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Thermodynamics Domain Guide

The laws, the ideal gas and its named processes, kinetic theory and equipartition, engines and the Carnot bound, entropy, calorimetry, and heat transfer — organised around the one question that unlocks most items: which variable is being held fixed?

Concise answer

Thermodynamics is bookkeeping with two rules. The first law says energy is conserved once heat is counted as a way of transferring it; the second says that of all the energy-conserving processes, only those that do not decrease total entropy actually happen. Everything else in the domain — named ideal-gas processes, engine efficiencies, the Carnot bound, calorimetry, conduction and radiation — is one of those two rules applied to a system whose constraint you must identify first.

Definitions

State function
A quantity determined by the current state alone: internal energy UU, temperature TT, pressure PP, volume VV, entropy SS. Heat QQ and work WW are not state functions — they depend on the path, which is why a cycle can return ΔU=0\Delta U = 0 while QQ and WW are both non-zero.
Internal energy of an ideal gas
U=nCVTU = nC_VT, a function of temperature only. This holds for every ideal-gas process, not just constant-volume ones, so ΔU=nCVΔT\Delta U = nC_V\Delta T is always available even during an isobaric or adiabatic change.
Reversible process
A quasi-static process that can be run backwards leaving no net change in the system or its surroundings. It is an idealisation: real processes generate entropy, and the Carnot bound is exactly the efficiency of the reversible limit.
Entropy
dS=dQrev/TdS = dQ_{\text{rev}}/T macroscopically, and S=kBlnΩS = k_B\ln\Omega microscopically, where Ω\Omega counts the microstates consistent with the macrostate. Because SS is a state function, its change can be computed along any convenient reversible path between the same endpoints.
Equipartition
In classical statistical mechanics each quadratic degree of freedom carries an average energy 12kBT\tfrac{1}{2}k_BT. Three translational degrees give U=32nRTU = \tfrac{3}{2}nRT for a monatomic gas; adding two rotational degrees gives 52nRT\tfrac{5}{2}nRT for a rigid diatomic near room temperature.
Coefficient of performance
For a refrigerator, COP=QC/W\mathrm{COP} = Q_C/W; for a heat pump, QH/WQ_H/W. Both exceed one for a useful device, which is why they are not called efficiencies — a COP of 4 does not violate anything.

Intuition

Every ideal-gas question is really the question 'what is being held fixed?'. Isothermal fixes TT, so ΔU=0\Delta U = 0 and Q=WQ = W. Adiabatic fixes Q=0Q = 0, so W=ΔUW = -\Delta U and the gas cools as it expands. Isobaric fixes PP, so W=PΔVW = P\Delta V. Isochoric fixes VV, so W=0W = 0 and Q=ΔUQ = \Delta U. Four sentences, one of which is always the intended shortcut — and each of them kills a term in the first law before you write it.

The second law is a counting statement, not a mystical one. S=kBlnΩS = k_B\ln\Omega says entropy measures how many microscopic arrangements produce the same macroscopic state, and processes run toward the overwhelmingly more numerous arrangements. That is why heat flows from hot to cold with no force pushing it, and why a Carnot engine — which passes heat through infinitesimal temperature differences — is the only kind that generates no entropy and therefore extracts the maximum work.

Temperature is not heat and neither is internal energy. Temperature measures the average energy per degree of freedom; internal energy is the total; heat is energy in transit because of a temperature difference. A large iceberg has more internal energy than a cup of boiling water and a lower temperature, and heat still flows from the cup to the iceberg. Keeping these three separate resolves most conceptual items in the domain without any calculation.

Concept walkthrough

ETS lists thermodynamics and statistical mechanics as one content area, and our learning model groups the laws, the ideal gas, kinetic theory, engines, calorimetry, heat transfer, and thermal expansion beneath it. Start with the sign convention, because a large share of wrong answers here are sign errors rather than physics errors. In the form used above, ΔU=QW\Delta U = Q - W, heat added to the gas is positive and work done by the gas is positive. Some texts write ΔU=Q+W\Delta U = Q + W with WW meaning work done on the gas; both are correct and they differ only in bookkeeping, so decide which one you use and never mix them mid-problem.

The ideal gas law, PV=nRT=NkBTPV = nRT = Nk_BT, links the state variables, and the named processes fix one of them. Isothermal: ΔU=0\Delta U = 0, W=nRTln(V2/V1)W = nRT\ln(V_2/V_1), and Q=WQ = W. Isochoric: W=0W = 0 and Q=nCVΔTQ = nC_V\Delta T. Isobaric: W=PΔVW = P\Delta V and Q=nCPΔTQ = nC_P\Delta T, with CP=CV+RC_P = C_V + R — a relation that holds for any ideal gas because expanding at constant pressure requires the extra work PΔV=nRΔTP\Delta V = nR\Delta T. Adiabatic: Q=0Q = 0, PVγPV^{\gamma} and TVγ1TV^{\gamma-1} are constant, and W=(P1V1P2V2)/(γ1)W = (P_1V_1 - P_2V_2)/(\gamma-1). Throughout, remember that ΔU=nCVΔT\Delta U = nC_V\Delta T is valid for every one of these, because UU depends only on TT.

Kinetic theory supplies the microscopic picture and three speeds that are routinely confused. From 12mv2=32kBT\tfrac{1}{2}m\langle v^{2}\rangle = \tfrac{3}{2}k_BT comes vrms=3kBT/m=3RT/Mv_{\text{rms}} = \sqrt{3k_BT/m} = \sqrt{3RT/M} with MM the molar mass in kilograms per mole. The mean speed is 8kBT/πm\sqrt{8k_BT/\pi m} and the most probable speed is 2kBT/m\sqrt{2k_BT/m}, so the ordering is always vmp<vavg<vrmsv_{\text{mp}} < v_{\text{avg}} < v_{\text{rms}}. Equipartition generalises this: each quadratic degree of freedom holds 12kBT\tfrac{1}{2}k_BT on average, which gives CV=32RC_V = \tfrac{3}{2}R for a monatomic gas, 52R\tfrac{5}{2}R for a rigid diatomic at ordinary temperatures, and the Dulong-Petit value 3R3R for a classical solid with three vibrational modes each contributing kinetic and potential terms.

Engines convert the first and second laws into a number. Over a complete cycle ΔU=0\Delta U = 0, so W=QHQCW = Q_H - Q_C and the efficiency is e=W/QH=1QC/QHe = W/Q_H = 1 - Q_C/Q_H. The Carnot bound, eCarnot=1TC/THe_{\text{Carnot}} = 1 - T_C/T_H in absolute temperature, is the ceiling for any engine between the same two reservoirs, and it is achieved only by a reversible cycle running infinitely slowly. Refrigerators and heat pumps are the same cycle read backwards, with COPfridge=QC/WTC/(THTC)\mathrm{COP}_{\text{fridge}} = Q_C/W \le T_C/(T_H-T_C) and COPpump=QH/WTH/(THTC)\mathrm{COP}_{\text{pump}} = Q_H/W \le T_H/(T_H-T_C). A claimed efficiency above the Carnot value is not an approximation error; it is an impossibility, and on a multiple-choice paper it is a free elimination.

Entropy makes the second law quantitative. For a reservoir at fixed TT exchanging heat QQ, ΔS=Q/T\Delta S = Q/T. For an ideal gas between two states, ΔS=nCVln(T2/T1)+nRln(V2/V1)\Delta S = nC_V\ln(T_2/T_1) + nR\ln(V_2/V_1), which reduces to nRln(V2/V1)nR\ln(V_2/V_1) for an isothermal change and to zero for a reversible adiabatic (hence 'isentropic'). Because SS is a state function, an irreversible process such as free expansion into a vacuum — where Q=0Q = 0 and W=0W = 0 and therefore ΔT=0\Delta T = 0 for an ideal gas — still has ΔS=nRln(V2/V1)>0\Delta S = nR\ln(V_2/V_1) > 0, computed along an imaginary reversible isothermal path. That single example contains the whole method: never compute ΔS\Delta S along the actual irreversible path.

Calorimetry and transport close the domain. Heating without a phase change costs Q=mcΔTQ = mc\Delta T; a phase change costs Q=mLQ = mL at constant temperature, and forgetting the latent term is the classic mixing-problem error. Steady conduction through a slab gives P=kAΔT/LP = kA\Delta T/L, so series slabs add thermal resistances L/kAL/kA exactly as resistors add. Radiation follows the Stefan-Boltzmann law P=σεAT4P = \sigma\varepsilon AT^{4} with σ=5.67×108 Wm2K4\sigma = 5.67\times10^{-8}\ \mathrm{W\,m^{-2}\,K^{-4}}, and net exchange with surroundings at T0T_0 is σεA(T4T04)\sigma\varepsilon A(T^{4}-T_0^{4}) — always in kelvin, where the fourth power makes a small temperature change matter enormously. Thermal expansion is ΔL=αL0ΔT\Delta L = \alpha L_0\Delta T with β3α\beta \approx 3\alpha for volume, and the counter-intuitive consequence worth remembering is that a hole in a heated plate gets larger, because every linear dimension scales together.

After this page, you should be able to

  • Apply ΔU=QW\Delta U = Q - W with a stated sign convention and identify, for any named process, which of QQ, WW, ΔU\Delta U, or ΔT\Delta T is zero.
  • Use PV=nRTPV = nRT together with PVγ=constantPV^{\gamma} = \text{constant} and TVγ1=constantTV^{\gamma-1} = \text{constant} to relate states across an adiabatic change.
  • Derive heat capacities from degrees of freedom: CV=32RC_V = \tfrac{3}{2}R and γ=53\gamma = \tfrac{5}{3} for a monatomic gas, CV=52RC_V = \tfrac{5}{2}R and γ=75\gamma = \tfrac{7}{5} for a rigid diatomic.
  • Compute engine efficiency, refrigerator COP, and the Carnot bound, and use the bound to reject impossible answer choices instantly.
  • Compute entropy changes for reservoirs and for an ideal gas, and use the sign of the total change to decide whether a process is reversible, possible, or impossible.
  • Handle calorimetry with phase changes, conduction through a slab, and radiation with the Stefan-Boltzmann law in absolute temperature.

Formulas and assumptions

First law and the four named processes

ΔU=QW,Wiso=nRTlnV2V1,Wisobaric=PΔV,Wadiabatic=P1V1P2V2γ1\Delta U = Q - W, \quad W_{\text{iso}} = nRT\ln\frac{V_2}{V_1}, \quad W_{\text{isobaric}} = P\Delta V, \quad W_{\text{adiabatic}} = \frac{P_1V_1-P_2V_2}{\gamma-1}

Variables

  • Q: heat added to the system
  • W: work done by the system
  • gamma: ratio Cp/Cv

Assumptions

  • Delta U = n Cv Delta T holds for every ideal-gas process, not only constant-volume ones.
  • Over a complete cycle Delta U = 0, so the net heat equals the net work.

Ideal gas law and adiabatic relations

PV=nRT=NkBT,PVγ=const,TVγ1=const,CP=CV+RPV = nRT = Nk_BT, \qquad PV^{\gamma} = \text{const}, \qquad TV^{\gamma-1} = \text{const}, \qquad C_P = C_V + R

Variables

  • R: 8.314 J / (mol K)
  • k_B: 1.381 x 10^-23 J/K
  • gamma: 5/3 monatomic, 7/5 rigid diatomic

Assumptions

  • Temperature must be absolute (kelvin) in every one of these relations.
  • The adiabatic relations assume a reversible (quasi-static) adiabatic process, not merely Q = 0.

Kinetic theory and equipartition

vrms=3kBTm=3RTM,vavg=8kBTπm,vmp=2kBTmv_{\text{rms}} = \sqrt{\frac{3k_BT}{m}} = \sqrt{\frac{3RT}{M}}, \quad v_{\text{avg}} = \sqrt{\frac{8k_BT}{\pi m}}, \quad v_{\text{mp}} = \sqrt{\frac{2k_BT}{m}}

Variables

  • M: molar mass in kg/mol
  • m: mass of one molecule
  • T: absolute temperature

Assumptions

  • The ordering is always v_mp < v_avg < v_rms; all three scale as the square root of T and inversely as the square root of mass.
  • Equipartition is classical: a degree of freedom freezes out when k T falls well below its quantum level spacing, which is why diatomic Cv is 5R/2 rather than 7R/2 at room temperature.

Engines, refrigerators, and the Carnot bound

e=WQH=1QCQH,eCarnot=1TCTH,COPfridgeTCTHTCe = \frac{W}{Q_H} = 1 - \frac{Q_C}{Q_H}, \quad e_{\text{Carnot}} = 1 - \frac{T_C}{T_H}, \quad \mathrm{COP}_{\text{fridge}} \le \frac{T_C}{T_H-T_C}

Variables

  • Q_H: heat absorbed from the hot reservoir per cycle
  • Q_C: heat rejected to the cold reservoir per cycle
  • T: absolute reservoir temperatures

Assumptions

  • The Carnot expression uses kelvin; using Celsius produces a plausible-looking but wrong number.
  • Any claimed efficiency above the Carnot value is impossible, which makes the bound a fast elimination tool.

Entropy

ΔS=dQrevT,ΔSgas=nCVlnT2T1+nRlnV2V1,S=kBlnΩ\Delta S = \int\frac{dQ_{\text{rev}}}{T}, \quad \Delta S_{\text{gas}} = nC_V\ln\frac{T_2}{T_1} + nR\ln\frac{V_2}{V_1}, \quad S = k_B\ln\Omega

Variables

  • Omega: number of accessible microstates
  • Q_rev: heat along a reversible path with the same endpoints

Assumptions

  • Entropy is a state function, so it must be computed along a reversible path even when the real process is irreversible.
  • Only the total entropy of system plus surroundings is forbidden from decreasing; a system alone can lose entropy freely.

Calorimetry and phase change

Q=mcΔT,Q=mL,iQi=0Q = mc\Delta T, \qquad Q = mL, \qquad \sum_i Q_i = 0

Variables

  • c: specific heat capacity
  • L: latent heat of fusion or vaporisation

Assumptions

  • Temperature does not change while a phase change is in progress, so the two formulas are never used simultaneously on the same mass.
  • The sum rule assumes the calorimeter is isolated; a stated container heat capacity must be included as another term.

Heat transfer and thermal expansion

Pcond=kAΔTL,Prad=σεAT4,ΔL=αL0ΔT,β3αP_{\text{cond}} = \frac{kA\Delta T}{L}, \quad P_{\text{rad}} = \sigma\varepsilon A T^{4}, \quad \Delta L = \alpha L_0\Delta T, \quad \beta \approx 3\alpha

Variables

  • k: thermal conductivity
  • sigma: 5.67 x 10^-8 W m^-2 K^-4
  • epsilon: emissivity, between 0 and 1

Assumptions

  • Radiation requires absolute temperature; the fourth power makes Celsius catastrophically wrong.
  • A hole in an expanding plate grows rather than shrinks, because every linear dimension scales by the same factor.

Worked example

One pair of reservoirs, two engines: where the entropy goes

A Carnot engine runs between TH=500 KT_H = 500\ \mathrm{K} and TC=300 KT_C = 300\ \mathrm{K} and absorbs QH=1000 JQ_H = 1000\ \mathrm{J} per cycle. Find its efficiency, work, and rejected heat, and the entropy change of each reservoir. Then a real engine between the same reservoirs absorbs the same QHQ_H but delivers only W=300 JW = 300\ \mathrm{J}. Find its efficiency and the entropy generated per cycle.

  1. 1Carnot efficiency comes straight from the absolute temperatures: e=1TC/TH=1300/500=0.40e = 1 - T_C/T_H = 1 - 300/500 = 0.40. Note that the same reservoirs in Celsius would give 127/227=0.881 - 27/227 = 0.88, a wrong answer that looks entirely reasonable — always convert first.
  2. 2Work and rejected heat follow from the definition and the first law over a cycle: W=eQH=0.40(1000)=400 JW = eQ_H = 0.40(1000) = 400\ \mathrm{J}, and QC=QHW=1000400=600 JQ_C = Q_H - W = 1000 - 400 = 600\ \mathrm{J}.
  3. 3Compute each reservoir's entropy change, treating each as isothermal: ΔSH=QH/TH=1000/500=2.00 J/K\Delta S_H = -Q_H/T_H = -1000/500 = -2.00\ \mathrm{J/K}, and ΔSC=+QC/TC=+600/300=+2.00 J/K\Delta S_C = +Q_C/T_C = +600/300 = +2.00\ \mathrm{J/K}.
  4. 4Add them. ΔStotal=2.00+2.00=0\Delta S_{\text{total}} = -2.00 + 2.00 = 0. The engine itself returns to its starting state each cycle, so its own entropy change is zero, and the universe's total change is zero — the signature of a reversible cycle, and the reason no engine can beat it.
  5. 5Now the real engine. Its efficiency is e=W/QH=300/1000=0.30e = W/Q_H = 300/1000 = 0.30, which is below the Carnot value of 0.400.40, as the second law requires. Its rejected heat is QC=1000300=700 JQ_C = 1000 - 300 = 700\ \mathrm{J}.
  6. 6Compute the entropy generated: ΔStotal=1000500+700300=2.000+2.333=+0.333 J/K\Delta S_{\text{total}} = -\dfrac{1000}{500} + \dfrac{700}{300} = -2.000 + 2.333 = +0.333\ \mathrm{J/K} per cycle. The lost work is exactly TCΔStotal=300(0.333)=100 JT_C\Delta S_{\text{total}} = 300(0.333) = 100\ \mathrm{J}, which is precisely the shortfall between 400 J400\ \mathrm{J} and 300 J300\ \mathrm{J}. Irreversibility is not a vague inefficiency; it is a number, and the second law prices it at TCT_C per unit of entropy generated.

Carnot: e=0.40e = 0.40, W=400 JW = 400\ \mathrm{J}, QC=600 JQ_C = 600\ \mathrm{J}, ΔStotal=0\Delta S_{\text{total}} = 0. Real engine: e=0.30e = 0.30, QC=700 JQ_C = 700\ \mathrm{J}, ΔStotal=+0.333 J/K\Delta S_{\text{total}} = +0.333\ \mathrm{J/K}, and the 100 J100\ \mathrm{J} of lost work equals TCΔStotalT_C\Delta S_{\text{total}} exactly. An engine claiming W=450 JW = 450\ \mathrm{J} from the same QHQ_H would require ΔStotal<0\Delta S_{\text{total}} < 0 and is impossible.

Common traps

  • Mixing the two sign conventions for the first law. ΔU=QW\Delta U = Q - W takes WW as work done by the gas; ΔU=Q+W\Delta U = Q + W takes it as work done on the gas. Either is fine; using both in one problem is not.
  • Using Celsius in PV=nRTPV = nRT, in the Carnot efficiency, or in the Stefan-Boltzmann law. All three demand kelvin, and all three produce believable wrong numbers when they do not get it.
  • Applying Q=nCVΔTQ = nC_V\Delta T to a constant-pressure process. The heat needs CPC_P; it is ΔU\Delta U, not QQ, that always uses CVC_V.
  • Treating an adiabatic process as isothermal because 'no heat flows'. With Q=0Q = 0 all the work comes from internal energy, so the temperature must change.
  • Believing a stated efficiency above the Carnot bound is merely optimistic. It is impossible, and spotting that eliminates answer choices without any calculation.
  • Computing ΔS\Delta S from the heat actually exchanged along an irreversible path. Entropy is a state function; use a reversible path with the same endpoints, which is why free expansion has ΔS=nRln(V2/V1)\Delta S = nR\ln(V_2/V_1) despite Q=0Q = 0.
  • Confusing vrmsv_{\text{rms}} with vavgv_{\text{avg}}, or putting molar mass in grams per mole into vrms=3RT/Mv_{\text{rms}} = \sqrt{3RT/M}.
  • Using γ=5/3\gamma = 5/3 for every gas. It is 7/57/5 for a rigid diatomic at ordinary temperatures, and the difference propagates through every adiabatic relation.
  • Forgetting the latent heat term in a mixing problem, so ice is treated as though it warms straight through 0C0\,^{\circ}\mathrm{C} without melting.
  • Reading 'entropy never decreases' as a statement about any system. Only the total entropy of system plus surroundings is constrained; a refrigerator lowers the entropy of its contents every second it runs.

Question depth and domain coverage vary by exam. Practice answers are checked after submission.

Sources

  1. GRE Subject Test Content and StructureETS. Accessed 2026-07-06. Use as a cited source for exam facts; do not imply affiliation or reproduce protected test material.
  2. University Physics Volume 2, Section 3.3: First Law of ThermodynamicsOpenStax. Accessed 2026-08-02. OpenStax textbook content is CC BY-NC-SA 4.0; attribute and avoid verbatim reuse beyond short cited references.
  3. University Physics Volume 2, Section 3.4: Thermodynamic ProcessesOpenStax. Accessed 2026-08-02. OpenStax textbook content is CC BY-NC-SA 4.0; attribute and avoid verbatim reuse beyond short cited references.
  4. University Physics Volume 2, Section 4.2: Heat EnginesOpenStax. Accessed 2026-08-02. OpenStax textbook content is CC BY-NC-SA 4.0; attribute and avoid verbatim reuse beyond short cited references.
  5. University Physics Volume 2, Section 4.5: The Carnot CycleOpenStax. Accessed 2026-08-02. OpenStax textbook content is CC BY-NC-SA 4.0; attribute and avoid verbatim reuse beyond short cited references.
  6. University Physics Volume 2, Section 4.6: EntropyOpenStax. Accessed 2026-08-02. OpenStax textbook content is CC BY-NC-SA 4.0; attribute and avoid verbatim reuse beyond short cited references.

Sources and corrections

Sources last checked 2026-08-15

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