AP EAPCET (Engineering) · Physics (JEE & NEET)
Thermodynamics and Kinetic Theory of Gases
Laws of thermodynamics, thermodynamic processes, heat engines, and the kinetic theory relating pressure and temperature to molecular motion.
Ten concepts. Start with one sign convention, identify the process from what is fixed or from its graph, and then let the first law do the bookkeeping. The kinetic-theory half connects those same state variables to molecular energy, speeds, heat capacities and effusion.
- AP EAPCET (Engineering)
- Medium level
- 10 concepts
- 5 practice questions
1The first law and internal energy
The first law is conservation of energy written for a gas: Q = ΔU + W. Two sign conventions carry the whole thing — Q counts positive when heat enters the gas, and W counts positive when the gas expands and pushes something outward. Whatever heat is not spent as work stays behind as internal energy.
The one line worth memorising is ΔU = nC_VΔT. Internal energy of an ideal gas depends only on temperature, so that expression holds on every path — isobaric, adiabatic, a jagged path nobody named — not just at constant volume. Q and W depend on how you got there; ΔU does not.
This is the physics convention. If a source writes ΔU = Q + w, its w means work done on the gas and equals −W. Never mix the two halfway through a solution. Here expansion against nonzero external pressure has W > 0, free expansion has W = 0, and compression has W < 0; heat supplied has Q > 0, heat rejected Q < 0; and for an ideal gas ΔU has the sign of T₂ − T₁.
Figure. Heat entering splits exactly two ways: part leaves again as work when the piston moves out, and the rest stays behind as internal energy. Nothing else can happen to it — that is the whole of the first law.
How it works
- Heat inQ > 0 when heat flows into the gas, negative when the gas loses heat.
- Work outW > 0 when the gas expands against nonzero external pressure. Free expansion has W = 0; compression has W < 0.
- What is leftThe remainder shows up as temperature: ΔU = nC_VΔT, on any path at all.
- Check the signsExpansion against pressure, heating, and heat supplied point to W > 0, ΔU > 0, and Q > 0 respectively; free expansion has W = 0.
The path you were never told
Two moles of a monatomic ideal gas are taken from 300 K to 400 K along an unspecified path, absorbing 5000 J of heat. Find the work done by the gas.
- C_V = (3/2)R = 1.5 \times 8.3112.47 J mol⁻¹ K⁻¹
- \Delta U = nC_V\Delta T = 2 \times 12.47 \times 1002493 J
- W = Q - \Delta U = 5000 - 24932507 J
Pro tip. The path was never needed. ΔU asked only for the two temperatures, and once you have it the first law hands you W for free. Whenever a question refuses to name the process, this is why.
An ideal gas expands freely into an evacuated chamber inside a rigid, insulated container. Its temperature
- Falls, because expanding gases cool
- Is unchanged
- Rises, because the molecules speed up
Insulated means Q = 0. Expanding into vacuum means there is nothing to push against, so W = 0 too. Hence ΔU = 0, and for an ideal gas that forces ΔT = 0. Gases cool on expansion only when they do work.
2Work is the area under the curve
For a quasistatic path, W = ∫P dV means that on a P–V diagram the work done by the gas is the area under the path. In general W = ∫P_ext dV, so free expansion into vacuum has W = 0 even while the volume increases.
Because it is an area under a path, W is path-dependent — two routes joining the same two states enclose different areas and cost different work, even though ΔU is identical for both. Close the path into a loop and ΔU vanishes entirely, so the net heat equals the net work equals the enclosed area: positive going clockwise (an engine), negative going anticlockwise (a refrigerator).
Figure. The two horizontal legs do all the work; the vertical legs do none. What survives is the rectangle itself, and going round it clockwise means the expansion happened at the higher pressure — so the gas comes out ahead.
Reading a P–V diagram
- Area underFor a quasistatic path, the area under the P–V curve is the work done by the gas.
- Direction signsMoving right (expansion) counts positive, moving left counts negative.
- Close the loopRound a cycle ΔU = 0, so net heat = net work = the area inside the loop.
A rectangular cycle
A gas is taken clockwise round A(2 L, 3×10⁵ Pa) → B(5 L, 3×10⁵ Pa) → C(5 L, 1×10⁵ Pa) → D(2 L, 1×10⁵ Pa) → A. Find the net work and the net heat per cycle.
- W_{AB} = P\Delta V = 3 \times 10^{5} \times 3 \times 10^{-3}+900 J
- W_{CD} = 1 \times 10^{5} \times (-3 \times 10^{-3})−300 J
- W_{net} = 900 - 300 (BC and DA give 0)600 J
- \Delta U = 0 round a cycle, so Q_{net} = W_{net}600 J absorbed
Pro tip. You never needed the two legs separately: the enclosed rectangle is ΔP × ΔV = 2×10⁵ × 3×10⁻³ = 600 J directly. Traverse the same rectangle anticlockwise and every sign flips — 600 J of work must then be supplied.
3Isothermal processes
Hold the temperature fixed and PV = constant: the path is a hyperbola, one of a family with the hotter isotherms further from the origin. Doing this in practice means good thermal contact with a reservoir and a change slow enough for the gas to keep up.
Because T never changes, ΔU = 0 and the first law gives Q = W. For a reversible quasistatic ideal-gas path, their common value is nRT ln(V₂/V₁). Every joule of heat absorbed comes straight back out as work along that reversible path; on compression every joule of work put in is rejected as heat.
Figure. Every point on one hyperbola is the same temperature, so moving along it changes P and V but not U. The work is the area under the arc from V₁ to V₂ — and because ΔU is zero, that same area is the heat that had to be supplied.
How it works
- Fix TReservoir contact plus a slow change keeps the gas at the reservoir's temperature.
- ΔU = 0An ideal gas's internal energy tracks T alone, so it does not move.
- Q = WFor a reversible quasistatic ideal-gas path, Q = W = nRT ln(V₂/V₁), positive on expansion.
Heat straight through
Two moles of an ideal gas expand reversibly and isothermally at 300 K from 2 L to 8 L. Find the work done and the heat absorbed.
- nRT = 2 \times 8.31 \times 3004986 J
- \ln(V_2/V_1) = \ln 41.386
- W = 4986 \times 1.3866.91 × 10³ J
- \Delta U = 0, so Q = W6.91 kJ absorbed
Pro tip. Compress the same gas from 8 L back to 2 L and ln(1/4) = −1.386, giving W = −6.91 kJ with 6.91 kJ of heat rejected. Same magnitude, both signs flipped — the isothermal path is perfectly reversible in the bookkeeping.
During the isothermal expansion of an ideal gas, the heat absorbed is
- Zero, since the temperature does not change
- Equal to the work done by the gas
- Equal to the increase in internal energy
Constant temperature makes ΔU zero, not Q. With ΔU = 0 the first law gives Q = W exactly. It is the adiabatic process that has Q = 0 — confusing the two is the standard slip.
4Adiabatic processes
Adiabatic means Q = 0 — either the walls are insulating, or the change is too fast for heat to go anywhere. The first law then reads ΔU = −W. An adiabatic expansion that does positive work cools an ideal gas, while free expansion does no work and leaves its temperature unchanged. Adiabatic compression that has work done on the gas heats it.
Three equivalent relations describe a reversible adiabatic path, and picking the right one saves the integration: PV^{\gamma} = constant, TV^{\gamma-1} = constant, and TP^{(1-\gamma)/\gamma} = constant, with γ = C_P/C_V fixed by the molecule's degrees of freedom. Through any given state the adiabat is steeper than the isotherm — slope −γP/V against −P/V — by exactly the factor γ.
The bulk modulus is B=-V\,dP/dV. Therefore an ideal gas has isothermal bulk modulus B_T=P, but under adiabatic compression B_S=\gamma P. The gas is effectively stiffer when heat cannot escape; this is why the speed of sound is v=\sqrt{B_S/\rho}=\sqrt{\gamma P/\rho} rather than \sqrt{P/\rho}.
Figure. Both curves pass through the same state, but the adiabat leaves it more steeply in both directions. Expand along it and the pressure collapses faster because the gas is cooling as well as spreading out.
How it works
- Set Q = 0Insulated, or fast enough that heat has no time to flow either way.
- Pick the pairUse PV^γ for a P–V question, TV^(γ−1) for a T–V one. No integral needed.
- Work from ΔUW = −ΔU = nC_V(T₁ − T₂), also written nR(T₁ − T₂)/(γ − 1).
- Differentiate for stiffnessFrom PV^γ = constant, dP/dV = −γP/V and hence the adiabatic bulk modulus is B_S = γP.
Compression that heats without heat
Two moles of a rigid diatomic ideal gas at 300 K are compressed reversibly and adiabatically to one thirty-second of their volume. Find the final temperature and the work done by the gas.
- \gamma = 7/5 for a rigid diatomic, so \gamma - 10.4
- T_2 = T_1(V_1/V_2)^{0.4} = 300 \times 32^{0.4}1200 K
- \Delta U = nC_V\Delta T = 2 \times 2.5 \times 8.31 \times 9003.74 × 10⁴ J
- W = -\Delta U−37.4 kJ
Pro tip. 32^0.4 = (2⁵)^(2/5) = 2² = 4 exactly — adiabatic questions are built so the volume ratio is a clean power of 2 or 3. If your exponent produces an ugly decimal, you have probably used γ where γ − 1 belongs.
At the point where an isotherm and an adiabat cross on a P–V diagram, the adiabat is
- Less steep, because no heat enters
- Steeper, by a factor γ
- Of exactly the same slope
Differentiating PV = constant gives dP/dV = −P/V; differentiating PV^γ = constant gives −γP/V. Since γ > 1 the adiabat always falls away faster — which is why an adiabatic expansion does less work than an isothermal one between the same volumes.
5Isobaric, isochoric and polytropic processes
An isobaric process holds pressure fixed. The gas moves along a horizontal line on a P–V graph, does W=P(V_2-V_1)=nR\Delta T, changes internal energy by nC_V\Delta T, and exchanges Q=nC_P\Delta T: heat is absorbed for \Delta T>0 and rejected for \Delta T<0. At fixed pressure, Charles's law gives V/T= constant, so V against kelvin temperature is a straight line through the origin.
An isochoric process holds volume fixed. Its P–V path is vertical, so dV=0 and W = 0; every joule of heat changes internal energy, Q=\Delta U=nC_V\Delta T. At fixed volume, P/T= constant, so P against kelvin temperature is a straight line through the origin.
A quasistatic polytropic path obeys PV^N= constant. It contains the familiar ideal-gas paths as special cases: N = 0 is isobaric, N = 1 is reversible isothermal, N = γ is reversible adiabatic, and the limiting case N → ∞ approaches an isochore. For N ≠ 1, W=(P_2V_2-P_1V_1)/(1-N); then use \Delta U=nC_V\Delta T and Q=\Delta U+W rather than trying to memorise a separate heat formula.
Figure. On P–V axes the fingerprints are immediate: isobaric is horizontal, isochoric vertical, isothermal a rectangular hyperbola. One panel carries the three rules the multi-graph table names.
Identify the process before calculating
- Read what is fixedP fixed means isobaric, V fixed is isochoric, T fixed is isothermal, and Q = 0 is adiabatic.
- Read the graphOn P–V axes: horizontal isobar, vertical isochore, rectangular-hyperbola isotherm, and a steeper falling adiabat.
- Use the first lawCompute W from the path and ΔU from temperature; Q follows from Q = ΔU + W with no new convention.
| Process | P–V graph | P–T graph (T on x-axis) | V–T graph (T on x-axis) |
|---|---|---|---|
| Isobaric, P fixed | Horizontal line | Horizontal line | Straight line through kelvin origin |
| Isochoric, V fixed | Vertical line | Straight line through kelvin origin | Horizontal line |
| Isothermal, T fixed | Rectangular hyperbola, PV = constant | Vertical line | Vertical line |
| Reversible adiabatic | PV^γ = constant; steeper than isotherm | T ∝ P^((γ−1)/γ) | T ∝ V^(1−γ) |
| Polytropic | PV^N = constant | T ∝ P^((N−1)/N) | T ∝ V^(1−N) |
Constant-pressure heating
One mole of a monatomic ideal gas is heated at constant pressure from 300 K to 600 K. Find W, ΔU and Q.
- W=nR\Delta T=1\times8.31\times300+2.49 kJ
- \Delta U=nC_V\Delta T=1\times(3R/2)\times300+3.74 kJ
- Q=\Delta U+W+6.23 kJ
- Check: Q=nC_P\Delta T=1\times(5R/2)\times300+6.23 kJ
Pro tip. All three signs are positive here: heat enters, temperature rises, and the gas expands against constant pressure. At constant volume the same temperature rise would have W = 0 and would need only 3.74 kJ.
A gas is heated at constant volume. Which statement is necessarily correct?
- All supplied heat becomes internal energy
- The gas does positive work
- Its pressure remains constant
At fixed volume dV = 0, so W = ∫P dV = 0 and Q = ΔU. The pressure rises with absolute temperature; it is not held fixed.
6Kinetic theory: where pressure comes from
Treat the gas as point molecules in ceaseless random motion, colliding elastically and feeling no forces in between. A molecule rebounding off a wall reverses v_x and hands the wall 2mv_x of momentum; add up every such bounce per second over the whole wall and the force per unit area comes out as P = (1/3)Nm⟨v²⟩/V, or equivalently P = (1/3)ρv_rms².
Set that beside the experimental PV = nRT and the two can only agree if (1/2)m⟨v²⟩ = (3/2)k_BT. Temperature is nothing but the average translational kinetic energy of a molecule, measured in different units — and notice that the molecular mass has dropped out.
Figure. One molecule striking the right-hand wall and rebounding reverses its x-velocity, so the wall absorbs 2mv_x. Pressure is nothing more than the time-average of billions of such kicks per square metre.
From one bounce to a pressure
- One moleculeAn elastic bounce off the wall reverses v_x, delivering 2mv_x of momentum.
- Add them upAveraging over all molecules and directions gives P = (1/3)Nm⟨v²⟩/V.
- Match PV = nRTComparing the two forces (1/2)m⟨v²⟩ = (3/2)k_BT per molecule.
Pressure is energy density
Two moles of any ideal gas occupy a 10 L vessel at 300 K. Find the total translational kinetic energy of the molecules and the pressure.
- nRT = 2 \times 8.31 \times 3004986 J
- KE = (3/2)nRT = 1.5 \times 49867479 J
- P = nRT/V = 4986/0.014.99 × 10⁵ Pa
- Check: P = (2/3)(KE/V) = (2/3)(7479/0.01)4.99 × 10⁵ Pa
Pro tip. The molecular mass never entered. Two moles of hydrogen and two moles of xenon at 300 K in the same vessel carry identical translational energy and press on the walls identically — the heavy molecules simply move more slowly to do it.
Two equal vessels at the same temperature hold equal numbers of hydrogen and oxygen molecules. Compared with hydrogen, the oxygen sample has
- A higher pressure, its molecules being heavier
- The same pressure and the same average translational KE per molecule
- A lower average kinetic energy per molecule
P = Nk_BT/V involves the number of molecules and the temperature, never the mass; and the average translational energy is (3/2)k_BT for every gas alike. Mass shows up in one place only — the rms speed.
7Molecular speeds
The molecules do not share one speed; they are spread over the Maxwell distribution, and three points on it get named. In descending order: v_rms = √(3RT/M), then v_avg = √(8RT/πM), then the most probable speed v_mp = √(2RT/M) at the peak — in the fixed ratio √3 : √(8/π) : √2, roughly 1.73 : 1.60 : 1.41.
All three scale the same way, as √(T/M). At a given temperature the lighter gas is faster, v₁/v₂ = √(M₂/M₁); for a given gas, doubling any characteristic speed costs four times the kelvin temperature. The molecular forms are v_{mp}=\sqrt{2k_BT/m}, v_{avg}=\sqrt{8k_BT/(\pi m)} and v_{rms}=\sqrt{3k_BT/m}. Heating also flattens and broadens the curve, sliding the peak to the right while keeping its total area fixed.
Figure. Heating does not slide the curve bodily to the right — it lowers and widens it as well, because the same number of molecules must spread over a wider range of speeds. The long tail on the right is what makes evaporation and chemical reactions possible at all.
Two scalings to keep
- Same T, lighter gasSpeeds go as 1/√M — hydrogen beats oxygen by a factor of 4.
- Same gas, hotterSpeeds go as √T, so 4× the kelvin temperature to double the speed.
- Which speed?v_rms for anything energetic; v_mp only when asked for the peak of the curve.
Oxygen, then hydrogen
Find the rms speed of oxygen molecules (M = 32 g mol⁻¹) at 300 K, then the rms speed of hydrogen (M = 2 g mol⁻¹) at the same temperature. Use R = 8.31 J mol⁻¹ K⁻¹.
- 3RT = 3 \times 8.31 \times 3007479 J mol⁻¹
- 3RT/M = 7479/0.0322.34 × 10⁵ m² s⁻²
- v_{rms}(O_2) = \sqrt{2.34 \times 10^{5}}483 m s⁻¹
- v_{rms}(H_2) = 483 \times \sqrt{32/2}1.93 × 10³ m s⁻¹
Pro tip. Put M in kg mol⁻¹ whenever R = 8.31 — using grams shrinks the answer by √1000, turning 483 m s⁻¹ into 15. And note the second line needed no fresh calculation, only the mass ratio: hydrogen molecules move four times faster than oxygen at the same temperature, which is a large part of why the Earth has kept its oxygen and lost nearly all its free hydrogen.
The rms speed of a gas at 300 K is v. Its rms speed is 2v at
- 600 K
- 1200 K
- 900 K
v_rms ∝ √T, so doubling the speed needs four times the absolute temperature: 4 × 300 = 1200 K. The 600 K answer treats the dependence as linear.
8Graham's law of effusion and diffusion
Graham's law says that at the same temperature and pressure the rate at which a gas effuses through a tiny hole, or approximately diffuses, is inversely proportional to the square root of its molar mass: r\propto1/\sqrt{M}. Hence r_1/r_2=\sqrt{M_2/M_1}. At equal pressure and temperature density is proportional to molar mass, so the same ratio may be written r_1/r_2=\sqrt{\rho_2/\rho_1}.
A time is the reciprocal of a rate. For equal amounts passing under the same conditions, t_1/t_2=r_2/r_1=\sqrt{M_1/M_2}. The law has the same mass dependence as every Maxwell speed because the faster molecules reach and cross the opening more often; do not reverse the ratio when the question switches from rate to time.
Figure. With oxygen's rate set to 1, helium's rate is √(32/4) = √8 ≈ 2.83. The bars compare rates under identical temperature, pressure and opening conditions.
Rate ratio without a sign error
- Put the asked gas on topFor r₁/r₂, put the other gas's molar mass M₂ in the numerator under the square root.
- Check lighter means fasterIf gas 1 is lighter, the computed r₁/r₂ must exceed 1.
- Invert for timeFor equal transferred amounts, t₁/t₂ = r₂/r₁; the faster gas takes less time.
Helium against oxygen
Helium and oxygen effuse through the same small opening at the same temperature and pressure. Compare their rates and the times needed for equal amounts to escape.
- r_{He}/r_{O_2}=\sqrt{M_{O_2}/M_{He}}=\sqrt{32/4}\sqrt8
- \sqrt82.83
- t_{He}/t_{O_2}=r_{O_2}/r_{He}1/2.83 = 0.354
Pro tip. The sanity check is physical: helium is lighter, so its rate must be larger and its time smaller. If both ratios come out on the same side of 1, one of them has not been inverted.
Gas A takes four times as long as gas B to effuse in equal amount under identical conditions. The molar-mass ratio M_A/M_B is
- 16
- 4
- 1/16
Time varies as √M. Thus t_A/t_B = 4 = √(M_A/M_B), and squaring gives M_A/M_B = 16.
9Degrees of freedom and specific heats
Equipartition says every active quadratic energy term carries (1/2)k_BT per molecule, i.e. (1/2)RT per mole. There are three translational terms for every molecule. A rigid linear molecule adds two rotational terms; a rigid non-linear molecule adds three. Each active vibrational mode contributes two terms — one kinetic and one potential — and therefore contributes k_BT per molecule rather than half of it.
From the total number f of active quadratic terms everything drops out: molar C_V=(f/2)R, then Mayer's relation C_P=C_V+R, and \gamma=C_P/C_V=1+2/f. The extra R in C_P is not extra molecular energy storage — it is the P\Delta V=R\Delta T of work one mole must do while expanding at constant pressure.
At ordinary JEE temperatures, vibrational modes of common diatomic gases are usually treated as frozen, so f = 5, C_V=5R/2, C_P=7R/2 and γ = 7/5. At higher temperature vibration becomes active and the heat capacities rise while γ falls. If the question asks for specific heat per unit mass rather than molar heat capacity, divide by molar mass: c_V=C_V/M and c_P=C_P/M.
Figure. Equipartition counts active quadratic terms: 3 translational for every gas, plus 2 rotations for a rigid linear molecule (f = 5), plus a third rotation when the molecule is non-linear (f = 6). The excluded bond-axis spin never earns a term.
How it works
- Count f3 for a monatom, 5 for a rigid linear molecule, 6 for a rigid non-linear molecule; add 2 for each active vibrational mode.
- C_V = (f/2)RInternal energy per mole is (f/2)RT, so heating at fixed V costs (f/2)R.
- Add R for C_PAt constant pressure the gas also does RΔT of work, so C_P = C_V + R.
| Gas | f | C_V | C_P | γ |
|---|---|---|---|---|
| Monatomic (He, Ar) | 3 | 1.5R | 2.5R | 5/3 ≈ 1.67 |
| Rigid diatomic (O₂, N₂) | 5 | 2.5R | 3.5R | 7/5 = 1.40 |
| Diatomic with vibration | 7 | 3.5R | 4.5R | 9/7 ≈ 1.29 |
| Rigid linear polyatomic | 5 | 2.5R | 3.5R | 7/5 = 1.40 |
| Non-linear polyatomic | 6 | 3R | 4R | 4/3 ≈ 1.33 |
γ of a mixture
One mole of helium is mixed with two moles of oxygen, both treated as ideal and the oxygen as rigid. Find C_V and γ of the mixture.
- C_V: helium (3/2)R, oxygen (5/2)R1.5R, 2.5R
- C_V = (1 \times 1.5R + 2 \times 2.5R)/32.17R
- C_P = C_V + R3.17R
- \gamma = C_P/C_V = 19/131.46
Pro tip. γ of a mixture is never the mole-weighted average of the γs — that would give (1.67 + 2×1.40)/3 = 1.49, not 1.46. Average the C's, which are energies per kelvin and therefore genuinely additive, and take the ratio only at the end.
C_P exceeds C_V by exactly R because
- At constant pressure the gas must also do PΔV = RΔT of work
- More degrees of freedom become active at constant pressure
- R is the energy carried by one degree of freedom
The molecule's degrees of freedom are a property of the molecule and do not care how you heat it — ΔU = nC_VΔT either way. The difference is entirely the expansion work, and for one mole of an ideal gas PΔV = RΔT exactly.
10Heat engines and the Carnot limit
An engine works in cycles, taking Q_H from a hot reservoir, dumping Q_C into a cold one and delivering the difference as work: W = Q_H − Q_C, with efficiency η = W/Q_H = 1 − Q_C/Q_H. The second law, in Kelvin's phrasing, forbids Q_C from being zero — no cycle turns heat entirely into work, so η < 1 always.
Carnot's theorem sharpens that into a number. Between two reservoirs no engine beats η = 1 − T_C/T_H, achieved by the reversible cycle of two isotherms and two adiabats, and the ceiling depends on the two temperatures alone — not on the gas, the design, or the engineering budget. Temperatures must be in kelvin. Run the same cycle backwards and it becomes a refrigerator, moving heat uphill with COP = Q_C/W = T_C/(T_H − T_C).
Figure. Heat enters only along AB, at T_H, and leaves only along CD, at T_C; the two adiabatic legs BC and DA exchange none. That is why the efficiency can depend on nothing but the two temperatures.
How it works
- Split the heatEvery joule from the source either leaves as work or is dumped into the sink.
- Kelvin onlyη = 1 − T_C/T_H is meaningless in Celsius — convert first, every time.
- Reverse itDriven backwards, the engine pumps heat: COP = T_C/(T_H − T_C).
The same machine, both ways
A Carnot engine runs between a source at 500 K and a sink at 300 K, absorbing 600 J per cycle. Find its efficiency, the work per cycle and the heat rejected — then its COP if it is run in reverse.
- \eta = 1 - 300/5000.40
- W = \eta Q_H = 0.4 \times 600240 J
- Q_C = 600 - 240360 J
- Reversed: COP = 300/(500 − 300)1.5
Pro tip. The last two lines are the same machine seen twice: 360 J moved for 240 J of work is 360/240 = 1.5, exactly the COP. A refrigerator's COP routinely exceeds 1, which is not a violation of anything — it moves heat rather than creating work.
An engine is claimed to absorb 600 J at 500 K and deliver 300 J of work, rejecting the rest at 300 K. This engine is
- Impossible — it exceeds the Carnot limit
- Possible, but inefficient
- Possible; it is exactly a Carnot engine
The claim is η = 300/600 = 0.50, while the Carnot ceiling between 500 K and 300 K is 1 − 300/500 = 0.40. No engine, reversible or not, can beat that ceiling, so the claim breaks the second law.
Notes
- First law and signs: This chapter uses Q=\Delta U+W, where Q>0 for heat supplied to the gas and W>0 for work done by the gas. Expansion against nonzero external pressure gives W>0, free expansion into vacuum gives W=0, and compression gives W<0; heating gives \Delta U>0 and cooling \Delta U<0 for an ideal gas. Some chemistry books instead write \Delta U=Q+w with w the work done on the gas, so w=-W.
- Thermodynamic processes: For a reversible isothermal ideal gas, T is constant and W=nRT\ln\tfrac{V_2}{V_1}. For a reversible adiabatic ideal gas with constant \gamma, Q=0 and PV^\gamma=\text{const}. Isobaric holds P constant, isochoric holds V constant, and a quasistatic polytropic path obeys PV^N=\text{const}.
- State graphs: On a P-V plot an isobar is horizontal, an isochore vertical, an isotherm a rectangular hyperbola and an adiabat a steeper falling curve. For an ideal gas, a fixed-volume P-T graph and a fixed-pressure V-T graph are straight lines through the kelvin origin.
- Kinetic theory: Pressure arises from molecular collisions, P=\tfrac13\dfrac{Nm\overline{v^2}}{V}, giving PV=nRT. The three molecular speeds are v_{mp}=\sqrt{2RT/M}, v_{avg}=\sqrt{8RT/(\pi M)} and v_{rms}=\sqrt{3RT/M}.
- Degrees of freedom and specific heats: Equipartition gives \tfrac12 k_BT per quadratic degree of freedom; each active vibrational mode contributes twice because it has kinetic and potential terms. For f active quadratic terms, C_V=\tfrac{f}{2}R, C_P=C_V+R and \gamma=1+\tfrac{2}{f}.
- Graham's law: At the same temperature and pressure, the rate of effusion or diffusion varies as 1/\sqrt{M}, so r_1/r_2=\sqrt{M_2/M_1} and the corresponding times obey t_1/t_2=\sqrt{M_1/M_2}.
- Second law and heat engines: No engine can convert heat entirely into work. A Carnot engine operating between T_H and T_C has the maximum efficiency \eta=1-\dfrac{T_C}{T_H} (temperatures in kelvin).
Formulas
- First law: Q=\Delta U+W,\quad W=\int P_{ext}\,dV; for a quasistatic path P_{ext}=P
- Reversible ideal-gas paths: W_{iso}=nRT\ln\dfrac{V_2}{V_1}; adiabatic PV^\gamma=\text{const} for constant \gamma
- Polytropic process: PV^N=\text{const},\quad W=\dfrac{P_2V_2-P_1V_1}{1-N} for N\ne1
- Ideal gas speeds: v_{mp}=\sqrt{\dfrac{2RT}{M}},\quad v_{avg}=\sqrt{\dfrac{8RT}{\pi M}},\quad v_{rms}=\sqrt{\dfrac{3RT}{M}}
- Specific heats: C_V=\tfrac{f}{2}R,\quad C_P=C_V+R,\quad \gamma=1+\tfrac{2}{f}
- Internal energy: \Delta U=nC_V\Delta T
- Adiabatic bulk modulus: B=-V\dfrac{dP}{dV}=\gamma P
- Graham's law: \dfrac{r_1}{r_2}=\sqrt{\dfrac{M_2}{M_1}}=\sqrt{\dfrac{\rho_2}{\rho_1}} at the same temperature and pressure
- Carnot efficiency: \eta=1-\dfrac{T_C}{T_H}
Exam traps & shortcuts
- For a reversible adiabatic ideal gas with constant \gamma, use TV^{\gamma-1}=\text{const} or T P^{(1-\gamma)/\gamma}=\text{const} to relate two states without computing work.
- For a cyclic process \Delta U=0, so net heat equals net work, which is just the area enclosed by the cycle on a P-V diagram.
- For signs, first decide the system and direction: heat entering is positive, expansion against nonzero external pressure does positive work, free expansion does zero work, and a rise in ideal-gas temperature makes \Delta U positive.
- On a common P-V graph through the same state, the adiabatic slope is -\gamma P/V while the isothermal slope is -P/V, so the adiabat is steeper.
- All characteristic molecular speeds depend on \sqrt{T/M}. Their order is v_{rms}>v_{avg}>v_{mp}, while Graham's rate ratio has the same inverse-square-root molar-mass dependence.
Reference tables
The system is the gas, and W means work done by the gas. Write these three definitions before substituting numbers; a negative answer then describes the opposite direction rather than an algebra mistake.
| Quantity | Positive | Negative | Zero in the common special case |
|---|---|---|---|
| Heat Q | Heat supplied to the gas | Heat rejected by the gas | Adiabatic process |
| Work W by gas | Expansion against nonzero external pressure | Compression, V₂ < V₁ | Isochoric process or free expansion into vacuum |
| Internal-energy change ΔU | Temperature rises for an ideal gas | Temperature falls for an ideal gas | Isothermal ideal-gas process or a complete cycle |
Every row uses Q = ΔU + W with W defined as work done by the gas. The ideal-gas relation ΔU = nC_VΔT remains valid on every row.
| Process | Held fixed | W by gas | ΔU | Q |
|---|---|---|---|---|
| Reversible isothermal ideal gas | T | nRT ln(V₂/V₁) | 0 | = W |
| Isobaric | P | PΔV = nRΔT | nC_VΔT | nC_PΔT |
| Isochoric | V | 0 | nC_VΔT | = ΔU |
| Reversible adiabatic ideal gas | Q = 0 | nR(T₁ − T₂)/(γ − 1) | nC_VΔT | 0 |
| Quasistatic polytropic | PV^N = constant | (P₂V₂ − P₁V₁)/(1 − N), N ≠ 1 | nC_VΔT | = ΔU + W |
| Free expansion, ideal gas | Into vacuum; rigid insulated vessel | 0 | 0, hence ΔT = 0 | 0 |
| Cyclic | Final state = initial state | Area enclosed on P–V graph | 0 over the cycle | = W_net |
Every line here should be reconstructible from the concept above it, not merely recalled.
| Quantity | Relation | Watch for |
|---|---|---|
| First law | Q = ΔU + W | W is work done by the gas |
| Internal energy | ΔU = nC_VΔT | Holds on every path, not just at constant V |
| Work | W = ∫P_ext dV; for quasistatic motion P_ext = P | Area under the P–V path |
| Reversible isothermal work | W = nRT ln(V₂/V₁) | ΔU = 0, so Q = W |
| Reversible adiabatic ideal-gas path | PV^γ = const, TV^(γ−1) = const | γ − 1, not γ, in the T–V form |
| Reversible adiabatic work | W = nR(T₁ − T₂)/(γ − 1) | Positive exactly when the gas cools |
| Adiabatic bulk modulus | B_S = γP; isothermal B_T = P | Sound speed is √(γP/ρ) |
| Polytropic path | PV^N = constant; W = (P₂V₂ − P₁V₁)/(1 − N) | N = 0, 1, γ, ∞ maps to isobaric, isothermal, adiabatic, isochoric |
| Specific heats | C_V = (f/2)R, C_P = C_V + R | Each active vibration adds 2 to f |
| Pressure | P = (1/3)ρv_rms² | ρ is mass per unit volume, not density of molecules |
| Energy per molecule | (3/2)k_BT of translation | Independent of molecular mass |
| Characteristic speeds | v_mp = √(2RT/M), v_avg = √(8RT/πM), v_rms = √(3RT/M) | v_rms > v_avg > v_mp; M in kg mol⁻¹ with R = 8.31 |
| Graham's law | r₁/r₂ = √(M₂/M₁) = √(ρ₂/ρ₁) | Time ratio is the inverse rate ratio |
| Carnot efficiency | η = 1 − T_C/T_H | Kelvin only; it is a ceiling, not a prediction |
| Refrigerator | COP = T_C/(T_H − T_C) | Routinely greater than 1 |
Recap
Read only this the night before.
- First law
- Q = ΔU + W, with heat into and work by the gas positive. Expansion against pressure has W > 0; free expansion W = 0; compression W < 0. ΔU = nC_VΔT on every path.
- The diagram
- Area under the path is W; area inside a closed loop is the net heat. Clockwise is positive.
- Isothermal vs adiabatic
- Isothermal: ΔU = 0, Q = W. Adiabatic: Q = 0, W = −ΔU, B = γP. The adiabat is steeper by γ.
- Other processes
- Isobaric: W = PΔV and Q = nC_PΔT. Isochoric: W = 0 and Q = ΔU. Polytropic: PV^N = constant.
- Counting
- f decides everything: C_V = (f/2)R, C_P = C_V + R, γ = 1 + 2/f. f = 3, 5, 6 gives 5/3, 7/5, 4/3.
- Molecules
- v_rms > v_avg > v_mp, and all go as √(T/M). Graham's rate goes as 1/√M; the time ratio is its inverse.
- Engines
- η = 1 − T_C/T_H is a ceiling nobody beats. Kelvin only. Reversed, COP = T_C/(T_H − T_C).
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