Angular Impulse-Angular Momentum Theorem (Integral): Time-Varying Torque

By Vegard Gjerde Based on Masterful Learning 12 min read
angular-impulse angular-momentum torque rotation classical-mechanics physics learning-strategies

The Angular Impulse-Angular Momentum Theorem (Integral) states that the change in angular momentum of a system equals the time integral of the net torque acting on it: ΔL=titfτnet(t)dt\Delta\vec{L} = \int_{t_i}^{t_f} \vec{\tau}_{\mathrm{net}}(t)\,dt. This form applies when torque varies with time, requiring integration over the interval to find the cumulative rotational effect. Mastering it requires elaboration, retrieval practice, self-explanation, and problem solving—core strategies in the Unisium Study System.

When net torque changes throughout a motion—a door slowing under friction, a turbine ramping down, or a diver’s angular momentum shifting mid-twist—you cannot use the simpler constant-torque form. The integral form accounts for every instant where torque varies, summing the rotational impulse over time to predict the final angular momentum.

Unisium hero image titled Angular Impulse-Angular Momentum Theorem (Integral) showing the principle equation and conditions card.
The angular impulse-momentum relation ΔL=titfτnet(t)dt\Delta\vec{L} = \int_{t_i}^{t_f} \vec{\tau}_{\mathrm{net}}(t)\,dt for time-varying net torque in an inertial frame.

On this page: The Principle | Conditions | Misconceptions | EE Questions | Retrieval Practice | Worked Example | Solve a Problem | FAQ


The Principle

Statement

The change in angular momentum of a system between two instants equals the time integral of the net torque acting on the system over that interval. This is the general form that applies regardless of whether torque is constant or time-varying.

Mathematical Form

ΔL=titfτnet(t)dt\Delta\vec{L} = \int_{t_i}^{t_f} \vec{\tau}_{\mathrm{net}}(t)\,dt

Where:

  • ΔL=LfLi\Delta\vec{L} = \vec{L}_f - \vec{L}_i = change in angular momentum (kgm2/s\mathrm{kg\cdot m^2/s})
  • τnet(t)\vec{\tau}_{\mathrm{net}}(t) = net torque as a function of time (Nm\mathrm{N\cdot m})
  • ti,tft_i, t_f = initial and final times defining the interval (s\mathrm{s})
  • The integral accumulates the rotational effect of torque over the entire interval

Alternative Forms

In different contexts, this appears as:

  • Scalar (fixed axis): ΔL=titfτnet(t)dt\Delta L = \int_{t_i}^{t_f} \tau_{\mathrm{net}}(t)\,dt (for rotation about a single axis with signed torque)
  • Constant torque special case: ΔL=τnetΔt\Delta\vec{L} = \vec{\tau}_{\mathrm{net}}\,\Delta t (when torque is constant over the interval; this is the simpler angular impulse form)

Conditions of Applicability

Condition: inertial; τnet(t)\vec{\tau}_{\mathrm{net}}(t); interval specified

Practical modeling notes

  • Inertial reference frame: The theorem assumes measurements are made in a non-accelerating frame. In a rotating or accelerating frame, fictitious torques appear.
  • Time-varying torque: This form is necessary when net torque changes during the motion (e.g., friction torque that depends on angular speed, or external forces that vary in time).
  • Interval specified: You must integrate over a defined time interval [ti,tf][t_i, t_f]. If the torque function is unknown or discontinuous, the integral may not be tractable analytically.

When It’s Not Directly Usable

  • Non-inertial frames: In accelerating or rotating frames, you must account for fictitious torques (centrifugal, Coriolis) before applying the theorem.
  • Unknown torque function: If τ(t)\tau(t) isn’t known, you can’t compute the integral from first principles—you need a torque-time graph, measurements, or a model that links τ\tau to ω\omega or other state variables.
  • No net torque: If τnet=0\vec{\tau}_{\mathrm{net}} = 0 for the entire interval, angular momentum is conserved and the integral is trivially zero.

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Common Misconceptions

Misconception 1: “Integration is only needed for complicated torque functions”

The truth: The integral form is the general statement of the theorem. Even when torque is constant, the result τnetΔt\vec{\tau}_{\mathrm{net}}\,\Delta t comes from evaluating the integral titfτnetdt\int_{t_i}^{t_f} \vec{\tau}_{\mathrm{net}}\,dt with τnet\vec{\tau}_{\mathrm{net}} as a constant.

Why this matters: Recognizing the integral form as fundamental helps you understand that the constant-torque version is a special case, not a separate principle. When you encounter time-dependent torque, you know immediately to integrate.

Misconception 2: “You always need an explicit function τ(t)\tau(t) to use this theorem”

The truth: You can evaluate the integral using graphical methods (area under a torque-time curve), average torque approximation, or by solving the differential equation when τ\tau depends on ω\omega or other state variables.

Why this matters: Students sometimes abandon the theorem when τ(t)\tau(t) is not given explicitly, missing opportunities to use graphical reasoning, approximation methods, or kinematic constraints.

Misconception 3: “Angular momentum is always conserved if no external forces act”

The truth: For a system, total angular momentum is conserved when net external torque is zero. Internal forces (action-reaction pairs) redistribute angular momentum among parts but do not change the system total.

Why this matters: Confusing external forces with external torques leads to errors. A skater pulling in their arms has no external torque, so total angular momentum is conserved even though internal forces do work and change rotational kinetic energy.


Elaborative Encoding

Use these questions to build deep understanding. (See Elaborative Encoding for the full method.)

Within the Principle

  • Why does the theorem involve an integral rather than just multiplying torque by elapsed time?
  • What does the vector nature of τnet(t)\vec{\tau}_{\mathrm{net}}(t) and ΔL\Delta\vec{L} tell you about three-dimensional rotations?

For the Principle

  • How do you decide whether torque is varying enough with time to require explicit integration, versus treating it as approximately constant?
  • If you know the angular momentum at two instants but not the torque function, can you still use this theorem? What information would you extract?

Between Principles

  • How does this integral form relate to the linear impulse-momentum theorem Δp=titfFnet(t)dt\Delta\vec{p} = \int_{t_i}^{t_f} \vec{F}_{\mathrm{net}}(t)\,dt?

Generate an Example

  • Describe a realistic scenario where net torque varies smoothly with time (not a sudden impulse), requiring you to integrate to find the change in angular momentum.

Retrieval Practice

Answer from memory, then click to reveal and check. (See Retrieval Practice for the full method.)

State the angular impulse-momentum theorem (integral form) in words: _____The change in angular momentum of a system equals the time integral of the net torque acting on it over the interval.
Write the canonical equation for the integral form: _____ΔL=titfτnet(t)dt\Delta\vec{L} = \int_{t_i}^{t_f} \vec{\tau}_{\mathrm{net}}(t)\,dt
State the canonical condition: _____inertial;τnet(t);interval specified\text{inertial};\, \vec{\tau}_{\mathrm{net}}(t);\, \text{interval specified}

Worked Example

Use this worked example to practice Self-Explanation.

Problem

A solid disk (moment of inertia I=0.50kgm2I = 0.50\,\mathrm{kg\cdot m^2}) rotates freely about a fixed axis. At t=0t=0, it spins at ωi=12rad/s\omega_i = 12\,\mathrm{rad/s}. A brake applies a time-varying frictional torque τfriction=bt2\tau_{\mathrm{friction}} = -bt^2 where b=2.0Nm/s2b = 2.0\,\mathrm{N\cdot m/s^2}. Find the angular velocity at t=2.0st = 2.0\,\mathrm{s}.

Step 1: Verbal Decoding

Target: ωf\omega_f at t=2.0st = 2.0\,\mathrm{s}

Given: II, ωi\omega_i, bb, tft_f

Constraints: fixed axis; friction torque opposes rotation; torque magnitude grows with time squared; no other torques

Step 2: Visual Decoding

Draw a disk rotating about a perpendicular axis through its center. Choose ++ in the initial rotation direction. Mark τ\tau opposite that direction.

(So ωi>0\omega_i > 0 and τ<0\tau < 0 throughout the interval.)

Step 3: Physics Modeling

  1. I(ωfωi)=0tf(bt2)dtI(\omega_f - \omega_i) = \int_{0}^{t_f} (-bt^2)\,dt

Step 4: Mathematical Procedures

  1. I(ωfωi)=[bt33]0tfI(\omega_f - \omega_i) = \left[-\frac{bt^3}{3}\right]_0^{t_f}
  2. I(ωfωi)=btf33I(\omega_f - \omega_i) = -\frac{b t_f^3}{3}
  3. ωf=ωibtf33I\omega_f = \omega_i - \frac{b t_f^3}{3I}
  4. ωf=12rad/s(2.0Nm/s2)(2.0s)33(0.50kgm2)\omega_f = 12\,\mathrm{rad/s} - \frac{(2.0\,\mathrm{N\cdot m/s^2})(2.0\,\mathrm{s})^3}{3(0.50\,\mathrm{kg\cdot m^2})}
  5. ωf=12rad/s10.67rad/s\omega_f = 12\,\mathrm{rad/s} - 10.67\,\mathrm{rad/s}
  6. ωf1.3rad/s\underline{\omega_f \approx 1.3\,\mathrm{rad/s}}

Step 5: Reflection

  • Units: [b][t3]/[I]=(Nm/s2)(s3)/(kgm2)=rad/s[b][t^3]/[I] = \mathrm{(N\cdot m/s^2)(s^3)/(kg\cdot m^2)} = \mathrm{rad/s}
  • Magnitude: Final ω\omega is much smaller than initial, consistent with braking torque that grows stronger over time.
  • Limiting case: If b=0b=0 (no torque), then ωf=ωi\omega_f = \omega_i, as expected.

Physics model with explanation

Principle: Angular impulse-momentum theorem (integral form) relates change in angular momentum to the time integral of net torque.

Conditions: Inertial frame; torque varies with time; interval [0,2.0s][0, 2.0\,\mathrm{s}] specified.

Relevance: Since τ(t)=bt2\tau(t) = -bt^2 is time-varying (quadratic), the simple τΔt\tau\Delta t formula would be incorrect. We must integrate over the interval.

Description: The net torque is purely frictional and opposes rotation. It grows stronger as time progresses (quadratic dependence), so the disk slows down at an increasing rate.

Goal: Integrate the torque function to find the total angular impulse, then use the relation ΔL=IΔω\Delta L = I\Delta\omega (for fixed II) to find the final angular velocity. The result shows the disk has slowed substantially but is still rotating.


Solve a Problem

Test your understanding with Problem Solving. Try it yourself before revealing the solution.

Click to show problem + solution

Problem

A thin rod (length L=1.2mL = 1.2\,\mathrm{m}, mass m=0.40kgm = 0.40\,\mathrm{kg}) rotates about a perpendicular axis through one end. At t=0t=0, it is at rest. A time-varying torque τ(t)=Ct\tau(t) = Ct where C=0.60Nm/sC = 0.60\,\mathrm{N\cdot m/s} is applied for 3.0s3.0\,\mathrm{s}. Find the angular velocity at t=3.0st = 3.0\,\mathrm{s}.

Step 1: Verbal Decoding

Target: ωf\omega_f at t=3.0st = 3.0\,\mathrm{s}

Given: LL, mm, CC, tft_f, ωi\omega_i

Constraints: axis through end; applied torque increases linearly with time; starts from rest

Step 2: Visual Decoding

Draw a rod pivoting about one end. Choose ++ counterclockwise. Mark τ\tau in that direction.

(So τ>0\tau > 0 for all t>0t > 0.)

Step 3: Physics Modeling

  1. Iωf=0tfCtdtI\omega_f = \int_{0}^{t_f} Ct\,dt
  2. I=13mL2I = \frac{1}{3}mL^2

Step 4: Mathematical Procedures

  1. Iωf=C[t22]0tfI\omega_f = C\left[\frac{t^2}{2}\right]_0^{t_f}
  2. Iωf=Ctf22I\omega_f = \frac{C t_f^2}{2}
  3. ωf=Ctf22I\omega_f = \frac{C t_f^2}{2I}
  4. I=13(0.40kg)(1.2m)2I = \frac{1}{3}(0.40\,\mathrm{kg})(1.2\,\mathrm{m})^2
  5. I=0.192kgm2I = 0.192\,\mathrm{kg\cdot m^2}
  6. ωf=(0.60Nm/s)(3.0s)22(0.192kgm2)\omega_f = \frac{(0.60\,\mathrm{N\cdot m/s})(3.0\,\mathrm{s})^2}{2(0.192\,\mathrm{kg\cdot m^2})}
  7. ωf=5.4Nms0.384kgm2\omega_f = \frac{5.4\,\mathrm{N\cdot m\cdot s}}{0.384\,\mathrm{kg\cdot m^2}}
  8. ωf14rad/s\underline{\omega_f \approx 14\,\mathrm{rad/s}}

Step 5: Reflection

  • Units: [C][t2]/[I]=(Nm/s)(s2)/(kgm2)=rad/s[C][t^2]/[I] = \mathrm{(N\cdot m/s)(s^2)/(kg\cdot m^2)} = \mathrm{rad/s}
  • Magnitude: About 2.22.2 revolutions per second is reasonable for a light rod with increasing torque over 33 seconds.
  • Limiting case: If C=0C=0 (no torque), then ωf=0\omega_f = 0, as expected.

PrincipleRelationship
Angular Impulse (Constant Torque)Special case when τnet\vec{\tau}_{\mathrm{net}} is constant; then ΔL=τnetΔt\Delta\vec{L} = \vec{\tau}_{\mathrm{net}}\,\Delta t
Torque-Angular Momentum FormDifferential form: τnet=dLdt\vec{\tau}_{\mathrm{net}} = \frac{d\vec{L}}{dt}; integrating this over time yields the impulse-momentum theorem
Angular Momentum ConservationWhen net torque is zero, ΔL=0\Delta\vec{L} = 0 and angular momentum is conserved

FAQ

When should I use the integral form instead of the constant-torque formula?

Use the integral form whenever net torque changes noticeably during the interval. If the problem statement gives τ(t)\tau(t) or describes a varying force, you must integrate. If torque is approximately constant (or if the problem says “constant torque”), you can simplify to ΔL=τnetΔt\Delta\vec{L} = \vec{\tau}_{\mathrm{net}}\,\Delta t.

Can I evaluate the integral graphically if I don’t have an explicit τ(t)\tau(t) function?

Yes. If you have a graph of torque versus time, the area under the curve from tit_i to tft_f gives ΔL\Delta L. This is often easier than trying to fit an algebraic function to experimental data.

Does this theorem apply to multi-body systems, like a system of connected rigid bodies?

Yes, as long as you sum the torques from all external sources acting on the entire system about a common axis or center of mass. Internal torques (action-reaction pairs) cancel by Newton’s third law. The theorem then gives the change in total angular momentum of the system.

What if moment of inertia changes during the motion (e.g., a spinning skater pulling in their arms)?

The theorem ΔL=τnetdt\Delta\vec{L} = \int \vec{\tau}_{\mathrm{net}}\,dt still holds as long as you correctly account for external torques. If there is no external torque, ΔL=0\Delta L = 0 (angular momentum is conserved) even though II and ω\omega individually change. When changing II, use L=I(t)ω(t)L = I(t)\omega(t) at each instant.

Is there an equivalent “power” or “work” version of this theorem for rotation?

Yes. The rotational work-energy theorem relates change in rotational kinetic energy to the work done by torques. The impulse-momentum form focuses on momentum changes over time, while work-energy focuses on energy changes over angular displacement. Both are correct but answer different questions.

How do I handle three-dimensional rotation where L\vec{L} and τ\vec{\tau} are not parallel?

In 3D, τnet=dLdt\vec{\tau}_{\mathrm{net}} = \frac{d\vec{L}}{dt} is a vector equation, and L\vec{L} can change direction even if its magnitude stays constant (precession). The integral form ΔL=titfτnet(t)dt\Delta\vec{L} = \int_{t_i}^{t_f} \vec{\tau}_{\mathrm{net}}(t)\,dt still holds as a vector equation. You integrate each component separately in a chosen coordinate system.

Can I use this theorem in a non-inertial reference frame?

You can, but you must add fictitious torques (due to the frame’s acceleration or rotation) to τnet\vec{\tau}_{\mathrm{net}}. It is usually simpler to work in an inertial frame and transform results afterward if needed.



How This Fits in Unisium

The Unisium Study System helps you master the angular impulse-momentum theorem (integral form) through elaborative encoding, retrieval practice, self-explanation, and problem solving. Our platform tracks your fluency with time-varying torque problems, generates targeted practice, and connects this principle to prerequisite concepts (like rotational kinematics) and advanced applications (like conservation laws in complex systems).

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