8.3 Second and Third Laws of Thermodynamics: Entropy, Carnot Engine, and Absolute Entropies

Key Takeaways

  • The Second Law establishes the direction of spontaneous change: the entropy of an isolated system increases in any irreversible process and remains constant in a reversible process (ΔSuniv≥0\Delta S_{univ} \ge 0).

  • The thermodynamic definition of entropy is dS=δqrevTdS = \frac{\delta q_{rev}}{T}, while the Clausius inequality dS≥δqTdS \ge \frac{\delta q}{T} confirms that irreversible heat flow produces internal entropy within the system.

  • A Carnot engine operates through four reversible stages between temperatures THT_H and TCT_C; its efficiency depends solely on reservoir temperatures: η=1−TCTH=−wnetqH\eta = 1 - \frac{T_C}{T_H} = \frac{-w_{net}}{q_H}.

  • Entropy changes for state transformations include isothermal expansion (ΔS=nRln⁡V2V1\Delta S = nR \ln\frac{V_2}{V_1}), isobaric heating (ΔS=nCp,mln⁡T2T1\Delta S = n C_{p,m} \ln\frac{T_2}{T_1}), and phase changes (ΔStr=ΔHtrTtr\Delta S_{tr} = \frac{\Delta H_{tr}}{T_{tr}}); Trouton's rule predicts ΔSvap≈85−88 J⋅mol−1⋅K−1\Delta S_{vap} \approx 85-88\text{ J}\cdot\text{mol}^{-1}\cdot\text{K}^{-1} for unassociated liquids.

  • The Third Law states that the entropy of a pure, perfectly crystalline substance at absolute zero is zero (S0 K=0S_{0\text{ K}} = 0); residual entropies in substances like CO,N2O\text{CO}, \text{N}_2\text{O}, and ice arise from frozen orientational disorder (S=kBln⁡WS = k_B \ln W).

Last updated: October 2026

Second and Third Laws of Thermodynamics: Entropy, Carnot Engine, and Absolute Entropies

While the First Law governs energy conservation, it cannot predict whether a physical or chemical process occurs spontaneously. The Second and Third Laws of Thermodynamics introduce entropy (SS) as the fundamental state function establishing the arrow of time, the theoretical efficiency limit of thermodynamic engines, and the quantification of absolute standard entropies.


1. Spontaneity and Statements of the Second Law

A spontaneous process is a transformation that proceeds in a definite direction without continuous input of external work. Natural processes disperse energy and matter, moving isolated systems toward macroscopic equilibrium.

Classic Formulations of the Second Law

  1. Clausius Statement: It is impossible to construct a cyclic thermodynamic device whose sole effect is the continuous transfer of heat from a cooler body to a hotter body without an input of external work.
  2. Kelvin-Planck Statement: It is impossible to construct a cyclic heat engine that extracts heat from a single thermal reservoir and converts it completely into mechanical work without rejecting a portion of heat to a colder reservoir.
  3. Entropy Formulation: The entropy of the universe (system plus surroundings) increases during any spontaneous, irreversible process and remains constant during a reversible process: ΔSuniv=ΔSsys+ΔSsurr>0[Irreversible / Spontaneous]\Delta S_{univ} = \Delta S_{sys} + \Delta S_{surr} > 0 \quad \text{[Irreversible / Spontaneous]} ΔSuniv=ΔSsys+ΔSsurr=0[Reversible / Equilibrium]\Delta S_{univ} = \Delta S_{sys} + \Delta S_{surr} = 0 \quad \text{[Reversible / Equilibrium]}

2. Thermodynamic Definition of Entropy and the Clausius Inequality

Entropy is defined differentially along a reversible thermal path:

dS≡δqrevTdS \equiv \frac{\delta q_{rev}}{T}

The Clausius Inequality

For any real, irreversible change between two states, the actual heat absorbed (δq\delta q) is less than the heat that would be absorbed along a reversible path (δqrev\delta q_{rev}) connecting the exact same states because internal dissipation generates entropy:

dS≥δqT  ⟺  ∮δqT≤0dS \ge \frac{\delta q}{T} \iff \oint \frac{\delta q}{T} \le 0 where the equality holds strictly for reversible transformations.

Entropy Change of the Surroundings (ΔSsurr\Delta S_{surr})

Because the surroundings act as an essentially infinite, constant-temperature heat reservoir operating quasi-statically, any heat exchanged by the system (qsysq_{sys}) enters or leaves the surroundings reversibly:

ΔSsurr=−qsysTsurr\Delta S_{surr} = -\frac{q_{sys}}{T_{surr}}

Worked Step-by-Step Calculation: Irreversible Heat Transfer

Scenario: A block of copper transfers 6000 J6000\text{ J} of heat directly and irreversibly from a high-temperature thermal reservoir at TH=600.0 KT_H = 600.0\text{ K} to a low-temperature reservoir at TC=300.0 KT_C = 300.0\text{ K}. Calculate ΔShot\Delta S_{hot}, ΔScold\Delta S_{cold}, and ΔSuniv\Delta S_{univ}.

Step 1: Compute entropy changes of individual reservoirs: ΔShot=qhotTH=−6000 J600.0 K=−10.00 J/K\Delta S_{hot} = \frac{q_{hot}}{T_H} = \frac{-6000\text{ J}}{600.0\text{ K}} = -10.00\text{ J/K} ΔScold=qcoldTC=+6000 J300.0 K=+20.00 J/K\Delta S_{cold} = \frac{q_{cold}}{T_C} = \frac{+6000\text{ J}}{300.0\text{ K}} = +20.00\text{ J/K}

Step 2: Compute net entropy change of the universe: ΔSuniv=ΔShot+ΔScold=−10.00 J/K+20.00 J/K=+10.00 J/K\Delta S_{univ} = \Delta S_{hot} + \Delta S_{cold} = -10.00\text{ J/K} + 20.00\text{ J/K} = +10.00\text{ J/K} Thermodynamic Deduction: Because ΔSuniv=+10.00 J/K>0\Delta S_{univ} = +10.00\text{ J/K} > 0, the Second Law is strictly satisfied. The spontaneous unidirectional flow of heat down a temperature gradient generates net entropy.


3. The Carnot Cycle and Theoretical Efficiency

The Carnot cycle represents an idealized, fully reversible four-stroke thermodynamic engine operating between a hot reservoir at THT_H and a cold reservoir at TCT_C.

StageThermodynamic ProcessBoundary Heat (qq)Boundary Work (ww)State Function Relation
1. Isothermal ExpansionReversible at THT_H (V1→V2V_1 \rightarrow V_2)qH=−w1=nRTHln⁡(V2/V1)>0q_H = -w_1 = nRT_H \ln(V_2/V_1) > 0w1=−nRTHln⁡(V2/V1)<0w_1 = -nRT_H \ln(V_2/V_1) < 0ΔU1=0\Delta U_1 = 0
2. Adiabatic ExpansionReversible (V2→V3V_2 \rightarrow V_3)q2=0q_2 = 0w2=nCv,m(TC−TH)<0w_2 = n C_{v,m}(T_C - T_H) < 0ΔU2=w2\Delta U_2 = w_2
3. Isothermal CompressionReversible at TCT_C (V3→V4V_3 \rightarrow V_4)qC=−w3=nRTCln⁡(V4/V3)<0q_C = -w_3 = nRT_C \ln(V_4/V_3) < 0w3=−nRTCln⁡(V4/V3)>0w_3 = -nRT_C \ln(V_4/V_3) > 0ΔU3=0\Delta U_3 = 0
4. Adiabatic CompressionReversible (V4→V1V_4 \rightarrow V_1)q4=0q_4 = 0w4=nCv,m(TH−TC)>0w_4 = n C_{v,m}(T_H - T_C) > 0ΔU4=w4\Delta U_4 = w_4

Volume Relationships and State Function Proof

For the two adiabatic stages: THTC=(V3V2)γ−1andTHTC=(V4V1)γ−1  ⟹  V3V2=V4V1  ⟺  V2V1=V3V4\frac{T_H}{T_C} = \left(\frac{V_3}{V_2}\right)^{\gamma - 1} \quad \text{and} \quad \frac{T_H}{T_C} = \left(\frac{V_4}{V_1}\right)^{\gamma - 1} \implies \frac{V_3}{V_2} = \frac{V_4}{V_1} \iff \frac{V_2}{V_1} = \frac{V_3}{V_4} Substituting this equality into the cyclic entropy sum: ∮δqrevT=qHTH+qCTC=nRln⁡(V2V1)+nRln⁡(V4V3)=nRln⁡(V2V1)−nRln⁡(V3V4)=0\oint \frac{\delta q_{rev}}{T} = \frac{q_H}{T_H} + \frac{q_C}{T_C} = nR \ln\left(\frac{V_2}{V_1}\right) + nR \ln\left(\frac{V_4}{V_3}\right) = nR \ln\left(\frac{V_2}{V_1}\right) - nR \ln\left(\frac{V_3}{V_4}\right) = 0 This proves mathematically that δqrevT\frac{\delta q_{rev}}{T} is an exact differential, establishing that entropy (SS) is a true state function.

Carnot Thermal Efficiency (η\eta)

The thermodynamic efficiency is defined as net mechanical work delivered per unit heat absorbed from the hot reservoir: η≡−wnetqH=qH+qCqH=1+qCqH\eta \equiv \frac{-w_{net}}{q_H} = \frac{q_H + q_C}{q_H} = 1 + \frac{q_C}{q_H} Because qCqH=−TCTH\frac{q_C}{q_H} = -\frac{T_C}{T_H}:

ηCarnot=1−TCTH=TH−TCTH\eta_{Carnot} = 1 - \frac{T_C}{T_H} = \frac{T_H - T_C}{T_H}

Carnot's Principles:

  1. No heat engine operating between two specified heat reservoirs can be more efficient than a reversible Carnot engine operating between the same two reservoirs (ηirr<ηCarnot\eta_{irr} < \eta_{Carnot}).
  2. All reversible heat engines operating between the same two temperatures possess the identical efficiency, completely independent of the working fluid (ideal gas, steam, chemical solution).

Worked Carnot Calculation

Scenario: A high-temperature geothermal powerplant extracts thermal steam at 227.0∘C227.0^\circ\text{C} (500.15 K500.15\text{ K}) and discharges rejected heat to a cooling pond at 27.0∘C27.0^\circ\text{C} (300.15 K300.15\text{ K}). If the plant extracts 120.0 MW120.0\text{ MW} of thermal heat from the underground steam field:

  • (a) What is the maximum theoretical efficiency?
  • (b) What is the minimum rate of waste heat rejected to the pond?

Step 1: Compute efficiency: η=1−TCTH=1−300.15 K500.15 K=1−0.60012=0.39988≈40.0%\eta = 1 - \frac{T_C}{T_H} = 1 - \frac{300.15\text{ K}}{500.15\text{ K}} = 1 - 0.60012 = 0.39988 \approx 40.0\%

Step 2: Compute net work rate (electric power) and rejected heat: W˙net=η⋅Q˙H=(0.39988)(120.0 MW)=47.99 MW≈48.0 MW\dot{W}_{net} = \eta \cdot \dot{Q}_H = (0.39988)(120.0\text{ MW}) = 47.99\text{ MW} \approx 48.0\text{ MW} Q˙C=Q˙H−W˙net=120.0 MW−48.0 MW=72.0 MW\dot{Q}_C = \dot{Q}_H - \dot{W}_{net} = 120.0\text{ MW} - 48.0\text{ MW} = 72.0\text{ MW}


4. Entropy Calculations Across Thermodynamic Pathways

1. Isothermal Ideal Gas Expansion / Compression

ΔS=∫12δqrevT=1T∫12P dV=nR∫V1V2dVV=nRln⁡(V2V1)=−nRln⁡(P2P1)\Delta S = \int_{1}^{2} \frac{\delta q_{rev}}{T} = \frac{1}{T} \int_{1}^{2} P\,dV = nR \int_{V_1}^{V_2} \frac{dV}{V} = nR \ln\left(\frac{V_2}{V_1}\right) = -nR \ln\left(\frac{P_2}{P_1}\right)

2. Isobaric Heating / Cooling (P=constP = \text{const})

ΔS=∫T1T2nCp,mT dT=nCp,mln⁡(T2T1)[if Cp is constant]\Delta S = \int_{T_1}^{T_2} \frac{n C_{p,m}}{T}\,dT = n C_{p,m} \ln\left(\frac{T_2}{T_1}\right) \quad \text{[if } C_p \text{ is constant]}

3. Isochoric Heating / Cooling (V=constV = \text{const})

ΔS=∫T1T2nCv,mT dT=nCv,mln⁡(T2T1)[if Cv is constant]\Delta S = \int_{T_1}^{T_2} \frac{n C_{v,m}}{T}\,dT = n C_{v,m} \ln\left(\frac{T_2}{T_1}\right) \quad \text{[if } C_v \text{ is constant]}

4. General State Change of an Ideal Gas (T1,P1→T2,P2T_1, P_1 \rightarrow T_2, P_2)

ΔS=nCp,mln⁡(T2T1)−nRln⁡(P2P1)\Delta S = n C_{p,m} \ln\left(\frac{T_2}{T_1}\right) - nR \ln\left(\frac{P_2}{P_1}\right)

5. Phase Transitions at Equilibrium (Ttr,P=1 barT_{tr}, P = 1\text{ bar})

At the normal transition temperature (e.g., normal boiling point TbT_b, normal melting point TmT_m), coexistence of two phases is in thermodynamic equilibrium (ΔG=0\Delta G = 0): ΔStr=ΔHtrTtr\Delta S_{tr} = \frac{\Delta H_{tr}}{T_{tr}}

  • Normal fusion: ΔSfus=ΔHfusTm\Delta S_{fus} = \frac{\Delta H_{fus}}{T_m}
  • Normal vaporization: ΔSvap=ΔHvapTb\Delta S_{vap} = \frac{\Delta H_{vap}}{T_b}

Trouton's Rule and Structural Anomalies

Trouton's Rule states that for a wide variety of non-associated, normal liquids, the standard molar entropy of vaporization at the normal boiling point is nearly constant:

ΔSvap∘=ΔHvapTb≈85−88 J⋅mol−1⋅K−1\Delta S_{vap}^\circ = \frac{\Delta H_{vap}}{T_b} \approx 85 - 88\text{ J}\cdot\text{mol}^{-1}\cdot\text{K}^{-1} Physical Origin: In all normal liquids, the molar volume expansion upon vaporization is approximately uniform (≈1000×\approx 1000\times), leading to a roughly identical increase in translational positional disorder.

Common Deviations from Trouton's Rule:

  • Positive Deviations (ΔSvap≫88 J/mol⋅K\Delta S_{vap} \gg 88\text{ J/mol}\cdot\text{K}): Strongly hydrogen-bonded liquids like water (ΔSvap=109.1 J/mol⋅K\Delta S_{vap} = 109.1\text{ J/mol}\cdot\text{K}) and ethanol (ΔSvap=110.0 J/mol⋅K\Delta S_{vap} = 110.0\text{ J/mol}\cdot\text{K}). The liquid phase possesses substantial three-dimensional structural ordering. Vaporization shatters this extensive H-bonded network, resulting in a dramatically larger entropy jump.
  • Negative Deviations (ΔSvap≪85 J/mol⋅K\Delta S_{vap} \ll 85\text{ J/mol}\cdot\text{K}): Carboxylic acids such as acetic acid (ΔSvap≈62 J/mol⋅K\Delta S_{vap} \approx 62\text{ J/mol}\cdot\text{K}) undergo vapor-phase dimerization via double hydrogen bonds (2CH3COOH⇌(CH3COOH)22\text{CH}_3\text{COOH} \rightleftharpoons (\text{CH}_3\text{COOH})_2), retaining significant order in the gaseous state.

5. Statistical Entropy and the Third Law

Boltzmann's Statistical Formulation

Ludwig Boltzmann established the microscopic foundation of entropy connecting thermodynamic state functions to quantum microstate multiplicity (WW):

S=kBln⁡WS = k_B \ln W where kB=RNA=1.38065×10−23 J/Kk_B = \frac{R}{N_A} = 1.38065 \times 10^{-23}\text{ J/K} is Boltzmann's constant, and WW is the thermodynamic probability (the total number of accessible microstates consistent with the macroscopic energy, volume, and composition).

The Third Law of Thermodynamics

  1. Nernst Heat Theorem (1906): In any chemical or physical transformation between pure crystalline substances in internal equilibrium, the entropy change approaches zero as temperature approaches absolute zero: lim⁡T→0 KΔS=0\lim_{T \to 0\text{ K}} \Delta S = 0
  2. Planck Formulation (1911): The absolute entropy of all pure, perfectly crystalline substances at absolute zero (0 K0\text{ K}) is identically zero: S(0 K)=0S(0\text{ K}) = 0 Microscopic Basis: In a perfect crystalline lattice at 0 K0\text{ K}, thermal motion ceases and every atom occupies its unique ground-state lattice position. Hence, only one unique microstate exists (W=1W = 1), yielding S=kBln⁡(1)=0S = k_B \ln(1) = 0.

Experimental Determination of Absolute Standard Entropies (S298∘S_{298}^\circ)

Because S(0 K)=0S(0\text{ K}) = 0, absolute entropies can be determined experimentally via calorimetric heat capacity measurements:

S∘(T)=∫0TmCp(s)T dT+ΔHfusTm+∫TmTbCp(l)T dT+ΔHvapTb+∫TbTCp(g)T dTS^\circ(T) = \int_{0}^{T_m} \frac{C_p(s)}{T}\,dT + \frac{\Delta H_{fus}}{T_m} + \int_{T_m}^{T_b} \frac{C_p(l)}{T}\,dT + \frac{\Delta H_{vap}}{T_b} + \int_{T_b}^{T} \frac{C_p(g)}{T}\,dT Near 0 K0\text{ K} (0 to ∼15 K0\text{ to } \sim 15\text{ K}), experimental heat capacities are extrapolated using Debye's T3T^3 Law for non-metallic crystalline solids: Cp≈aT3  ⟹  S(T)=∫0TaT3T dT=aT33=Cp(T)3C_p \approx a T^3 \implies S(T) = \int_{0}^{T} \frac{a T^3}{T}\,dT = \frac{a T^3}{3} = \frac{C_p(T)}{3}

Residual Entropy at 0 K0\text{ K}

When a real substance is cooled, kinetic barriers often freeze molecules in random orientations before true thermodynamic equilibrium is attained, resulting in residual entropy at 0 K0\text{ K} (S0 K>0S_{0\text{ K}} > 0):

SubstanceCrystal Packing / Disorder MechanismOrientations (WW)Residual Entropy (SresS_{res})Experimental Value
Carbon Monoxide (CO\text{CO})Dipole moment is minute (μ=0.11 D\mu = 0.11\text{ D}); crystal lattice freezes randomly as C-O\text{C-O} or O-C\text{O-C} (22 microstates per molecule).W=2NAW = 2^{N_A}S=Rln⁡2≈5.76 J/mol⋅KS = R \ln 2 \approx 5.76\text{ J/mol}\cdot\text{K}about 4.6 J/mol⋅K4.6\text{ J/mol}\cdot\text{K} (partial ordering)
Nitrous Oxide (N2O\text{N}_2\text{O})Linear molecule freezes with random N-N-O\text{N-N-O} versus O-N-N\text{O-N-N} orientation.W=2NAW = 2^{N_A}S=Rln⁡2≈5.76 J/mol⋅KS = R \ln 2 \approx 5.76\text{ J/mol}\cdot\text{K}about 4.8 J/mol⋅K4.8\text{ J/mol}\cdot\text{K}
Nitric Oxide (NO\text{NO})Forms anti-parallel dimers (NO)2(\text{NO})_2 with two random configurations per dimer.W=2NA/2W = 2^{N_A/2}S=12Rln⁡2≈2.88 J/mol⋅KS = \frac{1}{2} R \ln 2 \approx 2.88\text{ J/mol}\cdot\text{K}about 3 J/mol⋅K3\text{ J/mol}\cdot\text{K}
Water Ice (H2O\text{H}_2\text{O} Ice IhI_h)Pauling ice model: each oxygen is tetrahedrally bonded to 4 oxygens with 2 covalent O-H bonds and 2 H-bonds.W=(32)NAW = (\frac{3}{2})^{N_A}S=Rln⁡(1.5)≈3.37 J/mol⋅KS = R \ln(1.5) \approx 3.37\text{ J/mol}\cdot\text{K}3.4 J/mol⋅K3.4\text{ J/mol}\cdot\text{K}
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Carnot Cycle Four-Stage Reversible Heat Engine
Test Your Knowledge

A geothermal power plant operating on an ideal Carnot cycle receives steam at 227.0 °C (500.15 K) and rejects heat to a cooling river at 27.0 °C (300.15 K). If the heat extracted from the geothermal reservoir is 120.0 MW, what is the maximum theoretical thermodynamic efficiency and the minimum rate of waste heat rejected to the river?

A

Carnot efficiency = 88.1% and waste heat rejection rate = 14.3 MW

B

Carnot efficiency = 40.0% and waste heat rejection rate = 72.0 MW

C

Carnot efficiency = 25.0% and waste heat rejection rate = 90.0 MW

D

Carnot efficiency = 60.0% and waste heat rejection rate = 48.0 MW

Test Your Knowledge

An insulated block of metal transfers 6000 J of heat irreversibly from a high-temperature reservoir maintained at 600.0 K directly to a lower-temperature reservoir maintained at 300.0 K. What are the entropy changes of the hot reservoir (Delta S_hot), the cold reservoir (Delta S_cold), and the total universe (Delta S_univ)?

A

Delta S_hot = -20.0 J/K, Delta S_cold = +10.0 J/K, and Delta S_univ = -10.0 J/K

B

Delta S_hot = -10.0 J/K, Delta S_cold = +20.0 J/K, and Delta S_univ = +10.0 J/K

C

Delta S_hot = -10.0 J/K, Delta S_cold = +10.0 J/K, and Delta S_univ = 0 J/K

D

Delta S_hot = +10.0 J/K, Delta S_cold = -20.0 J/K, and Delta S_univ = -10.0 J/K

Test Your Knowledge

While non-polar liquids exhibit standard molar vaporization entropies close to 85-88 J/(molK) (Trouton's rule), liquid ethanol exhibits an anomalous Delta S_vap of 110.0 J/(molK), and crystalline carbon monoxide retains a residual entropy at 0 K close to the statistical value R ln 2 = 5.76 J/(molK) (about 4.6 J/(molK) is measured). What structural mechanisms account for these two physical observations?

A

Hydrogen bonding orders liquid ethanol, and CO freezes with random CO/OC orientations.

B

Ethanol has an unusually low boiling point relative to its molecular mass, while carbon monoxide possesses three degenerate nuclear spin states at absolute zero.

C

Ethanol vapor undergoes extensive gas-phase dimerization, while carbon monoxide molecules align in a perfectly ordered antiferroelectric crystalline lattice at 0 K.

D

Ethanol vapor has higher rotational symmetry than normal vapors, and carbon monoxide undergoes quantum tunneling between electronic ground states.

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