Full chapter
Thermodynamic Systems
All 4 topics and the revision summary on one page.
01
Internal energy and thermal equilibrium
Choose which matter belongs to the system. Its internal energy describes its microscopic energy, while heating and work describe energy crossing its boundary.
Define the system and its state
A thermodynamic system is the matter selected for an energy account. Its boundary separates it from the surroundings. For example, a gas inside a cylinder can be the system, with the piston and the room outside it. In a calorimeter, the selected system might instead include the sample, heater and vessel together.
Internal energy U is associated with the distribution of microscopic kinetic and potential energies of the system's particles. It excludes the kinetic energy of the whole system moving together and its gravitational potential energy relative to the surroundings.
At equilibrium, the macroscopic state determines U. Specify the amount, composition and phase as well as the relevant pressure, volume and temperature. A temperature reading alone does not determine the total internal energy of every possible sample.
Internal energy is a state quantity: its change between the same initial and final states does not depend on how the change occurred. Heating Q and work W are transfers during a process. Their separate values can depend on the route, even when the initial and final states are the same. A hot object has internal energy; it does not contain a stored quantity of heat Q.
Temperature describes a particle average
In the classical particle model, thermodynamic temperature is proportional to mean microscopic kinetic energy. For an ideal gas, the precise translational result is:
T is in kelvin. The particle-energy derivation concerns an average per particle, not equal energy for every particle. Increasing the number of particles at the same temperature does not change this average, but can increase the total energy.
For a monatomic ideal gas in this model, internal energy is the total translational kinetic energy:
N is the particle number and n the amount in mol. At the same T, doubling N doubles this U. Two such samples can therefore have the same temperature and different internal energies.
Keep the monatomic ideal-gas condition beside this total-energy equation. Molecular gases and other phases can have additional microscopic energy contributions, so U = 3NkT/2 is not a universal formula for every material.
Thermal contact and equilibrium
When systems at different temperatures are put in thermal contact without a competing imposed transfer, net energy moves by heating from higher to lower temperature. They approach a common temperature. At thermal equilibrium, there is no net heating between them.
Temperature sets the direction of net heating
Two unequal samples are in thermal contact, with insulated surroundings and no other transfer in this model. The dashed outline is their combined system boundary; the connector allows energy transfer between them.
During contact: different temperatures
After settling: thermal equilibrium
Equal temperature determines thermal equilibrium. It does not make the samples' masses or total internal energies equal.
The direction of net heating follows temperature, not which object has more total internal energy. At equal temperature, microscopic exchanges may continue in both directions while their net effect is zero.
A system can also receive energy without a temperature rise. During a phase change under the stated conditions, its microscopic potential-energy contribution can change while temperature remains constant.
Use the zeroth law
If systems A and B are each in thermal equilibrium with a third system C, then A and B are in thermal equilibrium with each other. This is the zeroth law of thermodynamics.
Use a third system to compare temperatures
A and B each reach thermal equilibrium with the same thermometer C at the same unchanged reading. The zeroth law gives the A-B equilibrium relation.
The lines state thermal equilibrium; they do not show an electrical circuit or fixed amounts of transferred energy. A sensor must settle in good contact, and a sensor with significant heat capacity can change a small sample's final state.
This makes a calibrated thermometer useful for comparing temperatures. Allow it to settle in good thermal contact. An early reading may describe the sensor while the sample is still at a different temperature.
A thermometer with substantial heat capacity can itself change a small sample's temperature. It then measures their changed equilibrium. A sensor with small heat capacity, suitable contact and a stable reading reduces this disturbance; equal readings do not imply that the thermometer exchanged equal amounts of energy with different samples.
Optional check Systems A and B separately reach thermal equilibrium with thermometer C at the same unchanged reading. If A and B are then put in thermal contact without other changes, what follows?
02
Heating, work and the first law
Internal energy can change through heating, work or both. Use one work convention throughout the calculation and identify which transfers enter the chosen system.
Set the signs before substituting
For the systems considered here, with no change in the whole system's bulk kinetic or gravitational potential energy, the first law is:
Q is positive for net energy transferred into the system by heating. Won is positive for net work done on it. A positive ΔU means its internal energy increases.
| Transfer | Into the system | Out of the system |
|---|---|---|
| Heating Q | Positive | Negative |
| Work Won | Positive work on it | Negative when it does work |
If work done by the gas is given instead, Wby = -Won, so the same law becomes ΔU = Q - Wby. Do not add positive work by the gas to Q in the work-on convention.
Derive constant-pressure displacement work
Choose the gas as the system. It expands against a constant absolute external pressure pext. For piston area A, the external resisting force has magnitude pextA. Moving the boundary outward through Δx increases the gas volume by ΔV = AΔx.
= pextAΔx = pextΔV
Won = -pextΔV
For expansion, ΔV is positive: the gas does positive work and Won is negative. For compression, ΔV is negative and work on the gas is positive. Use the total stated external pressure, including the surroundings and load, rather than only a gauge-pressure difference.
In a slow, frictionless piston process, the gas pressure is effectively equal to the external pressure. The area under that constant-pressure p-V path then gives the work magnitude. A general gas-pressure curve cannot automatically give work for an irreversible process in which gas and external pressures differ.
Estimate the work scale
Pressure of order 105 Pa acting through a volume increase of order 10-3 m3 gives work of order 102 J. If heating supplies a few hundred joules, an internal-energy increase of a few hundred joules is plausible, with expansion work taking some energy out.
Worked constant-pressure expansion
Separate the input from the energy retained
A fixed amount of monatomic ideal gas expands slowly against pext = 1.20 × 105 Pa, from 2.00 × 10-3 to 3.50 × 10-3 m3. It receives 450 J by heating. The piston is frictionless, and the equilibrium gas pressure is the stated external pressure.
Expansion is outward motion against an inward load
The gas expands slowly with a frictionless piston against constant external pressure pext = 1.20 × 105 Pa. In this quasistatic model, gas pressure is effectively equal to the external pressure.
Use piston area and its outward displacement
Dashed and solid piston faces mark the initial and final states on one length scale. The given area makes ΔV = 0.0100 × 0.150 = 1.50 × 10-3 m3. Blue is displacement; purple is the external load force.
The constant-pressure rectangle gives the work magnitude
For expansion, Wby = +180 J and Won = -180 J. With Q = +450 J, the gas gains ΔU = 450 - 180 = 270 J. Reversing the same path changes the work signs, not the geometric area.
= 1.50 × 10-3 m3
Wby = (1.20 × 105)(1.50 × 10-3)
= +180 J
Won = -180 J
ΔU = 450 + (-180) = +270 J
The p-V graph's scaled rectangle gives the same result: 1.20 × 1.50 × 105 × 10-3 = 180 J. Its geometric area is positive; the direction of the path determines the signed work.
The 450 J input supplies both the 180 J work output and the 270 J internal-energy increase. They are separate destinations for the same input.
There is an independent endpoint check. For this monatomic ideal gas, U = 3nRT/2 = 3pV/2:
U2 = (3/2)(1.20 × 105)(3.50 × 10-3) = 630 J
U2 - U1 = 270 J
If its initial temperature is 300 K, fixed amount and constant pressure give T2 = 300(3.50/2.00) = 525 K. The expansion is not isothermal.
Optional check A gas receives 450 J by heating and does 180 J of work during expansion. Using Delta U = Q + W_on, what is its internal-energy change?
Apply the same convention to different processes
| Process | Q / J | Won / J | ΔU / J |
|---|---|---|---|
| Reverse along the same constant-pressure path | -450 | +180 | -270 |
| Insulated compression with 90 J work input | 0 | +90 | +90 |
| Rigid closed system, 250 J heating and no other work | +250 | 0 | +250 |
In the reverse path, compression work enters the gas but more energy leaves by heating. The latter two rows are independent examples; they are not stated to reach the same endpoints as the expansion.
An insulated system can warm when work is done on it. Insulation makes Q zero under the stated model; it does not make ΔU zero or ensure constant temperature. A rigid boundary removes volume-displacement work, but electrical or other work could still enter unless excluded.
For expansion into a vacuum, pext = 0, so the displacement work is zero even though the volume increases. A volume increase alone therefore does not establish a positive work output.
03
Temperature change and calorimetry
Specific heat capacity relates a sample's heating to its temperature change. An apparatus input may also warm the vessel or supply losses, so isolate the sample's share before calculating c.
Define the property and its conditions
Specific heat capacity c is the energy required by heating per unit mass per unit temperature rise, without a change of state and under the stated process conditions.
c = Q/(mΔT)
Use c in J/(kg K), m in kg and the temperature change in K. A Celsius temperature interval has the same numerical size, so J/(kg °C) gives the same numerical c. An absolute temperature is not interchangeable with a temperature change.
Use a supplied approximately constant c over the interval. Its value can depend on temperature and process. Heating a gas at fixed pressure and at fixed volume are different conditions; do not treat one gas value as process-independent.
Choose the calorimeter boundary
For a system containing the sample, heater, vessel and temperature sensor, electrical input through the heater is work on that assembly. Energy lost to the surroundings by heating is a separate outward transfer. If the sample alone is selected instead, energy passing from the heater into the sample can be heating across its boundary.
Both descriptions can be consistent, but do not count the same input as both electrical work and heating in one account. A calibrated input-energy reading lets the thermal calculation proceed without assuming how the electrical instrument obtained it.
Choose the assembly boundary before allocating input energy
The dashed boundary includes the sample, heater, vessel and temperature sensor. A calibrated 6000 J electrical input is work into this assembly. Energy lost to the surroundings crosses it by heating.
For this assembly, 6000 - 680 = 5320 J remains. The independently supplied apparatus contribution is 40 × 8.0 = 320 J, leaving 5000 J for the sample. The apparatus is assumed to share the sample's stated endpoint temperature change.
A boundary around the sample alone uses the energy transferred into the sample by heating. Do not count the same electrical input once as assembly work and again as a second assembly heating input.
Decide whether corrections matter
Roughly 0.3 kg warming by about 10 K with a few kilojoules input suggests c of order 103 J/(kg K). Apparatus warming of a few hundred joules plus a loss of several hundred joules is of order 1 kJ, which is not automatically negligible beside a 6 kJ input.
Worked corrected calorimetry
Separate sample warming, apparatus warming and loss
A 0.250 kg condensed sample rises by 8.0 K during a measured 6000 J input. There is no phase change and volume work is negligible. Independently supplied apparatus heat capacity is 40 J/K, and the apparatus has the same 8.0 K change between endpoints. Estimated energy lost to the surroundings over that run is 680 J.
Net energy retained by sample
= 6000 - 320 - 680 = 5000 J
c = 5000/(0.250 × 8.0)
= 2500 J/(kg K)
The assembly's internal-energy increase is 6000 - 680 = 5320 J, shared as 5000 J in the sample and 320 J in the apparatus. For the sample-only boundary with negligible work, its net heating is 5000 J.
Allocating all the input to the sample would give c = 6000/(0.250 × 8.0) = 3000 J/(kg K), an overestimate. With positive apparatus and loss terms and no extra source, the sample receives less than the full input, so the corrected c must be below that uncorrected value.
The 1000 J correction is one sixth of the input. The uncorrected c is 20% above the corrected value, because (3000 - 2500)/2500 = 0.20. These percentages use different denominators.
Optional check A 0.250 kg sample warms by 8.0 K during a 6000 J input. Independently supplied corrections are 320 J for apparatus warming and 680 J lost to the surroundings. With no phase change or significant volume work, what is the sample's specific heat capacity?
Make the measurement represent the sample
- Mass: measure the sample separately or subtract the empty container mass. Record the balance range, resolution and zero or tare.
- Temperature: establish sensor contact, record its range and resolution, and use stable readings. Stir a suitable liquid so one sensor reading represents it; avoid treating a local heater hot spot as the whole sample's temperature.
- Input: measure the energy delivered over a defined interval. State whether the heater and vessel belong to the chosen system.
- Apparatus response: use independently determined heat capacity and justify the component temperature changes. Equal endpoint changes do not require every component to share one temperature at every instant.
- Loss: reduce avoidable transfer and estimate the remaining loss under comparable conditions. Record what evidence supports that correction.
Keep the vessel stable and the heater and sensor securely supported so a pulled lead cannot tip or spill the sample. Switch off before adjusting the heater, and let hot parts cool before handling them.
A cooling record or matched reference can help estimate background transfer only if relevant temperatures, exposed areas and surroundings are comparable. A no-heater control at a different temperature does not automatically reproduce the loss during heating. Correction values must come from calibration or other evidence, not be chosen to produce an expected c.
Apply energy conservation to thermal contact
Worked water mixture
Unequal masses need not meet at the arithmetic mean
Mix 0.200 kg water at 50.0°C with 0.300 kg water at 20.0°C. Use c = 4200 J/(kg K) for both. Neglect vessel heat capacity, losses, other work and changes of state.
Taking both water samples as an isolated combined system, energy lost by the hotter sample equals energy gained by the colder one. If the common final temperature is θf:
θf = (0.200 × 50.0 + 0.300 × 20.0)/0.500
= 32.0°C
The energy transferred is 0.200(4200)(50.0 - 32.0) = 15120 J, equal to 0.300(4200)(32.0 - 20.0). The transfer is internal to the combined system; it is not an extra energy input to it.
The final temperature is closer to the initial temperature of the larger heat capacity. Equal final temperature establishes thermal equilibrium, not equal total internal energies.
04
Phase change and latent heat
Decide whether the energy changes temperature or changes phase. At a phase change, energy can enter while temperature stays constant under the stated pressure and conditions.
Define specific latent heat
Specific latent heat l is the energy required by heating per unit mass for a stated change of phase at constant temperature under stated conditions. Its unit is J/kg.
Specific latent heat of fusion concerns melting; specific latent heat of vaporisation concerns liquid becoming vapour. Their values need not be equal. Freezing and condensation transfer energy out under the corresponding reversed conditions.
Here lowercase l denotes the specific quantity. Some references use L for it; check the definition and unit. A value in J/kg is not the total energy for an arbitrary sample.
During a phase change, energy can change microscopic potential energy and supply expansion work without raising temperature. Q = mcΔT describes warming within a phase, so setting ΔT = 0 in that equation does not prove that no energy entered during a phase change.
Split a multi-stage change
Before calculating precisely, roughly 0.1 kg multiplied by a supplied fusion latent heat of order 3 × 105 J/kg needs energy of order 3 × 104 J. Melting should therefore dominate the following account compared with its short warming stages.
Worked warming and melting
Ice at -5.0°C to water at 25.0°C
A 0.0800 kg ice sample ends as liquid water. Use cice = 2100 J/(kg K), lf = 3.34 × 105 J/kg and cwater = 4200 J/(kg K). The stated melting temperature is 0°C. Assume constant properties over each interval, negligible losses and container heat capacity, and negligible volume work for these condensed phases.
| Stage | Calculation | Energy / J |
|---|---|---|
| Warm ice from -5 to 0°C | 0.0800 × 2100 × 5.0 | 840 |
| Melt all ice at 0°C | 0.0800 × 3.34 × 105 | 26720 |
| Warm water from 0 to 25°C | 0.0800 × 4200 × 25.0 | 8400 |
= 35960 J ≈ 36.0 kJ
Use cumulative energy to separate warming from melting
For the stated 0.0800 kg ice/water sample, assume the supplied heat capacities and fusion latent heat, negligible loss and vessel capacity, and negligible volume work. The horizontal coordinate is energy supplied to the sample, not time.
A: 0 kJ, -5 °C. B: 0.840 kJ, 0 °C. C: 27.560 kJ, 0 °C. D: 35.960 kJ, 25 °C.
A-B warms ice; B-C melts it; C-D warms water. The initial stage is genuinely narrow on this energy scale. A flat temperature segment does not mean that energy input has stopped.
The first 840 J warms the ice. The next 26720 J melts it, so complete melting occurs at cumulative input 27560 J. Only after this can further input warm an entirely liquid sample in this model. The graph's energy widths do not by themselves specify stage durations.
Check whether all the material changes phase
Suppose a separate 0.0200 kg ice sample is already at its melting point and receives 5000 J, with negligible other transfers. Complete melting would require:
Mass melted = 5000/(3.34 × 105)
= 0.01497 kg ≈ 15.0 g
About 5.03 g of ice remains. Ice and water coexist at the melting temperature under the stated conditions; there is insufficient energy to melt everything and then warm the liquid.
Optional check A 20.0 g ice sample is already at its melting point. It receives 5000 J with negligible other transfers. Use l_f = 3.34 x 10^5 J/kg. What happens?
Account for work during vaporisation
Latent heating need not all become an internal-energy increase when the sample expands significantly. Choose a fixed sample as the system and use ΔU = Q + Won.
Worked phase-change energy account
Separate heating from expansion work
In a separate supplied model, 0.0100 kg vaporises at constant temperature against external pressure 2.0 × 105 Pa. Use lv = 1.80 × 106 J/kg and a volume increase of 0.0060 m3. These are supplied model properties, not stated values for water.
Wby = pextΔV = 1200 J
Won = -1200 J
ΔU = 18000 - 1200 = 16800 J
The heating supplies both the internal-energy increase and the work output. Constant temperature does not mean zero ΔU, and Q = ml does not automatically make ΔU equal to Q.
Measure fusion latent heat with a matched control
A melting investigation can compare water collected with a measured heater input against a comparable no-heater control. Begin with ice and apparatus at the melting temperature, drain pre-existing water before timed collection, and use the same collection geometry and duration. Measure collected mass with a tared collector and record the input and timing resolutions.
Compare collected melt with a matched no-input control
Begin with ice and apparatus at the melting temperature, and drain pre-existing water before each timed collection. The two runs use the same arrangement and 300 s interval. The supplied model assumes equal background heating and complete collection of the relevant melt.
Heater-on collection
Matched control: no heater input
The extra collected mass is 20.00 - 5.00 = 15.00 g. The measured heater input is 16.7 × 300 = 5010 J, giving lf = 5010/0.01500 = 3.34 × 105 J/kg under the stated assumptions.
This is an input-versus-extra-melt comparison. Initial warming, trapped water or a changed background transfer would undermine the simple subtraction. Because meltwater leaves the holder, a closed fixed-mass account for the holder would omit the outflow.
In the supplied comparison, measured heater power is 16.7 W = 16.7 J/s for 300 s. The heated run collects 20.00 g of water; the comparable control collects 5.00 g.
Extra melted mass = (20.00 - 5.00) g = 0.01500 kg
lf = 5010/0.01500
= 3.34 × 105 J/kg
This calculation assumes complete collection, equal background transfer in the two runs, and that the measured heater input accounts for the additional melting rather than appreciable apparatus warming or an unmatched loss. The control is a conditional correction, not a guarantee that every error has disappeared.
- Ice initially below its melting point: part of the input first warms it. Treating all that input as melting energy can make the inferred l too high.
- Water retained in the apparatus: the collected extra mass can be smaller than the mass actually melted. Dividing input by that underestimated mass can also give too large an l.
- Different background conditions: a heater can change temperature gradients or losses. A control that no longer matches these conditions cannot simply be subtracted as an equal background.
Water leaving the vessel crosses its boundary. Do not apply a closed, fixed-mass first-law account to that vessel while ignoring the outflow. The matched input-and-mass calculation above states the required assumptions without treating the draining vessel as such a system.
05
Revision summary
Choose the system, identify whether energy crosses its boundary as heating or work, then decide whether its temperature, phase or both change.
State quantities and process transfers
Internal energy U is associated with microscopic kinetic and potential energies. It excludes the whole system's bulk kinetic and external gravitational potential energies. At equilibrium the macroscopic state determines U, so ΔU between the same endpoints is independent of the route. Q and W describe transfers during a process and can depend on that route.
Thermodynamic temperature relates to mean microscopic kinetic energy in the classical model. For an ideal gas, mean translational energy is 3kT/2. Only for the stated monatomic ideal-gas model may its full internal energy here be written:
Equal temperature does not imply equal total U. Net heating is from hotter to colder; thermal equilibrium has no net heating. By the zeroth law, if A and B each equilibrate with C, then A and B are in equilibrium with each other.
Keep the work convention visible
Wby = -Won
Constant external pressure:
Wby = pextΔV
Won = -pextΔV
Heating into the system makes Q positive. Expansion makes Won negative; compression makes it positive. In the supplied expansion, 450 J enters by heating, 180 J leaves as work and U increases by 270 J.
Use absolute external pressure. A slow frictionless process permits the gas-pressure p-V area interpretation. Insulation means Q = 0, not necessarily ΔU = 0. A rigid boundary removes volume work but does not exclude all possible work transfers. Expansion into zero external pressure has no displacement work.
Select the thermal equation by stage
Specified phase change: Q = ml
Specific heat capacity is heating required per unit mass per unit temperature rise under stated conditions. Specific latent heat is heating required per unit mass for the specified phase change at constant temperature under stated pressure and conditions. Use compatible mass units and the appropriate property value.
For 0.0800 kg ice at -5.0°C becoming water at 25.0°C, the supplied stages require 840 + 26720 + 8400 = 35960 J. A horizontal temperature segment can have continuing energy input. An energy-axis graph does not directly give a time duration.
If energy is insufficient for a full phase change, calculate the mass changed using Q/l before attempting a temperature rise. If volume work is appreciable, use the first law too: the separate vaporisation example has Q = 18000 J but ΔU = 16800 J after 1200 J work output.
Check a measurement's energy destinations
A heater-and-sample assembly receives electrical work; the sample alone may receive heating from that heater. Do not count the same input twice. In the corrected calorimetry example:
c = 5000/(0.250 × 8.0) = 2500 J/(kg K)
Apparatus warming uses its actual endpoint temperature change; heat-loss corrections need independent evidence under comparable conditions. Assigning all input to the sample gives too high a c in this model.
The fusion comparison uses 5010 J for an extra 15.00 g melted, giving lf = 3.34 × 105 J/kg. It requires matched background transfer, correct initial thermal conditions and complete collection. The draining vessel alone is not a closed fixed-mass system.
Quantities and units
| Quantity | Symbol | Unit or meaning |
|---|---|---|
| Internal energy / change | U, ΔU | J; state quantity / endpoint change |
| Net heating transfer | Q | J; positive into system |
| Work done on system | Won | J; positive into system |
| Work done by system | Wby | J; Wby = -Won |
| External pressure | pext | Pa; absolute |
| Volume / change | V, ΔV | m3; expansion has positive change |
| Piston area / displacement | A, Δx | m2; m |
| Sample mass | m | kg |
| Thermodynamic temperature | T | K |
| Celsius temperature | θ or T | °C; read the stated unit |
| Temperature change | ΔT | K or °C intervals, with equal numerical size |
| Specific heat capacity | c | J/(kg K); stated process |
| Apparatus heat capacity | Capparatus | J/K; for the whole apparatus |
| Specific latent heat | l; lf, lv | J/kg; fusion or vaporisation as named |
| Power / elapsed time | P, t | W = J/s; s |
| Particle number / amount | N, n | Dimensionless; mol |
| Boltzmann / molar gas constant | k, R | J/K; J/(mol K) |
An unqualified W in the plus-sign first law means work on the system. The unit W in a power value means watt. Likewise, specific heat capacity c here is not the microscopic speed c used in a kinetic-gas derivation.
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