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Thermodynamics · JEE & NEET Physics

Thermodynamic Processes: notes and previous year questions

Isothermal, adiabatic, isobaric and isochoric processes: their laws, work, heat and curves.

Thermodynamic Processes in short

  • Isothermal: T fixed, slow, on a reservoir; PV = constant; ΔU = 0 and Q = W.
  • Adiabatic: Q = 0 (fast or insulated); PVᵞ = constant; ΔU = −W.
  • An adiabatic expansion cools a gas; an adiabatic compression heats it.
  • Isobaric: P fixed; V/T constant; W = PΔV and Q = nCₚΔT.

1The four processes

From a starting point A on a P–V graph, a gas can change in many ways. Four are special:

ProcessWhat is fixedCurveHow to make it
Isobaricpressure Phorizontal linea free piston with a fixed load
Isochoricvolume Vvertical linea rigid closed container
Isothermaltemperature Thyperbola PV = constslow, conducting walls, a reservoir
Adiabaticno heat, Q = 0steeper curvefast, or insulated walls

2Isothermal

A gas on a large reservoir expands slowly. It would cool as it pushes the piston, but heat flows in and keeps TT fixed. With PV=nRTPV = nRT and TT constant:

PV=constant,P1V1=P2V2PV = \text{constant},\quad P_1V_1 = P_2V_2A rectangular hyperbola on the P–V graph.

For an ideal gas ΔU=0\Delta U = 0, so Q=WQ = W. Putting P=nRT/VP = nRT/V into W=∫P dVW = \int P\,dV:

W=nRTln⁡V2V1=nRTln⁡P1P2W = nRT\ln\frac{V_2}{V_1} = nRT\ln\frac{P_1}{P_2}

In an isothermal compression, W<0W < 0 and the same amount of heat flows out to the reservoir. Either way the process must be slow.

3Adiabatic

With insulated walls, or a change too fast for heat to flow, Q=0Q = 0 and ΔU=−W\Delta U = -W. A diesel engine squeezes air about 10 times: it heats from 300 K to about 750 K, hot enough to light the fuel without a spark.

Where the law comes from. nCv dT=−P dVnC_v\,dT = -P\,dV; from PV=nRTPV = nRT, P dV+V dP=nR dTP\,dV + V\,dP = nR\,dT. Eliminating dTdT and using Cp=Cv+RC_p = C_v + R gives γ dVV=−dPP\gamma\,\frac{dV}{V} = -\frac{dP}{P}; integrating, γln⁡V+ln⁡P\gamma \ln V + \ln P = constant.

PVγ=constantPV^\gamma = \text{constant}
TVγ−1=constantTV^{\gamma - 1} = \text{constant}
TγP1−γ=constantT^\gamma P^{1 - \gamma} = \text{constant}
W=nR(T1−T2)γ−1=P1V1−P2V2γ−1W = \frac{nR(T_1 - T_2)}{\gamma - 1} = \frac{P_1V_1 - P_2V_2}{\gamma - 1}

An adiabatic expansion cools the gas; a compression warms it. Real examples: a bicycle pump, diesel ignition, sound waves (which is why γ is in the speed of sound), and rising air that cools to form clouds.

4Steeper curves

Differentiating PV=KPV = K gives the isothermal slope; differentiating PVγ=KPV^\gamma = K gives the adiabatic one:

(dPdV)iso=−PV\left(\frac{dP}{dV}\right)_{\text{iso}} = -\frac{P}{V}
(dPdV)adia=−γPV\left(\frac{dP}{dV}\right)_{\text{adia}} = -\gamma\frac{P}{V}

So through the same point the adiabatic is γ times steeper: in an expansion its pressure falls faster because the gas also cools. Steepness order: isochoric (vertical) > adiabatic > isothermal > isobaric (flat). If an isothermal slope is −2 atm/L, the adiabatic one (γ=1.4\gamma = 1.4) is −2.8 atm/L.

5Isobaric and isochoric

Isobaric (P fixed)Isochoric (V fixed)
Gas lawV/T = constant (Charles)P/T = constant (Gay-Lussac)
WorkW=PΔV=nRΔTW = P\Delta V = nR\Delta TW=0W = 0
HeatQ=nCpΔTQ = nC_p\Delta TQ=ΔU=nCvΔTQ = \Delta U = nC_v\Delta T
Graphhorizontal linevertical line, no area

6Comparing processes

Expand from the same start to the same final volume (6×1056 \times 10^5 Pa, 1 L to 4 L): the isobaric line stays highest (1800 J of work), the isothermal falls (about 832 J), and the adiabatic falls fastest (about 638 J). The isobaric gas ends hotter (T × 4), the isothermal the same, the adiabatic cooler (T × 0.57).

Wisobaric>Wisothermal>WadiabaticW_{\text{isobaric}} > W_{\text{isothermal}} > W_{\text{adiabatic}}

Summary

Key ideas

  • Isothermal: T fixed, slow, on a reservoir; PV = constant; ΔU = 0 and Q = W.
  • Adiabatic: Q = 0 (fast or insulated); PVᵞ = constant; ΔU = −W.
  • An adiabatic expansion cools a gas; an adiabatic compression heats it.
  • Isobaric: P fixed; V/T constant; W = PΔV and Q = nCₚΔT.
  • Isochoric: V fixed; P/T constant; W = 0 and Q = ΔU = nCᵥΔT.
  • Work is the area under the curve on a P–V graph.
  • Through one point the adiabatic is γ times steeper than the isothermal.
  • Between the same volumes, isobaric work > isothermal > adiabatic.

Every equation

Isothermal law
P1V1=P2V2P_1V_1 = P_2V_2
Isothermal work
W=nRTln⁡(V2/V1)W = nRT\ln(V_2/V_1)
Isothermal work
W=nRTln⁡(P1/P2)W = nRT\ln(P_1/P_2)
Adiabatic law
PVγ=constPV^\gamma = \text{const}
Adiabatic law
TVγ−1=constTV^{\gamma-1} = \text{const}
Adiabatic law
TγP1−γ=constT^\gamma P^{1-\gamma} = \text{const}
Adiabatic work
W=nR(T1−T2)γ−1W = \frac{nR(T_1 - T_2)}{\gamma - 1}
Adiabatic work
W=P1V1−P2V2γ−1W = \frac{P_1V_1 - P_2V_2}{\gamma - 1}
Isobaric
V/T=const, W=PΔV=nRΔTV/T = \text{const},\ W = P\Delta V = nR\Delta T
Isobaric heat
Q=nCpΔTQ = nC_p\Delta T
Isochoric
P/T=const, W=0P/T = \text{const},\ W = 0
Isochoric heat
Q=ΔU=nCvΔTQ = \Delta U = nC_v\Delta T
Isothermal slope
dP/dV=−P/VdP/dV = -P/V
Adiabatic slope
dP/dV=−γP/VdP/dV = -\gamma P/V

Previous year questions with solutions

Real JEE and NEET questions on thermodynamic processes. Try each one before you open the solution.

Q1NEET 2026One correct option

An electric heater supplies heat to a system at a rate of 100 W . If the system performs work at a rate of 75 J/s75\ \mathrm{J/s}, then the rate at which internal energy increases will be:

  1. A75 W
  2. B100 W
  3. C125 W
  4. D25 W
Show answer and solution

Answer: Option D

The first law holds for every second of the process, so it can be written as rates: heat in per second == rise of internal energy per second ++ work done per second.

100=dUdt+75100 = \dfrac{dU}{dt} + 75, so dUdt=25 W\dfrac{dU}{dt} = 25\ \mathrm{W}.

The trap is A, 75 W75\ \mathrm{W}, the rate of doing work, and B, 100 W100\ \mathrm{W}, the whole heating rate — as if no work were done. C, 125 W125\ \mathrm{W}, adds the work to the heat, getting the sign of WW backwards: work done BY the system is energy leaving it.

Q2JEE Main 2026One correct option

Heat is supplied to a diatomic gas at constant pressure. Then the ratio of ΔQ:ΔU:ΔW\Delta Q:\Delta U:\Delta W is ______.

  1. A2 : 3 : 5
  2. B5 : 3 : 2
  3. C2 : 5 : 7
  4. D7 : 5 : 2
Show answer and solution

Answer: Option D

At constant pressure, per mole and per kelvin: ΔQ=CP ΔT\Delta Q = C_{P}\,\Delta T, ΔU=CV ΔT\Delta U = C_{V}\,\Delta T and ΔW=R ΔT\Delta W = R\,\Delta T. For a diatomic gas CV=52RC_{V} = \dfrac{5}{2}R and CP=72RC_{P} = \dfrac{7}{2}R, so

ΔQ:ΔU:ΔW=72:52:1=7:5:2\Delta Q : \Delta U : \Delta W = \dfrac{7}{2} : \dfrac{5}{2} : 1 = 7 : 5 : 2

Check with the first law: 7=5+27 = 5 + 2.

The trap is B, 5:3:25 : 3 : 2, which is the monatomic gas (52:32:1\dfrac{5}{2} : \dfrac{3}{2} : 1). A and C list the same numbers backwards, in the order W:U:QW : U : Q — and neither passes the check that QQ is the sum of the other two.

Q3JEE Main 2026Numerical answer

A diatomic gas (γ=1.4)(\gamma =1.4) does 100 J of work when it is expanded isobarically. Then the heat given to the gas ____\_\_\_\_ J.

Show answer and solution

Answer: 350

At constant pressure W=nR ΔTW = nR\,\Delta T and Q=nCP ΔTQ = nC_{P}\,\Delta T, so QW=CPR\dfrac{Q}{W} = \dfrac{C_{P}}{R}. With γ=1.4=75\gamma = 1.4 = \dfrac{7}{5} the gas is diatomic, CP=72RC_{P} = \dfrac{7}{2}R, and QW=72\dfrac{Q}{W} = \dfrac{7}{2} (the same as γγ−1=1.40.4=3.5\dfrac{\gamma}{\gamma - 1} = \dfrac{1.4}{0.4} = 3.5).

Q=3.5×100=350 JQ = 3.5 \times 100 = 350\ \mathrm{J}: 100 J100\ \mathrm{J} goes into work and 250 J250\ \mathrm{J} into internal energy.

The trap is 250 J250\ \mathrm{J}, which is ΔU\Delta U and forgets the work itself. Another is 140 J140\ \mathrm{J}, γ×100\gamma \times 100, which treats γ\gamma as the ratio of heat to work — that ratio is CPR\dfrac{C_{P}}{R}, not CPCV\dfrac{C_{P}}{C_{V}}.

Practice questions, easy to hard

Three questions from the thermodynamic processes practice ladder: one easy, one medium, one hard.

Q4One correct option

Two simple processes follow straight from the first law.

Constant volume (isochoric): the gas pushes nothing back, so W=0W = 0 and all the heat goes into internal energy, Q=ΔU=nCV ΔTQ = \Delta U = nC_{V}\,\Delta T.

Constant pressure (isobaric): W=p ΔV=nR ΔTW = p\,\Delta V = nR\,\Delta T (from pV=nRTpV = nRT), and Q=ΔU+W=n(CV+R) ΔT=nCP ΔTQ = \Delta U + W = n(C_{V} + R)\,\Delta T = nC_{P}\,\Delta T. So the fraction of the heat that becomes work is

WQ=RCP=1−1γ\dfrac{W}{Q} = \dfrac{R}{C_{P}} = 1 - \dfrac{1}{\gamma}

and the fraction that becomes internal energy is CVCP=1γ\dfrac{C_{V}}{C_{P}} = \dfrac{1}{\gamma}.

A monatomic ideal gas is given 500 J500\ \mathrm{J} of heat at constant pressure. How much work does it do?

  1. A300 J300\ \mathrm{J}
  2. B500 J500\ \mathrm{J}
  3. C200 J200\ \mathrm{J}
  4. D143 J143\ \mathrm{J}
Show answer and solution

Answer: Option C

For a monatomic gas CV=32RC_{V} = \dfrac{3}{2}R and CP=52RC_{P} = \dfrac{5}{2}R, so WQ=RCP=25\dfrac{W}{Q} = \dfrac{R}{C_{P}} = \dfrac{2}{5} and W=25×500=200 JW = \dfrac{2}{5} \times 500 = 200\ \mathrm{J}. The other 300 J300\ \mathrm{J} raises the internal energy.

The trap is A, 300 J300\ \mathrm{J}, which is ΔU\Delta U, not WW. B, 500 J500\ \mathrm{J}, sends all the heat into work — but the gas warms up as it expands at constant pressure. D, 143 J143\ \mathrm{J}, uses the diatomic fraction 27\dfrac{2}{7}.

Q5Numerical answer

Many processes follow pVx=constantpV^{x} = \text{constant} for some number xx — a polytropic process. x=0x = 0 is constant pressure, x=1x = 1 is isothermal, x=γx = \gamma is adiabatic. Integrating p dVp\,dV gives the work for any x≠1x \neq 1:

W=p1V1−p2V2x−1=nR(T1−T2)x−1W = \dfrac{p_{1}V_{1} - p_{2}V_{2}}{x - 1} = \dfrac{nR(T_{1} - T_{2})}{x - 1}

(With x=γx = \gamma this is the adiabatic formula you already know.)

One mole of an ideal gas is heated so that its pressure stays proportional to its volume, p=kVp = kV — that is, pV−1pV^{-1} constant, x=−1x = -1. Its temperature rises from 300 K300\ \mathrm{K} to 400 K400\ \mathrm{K}. How much work does it do, in joules? Take R=8.3 J mol−1 K−1R = 8.3\ \mathrm{J\,mol^{-1}\,K^{-1}}.

Show answer and solution

Answer: 415 J

W=nR(T1−T2)x−1=8.3×(300−400)−1−1=−830−2=415 JW = \dfrac{nR(T_{1} - T_{2})}{x - 1} = \dfrac{8.3 \times (300 - 400)}{-1 - 1} = \dfrac{-830}{-2} = 415\ \mathrm{J}.

Check by area: p=kVp = kV is a straight line through the origin, and the area under it is k(V22−V12)2=p2V2−p1V12=R ΔT2\dfrac{k(V_{2}^{2} - V_{1}^{2})}{2} = \dfrac{p_{2}V_{2} - p_{1}V_{1}}{2} = \dfrac{R\,\Delta T}{2}.

The trap is reading "pp proportional to VV" as x=+1x = +1: written as pVxpV^{x} constant, p=kVp = kV is pV−1=kpV^{-1} = k, so x=−1x = -1 (and x=+1x = +1 would divide by zero). Another is nR ΔT=830 JnR\,\Delta T = 830\ \mathrm{J}, the constant-pressure answer, twice too big.

Q6One correct option

Take logs of pVx=constantpV^{x} = \text{constant}: log⁡p=−xlog⁡V+constant\log p = -x\log V + \text{constant}. So on a graph of log⁡p\log p against log⁡V\log V, every polytropic process is a straight line, and its slope is −x-x. Reading the slope gives xx, and xx gives the heat capacity C=CV+R1−xC = C_{V} + \dfrac{R}{1 - x}.

On a graph of log⁡p\log p against log⁡V\log V, a process is a straight line of slope −γ-\gamma. Which process is it?

  1. Aisothermal
  2. Bisobaric
  3. Cadiabatic
  4. Disochoric
Show answer and solution

Answer: Option C

Slope −γ-\gamma means x=γx = \gamma: pVγpV^{\gamma} is constant, the adiabatic, with C=0C = 0.

The trap is A, isothermal, which is x=1x = 1 and slope −1-1. B, isobaric, is x=0x = 0, a horizontal line. D, isochoric, keeps log⁡V\log V fixed — a vertical line, with no finite slope at all.