Thermodynamics in NEET Physics is largely about applying one core relationship — the first law — correctly across different processes. Most mistakes come from mixing up sign conventions or forgetting which quantity is held constant in a given process, not from not knowing the formulas at all.
NEET weightage: High · NCERT Physics Class 11, Part 2, Chapter 12
What you’ll learn
Thermodynamic state variables, and the difference between state and path functions
The zeroth and first laws of thermodynamics
Isothermal, adiabatic, isobaric and isochoric processes, and what stays constant in each
Specific heat capacities Cp and Cv, and why Cp > Cv for a gas
Carnot's engine and thermodynamic efficiency
Key concepts
First law of thermodynamics
ΔQ = ΔU + ΔW, where ΔQ is heat supplied to the system, ΔU is the change in internal energy, and ΔW is work done BY the system. It is essentially a statement of energy conservation applied to thermal systems: heat added either raises internal energy or does work, or both.
Isothermal process
Temperature stays constant (ΔT = 0), so for an ideal gas ΔU = 0 and all heat supplied goes into work done: ΔQ = ΔW. Requires the process to happen slowly enough, or with a perfectly conducting boundary, for temperature to stay uniform.
Adiabatic process
No heat is exchanged with the surroundings (ΔQ = 0), so ΔU = −ΔW. Any work done by the gas comes entirely at the expense of its internal energy (and hence its temperature falls during adiabatic expansion).
Isobaric and isochoric processes
Isobaric: pressure is constant; work done W = PΔV. Isochoric (constant volume): ΔV = 0, so no work is done (W = 0) and all supplied heat changes internal energy: ΔQ = ΔU.
Specific heats Cp and Cv
Cv is the specific heat at constant volume, Cp at constant pressure. For an ideal gas, Cp − Cv = R (Mayer's relation) — Cp is larger because, at constant pressure, some of the supplied heat also does expansion work rather than only raising temperature.
Carnot engine and efficiency
A Carnot engine is an idealised, reversible heat engine operating between two temperatures. Its efficiency η = 1 − T₂/T₁ (temperatures in Kelvin) is the maximum possible efficiency for any engine operating between those two temperatures — no real engine can exceed it.
Key formulas
First law of thermodynamics
ΔQ = ΔU + ΔW
Isothermal process
ΔU = 0, so ΔQ = ΔW
Adiabatic process
ΔQ = 0, so ΔU = −ΔW
Isochoric (constant volume)
W = 0, so ΔQ = ΔU
Isobaric work done
W = PΔV
Mayer's relation
Cp − Cv = R
Carnot engine efficiency
η = 1 − T₂ / T₁
Common mistakes to avoid
Using ΔW = W done ON the gas instead of BY the gas without adjusting the sign — check your textbook's sign convention before substituting into ΔQ = ΔU + ΔW.
Assuming ΔU = 0 in an adiabatic process — that's true for isothermal, not adiabatic. In an adiabatic process it's ΔQ that is zero.
Forgetting that Carnot efficiency requires temperatures in Kelvin, not Celsius.
Treating Cp and Cv as constants that don't depend on whether the gas is monatomic or diatomic — their values (and hence Cp − Cv, though that stays R) differ by gas type through the degrees of freedom.
Assuming heat added always raises temperature — during isothermal expansion, heat added does work instead, so temperature doesn't change at all.
Worked examples
An ideal gas absorbs 500 J of heat and does 200 J of work while expanding. What is the change in its internal energy?
Using ΔQ = ΔU + ΔW: 500 = ΔU + 200, so ΔU = 300 J. The internal energy increases by 300 J — only part of the absorbed heat went into external work; the rest raised the gas's internal energy.
A gas undergoes an adiabatic expansion and does 150 J of work on its surroundings. What happens to its internal energy, and by how much?
Adiabatic means ΔQ = 0, so from the first law, ΔU = −ΔW = −150 J. The internal energy decreases by 150 J, which is why gas temperature drops during adiabatic expansion (e.g. in a rapidly expanding gas cylinder).
Quick revision
First law: ΔQ = ΔU + ΔW — memorise it once, then just track which term is zero for each process.
Mayer's relation: Cp − Cv = R, and Cp > Cv always for an ideal gas.
Carnot efficiency η = 1 − T₂/T₁, with temperatures strictly in Kelvin — this is the theoretical maximum, real engines are always less efficient.
Practise yourself
A gas is compressed isothermally, and 300 J of work is done on the gas. How much heat is released by the gas?
Show answer and reasoning
300 J. For an isothermal process ΔU = 0, so ΔQ = ΔW. Work done ON the gas is −300 J of work done BY the gas, so ΔQ = −300 J, meaning the gas releases 300 J of heat to keep its temperature constant.
In an isochoric process, a gas absorbs 400 J of heat. What is the work done by the gas, and what is the change in internal energy?
Show answer and reasoning
Work done W = 0, because volume doesn't change (no PΔV term). By the first law, ΔQ = ΔU + ΔW = ΔU + 0, so ΔU = 400 J — all the absorbed heat goes into increasing internal energy.
A Carnot engine operates between a source at 500 K and a sink at 300 K. What is its efficiency?
Show answer and reasoning
η = 1 − T₂/T₁ = 1 − 300/500 = 1 − 0.6 = 0.4, i.e. 40%. This is the maximum theoretical efficiency for any engine operating between these two temperatures.
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Related NEET Physics concepts
Kinetic Theory of Gases — the molecular picture behind pressure, temperature and internal energy used throughout this chapter
Properties of Matter (thermal properties) — heat transfer, specific heat capacity and calorimetry that this chapter builds on
Chemistry's Thermodynamics chapter — the same first-law framework applied to chemical reactions (enthalpy, entropy, Gibbs energy)
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