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AQA A-level Physics revision notes

Engineering physics (A-level only)

Section 3.11
Year 2
Year 2: this is content the exam board adds beyond the AS subject content, for the full A-level.
12 specification points
Optional · choose 1 of 5

Notes and three levels of exam-style practice for each registered specification point in this section.

Checked against AQA 7408 section 3.11

Checked against AQA 7408 section 3.11. Review basis: the qualification registry sourced from the AQA A-level Physics (7408) specification; registry verification recorded 11 July 2026.

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In the exam: Data and formulae booklet provided · calculator allowed in every paper

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3.11.1.1

Concept of moment of inertia

Notes
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Your confidence:

A self-report of how sure you feel. It does not measure mastery. Evidence from your answers reaches secure after the latest Tier 2/3 attempt is correct, with three correct distinct drills across at least two dates and two practice sources.

Explanation

  • Moment of inertia II measures an object's resistance to angular acceleration about a specified axis, so it is the rotational analogue of mass. For a point mass, I=mr2I=mr^2; for several point masses, I=mr2I=\sum mr^2, where rr is the perpendicular distance from the axis.
  • Its unit is kg m2\text{kg m}^2.
  • Both the total mass and its distribution matter: moving mass farther from the axis increases II strongly because distance is squared.
  • For an extended object, the supplied expression represents the sum over all its small mass elements.
  • Examiners expect the stated axis to be used and every separate contribution to be included.
Point masses contribute according to their squared perpendicular distance from the rotation axis.
Worked example

Two point masses, 0.40kg0.40\,\text{kg} and 0.25kg0.25\,\text{kg}, are fixed 0.18m0.18\,\text{m} and 0.32m0.32\,\text{m} from an axis. Calculate their total moment of inertia.

  1. 1.Write one contribution for each mass: I=mr2I=\sum mr^2.
  2. 2.Substitute: I=(0.40)(0.18)2+(0.25)(0.32)2I=(0.40)(0.18)^2+(0.25)(0.32)^2.
  3. 3.Evaluate: I=0.01296+0.02560=0.03856kg m2I=0.01296+0.02560=0.03856\,\text{kg m}^2.

Answer: I=3.9×102kg m2I=3.9\times10^{-2}\,\text{kg m}^2 to two significant figures.

Common mistakes

  • Don't use the diameter or distance between masses instead of each perpendicular distance from the stated axis.
  • Don't add mrmr contributions and forget that the distance is squared in I=mr2I=\sum mr^2.
  • Don't treat moment of inertia as depending only on total mass and ignore how that mass is distributed.

Exam tip

For a multi-part rotor, calculate and label each component's II before adding the contributions.

Tier 1 · Easy

ORIGINAL

Two small balancing masses rotate about the same shaft. A 0.30kg0.30\,\text{kg} mass is 0.22m0.22\,\text{m} from the shaft and a 0.45kg0.45\,\text{kg} mass is 0.12m0.12\,\text{m} from it. Calculate their combined moment of inertia.

[2 marks]

Total for this question: 2

Tier 2 · Standard

ORIGINAL

A training flywheel has moment of inertia 0.080kg m20.080\,\text{kg m}^2 before four identical 0.25kg0.25\,\text{kg} sliders are attached. Determine the total moment of inertia when every slider is fixed 0.30m0.30\,\text{m} from the axis.

[3 marks]

Total for this question: 3

Tier 3 · Hard

ORIGINAL

A prototype rotor consists of a uniform disc of mass 6.0kg6.0\,\text{kg} and radius 0.25m0.25\,\text{m}, a shaft with moment of inertia 0.028kg m20.028\,\text{kg m}^2, and three identical point masses fixed 0.35m0.35\,\text{m} from the axis. The total moment of inertia is 0.456kg m20.456\,\text{kg m}^2. The disc expression is I=12MR2I=\frac12MR^2. Determine the mass of each point mass.

[5 marks]

Total for this question: 5

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3.11.1.2

Rotational kinetic energy

Notes
Evidence from your answers: none yet
Your confidence:

A self-report of how sure you feel. It does not measure mastery. Evidence from your answers reaches secure after the latest Tier 2/3 attempt is correct, with three correct distinct drills across at least two dates and two practice sources.

Explanation

  • A rigid rotating object stores kinetic energy Ek=12Iω2E_k=\frac12I\omega^2, directly analogous to translational energy 12mv2\frac12mv^2. Increasing moment of inertia increases the stored energy in direct proportion, whereas increasing angular speed has a squared effect.
  • A flywheel therefore stores substantial energy when mass is placed far from its axis and it rotates rapidly.
  • In machinery, a flywheel absorbs energy when driving torque exceeds demand and releases energy when demand exceeds the drive, smoothing changes in torque and speed.
  • Flywheels can also store energy in vehicles and production machines.
  • Calculations require II in kg m2\text{kg m}^2 and ω\omega in rad s1\text{rad s}^{-1}.
Worked example

A flywheel of moment of inertia 2.8kg m22.8\,\text{kg m}^2 speeds up from 12rad s112\,\text{rad s}^{-1} to 30rad s130\,\text{rad s}^{-1}. Calculate the increase in rotational kinetic energy.

  1. 1.Use ΔEk=12I(ω22ω12)\Delta E_k=\frac12I(\omega_2^2-\omega_1^2).
  2. 2.Substitute: ΔEk=12(2.8)(302122)\Delta E_k=\frac12(2.8)(30^2-12^2).
  3. 3.Evaluate: ΔEk=1.4(756)=1058.4J\Delta E_k=1.4(756)=1058.4\,\text{J}.

Answer: The rotational kinetic energy increases by 1.1×103J1.1\times10^3\,\text{J}.

Common mistakes

  • Don't use Ek=Iω2E_k=I\omega^2 and omit the factor of one half.
  • Don't substitute revolutions per second directly for ω\omega instead of converting with ω=2πf\omega=2\pi f.
  • Don't calculate the change using (ω2ω1)2(\omega_2-\omega_1)^2 rather than ω22ω12\omega_2^2-\omega_1^2.

Exam tip

For an energy change, write the final and initial 12Iω2\frac12I\omega^2 terms explicitly before subtracting.

Tier 1 · Easy

ORIGINAL

A small flywheel has moment of inertia 0.85kg m20.85\,\text{kg m}^2 and angular speed 14rad s114\,\text{rad s}^{-1}. Calculate its rotational kinetic energy.

[2 marks]

Total for this question: 2

Tier 2 · Standard

ORIGINAL

An energy-recovery flywheel of moment of inertia 40kg m240\,\text{kg m}^2 stores 32kJ32\,\text{kJ} as rotational kinetic energy. Determine its angular speed.

[3 marks]

Total for this question: 3

Tier 3 · Hard

ORIGINAL

A machine flywheel with moment of inertia 18kg m218\,\text{kg m}^2 slows from 75rad s175\,\text{rad s}^{-1} to 45rad s145\,\text{rad s}^{-1} in 5.5s5.5\,\text{s}. During this interval, 72%72\% of the decrease in rotational kinetic energy is transferred usefully. Calculate the mean useful power.

[5 marks]

Total for this question: 5

3.11.1.3

Rotational motion

Notes
Evidence from your answers: none yet
Your confidence:

A self-report of how sure you feel. It does not measure mastery. Evidence from your answers reaches secure after the latest Tier 2/3 attempt is correct, with three correct distinct drills across at least two dates and two practice sources.

Explanation

  • Angular displacement θ\theta is measured in radians. Angular velocity is ω=Δθ/Δt\omega=\Delta\theta/\Delta t for a chosen positive direction; angular speed is its magnitude.
  • Angular acceleration is α=Δω/Δt\alpha=\Delta\omega/\Delta t. For uniform angular acceleration, the translational equations have direct rotational analogues: ω2=ω1+αt\omega_2=\omega_1+\alpha t, θ=12(ω1+ω2)t\theta=\frac12(\omega_1+\omega_2)t, θ=ω1t+12αt2\theta=\omega_1t+\frac12\alpha t^2, and ω22=ω12+2αθ\omega_2^2=\omega_1^2+2\alpha\theta.
  • On an angular-velocity–time graph, gradient gives angular acceleration and signed area gives angular displacement. A changing gradient represents non-uniform angular acceleration.
  • A straight graph section therefore represents constant angular acceleration over that interval.
  • Examiners may require both graphical interpretation and equation selection.
Gradient gives angular acceleration and area under an angular-velocity–time graph gives angular displacement.
Worked example

A rotor accelerates uniformly from 8.0rad s18.0\,\text{rad s}^{-1} to 26rad s126\,\text{rad s}^{-1} in 6.0s6.0\,\text{s}. Calculate its angular acceleration and angular displacement.

  1. 1.α=(ω2ω1)/t=(268.0)/6.0=3.0rad s2\alpha=(\omega_2-\omega_1)/t=(26-8.0)/6.0=3.0\,\text{rad s}^{-2}.
  2. 2.For uniform acceleration, θ=12(ω1+ω2)t\theta=\frac12(\omega_1+\omega_2)t.
  3. 3.θ=12(8.0+26)(6.0)=102rad\theta=\frac12(8.0+26)(6.0)=102\,\text{rad}.

Answer: α=3.0rad s2\alpha=3.0\,\text{rad s}^{-2} and θ=1.0×102rad\theta=1.0\times10^2\,\text{rad}.

Common mistakes

  • Don't use degrees in the rotational equations instead of converting angular displacement to radians.
  • Don't read the height of an ω\omegatt graph as angular acceleration instead of using its gradient.
  • Don't treat rotational frequency in hertz as angular velocity without multiplying by 2π2\pi.

Exam tip

On an ω\omegatt graph, label gradient and area with their physical quantities before calculating.

Tier 1 · Easy

ORIGINAL

The angular speed of a mixer rotor rises uniformly from 5.0rad s15.0\,\text{rad s}^{-1} to 17rad s117\,\text{rad s}^{-1} in 4.0s4.0\,\text{s}. Calculate its angular acceleration.

[2 marks]

Total for this question: 2

Tier 2 · Standard

ORIGINAL

A rotor starts from rest and has constant angular acceleration 4.2rad s24.2\,\text{rad s}^{-2} for 6.0s6.0\,\text{s}. Determine the number of revolutions completed.

[3 marks]

Total for this question: 3

Tier 3 · Hard

ORIGINAL

A flywheel's angular speed rises uniformly from 12rad s112\,\text{rad s}^{-1} to 48rad s148\,\text{rad s}^{-1} in 6.0s6.0\,\text{s}, remains at 48rad s148\,\text{rad s}^{-1} for 5.0s5.0\,\text{s}, then falls uniformly to 18rad s118\,\text{rad s}^{-1} in 10s10\,\text{s}. Determine its total angular displacement and the corresponding number of revolutions.

[5 marks]

Total for this question: 5

3.11.1.4

Torque and angular acceleration

Notes
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Your confidence:

A self-report of how sure you feel. It does not measure mastery. Evidence from your answers reaches secure after the latest Tier 2/3 attempt is correct, with three correct distinct drills across at least two dates and two practice sources.

Explanation

  • Torque is the turning effect of a force. For a force perpendicular to the radius, T=FrT=Fr, where rr is the perpendicular distance from the axis to the force's line of action; torque has unit N m\text{N m}.
  • The rotational form of Newton's second law is T=IαT=I\alpha, so the resultant torque produces angular acceleration in proportion to 1/I1/I.
  • Driving and resisting torques act in opposite rotational senses and must be combined with signs before applying this equation.
  • If the force is not perpendicular, the perpendicular force component or perpendicular moment arm is required.
  • Examiners expect a resultant torque, not merely the applied driving torque.
A tangential force at radius rr produces torque T=FrT=Fr about the axis.
Worked example

A motor supplies 36N m36\,\text{N m} to a rotor while friction provides 5.0N m5.0\,\text{N m} in the opposite direction. The rotor has I=4.0kg m2I=4.0\,\text{kg m}^2. Calculate its angular acceleration.

  1. 1.Find the resultant torque: T=365.0=31N mT=36-5.0=31\,\text{N m}.
  2. 2.Use T=IαT=I\alpha and rearrange to α=T/I\alpha=T/I.
  3. 3.α=31/4.0=7.75rad s2\alpha=31/4.0=7.75\,\text{rad s}^{-2}.

Answer: α=7.8rad s2\alpha=7.8\,\text{rad s}^{-2} to two significant figures.

Common mistakes

  • Don't use the distance to the point of application when it is not the perpendicular distance to the force's line of action.
  • Don't substitute the driving torque into T=IαT=I\alpha without subtracting the resisting torque.
  • Don't substitute force in newtons directly into T=IαT=I\alpha without first calculating torque.

Exam tip

Draw a rotational sense beside every torque and form the signed resultant before using T=IαT=I\alpha.

Tier 1 · Easy

ORIGINAL

A tangential force of 85N85\,\text{N} acts at the rim of a wheel of radius 0.16m0.16\,\text{m}. Calculate the torque about the axle.

[2 marks]

Total for this question: 2

Tier 2 · Standard

ORIGINAL

A constant resultant torque of 24N m24\,\text{N m} acts on a rotor with moment of inertia 3.2kg m23.2\,\text{kg m}^2. Its initial angular speed is 6.0rad s16.0\,\text{rad s}^{-1}. Determine its angular speed after 3.0s3.0\,\text{s}.

[3 marks]

Total for this question: 3

Tier 3 · Hard

ORIGINAL

A drive supplies a constant torque of 54N m54\,\text{N m} to a flywheel of moment of inertia 6.2kg m26.2\,\text{kg m}^2. Bearing friction provides a constant opposing torque of 7.5N m7.5\,\text{N m}. The initial angular speed is 10rad s110\,\text{rad s}^{-1}. Calculate the angular speed after 4.5s4.5\,\text{s}.

[5 marks]

Total for this question: 5

3.11.1.5

Angular momentum

Notes
Evidence from your answers: none yet
Your confidence:

A self-report of how sure you feel. It does not measure mastery. Evidence from your answers reaches secure after the latest Tier 2/3 attempt is correct, with three correct distinct drills across at least two dates and two practice sources.

Explanation

  • For a rigid body rotating about a fixed axis, angular momentum is L=IωL=I\omega, measured in kg m2 s1\text{kg m}^2\text{ s}^{-1}. Total angular momentum is conserved when the resultant external torque is zero.
  • Consequently, reducing II increases ω\omega so that the signed total IωI\omega remains constant, as in a spinning athlete drawing in the arms.
  • A constant torque acting for time Δt\Delta t provides angular impulse TΔt=Δ(Iω)T\Delta t=\Delta(I\omega).
  • Direction matters: opposite rotations have opposite angular momenta.
  • When rotating objects couple and move together, angular momentum can be conserved even though rotational kinetic energy decreases, because the coupling is inelastic.
Worked example

A skater has I=3.6kg m2I=3.6\,\text{kg m}^2 at 5.0rad s15.0\,\text{rad s}^{-1} and reduces the moment of inertia to 2.0kg m22.0\,\text{kg m}^2. Calculate the new angular speed when external torque is negligible.

  1. 1.State conservation: I1ω1=I2ω2I_1\omega_1=I_2\omega_2.
  2. 2.Substitute: (3.6)(5.0)=(2.0)ω2(3.6)(5.0)=(2.0)\omega_2.
  3. 3.Rearrange: ω2=18/2.0=9.0rad s1\omega_2=18/2.0=9.0\,\text{rad s}^{-1}.

Answer: The new angular speed is 9.0rad s19.0\,\text{rad s}^{-1}.

Common mistakes

  • Don't conserve angular momentum despite a non-zero external torque acting during the stated interval.
  • Don't conserve rotational kinetic energy when two rotating parts lock together in an inelastic coupling.
  • Don't drop the sign of angular velocity when two bodies initially rotate in opposite directions.

Exam tip

A conservation answer must state that the resultant external torque is zero or negligible.

Tier 1 · Easy

ORIGINAL

A turntable has moment of inertia 2.4kg m22.4\,\text{kg m}^2 and rotates at 18rad s118\,\text{rad s}^{-1}. Calculate its angular momentum.

[2 marks]

Total for this question: 2

Tier 2 · Standard

ORIGINAL

A flywheel with moment of inertia 0.80kg m20.80\,\text{kg m}^2 rotates at 30rad s130\,\text{rad s}^{-1}. It is coupled to a stationary coaxial wheel of moment of inertia 1.20kg m21.20\,\text{kg m}^2, and the pair then rotate together. Determine their common angular speed.

[3 marks]

Total for this question: 3

Tier 3 · Hard

ORIGINAL

A rotating platform and athlete initially have moment of inertia 4.8kg m24.8\,\text{kg m}^2 and angular speed 9.0rad s19.0\,\text{rad s}^{-1}. An external constant opposing torque of 3.2N m3.2\,\text{N m} acts for 1.5s1.5\,\text{s}. The athlete then changes position so that the combined moment of inertia is 3.0kg m23.0\,\text{kg m}^2. Determine the final angular speed, assuming the position change itself involves negligible external torque.

[5 marks]

Total for this question: 5

3.11.1.6

Work and power

Notes
Evidence from your answers: none yet
Your confidence:

A self-report of how sure you feel. It does not measure mastery. Evidence from your answers reaches secure after the latest Tier 2/3 attempt is correct, with three correct distinct drills across at least two dates and two practice sources.

Explanation

  • A constant torque acting through angular displacement transfers work W=TθW=T\theta, with θ\theta in radians. The instantaneous rate of energy transfer is rotational power P=TωP=T\omega.
  • These equations parallel W=FsW=Fs and P=FvP=Fv.
  • In real rotating machinery, frictional torque removes mechanical energy and must appear in the torque, work or power balance.
  • At constant angular speed, resultant torque is zero, but the driving torque can still balance load and friction torques and therefore transfer power.
  • When torque or angular speed varies, P=TωP=T\omega uses simultaneous values; total work may instead be found from the energy change or an appropriate torque-angle area.
Worked example

A shaft turns at 900rev min1900\,\text{rev min}^{-1}. It supplies a load torque of 48N m48\,\text{N m} and overcomes friction torque 6.0N m6.0\,\text{N m}. Calculate the motor power.

  1. 1.The motor torque is T=48+6.0=54N mT=48+6.0=54\,\text{N m}.
  2. 2.900rev min1=15rev s1900\,\text{rev min}^{-1}=15\,\text{rev s}^{-1}, so ω=2π(15)=94.2rad s1\omega=2\pi(15)=94.2\,\text{rad s}^{-1}.
  3. 3.P=Tω=(54)(94.2)=5.09×103WP=T\omega=(54)(94.2)=5.09\times10^3\,\text{W}.

Answer: The motor power is 5.1kW5.1\,\text{kW} to two significant figures.

Common mistakes

  • Don't use angular displacement in revolutions in W=TθW=T\theta instead of converting it to radians.
  • Don't omit frictional torque when finding the driving power required by real machinery.
  • Don't conclude that power transfer is zero at steady speed because the resultant torque is zero.

Exam tip

Distinguish driving, load and friction torques before selecting the torque used in P=TωP=T\omega.

Tier 1 · Easy

ORIGINAL

A constant torque of 18N m18\,\text{N m} turns a shaft through 3.5rad3.5\,\text{rad}. Calculate the work done by the torque.

[2 marks]

Total for this question: 2

Tier 2 · Standard

ORIGINAL

A motor provides a torque of 42N m42\,\text{N m} while its shaft rotates at 1200rev min11200\,\text{rev min}^{-1}. Determine the power transferred by the shaft.

[3 marks]

Total for this question: 3

Tier 3 · Hard

ORIGINAL

A motor maintains a constant angular speed of 32rad s132\,\text{rad s}^{-1} for 25s25\,\text{s} while supplying torque 84N m84\,\text{N m}. Bearing friction opposes the motion with torque 9.0N m9.0\,\text{N m}; the remaining torque acts on the load. Calculate the useful power and the useful energy transferred to the load.

[5 marks]

Total for this question: 5

3.11.2.1

First law of thermodynamics

Notes
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Your confidence:

A self-report of how sure you feel. It does not measure mastery. Evidence from your answers reaches secure after the latest Tier 2/3 attempt is correct, with three correct distinct drills across at least two dates and two practice sources.

Explanation

  • AQA writes the First Law as Q=ΔU+WQ=\Delta U+W. Here QQ is energy transferred to the system by heating, ΔU\Delta U is the increase in internal energy, and WW is work done by the system.
  • Thus heating gives positive QQ, cooling negative QQ, expansion normally positive WW, and compression negative WW.
  • Rearranging to $\Delta U=Q-W$ helps preserve this sign convention.
  • Internal energy is a state function, so its change depends only on the initial and final states.
  • Over a complete cycle ΔU=0\Delta U=0, although non-zero net heat transfer can equal the net work done by the gas.
Worked example

During compression, 300J300\,\text{J} of work is done on a gas while 80J80\,\text{J} leaves by heating. Calculate ΔU\Delta U using Q=ΔU+WQ=\Delta U+W.

  1. 1.Energy leaving by heating gives Q=80JQ=-80\,\text{J}.
  2. 2.Work done on the gas means work done by the gas is W=300JW=-300\,\text{J}.
  3. 3.ΔU=QW=80(300)=+220J\Delta U=Q-W=-80-(-300)=+220\,\text{J}.

Answer: The internal energy increases by 220J220\,\text{J}.

Common mistakes

  • Don't make work done on the gas positive even though WW is defined as work done by the gas.
  • Don't treat energy leaving by heating as positive QQ.
  • Don't assume ΔU=0\Delta U=0 for any process rather than only a return to the same thermodynamic state.

Exam tip

Write the signs of QQ and WW in words before substituting into ΔU=QW\Delta U=Q-W.

Tier 1 · Easy

ORIGINAL

A gas receives 520J520\,\text{J} by heating and does 180J180\,\text{J} of work. Calculate its change in internal energy using AQA's convention Q=ΔU+WQ=\Delta U+W.

[2 marks]

Total for this question: 2

Tier 2 · Standard

ORIGINAL

A gas is compressed so that 240J240\,\text{J} of work is done on it. During the compression, 90J90\,\text{J} of energy leaves the gas by heating. Using Q=ΔU+WQ=\Delta U+W and taking work output from the gas as positive, determine ΔU\Delta U.

[3 marks]

Total for this question: 3

Tier 3 · Hard

ORIGINAL

A gas completes a two-process cycle. In process A it receives 3.2kJ3.2\,\text{kJ} by heating and its internal energy increases by 1.1kJ1.1\,\text{kJ}. In process B the gas returns to its initial state while 1.4kJ1.4\,\text{kJ} leaves it by heating. Determine the net work done by the gas during the cycle. State the signs used in Q=ΔU+WQ=\Delta U+W.

[5 marks]

Total for this question: 5

3.11.2.2

Non-flow processes

Notes
Evidence from your answers: none yet
Your confidence:

A self-report of how sure you feel. It does not measure mastery. Evidence from your answers reaches secure after the latest Tier 2/3 attempt is correct, with three correct distinct drills across at least two dates and two practice sources.

Explanation

  • The required non-flow changes are isothermal, adiabatic, constant pressure and constant volume. An ideal gas obeys pV=nRTpV=nRT.
  • During an isothermal change, temperature is constant and pV=constantpV=\text{constant}; for an ideal gas, ΔU=0\Delta U=0, so Q=WQ=W. During an adiabatic change, Q=0Q=0 and pVγ=constantpV^\gamma=\text{constant}, so ΔU=W\Delta U=-W.
  • At constant pressure, work done by the gas is W=pΔVW=p\Delta V. At constant volume, ΔV=0\Delta V=0 and W=0W=0.
  • Each process must also satisfy Q=ΔU+WQ=\Delta U+W.
  • Rapid well-insulated changes are commonly close to adiabatic because little energy transfers by heating.
Worked example

An ideal gas expands isothermally from 1.50×103m31.50\times10^{-3}\,\text{m}^3 at 320kPa320\,\text{kPa} to 4.0×103m34.0\times10^{-3}\,\text{m}^3. Calculate the final pressure and state ΔU\Delta U.

  1. 1.For an isothermal change, p1V1=p2V2p_1V_1=p_2V_2.
  2. 2.p2=(320)(1.5/4.0)=120kPap_2=(320)(1.5/4.0)=120\,\text{kPa}.
  3. 3.The ideal-gas temperature is unchanged, so its internal energy is unchanged.

Answer: p2=120kPap_2=120\,\text{kPa} and ΔU=0\Delta U=0.

Common mistakes

  • Don't equate adiabatic with constant temperature rather than with zero heat transfer.
  • Don't use pV=constantpV=\text{constant} for an adiabatic change instead of pVγ=constantpV^\gamma=\text{constant}.
  • Don't calculate non-zero work for a constant-volume process even though ΔV=0\Delta V=0.

Exam tip

Name the defining constraint first, then apply both its process equation and the First Law.

Tier 1 · Easy

ORIGINAL

A rigid sealed vessel receives 450J450\,\text{J} by heating. State the work done by the gas and calculate its increase in internal energy.

[2 marks]

Total for this question: 2

Tier 2 · Standard

ORIGINAL

An ideal gas expands isothermally from pressure 240kPa240\,\text{kPa} and volume 2.0×103m32.0\times10^{-3}\,\text{m}^3 to volume 5.0×103m35.0\times10^{-3}\,\text{m}^3. Determine its final pressure and state its change in internal energy.

[3 marks]

Total for this question: 3

Tier 3 · Hard

ORIGINAL

A gas is compressed adiabatically from p1=100kPap_1=100\,\text{kPa} and V1=4.8×103m3V_1=4.8\times10^{-3}\,\text{m}^3 to V2=1.8×103m3V_2=1.8\times10^{-3}\,\text{m}^3. Take γ=1.40\gamma=1.40. During the compression, 720J720\,\text{J} of work is done on the gas. Calculate the final pressure and the change in internal energy.

[5 marks]

Total for this question: 5

3.11.2.3

The p-V diagram

Notes
Evidence from your answers: none yet
Your confidence:

A self-report of how sure you feel. It does not measure mastery. Evidence from your answers reaches secure after the latest Tier 2/3 attempt is correct, with three correct distinct drills across at least two dates and two practice sources.

Explanation

  • A thermodynamic process is shown as a path on a pressure–volume diagram. Motion to larger volume is expansion; motion to smaller volume is compression.
  • The work done by the gas is the signed area under the path. For constant pressure, W=pΔVW=p\Delta V; an expansion gives positive work and a compression negative work.
  • For a cycle, the net work per cycle is the area enclosed by the loop, not the total area beneath one branch.
  • A clockwise loop represents positive net work by the gas, while an anticlockwise loop requires net work input.
  • Pressure must be in pascals and volume in m3\text{m}^3 for the area to be in joules.
The enclosed area of a clockwise ppVV cycle is the positive net work done by the gas.
Worked example

A rectangular clockwise cycle spans V=2.0V=2.0 to 5.0×103m35.0\times10^{-3}\,\text{m}^3 and p=120p=120 to 360kPa360\,\text{kPa}. Calculate the net work per cycle.

  1. 1.The net work is the enclosed rectangular area: W=ΔpΔVW=\Delta p\,\Delta V.
  2. 2.Δp=(360120)×103=2.40×105Pa\Delta p=(360-120)\times10^3=2.40\times10^5\,\text{Pa}.
  3. 3.W=(2.40×105)(3.0×103)=720JW=(2.40\times10^5)(3.0\times10^{-3})=720\,\text{J}.

Answer: The gas does +720J+720\,\text{J} of net work per cycle.

Common mistakes

  • Don't use the full area from the pressure axis to the upper branch instead of the area enclosed by the cycle.
  • Don't leave pressure in kilopascals when calculating an area expected in joules.
  • Don't assign positive work to an anticlockwise cycle rather than to a clockwise cycle.

Exam tip

For an estimate from a curved path, state that work is the area under the graph and show how that area was approximated.

Tier 1 · Easy

ORIGINAL

A gas expands at constant pressure 180kPa180\,\text{kPa} from volume 1.2×103m31.2\times10^{-3}\,\text{m}^3 to 3.7×103m33.7\times10^{-3}\,\text{m}^3. Calculate the work done by the gas.

[2 marks]

Total for this question: 2

Tier 2 · Standard

ORIGINAL

A gas follows a clockwise rectangular cycle on a pp-VV diagram between pressures 150kPa150\,\text{kPa} and 400kPa400\,\text{kPa} and between volumes 1.0×103m31.0\times10^{-3}\,\text{m}^3 and 3.5×103m33.5\times10^{-3}\,\text{m}^3. Determine the net work done per cycle.

[3 marks]

Total for this question: 3

Tier 3 · Hard

ORIGINAL

On a pp-VV diagram, a gas expands along a straight line from (0.8×103m3,600kPa)(0.8\times10^{-3}\,\text{m}^3,600\,\text{kPa}) to (3.2×103m3,200kPa)(3.2\times10^{-3}\,\text{m}^3,200\,\text{kPa}). It then compresses at constant pressure 200kPa200\,\text{kPa} to its initial volume before returning at constant volume to its initial state. Calculate the net work done by the gas in the cycle.

[5 marks]

Total for this question: 5

3.11.2.4

Engine cycles

Notes
Evidence from your answers: none yet
Your confidence:

A self-report of how sure you feel. It does not measure mastery. Evidence from your answers reaches secure after the latest Tier 2/3 attempt is correct, with three correct distinct drills across at least two dates and two practice sources.

Explanation

  • A four-stroke petrol engine completes induction, compression, power and exhaust strokes; it compresses a fuel–air mixture before spark ignition. A diesel engine compresses air before fuel injection and ignition.
  • Their indicator diagrams show measured pressure–volume cycles, which can be compared with theoretical cycles without requiring constructional detail. Indicated power equals loop area multiplied by cycles per second per cylinder and cylinder count.
  • Input power is calorific value times fuel mass-flow rate. Brake power is TωT\omega, and friction power is indicated power minus brake power.
  • Overall, thermal and mechanical efficiencies are respectively brake/input, indicated/input and brake/indicated power.
  • Other supplied cycles require interpretation using the same ideas.
Worked example

A four-cylinder four-stroke engine runs at 1800rev min11800\,\text{rev min}^{-1}. Each indicator loop has area 500J500\,\text{J}. Calculate the indicated power.

  1. 1.1800rev min1=30rev s11800\,\text{rev min}^{-1}=30\,\text{rev s}^{-1}.
  2. 2.A four-stroke cylinder completes one cycle per two revolutions, giving 15cycles s115\,\text{cycles s}^{-1}.
  3. 3.Pi=(500)(15)(4)=3.0×104WP_i=(500)(15)(4)=3.0\times10^4\,\text{W}.

Answer: The indicated power is 30kW30\,\text{kW}.

Common mistakes

  • Don't use crankshaft revolutions per second as cycles per second for a four-stroke cylinder and double the indicated power.
  • Don't calculate thermal efficiency using brake power instead of indicated power.
  • Don't subtract indicated power from brake power and obtain a negative friction power.

Exam tip

Write the three efficiency ratios in words before substituting because their numerators are different.

Tier 1 · Easy

ORIGINAL

An engine produces a steady crankshaft torque of 140N m140\,\text{N m} at 3000rev min13000\,\text{rev min}^{-1}. Calculate its brake power.

[2 marks]

Total for this question: 2

Tier 2 · Standard

ORIGINAL

The area enclosed by the indicator diagram for one cylinder of a four-stroke engine is 620J620\,\text{J} per cycle. The four-cylinder engine runs at 2400rev min12400\,\text{rev min}^{-1}. Determine the indicated power.

[3 marks]

Total for this question: 3

Tier 3 · Hard

ORIGINAL

A four-cylinder, four-stroke engine runs at 3000rev min13000\,\text{rev min}^{-1}. Each cylinder's indicator-loop area is 380J380\,\text{J}. The brake torque is 105N m105\,\text{N m}. Fuel of calorific value 44.0MJ kg144.0\,\text{MJ kg}^{-1} is supplied at 1.60×103kg s11.60\times10^{-3}\,\text{kg s}^{-1}. Determine the indicated power, brake power, friction power, and thermal efficiency.

[6 marks]

Total for this question: 6

3.11.2.5

Second Law and engines

Notes
Evidence from your answers: none yet
Your confidence:

A self-report of how sure you feel. It does not measure mastery. Evidence from your answers reaches secure after the latest Tier 2/3 attempt is correct, with three correct distinct drills across at least two dates and two practice sources.

Explanation

  • The First Law alone does not forbid complete conversion of heat into work, but the Second Law requires a heat engine to operate between a hot source and a colder sink.
  • Each cycle receives QHQ_H, produces work WW and rejects QCQ_C, so QH=W+QCQ_H=W+Q_C and η=W/QH=(QHQC)/QH\eta=W/Q_H=(Q_H-Q_C)/Q_H.
  • The maximum theoretical efficiency is ηmax=(THTC)/TH\eta_{\max}=(T_H-T_C)/T_H, with temperatures in kelvin.
  • Practical efficiency is lower because of friction, unwanted heat transfer, incomplete combustion and irreversible finite-rate processes.
  • Combined heat and power schemes improve total energy use by using both WW and useful rejected heat, but this utilisation fraction is not the engine's heat-to-work efficiency.
A heat engine must reject energy QCQ_C to a cold sink while producing work.
Worked example

An engine receives 8.0kJ8.0\,\text{kJ} and rejects 5.2kJ5.2\,\text{kJ} per cycle. Calculate its efficiency.

  1. 1.Use energy conservation: W=QHQC=8.05.2=2.8kJW=Q_H-Q_C=8.0-5.2=2.8\,\text{kJ}.
  2. 2.Use η=W/QH\eta=W/Q_H.
  3. 3.η=2.8/8.0=0.35\eta=2.8/8.0=0.35.

Answer: The efficiency is 0.350.35, or 35%35\%.

Common mistakes

  • Don't claim a cyclic engine can turn all QHQ_H into work without rejecting energy to a sink.
  • Don't use temperatures in degrees Celsius in ηmax=(THTC)/TH\eta_{\max}=(T_H-T_C)/T_H.
  • Don't call the combined work-plus-heating utilisation fraction a heat-engine efficiency.

Exam tip

When comparing actual and maximum efficiency, identify at least one irreversible loss mechanism in the practical engine.

Tier 1 · Easy

ORIGINAL

A heat engine receives 5.0kJ5.0\,\text{kJ} from its hot source and rejects 3.2kJ3.2\,\text{kJ} to its sink each cycle. Calculate its efficiency.

[2 marks]

Total for this question: 2

Tier 2 · Standard

ORIGINAL

An engine operates between a source at 720K720\,\text{K} and a sink at 310K310\,\text{K}. Determine its maximum theoretical efficiency and explain why a practical engine operating at these temperatures has a lower efficiency.

[3 marks]

Total for this question: 3

Tier 3 · Hard

ORIGINAL

A combined heat and power plant receives thermal energy at 120MW120\,\text{MW} and produces 45MW45\,\text{MW} of electrical work. It supplies 60MW60\,\text{MW} of otherwise rejected heat to nearby buildings. The engine source and sink temperatures are 850K850\,\text{K} and 300K300\,\text{K}. Calculate the engine efficiency, the total useful-energy fraction, and the maximum theoretical efficiency. Explain the difference between the last two quantities.

[5 marks]

Total for this question: 5

3.11.2.6

Reversed heat engines

Notes
Evidence from your answers: none yet
Your confidence:

A self-report of how sure you feel. It does not measure mastery. Evidence from your answers reaches secure after the latest Tier 2/3 attempt is correct, with three correct distinct drills across at least two dates and two practice sources.

Explanation

  • A reversed heat engine uses work input WW to transfer energy QCQ_C from a cold region to a hot region, delivering QH=QC+WQ_H=Q_C+W. A refrigerator's useful transfer is QCQ_C, so COPref=QC/W=QC/(QHQC)\mathrm{COP}_{\text{ref}}=Q_C/W=Q_C/(Q_H-Q_C).
  • A heat pump's useful transfer is QHQ_H, so COPhp=QH/W=QH/(QHQC)\mathrm{COP}_{\text{hp}}=Q_H/W=Q_H/(Q_H-Q_C). Hence COPhp=COPref+1\mathrm{COP}_{\text{hp}}=\mathrm{COP}_{\text{ref}}+1.
  • Ideal limits are TC/(THTC)T_C/(T_H-T_C) and TH/(THTC)T_H/(T_H-T_C) respectively, using kelvin. COP can exceed one because it compares heat transferred with work input; it is not a conversion efficiency.
  • Only the basic principles and uses of refrigerators and heat pumps are required.
  • Detailed device cycles are not required.
Work input drives heat from a cold region to a hot region in a reversed heat engine.
Worked example

A refrigerator removes 7.5kJ7.5\,\text{kJ} from its cold space while using 2.5kJ2.5\,\text{kJ} of work. Calculate both refrigerator and heat-pump COP values for the same device.

  1. 1.COPref=QC/W=7.5/2.5=3.0\mathrm{COP}_{\text{ref}}=Q_C/W=7.5/2.5=3.0.
  2. 2.QH=QC+W=7.5+2.5=10.0kJQ_H=Q_C+W=7.5+2.5=10.0\,\text{kJ}.
  3. 3.COPhp=QH/W=10.0/2.5=4.0\mathrm{COP}_{\text{hp}}=Q_H/W=10.0/2.5=4.0.

Answer: COPref=3.0\mathrm{COP}_{\text{ref}}=3.0 and COPhp=4.0\mathrm{COP}_{\text{hp}}=4.0.

Common mistakes

  • Don't use QHQ_H as the useful transfer when calculating refrigerator COP.
  • Don't use temperatures in degrees Celsius in the ideal COP expressions.
  • Don't reject a COP above one as impossible by confusing COP with efficiency.

Exam tip

Identify the desired heat transfer first: QCQ_C for refrigeration and QHQ_H for space heating.

Tier 1 · Easy

ORIGINAL

A refrigerator removes 360J360\,\text{J} from its cold compartment for every 120J120\,\text{J} of electrical work supplied. Calculate its coefficient of performance.

[2 marks]

Total for this question: 2

Tier 2 · Standard

ORIGINAL

A heat pump delivers 14kW14\,\text{kW} to a building while consuming 4.0kW4.0\,\text{kW} of electrical power. Determine its heat-pump coefficient of performance and the rate at which it extracts energy from outside.

[3 marks]

Total for this question: 3

Tier 3 · Hard

ORIGINAL

A heat pump keeps a building at 293K293\,\text{K} when the outside temperature is 268K268\,\text{K}. Its actual coefficient of performance is 42%42\% of the maximum theoretical value. Calculate the electrical power required when the heat delivered to the building is 18kW18\,\text{kW}.

[5 marks]

Total for this question: 5

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