Class 11 · Notes

Thermodynamics— Notes, Formulas & Revision

Complete revision notes and formulas for Thermodynamics (Class 11). Curated for JEE, NEET, AP Physics, SAT, and CUET. Tap any topic to open the live simulation and full PYQ set.

Isothermal Process

PV = const — see hyperbola on PV plot.

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Isothermal process: temperature stays CONSTANT throughout (ΔT = 0).

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For an ideal gas: ΔU = 0 (U depends only on T).

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First law: Q = W. All heat in becomes work out (or vice versa).

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On a PV diagram: HYPERBOLA (PV = constant, Boyle's law).

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Work done by gas: W = nRT·ln(V_f/V_i) = nRT·ln(P_i/P_f).

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Slow expansion in contact with thermal reservoir at constant T ⇒ approximately isothermal.

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Slope on PV diagram: less steep than adiabatic (because P drops less for same V increase).

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Used in: refrigeration cycles, theoretical engine analysis (Carnot cycle).

Equation of state

Boyle's law at constant T.

Work done by gas (expansion)

Logarithmic — moderate work compared to other processes.

Heat absorbed

Equal to work since ΔU = 0.

Internal energy change

Isothermal + ideal gas ⇒ T unchanged ⇒ U unchanged.

Isothermal ⇒ ΔT = 0, ΔU = 0 (ideal gas).

All heat absorbed becomes work output (or work in becomes heat out for compression).

PV = const ⇒ hyperbolic curve on PV diagram.

Slow expansion in contact with thermostat — heat flows in continuously to maintain T.

Isothermal work is LESS than adiabatic work for same V change (slope shallower).

Real isothermal processes are SLOW — fast processes are usually adiabatic.

Adiabatic Process

PV^γ = const — steeper than isotherm.

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Adiabatic process: NO heat exchange with surroundings (Q = 0).

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Achieved by: thermal insulation OR fast process (no time for heat to flow).

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First law: ΔU = −W. If gas expands (W > 0), T DROPS. Compression heats it up.

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For ideal gas: PV^γ = constant, where γ = C_p/C_v.

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Equivalently: TV^(γ−1) = const, or T·P^((1−γ)/γ) = const.

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Adiabatic curve on PV diagram is STEEPER than isotherm (P drops faster for same V increase).

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Examples: rapid compression in a diesel engine (no time for heat loss), atmospheric air parcels rising.

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Adiabatic expansion is how gas in clouds cools and condenses (rising air, lower P, lower T).

Adiabatic condition

No heat exchange.

PV relation

γ = C_p/C_v (1.67 for monatomic, 1.4 for diatomic).

TV relation

Useful for T-V problems.

Work done by gas (adiabatic)

Direct formula for adiabatic work.

ΔU for adiabatic

Q = 0 in first law.

Adiabatic = no heat flow. Either insulated or too fast for heat to flow.

Adiabatic expansion: gas COOLS (energy goes to work).

Adiabatic compression: gas HEATS UP (work done on gas becomes internal energy).

PV^γ vs PV: adiabatic curve drops steeper than isothermal (γ > 1).

Diesel engine: adiabatic compression heats air to ignition temperature.

Atmosphere: parcels rising cool adiabatically (~9.8°C per km dry adiabatic lapse rate).

Isochoric Process

V = const, W = 0, Q = ΔU.

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Isochoric (or isovolumetric) process: volume stays CONSTANT (ΔV = 0).

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No work done: W = P·ΔV = 0.

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First law: Q = ΔU. All heat goes into internal energy.

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Heat absorbed: Q = nC_v·ΔT.

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On PV diagram: VERTICAL line.

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Pressure-temperature link: P/T = constant (Gay-Lussac's law).

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Examples: heating gas in a sealed rigid container, pressure cooker partially.

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Used in Otto cycle (gasoline engine) — constant-volume heat addition (idealized).

Equation

Gay-Lussac's law.

Work done

ΔV = 0 ⇒ no work.

Heat absorbed

Equal to ΔU.

First law (isochoric)

All heat goes to internal energy.

Isochoric ⇒ ΔV = 0 ⇒ W = 0 ⇒ Q = ΔU.

Most direct conversion of heat to internal energy.

On PV diagram: VERTICAL line. No area swept ⇒ no work.

Doubling absolute T at constant V doubles pressure (Gay-Lussac).

Sealed rigid containers: heating them is purely isochoric.

Heat exchange ↔ internal energy directly — no work distraction.

Isobaric Process

P = const, W = PΔV.

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Isobaric process: pressure stays CONSTANT (ΔP = 0).

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On PV diagram: HORIZONTAL line.

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Work done by gas: W = P·ΔV — simple area calculation.

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Heat absorbed: Q = nC_p·ΔT, where C_p = (f/2 + 1)R = molar specific heat at constant P.

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Change in internal energy: ΔU = nC_v·ΔT (always, for ideal gas).

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Volume and temperature linked: V/T = constant (Charles's law).

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Examples: water boiling in an open pot (P_atm constant), gas expansion against atmospheric pressure.

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C_p > C_v because some heat goes into expansion work (Mayer's relation: C_p − C_v = R).

Equation (Charles's law)

Volume proportional to absolute T.

Work done by gas

Pressure times volume change.

Heat absorbed

C_p for constant pressure.

Internal energy change

Always — depends only on T for ideal gas.

C_p vs C_v

Mayer's relation; extra R goes to expansion work.

Isobaric ⇒ ΔP = 0 ⇒ work = PΔV.

On PV diagram: HORIZONTAL line. Area = work.

Q is split between ΔU and W: Q = ΔU + W.

Heating gas at constant P: gas expands → does work → needs more heat for same ΔT (hence C_p > C_v).

Charles's law: V/T = const at constant P.

Cooking in open pot: water at 100°C, atmospheric pressure ⇒ isobaric until water boils away.

First Law of Thermodynamics

ΔU = Q − W — heat in, work out.

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First law of thermodynamics: ΔU = Q − W. Energy conservation applied to a thermodynamic system.

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Q = heat ADDED to the system (positive when heat enters).

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W = work done BY the system on surroundings (positive when gas expands).

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ΔU = change in internal energy.

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Alternative sign convention: ΔU = Q + W where W = work done ON the system. Use one convention consistently.

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For an ideal gas: ΔU = nC_v·ΔT, regardless of process.

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Different processes redistribute Q and W differently — but ΔU = nC_v·ΔT always (for ideal gas).

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Cannot create or destroy energy — only transform between heat, work, and internal energy.

First law

Q in (positive), W out (positive). ΔU = change in internal energy.

Sign convention

Be consistent throughout problem.

Differential form

For infinitesimal changes.

Ideal gas (any process)

Always — U depends only on T for ideal gas.

Δ U = Q − W (or ΔU = Q + W_on_system; sign convention varies).

Free expansion of ideal gas: Q = 0, W = 0 (no resistance), so ΔU = 0 ⇒ T unchanged.

Adiabatic: Q = 0 ⇒ ΔU = −W. If gas expands (W > 0), T drops.

Isothermal (ideal gas): ΔU = 0 ⇒ Q = W. All heat in becomes work out.

Energy conservation: every joule of heat is accounted for as work or internal-energy change.

1st law is universal — applies to engines, refrigerators, chemical reactions, biological systems.

Work in Gas Expansion

W = ∫P dV — area under PV curve, 3 paths.

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Work done by gas in a process: W = ∫P·dV. Always equals the AREA UNDER the curve on a PV diagram.

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Sign convention: V increases (expansion) ⇒ W > 0 (gas does work). V decreases (compression) ⇒ W < 0 (work done on gas).

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Different processes give different work for same initial-final V — work is a PATH FUNCTION.

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Isobaric: W = PΔV (rectangle area).

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Isothermal: W = nRT·ln(V_f/V_i) (under hyperbola).

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Adiabatic: W = (P_iV_i − P_fV_f)/(γ−1).

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Isochoric: W = 0 (ΔV = 0).

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Cycle: W_net = enclosed area.

General work

Area under PV curve.

Isobaric

Constant pressure.

Isothermal (ideal gas)

Logarithmic.

Adiabatic (ideal gas)

γ = C_p/C_v.

Isochoric

No volume change ⇒ no work.

Work is a PATH FUNCTION — depends on HOW the process proceeds, not just endpoints.

Different processes between same initial and final states give different W values.

Area under PV curve = work. Positive for expansion, negative for compression.

Isochoric: W = 0 (vertical line — no horizontal sweep).

Isobaric: W = PΔV (rectangle).

Cycles: net W = enclosed area; clockwise positive, counter-clockwise negative.

Heat Engine Cycle

Rectangular cycle on PV — η = W_net / Q_in.

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Heat engine: device that converts HEAT into WORK over a cycle.

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Takes heat Q_h from a hot reservoir, dumps heat Q_c to a cold reservoir, produces work W = Q_h − Q_c.

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Efficiency: η = W/Q_h = 1 − Q_c/Q_h.

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Real engines: gasoline (Otto cycle), diesel (Diesel cycle), gas turbine (Brayton), steam (Rankine).

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Maximum possible efficiency: Carnot's η = 1 − T_c/T_h.

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Heat engines are CYCLIC: return to initial state, ΔU = 0 over cycle, Q_net = W_net.

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On PV diagram: clockwise closed loop. Enclosed area = net work output.

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Kelvin-Planck statement (2nd law): No engine can convert 100% of heat to work in a cycle.

Heat engine efficiency

Fraction of input heat that becomes useful work.

Work output

Conservation of energy over the cycle.

Carnot limit

Upper bound on efficiency for given reservoir temperatures.

Real efficiency factor

Real engines run irreversibly ⇒ less efficient.

Heat engine PRODUCES WORK from heat. Refrigerator does the opposite.

Efficiency is ALWAYS < 100% — Kelvin-Planck statement of 2nd law.

Higher T_h or lower T_c ⇒ better Carnot limit ⇒ potentially better real efficiency.

Power plants: typical ~ 35-45% efficient. Gas turbine combined cycle: up to ~60%.

Gasoline car: ~25-35%. Diesel: ~35-45%.

Real engines waste heat as 'cold reservoir' exhaust — usually atmosphere.

Refrigerator / Heat Pump

COP = Q_c / W — work input pulls heat from cold.

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Refrigerator: device that EXTRACTS heat from a cold reservoir and DUMPS it to a hot reservoir, using work INPUT.

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Reverse of heat engine — runs the cycle counter-clockwise.

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Work IN, heat OUT to atmosphere. Q_h = W + Q_c (energy conservation).

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Coefficient of Performance: COP = Q_c/W = heat extracted per unit work input.

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Carnot refrigerator COP: COP_max = T_c/(T_h − T_c). Can exceed 1.

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Heat pump: same machine but operated for HEATING. COP_heat = Q_h/W = 1 + COP_ref.

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Real refrigerators: COP ~ 2-4 for household, 3-5 for AC. Heat pumps: 3-5 for heating.

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Clausius statement (2nd law): Cannot transfer heat from cold to hot without work input.

Refrigerator energy balance

Hot dumped = work input + cold extracted.

Coefficient of performance (refrigerator)

Higher COP = more efficient cooling per joule.

Carnot COP_ref

Maximum possible.

Heat pump COP

For HEATING applications.

Refrigerator = REVERSED heat engine. Uses work to pump heat 'uphill'.

COP > 1 means more heat moved than work invested — common because work input ALSO becomes heat at the hot side.

Carnot COP is the upper bound: larger when reservoirs are close in T.

Heat pump for heating: gives Q_h = W + Q_c — total heating output exceeds work input, very efficient in mild climates.

Clausius statement: heat flowing from cold to hot REQUIRES work — 2nd law in disguise.

Refrigerator works because of phase changes (refrigerant evaporates, absorbs heat; condenses, releases heat).

Carnot Engine

η = 1 − T_c/T_h — ideal max efficiency.

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Carnot engine: theoretical ideal engine — most efficient possible between two reservoirs at temperatures T_hot and T_cold.

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Cycle: isothermal expansion at T_hot → adiabatic expansion → isothermal compression at T_cold → adiabatic compression.

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Carnot efficiency: η_Carnot = 1 − T_cold/T_hot (temperatures in KELVIN!).

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All reversible engines between same two reservoirs have SAME efficiency = η_Carnot.

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No real engine can exceed Carnot efficiency (2nd law of thermodynamics).

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Engine output = work; engine sucks heat Q_h from hot, dumps Q_c to cold, produces W = Q_h − Q_c.

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Carnot engine is REVERSIBLE — can run backward as a refrigerator with max COP.

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Higher T_hot or lower T_cold ⇒ higher efficiency.

Carnot efficiency

T in Kelvin. Upper bound for any engine.

Heat-temperature ratio (reversible)

Defines absolute T scale.

Work output

Maximum for given Q_h and reservoirs.

Carnot refrigerator COP

Maximum cooling per unit work; can be > 1.

Carnot is THEORETICAL — assumes infinitely slow, reversible processes. Real engines never reach it.

Temperatures MUST be in KELVIN for the formula to work.

η_Carnot = 0 if T_c = T_h (no temperature difference, no engine).

η_Carnot < 1 always — impossible to convert ALL heat to work (Kelvin's statement of 2nd law).

Carnot's theorem: ALL reversible engines between same T have same η. Irreversible engines are LESS efficient.

Real-world: power plants reach 40-50% efficiency vs Carnot limit of ~65% at typical T_h/T_c.

Real vs Ideal Engine

Compare side-by-side — losses in real systems.

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Ideal (Carnot) engine: reversible, infinitely slow, max efficiency.

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Real engines: irreversible, finite speed, lower efficiency.

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Sources of inefficiency: friction, turbulence, heat leakage, fast non-quasi-static processes, incomplete combustion.

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Real engine efficiency = η_real < η_Carnot = 1 − T_c/T_h.

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Carnot's theorem: NO engine can exceed Carnot efficiency; only reversible engines reach it.

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Practical efficiencies: gasoline ~25-35%, diesel ~35-45%, gas turbine ~30-40%, combined cycle ~50-60%.

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Higher T_hot (more efficient) requires advanced materials — engineering trade-off.

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Engine output power = efficiency × heat input rate.

Real efficiency

Measured directly from engine operation.

Carnot bound

Theoretical upper limit.

Reduction factor

Typical for real engines (depends on quality).

Carnot efficiency is THEORETICAL UPPER BOUND.

Real engines lose to friction, finite speeds, heat leaks, non-equilibrium combustion.

η_real / η_Carnot ≈ 0.5-0.8 for well-designed engines.

Increasing T_h is key to higher η — modern gas turbines push T_h to ~1500°C using ceramic blades and cooling.

Diesel engines achieve higher η than gasoline because higher T_h (compression-ignition vs spark).

Carnot bound is INDEPENDENT of working fluid — only T_h and T_c matter.

PV Diagram Explorer

Switch between 4 processes on a single plot.

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PV diagram: pressure (P) on y-axis vs volume (V) on x-axis. Represents thermodynamic processes graphically.

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Each point: a specific state with P, V, T (and n) defined.

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Each curve: a process. Slope and shape tell what kind of process.

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Isothermal (PV = const): hyperbola.

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Adiabatic (PV^γ = const): steeper than isothermal.

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Isobaric: horizontal line.

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Isochoric: vertical line.

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Area under curve = work done by gas: W = ∫P·dV.

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Cyclic process: closed loop on PV. Enclosed area = net work over cycle.

Work done by gas (any process)

Area under the curve in PV diagram.

Cycle work

Net work in a complete cycle.

Isothermal work

Logarithmic.

Adiabatic work

Useful for gas processes without heat exchange.

Isobaric work

Constant P × ΔV.

PV diagram visualizes thermodynamic processes — read off P, V, T at each point.

Area under curve = W. Sign matters: expansion (V increases) ⇒ positive W; compression ⇒ negative.

Cycles: clockwise = engine (positive W_net), counter-clockwise = refrigerator (negative W_net).

Isotherm < adiabat in slope: for same V change, P drops less in isotherm than adiabat.

ΔU = 0 along isotherm of ideal gas (only T fixed) — useful shortcut.

All four basic processes (isothermal, adiabatic, isobaric, isochoric) have distinct shapes on PV.

T–S Diagram (Carnot)

Carnot rectangle — area = work done.

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TS diagram: temperature (T) vs entropy (S). Useful complement to PV diagram.

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Each point: a thermodynamic state. Each curve: a process.

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Isothermal: HORIZONTAL line (T = const).

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Adiabatic (reversible): VERTICAL line (S = const, isentropic).

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Area under T-S curve = heat absorbed: Q = ∫T·dS.

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Cyclic process: closed loop. Enclosed area = net heat absorbed = net work output (for an engine).

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Carnot cycle on TS: PERFECT RECTANGLE — two isotherms (horizontal) + two adiabats (vertical).

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TS diagram makes 2nd law of thermodynamics visually direct: entropy can only stay constant (reversible) or increase.

Heat absorbed

Area under T-S curve.

Entropy change (reversible)

Definition of entropy.

Adiabatic = isentropic (reversible)

Reversible adiabatic: vertical line on TS.

Carnot cycle area

Carnot rectangle on TS diagram.

T-S diagrams show heat flow visually (area under curve).

Isothermal: horizontal. Reversible adiabatic: vertical.

Cycle on TS: clockwise = engine (Q > 0 net, area encloses heat absorbed).

Carnot cycle is a RECTANGLE on TS — easiest place to compute efficiency.

Real processes are IRREVERSIBLE — S of universe increases (2nd law).

TS diagrams used heavily in steam engine and refrigeration design.

Cyclic Process

ΔU = 0, W = ∮P dV — engine vs refrigerator direction.

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Cyclic process: gas returns to its initial state after a series of processes.

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Net change in any state function over a cycle is ZERO: ΔU_cycle = 0, ΔT_cycle = 0, ΔP_cycle = 0, ΔV_cycle = 0.

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First law for a cycle: Q_net = W_net. Net heat input = net work output.

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On PV diagram: closed curve. Area enclosed = net work done by gas.

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Clockwise cycle on PV: net work > 0 (heat engine).

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Counter-clockwise: net work < 0 (refrigerator/heat pump).

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Examples: Carnot, Otto (gasoline), Diesel, Brayton, Stirling cycles — all engine/refrigerator cycles.

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Efficiency of a heat engine cycle: η = W_net/Q_hot — fraction of input heat converted to useful work.

Net first law over cycle

U is a state function.

Work done = enclosed area

Area inside the closed PV curve.

Efficiency (heat engine)

Fraction of input heat that becomes useful work.

Coefficient of performance (refrigerator)

Heat extracted from cold reservoir per unit work input.

Over a cycle, ΔU = 0 always — state functions are PERIODIC.

Net work = NET heat absorbed (not just total heat in).

PV diagram area: clockwise ⇒ engine, counter-clockwise ⇒ refrigerator.

Real engines run on cycles — gasoline car: Otto cycle, jets: Brayton cycle.

Maximum efficiency for given hot/cold reservoirs: Carnot cycle.

Refrigerator COP can exceed 1 — heat extracted > work input (heat is also dumped from work).

Internal Energy of Ideal Gas

U = (f/2) nRT — depends only on T.

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Internal energy U: total energy of all microscopic motions and interactions inside a system.

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For an ideal gas, U depends ONLY on temperature: U = (f/2)·n·R·T, where f = degrees of freedom.

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Monatomic gas (He, Ar): f = 3, U = (3/2)nRT. Diatomic gas (N₂, O₂): f = 5, U = (5/2)nRT (translation + rotation).

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Polyatomic: more degrees of freedom (translation + rotation + vibration).

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ΔU depends only on initial and final STATES — not on path (state function).

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Real gases also have potential energy of intermolecular forces; U depends on V slightly.

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First law of thermodynamics: ΔU = Q − W. U changes when heat enters or work is done by gas.

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Equipartition theorem: each degree of freedom contributes ½k_BT per molecule (½RT per mole).

Internal energy (ideal gas)

Depends only on T for ideal gas.

Change in internal energy

C_v = molar specific heat at constant volume = (f/2)R.

Equipartition (per molecule)

Each quadratic degree of freedom: ½k_BT.

Monatomic ideal gas

Only translational KE.

Diatomic (room T)

Translation + rotation (vibration frozen out at room T).

U is a STATE FUNCTION — depends only on the state, not on how you got there.

Ideal gas: U = f(T) only. Real gases have small V-dependence due to intermolecular forces.

Heating ideal gas at constant V: all heat goes to ΔU = nC_vΔT. Heating at constant P: some heat is work.

Specific heat C_p > C_v by R (Mayer's relation): heat for V change becomes work.

Equipartition predicts U; quantum effects FREEZE OUT vibrational modes at low T.

Common pitfall: thinking heat = internal energy. NO: heat is energy in transit; U is energy stored.

Thermodynamics on sciphylab (also known as SciPhy, SciPhy Lab, SciPhy Labs). Free physics revision for Class 11, JEE Mains, JEE Advanced, NEET UG, AP Physics 1/2/C, SAT Subject Physics, and CUET-UG.