OO.

A particle going in a straight line has angular momentum

This surprises everybody, so meet it now. A particle moving at constant velocity along a straight line, with no forces on it at all, has a perfectly good, perfectly constant angular momentum about any point OO that is not on that line.

The reason is in the second reading. As the particle moves, rr grows and θ\theta shrinks, but the product rsinθr\sin\theta is just the perpendicular distance dd from OO to the line of motion — and that never changes. So

l=mvd=constantl = m v d = \text{constant}

and the direction of l\vec{l}, perpendicular to the fixed plane containing OO and the line, does not change either.

Key Point: Angular momentum does not require going round in a circle. It requires only that the particle's line of motion misses the point you are measuring about.

That result is not a curiosity — it is a consistency check on the whole framework. A free particle has no force on it, therefore no torque about OO, therefore its angular momentum about OO had better be constant. It is. The next block turns that "therefore" into an equation.

The Rotational Newton's Second Law: dldt=τ\dfrac{d\vec{l}}{dt} = \vec{\tau}

Force and momentum are tied together by F=dp/dt\vec{F} = d\vec{p}/dt. Torque and angular momentum are tied together in exactly the same way, and the proof takes four lines.

The derivation

Start from the definition and differentiate with respect to time, using the product rule (which holds for cross products, provided you keep the order of the factors):

dldt=ddt(r×p)=drdt×p  +  r×dpdt\frac{d\vec{l}}{dt} = \frac{d}{dt}\left(\vec{r} \times \vec{p}\right) = \frac{d\vec{r}}{dt} \times \vec{p} \;+\; \vec{r} \times \frac{d\vec{p}}{dt}

Look at the first term. dr/dtd\vec{r}/dt is the velocity v\vec{v}, and p=mv\vec{p} = m\vec{v}, so

drdt×p=v×mv=m(v×v)=0\frac{d\vec{r}}{dt} \times \vec{p} = \vec{v} \times m\vec{v} = m\,(\vec{v} \times \vec{v}) = 0

because the cross product of any vector with itself vanishes. The first term is gone.

In the second term, Newton's second law gives dp/dt=Fd\vec{p}/dt = \vec{F}, so

r×dpdt=r×F=τ\vec{r} \times \frac{d\vec{p}}{dt} = \vec{r} \times \vec{F} = \vec{\tau}

Putting the two together:

Key Point — the rotational analogue of Newton's second law: dldt=τ\frac{d\vec{l}}{dt} = \vec{\tau} The rate of change of a particle's angular momentum about a point equals the torque about that same point. Both must be taken about the same origin — mixing origins makes the statement false.

Set it beside its partner and the correspondence is exact:

Translation Rotation
F=dpdt\vec{F} = \dfrac{d\vec{p}}{dt} τ=dldt\vec{\tau} = \dfrac{d\vec{l}}{dt}
no net force \Rightarrow p\vec{p} constant no net torque \Rightarrow l\vec{l} constant

How to read the equation

The torque does not "cause rotation" in some vague sense. It does something sharper: it tells l\vec{l} which way to change, and how fast.

  • τ\vec{\tau} parallel to l\vec{l}: the angular momentum grows in length, direction unchanged.
  • τ\vec{\tau} antiparallel to l\vec{l}: it shrinks — braking.
  • τ\vec{\tau} perpendicular to l\vec{l}: the length of l\vec{l} does not change at all, but its direction swings. This is precisely what makes a spinning top precess instead of falling over, and a bicycle wheel held by one end of its axle turn slowly about that string rather than dropping.

The last case is worth pausing on, because it is the answer to a question that has probably bothered you since Section 1. Differentiate l2=lll^2 = \vec{l} \cdot \vec{l}:

ddt(l2)=2ldldt=2lτ\frac{d}{dt}(l^2) = 2\,\vec{l} \cdot \frac{d\vec{l}}{dt} = 2\,\vec{l} \cdot \vec{\tau}

so the magnitude of l\vec{l} changes only through the component of τ\vec{\tau} along l\vec{l}. A perpendicular torque redirects, it does not speed up.

[JEE Tip] Whenever a problem says "the angular momentum is constant in magnitude but changing in direction", it is telling you τl=0\vec{\tau} \cdot \vec{l} = 0. That is often the fastest way in.

From One Particle to a Whole Body: dLdt=τext\dfrac{d\vec{L}}{dt} = \vec{\tau}_{ext}

A rigid body is a system of particles, so add up.

L=l1+l2++ln=iri×pi\vec{L} = \vec{l}_1 + \vec{l}_2 + \dots + \vec{l}_n = \sum_i \vec{r}_i \times \vec{p}_i

That is the total angular momentum of the system about the chosen origin. Differentiating term by term and using the single-particle result on each,

dLdt=idlidt=iτi=iri×Fi\frac{d\vec{L}}{dt} = \sum_i \frac{d\vec{l}_i}{dt} = \sum_i \vec{\tau}_i = \sum_i \vec{r}_i \times \vec{F}_i

Now the crucial step. The force Fi\vec{F}_i on particle ii is partly external (gravity, a push, a string from outside) and partly internal (the forces the other particles of the system exert on it). Split the total torque to match:

τ=τext+τint\vec{\tau} = \vec{\tau}_{ext} + \vec{\tau}_{int}

Why the internal torques cancel

Take any two particles ii and jj. By Newton's third law the forces they exert on each other are equal and opposite: Fji=Fij\vec{F}_{ji} = -\vec{F}_{ij}. Their combined torque about the origin is

ri×Fij+rj×Fji=ri×Fijrj×Fij=(rirj)×Fij\vec{r}_i \times \vec{F}_{ij} + \vec{r}_j \times \vec{F}_{ji} = \vec{r}_i \times \vec{F}_{ij} - \vec{r}_j \times \vec{F}_{ij} = (\vec{r}_i - \vec{r}_j) \times \vec{F}_{ij}

Here comes the extra assumption. Newton's third law by itself only says the two forces are equal and opposite. We now assume something slightly stronger, and true of every force in this chapter:

Key Point — the central-force assumption: The internal forces between two particles act along the line joining them. Such forces are called central.

If Fij\vec{F}_{ij} lies along the line joining the particles, then it is parallel to rirj\vec{r}_i - \vec{r}_j, which is exactly the vector along that line. The cross product of parallel vectors is zero, so the pair contributes nothing. Every internal pair cancels the same way, so τint=0\vec{\tau}_{int} = 0 and

Internal force pair cancelling, and a central force keeping L constant

Key Point — the equation of rotational motion for a system: dLdt=τext\frac{d\vec{L}}{dt} = \vec{\tau}_{ext} The rate of change of the total angular momentum of a system about a point equals the total external torque about that same point. Internal forces cannot change L\vec{L}, however violent they are.

This is the exact rotational twin of dP/dt=Fextd\vec{P}/dt = \vec{F}_{ext} from Section 3, and it holds for any system of particles — a rigid body, a cloud of gas, an exploding shell — not just for bodies that hold their shape.

Conservation of angular momentum

Set the external torque to zero and the law falls out.

Key Point — conservation of angular momentum: If the total external torque on a system is zero, then dLdt=0L=constant\frac{d\vec{L}}{dt} = 0 \qquad \Rightarrow \qquad \vec{L} = \text{constant} Because this is a vector equation, it is really three separate statements: Lx=constant,Ly=constant,Lz=constantL_x = \text{constant}, \qquad L_y = \text{constant}, \qquad L_z = \text{constant} and each component is conserved separately.

That last point is more useful than it looks. If the external torque has zero component along one particular axis — even though it is not zero overall — then the angular momentum about that axis is still conserved. Many problems turn on exactly this partial conservation.

L\vec{L} constant while p\vec{p} is not

The two conservation laws are independent, and it is worth seeing a case where one holds and the other does not.

Consider a planet or comet orbiting a star. The gravitational pull is always directed straight at the star, so about the star

τ=r×F=0since F is parallel to r\vec{\tau} = \vec{r} \times \vec{F} = 0 \qquad \text{since } \vec{F} \text{ is parallel to } \vec{r}

Therefore L\vec{L} about the star is constant — fixed in magnitude and fixed in direction, which is why the orbit stays in one plane for ever. Meanwhile the linear momentum p\vec{p} is changing continuously: the force is not zero, so p\vec{p} swings round and its magnitude rises and falls as the comet comes in and goes out. At the two ends of the orbit, where r\vec{r} and v\vec{v} are perpendicular,

r1p1=r2p2r1v1=r2v2r_1 p_1 = r_2 p_2 \qquad \Rightarrow \qquad r_1 v_1 = r_2 v_2

so the comet races through its close approach and crawls at its far point. That is Kepler's law of equal areas, and it is nothing but conservation of angular momentum.

System P\vec{P} conserved? L\vec{L} conserved?
comet orbiting a star (about the star) no, gravity is an external force yes, the force is central so the torque is zero
two skaters pushing off each other on ice yes, no external horizontal force yes, no external torque either
a ball falling freely (about a point on its own line of fall) no, weight acts yes, the line of action passes through the point
a ball falling freely (about a point to one side) no no, the weight has a moment arm

[JEE Tip] Read the last two rows together. Whether L\vec{L} is conserved depends on which point you chose. Always name the point before you claim conservation.

Section 10 takes this law and specialises it to rotation about a fixed axis, where it becomes the rule that makes a spinning skater speed up the instant she pulls her arms in. Section 7 takes the case τext=0\vec{\tau}_{ext} = 0 and Fext=0\vec{F}_{ext} = 0 and calls it equilibrium.

Solved Examples

Every cross product below has been recomputed with a vector library and checked twice over — that the answer is perpendicular to both inputs, and that its length really is absinθab\sin\theta. Where a rate of change is claimed, it was obtained by differentiating the actual trajectory numerically. g=10g = 10 m/s2^2 is used in Example 7 and nowhere else in this section.

Example 1: Torque in component form

A force F=7i^+3j^5k^\vec{F} = 7\hat{i} + 3\hat{j} - 5\hat{k} N acts on a particle whose position vector is r=i^j^+k^\vec{r} = \hat{i} - \hat{j} + \hat{k} m. Find the torque of this force about the origin, and its magnitude.

Solution:

  1. Set up the determinant. τ=r×F=i^j^k^111735\vec{\tau} = \vec{r} \times \vec{F} = \begin{vmatrix} \hat{i} & \hat{j} & \hat{k} \\ 1 & -1 & 1 \\ 7 & 3 & -5 \end{vmatrix}

  2. Expand along the top row. τ=i^[(1)(5)(1)(3)]j^[(1)(5)(1)(7)]+k^[(1)(3)(1)(7)]\vec{\tau} = \hat{i}\,[(-1)(-5) - (1)(3)] - \hat{j}\,[(1)(-5) - (1)(7)] + \hat{k}\,[(1)(3) - (-1)(7)] =i^[53]j^[57]+k^[3+7]= \hat{i}\,[5 - 3] - \hat{j}\,[-5 - 7] + \hat{k}\,[3 + 7] τ=2i^+12j^+10k^ N m\vec{\tau} = 2\hat{i} + 12\hat{j} + 10\hat{k} \text{ N m}

  3. Magnitude. τ=22+122+102=4+144+100=24815.7 N m|\vec{\tau}| = \sqrt{2^2 + 12^2 + 10^2} = \sqrt{4 + 144 + 100} = \sqrt{248} \approx 15.7 \text{ N m}

  4. Two free checks. The answer must be perpendicular to both inputs: τr=212+10=0,τF=14+3650=0\vec{\tau} \cdot \vec{r} = 2 - 12 + 10 = 0, \qquad \vec{\tau} \cdot \vec{F} = 14 + 36 - 50 = 0 Both zero, so the arithmetic is sound.

Final Answer: τ=2i^+12j^+10k^\vec{\tau} = 2\hat{i} + 12\hat{j} + 10\hat{k} N m, of magnitude about 15.7 N m.

Takeaway: Always run the two dot products. They cost ten seconds and catch nearly every sign slip in a 3×33 \times 3 determinant. [Board Important] Write the unit as N m, never as a joule.

Example 2: One spanner, three readings

A spanner 0.25 m long turns a nut at OO. A force of 60 N is applied at the far end of the spanner, at 30°30° to the spanner's length. Find the torque about the nut three different ways, and check that they agree.

Solution:

  1. Reading 1 — magnitudes and the angle. τ=rFsinθ=0.25×60×sin30°=0.25×60×0.5=7.5 N m\tau = rF\sin\theta = 0.25 \times 60 \times \sin 30° = 0.25 \times 60 \times 0.5 = 7.5 \text{ N m}

  2. Reading 2 — the moment arm. Extend the line along which the force acts and drop a perpendicular on to it from OO: r=rsinθ=0.25×0.5=0.125 mr_\perp = r\sin\theta = 0.25 \times 0.5 = 0.125 \text{ m} τ=rF=0.125×60=7.5 N m\tau = r_\perp F = 0.125 \times 60 = 7.5 \text{ N m}

  3. Reading 3 — the useful component. Split the 60 N at the point of application: F=Fsinθ=60×0.5=30 N(the turning part)F_\perp = F\sin\theta = 60 \times 0.5 = 30 \text{ N} \quad \text{(the turning part)} F=Fcosθ=60×0.86652 N(pulls along the spanner, turns nothing)F_\parallel = F\cos\theta = 60 \times 0.866 \approx 52 \text{ N} \quad \text{(pulls along the spanner, turns nothing)} τ=rF=0.25×30=7.5 N m\tau = r F_\perp = 0.25 \times 30 = 7.5 \text{ N m}

  4. What would be better. Pulling at 90°90° instead would give τ=0.25×60=15\tau = 0.25 \times 60 = 15 N m — double, for the same effort.

Final Answer: 7.5 N m by all three routes; pulling at right angles would double it to 15 N m.

Takeaway: Most of a slanted force is wasted. At 30°30° only half of the 60 N does any turning; the other 52 N simply tries to pull the spanner off the nut. That is why you are told to pull a spanner square.

Example 3: The same force, two different points

A force F=20j^\vec{F} = 20\hat{j} N acts at the point PP whose position vector is 3i^3\hat{i} m. Find the torque of this force (a) about the origin OO, (b) about the point AA at 5i^5\hat{i} m, and (c) find every point about which this force has zero torque.

Solution:

  1. (a) About OO. The position vector of PP from OO is 3i^3\hat{i}: τO=(3i^)×(20j^)=60(i^×j^)=60k^ N m\vec{\tau}_O = (3\hat{i}) \times (20\hat{j}) = 60\,(\hat{i} \times \hat{j}) = 60\hat{k} \text{ N m} Anticlockwise as seen from the +z+z side.

  2. (b) About AA. Now the position vector of PP is measured from AA: r=3i^5i^=2i^ m\vec{r}^{\,\prime} = 3\hat{i} - 5\hat{i} = -2\hat{i} \text{ m} τA=(2i^)×(20j^)=40k^ N m\vec{\tau}_A = (-2\hat{i}) \times (20\hat{j}) = -40\hat{k} \text{ N m} Smaller, and clockwise — the opposite sense.

  3. Check with the shifting rule. With d=5i^\vec{d} = 5\hat{i}, τA=τOd×F=60k^(5i^×20j^)=60k^100k^=40k^ N m\vec{\tau}_A = \vec{\tau}_O - \vec{d} \times \vec{F} = 60\hat{k} - (5\hat{i} \times 20\hat{j}) = 60\hat{k} - 100\hat{k} = -40\hat{k} \text{ N m} Agreement.

  4. (c) Zero torque. The torque vanishes about any point on the line of action of the force — the vertical line x=3x = 3 m. About a point on that line the moment arm is zero.

Final Answer: (a) 60k^60\hat{k} N m; (b) 40k^-40\hat{k} N m; (c) every point on the line x=3x = 3 m.

Takeaway: "The torque of this force" is not a complete phrase. Until you name the point, the question has no answer — and moving the point can even flip the sense. [JEE Tip] Write "about OO" or "about the hinge" in the first line of every torque solution.

Example 4: Net torque on a hinged rod

A light rod lies along the xx-axis, hinged at the origin. Three forces act on it, all in the xyxy-plane: 10 N in the y-y direction at x=1x = 1 m; 15 N in the +y+y direction at x=3x = 3 m; and 8 N in the +x+x direction at x=4x = 4 m. Find the net torque about the hinge, and say which way the rod starts to turn.

Solution:

  1. Fix the sign convention. Anticlockwise (along +k^+\hat{k}) is positive.

  2. The 10 N force. Moment arm 1 m, force downward, so it turns the rod clockwise: τ1=(1)(10)=10 N m\tau_1 = -(1)(10) = -10 \text{ N m}

  3. The 15 N force. Moment arm 3 m, force upward, anticlockwise: τ2=+(3)(15)=+45 N m\tau_2 = +(3)(15) = +45 \text{ N m}

  4. The 8 N force. It acts along the rod, so its line of action runs straight through the hinge. Moment arm zero: τ3=0\tau_3 = 0

  5. Add. τnet=10+45+0=+35 N m\tau_{net} = -10 + 45 + 0 = +35 \text{ N m}

Final Answer: 35 N m anticlockwise; the rod begins to turn anticlockwise about the hinge.

Takeaway: A force along the rod does nothing to turn it, no matter how large — it is taken entirely by the hinge. This is exactly the door pushed towards its hinges. [NEET Important] Set the sign convention down in writing before you add anything.

Example 5: Angular momentum of a particle, in components

A particle of mass 2 kg is at r=2i^j^\vec{r} = 2\hat{i} - \hat{j} m, moving with velocity v=3i^+4j^\vec{v} = 3\hat{i} + 4\hat{j} m/s. Find its angular momentum about the origin, and verify the answer using the perpendicular distance.

Solution:

  1. Momentum first. p=mv=2(3i^+4j^)=6i^+8j^ kg m/s,p=36+64=10 kg m/s\vec{p} = m\vec{v} = 2(3\hat{i} + 4\hat{j}) = 6\hat{i} + 8\hat{j} \text{ kg m/s}, \qquad |\vec{p}| = \sqrt{36 + 64} = 10 \text{ kg m/s}

  2. The cross product. Both vectors lie in the xyxy-plane, so only the k^\hat{k} term survives: l=r×p=i^j^k^210680=k^[(2)(8)(1)(6)]=22k^ kg m2/s\vec{l} = \vec{r} \times \vec{p} = \begin{vmatrix} \hat{i} & \hat{j} & \hat{k} \\ 2 & -1 & 0 \\ 6 & 8 & 0 \end{vmatrix} = \hat{k}\,[(2)(8) - (-1)(6)] = 22\hat{k} \text{ kg m}^2\text{/s}

  3. Verify with l=rpl = r_\perp p. The perpendicular distance from the origin to the line along which the particle moves is r=r×pp=2210=2.2 mr_\perp = \frac{|\vec{r} \times \vec{p}|}{|\vec{p}|} = \frac{22}{10} = 2.2 \text{ m} and then l=rp=2.2×10=22l = r_\perp p = 2.2 \times 10 = 22 kg m2^2/s. Consistent.

Final Answer: l=22k^\vec{l} = 22\hat{k} kg m2^2/s, out of the page; the line of motion misses the origin by 2.2 m.

Takeaway: For any planar problem, only the k^\hat{k} component of r×p\vec{r} \times \vec{p} survives, and it is just lz=m(xvyyvx)l_z = m(x v_y - y v_x). Memorise that one line — it turns most two-dimensional angular momentum questions into a single subtraction.

Example 6: A free particle keeps its angular momentum

A particle of mass 0.5 kg moves in a straight line at a constant 4 m/s along the line y=3y = 3 m, in the +x+x direction. Show that its angular momentum about the origin is the same at x=0x = 0, x=4x = 4 m and x=8x = 8 m, and explain why that had to happen.

Solution:

  1. The momentum is the same everywhere: p=0.5×4i^=2i^\vec{p} = 0.5 \times 4\,\hat{i} = 2\hat{i} kg m/s.

  2. Compute lz=m(xvyyvx)l_z = m(x v_y - y v_x) at each place. Here vy=0v_y = 0 and vx=4v_x = 4, so lz=myvx=(0.5)(3)(4)=6l_z = -m y v_x = -(0.5)(3)(4) = -6 kg m2^2/s.

  • At x=0x = 0: lz=6l_z = -6

  • At x=4x = 4: lz=6l_z = -6

  • At x=8x = 8: lz=6l_z = -6

    The xx-coordinate never enters, so the value cannot change.

  1. The geometric reason. Use l=rpl = r_\perp p. The perpendicular distance from the origin to the line of motion is d=3d = 3 m, whatever the particle's position along that line. So l=mvd=0.5×4×3=6 kg m2/sl = m v d = 0.5 \times 4 \times 3 = 6 \text{ kg m}^2\text{/s} constant. As the particle moves away, rr grows and θ\theta shrinks in exactly compensating proportion.

  2. The dynamical reason, which is the real one. No force acts on the particle, so the torque about the origin is zero, so dl/dt=0d\vec{l}/dt = 0. Angular momentum must be conserved; the geometry above is just that law seen from the side.

Final Answer: l=6k^\vec{l} = -6\hat{k} kg m2^2/s at every point, that is 6 kg m2^2/s into the page; it is constant because there is no torque about the origin.

Takeaway: A particle does not have to orbit anything to have angular momentum. It only has to miss the point you are measuring about. [JEE Tip] If a question asks for the angular momentum of a particle moving in a straight line, find the perpendicular distance from the point to the line and multiply by mvmv. Do not attempt any geometry beyond that.

Example 7: A projectile, and a direct test of dl/dt=τd\vec{l}/dt = \vec{\tau}

A 1 kg ball is thrown from the origin with velocity 10i^+20j^10\hat{i} + 20\hat{j} m/s. Taking g=10g = 10 m/s2^2, find its angular momentum about the launch point at t=2t = 2 s, find the torque of gravity about the same point at that instant, and verify that one is the rate of change of the other.

Solution:

  1. Write the motion. r(t)=10ti^+(20t5t2)j^,v(t)=10i^+(2010t)j^\vec{r}(t) = 10t\,\hat{i} + (20t - 5t^2)\,\hat{j}, \qquad \vec{v}(t) = 10\hat{i} + (20 - 10t)\,\hat{j}

  2. At t=2t = 2 s. r=20i^+(4020)j^=20i^+20j^ m,v=10i^+0j^ m/s\vec{r} = 20\hat{i} + (40 - 20)\hat{j} = 20\hat{i} + 20\hat{j} \text{ m}, \qquad \vec{v} = 10\hat{i} + 0\hat{j} \text{ m/s} (The ball is at the top of its flight, moving horizontally.)

  3. Angular momentum, using lz=m(xvyyvx)l_z = m(x v_y - y v_x): lz=1[(20)(0)(20)(10)]=200 kg m2/sl_z = 1\,[(20)(0) - (20)(10)] = -200 \text{ kg m}^2\text{/s}

  4. Torque of gravity about the launch point. The weight is W=10j^\vec{W} = -10\hat{j} N acting at r\vec{r}: τz=xWyyWx=(20)(10)(20)(0)=200 N m\tau_z = x W_y - y W_x = (20)(-10) - (20)(0) = -200 \text{ N m}

  5. Now verify the law. In general lz(t)=m[xvyyvx]=10t(2010t)(20t5t2)(10)=200t100t2200t+50t2=50t2l_z(t) = m\,[x v_y - y v_x] = 10t(20 - 10t) - (20t - 5t^2)(10) = 200t - 100t^2 - 200t + 50t^2 = -50t^2 dlzdt=100t\frac{dl_z}{dt} = -100t and the torque at time tt is τz=xWy=(10t)(10)=100t\tau_z = x W_y = (10t)(-10) = -100t. They match at every instant, and at t=2t = 2 s both equal 200-200.

Final Answer: lz=200l_z = -200 kg m2^2/s and τz=200\tau_z = -200 N m at t=2t = 2 s; and dlz/dt=100t=τzdl_z/dt = -100t = \tau_z throughout the flight.

Takeaway: Notice that lz=50t2l_z = -50t^2 grows all through the flight even though the ball starts with zero angular momentum — gravity keeps supplying torque. [JEE Tip] In projectile questions the torque of gravity about the launch point is simply mgx-mgx, so the angular momentum is easiest to get by integrating that, not by re-doing the cross product each time.

Example 8: Circular motion, seen from two different points

A particle of mass 0.2 kg moves in a horizontal circle of radius 0.5 m at a steady speed of 3 m/s. Find its angular momentum (a) about the centre of the circle and (b) about a point QQ lying in the same plane, 2 m from the centre. In which case is l\vec{l} constant?

Solution:

  1. (a) About the centre. Here r\vec{r} and v\vec{v} are always perpendicular, so sinθ=1\sin\theta = 1: l=mvr=0.2×3×0.5=0.30 kg m2/sl = m v r = 0.2 \times 3 \times 0.5 = 0.30 \text{ kg m}^2\text{/s} Its direction is along the axis of the circle, and it never changes. So about the centre, l\vec{l} is constant in magnitude and direction.

  2. Why that is consistent. The force keeping the particle on the circle points at the centre. About the centre its moment arm is zero, so τ=0\vec{\tau} = 0 and l\vec{l} must be constant.

  3. (b) About QQ. Put the centre at the origin and QQ at (2,0)(-2, 0). When the particle is at angle ϕ\phi its position relative to QQ is (0.5cosϕ+2,  0.5sinϕ)(0.5\cos\phi + 2,\; 0.5\sin\phi) and its velocity is 3(sinϕ,cosϕ)3(-\sin\phi, \cos\phi). Then lz=m[xvyyvx]=0.2[(0.5cosϕ+2)(3cosϕ)+1.5sin2ϕ]=0.2[1.5+6cosϕ]l_z = m\,[x v_y - y v_x] = 0.2\,[(0.5\cos\phi + 2)(3\cos\phi) + 1.5\sin^2\phi] = 0.2\,[1.5 + 6\cos\phi] lz=0.30+1.20cosϕl_z = 0.30 + 1.20\cos\phi

  4. Read it. This swings between 0.30+1.20=1.500.30 + 1.20 = 1.50 and 0.301.20=0.900.30 - 1.20 = -0.90 kg m2^2/s. It is not constant, and it even changes sign. About QQ the centre-directed force does have a moment arm, so there is a torque, and l\vec{l} obediently changes.

Final Answer: (a) 0.30 kg m2^2/s, constant; (b) 0.30+1.20cosϕ0.30 + 1.20\cos\phi kg m2^2/s, varying between 0.90-0.90 and 1.501.50 and therefore not conserved.

Takeaway: Conservation of angular momentum is a statement about a chosen point, not about the motion. The very same particle in the very same circle has a conserved l\vec{l} about one point and a wildly varying l\vec{l} about another.

Example 9: Zero momentum, non-zero angular momentum

Two particles, each of mass 1 kg, are at (0,1)(0, 1) m and (0,1)(0, -1) m. The first moves with velocity 4i^4\hat{i} m/s and the second with 4i^-4\hat{i} m/s. Find the total linear momentum and the total angular momentum about the origin. Then find the total angular momentum about the point (7,3)(7, -3) m.

Solution:

  1. Total linear momentum. P=1(4i^)+1(4i^)=0\vec{P} = 1(4\hat{i}) + 1(-4\hat{i}) = 0 The system as a whole is going nowhere: its centre of mass is at rest.

  2. Angular momentum about the origin, particle by particle, using lz=m(xvyyvx)l_z = m(x v_y - y v_x): l1z=1[(0)(0)(1)(4)]=4 kg m2/sl_{1z} = 1\,[(0)(0) - (1)(4)] = -4 \text{ kg m}^2\text{/s} l2z=1[(0)(0)(1)(4)]=4 kg m2/sl_{2z} = 1\,[(0)(0) - (-1)(-4)] = -4 \text{ kg m}^2\text{/s} Lz=44=8 kg m2/sL_z = -4 - 4 = -8 \text{ kg m}^2\text{/s} Both contributions have the same sign, because the two particles are turning the same way round the origin.

  3. About (7,3)(7, -3) m. Shift both position vectors: particle 1 is now at (7,4)(-7, 4) and particle 2 at (7,2)(-7, 2). l1z=1[(7)(0)(4)(4)]=16,l2z=1[(7)(0)(2)(4)]=+8l_{1z} = 1\,[(-7)(0) - (4)(4)] = -16, \qquad l_{2z} = 1\,[(-7)(0) - (2)(-4)] = +8 Lz=16+8=8 kg m2/sL_z = -16 + 8 = -8 \text{ kg m}^2\text{/s} The same answer.

  4. Why the shift made no difference. Moving the origin by d\vec{d} changes L\vec{L} by d×P-\vec{d} \times \vec{P}, and here P=0\vec{P} = 0.

Final Answer: P=0\vec{P} = 0 but L=8k^\vec{L} = -8\hat{k} kg m2^2/s; and because P=0\vec{P} = 0, that value of L\vec{L} is the same about every point.

Takeaway: Zero total momentum does not mean zero total angular momentum. A system can be spinning furiously while going nowhere — which is exactly what a flywheel does. [JEE Tip] When the total momentum of a system is zero, its angular momentum is origin-independent. That is a genuine shortcut, and it is why the centre-of-mass frame is so convenient.

Example 10: A comet, where L\vec{L} holds and p\vec{p} does not

A comet moving round a star is 1.0×10111.0 \times 10^{11} m from it at closest approach, travelling at 4.0×1044.0 \times 10^4 m/s. At its farthest point it is 2.0×10112.0 \times 10^{11} m away. Find its speed there. What happens to its linear momentum along the way?

Solution:

  1. Identify the conserved quantity. Gravity always pulls the comet straight towards the star, so F\vec{F} is parallel to r\vec{r} and τ=r×F=0about the star\vec{\tau} = \vec{r} \times \vec{F} = 0 \quad \text{about the star} With no external torque about the star, L\vec{L} about the star is constant.

  2. Use the simple form at the two ends. At closest approach and at the farthest point the velocity is perpendicular to the radius, so sinθ=1\sin\theta = 1 and l=mvrl = mvr at both: mv1r1=mv2r2m v_1 r_1 = m v_2 r_2

  3. Solve. v2=v1r1r2=4.0×104×1.0×10112.0×1011=2.0×104 m/sv_2 = v_1 \frac{r_1}{r_2} = 4.0 \times 10^4 \times \frac{1.0 \times 10^{11}}{2.0 \times 10^{11}} = 2.0 \times 10^4 \text{ m/s}

  4. What linear momentum does. Its magnitude halves, from m(4.0×104)m(4.0 \times 10^4) to m(2.0×104)m(2.0 \times 10^4), and its direction turns through 180°180° between the two ends. Linear momentum is not conserved at all — gravity is a large external force. Angular momentum is conserved because that force has no moment about the star.

Final Answer: 2.0×1042.0 \times 10^4 m/s at the far point; p|\vec{p}| halves and swings right round, while L\vec{L} does not change by a hair.

Takeaway: A central force conserves angular momentum and destroys the conservation of linear momentum. Doubling the distance halves the speed — the comet sprints past the star and crawls at the far end. This is Kepler's second law in one line. [NEET Important] The condition is that the force points at the chosen point, not that the force is small.

Example 11: Why internal forces never appear

Two particles of a system sit at ri=i^+2j^\vec{r}_i = \hat{i} + 2\hat{j} m and rj=4i^+6j^\vec{r}_j = 4\hat{i} + 6\hat{j} m. They attract each other along the line joining them with a force of 5 N. Show explicitly that this internal pair contributes nothing to the total torque about the origin.

Solution:

  1. Find the line joining them. rjri=3i^+4j^,rjri=9+16=5 m\vec{r}_j - \vec{r}_i = 3\hat{i} + 4\hat{j}, \qquad |\vec{r}_j - \vec{r}_i| = \sqrt{9 + 16} = 5 \text{ m} so the unit vector from ii towards jj is u^=0.6i^+0.8j^\hat{u} = 0.6\hat{i} + 0.8\hat{j}.

  2. Write the two forces. Particle ii is pulled towards jj: Fij=5u^=3i^+4j^ N,Fji=3i^4j^ N\vec{F}_{ij} = 5\hat{u} = 3\hat{i} + 4\hat{j} \text{ N}, \qquad \vec{F}_{ji} = -3\hat{i} - 4\hat{j} \text{ N}

  3. Torque on particle ii about the origin. τiz=(1)(4)(2)(3)=46=2 N m\tau_{iz} = (1)(4) - (2)(3) = 4 - 6 = -2 \text{ N m}

  4. Torque on particle jj. τjz=(4)(4)(6)(3)=16+18=+2 N m\tau_{jz} = (4)(-4) - (6)(-3) = -16 + 18 = +2 \text{ N m}

  5. Add. τiz+τjz=2+2=0\tau_{iz} + \tau_{jz} = -2 + 2 = 0

  6. The general reason, in one line. ri×Fij+rj×(Fij)=(rirj)×Fij=0\vec{r}_i \times \vec{F}_{ij} + \vec{r}_j \times (-\vec{F}_{ij}) = (\vec{r}_i - \vec{r}_j) \times \vec{F}_{ij} = 0 because Fij\vec{F}_{ij} lies along rirj\vec{r}_i - \vec{r}_j, and parallel vectors have zero cross product. Nothing about the choice of origin entered, so the cancellation holds about every point.

Final Answer: the two torques are 2-2 N m and +2+2 N m; they sum to zero, about the origin and about any other point.

Takeaway: This is why dL/dt=τextd\vec{L}/dt = \vec{\tau}_{ext} works. Notice what the proof actually needs: not merely that the forces are equal and opposite, but that they act along the line joining the particles. Newton's third law alone would not be enough.

Example 12: A torque that turns l\vec{l} without changing its size

A 3 kg particle is at r=2i^\vec{r} = 2\hat{i} m with velocity v=5j^\vec{v} = 5\hat{j} m/s, and a force F=6k^\vec{F} = 6\hat{k} N acts on it. Find l\vec{l} and τ\vec{\tau} about the origin, and describe how l\vec{l} is changing at this instant.

Solution:

  1. Angular momentum. p=3(5j^)=15j^\vec{p} = 3(5\hat{j}) = 15\hat{j} kg m/s, so l=(2i^)×(15j^)=30(i^×j^)=30k^ kg m2/s\vec{l} = (2\hat{i}) \times (15\hat{j}) = 30\,(\hat{i} \times \hat{j}) = 30\hat{k} \text{ kg m}^2\text{/s}

  2. Torque. τ=(2i^)×(6k^)=12(i^×k^)=12j^ N m\vec{\tau} = (2\hat{i}) \times (6\hat{k}) = 12\,(\hat{i} \times \hat{k}) = -12\hat{j} \text{ N m} (using i^×k^=j^\hat{i} \times \hat{k} = -\hat{j}).

  3. Compare their directions. τl=(12j^)(30k^)=0\vec{\tau} \cdot \vec{l} = (-12\hat{j}) \cdot (30\hat{k}) = 0 They are perpendicular.

  4. Read the physics. Since ddt(l2)=2lτ=0\dfrac{d}{dt}(l^2) = 2\,\vec{l} \cdot \vec{\tau} = 0, the magnitude of l\vec{l} is momentarily unchanging: it stays at 30 kg m2^2/s. But l\vec{l} itself is changing at the rate dl/dt=12j^d\vec{l}/dt = -12\hat{j}, so its direction is swinging — the vector is tipping from k^\hat{k} towards j^-\hat{j} at 1212 units per second.

Final Answer: l=30k^\vec{l} = 30\hat{k} kg m2^2/s and τ=12j^\vec{\tau} = -12\hat{j} N m; the two are perpendicular, so l|\vec{l}| is constant while the direction of l\vec{l} turns.

Takeaway: A torque perpendicular to the angular momentum steers it instead of speeding it up — precisely the mechanism behind a precessing top and a gyroscope. [JEE Tip] Any time you are told L|\vec{L}| is constant but L\vec{L} is not, you are being told τL=0\vec{\tau} \cdot \vec{L} = 0.