How to Use This Section

This is the last section of the chapter, and it has exactly one job: to be read the night before the paper, and again in the queue outside the hall.

Nothing new is taught here. Every card below compresses something an earlier section worked through properly, in the same notation and with the same numbers. So if a line here surprises you, that is not a line to memorise — it is a signal to go back and reread the section that owns it.

Six cards, three figures, four reference tables, one decision chart, one mistake checklist, one 60-second list and one fast self-test. Screenshot the heating curve and the blackbody spectrum.

Seven Notation Reminders

This chapter has the worst symbol collisions in the whole year's physics. Hold to these and you can read anybody's formula sheet without stumbling.

  • TT is an absolute temperature in KELVIN. tt or tCt_C is Celsius. Every fourth power, every ratio and every gas-law substitution in this chapter needs kelvin. Only a difference ΔT\Delta T is safe in Celsius, because a rise of 1°C and a rise of 1 K are the same interval.
  • LL with a subscript is latent heat; a bare LL is a LENGTH. So LfL_f for fusion, LvL_v for vaporisation, and a plain LL for the length of a rod or the thickness of a slab.
  • α\alpha is the coefficient of linear expansion and nothing else. β\beta is areal (superficial), γ\gamma is volume. They are also written αL\alpha_L, αA\alpha_A, αV\alpha_V.
  • ss, CC and SS are three different quantities. ss is the specific heat capacity per kilogram in J/(kg K); CC is the molar specific heat per mole in J/(mol K); SS is the heat capacity of a whole named body in J/K, so S=msS = ms.
  • KK is thermal conductivity in W/(m K); lowercase kk is the cooling constant in Newton's law, in s1^{-1}. Conductivity is also written kk or λ\lambda, so check which one a formula sheet means before you trust it.
  • In radiation, absorptive power is aa, never α\alpha, and emissivity is ee. Absorptivity is also written α\alpha or aλa_\lambda; here α\alpha belongs to expansion. σ\sigma is always the Stefan-Boltzmann constant and bb is always Wien's constant.
  • RR does double duty. In the conduction cards RR is thermal resistance in K/W. In the one place molar specific heats appear, RR is the gas constant, 8.31 J/(mol K). They never share an equation, but say which one you mean.

The constants sheet

Every number on these cards uses one of these. Never mix g=9.8g = 9.8 and g=10g = 10 inside one problem, and never mix 273273 with 273.15273.15 — pick one, write it at the top of your working, and use it everywhere.

Constant Value
Specific heat capacity of water 4186 J/(kg K)
Specific heat capacity of ice 2100 J/(kg K)
Specific heat capacity of steam 2010 J/(kg K)
Latent heat of fusion of ice LfL_f 3.33×1053.33 \times 10^{5} J/kg
Latent heat of vaporisation of water LvL_v 22.6×10522.6 \times 10^{5} J/kg
Stefan-Boltzmann constant σ\sigma 5.67×1085.67 \times 10^{-8} W/(m2^2 K4^4)
Wien's displacement constant bb 2.9×1032.9 \times 10^{-3} m K
Gas constant RR 8.31 J/(mol K), so 3R253R \approx 25 J/(mol K)
Triple point of water 273.16 K, the defining fixed point
Ice point 273.15 K, rounded to 273 K in most radiation problems
Mechanical equivalent of heat 1 cal =4.186= 4.186 J

The comparison table — learn the pattern, not the digits

One table for all three material properties, so you can see at a glance that they are unrelated to one another.

Substance ss in J/(kg K) KK in W/(m K) α\alpha in K1^{-1}
Silver 236.1 406 1.9×1051.9 \times 10^{-5}
Copper 386.4 385 1.7×1051.7 \times 10^{-5}
Aluminium 900 205 2.3×1052.3 \times 10^{-5}
Brass 109 1.8×1051.8 \times 10^{-5}
Iron 450 79 1.2×1051.2 \times 10^{-5}
Steel 450 50.2 1.2×1051.2 \times 10^{-5}
Lead 127.7 34.7 2.9×1052.9 \times 10^{-5}
Ice 2100 1.6
Glass (ordinary) 840 0.8 0.9×1050.9 \times 10^{-5}
Brick 0.72
Water 4186 0.6 γ=20.7×105\gamma = 20.7 \times 10^{-5}
Body fat 0.20
Wood 0.12
Thermacole (EPS) 0.033
Air about 1005 0.024 γ=1T\gamma = \frac{1}{T}
Invar 0.12×1050.12 \times 10^{-5}

Typical values at ordinary room temperature. Water and air are liquids and gases, so the volume coefficient γ\gamma is quoted for them instead of a linear α\alpha; a dash means the chapter never needed that number.

Six readings off it, every one of which has been an examination question:

  1. Thermal conductivity spans nearly four orders of magnitude — silver at 406 down to air at 0.024, a factor of about 17000. Nothing else in the table varies remotely that much.
  2. Specific heat capacity varies by only a factor of about 30 across the whole table, and water sits at the top of it. That one number, 4186 J/(kg K), is behind the car radiator, the sea breeze and the moderate coastal climate.
  3. Expansion coefficients are all around 10510^{-5} K1^{-1} for metalslead is the largest at 2.9×1052.9 \times 10^{-5} and iron and steel the smallest at 1.2×1051.2 \times 10^{-5}, a factor of about two and a half across every ordinary metal in the list. Invar, engineered to sit still, is the deliberate exception. Liquids are about ten times larger than a metal and a gas is about a hundred times larger again.
  4. The three properties are independent of one another. Lead conducts about forty times better than glass and expands more than three times as much, yet stores only about a seventh as much heat per kilogram. Knowing one tells you nothing about the others.
  5. Air is the best insulator in the table, which is why fur, feathers, wool, thermacole and double glazing all work by trapping still air rather than by being clever materials themselves.
  6. Invar barely moves at all, which is exactly what it was invented for — pendulum rods, measuring tapes and anything that must not change length with the weather.

Five topics on these cards that the body text does not carry

Areal expansion and the α:β:γ=1:2:3\alpha : \beta : \gamma = 1 : 2 : 3 ratio, bimetallic strips, thermal resistance in series and in parallel, Kirchhoff's law and Prevost's theory, and the greenhouse effect and solar constant all sit outside the rationalised syllabus body text. Boards, JEE Main, JEE Advanced and NEET ask them every year, so they are on these cards in full.

Card 1 — Temperature, the Scales, and Thermal Expansion

Heat and temperature, kept apart

Key Point: Temperature measures the degree of hotness and decides the direction heat flows. Heat is energy in transit, flowing only because of a temperature difference. A body does not contain heat — it contains internal energy, and heat is what crosses the boundary.

A bucket of warm water holds far more internal energy than a red-hot spark, yet the spark is at the higher temperature and heat flows from spark to water.

Key Point — the zeroth law: if AA is in thermal equilibrium with CC, and BB is in thermal equilibrium with CC, then AA and BB are in thermal equilibrium with each other. This is what makes temperature a measurable quantity and a thermometer possible at all.

A diathermic wall lets equilibrium happen; an adiabatic wall prevents it. Units: 11 cal =4.186= 4.186 J.

The scales

Key Point — the conversion, from the two fixed points:  tF32180=tC100that istF=95tC+32 \boxed{\ \frac{t_F - 32}{180} = \frac{t_C}{100} \qquad\text{that is}\qquad t_F = \frac{9}{5}t_C + 32\ } and the absolute scale,  T=tC+273.15 \boxed{\ T = t_C + 273.15\ } A degree Celsius and a kelvin are the same size, so a rise of 50°50°C is a rise of 50 K. Only the zero differs.

  • The two scales read alike at 40°-40°: 40°-40°C =40°= -40°F. It is the one temperature where they agree.
  • Normal body temperature 37°37°C is 95(37)+32=98.6°\frac{9}{5}(37) + 32 = 98.6°F, which is where clinical thermometers get that number.
  • A temperature interval converts differently from a temperature: a rise of 50°50°C is a rise of 90°90°F, because only the 95\frac{9}{5} applies, not the 32.

Key Point — the absolute scale: the triple point of water, 273.16 K, is the single defining fixed point, chosen because a triple point occurs at exactly one pressure and one temperature and therefore cannot drift. A constant-volume gas thermometer reads T=273.16×PPtrT = 273.16 \times \frac{P}{P_{\text{tr}}} and its readings become independent of which gas is used as the pressure is reduced. Absolute zero, 0 K =273.15°= -273.15°C, is where the pressure of an ideal gas would extrapolate to zero. It can be approached, never reached.

The ideal-gas equation PV=μRTPV = \mu R T needs TT in kelvin, always.

Key Point — THE KELVIN RULE, the most valuable line in this section: Wherever temperature appears as a ratio, a product or a powerT2T1\frac{T_2}{T_1}, T4T^4, PV=μRTPV = \mu RT, λmT=b\lambda_m T = b — it must be in kelvin. Wherever only a difference ΔT\Delta T appears — ΔL=αLΔT\Delta L = \alpha L \Delta T, Q=msΔTQ = ms\Delta T, H=KAΔTLH = \frac{KA\Delta T}{L}, dTdt=k(TTs)-\frac{dT}{dt} = k(T - T_s) — Celsius and kelvin give the same number.

Here is that rule doing its job. A body goes from 27°27°C to 327°327°C. The rise is 300°300°C, and also 300 K. The ratio of absolute temperatures is 600300=2\frac{600}{300} = 2, not 32727=12.1\frac{327}{27} = 12.1. One of those is a factor of six wrong.

Thermal expansion

Key Point — the three coefficients:  ΔL=αLΔTΔA=βAΔTΔV=γVΔT \boxed{\ \Delta L = \alpha L\,\Delta T \qquad \Delta A = \beta A\,\Delta T \qquad \Delta V = \gamma V\,\Delta T\ } and for an isotropic solid  β=2α,γ=3α,α:β:γ=1:2:3 \boxed{\ \beta = 2\alpha, \qquad \gamma = 3\alpha, \qquad \alpha : \beta : \gamma = 1 : 2 : 3\ } All three coefficients have the unit K1^{-1}.

Where the 2 and the 3 come from, and what they cost. Every length is multiplied by (1+αΔT)(1 + \alpha\Delta T), so an area is multiplied by (1+αΔT)2(1 + \alpha\Delta T)^2 and a volume by (1+αΔT)3(1 + \alpha\Delta T)^3. Writing x=αΔTx = \alpha\Delta T, (1+x)2=1+2x+x2and(1+x)3=1+3x+3x2+x3(1+x)^2 = 1 + 2x + x^2 \qquad\text{and}\qquad (1+x)^3 = 1 + 3x + 3x^2 + x^3 Keeping only the linear term gives β=2α\beta = 2\alpha and γ=3α\gamma = 3\alpha. These are first-order approximations, not identities. For aluminium heated through 100 K, x=2.3×103x = 2.3 \times 10^{-3}, and the neglected terms are 0.115% of the areal answer and 0.23% of the volume answer. Genuinely negligible — but earned, not assumed.

Result Formula The thing that catches people
New length L=L(1+αΔT)L^{\,\prime} = L(1 + \alpha\,\Delta T) the factor multiplies every length in the body
A hole in a plate ΔAhole=2αAholeΔT\Delta A_{\text{hole}} = 2\alpha A_{\text{hole}}\Delta T the hole gets BIGGER, exactly as if filled with the metal
Apparent expansion of a liquid γapparent=γrealγvessel\gamma_{\text{apparent}} = \gamma_{\text{real}} - \gamma_{\text{vessel}} the vessel expanded too
Density ρρ(1γΔT)\rho^{\,\prime} \approx \rho(1 - \gamma\,\Delta T) density falls on heating
An ideal gas γgas=1T\gamma_{\text{gas}} = \frac{1}{T} TT in kelvin; about 1273\frac{1}{273} K1^{-1} near 0°C
Constrained rod thermal stress =YαΔT= Y\alpha\,\Delta T independent of the length; enormous for steel

Key Point — the hole. Heat a plate with a hole in it and the hole expands. Imagine the disc of metal that was drilled out: it would grow by 2αAΔT2\alpha A \Delta T, and it must still fit, so the hole grows by exactly the same amount. A ring, a washer, a bearing and the bore of a pipe all get larger on heating.

Typical sizes, three decades apart: metals about 10510^{-5} K1^{-1}, liquids about 10410^{-4} K1^{-1}, a gas about 3.7×1033.7 \times 10^{-3} K1^{-1} at room temperature.

Where it shows up: expansion gaps in rails and bridges, the loop in a steam pipe, shrink-fitting a rim onto a wheel, the systematic error of a steel tape used at the wrong temperature, and the bimetallic strip, which always bends towards the metal that expands less — brass on iron curls towards the iron on heating.

Key Point — the anomaly of water: between 0°C and 4°C water contracts when heated, so it is densest at 4°C. That is why a lake freezes from the top down, why the water at the bottom stays at 4°C, and why fish survive the winter.

[Board Important] "Why does a hole in a metal plate get bigger when the plate is heated?" and "Why does a lake freeze from the top downwards?" are both standard three-markers. Neither needs a number — they need the reasoning above, written out.

Card 2 — Heat Capacity, Calorimetry and Latent Heat

The three capacities, kept apart

Quantity Symbol Definition SI unit Belongs to
Heat capacity SS ΔQΔT\dfrac{\Delta Q}{\Delta T} J/K the body
Specific heat capacity ss 1mΔQΔT\dfrac{1}{m}\dfrac{\Delta Q}{\Delta T} J/(kg K) the substance
Molar specific heat capacity CC 1μΔQΔT\dfrac{1}{\mu}\dfrac{\Delta Q}{\Delta T} J/(mol K) the substance

They are linked by S=msS = ms and C=sMC = sM, with MM the molar mass in kg/mol.

Key Point — the working equation that runs through the rest of the chapter:  ΔQ=msΔT \boxed{\ \Delta Q = m\,s\,\Delta T\ }

Two experimental facts worth carrying:

  • Dulong-Petit. Most simple solids have C3R25C \approx 3R \approx 25 J/(mol K). Check it: copper, 386.4×0.0635=24.5386.4 \times 0.0635 = 24.5; aluminium, 900×0.0270=24.3900 \times 0.0270 = 24.3; lead, 127.7×0.2072=26.5127.7 \times 0.2072 = 26.5. Carbon is the famous exception at about 6.1 J/(mol K).
  • Mayer's relation. For an ideal gas CpCv=RC_p - C_v = R, so Cp>CvC_p > C_v always — at constant pressure the gas also does work as it expands, and that work has to be paid for. "The specific heat of a gas" is meaningless until you say which process.

Water's 4186 J/(kg K) is exceptionally large, and a great deal follows from that single number: water as the coolant in engines and reactors, the sea moderating a coastal climate, the land and sea breeze reversing between day and night, and a hot-water bottle beating a hot brick.

Calorimetry

Key Point — the principle: in a thermally isolated system, heat lost by the hot bodies equals heat gained by the cold ones:  ΔQ=0that isQlost=Qgained \boxed{\ \sum \Delta Q = 0 \qquad\text{that is}\qquad Q_{\text{lost}} = Q_{\text{gained}}\ } It is nothing but conservation of energy. The marks are in the bookkeeping.

Key Point — water equivalent:  W=mcscsw \boxed{\ W = \frac{m_c s_c}{s_w}\ } the mass of water that would absorb the same heat as the calorimeter. Its SI unit is the kilogram. Once you have it, fold the vessel into the arithmetic as though it were that much extra water — a calorimeter of water equivalent 30 g holding 170 g of water behaves in every heat balance exactly like 200 g of water.

The five-step recipe, in order:

  1. List every body: the hot one, the cold one, the calorimeter, the stirrer, the thermometer if its heat capacity is given.
  2. Decide which are losing heat and which are gaining.
  3. Write one equation, ΔQ=0\sum \Delta Q = 0, with a msΔTms\Delta T term for every body and an mLfmL_f or mLvmL_v term for every phase change.
  4. Solve for the single unknown.
  5. Check that the answer lies between the two starting temperatures. If it does not, a sign is wrong.

Key Point — the trap that catches everyone. If a phase change is possible, compute the heat available and the heat required separately, and compare them before assuming a final temperature. For ice at 0°C dropped into warm water: the heat available is mwsw(tw0)m_w s_w (t_w - 0) and the heat needed to melt all the ice is miceLfm_{\text{ice}} L_f.

  • Available more than needed: all the ice melts and the mixture settles somewhere above 0°C.
  • Available less than needed: the temperature pins at 0°C with only QavailableLf\frac{Q_{\text{available}}}{L_f} of the ice melted, and ice and water coexist. Never assume the ice all melts. That assumption is the single most expensive habit in this topic.

Latent heat, and the curve

Key Point:  Q=mLf(melting or freezing)Q=mLv(boiling or condensing) \boxed{\ Q = m L_f \quad\text{(melting or freezing)} \qquad Q = m L_v \quad\text{(boiling or condensing)}\ } with Lf=3.33×105L_f = 3.33 \times 10^{5} J/kg and Lv=22.6×105L_v = 22.6 \times 10^{5} J/kg for water, both in J/kg. During a change of state the temperature does not change at all — the energy goes into breaking the bonds that hold the state together, not into raising kinetic energy.

Ice to steam heating curve to scale with both latent heat plateaus labelled

Read the figure and you have the whole topic:

  • Sloping segment \Rightarrow Q=msΔTQ = ms\Delta T, temperature rising, one phase only. Flat segment \Rightarrow Q=mLfQ = mL_f or mLvmL_v, temperature frozen, two phases coexisting.
  • The steeper the slope, the smaller the specific heat capacity. Ice and steam are steeper than water because 2100 and 2010 are smaller than 4186.
  • The vaporisation plateau is 6.8 times as long as the fusion plateau, because LvLf=22.63.33=6.79\frac{L_v}{L_f} = \frac{22.6}{3.33} = 6.79. Melting only loosens the lattice; boiling has to separate the molecules altogether.
  • Taking 1 kg from ice at 20°-20°C to steam at 120°120°C costs 42+333+419+2260+40=309442 + 333 + 419 + 2260 + 40 = 3094 kJ, and 73% of that is the boiling plateau alone.
  • That is why steam at 100°100°C scalds far worse than water at 100°100°C: every gram of steam that condenses on the skin delivers 2260 J/g before it even begins to cool.

Pressure moves both points, in opposite directions. Raising the pressure lowers the melting point of ice — that is regelation, and it is why a loaded wire passes through a block of ice leaving it whole. Raising the pressure raises the boiling point, which is a pressure cooker; lowering it drops the boiling point, which is why rice will not cook properly on a mountain.

Evaporation is a surface process at any temperature, it cools what is left behind, and it is not boiling — boiling happens throughout the bulk at one fixed temperature. Sublimation is solid straight to vapour, as dry ice and camphor do.

[NEET Important] Latent heat is quoted per kilogram, so a mass in grams must be converted before it is multiplied. Half the wrong answers in this topic are a factor of 1000, not a misunderstanding.

Card 3 — Conduction, Convection and Thermal Resistance

The three modes in one line each

Mode What actually moves Needs a medium?
Conduction energy passed particle to particle, no bulk motion yes, solids especially
Convection the fluid itself, carrying energy with it yes, must be a fluid
Radiation electromagnetic waves no

Conduction

Key Point — the conduction law, in the steady state:  H=ΔQΔt=KATCTDL \boxed{\ H = \frac{\Delta Q}{\Delta t} = K A \frac{T_C - T_D}{L}\ } HH is the heat current in watt, KK the thermal conductivity in W/(m K), AA the area perpendicular to the flow and LL the thickness along it. The quantity TCTDL\frac{T_C - T_D}{L} is the temperature gradient, in K/m. Because only a difference appears, °°C and K give the same number here.

In the steady state the temperature at each point has stopped changing, the same HH passes every cross-section, and for a uniform lagged bar the temperature falls linearly along the length.

Metals conduct far better than non-metals because free electrons carry the energy as well as the lattice vibrations — the same electrons that make them electrical conductors.

Thermal resistance — the tool that makes composite problems easy

Key Point:  R=LKAH=ΔTR \boxed{\ R = \frac{L}{KA} \qquad\Longrightarrow\qquad H = \frac{\Delta T}{R}\ } in exact analogy with Ohm's law. The SI unit of thermal resistance is K/W.

Electricity Heat
potential difference VV temperature difference ΔT\Delta T
current II heat current HH, in watt
resistance R=ρLAR = \frac{\rho L}{A} thermal resistance R=LKAR = \frac{L}{KA}
I=VRI = \frac{V}{R} H=ΔTRH = \frac{\Delta T}{R}

Key Point — series and parallel: In SERIES (slabs joined end to end, one behind the other): the same HH passes through both, the temperature drops add, and R=R1+R2with equal thicknessesKeq=2K1K2K1+K2R = R_1 + R_2 \qquad\text{with equal thicknesses}\qquad K_{\text{eq}} = \frac{2K_1K_2}{K_1 + K_2} In PARALLEL (slabs side by side between the same two reservoirs): the same ΔT\Delta T sits across both, the currents add, and 1R=1R1+1R2with equal lengthsKeq=K1A1+K2A2A1+A2\frac{1}{R} = \frac{1}{R_1} + \frac{1}{R_2} \qquad\text{with equal lengths}\qquad K_{\text{eq}} = \frac{K_1A_1 + K_2A_2}{A_1 + A_2}

Three consequences worth memorising:

  • In series, the bigger resistance takes the bigger temperature drop. A thin layer of a poor conductor can dominate an entire wall.
  • In parallel, the better conductor carries the bigger share of the current, in the ratio of the conductances.
  • The junction temperature between two rods in series comes from setting the two currents equal, K1A(T1Tj)L1=K2A(TjT2)L2\frac{K_1A(T_1 - T_j)}{L_1} = \frac{K_2A(T_j - T_2)}{L_2}, and solving for TjT_j. For a copper rod and a steel rod of equal size with free ends at 100°100°C and 0°C, the junction sits at 88.5°88.5°C — right up near the hot end, because copper's resistance is tiny compared with steel's.

Why insulation works. Fur, feathers, wool, thermacole and double glazing all work by trapping still air, whose conductivity is 0.024 W/(m K) — about 16000 times worse than copper. Two thin blankets beat one thick one because of the air layer between them. A metal spoon feels colder than a wooden one at the same temperature because it conducts heat away from your finger far faster; the spoon is not colder, your finger is.

Convection, in one card corner

Convection is bulk transport of the fluid itself. The heated fluid expands, becomes less dense, rises, and cooler fluid sinks to replace it. It is therefore impossible in a solid and impossible in free fall or orbit, where there is no effective gravity to sort the fluid by density.

  • Natural convection is driven by that density difference: a pan of water, a chimney, a room heater at floor level.
  • Forced convection is driven by a pump or fan: a car radiator, a room fan, and the blood in your circulatory system carrying heat from the core to the skin.
  • The sea breeze by day and the land breeze by night follow directly from water's large specific heat capacity: the land heats and cools quickly, the sea barely changes. The monsoon is the same mechanism on a continental scale.
  • A heater goes at floor level and an air conditioner high on a wall, because each needs to sit where its treated air will be carried through the room by the circulation it sets up.

[JEE Tip] Almost every conduction question at this level is a resistance network in disguise. Convert each slab or rod to R=LKAR = \frac{L}{KA} first, combine them as series and parallel, then use H=ΔTRH = \frac{\Delta T}{R} once at the end. It replaces three lines of algebra with one.

Card 4 — Radiation, and Newton's Law of Cooling

The vocabulary, settled first

Thermal radiation is electromagnetic waves, travelling at 3×1083 \times 10^{8} m/s, needing no medium at all. That is what gets the Sun's energy across empty space.

Key Point — Prevost's theory of heat exchange: every body emits and absorbs radiation at all times, at every temperature above absolute zero. A body in equilibrium with its surroundings is not idle — it is emitting and absorbing at equal rates.

  • Absorptive power aa is the fraction of incident radiation absorbed. It is a pure number between 0 and 1.
  • Emissivity ee is the ratio of a body's emissive power to that of a blackbody at the same temperature. Also a pure number between 0 and 1.
  • A blackbody absorbs everything falling on it, so a=1a = 1 and e=1e = 1. A small hole in a large cavity is the practical realisation: a ray that enters is reflected so many times inside that it has essentially no chance of finding its way out again.

Wien's displacement law

Key Point:  λmT=b=2.9×103 m K \boxed{\ \lambda_m T = b = 2.9 \times 10^{-3}\ \text{m K}\ } λm\lambda_m is the wavelength at which the emission is most intense, and TT is in kelvin. Hotter means a shorter peak wavelength.

Blackbody curves at three temperatures with Wien peaks marked and Stefan area bars

This is why a heated body glows dull red, then orange, then white as it gets hotter — the peak marches in from the infrared towards the blue. It is also how a star's surface temperature is read off its colour: the Sun peaks near 500 nm, giving about 5800 K.

The Stefan-Boltzmann law

Key Point:  H=σAeT4and, exchanging with surroundings at Ts,Hnet=σAe(T4Ts4) \boxed{\ H = \sigma A e\, T^4 \qquad\text{and, exchanging with surroundings at } T_s, \qquad H_{\text{net}} = \sigma A e\left(T^4 - T_s^4\right)\ } with σ=5.67×108\sigma = 5.67 \times 10^{-8} W/(m2^2 K4^4). Both temperatures in kelvin, always.

The fourth power is unforgiving and it is what questions are built on. Doubling the absolute temperature multiplies the radiated power by 24=162^4 = 16, so a body at 6000 K radiates sixteen times as much per square metre as one at 3000 K, not twice as much. Panel (b) of the figure is that statement drawn.

The substitution, done properly. A body at 27°27°C in surroundings at 0°C: put T=300T = 300 K and Ts=273T_s = 273 K, giving σ(30042734)=144\sigma(300^4 - 273^4) = 144 W/m2^2 per unit emissivity. Putting the Celsius numbers in instead gives σ(27404)=0.03\sigma(27^4 - 0^4) = 0.03 W/m2^2 — nearly five thousand times too small, and instantly recognisable as wrong.

Kirchhoff's law

Key Point: at a given temperature and a given wavelength, the ratio of the emissive power to the absorptive power is the same for every body, and equals the emissive power of a blackbody. In short: a good absorber is a good emitter.

Its evidence, all examinable:

  • A blackened vessel of hot water cools faster than an identical polished one, and a blackened one also warms faster in the sun.
  • Wearing white in summer helps because a poor absorber of sunlight is what you want; the same cloth is a poor emitter too, which is why the choice matters much less at night.
  • The dark Fraunhofer lines in the solar spectrum: the cooler gases of the Sun's atmosphere absorb exactly the wavelengths they would themselves emit.

Newton's law of cooling

Key Point — the law, and its honest status:  dTdt=k(TTs)withk=4σAeTs3ms \boxed{\ -\frac{dT}{dt} = k\,(T - T_s) \qquad\text{with}\qquad k = \frac{4\sigma A e\, T_s^{3}}{m s}\ } It is an approximation, obtained from the Stefan-Boltzmann law by a binomial expansion of (Ts+ΔT)4(T_s + \Delta T)^4 and valid only while the excess TTsT - T_s is small compared with TsT_s. It is not a law of nature in its own right.

Key Point — Celsius is safe here, and only here. Newton's law contains nothing but the difference TTsT - T_s, and a difference is the same number in Celsius and in kelvin. So a cooling problem may be worked entirely in °°C. The moment a fourth power or a ratio appears — including inside the expression for kk, where TsT_s is cubed — you are back to kelvin.

The two forms you actually use:

Form Statement When
Exponential T=Ts+(T0Ts)ektT = T_s + (T_0 - T_s)e^{-kt}, so the excess decays exponentially any drop, and compulsory for a large one
Log plot ln(TTs)=kt+ln(T0Ts)\ln(T - T_s) = -kt + \ln(T_0 - T_s): a straight line of slope k-k reading a laboratory graph
Average temperature T1T2t=k(T1+T22Ts)\frac{T_1 - T_2}{t} = k\left(\frac{T_1 + T_2}{2} - T_s\right) a small drop across one stage; what most exam problems want
Time constant 1k\frac{1}{k}, the time for the excess to fall to 1e\frac{1}{e}, about 37% reading a kk

How good is each approximation? Both have been measured.

  • The average-temperature shortcut is excellent while the drop in one stage is small compared with the excess. Water cooling from 70°70°C to 60°60°C, then 60°60°C to 50°50°C, in a 20°20°C room: the shortcut gives 6.43 min against an exact 6.45 min, an error of 0.27-0.27%. But a body falling from 90°90°C to 30°30°C in a 20°20°C room in one step is off by 23-23%, and there the logarithm is compulsory.
  • Newton's law itself understates the true radiative loss, because the binomial expansion throws away positive terms. At an excess of 10 K it predicts 95.1% of the true rate, and the half-life of the excess comes out about 3.7% too long. At an excess of 100 K it predicts only 61.7% of the true rate, and the half-life is about 42% too long. Do not present the law as exact.

Key Point — the range of validity, stated honestly: for radiation alone, Newton's law is good to about 5% out to an excess of roughly 10 K. In a real laboratory, where convection also carries heat away and convective loss is much closer to linear in ΔT\Delta T, it works usefully out to about 30 to 40 K.

Two applications that carry marks

The solar constant is the solar energy received per unit time per unit area on a surface held perpendicular to the Sun's rays just outside the atmosphere, about 1.4 kW/m2^2. At ground level roughly 1.0 kW/m2^2 survives the journey down.

The greenhouse effect. Short-wavelength sunlight passes freely through the atmosphere and warms the ground. The ground, being far cooler than the Sun, re-radiates in the long-wavelength infrared — exactly where carbon dioxide, water vapour and methane absorb strongly. That energy is trapped and re-emitted downwards, and the surface settles about 33°33°C warmer than it otherwise would. It is what makes the planet habitable; raising the concentration of those gases shifts the balance. A parked car in the sun is the same physics on a small scale.

[JEE Tip] Before applying Newton's law of cooling, form the ratio TTsTs\frac{T - T_s}{T_s} in kelvin. Below about 0.05 the law is excellent; above about 0.15 it is doing real damage, and if the question asks you to comment, that ratio is the answer.

Card 5 — Which Tool Does This Question Want?

This is the most valuable card in the section. Almost nobody loses marks in this chapter because they cannot do the arithmetic. They lose them by reaching for the wrong equation in the first five seconds, and then computing a perfectly accurate answer to a question nobody asked.

Decision chart from question wording to expansion calorimetry conduction or radiation

The one question that decides it

Is the body growing, mixing, conducting or glowing? Four verbs, four tools. Everything in the chapter is one of them.

If the question is about a body that… you want and the formula is
changes SIZE when heated expansion ΔL=αLΔT\Delta L = \alpha L \Delta T, with β=2α\beta = 2\alpha and γ=3α\gamma = 3\alpha
touches another body and they settle calorimetry ΔQ=0\sum \Delta Q = 0, with msΔTms\Delta T and mLfmL_f or mLvmL_v terms
lets heat cross a solid conduction H=KAΔTL=ΔTRH = \frac{KA\Delta T}{L} = \frac{\Delta T}{R}, R=LKAR = \frac{L}{KA}
loses heat through space radiation σAe(T4Ts4)\sigma A e (T^4 - T_s^4), λmT=b\lambda_m T = b, dTdt=k(TTs)-\frac{dT}{dt} = k(T-T_s)

The cue words, which is what you will actually recognise

Wording in the question What it is telling you
"a rod is heated through", "a gap is left between rails" linear expansion, ΔL=αLΔT\Delta L = \alpha L \Delta T
"a circular hole in a plate", "an iron ring is slipped onto" areal expansion, and the hole gets bigger
"filled to the brim and heated", "overflows" apparent expansion, γapparent=γrealγvessel\gamma_{\text{apparent}} = \gamma_{\text{real}} - \gamma_{\text{vessel}}
"clamped between rigid walls", "cannot expand" thermal stress YαΔTY\alpha\Delta T
"a steel tape reads", "a pendulum clock" an expansion error, not a length
"mixed in a calorimeter", "the final temperature of the mixture" calorimetry, ΔQ=0\sum \Delta Q = 0
"water equivalent", "a calorimeter of mass mm and specific heat" fold the vessel in as extra water
"ice at 0°C is dropped into", "steam is passed into" calorimetry with a phase change — branch before you assume
"how much heat to melt / to boil / to freeze" latent heat, mLfmL_f or mLvmL_v
"a heater takes so many minutes" power ×\times time == the heat, then msΔTms\Delta T or mLfmL_f or mLvmL_v
"a wall of thickness", "a slab", "a lagged rod", "K=K =" conduction, H=KAΔTLH = \frac{KA\Delta T}{L}
"joined end to end" / "placed side by side" thermal resistances in series / in parallel
"the temperature of the junction" equate the two heat currents
"ice forms on a pond", "the boiler base", "the icebox wall" conduction, usually with a latent heat at one end
"emissivity", "a blackbody", "surroundings at" Stefan-Boltzmann, σAe(T4Ts4)\sigma A e (T^4 - T_s^4), kelvin
"peaks at a wavelength of", "the colour of a star" Wien, λmT=b\lambda_m T = b, kelvin
"a good absorber is a good emitter", "blackened and polished" Kirchhoff
"cools from … to … in … minutes" Newton's law of cooling, average-temperature form
"a graph of ln(TTs)\ln(T - T_s) against tt" slope =k= -k, intercept =ln(T0Ts)= \ln(T_0 - T_s)

Six traps that live in exactly this decision

  1. Celsius where kelvin is required. A fourth power, a ratio or a gas law needs the absolute temperature. A difference ΔT\Delta T does not. This decides more marks than everything else on this card put together.
  2. Assuming all the ice melts. Compute the heat available and the heat required, compare them, and only then decide whether the answer pins at 0°C.
  3. Reaching for conduction when the question says "in a vacuum" or "in space". No medium means radiation only — conduction and convection are both out.
  4. Using Newton's law of cooling at a large excess. It is a small-excess approximation. At an excess of 100 K it is wrong by nearly 40% on the rate.
  5. Confusing KK with kk. KK is thermal conductivity, W/(m K). kk is the cooling constant, s1^{-1}. Different quantities, different units, and a formula sheet that uses kk for conductivity will happily let you mix them.
  6. Forgetting that a hole expands. A ring, a washer, a bearing and the bore of a pipe all get larger on heating, never smaller.

[JEE Tip] When a question gives you a mass, a specific heat and a latent heat, it is telling you that the substance crosses a phase boundary somewhere in the answer. Write down every stage of the journey before you compute anything — msΔTms\Delta T, then mLfmL_f, then msΔTms\Delta T again — and add them at the end.

Card 6 — The Mistakes That Cost the Most Marks

Every one of these was flagged somewhere in the earlier sections. They are ordered by how often they actually turn up in answer scripts.

1. Celsius where kelvin is required. This is the commonest error in the entire chapter. Any temperature that enters a power, a product or a ratio must be absolute. σAeT4\sigma A e T^4, λmT=b\lambda_m T = b, PV=μRTPV = \mu R T, T2T1\frac{T_2}{T_1}, and the Ts3T_s^3 inside the cooling constant — all kelvin. A body at 327°327°C radiates as 6004600^4, not as 3274327^4, and the difference is a factor of eleven. Write "K" next to every temperature you substitute.

2. Assuming all the ice melts. Compare the heat available with the heat required before you assume anything. If the water cannot supply miceLfm_{\text{ice}}L_f, the mixture pins at 0°C with only part of the ice melted, and the answer is 0°C with a mass, not a temperature above zero.

3. Forgetting the latent-heat term altogether. If the journey crosses 0°C or 100°100°C, an mLfmL_f or mLvmL_v term belongs in the balance. A calculation that takes ice at 10°-10°C straight to water at 20°20°C with a single msΔTms\Delta T has left out the largest term in the sum.

4. Thinking a hole gets smaller when the plate is heated. It gets bigger, by 2αAΔT2\alpha A\Delta T, exactly as though it were filled with the same metal. Rings, washers, bearings and pipe bores all grow.

5. Treating Newton's law of cooling as exact. It is a binomial approximation to the Stefan-Boltzmann law, valid only for a small excess. At an excess of 10 K it gives 95.1% of the true rate of loss; at 100 K, only 61.7%. If a question asks you to comment on its validity, form TTsTs\frac{T - T_s}{T_s} in kelvin and say what you find.

6. Writing a bare LL for latent heat. Use LfL_f and LvL_v. A bare LL in this chapter is a length — the length of a rod, the thickness of a slab — and the two appear in the same problem more often than you would like.

7. Confusing ss, CC and SS — or KK and kk. ss is per kilogram, CC is per mole, SS belongs to a whole body. KK is conductivity in W/(m K); kk is the cooling constant in s1^{-1}. Write the unit beside the symbol and the confusion cannot survive.

8. Using the wrong area or the wrong length in the conduction law. AA is the area perpendicular to the heat flow; LL is the thickness along it. For a rod it is the cross-section and the length; for a wall it is the wall's face and its thickness. Swapping them is common and expensive.

9. Adding conductivities instead of resistances. Slabs in series add their resistances; slabs in parallel add their conductances. KeqK_{\text{eq}} is never the simple average unless the geometry happens to make it so.

10. Leaving a mass in grams inside a latent-heat or specific-heat term. LfL_f and ss are quoted per kilogram. A factor of 1000 is the commonest arithmetic slip in this chapter.

11. Quoting β=2α\beta = 2\alpha and γ=3α\gamma = 3\alpha as exact identities. They are first-order results from (1+αΔT)2(1+\alpha\Delta T)^2 and (1+αΔT)3(1+\alpha\Delta T)^3. The neglected terms are tiny — a fraction of a per cent for a metal over 100 K — but if a question asks you to justify the relations, that expansion is the mark.

12. Forgetting that water is densest at 4°C. Between 0°C and 4°C water contracts when heated. Every lake question turns on this.

13. Ignoring the surroundings in a radiation problem. A body in a room does not simply radiate σAeT4\sigma A e T^4; it also absorbs, so the net loss is σAe(T4Ts4)\sigma A e (T^4 - T_s^4). Leaving out the Ts4T_s^4 term overstates the answer, sometimes badly.

14. Losing the sign in a cooling problem. dTdt=k(TTs)-\frac{dT}{dt} = k(T - T_s): the body's temperature falls, so dTdt\frac{dT}{dt} is negative and kk is positive. And equal temperature drops take longer and longer as the body cools. Any answer where the second stage is quicker than the first is wrong on sight.

Key Point: Three more that cost single marks each — quoting a specific heat capacity with the units of a molar specific heat, forgetting that emissivity and absorptive power are pure numbers with no unit at all, and mixing 273273 with 273.15273.15 inside one problem.


The 60-Second Revision

You are in the queue outside the hall. This is the irreducible minimum.

Scales. tF=95tC+32t_F = \frac{9}{5}t_C + 32; the scales agree at 40°-40°. T=tC+273.15T = t_C + 273.15. Triple point 273.16 K. Absolute zero 0 K. TT in a power or a ratio is always kelvin; ΔT\Delta T is the same in both.

Expansion. ΔL=αLΔT\Delta L = \alpha L\Delta T, ΔA=βAΔT\Delta A = \beta A\Delta T, ΔV=γVΔT\Delta V = \gamma V\Delta T, with β=2α\beta = 2\alpha, γ=3α\gamma = 3\alpha, ratio 1:2:31:2:3. A hole gets bigger. γapparent=γrealγvessel\gamma_{\text{apparent}} = \gamma_{\text{real}} - \gamma_{\text{vessel}}. Clamped rod: stress =YαΔT= Y\alpha\Delta T. Water is densest at 4°C.

Heat capacity. ΔQ=msΔT\Delta Q = ms\Delta T; S=msS = ms in J/K; C=sMC = sM in J/(mol K); C3R25C \approx 3R \approx 25 J/(mol K) for simple solids; CpCv=RC_p - C_v = R. Water 4186 J/(kg K), the largest in the table.

Calorimetry. ΔQ=0\sum \Delta Q = 0. Water equivalent W=mcscswW = \frac{m_c s_c}{s_w}, in kg. Check the phase change before assuming a final temperature.

Latent heat. Q=mLfQ = mL_f or mLvmL_v; Lf=3.33×105L_f = 3.33 \times 10^{5} and Lv=22.6×105L_v = 22.6 \times 10^{5} J/kg, a ratio of 6.8. Temperature is constant during a change of state. Steam scalds because of that 2260 kJ/kg.

Conduction. H=KAΔTL=ΔTRH = \frac{KA\Delta T}{L} = \frac{\Delta T}{R} with R=LKAR = \frac{L}{KA} in K/W. Series: R=R1+R2R = R_1 + R_2, same HH. Parallel: conductances add, same ΔT\Delta T. Air 0.024 W/(m K) is the insulator; copper 385 is the conductor.

Convection. Bulk motion of the fluid; impossible in a solid. Natural against forced; sea breeze by day, land breeze by night.

Radiation. H=σAeT4H = \sigma A e T^4, net σAe(T4Ts4)\sigma A e (T^4 - T_s^4), σ=5.67×108\sigma = 5.67 \times 10^{-8}. Double TT and the power goes up sixteen times. Wien λmT=b=2.9×103\lambda_m T = b = 2.9 \times 10^{-3} m K, hotter means shorter. Kirchhoff: a good absorber is a good emitter. Blackbody: a=1a = 1, e=1e = 1.

Cooling. dTdt=k(TTs)-\frac{dT}{dt} = k(T - T_s), k=4σAeTs3msk = \frac{4\sigma A e T_s^3}{ms}, an approximation for a small excess. T=Ts+(T0Ts)ektT = T_s + (T_0 - T_s)e^{-kt}; ln(TTs)\ln(T - T_s) against tt is a straight line of slope k-k. Average form T1T2t=k(T1+T22Ts)\frac{T_1 - T_2}{t} = k\left(\frac{T_1+T_2}{2} - T_s\right). Celsius is safe here.

Habits. Convert every temperature to kelvin before a power or a ratio. Convert grams to kilograms. Ask whether a phase change happens. Write the unit beside every symbol. Check that a mixture's answer lies between the two starting temperatures.


The Fast Self-Test

Cover the answers. Sixteen questions, five minutes. Anything you miss tells you which card to reopen tonight.

  1. State the zeroth law, and say why it is needed before a thermometer can mean anything.
  2. Convert 37°37°C to Fahrenheit, and say at what temperature the two scales read alike.
  3. Why is the triple point of water preferred to the melting point of ice as the defining fixed point?
  4. In which of these may Celsius be substituted directly: λmT=b\lambda_m T = b, Q=msΔTQ = ms\Delta T, σAeT4\sigma A e T^4, dTdt=k(TTs)-\frac{dT}{dt} = k(T - T_s)?
  5. Write the three expansion coefficients, their ratio, and where that ratio comes from.
  6. A circular hole is cut in a metal plate and the plate is heated. What happens to the hole, and why?
  7. Distinguish ss, CC and SS, with units. What is the Dulong-Petit value?
  8. State the principle of calorimetry, and define water equivalent with its SI unit.
  9. Ice at 0°C is dropped into warm water. What must you check before assuming a final temperature?
  10. Why is the temperature constant during melting? Which is bigger, LfL_f or LvL_v, and by what factor?
  11. Write the conduction law and define the temperature gradient. Does it need Celsius or kelvin?
  12. Write the thermal resistance of a slab, and the rules for combining slabs in series and in parallel.
  13. State Wien's law and the Stefan-Boltzmann law. What happens to the radiated power if the absolute temperature is doubled?
  14. State Kirchhoff's law and give one piece of everyday evidence for it.
  15. Write Newton's law of cooling, both forms. Why is it only an approximation, and how far can it be trusted?
  16. Name the four tools of this chapter and the verb that selects each one.

Answers. 1. If AA and BB are each in thermal equilibrium with CC, they are in equilibrium with each other; without it, "temperature" would not be a consistent property and a thermometer could not stand in for direct contact. 2. 95(37)+32=98.6°\frac{9}{5}(37) + 32 = 98.6°F; they agree at 40°-40°. 3. Because a triple point occurs at exactly one pressure and one temperature, so it cannot drift with the surrounding conditions, while a melting point shifts with pressure. 4. Q=msΔTQ = ms\Delta T and dTdt=k(TTs)-\frac{dT}{dt} = k(T - T_s) — both contain only a difference. The other two contain a product and a fourth power, so they need kelvin. 5. ΔL=αLΔT\Delta L = \alpha L\Delta T, ΔA=βAΔT\Delta A = \beta A\Delta T, ΔV=γVΔT\Delta V = \gamma V\Delta T; α:β:γ=1:2:3\alpha : \beta : \gamma = 1 : 2 : 3; from keeping the linear term of (1+αΔT)2(1+\alpha\Delta T)^2 and (1+αΔT)3(1+\alpha\Delta T)^3. 6. It gets bigger, by 2αAΔT2\alpha A\Delta T — the hole expands exactly as the disc of metal removed from it would have. 7. ss is per kilogram, J/(kg K); CC is per mole, J/(mol K); SS belongs to a whole body, J/K, with S=msS = ms; Dulong-Petit is C3R25C \approx 3R \approx 25 J/(mol K). 8. In an isolated system heat lost equals heat gained, ΔQ=0\sum \Delta Q = 0; the water equivalent W=mcscswW = \frac{m_c s_c}{s_w} is the mass of water that would absorb the same heat as the calorimeter, in kilograms. 9. Whether the heat available from the water, mwswΔtm_w s_w \Delta t, is enough to supply miceLfm_{\text{ice}}L_f; if it is not, the mixture pins at 0°C with only part of the ice melted. 10. Because the energy goes into breaking the bonds holding the state together rather than into kinetic energy; LvL_v is bigger, by a factor of 22.63.33=6.8\frac{22.6}{3.33} = 6.8. 11. H=KAΔTLH = \frac{KA\Delta T}{L}, gradient =ΔTL= \frac{\Delta T}{L} in K/m; only a difference appears, so Celsius and kelvin give the same number. 12. R=LKAR = \frac{L}{KA} in K/W; series R=R1+R2R = R_1 + R_2 with the same HH, parallel 1R=1R1+1R2\frac{1}{R} = \frac{1}{R_1} + \frac{1}{R_2} with the same ΔT\Delta T. 13. λmT=b=2.9×103\lambda_m T = b = 2.9 \times 10^{-3} m K and H=σAeT4H = \sigma A e T^4; doubling the absolute temperature multiplies the power by 16. 14. At a given temperature and wavelength the ratio of emissive to absorptive power is the same for all bodies, so a good absorber is a good emitter; a blackened vessel cools faster than an identical polished one. 15. dTdt=k(TTs)-\frac{dT}{dt} = k(T - T_s), solving to T=Ts+(T0Ts)ektT = T_s + (T_0 - T_s)e^{-kt}, with the average-temperature form T1T2t=k(T1+T22Ts)\frac{T_1 - T_2}{t} = k\left(\frac{T_1+T_2}{2} - T_s\right); it is a binomial approximation to the fourth-power law, trustworthy to about 5% out to an excess of roughly 10 K for pure radiation and to about 30 to 40 K when convection is also acting. 16. Expansion when a body grows, calorimetry when two bodies mix, conduction when heat crosses a solid, radiation when heat leaves through space.

That is the whole chapter. Go and get the marks.