Educerie
Level

This whole subtopic is higher level. Nothing in it is on an SL paper.

Educerie · IB Diploma · Physics

Theme B The particulate nature of matter · B.4 Thermodynamics

Level
HL only, the whole subtopic. If you are SL, none of this is on your papers.
Themes (key concepts)
energy and particles. The first law is conservation of energy written for a gas; the second law comes from counting the ways particles can be arranged, and it decides which energy transfers can happen at all.
The question this unit answers
how can the energy stored in and transferred by a system be analysed, and what decides the direction in which the system will evolve?
Where it is examined
HL Paper 1A multiple choice (sign conventions, which quantity is zero in which process); HL Paper 2, where a gas cycle on a P–V diagram is a standard structured question worth 6 to 10 marks across its parts (work from areas, Q for each stage, efficiency, comparison with Carnot), and where the second law appears as a 2 to 4 mark explanation; Paper 1B data questions on gas experiments.

What you must be able to do

You must be able toLevelWhat it looks like in the exam
Distinguish closed and isolated systemsHL"State what is meant by an isolated system" (1 mark)
Apply the first law Q = ΔU + W with the Clausius sign conventionHLPaper 2, 2 or 3 marks per stage of a process
Calculate work as W = PΔV, and as the area under a P–V graph when pressure changesHL"Determine the work done by the gas from A to B" (2 marks)
Use ΔU = (3/2)NkBΔT = (3/2)nRΔT for a monatomic ideal gasHLInside most cycle calculations
Describe isovolumetric, isobaric, isothermal and adiabatic processes and draw them on a P–V diagramHL"Identify the process from C to D" (1 mark), "Sketch…" (2 marks)
Use PV^(5/3) = constant for adiabatic changes of a monatomic ideal gasHL"Calculate the pressure at the end of the adiabatic compression" (2 marks)
Explain how a cyclic process runs a heat engine and calculate its efficiencyHL"Calculate the efficiency of the engine" (2 or 3 marks)
Describe the Carnot cycle and use ηCarnot = 1 − Tc/ThHL"Compare the efficiency with the Carnot efficiency" (2 marks)
Define entropy and use ΔS = ΔQ/T and S = kB ln Ω, including a coin model of microstatesHL"Calculate the change in entropy of…" (2 marks)
State the second law in Clausius, Kelvin and entropy forms, and apply it to reversible, irreversible and non-isolated systemsHL"Explain how the entropy of the water can decrease without breaking the second law" (3 marks)

Before you start

You need B.3 in full: PV = nRT, P–V diagrams and isotherms, and U = (3/2)nRT for a monatomic ideal gas, whose internal energy depends only on temperature. You also need work = force × displacement from A.3 and the idea of thermal energy transfer from B.1. Every temperature is in kelvin.


1The idea in one paragraph

A gas in a cylinder can gain or lose energy in two ways: by heat, thermal energy that flows because of a temperature difference, and by work, when its boundary moves against a force. The first law of thermodynamics is conservation of energy for the gas: heat in equals the rise in internal energy plus the work the gas does. Take the gas round a closed loop of changes and it returns to where it started, so any net heat absorbed has been turned into work: that is a heat engine. The second law says the conversion is never complete. Some energy must always be rejected to something colder, and the best any engine working between two temperatures can do is the Carnot efficiency, 1 − Tc/Th. Behind the second law is entropy: a count of how many microscopic arrangements match what you see. Isolated systems drift towards the macrostates with the most arrangements, and that drift is why heat flows from hot to cold and never back on its own.

2Systems, and the sign convention

A system is whatever you choose to draw a boundary around: here, usually, a fixed amount of gas in a cylinder. Two kinds matter.

  • A closed system exchanges no matter with its surroundings, but energy can cross the boundary in both directions, as heat or as work. A gas sealed in a cylinder with a movable piston is closed.
  • An isolated system exchanges neither matter nor energy. Nothing crosses the boundary at all. A perfectly insulated, rigid, sealed box would be isolated; so, taken as a whole, is the universe.

The IB uses the Clausius sign convention, and every mark in this subtopic depends on it. Figure 1 shows it on a cylinder.

Figure 1 · A gas as a closed system, with the IB sign convention Figure 1 · A gas as a closed system, with the IB sign convention gas: internal energy U Q > 0: heat supplied to the gas W > 0: gas expands, does work on piston Signs to learn Q > 0 heat in, Q < 0 heat out W > 0 gas expands W < 0 gas is compressed ΔU > 0 temperature rises Q is energy supplied to the gas as heat; W is work done by the gas. Q = ΔU + W.
Figure 1 · A gas as a closed system, with the IB sign convention
  • Q is the resultant thermal energy supplied to the system. Heat in: Q is positive. Heat out: Q is negative.
  • W is the resultant work done by the system. The gas expands and pushes the piston out: W is positive. The gas is compressed, so work is done on it: W is negative.
  • ΔU is the change in the system's internal energy. For an ideal gas, ΔU is positive exactly when the temperature rises.

3The first law of thermodynamics

Energy supplied to the gas as heat has only two places to go: into the gas's internal energy, or out again as work done by the gas. So:

Q = ΔU + W

This is conservation of energy applied to a closed system, nothing more. What makes it tricky is the signs.

Worked example 1: the signs in action. (a) A gas absorbs 500 J of heat and does 200 J of work pushing a piston out. (b) A different gas is compressed, with 150 J of work done on it, while it loses 40 J of heat to the surroundings. Find ΔU in each case.

(a) Q = +500 J, W = +200 J
ΔU = Q − W = 500 − 200 = +300 Jtemperature rises
(b) Q = −40 J, W = −150 Jheat out, work done ON the gas
ΔU = Q − W = −40 − (−150) = +110 Jtemperature rises

In (b), compression pushes 150 J in, heat leaks 40 J out, and 110 J stays. If your answer came out as −190 J, you added the work instead of subtracting a negative.

Internal energy of a monatomic ideal gas. From B.3, U = (3/2)nRT, so

ΔU = (3/2)NkBΔT = (3/2)nRΔT

and since PV = nRT, the same thing can be written ΔU = (3/2)Δ(PV). That last form is a gift in cycle questions: you can read ΔU straight off the pressure and volume at two points of a P–V diagram without ever finding n or T.

4Work done by a gas, and the area under the curve

Picture the gas pushing a piston of area A through a small distance Δx at constant pressure P. The force is PA, so the work is PA × Δx, and AΔx is the change in volume:

W = PΔV (constant pressure)

On a P–V diagram that is the area of a rectangle, as Figure 2(a) shows. If the pressure changes as the gas expands, split the change into thin strips; each strip is a small PΔV, and together they add up to the area under the line. That is true whatever the shape of the line, and it is how the guide expects you to handle "situations where pressure is not constant".

Figure 2 · Work done by a gas is the area under its P–V line Figure 2 · Work done by a gas is the area under its P–V line (a) Constant pressure Pressure P / 10⁵ Pa Volume V / 10⁻³ m³ W = PΔV 2 5 1.0 (b) Pressure falls as it expands Pressure P / 10⁵ Pa Volume V / 10⁻³ m³ W = area 4.0 1 X 1.0 4 Y Constant pressure: W = PΔV, a rectangle. Changing pressure: the area is still W, whatever its shape.
Figure 2 · Work done by a gas is the area under its P–V line

The area gives the size; the direction gives the sign. Moving to the right (expansion), W is positive. Moving to the left (compression), W is negative. A vertical line (constant volume) has no area under it, so W = 0.

Worked example 2: pressure not constant. A monatomic ideal gas goes from X (1.0 × 10⁻³ m³, 4.0 × 10⁵ Pa) to Y (4.0 × 10⁻³ m³, 1.0 × 10⁵ Pa) along the straight line of Figure 2(b). Determine W, ΔU and Q.

W = area of trapezium = ½ (4.0 × 105 + 1.0 × 105) × 3.0 × 10−3
W = +750 Jexpansion, so positive
ΔU = (3/2) Δ(PV) = 1.5 × (100 − 400)PV at X = 400 J, at Y = 100 J
ΔU = −450 J
Q = ΔU + W = −450 + 750 = +300 J

The gas does 750 J of work but only 300 J came in as heat; the other 450 J came out of its internal energy, so it cooled. The guide says quantitative problems use monatomic ideal gases, which is why (3/2) is safe here.

5Four processes, each keeping one thing fixed

The guide names four processes. Each is obtained by keeping one quantity fixed, and each makes one term of the first law vanish or simplifies it. Figure 3 draws all four from the same starting state S.

Figure 3 · Four processes from the same starting state Figure 3 · Four processes from the same starting state Pressure P Volume V S isovolumetric: V fixed isobaric: P fixed isothermal: T fixed adiabatic: Q = 0 The adiabat is steeper than the isotherm: with no heat supplied, the gas cools as it expands.
Figure 3 · Four processes from the same starting state
ProcessWhat is fixedOn a P–V diagramFirst law becomes
Isovolumetric (isochoric)volumevertical lineW = 0, so Q = ΔU
Isobaricpressurehorizontal lineW = PΔV, Q = ΔU + PΔV
Isothermaltemperaturecurve PV = constantΔU = 0, so Q = W
Adiabaticno heat crosses: Q = 0curve PV^(5/3) = constant, steeper0 = ΔU + W, so W = −ΔU

Students swap the last two rows. Isothermal: T is fixed, so ΔU = 0; if the gas expands and does work, exactly that much heat must flow in. It needs a slow change with good thermal contact. Adiabatic: no heat crosses, so the work done by an expanding gas comes out of its internal energy and it cools; compress it and it heats up. It needs good insulation or a change too fast for heat to flow, like the compression stroke of a diesel engine, which heats the air enough to ignite the fuel.

That cooling is why the adiabat in Figure 3 is steeper than the isotherm. Expanding from S, both lose pressure because the volume grows, but the adiabatic gas also cools, so its pressure falls further. For a monatomic ideal gas the adiabat obeys:

PV^(5/3) = constant (adiabatic, monatomic ideal gas)

Worked example 3: an adiabatic compression. Helium at 1.0 × 10⁵ Pa and 300 K occupies 1.20 × 10⁻³ m³. It is compressed adiabatically to 0.30 × 10⁻³ m³. Calculate the final pressure, the final temperature and the work done.

P2 = P1 (V1 ÷ V2)5/3 = 1.0 × 105 × 45/3
P2 = 1.0 × 106 Pa
T2 = T1 × P2V2 ÷ P1V1 = 300 × 302.4 ÷ 120from PV = nRT
T2 = 756 K ≈ 760 K
ΔU = (3/2)(P2V2 − P1V1) = 1.5 × (302.4 − 120) = 274 J
W = −ΔU = −274 JQ = 0; work done ON the gas

The volume went down by a factor of 4 and the pressure up by more than 10, because the temperature rose as well. An isothermal compression by the same factor would only have multiplied the pressure by 4.

6Cycles and heat engines

A cyclic process takes a gas through a series of changes and back to its starting state. Because it ends where it began, its temperature is the same, so over a whole cycle ΔU = 0. The first law then says:

Over a cycle: net Q = net W

On a P–V diagram, the net work in a cycle is the area enclosed by the loop. Run clockwise, the gas does more work expanding (at higher pressure) than is done on it while it is compressed, so net work is positive: the cycle is an engine.

A heat engine is any device that runs a cycle like this to turn thermal energy into work. Figure 4 shows the energy flows. The engine takes in energy Qh from a hot reservoir (burning fuel, steam from a boiler), does useful work W, and rejects the remainder Qc to a cold reservoir (the air, a river, a cooling tower). Energy is conserved, so Qh = W + Qc. Its efficiency is

η = useful work ÷ input energy = W ÷ Qh

Figure 4 · A heat engine as a flow of energy Figure 4 · A heat engine as a flow of energy hot reservoir at Th cold reservoir at Tc engine Qh = 1800 J W = 400 J useful work Qc = 1400 J η = 400 ÷ 1800 = 0.22 Energy in = work out + energy rejected, and the energy rejected can never be zero.
Figure 4 · A heat engine as a flow of energy

Worked example 4: an engine cycle. A monatomic ideal gas is taken round the rectangular cycle of Figure 5. Find Q for each stage, the net work and the efficiency.

Figure 5 · A cycle: net work is the enclosed area Figure 5 · A cycle: net work is the enclosed area Pressure P / 10⁵ Pa Volume V / 10⁻³ m³ net W = 400 J A B C D 1.0 3.0 1.0 3.0 +300 J +1500 J −900 J −500 J Monatomic ideal gas, run clockwise. Heat values are Q for each stage.
Figure 5 · A cycle: net work is the enclosed area

Use ΔU = (3/2)Δ(PV), with P in Pa and V in m³, so PV is in joules. PV is 100 J at A, 300 J at B, 900 J at C and 300 J at D.

StageProcessW / JΔU / JQ = ΔU + W / J
A → Bconstant volume, P rises01.5 × (300 − 100) = +300+300
B → Cconstant pressure, expands3.0 × 10⁵ × 2.0 × 10⁻³ = +6001.5 × (900 − 300) = +900+1500
C → Dconstant volume, P falls01.5 × (300 − 900) = −900−900
D → Aconstant pressure, compressed1.0 × 10⁵ × (−2.0 × 10⁻³) = −2001.5 × (100 − 300) = −300−500
Whole cycle+4000+400

The net work, 400 J, is the area of the rectangle, 2.0 × 10⁵ Pa × 2.0 × 10⁻³ m³, which is a good check. The input energy is only the heat that comes in: 300 + 1500 = 1800 J. The 1400 J that leaves on C → D and D → A is Qc.

η = W ÷ Qh = 400 ÷ 1800 = 0.22

The classic mistake is to divide by the net heat, 400 J, and get an efficiency of 1.

7The Carnot cycle and the limit on efficiency

The Carnot cycle is an ideal, reversible cycle made of two isotherms and two adiabats, shown in Figure 6.

Figure 6 · The Carnot cycle: two isotherms and two adiabats Figure 6 · The Carnot cycle: two isotherms and two adiabats Pressure P Volume V Th isotherm Tc isotherm A B C D Qh in at Th Qc out at Tc adiabatic expansion adiabatic compression Heat enters only on A → B and leaves only on C → D.
Figure 6 · The Carnot cycle: two isotherms and two adiabats
  • A → B: isothermal expansion at the hot temperature Th. Heat Qh flows in.
  • B → C: adiabatic expansion. No heat; the gas does work and cools from Th to Tc.
  • C → D: isothermal compression at the cold temperature Tc. Heat Qc flows out.
  • D → A: adiabatic compression. No heat; the gas warms from Tc back to Th.

All the heat enters at the single highest temperature and leaves at the single lowest one, with no heat flowing across a temperature difference on the way. That is what makes it the most efficient cycle possible between two reservoirs. Its efficiency depends only on those two temperatures:

ηCarnot = 1 − Tc ÷ Th (temperatures in kelvin)

No real engine working between the same two temperatures can beat this. Real engines have friction, heat leaks, and heat flowing across finite temperature differences, all of which are irreversible and push the efficiency below the Carnot value.

Worked example 5: a power station. Steam enters a turbine at 540 °C and the condenser is at 30 °C. Find the maximum possible efficiency.

Th = 540 + 273 = 813 K, Tc = 30 + 273 = 303 K
ηCarnot = 1 − 303 ÷ 813 = 0.63

Real power stations manage far less, and even the ideal limit leaves over a third of the input to be rejected, which is why they need cooling towers or a river. Plug in degrees Celsius instead (1 − 30/540 = 0.94) and the answer is wildly wrong.

For the cycle of Figure 5, the hottest point is C and the coldest A. Since T ∝ PV, TC ÷ TA = 900 ÷ 100 = 9, so a Carnot engine between those temperatures would reach 1 − 1/9 = 0.89. The rectangular cycle's 0.22 is far below it, because it takes in heat at every temperature from TA up to TC, not just at the top.

The history is a nature-of-science point: the steam engine came before the theory, and the question of why engines could not be made more efficient is what led to the second law.

8Entropy, two ways

Entropy, S, is a thermodynamic quantity that relates to the disorder of the particles in a system: roughly, how spread out the energy is and how many ways the particles could be arranged without the system looking any different. The guide gives two ways to calculate it.

From heat and temperature. When a quantity of heat ΔQ is transferred to a system at temperature T, its entropy changes by

ΔS = ΔQ ÷ T

with ΔQ positive for heat in and T in kelvin. The unit of entropy is J K⁻¹. The formula applies directly when T stays constant, as in melting or boiling, or when ΔQ is small enough that T barely moves.

Worked example 6: melting ice. 0.50 kg of ice at 0 °C melts in a room at 20 °C. The specific latent heat of fusion of ice is 3.34 × 10⁵ J kg⁻¹. Find the entropy change of the ice, of the room, and of the two together.

Q = mL = 0.50 × 3.34 × 105 = 1.67 × 105 J
ΔSice = +1.67 × 105 ÷ 273 = +612 J K−1
ΔSroom = −1.67 × 105 ÷ 293 = −570 J K−1the room loses the same Q
ΔStotal = 612 − 570 = +42 J K−1

The ice gains more entropy than the room loses, because the same Q is divided by a smaller temperature. That is the whole second law in a single example.

From counting microstates. A macrostate is what you can measure: pressure, volume, temperature, or, with coins, how many heads. A microstate is one exact arrangement of every particle, or every coin, that gives that macrostate. If Ω is the number of microstates for a macrostate, then

S = kB ln Ω

where kB is the Boltzmann constant. The guide suggests a coin model, and Figure 7 uses it. Throw four coins. There is only one way to get four heads (HHHH), but six ways to get two heads (HHTT, HTHT, HTTH, THHT, THTH, TTHH). Every microstate is equally likely, so two heads turns up six times as often as four heads.

Figure 7 · Counting microstates with coins Figure 7 · Counting microstates with coins (a) 4 coins: 16 microstates Microstates Ω Number of heads 1 0 4 1 6 2 4 3 1 4 (b) 100 coins Share of all microstates Number of heads 0 50 100 Ω(50 heads) ≈ 1.0 × 10²⁹ Ω(100 heads) = 1 With more coins, the evenly mixed macrostates hold almost all the microstates. That is why disorder wins.
Figure 7 · Counting microstates with coins

The entropy of the two-heads macrostate is kB ln 6 = 1.38 × 10⁻²³ × 1.79 = 2.5 × 10⁻²³ J K⁻¹; that of four heads is kB ln 1 = 0. Scale up: 100 coins have about 1.0 × 10²⁹ microstates with 50 heads and one with 100 heads. With 10²³ molecules, the evenly spread macrostates hold so many of the microstates that a system left alone is practically certain to be found in them. That is what "entropy increases" means: ordered arrangements are so outnumbered they are never chosen by chance.

9The second law of thermodynamics

The guide wants the second law in three forms. They say the same thing from different sides.

Clausius form. Thermal energy cannot flow spontaneously from a colder body to a hotter one. A refrigerator moves heat from cold to hot, but only because work is done on it; with no work, heat only flows from hot to cold.

Kelvin form. No cyclic process can take thermal energy from a single reservoir and convert it completely into work. Every heat engine must reject some energy to a colder reservoir, so η < 1 always. This is the form behind the Carnot limit and behind the guide's linking question on why every engine and energy source has an upper limit on efficiency.

Entropy form. The entropy of an isolated system never decreases. In a reversible process (an idealisation, like the Carnot cycle) it stays constant; in an irreversible process it increases. Processes in real isolated systems are almost always irreversible (friction, heat flowing across a temperature difference, gases mixing), so the entropy of a real isolated system always increases.

Figure 8 shows why the Clausius form and the entropy form are the same law. Let 1000 J flow from a body at 400 K to a body at 300 K, both inside an isolated system.

Figure 8 · 1000 J flows from hot to cold: entropy goes up Figure 8 · 1000 J flows from hot to cold: entropy goes up hot body T = 400 K ΔS = −1000 ÷ 400 = −2.50 J K⁻¹ cold body T = 300 K ΔS = +1000 ÷ 300 = +3.33 J K⁻¹ Q = 1000 J total ΔS = +0.83 J K⁻¹ > 0 The cold body gains more entropy than the hot body loses, because the same Q is divided by a smaller T.
Figure 8 · 1000 J flows from hot to cold: entropy goes up

The total entropy rises by 0.83 J K⁻¹, so the flow is allowed. Run it backwards, from cold to hot, and every sign flips: the total would fall by 0.83 J K⁻¹, which the entropy form forbids. That is the Clausius statement.

Entropy can fall locally. The second law is about isolated systems. A system that is not isolated can lose entropy, as long as its surroundings gain at least as much. Water freezing in a freezer becomes more ordered and its entropy falls; but the freezer pumps that heat, plus the work its motor does, out into the kitchen, and the kitchen's entropy rises by more. A growing plant builds ordered structures, paid for by sunlight arriving from a very hot Sun and heat leaving to cold space. Whenever you meet a local decrease, find the surroundings where the larger increase happens.

The universe. As the ultimate isolated system, the universe's entropy can only rise. That gives time a direction (eggs break, never un-break) and points to a far future where energy is spread so evenly that no work can be extracted anywhere.

10Where marks are lost

  1. Getting the sign of W wrong. W is work done by the gas. Compression means W is negative. Writing Q = ΔU − W is the other textbook convention and gives the wrong answers here.
  2. Saying "no heat, so no temperature change". In an adiabatic process Q = 0 but the temperature does change, because work is done. The process with no temperature change is isothermal.
  3. Using degrees Celsius in ηCarnot or ΔS = ΔQ/T. Both need kelvin. 1 − 30/540 is not an efficiency.
  4. Dividing by net heat when finding efficiency. Efficiency is W ÷ (heat in). Adding the negative heats as well gives η = 1.
  5. Area under the line for a cycle. For a cycle, the net work is the area inside the loop, not the area under one side of it.
  6. "Entropy always increases." Only for an isolated system. A fridge, a living cell and freezing water all show local decreases.
  7. Drawing the adiabat shallower than the isotherm. From the same point, the adiabatic curve is always steeper.
  8. Using PV^(5/3) for an isothermal change. PV = constant for isothermal; PV^(5/3) = constant only for adiabatic changes of a monatomic ideal gas.

11Draw it right

  1. Every P–V diagram has P on the vertical axis and V on the horizontal, each with a unit if values are given.
  2. Isovolumetric changes are vertical, isobaric horizontal, isothermal a curve PV = constant, adiabatic a steeper curve. Label each process.
  3. Put an arrow on every stage of a process or cycle. The direction decides the sign of W.
  4. Shade the area that is the work: under the line for one stage, inside the loop for a cycle.
  5. A Carnot cycle has exactly two isotherms (labelled Th and Tc) and two adiabats joining them, with heat in on the upper isotherm and heat out on the lower one.
  6. A heat engine diagram shows a hot reservoir, the engine, a cold reservoir, and three labelled arrows: Qh in, W out, Qc out, with the widths (if you draw them) matching Qh = W + Qc.

12Try it

Marks in brackets. Take R = 8.31 J K⁻¹ mol⁻¹, kB = 1.38 × 10⁻²³ J K⁻¹. All gases are monatomic ideal gases. Answers and marker's notes are at the end.

Q1. (Paper 1A style) An ideal gas expands adiabatically. Which is correct? 1 mark

A. Q = 0, W > 0, ΔU < 0 &nbsp;&nbsp; B. Q = 0, W > 0, ΔU > 0 &nbsp;&nbsp; C. Q > 0, W > 0, ΔU = 0 &nbsp;&nbsp; D. Q = 0, W < 0, ΔU < 0

Q2. 0.20 mol of gas is heated at a constant pressure of 2.0 × 10⁵ Pa from 300 K to 400 K.

(a) Calculate the change in internal energy of the gas. 2 marks

(b) Show that the work done by the gas is about 170 J. 2 marks

(c) Calculate the thermal energy supplied to the gas. 1 mark

Q3. Gas at 2.0 × 10⁵ Pa occupies 4.0 × 10⁻³ m³. It expands adiabatically to 8.0 × 10⁻³ m³.

(a) Calculate the final pressure. 2 marks

(b) Determine the work done by the gas. 2 marks

(c) Explain, using the first law, why the temperature of the gas falls. 2 marks

Q4. An engine takes in 2.5 kJ of energy per cycle from combustion gases at 1200 K and rejects energy to the air at 400 K. It does 0.60 kJ of useful work per cycle.

(a) Calculate the efficiency of the engine and the energy rejected per cycle. 2 marks

(b) Calculate the Carnot efficiency for these temperatures. 1 mark

(c) Explain, with reference to the second law, why no engine could have an efficiency of 1. 2 marks

Q5. (a) Six coins are tossed. Determine the entropy of the macrostate "three heads", using S = kB ln Ω. 2 marks

(b) 200 J of thermal energy flows from a body at 500 K to a body at 250 K. Calculate the total change in entropy, and explain what your answer shows. 3 marks

(c) Water in a freezer turns to ice and its entropy decreases. Explain why this does not break the second law. 2 marks

Q6. (Paper 1B style) A gas in a sealed syringe is compressed quickly while a sensor records its pressure. The data are invented for this question; assume their uncertainties are too small to affect your conclusions.

V / cm³50403020
P / kPa100143225420

(a) Using the first and last readings, show that the compression is not isothermal. 2 marks

(b) Using the first and last readings, deduce whether the compression is adiabatic. 2 marks

(c) Suggest a reason for your answer to (b). 1 mark

13In one breath

Closed systems exchange energy but not matter; isolated systems exchange neither. The first law, Q = ΔU + W, is energy conservation with Q the heat supplied to the gas and W the work done by it, so compression makes W negative, and for a monatomic ideal gas ΔU = (3/2)nRΔT = (3/2)Δ(PV). Work is PΔV at constant pressure and the area under the P–V line otherwise. Isovolumetric: W = 0. Isobaric: W = PΔV. Isothermal: ΔU = 0, so Q = W. Adiabatic: Q = 0, W = −ΔU, PV^(5/3) constant, steeper than an isotherm. Over a cycle ΔU = 0, net work is the enclosed area, and efficiency is W over heat in. The Carnot cycle sets the limit 1 − Tc/Th, in kelvin. Entropy: ΔS = ΔQ/T, and S = kB ln Ω counts microstates. The second law: heat does not flow unaided from cold to hot; no engine turns heat wholly into work; the entropy of an isolated system never falls and rises in every real process, though it can fall locally if the surroundings gain more.


Answers

Q1. A. No heat crosses (Q = 0); the gas expands, so it does work (W > 0); by Q = ΔU + W, ΔU = −W < 0, and the gas cools. A only. C describes an isothermal expansion; D has the sign of W for a compression.

Q2. (a) ΔU = (3/2)nRΔT = 1.5 × 0.20 × 8.31 × 100 = 249 J. (b) At constant pressure, W = PΔV = nRΔT = 0.20 × 8.31 × 100 = 166 J, about 170 J. (c) Q = ΔU + W = 249 + 166 = 415 J. (a) M1 for (3/2)nRΔT, A1 for 249 J. (b) M1 for recognising PΔV = nRΔT at constant pressure (or finding both volumes from PV = nRT), A1 for 166 J shown to three significant figures. (c) A1 for 415 J, ECF from (a) and (b).

Q3. (a) P₂ = P₁(V₁ ÷ V₂)^(5/3) = 2.0 × 10⁵ × 0.5^(5/3) = 6.3 × 10⁴ Pa. (b) Q = 0, so W = −ΔU = −(3/2)(P₂V₂ − P₁V₁) = −1.5 × (6.30 × 10⁴ × 8.0 × 10⁻³ − 2.0 × 10⁵ × 4.0 × 10⁻³) = −1.5 × (504 − 800) = +444 J (4.4 × 10² J). (c) The process is adiabatic, so Q = 0 and the first law gives ΔU = −W. The gas expands and does positive work, so ΔU is negative; the internal energy of an ideal gas is proportional to its temperature, so the temperature falls. (a) M1 for PV^(5/3) = constant, A1. (b) M1 for W = −ΔU with ΔU from (3/2)Δ(PV), A1 for 444 J; ECF from (a). (c) 1 for Q = 0 leading to ΔU = −W, 1 for linking the fall in internal energy to a fall in temperature. "Adiabatic means the temperature falls" with no first-law reasoning scores 0.

Q4. (a) η = W ÷ Qh = 0.60 ÷ 2.5 = 0.24. Qc = Qh − W = 2.5 − 0.60 = 1.9 kJ. (b) ηCarnot = 1 − 400 ÷ 1200 = 0.67. (c) The Kelvin form of the second law: no cyclic process can take heat from a reservoir and convert all of it to work. Some energy must be rejected to a cold reservoir, so W < Qh and η < 1. (Equivalently: for η = 1, Tc would have to be 0 K.) (a) 1 for each value. (b) 1. (c) 1 for stating that energy must be rejected to a colder reservoir / the Kelvin form, 1 for concluding W < Qh. Blaming friction alone scores 0 for (c): even a frictionless engine obeys the limit.

Q5. (a) Number of ways to get three heads from six coins = (6 × 5 × 4) ÷ (3 × 2 × 1) = 20. S = kB ln 20 = 1.38 × 10⁻²³ × 3.00 = 4.1 × 10⁻²³ J K⁻¹. (b) Hot body: ΔS = −200 ÷ 500 = −0.40 J K⁻¹. Cold body: ΔS = +200 ÷ 250 = +0.80 J K⁻¹. Total: +0.40 J K⁻¹. The total entropy increases, so the process is irreversible and happens spontaneously; the reverse flow would decrease entropy and cannot happen on its own. (c) The water is not an isolated system. The freezer transfers the heat removed from the water, plus the work done by its motor, to the surroundings. The entropy increase of the surroundings is at least as great as the decrease of the water, so the total entropy does not decrease. (a) M1 for Ω = 20, A1. (b) M1 for both entropy changes with correct signs, A1 for +0.40 J K⁻¹, 1 for interpreting the increase. (c) 1 for "not isolated", 1 for a larger increase in the surroundings.

Q6. (a) PV at 50 cm³: 100 × 50 = 5000 kPa cm³. PV at 20 cm³: 420 × 20 = 8400 kPa cm³. PV is not constant, so the compression is not isothermal. (b) PV^(5/3) at 50 cm³: 100 × 50^(5/3) = 6.8 × 10⁴; at 20 cm³: 420 × 20^(5/3) = 6.2 × 10⁴ (both in kPa cm⁵). PV^(5/3) falls by about 9%, so the compression is not exactly adiabatic either: the final pressure (420 kPa) is below the adiabatic prediction (about 460 kPa). (c) Some thermal energy leaks from the warming gas through the walls of the syringe during the compression, so Q is not zero and the gas ends cooler, at lower pressure, than an adiabatic compression predicts. (a) M1 for both PV values, A1 for the conclusion. (b) M1 for both PV^(5/3) values or the adiabatic prediction of about 460 kPa, A1 for the conclusion that it is between isothermal and adiabatic. (c) 1 for heat loss through the walls because the compression is not fast enough or the syringe not insulated.


Educerie · written from the published IB Diploma Programme Physics guide, first assessment 2025, section B.4 Thermodynamics. Original text, examples and questions. Diagrams drawn by Educerie. Last reviewed 25 September 2026.

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