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Thermodynamic Systems overview

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:

Mean translational kinetic energy per particle = (3/2)kT

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:

U = (3/2)NkT = (3/2)nRT

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

Net heating transfers energy from hotter A to colder BSamples A and B have unequal amounts, shown schematically by different-sized blocks. A thermal connector links them inside an insulated combined system boundary. A has the higher temperature T sub A and B the lower T sub B. The orange arrow along the connector is net energy transfer by heating from A to B, not matter flow. Energy is redistributed within the insulated combined system. The block sizes and temperatures are qualitative, not a numerical mixing or energy-scale drawing.ABTATBmAmBTA > TBNet heating: A to BmA ≠ mBInsulated combined boundary

After settling: thermal equilibrium

Unequal samples share one temperature without net heatingSamples A and B have unequal amounts, shown schematically by different-sized blocks. A thermal connector links them inside an insulated combined system boundary. Both temperatures are labelled T sub f. There is no net-transfer arrow because the pair is in thermal equilibrium. Their masses remain unequal; a common temperature does not imply equal total internal energies. The block sizes and temperatures are qualitative, not a numerical mixing or energy-scale drawing.ABTfTfmAmBTA = TB = TfNo net heating between themmA ≠ mBInsulated combined boundary

Equal temperature determines thermal equilibrium. It does not make the samples' masses or total internal energies equal.

Unequal samples exchange energy by heating from hotter to colder. At their common equilibrium temperature, the net transfer stops. Equal temperature does not imply equal mass or equal total internal energy.

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.

Equilibrium with C implies equilibrium between A and BThree named systems form a relationship diagram. Solid lines link A to thermometer C and B to C; each is labelled with equality of their settled temperatures. A dashed upper line links A and B, labelled as the inferred equal-temperature relation. These are thermal-equilibrium relations, not circuit wires, particle paths or arrows of energy flow. C is the same thermometer at the same unchanged reading in both comparisons. The diagram does not assign equal heat capacities or equal energy transfers to A, B or C.ABThereforeTA = TBTA = TCTB = TCCSame thermometer, same reading

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.

The relationships show thermal equilibrium, not paths carrying fixed amounts of energy. If A and B separately equilibrate with thermometer C at the same unchanged reading, they have the same temperature.

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?
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:

ΔU = Q + Won

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.

Signs for the work-on form of the first law
TransferInto the systemOut of the system
Heating QPositiveNegative
Work WonPositive work on itNegative 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.

Wby = force × outward displacement
= 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

A 0.150-metre piston displacement increases gas volume by 0.00150 cubic metresA horizontal cylinder has its fixed gas-facing end at drawing coordinate sixty. The initial piston gas-facing position is 180, shown dashed; the final position is 270, shown solid. Axial distances therefore use six hundred drawing units per metre: initial gas length 0.200 metres, final 0.350 metres and outward displacement 0.150 metres. The cross-section is schematic; its given constant area is 0.0100 square metres. The blue arrow points right for piston displacement. The separate purple external-load force on the piston points left and has magnitude p external times area, 1200 newtons. It is the external load force, not a claimed net force on the slowly moving piston. The two positions are alternative states of one piston. Work by the gas is positive 180 joules; work on the gas is negative 180 joules.GasΔx = +0.150 mFext = 1200 N0.200 m0.350 mArea A = 0.0100 m2

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

The expansion from two to 3.5 thousandths of a cubic metre does 180 joules of workThe volume axis is in units of ten to the minus three cubic metres, and the pressure axis is in units of ten to the five pascals. A horizontal path from volume two to 3.50 has pressure 1.20. The expansion arrow points right. The shaded rectangle has width 1.50 and height 1.20 in these axis units, so its area represents 1.50 times 1.20 times one hundred joules, or 180 joules. With the stated slow frictionless condition, plotted gas pressure equals the constant external pressure. This gives positive work by the gas and negative work on it during expansion. Reversing the path changes the work signs while leaving the positive geometric rectangle unchanged.0.01.02.03.54.00.00.40.81.21.6180 Jp / 105 PaV / 10-3 m3

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.

The piston area is 0.0100 m2, with initial and final gas lengths 0.200 and 0.350 m. External force and outward displacement are opposite. The constant-pressure graph uses the slow-process pressure equality; its 180 J area is work by the expanding gas.
ΔV = (3.50 - 2.00) × 10-3
= 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:

U1 = (3/2)(1.20 × 105)(2.00 × 10-3) = 360 J
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?
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

Separate thermal processes, all using work done on the system
ProcessQ / JWon / JΔU / J
Reverse along the same constant-pressure path-450+180-270
Insulated compression with 90 J work input0+90+90
Rigid closed system, 250 J heating and no other work+2500+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.

Q = mcΔT
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.

Electrical work warms both the sample and apparatus while some energy leaves by heatingA dashed assembly boundary encloses a 0.250-kilogram sample, its vessel, an immersed heater and a temperature sensor. Two wires connect the heater to an external calibrated input device. An orange downward energy-transfer arrow crosses the assembly boundary beside the wires and denotes 6000 joules of electrical work, not an additional heating input. A separate outward orange arrow denotes 680 joules lost by heating. The apparatus has independently supplied heat capacity forty joules per kelvin, and both apparatus and sample have an eight-kelvin endpoint temperature rise. Of the 5320 joules retained by the assembly, 320 warm the apparatus and 5000 warm the sample. The sample's specific heat capacity is therefore 2500 joules per kilogram per kelvin. The liquid-like sample drawing is schematic and does not identify the sample as water or prescribe an instrument specification.Calibratedwork input6000 JSensorSample0.250 kgHeaterLoss680 JSettled rise: 8.0 KAssembly boundary

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.

The marked assembly includes the sample, heater, vessel and sensor. Electrical input is work into that assembly, while heat loss leaves it. Sample mass and apparatus heat capacity are distinct; a sample-only account uses the net energy reaching that sample.

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.

Apparatus energy increase = 40 × 8.0 = 320 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?
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:

0.200c(50.0 - θf) = 0.300c(θf - 20.0)
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.

Q = ml

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.

Energy entering each stage of the supplied ice-to-water model
StageCalculationEnergy / J
Warm ice from -5 to 0°C0.0800 × 2100 × 5.0840
Melt all ice at 0°C0.0800 × 3.34 × 10526720
Warm water from 0 to 25°C0.0800 × 4200 × 25.08400
Total input = 840 + 26720 + 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 true energy scale shows that melting dominates the supplied ice-to-water accountTemperature in degrees Celsius is plotted against cumulative input energy in kilojoules. The exact endpoints are A, zero kilojoules and minus five degrees; B, 0.840 kilojoules and zero degrees; C, 27.560 kilojoules and zero degrees; and D, 35.960 kilojoules and 25 degrees. One linear energy scale is used throughout: 250 drawing units for 36 kilojoules. Consequently the initial warming interval is only 5.8333 drawing units wide and has not been widened. Leaders and a separate point key identify the closely spaced initial energy coordinates. The long horizontal B-to-C segment requires 26.720 kilojoules of melting energy at constant temperature. The final water-warming stage uses 8.400 kilojoules. The arrowed horizontal energy axis is at zero degrees Celsius, and A is below it. The graph gives no elapsed duration or heating-rate assumption.010203036-50102025ABCDTemperature / °CCumulative input energy / kJ

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 horizontal axis is cumulative energy entering the sample, not time. The four model endpoints are 0, 0.840, 27.560 and 35.960 kJ. The long horizontal interval represents melting with continued energy input at constant temperature.

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:

Qall = 0.0200(3.34 × 105) = 6680 J
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?
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.

Q = mlv = 0.0100(1.80 × 106) = 18000 J
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

A 16.7-watt heater run collects twenty grams of melt in 300 secondsBoth panels have the same draining ice holder, immersed heater, perforated support, outlet and tared collector on a balance. Ice and apparatus start at the melting temperature. Two wires connect the heater to its input device. The measured heater input is 16.7 watts for 300 seconds, or 5010 joules. The supplied final collected-water mass is 20.00 grams. An inward orange arrow identifies the assumed matched background heating in each run. The perforated support retains ice while water drains through the open outlet into the collector; a droplet illustrates collection during the run. The balance label gives the supplied final water mass after taring the container. Water levels are schematic, not calibrated volume measurements. No boundary labels this draining holder as a closed fixed-mass system. Subtracting the two collected masses isolates the heater contribution only under the stated matching and collection assumptions.Collect for 300 sHeater on16.7 WIce at 0 °CMatchedbackgroundSupportTaredcollector20.00 g

Matched control: no heater input

The matching no-heater-input control collects five grams in 300 secondsBoth panels have the same draining ice holder, immersed heater, perforated support, outlet and tared collector on a balance. Ice and apparatus start at the melting temperature. Two wires connect the heater to its input device. The same heater is unpowered during the 300-second control, and the supplied final collected-water mass is 5.00 grams. An inward orange arrow identifies the assumed matched background heating in each run. The perforated support retains ice while water drains through the open outlet into the collector; a droplet illustrates collection during the run. The balance label gives the supplied final water mass after taring the container. Water levels are schematic, not calibrated volume measurements. No boundary labels this draining holder as a closed fixed-mass system. Subtracting the two collected masses isolates the heater contribution only under the stated matching and collection assumptions.Collect for 300 sHeater off0 WIce at 0 °CMatchedbackgroundSupportTaredcollector5.00 g

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.

The heater-on and control arrangements collect meltwater over the same 300 s interval. Background heating is assumed comparable. This is an input-versus-extra-melt comparison; the draining vessel alone is not a closed fixed-mass system.

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.

Heater input = 16.7 × 300 = 5010 J
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:

U = (3/2)NkT = (3/2)nRT

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

ΔU = Q + Won
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

Within one phase: Q = mcΔT
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:

Sample energy = 6000 - 320 - 680 = 5000 J
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

Symbols, units and transfer conventions used in thermodynamics
QuantitySymbolUnit or meaning
Internal energy / changeU, ΔUJ; state quantity / endpoint change
Net heating transferQJ; positive into system
Work done on systemWonJ; positive into system
Work done by systemWbyJ; Wby = -Won
External pressurepextPa; absolute
Volume / changeV, ΔVm3; expansion has positive change
Piston area / displacementA, Δxm2; m
Sample massmkg
Thermodynamic temperatureTK
Celsius temperatureθ or T°C; read the stated unit
Temperature changeΔTK or °C intervals, with equal numerical size
Specific heat capacitycJ/(kg K); stated process
Apparatus heat capacityCapparatusJ/K; for the whole apparatus
Specific latent heatl; lf, lvJ/kg; fusion or vaporisation as named
Power / elapsed timeP, tW = J/s; s
Particle number / amountN, nDimensionless; mol
Boltzmann / molar gas constantk, RJ/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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