Along a streamline of an ideal incompressible fluid: P + ½ ρ v² + ρ g h = constant. Higher speed → lower pressure. Basis of aerofoil lift, venturi meter, atomiser.
-- NCERT, p. 6Bernoullis Principle
Lesson
The high-frequency trap with Bernoulli's equation is forgetting the height term. When a pipe changes both cross-section and elevation, aspirants who drop the ρgh term get a plausible-looking but wrong pressure or velocity — and lose marks to negative marking.
Bernoulli's principle states that for steady, incompressible, non-viscous flow along a streamline:
P + ½ρv² + ρgh = constant
This is energy conservation per unit volume. P is the pressure energy density, ½ρv² is the kinetic energy density, and ρgh is the gravitational potential energy density (NCERT Class 11 Physics Chapter 9, page 6).
Three conditions must hold for the equation to apply: (1) the flow is steady (no turbulence), (2) the fluid is incompressible (constant ρ), and (3) the fluid is non-viscous (no energy loss to friction). If any condition breaks — turbulent flow, compressible gas at high speed, or significant viscosity — Bernoulli's equation gives incorrect results.
How NEET uses this: Questions typically give two points along a pipe system (often a Venturi meter or a pipe with a constriction at a different height) and ask for the pressure difference or the velocity at one point. The continuity equation A₁v₁ = A₂v₂ is almost always needed alongside Bernoulli's equation to eliminate one unknown velocity.
Watch out: When both points are at the same height, the ρgh terms cancel and you get P₁ + ½ρv₁² = P₂ + ½ρv₂². Many aspirants memorise only this simplified form and then apply it to problems where heights differ — that is exactly the distractor NTA exploits.
Practice MCQs
Select an option to see the explanation. Wrong answers show why your choice was tempting — and name the exact trap it exploits.
Bernoulli's theorem is a statement of conservation of which quantity for a fluid in streamline flow?
Which of the following is NOT a necessary condition for Bernoulli's equation to be valid?
In Bernoulli's equation P + ½ρv² + ρgh = constant, the term ½ρv² represents:
Water flows through a horizontal pipe that narrows from cross-sectional area 4.0 × 10⁻² m² to 2.0 × 10⁻² m². If the speed of water in the wider section is 2.0 m/s, what is the speed in the narrower section?
Water flows steadily through a horizontal pipe. At point 1, the pressure is 3.0 × 10⁵ Pa and the speed is 2.0 m/s. At point 2 (same height), the speed is 4.0 m/s. Taking ρ = 1.0 × 10³ kg/m³, the pressure at point 2 is:
A Venturi meter has a wide section of area 4.0 × 10⁻² m² and a constriction of area 1.0 × 10⁻² m², both at the same height. If the pressure difference between the two sections is 4.5 × 10³ Pa and ρ = 1.0 × 10³ kg/m³, the speed of flow in the wide section is:
An ideal fluid flows through a pipe that rises vertically by height h while maintaining the same cross-sectional area throughout. Compared to the bottom, the pressure at the top is:
Water (ρ = 1.0 × 10³ kg/m³) flows through a pipe that narrows from area 8.0 × 10⁻² m² to 4.0 × 10⁻² m² while rising 5.0 m. The speed in the wider lower section is 2.0 m/s and the pressure there is 2.0 × 10⁵ Pa. Taking g = 10 m/s², the pressure in the narrower upper section is:
Quick recall before you leave
Worked Example
- 1
Given
A pipe carries water (ρ = 1.00 × 10³ kg/m³) from ground level to a point 3.0 m higher. At the ground-level section, the pipe area is 6.0 × 10⁻² m², the speed is 3.0 m/s, and the gauge pressure is 2.50 × 10⁵ Pa. At the upper section the pipe area is 3.0 × 10⁻² m². Take g = 10 m/s² (exact, problem-defined).
- 2
Required
Find the gauge pressure at the upper section.
- 3
Concept
Bernoulli's equation along a streamline connects pressure, speed, and height. The continuity equation connects speeds at different cross-sections.
- 4
Formula
Continuity: A₁v₁ = A₂v₂ Bernoulli: P₁ + ½ρv₁² + ρgh₁ = P₂ + ½ρv₂² + ρgh₂
- 5
Substitution
From continuity: v₂ = (6.0 × 10⁻² / 3.0 × 10⁻²) × 3.0 = 6.0 m/s Set h₁ = 0, h₂ = 3.0 m. P₂ = P₁ + ½ρ(v₁² − v₂²) − ρgΔh P₂ = 2.50 × 10⁵ + ½(1.00 × 10³)(9.0 − 36.0) − (1.00 × 10³)(10)(3.0)
- 6
Calculation
½(1.00 × 10³)(−27.0) = −1.35 × 10⁴ Pa (1.00 × 10³)(10)(3.0) = 3.00 × 10⁴ Pa P₂ = 2.50 × 10⁵ − 1.35 × 10⁴ − 3.00 × 10⁴ P₂ = 2.50 × 10⁵ − 4.35 × 10⁴ = 2.065 × 10⁵ Pa Note: g = 10 m/s² is stated as exact (problem-defined constant) and the integer 2 in the area ratio is a counting ratio. Neither limits significant figures. The given data (three significant figures) governs the final answer.
- 7
Final answer
P₂ = 2.07 × 10⁵ Pa (to three significant figures). The pressure drops because both the increased speed and the increased height drain pressure energy from the fluid.
- 8
Common trap
Forgetting the ρgΔh term. If you drop it, you get P₂ = 2.50 × 10⁵ − 1.35 × 10⁴ = 2.365 × 10⁵ Pa — a plausible-looking but wrong answer. This is the distractor NTA builds into the options (per pattern description: "drops ρgh term").
- 9
Similar NEET-style question
Oil (ρ = 8.0 × 10² kg/m³) flows through a horizontal pipe that widens from area 2.0 × 10⁻² m² to 8.0 × 10⁻² m². If the speed in the narrow section is 8.0 m/s and the pressure there is 1.0 × 10⁵ Pa, find the pressure in the wide section. (Answer: Apply continuity to get v₂ = 2.0 m/s, then Bernoulli at constant height gives P₂ = 1.0 × 10⁵ + ½(800)(64 − 4) = 1.0 × 10⁵ + 2.4 × 10⁴ = 1.24 × 10⁵ Pa.) ---
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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