Q = m c ΔT, where m is mass, c is specific heat capacity (J/kg/K). Heat capacity C = m c (J/K). For water: c = 4186 J/kg/K (one of the highest specific heats).
-- NCERT, p. 5Specific Heat Calorimetry
Lesson
The high-frequency trap in calorimetry problems is forgetting that heat exchange depends on mass × specific heat × temperature change — not on any single factor alone. Two bodies made of the same material but with different masses need different amounts of heat for the same temperature rise, and NEET distractors routinely isolate one variable to bait you.
Specific heat capacity (c) is the heat required to raise 1 kg of a substance by 1 K. The governing equation is Q = mcΔT, where Q is the heat transferred, m is the mass, and ΔT is the temperature change (NCERT Class 11 Physics Chapter 11, page 5). The SI unit of specific heat is J kg⁻¹ K⁻¹. Water has an unusually high specific heat (~4186 J kg⁻¹ K⁻¹), which is why it is the standard calorimetric liquid.
Calorimetry applies conservation of energy to heat exchange. When a hot body is placed in contact with a cold body inside an insulated calorimeter:
Heat lost by hot body = Heat gained by cold body
m₁c₁(T₁ − T_eq) = m₂c₂(T_eq − T₂)
where T_eq is the final equilibrium temperature. This equation assumes no phase change occurs — if one body reaches its melting or boiling point during the exchange, the latent heat formula Q = mL must be applied for the phase-change portion before continuing with Q = mcΔT for any further temperature change.
Watch out: When the problem gives two objects of the same material but different dimensions, the distractor that compares only specific heats (ignoring mass differences) is a common wrong option. Always compute or compare Q = mcΔT as a product — never drop a factor.
Practice MCQs
Select an option to see the explanation. Wrong answers show why your choice was tempting — and name the exact trap it exploits.
The SI unit of specific heat capacity is:
When heat is supplied to a body undergoing a phase change at constant pressure, its temperature:
In calorimetry, the principle of method of mixtures is based on:
A copper block of mass 2.0 kg at 100 °C is placed in 1.0 kg of water at 20 °C in an insulated calorimeter. Given c_copper = 390 J kg⁻¹ K⁻¹ and c_water = 4200 J kg⁻¹ K⁻¹, the equilibrium temperature is closest to:
Two iron spheres A and B have radii r and 2r respectively. Both are heated through the same temperature rise ΔT. The ratio of heat absorbed Q_A : Q_B is:
10 g of ice at 0 °C is mixed with 10 g of water at 100 °C in an insulated container. Given L_fusion = 3.36 × 10⁵ J/kg and c_water = 4200 J kg⁻¹ K⁻¹, the final temperature of the mixture is:
A 500 g aluminium vessel (c_Al = 900 J kg⁻¹ K⁻¹) contains 300 g of water at 25 °C. A 200 g iron block (c_Fe = 450 J kg⁻¹ K⁻¹) heated to T_i is dropped in. The equilibrium temperature is 30 °C. The initial temperature of the iron block is closest to:
Equal masses of water, copper, and aluminium are given the same amount of heat Q. Which statement correctly describes the final temperature ranking? (c_water > c_Al > c_Cu)
Worked Example
Pattern: Two bodies of given material and dimensions; find ratio of heat needed for the same temperature change (NEET pattern: heat capacity two bodies).
- 1
Given
Two solid cubes are made of the same metal (density ρ, specific heat c). Cube A has side length a = 0.10 m. Cube B has side length b = 0.20 m. Both are heated through the same temperature rise ΔT = 50 K.
- 2
Required
Find the ratio Q_A : Q_B.
- 3
Concept
Heat absorbed depends on mass, specific heat, and temperature change: Q = mcΔT. Since both cubes share the same material (same c and ρ) and the same ΔT, the ratio reduces to a comparison of masses. Mass = ρ × volume = ρ × (side)³.
- 4
Formula
Q = mcΔT, where m = ρ × side³.
- 5
Substitution
Q_A = ρ × (0.10)³ × c × 50 Q_B = ρ × (0.20)³ × c × 50 Q_A/Q_B = (0.10)³ / (0.20)³
- 6
Calculation
(0.10)³ = 1.0 × 10⁻³ m³ (0.20)³ = 8.0 × 10⁻³ m³ Q_A/Q_B = (1.0 × 10⁻³) / (8.0 × 10⁻³) = 1/8 Note on exact values: the side lengths 0.10 m and 0.20 m, the temperature rise 50 K, and the density and specific heat are treated as exact problem-defined values. They do not limit significant figures in the ratio.
- 7
Final answer
Q_A : Q_B = 1 : 8 Cube B requires 8 times more heat than cube A for the same temperature rise, because its volume (and hence mass) is 8 times larger.
- 8
Common trap
The distractor that gives 1 : 2 compares side lengths (linear dimensions). The distractor 1 : 4 compares surface areas (∝ side²). Heat depends on mass, which scales as volume (∝ side³). Always trace Q = mcΔT back to mass, and mass back to volume when density is the same.
- 9
Similar NEET-style question
Two aluminium cylinders P and Q have the same height but radii r and 3r respectively. If both are heated through the same temperature rise, find Q_P : Q_Q. Answer: Mass ∝ πr²h, so Q_P/Q_Q = r²/(3r)² = 1/9. The ratio is 1 : 9. ---
Before solving, remember these
Formulas
12 formulas — click to collapse
Bernoulli's equation
Conservation of energy along a streamline of incompressible non-viscous flow.
| Symbol | Quantity | SI Unit |
|---|---|---|
| P | pressure | Pa |
| rho | density | kg/m^3 |
| v | speed | m/s |
| g | gravity | m/s^2 |
| h | height | m |
Valid when
- Steady, non-viscous, incompressible flow
- Along a single streamline
- No work added/removed
Bulk modulus
Resistance of a material to uniform compression. Inverse: compressibility.
| Symbol | Quantity | SI Unit |
|---|---|---|
| K | bulk modulus | Pa |
| V | volume | m^3 |
| P | pressure | Pa |
Valid when
- Isotropic compression
- Within elastic regime
Capillary rise/depression
Height a liquid rises (or falls) in a capillary tube. cos(theta) > 0: rises (wetting); < 0: depresses.
| Symbol | Quantity | SI Unit |
|---|---|---|
| h | capillary height | m |
| T | surface tension | N/m |
| theta | contact angle | rad |
| rho | density | kg/m^3 |
| r | tube radius | m |
Valid when
- Narrow tube (capillary regime)
- Constant theta
Pressure in static fluid
Pressure at depth h below free surface of fluid of density rho.
| Symbol | Quantity | SI Unit |
|---|---|---|
| P | total pressure | Pa |
| P0 | atmospheric/surface pressure | Pa |
| rho | density | kg/m^3 |
| h | depth | m |
Valid when
- Static fluid (no flow)
- Constant g
- Constant rho (incompressible)
Latent heat
Heat absorbed/released during phase change at constant T. L_fusion or L_vaporisation.
| Symbol | Quantity | SI Unit |
|---|---|---|
| Q | heat | J |
| m | mass | kg |
| L | latent heat | J/kg |
Valid when
- Phase transition (constant T during)
- All mass m undergoes the transition
Specific heat / heat capacity
Heat required to raise mass m by temperature Delta_T. Specific heat c is material property.
| Symbol | Quantity | SI Unit |
|---|---|---|
| Q | heat | J |
| m | mass | kg |
| c | specific heat | J/kg/K |
| Delta_T | temp change | K |
Valid when
- No phase change during heating
- c approximately constant in temp range
Stefan-Boltzmann radiation law
Radiation power from a body. Black body epsilon=1; net to surroundings P = sigma*epsilon*A*(T^4 - T_s^4).
| Symbol | Quantity | SI Unit |
|---|---|---|
| sigma | Stefan-Boltzmann = 5.67e-8 | W/m^2/K^4 |
| epsilon | emissivity (0-1) | - |
| A | surface area | m^2 |
| T | absolute temp | K |
Valid when
- Body in radiative equilibrium
- T in kelvins
Stokes' law (viscous drag on sphere)
Drag force on a sphere of radius r moving with velocity v through viscous fluid (low Reynolds number).
| Symbol | Quantity | SI Unit |
|---|---|---|
| F | drag force | N |
| eta | viscosity | Pa*s |
| r | sphere radius | m |
| v | velocity | m/s |
Valid when
- Smooth, slow flow (low Reynolds number)
- Spherical body
- Newtonian fluid
Excess pressure inside drop/bubble
Excess internal pressure due to surface tension. Bubble has 2 surfaces, hence factor 4.
| Symbol | Quantity | SI Unit |
|---|---|---|
| Delta_P | excess pressure | Pa |
| T | surface tension | N/m |
| r | radius | m |
Valid when
- Spherical drop or bubble
- Constant T (one fluid pair)
Terminal velocity of sphere in viscous fluid
Constant velocity reached when net force is zero (gravity balanced by buoyancy + viscous drag).
| Symbol | Quantity | SI Unit |
|---|---|---|
| v_t | terminal velocity | m/s |
| r | sphere radius | m |
| rho_s | sphere density | kg/m^3 |
| rho_f | fluid density | kg/m^3 |
| eta | viscosity | Pa*s |
Valid when
- Steady state (net force zero)
- Stokes regime applicable
Thermal expansion (linear/area/volume)
Fractional change in length, area, volume per degree temperature change.
| Symbol | Quantity | SI Unit |
|---|---|---|
| alpha | linear coefficient | 1/K |
| beta | volume coefficient | 1/K |
| Delta_T | temperature change | K |
Valid when
- Isotropic material
- Modest temperature range (alpha ~ constant)
Young's modulus
Ratio of longitudinal stress to longitudinal strain in a stretched wire/rod within elastic limit.
| Symbol | Quantity | SI Unit |
|---|---|---|
| Y | Young's modulus | Pa |
| F | applied force | N |
| A | cross-section area | m^2 |
| L | original length | m |
| Delta_L | extension | m |
Valid when
- Within elastic limit (Hooke's law region)
- Uniform cross-section
- Force along length
Exam Traps & Common Mistakes
These are the exact patterns that cause wrong answers in NEET. Each trap includes when it triggers and how to avoid it.
5 items — click to collapse
Category: Similar Terms
Student uses 2T/r for soap bubble (drop formula). Bubble has 2 surfaces → 4T/r.
When it triggers
Question mentions soap bubble OR liquid drop OR air bubble in liquid.
How to avoid
Drop in air: 1 surface → 2T/r. Soap bubble in air: 2 surfaces → 4T/r. Air bubble in liquid: 1 surface → 2T/r.
Category: Similar Terms
Student uses Y formula when problem is about volumetric compression (use K) or vice versa.
When it triggers
Problem describes longitudinal stretching (use Y), volumetric pressure (use K), or shear (use G).
How to avoid
Y: longitudinal stress/strain. K: volumetric. G: shear. Match modulus to deformation type.
Root cause: concept gap
Correction
Drop in air: 1 surface → ΔP = 2T/r. Soap bubble: 2 surfaces (inner + outer) → ΔP = 4T/r. Air bubble inside liquid: 1 surface → 2T/r.
Root cause: formula misuse
Correction
v_t ∝ r² (because Stokes drag ∝ r v, gravity ∝ r³ - r³ = r³_diff). Doubling radius quadruples terminal velocity, not doubles.
Root cause: formula misuse
Correction
Y for longitudinal stretch (FL/A·ΔL); K for volumetric compression (-V·dP/dV); G for shear. Match modulus type to deformation type before computing.
Past Year Questions
15 questions from NEET 2020, 2021, 2022, 2023, 2024, 2025. Answers verified against NTA official keys. — click to collapse
If a soap bubble expands, the pressure inside the bubble
How NEET usually asks this
5 recurring patterns from past papers — click to collapse
Apply Bernoulli's equation to flow through pipes of varying cross-section / heights / Venturi-like geometries.
Common distractors
forgets height term
Drops rho*g*h term
equates pressures incorrectly
Picks wrong reference points
Two bodies of given material and dimensions; find ratio of heat needed for same temp change. Q ∝ m c.
Common distractors
ignores mass difference
Compares only specific heats, not masses
Energy to form a bubble of given radius from soap solution; or pressure inside vs outside. Bubble has 2 surfaces (factor 4T/r).
Common distractors
uses 2T r instead of 4T r for bubble
Treats soap bubble like a drop
Sphere falling in viscous liquid; find terminal velocity or shape of v(t) curve. v_t ∝ r^2.
Common distractors
expects linear acceleration
Default to constant acceleration without recognising drag-induced terminal v
Wire stretching: given Y, length, area, force or stress, find elongation or stress at limit. Y = FL/(A delta_L).
Common distractors
uses bulk modulus formula
Confuses Y with K
Sources
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