Quick revisionFluids I + II on one pageEach idea in one line, its formula, the trap and how NEET asks it Class 11 · Chapter 9 · Part 1

Fluids I: pressure, floating and flow

Why dams are thick at the bottom, why ships float, why a hose nozzle speeds water up and why aeroplanes stay up. Every idea from your Module Test-05, taken from zero to exam level.

Most of CUT-6 45 Qs in Test-05 Viscosity & surface tension → Fluids II
9.1 Basics

What is a fluid?

Push a book sideways and it slides as one piece: it keeps its shape. Push water sideways and it simply flows. That is the whole difference. A fluid is anything that flows. Liquids and gases are both fluids.

Why do fluids flow? A solid can resist a sideways (shearing) push by deforming a little and pushing back. A fluid at rest cannot. Even a tiny sideways force makes its layers slide over each other. So a fluid at rest can push on a surface only at right angles to it. This one fact explains a lot of the chapter.

  • Liquids have a fixed volume but no fixed shape. They are nearly incompressible, so in this chapter we treat their density as constant.
  • Gases fill whatever container they are in and are easily compressed.
Definition

Density \( \rho = \dfrac{m}{V} \), SI unit kg m⁻³, dimensions [ML⁻³].
Relative density (specific gravity) \( = \dfrac{\rho}{\rho_{\text{water at }4^\circ\text{C}}} \). It is a pure number with no unit. Mercury has RD 13.6, so \( \rho_{Hg} = 13.6 \times 1000 = 13600 \) kg m⁻³.

Density and relative density
\[ \rho = \frac{m}{V}, \qquad \text{RD} = \frac{\rho}{1000\ \text{kg m}^{-3}} \]
1 g cm⁻³ = 1000 kg m⁻³. Water: 1000; seawater: 1030; ice: about 917 (problems often use 900); mercury: 13600; air: about 1.2–1.3 kg m⁻³.
Symbols and assumptions: ρ = density (kg/m³); m = mass (kg); V = volume (m³); RD = relative density compared with water of density 1000 kg/m³, dimensionless.
Mixing two liquids
\[ \rho_{\text{equal }V} = \frac{\rho_1 + \rho_2}{2}, \qquad \rho_{\text{equal }m} = \frac{2\rho_1\rho_2}{\rho_1 + \rho_2} \]
Always use total mass ÷ total volume. The equal-mass result (harmonic mean) is always the smaller one.
Symbols and assumptions: ρ₁, ρ₂ = original liquid densities (kg/m³); ρ_equal V = mixture density when equal volumes are mixed; ρ_equal m = mixture density when equal masses are mixed. Both formulas assume volumes add without contraction or expansion.
What "ideal fluid" means in questions

The ideal flow model uses an incompressible fluid (constant ρ), negligible viscosity and steady flow. Bernoulli's equation then relates points along a streamline, provided no pump or dissipative loss acts between them. If the flow is also irrotational, the same Bernoulli constant applies across streamlines. Viscosity, Stokes' law and surface tension are in Fluids II.

Worked example · Numerical

Two liquids of densities 0.8 g cm⁻³ and 1.2 g cm⁻³ are mixed. Find the density of the mixture if (a) equal volumes are mixed, (b) equal masses are mixed.

Show solution
  1. (a) Take volume \(V\) of each. Mass = \(0.8V + 1.2V = 2V\), total volume \(2V\), so \(\rho = 1.0\) g cm⁻³.
  2. (b) Take mass \(m\) of each. Volume = \(m/0.8 + m/1.2 = m(1.25 + 0.833) = 2.083m\). So \(\rho = 2m / 2.083m = 0.96\) g cm⁻³.
  3. Check with the formula: \(2(0.8)(1.2)/(2.0) = 0.96\). ✓

Answer: (a) 1.0 g cm⁻³ = 1000 kg m⁻³; (b) 0.96 g cm⁻³ = 960 kg m⁻³

9.2 Basics

Pressure: force spread over an area

A sharp knife cuts but a blunt one does not, even though your hand pushes just as hard. A camel walks on sand without sinking because its feet are wide. School-bag straps are made wide so they do not dig into your shoulders. In each case what matters is not just the force but how much area it is spread over. That quantity is pressure.

Definition

Pressure is the normal force per unit area: \( P = \dfrac{F_\perp}{A} \). More precisely, \( P = \lim_{\Delta A\to 0} \dfrac{\Delta F}{\Delta A} \) is the pressure at a point.
SI unit: pascal, 1 Pa = 1 N m⁻². Dimensions [ML⁻¹T⁻²], the same as stress and energy per unit volume.

9.2.1 Core

Pascal's law: pressure in a fluid at rest

A fluid at rest cannot sustain a sideways shear stress. On every little surface inside it, the neighbouring fluid pushes normally. At one point the pressure has the same value whichever way that surface faces; changing its orientation changes the direction of force, not the scalar pressure.

Three facts about pressure in a fluid at rest. All three are tested:

  1. Pressure is a scalar. It has no direction. What has a direction is the force the fluid exerts on a surface, and that force is always normal (perpendicular) to the surface.
  2. At a point, pressure is the same in every direction. A tiny probe at one point feels the same push from above, below and the sides. (NCERT shows this with a small triangular wedge of fluid: the forces balance only if \(P_a = P_b = P_c\).)
  3. Pressure increases with depth. Deeper water has more water above it pushing down.
Exam trap · your Test-05 Q3

"Pressure at a point in a fluid acts vertically downward" is false. Pressure has no direction; it acts equally in all directions at a point. "The force exerted by a fluid at rest on a surface is normal to the surface" is true. So in that A–R question the assertion is false and the reason is true.

Why equal height means equal pressure

Imagine a thin horizontal cylinder of liquid of end area A. Its weight acts downward, so it supplies no horizontal force. The pressure forces on its two ends are P₁A and P₂A in opposite directions. Horizontal equilibrium requires P₁A = P₂A, hence P₁ = P₂. If pressures differed, the liquid would accelerate instead of staying at rest.

This comparison applies within the same connected fluid in equilibrium. It does not equate the pressures in two unrelated sealed vessels merely because their points are at the same height. Across a flat liquid–liquid interface, pressure is continuous when interfacial curvature effects are negligible.

Pascal's law at one level
\[P_1=P_2\quad\text{at equal height in a connected fluid at rest}\]
P₁ and P₂ are pressures at two points, in Pa. For a small fluid wedge at one point, balancing forces and the projected face areas similarly gives equal pressure in every orientation. Pressure is not the same at every depth: deeper points generally have greater pressure.
Symbols and assumptions: P₁, P₂ = equilibrium pressures (Pa) at two points at the same height in a connected fluid. Different depths can have different pressures.
Two related uses of Pascal's law

NCERT 9.2.1 introduces equal pressure in equilibrium. Section 9.2.4 uses the undiminished transmission of an added pressure in hydraulic machines. Equal added pressure does not remove the pre-existing difference ρgΔh between different heights.

Check pressure and direction

9.2.2 Core

Variation of pressure with depth

A lower layer of water supports the layers above it. Pressure therefore increases downward. We can derive the amount of that increase by balancing forces on a small vertical column; we do not need to guess from the total amount of liquid in the vessel.

Why \(P = P_0 + \rho g h\)

Imagine a vertical cylinder of liquid with cross-section \(A\) and height \(h\), its top at the surface. It is in equilibrium, so the upward push on its bottom must hold up the downward push on its top plus its own weight:

\( P A = P_0 A + mg = P_0 A + (\rho A h) g \;\Rightarrow\; P = P_0 + \rho g h \).

Note that \(A\) cancels. Pressure depends only on vertical depth, not on how wide the vessel is, what shape it has, or how much liquid there is.

Pressure at depth h
\[ P = P_0 + \rho g h \]
\(P_0\) = pressure at the free surface (usually atmospheric, 1.013 × 10⁵ Pa), ρ = liquid density, h = vertical depth below the surface.
Symbols and assumptions: P = absolute pressure at the point (Pa); P₀ = pressure at the free surface (Pa); ρ = liquid density (kg/m³); g = gravitational acceleration (m/s²); h = vertical depth below the surface (m). The liquid is at rest and its density is uniform.
Between any two points
\[ P_2 - P_1 = \rho g (h_2 - h_1) \]
Only the vertical separation matters. Points at the same level in the same connected liquid at rest have the same pressure.
Symbols and assumptions: P₁, P₂ = pressures (Pa); h₁, h₂ = depths (m) measured downward from the same reference level; ρ = uniform density (kg/m³); g = gravitational acceleration (m/s²). A deeper point has greater h and greater P.
Interactive

Depth probe: pressure grows linearly with depth

Absolute P–
In atm–
Gauge ρgh–
Density–

Tap inside the tank to move the probe. The eight arrows are always equal in length: pressure at a point is the same in every direction. The graph on the right is a straight line that starts at \(P_0\), not at zero, with slope ρg. Try mercury and watch the slope jump (note that its scale changes).

Shape does not matter: the hydrostatic paradox

Fill three differently shaped vessels with the same base area to the same height. The pressure at the bottom, and so the force on the base, is the same in all three, even though they hold very different amounts of water. How can the base of the narrow-necked vessel feel more than the weight of the water in it? Because its sloping walls push down on the water. In the flared vessel the walls hold some of the water up.

Interactive

Hydrostatic paradox: same height, same pressure, different weights

Gauge P at base–
Base force F (20 cm²)–

"W = 2.12 F" means the water in that vessel weighs 2.12 times the force on its base. Change the height: the pressure arrows stay equal in all three, and only the straight vessel always has W = F. The walls of B and C carry the difference.

Force on a side wall: why dams are thick at the bottom

water P = ρgh grows with depth dam
Gauge pressure on the wall rises from 0 at the surface to ρgH at the bottom, so the bottom of the dam must be strongest.
Force on a vertical wall of width w, liquid depth H
\[ F = \underbrace{\frac{\rho g H}{2}}_{\text{average pressure}} \times (H w) = \frac{\rho g H^2 w}{2} \]
Gauge force (the atmosphere usually acts on both sides and cancels). The resultant acts at H/3 above the base. On the base itself, F = ρgH × (base area).
Symbols and assumptions: F = net force from the water (N); ρ = liquid density (kg/m³); g = gravitational acceleration (m/s²); H = vertical wetted depth (m); w = wall width (m). Atmospheric pressure acts on both sides and cancels; water is on only one side.
Worked example · Numerical

Find the absolute and gauge pressure 20 m below the surface of a lake. (\(P_0 = 1.01\times10^5\) Pa, \(g = 10\) m s⁻²)

Show solution
  1. Gauge: \(\rho g h = 1000 \times 10 \times 20 = 2.0\times10^5\) Pa.
  2. Absolute: \(P_0 + \rho g h = 1.01\times10^5 + 2.0\times10^5 = 3.01\times10^5\) Pa ≈ 3 atm.

Answer: gauge 2.0 × 10⁵ Pa, absolute 3.01 × 10⁵ Pa

Worked example · Numerical

A dam holds water 6 m deep along a width of 10 m. Find the total force of the water on the dam. (\(g = 10\) m s⁻²)

Show solution
  1. Average gauge pressure = \(\rho g H/2 = 1000 \times 10 \times 6 / 2 = 3\times10^4\) Pa.
  2. Area = \(6 \times 10 = 60\) m², so \(F = 3\times10^4 \times 60 = 1.8\times10^6\) N.

Answer: 1.8 × 10⁶ N (using ρgH over the whole wall would wrongly double it)

If density changes with depth

The simple product ρgh assumes constant density. If density is ρ(z), divide the liquid into thin horizontal slices. A slice of thickness dz adds pressure dP = ρ(z)g dz. Add the contributions by integrating. Here z measures depth downward from the free surface:

\[P(h)-P_0=g\int_0^h\rho(z)\,dz.\]

For separate uniform layers, integration becomes a sum: P − P₀ = g(ρ₁h₁ + ρ₂h₂ + …), where ρᵢ and hᵢ are each layer's density and vertical thickness. At a given depth, include all the layers above that point.

Try pressure, depth and wall force

★ Exam

Connected cylinders: final level and work done

Two upright vessels are connected at their bottoms by a pipe. Initially, the taller column gives a greater pressure at its end of the pipe. Water flows toward the shorter column. With the same liquid and equal air pressure above both surfaces, the final state at rest has equal surface heights, because the bottom pressures must match.

Equal heights do not necessarily mean equal volumes. A wider cylinder holds more water at the same height. To find the final height, conserve the total liquid volume. Assume both vessels have constant cross-sectional areas and a common bottom level, and the pipe's volume is negligible.

Final height: conserve volume
\[A_1h_1+A_2h_2=(A_1+A_2)h_f,\qquad h_f=\frac{A_1h_1+A_2h_2}{A_1+A_2}\]
A₁, A₂ = vessel areas (m²); h₁, h₂ = initial depths (m); h_f = final common depth (m). For equal areas, h_f = (h₁ + h₂)/2. A common surface pressure and the same liquid are essential assumptions.
Symbols and assumptions: A₁, A₂ = constant vessel areas (m²); h₁, h₂ = initial depths above the common bottom (m); h_f = settled common depth (m). Both surfaces have the same imposed pressure; the pipe volume is neglected.

Where does the lost gravitational energy go?

A uniform water column of height h and area A has mass ρAh. Its centre of mass is h/2 above the bottom, so its gravitational potential energy is U = ρgAh²/2. Add this energy for the two vessels before and after the transfer.

Gravity does positive work as the water redistributes: W_g = U_initial − U_final. During transfer some energy becomes kinetic; as real water settles, viscosity turns it into internal energy. In a perfectly lossless model, the liquid would keep oscillating instead of settling. This is why equalisation does not imply conservation of the initial gravitational potential energy.

Work by gravity during equalisation
\[W_g=\frac{\rho g}{2}\left[A_1h_1^2+A_2h_2^2-(A_1+A_2)h_f^2\right]=\frac{\rho gA_1A_2}{2(A_1+A_2)}(h_1-h_2)^2\]
W_g = work done by gravity (J); ρ = liquid density (kg/m³); g = gravitational acceleration (m/s²). A₁, A₂, h₁, h₂ and h_f have the meanings above. This is the decrease in gravitational potential energy between the initial and settled final states, not useful work automatically delivered by a machine.
Symbols and assumptions: W_g = work by gravity (J); ρ = common liquid density (kg/m³); g = gravitational acceleration (m/s²); A₁, A₂ = vessel areas (m²); h₁, h₂ = initial depths (m); h_f = final depth (m).
Shortcut for equal-area cylinders
\[W_g=\frac{\rho gA}{4}(h_1-h_2)^2\]
A = area of each cylinder, not their combined area. This special case follows by putting A₁ = A₂ = A in the general formula. The height difference is squared; exchanging the two initial heights leaves the result unchanged.
Symbols and assumptions: W_g = work by gravity (J); ρ = liquid density (kg/m³); g = gravitational acceleration (m/s²); A = area of each cylinder (m²); h₁, h₂ = initial depths (m). Only use this form when the vessel areas are equal.
Interactive

Before and after opening the connecting pipe

Final common depth–
Work done by gravity–
Volume transferred–

Water: ρ = 1000 kg/m³, g = 10 m/s² for comparison with Test-05 Q4. Both surfaces are open to the same atmosphere. The widths illustrate different areas; heights share one scale.

Worked example · Energy (like Test-05 Q4)

Two identical tanks, each of base area 3 m², stand side by side. One has water 8 m deep and the other 2 m deep. They are joined at the bottom by a thin pipe and the levels equalise. How much work does gravity do? (\(g = 10\) m s⁻²)

Show solution
  1. Final level = (8 + 2)/2 = 5 m in each tank.
  2. Effectively a 3 m thick layer (from 5 to 8 m) moves from the first tank into the second (from 2 to 5 m). Mass = \(1000 \times 3 \times 3 = 9000\) kg.
  3. Its centre of mass falls from 6.5 m to 3.5 m, a drop of 3 m.
  4. \(W = mg\Delta h = 9000 \times 10 \times 3 = 2.7\times10^5\) J.
  5. Shortcut: \(W = \rho g A (h_1 - h_2)^2/4\). In Test-05 Q4 (2 m², 6 m and 4 m) this gives \(1000\cdot10\cdot2\cdot4/4 = 2\times10^4\) J.

Answer: 2.7 × 10⁵ J

Choose the correct setup

Open connected vessels equalise height. Cylinders with loaded pistons instead have different surface pressures; their final heights can differ. Start by writing the pressure at one common level, including any piston force divided by its area. Do not apply the open-vessel average-height shortcut to a hydraulic press.

Now try the question from Test-05

9.2.3 Core

Atmospheric pressure, gauge pressure and the U-tube

We live at the bottom of an ocean of air several hundred kilometres deep. Its weight presses on everything with about 10⁵ N on every square metre, roughly the weight of a 10-tonne truck on each m². We don't get crushed because the fluids inside our body push back just as hard.

You use this every day. When you drink through a straw, you don't "pull" the juice up. You lower the pressure inside the straw, and the atmosphere pressing on the juice in the glass pushes it up. A suction hook sticks because you squeeze the air out from behind it and the atmosphere then holds it against the wall.

Measuring it: the mercury barometer

vacuum (P ≈ 0) h = 76 cm (vertical) P₀ pushes here mercury dish
Torricelli's barometer: the column stops where its weight per area equals P₀. The space above is (almost) a vacuum.
Barometer
\[ P_0 = \rho_{Hg}\, g\, h \]
At sea level h = 0.76 m: \(13600 \times 9.8 \times 0.76 = 1.013\times10^5\) Pa. With water the column would be 10.3 m tall. The height is the vertical height. It does not depend on the tube's width or tilt; tilting only makes the column longer along the tube.
Symbols and assumptions: P₀ = atmospheric pressure (Pa); ρ_Hg = mercury density (kg/m³); g = gravitational acceleration (m/s²); h = vertical height difference between mercury surfaces (m). Pressure above the closed-end column is treated as negligible.
UnitEqualsNote
1 atm1.013 × 10⁵ Pa = 76 cm Hg = 760 mm Hgsea-level average
1 torr1 mm Hg = 133 Pamedicine (blood pressure 120/80 mm Hg)
1 bar10⁵ Pameteorology; 1 millibar = 100 Pa
1 Pa1 N m⁻²SI unit

Gauge pressure vs absolute pressure

Absolute pressure P

The actual total pressure, measured from a perfect vacuum. Example: at 20 m depth in water, P ≈ 3 atm.

Gauge pressure P − P₀

The pressure above atmospheric. Tyre gauges and BP machines read this. At 20 m depth the gauge pressure is ρgh ≈ 2 atm. A negative gauge pressure means a partial vacuum (suction).

Open-tube manometer
\[ P_{\text{gas}} = P_0 + \rho g h \qquad (h = \text{difference in liquid levels}) \]
If the open side stands higher, the gas pressure is above atmospheric (h positive). If the open side is lower, the gas pressure is below atmospheric (subtract).
Symbols and assumptions: P_gas = gas absolute pressure (Pa); P₀ = atmospheric pressure (Pa); ρ = manometer-liquid density (kg/m³); g = gravitational acceleration (m/s²); h = vertical level difference (m). The displayed plus sign applies when the open-arm surface is higher; use a minus sign when it is lower.

U-tube with two liquids that don't mix

Pour oil into one arm of a U-tube containing water. The oil floats on the water and pushes the water up the other arm. To solve these, use one rule: in the same liquid, at the same level, at rest, the pressure is the same. Choose the level of the oil–water interface. Below it, both arms contain water.

\(P_0 + \rho_1 g h_1 = P_0 + \rho_2 g h_2 \;\Rightarrow\; \rho_1 h_1 = \rho_2 h_2\), with both heights measured from the interface level.

Interactive

U-tube: manometer and two-liquid balance

Level difference h–
Gauge P–
Absolute P–
Water column above A–
Oil surface higher by–

Every 1.33 kPa above atmospheric pushes the mercury 1 cm higher on the open side. Drop the gas pressure below 101.3 kPa and the open side goes lower.

The lighter oil needs a taller column to balance the water: ρ₁h₁ = ρ₂h₂, with heights measured from the interface line A–B.

Exam trap

In two-liquid U-tubes, students measure heights from the bottom of the tube. Always measure from the interface level. Also read carefully whether the question asks for the water column above the interface, or the difference between the two free surfaces.

Worked example · U-tube

Water is in a U-tube. Oil (ρ = 900 kg m⁻³) is poured into the left arm until the oil column is 12 cm long. How far above the oil–water interface does the water stand in the right arm, and which free surface is higher?

Show solution
  1. Equal pressure at the interface level: \(900 \times 12 = 1000 \times h_2\).
  2. \(h_2 = 10.8\) cm above the interface.
  3. The oil surface is 12 − 10.8 = 1.2 cm higher than the water surface.

Answer: 10.8 cm; the oil surface is 1.2 cm higher

Worked example · Manometer

An open mercury manometer attached to a gas cylinder shows the mercury 20 cm higher in the open arm. Find the gauge and absolute pressure of the gas in pascal. (P₀ = 1.013 × 10⁵ Pa, g = 9.8 m s⁻²)

Show solution
  1. Gauge = \(\rho g h = 13600 \times 9.8 \times 0.20 = 2.67\times10^4\) Pa.
  2. Absolute = \(1.013\times10^5 + 0.267\times10^5 = 1.28\times10^5\) Pa (= 96 cm of Hg).

Answer: gauge 2.67 × 10⁴ Pa, absolute 1.28 × 10⁵ Pa

Practice: barometers, manometers, U-tubes

9.2.4 Core

Hydraulic machines: applying Pascal's law

Squeeze the end of a toothpaste tube and paste comes out at the nozzle, far from your fingers. Press one side of a water-filled balloon and it bulges everywhere else. An enclosed liquid passes any extra push on to every part of itself. That is Pascal's law, and it lets a mechanic lift a car with one hand.

Pascal's law (two forms)

(1) The pressure in a fluid at rest is the same at all points at the same height. (If gravity is ignored, it is the same everywhere.)
(2) A change in pressure applied to an enclosed incompressible fluid is transmitted undiminished to every point of the fluid and to the walls of the container.

The hydraulic lift

Two pistons of areas \(A_1\) (small) and \(A_2\) (large) sit on the same enclosed liquid. Push the small one with \(F_1\). That adds pressure \(P = F_1/A_1\), which reaches the large piston unchanged, so it is pushed up with \(F_2 = P A_2\).

Force multiplication
\[ \frac{F_1}{A_1} = \frac{F_2}{A_2} \;\Rightarrow\; F_2 = F_1 \frac{A_2}{A_1} = F_1\left(\frac{d_2}{d_1}\right)^2 \]
Mechanical advantage = A₂/A₁. For round pistons, area ∝ (diameter)², so square the diameter ratio.
Symbols and assumptions: F₁ = input force (N); F₂ = balanced load force (N); A₁, A₂ = piston areas (m²); d₁, d₂ = piston diameters in matching units. These are force magnitudes due to the same added pressure; piston weight, friction and height corrections are neglected.
No free energy
\[ A_1 x_1 = A_2 x_2, \qquad F_1 x_1 = F_2 x_2 \]
The liquid volume pushed out of the small cylinder equals the volume entering the big one. The big piston rises only x₂ = x₁A₁/A₂, so work in = work out (ideal machine).
Symbols and assumptions: A₁, A₂ = piston areas (m²); x₁, x₂ = piston displacement magnitudes (m); F₁, F₂ = corresponding forces (N). A₁x₁ = A₂x₂ conserves volume, and F₁x₁ = F₂x₂ conserves work in the ideal machine.
Interactive

Hydraulic lift: force up, distance down

Output F₂–
A₂/A₁–
Pressure–
Big piston rises–
Work in–
Work out–

Diameter ratio 5 gives area ratio 25: 30 N becomes 750 N. But pushing the small piston 12 cm lifts the load less than 5 mm. Work in = work out, always.

Exam trap · your Test-05 Q5

Arms of diameter 1.4 cm and 7 cm, 20 N applied. The diameter ratio is 5, but force scales with area, so the factor is 5² = 25 and F₂ = 500 N. The answer 100 N comes from using the diameter ratio directly. Q1 is the same idea: syringes of 1 cm and 3 cm, 10 N → 10 × 9 = 90 N. If radii are given, square them the same way.

Hydraulic brakes. A light push on the brake pedal moves a piston in a small master cylinder. The pressure travels through the brake oil to larger pistons at each wheel, which press the brake pads with a much larger force. The added pressure is transmitted through the brake oil. The force at each piston equals this pressure increase times its piston area; actual front and rear braking forces can differ by design.

Worked example · Numerical

In a hydraulic press the piston diameters are 2 cm and 10 cm. A force of 30 N is applied to the small piston and it moves down 50 cm. Find the force on the large piston and how far it rises.

Show solution
  1. Area ratio \(= (10/2)^2 = 25\), so \(F_2 = 30 \times 25 = 750\) N.
  2. Volume is conserved: \(x_2 = x_1 \times A_1/A_2 = 50/25 = 2\) cm.
  3. Check: work in = \(30 \times 0.5 = 15\) J; work out = \(750 \times 0.02 = 15\) J. ✓

Answer: 750 N; the large piston rises 2 cm

Worked example · Numerical

A car lift has a large piston of area 0.2 m² carrying a car of mass 1600 kg. What force must be applied on the small piston of area 0.002 m²? What is the pressure in the oil? (g = 10 m s⁻²)

Show solution
  1. Load \(F_2 = 1600 \times 10 = 1.6\times10^4\) N. Pressure \(= F_2/A_2 = 8\times10^4\) Pa.
  2. \(F_1 = P A_1 = 8\times10^4 \times 0.002 = 160\) N.

Answer: 160 N; pressure 8 × 10⁴ Pa (gauge)

Worked example · Statement I / II

Statement I: A hydraulic lift multiplies force. Statement II: A hydraulic lift multiplies energy, because the output force is larger than the input force.

Show solution
  1. I is correct: F₂ = F₁A₂/A₁.
  2. II is incorrect: the large piston moves a smaller distance, so F₁x₁ = F₂x₂. No machine creates energy.

Answer: Statement I correct, Statement II incorrect

From your Test-05

★ Coaching topic Core

Buoyancy, Archimedes and floating

In a swimming pool you can lift a friend with one arm. A steel ship weighing thousands of tonnes floats, while a steel nail sinks. A bucket of water feels lighter while it is still under the surface of the well. All of these come from one upward push, the buoyant force (upthrust).

Where does it come from? Think of a cube held under water. Pressure pushes on all six faces. The side pushes cancel. But the bottom face is deeper than the top face, so it is pushed harder: \(F_B = (P_{bottom} - P_{top})A = \rho_l g h A = \rho_l g V\). The net push is upward and equals the weight of a cube of liquid the same size. The material of the body does not appear anywhere in this result.

Archimedes' principle

A body wholly or partly immersed in a fluid experiences an upward buoyant force equal to the weight of the fluid it displaces. The force acts at the centre of buoyancy, the centre of mass of the displaced fluid.

Exam trap · your Test-05 Q15

Buoyant force = weight of the liquid displaced. It is not "the weight of the body" (that equality holds only for a floating body), not "the volume of the body", and not "the weight of the body minus the weight of the liquid". For a fully immersed body it does not depend on depth or on what the body is made of.

Buoyant force
\[ F_B = \rho_l\, V_{sub}\, g \]
ρ_l = density of the liquid, V_sub = submerged volume. F_B vs V_sub is a straight line through the origin with slope ρ_l g, and it becomes flat once the body is fully under (Test-05 Q36).
Symbols and assumptions: F_B = upward buoyant force (N); ρ_l = liquid density (kg/m³); V_sub = displaced/submerged volume (m³); g = gravitational acceleration (m/s²). The submerged volume need not be the whole body volume.
Floating (equilibrium)
\[ \rho_b V g = \rho_l V_{sub} g \;\Rightarrow\; \frac{V_{sub}}{V} = \frac{\rho_b}{\rho_l} \]
Fraction submerged = density ratio. Ice (900) in water: 90% under. Wood (600) in water: 60% under.
Symbols and assumptions: ρ_b = mean body density (kg/m³); ρ_l = liquid density (kg/m³); V = total body volume (m³); V_sub = submerged volume (m³); g = gravitational acceleration (m/s²). The body floats freely with no other vertical support or force.
Apparent weight (fully immersed)
\[ W_{app} = W - F_B = W\left(1 - \frac{\rho_l}{\rho_b}\right) \]
Loss of weight = F_B. Relative density of a solid = W_air ÷ (W_air − W_water).
Symbols and assumptions: W_app = support-force magnitude/readout (N); W = true weight (N); F_B = buoyancy (N); ρ_l = liquid density; ρ_b = mean body density, both in kg/m³. A negative W − F_B means a downward restraint is needed, not a negative reading on an ordinary hanging spring balance.
Body at the interface of two liquids
\[ \rho_b V = \rho_1 V_1 + \rho_2 V_2 \]
V₁ + V₂ = V. The body's density is the volume-weighted average of the two liquids.
Symbols and assumptions: ρ_b = mean body density; ρ₁, ρ₂ = upper/lower liquid densities, all in kg/m³; V = total body volume; V₁, V₂ = volumes in the two liquids, all in m³. The displayed form assumes V₁ + V₂ = V; no part is in air.
Compare densitiesWhat happensNet force when fully under
ρ_body < ρ_liquidRises and floats, partly submerged (fraction ρ_b/ρ_l)Upward: accelerates up with a = (ρ_l/ρ_b − 1)g if released under water and drag is ignored
ρ_body = ρ_liquidFloats fully submerged at any depth (neutral)Zero
ρ_body > ρ_liquidSinks; apparent weight W(1 − ρ_l/ρ_b)Downward: a = (1 − ρ_l/ρ_b)g
Interactive

Floating lab: drop a block, watch it settle

Result–
Submerged–
F_B / W–
Apparent weight–
In lower liquid–

Arrows are drawn to scale. While the block bobs, F_B changes with depth. It settles where F_B = W. Make the block denser than the liquid: it sinks and the floor supplies the missing force N. In two-liquid mode a block with ρ₁ < ρ < ρ₂ stops at the interface.

Level-change puzzles (Test-05 Q12 type)

Use one idea: a floating object displaces its own weight of water; a sunk object displaces only its own volume. For anything denser than water, displacing its weight takes more water than displacing its volume.

SituationWater level in the tankWhy
Coin / stone on a floating block (or boat) falls or is thrown into the waterFalls; the block rises (floats higher)Before: the coin displaced m/ρ_w. After: only m/ρ_coin, which is less.
Wooden piece taken off the boat and dropped in the waterUnchangedIt still floats, so it still displaces its own weight.
Ice floating in water meltsUnchangedThe meltwater exactly fills the "hole" the ice was making.
Ice with a stone inside meltsFallsThe stone ends up sunk.
Ice with an air bubble or wood inside meltsUnchangedAir/wood still floats (air's mass ≈ 0).
Ice floating in salt water (or any liquid denser than water) meltsRisesMeltwater m/ρ_w > displaced m/ρ_salt.
Exam trap · your Test-05 Q12

A block carrying a coin floats in a tank. The coin slips off and sinks. Two things happen: the block rises (it is lighter, so less of it needs to be under water, and L, its height above the water, increases), and the water level h falls (the coin now displaces only its own volume). Students often say "the level stays the same". It doesn't.

Hollow bodies: material density and mean density differ

A sealed hollow metal ball can float even if its metal is denser than water. Its weight depends on the volume of metal, while the water displaced depends on the outer submerged volume, including the sealed cavity. Use the total mass divided by the outer volume to decide whether it can float.

For outer radius R, cavity radius a and material density ρ_s, ignoring the mass of enclosed air, \(M=\rho_s\frac{4\pi}{3}(R^3-a^3)\). The mean density is \(\bar\rho=M/(4\pi R^3/3)=\rho_s[1-(a/R)^3]\). Here M is the mass in kg, R and a are radii in m, and both densities are in kg/m³.

“Just floats” in the ideal question means fully immersed neutral equilibrium: mean density equals liquid density ρ_l. Hence \((a/R)^3=1-\rho_l/\rho_s\). The same ratio applies to cavity diameter divided by outer diameter. If water enters an open cavity, do not treat that water-filled space as the same sealed displaced volume.

Variable-density sphere: average over volume, not radius

In Test-05 Q13, the sphere's density varies with radial distance r from its centre. An outer shell contains more volume than an equally thick inner shell: for a thin shell, \(dV=4\pi r^2dr\). Therefore a simple average of centre and surface densities is wrong.

For sphere radius R and density \(\rho(r)=\rho_0(1-r/R)\), where ρ₀ is its central density, add the shell masses:

\[M=\int_0^R\rho(r)\,4\pi r^2dr=4\pi\rho_0\left[\frac{R^3}{3}-\frac{R^3}{4}\right]=\frac{\pi\rho_0R^3}{3}.\]

Dividing by total volume \(4\pi R^3/3\) gives \(\bar\rho=\rho_0/4\). Use this mean density in the ordinary floating relation \(V_\text{sub}/V=\bar\rho/\rho_l\). Here V is the sphere volume and V_sub is its submerged volume. This calculation averages the body's density; it differs from integrating a liquid's pressure through depth.

A burning candle: follow its bottom and top separately

Let a uniform floating candle have current length ℓ and submerged fraction f = ρ_c/ρ_l, where ρ_c and ρ_l are candle and liquid densities. Its immersed length is fℓ. If burning decreases total length at rate b, that immersed length decreases at rate fb. Relative to a nearly fixed water surface, the bottom therefore rises at fb, while the top falls at (1 − f)b.

For a half-submerged candle, f = 1/2. Burning at b = 4 cm/hour makes the bottom rise at 2 cm/hour and the top fall at 2 cm/hour. The large vessel in Q6 (D ≫ d, with D and d the vessel and candle diameters) makes the change of outside liquid level negligible. The model assumes uniform density and cross-section and no retained wax changing the mass balance.

More things that get asked

  • Extra load to sink a floater (Q11): extra mass needed = ρ_l × (unsubmerged volume). A 1 m³ cube half under water needs 1000 × 0.5 = 500 kg more.
  • Burning candle (Q6): the fraction submerged stays ρ_c/ρ_w. If the candle shortens at rate r, the submerged length shrinks at (ρ_c/ρ_w)r, so the bottom rises at that rate. Half-submerged, burning 4 cm/h → bottom rises 2 cm/h.
  • Hollow and variable-density bodies (Q9, Q13): use the average density = total mass ÷ total volume. "Just floats" (fully submerged at rest) means ρ_avg = ρ_l. See the shell-mass calculation above and Problem patterns.
  • Body on a spring, fully submerged (Q10): if it hangs from a spring, kx = mg − F_B. If it is tied to the bottom by a spring (a floater held under), kx = F_B − mg.
  • Accelerating container: in a lift accelerating up with a, replace g by g + a. Weight and buoyancy both scale, so the fraction submerged does not change. In free fall there is no buoyancy at all.
  • Rising body (like a bubble, Q14): with drag neglected, net upward force F_B − W = ma gives a = (ρ_l/ρ_b − 1)g. For a = g/100, ρ_l/ρ_b = 1.01.
Worked example · Numerical (like Q8, Q11)

A cube of side 0.5 m floats in water with 40% of its volume submerged. (a) What is its density? (b) What extra mass placed on it will just submerge it completely?

Show solution
  1. (a) Fraction submerged = ρ_b/ρ_w ⇒ ρ_b = 0.4 × 1000 = 400 kg m⁻³.
  2. (b) Volume = 0.125 m³. Unsubmerged part = 0.6 × 0.125 = 0.075 m³.
  3. To push it all under, the extra weight must equal the extra buoyancy: Δm = 1000 × 0.075 = 75 kg.

Answer: 400 kg m⁻³; 75 kg

Worked example · Ratio (like Q7, Q45)

A sphere of density d floats at the interface of two immiscible liquids of densities 0.8d (upper) and 1.4d (lower), fully submerged. Find the ratio of its volume in the lower liquid to that in the upper liquid.

Show solution
  1. Let a fraction x be in the lower liquid: \(d = 1.4d\,x + 0.8d(1 - x)\).
  2. \(1 = 0.8 + 0.6x \Rightarrow x = 1/3\).
  3. Lower : upper = 1/3 : 2/3 = 1 : 2.
  4. General form (Q45): with liquids ρ (upper) and nρ (lower) and fraction p in the lower one, \(d = p(n\rho) + (1-p)\rho = \{1 + (n-1)p\}\rho\).

Answer: 1 : 2

Worked example · Apparent weight

A stone of mass 2 kg and density 2500 kg m⁻³ is fully immersed in water. Find the buoyant force and its apparent weight. (g = 10 m s⁻²)

Show solution
  1. Volume = 2/2500 = 8 × 10⁻⁴ m³.
  2. F_B = 1000 × 8 × 10⁻⁴ × 10 = 8 N.
  3. Apparent weight = 20 − 8 = 12 N. Check: W(1 − ρ_l/ρ_b) = 20(1 − 0.4) = 12 N. ✓

Answer: 8 N; 12 N

From your Test-05 (the ones marked on your paper first)

See all buoyancy questions in Practice →

9.3 Basics

Streamline, laminar and turbulent flow

Watch smoke rising from an incense stick. For the first few centimetres it rises as a smooth, steady thread. Higher up it suddenly breaks into swirls and eddies. A slow river glides smoothly; white-water rapids churn. These are the two kinds of flow: streamline (smooth) and turbulent (chaotic).

Steady flow

The flow is steady if the velocity of the fluid at each fixed point in space does not change with time. Different points can have different velocities. A single particle can speed up or slow down as it moves from one point to another.

Exam trap · your Test-05 Q16

"In steady flow the velocity of every fluid particle is constant" is false. Steady means constant velocity at a point, not for a particle. A particle entering a narrow section speeds up (continuity), yet the flow is still perfectly steady, because every particle that passes that point has the same velocity there.

Streamline. In steady flow, the path a particle follows is a streamline. Every particle passing through a given point follows the same streamline. The tangent to a streamline at any point gives the direction of the velocity there.

  • Two streamlines never cross. At a crossing a particle would have two velocities at once, which is impossible.
  • Crowded streamlines mean fast flow; widely spaced streamlines mean slow flow. (You will see this in the continuity and aerofoil sims.)
  • Tube of flow: a bundle of streamlines. No fluid crosses its side walls, so whatever mass enters one end must leave the other. That gives the equation of continuity.

Streamline / laminar

Smooth, orderly; layers (laminae) slide past each other. Velocity at a point is constant in time. Happens at low speeds. Example: slow honey, gentle stream, the low part of incense smoke.

Turbulent

Irregular, with eddies and swirls; velocity at a point changes randomly. Happens above a critical speed. Examples: rapids, wake of a ship, smoke higher up, blood flow past a narrowed artery. Turbulence dissipates energy.

Link to Fluids II: Reynolds number

Whether a flow is laminar or turbulent depends on \( R_e = \dfrac{\rho v d}{\eta} \) (d = size of pipe or object, η = viscosity). The convention in your coaching test uses Re < 1000 for laminar and Re > 2000 for turbulent flow; these are approximate, geometry-dependent ranges. Details are in Fluids II. For Test-05 Q18: a smaller model (smaller d) needs a larger v to reach the same Re, so turbulence starts at a higher speed for the small model.

Worked example · Assertion–Reason

A: Water flowing through a pipe that narrows can be in steady flow even though each particle speeds up in the narrow part. R: Steady flow requires the velocity at every point of space to remain constant in time.

Show solution
  1. R is the definition of steady flow, so R is true.
  2. Speeding up as a particle moves from one point to another does not change the velocity at any fixed point over time. So A is true, and R explains it.

Answer: both true, R is the correct explanation of A

Worked example · Concept

Which of these flows is most likely turbulent? (a) honey poured slowly (b) water in a thin capillary (c) a river in flood through a rocky gorge (d) blood in a capillary.

Show solution
  1. Turbulence needs a high Re = ρvd/η: high speed, large size, low viscosity.
  2. Honey (very high η), capillaries (tiny d) and blood in capillaries (tiny d, slow) are all laminar. The flooded river has high speed and large size.

Answer: (c)

From your Test-05

9.3 Core

Equation of continuity

Put your thumb over the end of a garden hose and the water shoots out much faster. A river flows lazily where it is wide and races through a narrow gorge. The water has nowhere else to go: the same amount must pass every section each second, so where the passage is narrow the water must move faster.

Derivation. In time Δt, the fluid entering section 1 occupies a length v₁Δt, so its mass is ρ₁A₁v₁Δt. The same mass must leave through section 2 (no fluid crosses the walls of the tube of flow, and none piles up in steady flow): ρ₁A₁v₁ = ρ₂A₂v₂. For an incompressible liquid ρ₁ = ρ₂.

Equation of continuity (conservation of mass)
\[ A_1 v_1 = A_2 v_2 = Q \]
Q = volume flow rate (m³ s⁻¹), constant along the pipe. Mass flow rate = ρQ (kg s⁻¹).
Symbols and assumptions: A₁, A₂ = cross-sectional areas (m²); v₁, v₂ = section-average flow speeds (m/s); Q = volume flow rate (m³/s). This form requires steady incompressible flow with no leak between the sections.
Round pipes
\[ v \propto \frac{1}{A} \propto \frac{1}{d^2}, \qquad \frac{v_1}{v_2} = \left(\frac{d_2}{d_1}\right)^2 \]
Halve the diameter → 4× the speed. Kinetic energy per volume ½ρv² ∝ 1/d⁴.
Symbols and assumptions: v = section-average speed (m/s); A = area (m²); d = diameter (m); indices 1 and 2 identify two sections. Ratios assume the same conserved volume flow rate; diameter ratios must be squared.
Branching and many holes
\[ A v = \sum_i A_i v_i, \qquad A_1 v_1 = n\,a\,v_2 \]
Flow in = total flow out. Spray pumps and shower heads: n holes, each of area a.
Symbols and assumptions: A, v = inlet area (m²) and mean speed (m/s); A_i, v_i = area and outward mean speed of outlet i; n = number of identical holes; a = area of each hole (m²); A₁, v₁ = inlet values; v₂ = speed at each identical outlet (m/s).
Interactive

Continuity: same volume through every section, every second

Throat speed v₂–
d₂/d₁–
Q (A₁ = 10 cm²)–

The two counters stay equal: the same number of dots crosses the wide gate and the narrow gate. To manage that, dots in the throat must move faster. Notice the streamlines crowding together there. Area ratio 0.25 means diameter ratio 0.5 and speed × 4.

Why a falling stream of tap water narrows (Test-05 Q25). Once it leaves the tap, water speeds up under gravity: \(v^2 = v_0^2 + 2gh\). Since Av is constant, a larger v means a smaller A, so the stream gets thinner as it falls. This is continuity, not surface tension.

Exam trap

Areas go as the square of diameters (or radii). Test-05 Q22: diameters 6.4 cm and 3.2 cm → area ratio 4 → v_min : v_max = 1 : 4 (not 1 : 2). Q27: diameter ratio 2.5 : 3.75 = 2 : 3 → speed ratio 9 : 4 → KE per volume ratio (9/4)² = 81 : 16.

Worked example · Numerical (like Q19)

A spray pump has a cylindrical tube of cross-section 6 cm² ending in a nozzle with 30 fine holes, each of area 0.5 mm². Liquid moves in the tube at 1.5 m per minute. Find the speed at which it leaves the holes.

Show solution
  1. Convert: A₁ = 6 × 10⁻⁴ m², v₁ = 1.5/60 = 0.025 m s⁻¹, total hole area = 30 × 0.5 × 10⁻⁶ = 1.5 × 10⁻⁵ m².
  2. \(v_2 = \dfrac{A_1 v_1}{n a} = \dfrac{6\times10^{-4}\times0.025}{1.5\times10^{-5}} = 1\) m s⁻¹.

Answer: 1 m s⁻¹ (for Q19's numbers: 8 cm², 20 × 1 mm², 1 m/min → 2/3 m s⁻¹)

Worked example · Branching (like Q44)

Water flows at 2 m s⁻¹ in a pipe of area 3A. It splits into two branches of areas A and 2A. The speed in the first branch is 3 m s⁻¹. Find the speed in the second.

Show solution
  1. Flow in = flow out: \(3A \times 2 = A \times 3 + 2A \times V\).
  2. \(6 = 3 + 2V \Rightarrow V = 1.5\) m s⁻¹.

Answer: 1.5 m s⁻¹ (Q44: 2A·4 = (A/2)·4 + A·V → V = 6 m s⁻¹)

Worked example · Tap stream

Water leaves a tap at 1 m s⁻¹ with cross-section 1 cm². What is the cross-section of the stream 15 cm below the tap? (g = 10 m s⁻²)

Show solution
  1. \(v^2 = 1^2 + 2(10)(0.15) = 4 \Rightarrow v = 2\) m s⁻¹.
  2. \(A = A_0 v_0 / v = 1 \times 1/2 = 0.5\) cm². (The radius shrinks by a factor √2.)

Answer: 0.5 cm²

From your Test-05

9.4 Core

Bernoulli's principle

Hold a strip of paper just below your lips and blow over it: it rises. Hang two sheets of paper close together and blow between them: they come together, not apart. A shower curtain gets sucked inward when the shower runs. In each case fast-moving air has lower pressure. Bernoulli's principle explains why, and it is just energy conservation for a flowing fluid.

The idea behind the derivation

Follow a small slug of fluid of volume ΔV and mass Δm = ρΔV along a tube of flow, from section 1 (pressure P₁, speed v₁, height h₁) to section 2 (P₂, v₂, h₂).

  1. The fluid behind pushes it forward: work done = P₁A₁Δx₁ = P₁ΔV. The fluid ahead pushes back: work = −P₂ΔV. Net work by pressure = (P₁ − P₂)ΔV.
  2. Work–energy theorem: this net work = change in KE + change in PE = ½Δm(v₂² − v₁²) + Δm g(h₂ − h₁).
  3. Divide by ΔV (with Δm/ΔV = ρ) and rearrange: P₁ + ½ρv₁² + ρgh₁ = P₂ + ½ρv₂² + ρgh₂.
Bernoulli's equation (along a streamline)
\[ P + \tfrac{1}{2}\rho v^2 + \rho g h = \text{constant} \]
Each term is energy per unit volume (J m⁻³ = Pa): P = pressure energy, ½ρv² = kinetic energy, ρgh = potential energy, all per unit volume. Valid along a streamline for steady, incompressible flow with negligible viscosity and no added work or energy loss. Irrotational flow permits comparison across streamlines.
Symbols and assumptions: P = local pressure (Pa); ρ = density (kg/m³); v = speed (m/s); g = gravitational acceleration (m/s²); h = height (m) measured upward from a chosen datum. Unlike the earlier depth h, this h is an upward elevation.
Per unit mass
\[ \frac{P}{\rho} + \frac{v^2}{2} + g h = \text{const} \]
Units J kg⁻¹.
Symbols and assumptions: P = pressure (Pa); ρ = density (kg/m³); v = speed (m/s); g = gravitational acceleration (m/s²); h = upward elevation (m). Each term has units J/kg; the ideal Bernoulli assumptions still apply.
Per unit weight ("heads")
\[ \frac{P}{\rho g} + \frac{v^2}{2g} + h = \text{const} \]
Pressure head + velocity head + elevation head, each a length (m).
Symbols and assumptions: P = pressure (Pa); ρ = density (kg/m³); g = gravitational acceleration (m/s²); v = speed (m/s); h = upward elevation (m). Every term is a head in metres; a head is energy per unit weight.
Exam traps · your Test-05 Q21 and Q42
  • Bernoulli's equation is the law of conservation of energy (Q42). Continuity is conservation of mass. Neither is conservation of linear momentum.
  • Correct form (Q21): \(P + \tfrac12\rho v^2 + \rho g h\). Watch for wrong options like \(P + \tfrac12\rho v + \rho g h\), \(P + \tfrac12 v^2 + gh\) (mixing per-volume and per-mass terms), or \(P + \rho v^2 + \rho g h\).
  • For a fluid at rest (v = 0) it reduces to P + ρgh = const, which is the hydrostatics you already know.
Interactive

Energy per volume: P + ½ρv² + ρgh stays the same

v₂–
P₁ (pump)–
P₂–
P₁ − P₂–

The two bars always end at the same total. Raise section 2: the green ρgh grows and pressure is used up to pay for it. Narrow it: the coral ½ρv² grows (v₂ = v₁A₁/A₂) and pressure drops again. With h = 0 you get the horizontal-pipe rule: faster means lower pressure.

Static, dynamic and stagnation pressure

In a horizontal pipe, P + ½ρv² = const. P is the static pressure (what a gauge moving with the fluid would read). ½ρv² is the dynamic pressure. Where the fluid is brought to rest, at the nose of an object or the mouth of a tube facing the flow, all of it turns into pressure. The stagnation pressure there is P + ½ρv².

An L-shaped (pitot) tube with its open end facing the current therefore holds a column h = v²/2g higher than a plain vertical tube (Test-05 Q39).

Shortcuts
  • Horizontal pipe: narrowest section → maximum speed → minimum pressure; widest section → minimum speed → maximum pressure (Q41).
  • Liquid escaping from a region at pressure P₁ into a region at P₂ through a valve: ½ρv² = P₁ − P₂, so v ∝ √(P₁ − P₂) (Q43).
  • ΔP between two sections of a horizontal pipe = ½ρ(v₂² − v₁²). Find v₂ from continuity first.
Worked example · Numerical

Water flows at 2 m s⁻¹ through a horizontal pipe. At a constriction the area halves. Find the pressure difference between the wide and narrow parts.

Show solution
  1. Continuity: v₂ = 2 × 2 = 4 m s⁻¹.
  2. \(P_1 - P_2 = \tfrac12\rho(v_2^2 - v_1^2) = \tfrac12(1000)(16 - 4) = 6000\) Pa.

Answer: 6.0 × 10³ Pa (higher in the wide part)

Worked example · Numerical with height

Water at pressure 2.0 × 10⁵ Pa flows at 3 m s⁻¹ in a pipe at ground level. The pipe rises 5 m and its area halves. Find the pressure at the upper point. (g = 10 m s⁻²)

Show solution
  1. Continuity: v₂ = 6 m s⁻¹.
  2. \(P_2 = P_1 - \tfrac12\rho(v_2^2 - v_1^2) - \rho g h = 2.0\times10^5 - 500(36 - 9) - 1000(10)(5)\).
  3. \(= 200000 - 13500 - 50000 = 1.365\times10^5\) Pa.

Answer: 1.37 × 10⁵ Pa

Worked example · Pitot tube (like Q39)

A river flows at 2 m s⁻¹. An L-shaped glass tube is dipped in it with its open end facing upstream. How high above the river surface does water rise in the vertical arm? (g = 10 m s⁻²)

Show solution
  1. At the tube's mouth the water is brought to rest, so its kinetic energy per volume ½ρv² becomes extra pressure.
  2. That pressure holds a column h with ρgh = ½ρv² ⇒ h = v²/2g = 4/20 = 0.2 m.

Answer: 20 cm above the surface

From your Test-05

9.4.1 Exam

Speed of efflux: Torricelli's law

Poke holes at different heights in a plastic bottle full of water. The lowest hole squirts hardest, because it has the most water above it. But it does not necessarily throw the water farthest: a hole lower down also has less height to fall from. That trade-off is the most-asked graph and range question in this chapter.

Derivation. Apply Bernoulli between a point on the free surface (pressure P₀, speed ≈ 0 because the tank is much wider than the hole) and the hole at depth h below the surface (pressure P₀, since it opens to air, speed v):

\(P_0 + 0 + \rho g h = P_0 + \tfrac12\rho v^2 + 0 \;\Rightarrow\; v = \sqrt{2gh}\).

This is the same speed a stone gains falling freely through h. Here h is measured down from the free surface, not up from the bottom.

Speed of efflux
\[ v = \sqrt{2 g h} \]
h = depth of the hole below the free surface. Independent of the liquid's density and the hole's size.
Symbols and assumptions: v = exit speed (m/s); g = gravitational acceleration (m/s²); h = vertical depth of the hole below the free surface (m). Both surface and exit are at the same pressure; the tank area is much larger than the hole area and losses are neglected.
Extra pressure on the surface (closed tank, piston, load)
\[ v = \sqrt{2gh + \frac{2(P - P_0)}{\rho}} \]
An extra pressure ΔP on the surface adds ΔP/ρg to the effective head (Test-05 Q35).
Symbols and assumptions: v = exit speed (m/s); h = hole depth below the free surface (m); P = pressure on the liquid surface (Pa); P₀ = pressure outside the hole (Pa); ρ = liquid density (kg/m³); g = gravitational acceleration (m/s²). A piston load M adds Mg/A to surface pressure, with M its mass and A the piston area.
Horizontal range on the ground
\[ R = v\sqrt{\frac{2y}{g}} = 2\sqrt{h\,y} = 2\sqrt{h(H-h)} \]
h = depth below surface, y = height of hole above the ground, H = h + y (liquid surface above the ground). Maximum R = H when h = y = H/2. Holes at depth h and at depth H − h give the same range.
Symbols and assumptions: R = horizontal range (m); v = horizontal exit speed (m/s); y = hole height above the landing level (m); h = hole depth below the liquid surface (m); H = surface height above the landing level (m), so y = H − h; g = gravitational acceleration (m/s²). Air resistance and changes in surface height during flight are neglected.
Time to empty (hole at the bottom)
\[ t = \frac{A}{a}\sqrt{\frac{2H}{g}} \;\propto\; \sqrt{H} \]
A = tank area, a = hole area. From H₁ to H₂: \( t = \frac{A}{a}\sqrt{\frac{2}{g}}\,(\sqrt{H_1} - \sqrt{H_2}) \). The first half of the height drains in only 29% of the total time.
Symbols and assumptions: t = emptying time (s); A = constant tank cross-sectional area (m²); a = hole area (m²); H = initial water depth (m); g = gravitational acceleration (m/s²). The hole is small compared with the tank and viscous/contraction losses are neglected.
Thrust (reaction) of the jet
\[ F = \rho a v^2 = 2\rho a g h \]
Momentum per second carried out by the jet. This is twice the hydrostatic force ρgh·a on a plugged hole. Two holes on opposite walls at depths h₁, h₂: net force 2ρag(h₂ − h₁) (Q40).
Symbols and assumptions: F = horizontal reaction-force magnitude (N); ρ = liquid density (kg/m³); a = hole area (m²); v = exit speed (m/s); g = gravitational acceleration (m/s²); h = hole depth below the surface (m). The second form uses v² = 2gh.
Interactive

Water jet from a hole: speed, range and the mirror hole

Mirror hole
Depth below surface–
Efflux speed v–
Range R–
Best possible–

Slide the hole to 50% of H: the jet lands on the green "max" mark and R = H. Turn on the mirror hole: a hole as far above the middle as yours is below it lands at exactly the same spot. Add top pressure: every jet speeds up and the best hole moves higher.

√2gH v H hole height y above bottom
Test-05 Q37: v = √(2g(H − y)) falls as the hole is raised, curving down to zero at y = H.
H R H/2 H
R = 2√(y(H − y)) is symmetric about H/2 (maximum R = H there). The purple pair are mirror holes with equal range.
Exam traps · your Test-05 Q30, Q31
  • Maximum range needs the hole at half the height of the liquid surface above the ground (Q30). If the tank stands on a block, measure H from the ground, not from the tank's base.
  • Time to empty ∝ √H, not ∝ H (Q31). Four times the height takes twice the time. The outflow slows down as the level falls.
  • v = √(2gh) uses depth below the surface. If a question gives the hole's height above the base, use h = H − y.
Worked example · Range (like Q34)

A tank stands on a platform. A small hole in its side is 45 cm below the water surface and 80 cm above the ground. How far from the tank does the jet hit the ground?

Show solution
  1. \(R = 2\sqrt{h y} = 2\sqrt{45 \times 80} = 2\sqrt{3600} = 120\) cm.
  2. Q34 is the same shape: hole 70 cm below the surface and 140 cm above the ground → \(2\sqrt{70\times140} = 140\sqrt2\) cm.

Answer: 120 cm = 1.2 m

Worked example · Extra pressure (like Q35)

A tank of water has a hole 0.8 m below the surface. A piston resting on the water adds a pressure of 10⁴ Pa. Find the efflux speed. (g = 10 m s⁻²)

Show solution
  1. \(\tfrac12\rho v^2 = \Delta P + \rho g h\) ⇒ \(v^2 = 2(\Delta P/\rho + gh) = 2(10 + 8) = 36\).
  2. \(v = 6\) m s⁻¹. (Without the piston it would be √16 = 4 m s⁻¹.)

Answer: 6 m s⁻¹

Worked example · Time and ratio (like Q31)

A tank of area 1 m² holds water 5 m deep and drains through a hole of area 10 cm² at its bottom. (a) How long does it take to empty? (b) How long to drain from 5 m to 1.25 m? (g = 10 m s⁻²)

Show solution
  1. (a) \(A/a = 1/10^{-3} = 1000\). \(t = 1000\sqrt{2\times5/10} = 1000\) s.
  2. (b) \(t = 1000\sqrt{2/10}\,(\sqrt5 - \sqrt{1.25}) = 1000 \times 0.447 \times 1.118 = 500\) s.
  3. So three-quarters of the height drains in half the time, and the last 1.25 m takes the other 500 s.

Answer: (a) 1000 s; (b) 500 s

From your Test-05 (all seven efflux questions)

★ Coaching topic Exam

The venturimeter

How do you measure how much water flows through a pipe each second without putting anything in its way? Narrow the pipe smoothly to a throat and back again. In the throat the water speeds up (continuity), so its pressure drops (Bernoulli). Measure that pressure drop with a manometer and you can calculate the flow rate. That device is a venturimeter, and it uses both laws together.

Two equations, two unknowns
\[ A_1v_1 = A_2v_2, \qquad P_1 - P_2 = \tfrac12\rho\,(v_2^2 - v_1^2) \]
Substitute v₂ = v₁A₁/A₂ into Bernoulli and solve for v₁.
Symbols and assumptions: A₁, A₂ = pipe areas (m²); v₁, v₂ = flow speeds (m/s); P₁, P₂ = pressures (Pa); ρ = liquid density (kg/m³). The sections are horizontal and the flow is ideal, steady and incompressible.
Venturimeter result
\[ v_1 = \sqrt{\frac{2\,\Delta P}{\rho\left[(A_1/A_2)^2 - 1\right]}}, \qquad Q = A_1 v_1 = A_1A_2\sqrt{\frac{2\,\Delta P}{\rho\,(A_1^2 - A_2^2)}} \]
ΔP = P₁ − P₂. With vertical tubes of the same liquid, ΔP = ρgΔh. With a U-tube manometer holding a heavier liquid ρ_m (e.g. mercury under water), ΔP = (ρ_m − ρ)gh.
Symbols and assumptions: v₁ = speed in the wider section (m/s); A₁ = wider area and A₂ = throat area (m²), with A₁ > A₂; ΔP = P₁ − P₂ (Pa), positive; ρ = liquid density (kg/m³); Q = volume flow rate (m³/s). The pressure difference is measured at equal elevation.
Interactive

Venturimeter: the column over the throat drops

Third tube
Throat speed v₂–
Δh (columns 1 − 2)–
P₁ − P₂ = ρgΔh–
Flow Q (A₁ = 20 cm²)–
Pitot rise v₁²/2g–

Columns 1 and 3 stand at the same height (same area, same speed, no friction). The throat column drops by (v₂² − v₁²)/2g. Push the flow high enough and the throat pressure goes below atmospheric, so air or liquid would be sucked in. That is how sprayers, perfume atomisers, carburettors and Bunsen burners work. Switch on the pitot tube to see the extra v²/2g.

How it is asked
  • "A venturimeter works on the principle of …" → Bernoulli's theorem (together with continuity) (Test-05 Q20).
  • Given A₁, A₂ and the pressure difference (or Δh), find Q. Convert cm² → m² (× 10⁻⁴) before using the formula, then convert back.
  • Ratio form: if Δh is made 4 times larger, Q doubles (Q ∝ √Δh).
Worked example · Numerical (like Q26)

Water flows through a horizontal pipe of cross-section 20 cm² that narrows to 10 cm². The pressure difference between the two sections is 60 Pa. Find the volume flow rate.

Show solution
  1. A₁ = 2 × 10⁻³ m², A₂ = 1 × 10⁻³ m², A₁² − A₂² = 3 × 10⁻⁶ m⁴.
  2. \(Q = A_1A_2\sqrt{\dfrac{2\Delta P}{\rho(A_1^2 - A_2^2)}} = 2\times10^{-6}\sqrt{\dfrac{120}{1000\times3\times10^{-6}}} = 2\times10^{-6}\times200\).
  3. Q = 4 × 10⁻⁴ m³ s⁻¹ = 400 cm³ s⁻¹. (For Q26's 15 Pa, the root is √10⁴ = 100, giving 200 cm³ s⁻¹.)

Answer: 400 cm³ s⁻¹

Worked example · Manometer heights

In a venturimeter (A₁ = 10 cm², A₂ = 5 cm²) carrying water, the vertical tubes over the wide part and the throat differ in height by 15 cm. Find v₁, v₂ and Q. (g = 10 m s⁻²)

Show solution
  1. ΔP = ρgΔh = 1000 × 10 × 0.15 = 1500 Pa. Area ratio = 2.
  2. \(v_1 = \sqrt{\dfrac{2\times1500}{1000\,(4 - 1)}} = 1\) m s⁻¹, so v₂ = 2 m s⁻¹.
  3. Q = A₁v₁ = 10⁻³ m³ s⁻¹ = 1000 cm³ s⁻¹ (1 litre per second).
  4. Check: ½ρ(v₂² − v₁²) = 500 × 3 = 1500 Pa. ✓

Answer: 1 m s⁻¹, 2 m s⁻¹, 1 L s⁻¹

From your Test-05

9.4.2 Core

Dynamic lift and the Magnus effect

Aeroplanes, spinning cricket balls and a roof lifted by a storm all involve a pressure difference created by moving air. Start with the pressure: a surface feels a greater push from the side at higher pressure. In the ideal, horizontal-flow model, Bernoulli relates that difference to the air speeds.

For speeds \(v_\text{top}\) and \(v_\text{bottom}\), measured relative to the wing, subtract the two Bernoulli equations using the same upstream conditions. Faster flow over the top gives lower pressure there, so the bottom pushes up more strongly than the top pushes down.

Uniform-pressure approximation for a wing
\[P_\text{bottom}-P_\text{top}=\frac12\rho(v_\text{top}^{2}-v_\text{bottom}^{2}),\qquad F_\text{lift}=\Delta P\,A\]
ρ is the air density; A is the effective wing area. Positive F means upward lift. A real wing has a varying pressure distribution, so its total force is found by adding pressure forces over the surface.
Symbols and assumptions: P_bottom, P_top = air pressures below/above the wing (Pa); v_top, v_bottom = air speeds relative to the wing (m/s); ρ = air density (kg/m³); ΔP = P_bottom − P_top; A = effective wing area (m²); F_lift = signed upward lift (N).
Interactive

Pressure lift and a spinning ball

P below − P above–
Signed lift–

Make the two wing speeds equal: the model gives zero lift. Reverse their order: the force reverses. In spinning-ball mode, reversing spin reverses the sideways force; spin strength is illustrative, not a calibrated angular speed.

Why a spinning ball curves: the Magnus effect

View a moving ball in its own frame: air flows past it. Viscosity couples nearby air to its rotating surface. Spin changes the flow around opposite sides and makes the pressure distribution asymmetric. The resulting force is transverse to the ball's motion, bending its path. Reverse the spin while keeping the motion the same and the deflection reverses.

In the model above, air travels left to right and the ball moves left relative to the air. When its top surface moves with the air, the faster upper flow corresponds to lower pressure and an upward force. With the opposite spin, the faster side and force reverse. Always draw the relative airflow and rotation before deciding the direction.

Avoid the equal-transit-time story

Air parcels separated at the front of a wing do not have to meet at the trailing edge. A longer upper path alone does not establish the speed. Wing shape and angle of attack create the flow and pressure distribution; the wing also deflects air downward. Bernoulli and momentum conservation describe compatible parts of the same lift process. NASA explains both views of lift.

Level flight and a small difference in air speeds

For steady level flight, the vertical lift balances aircraft weight Mg, where M is its mass in kg and g is gravitational acceleration. If the lower airflow speed is v and the upper speed is v + δv, then \(\Delta P=\tfrac12\rho[(v+\delta v)^2-v^2]=\rho v\delta v+\tfrac12\rho(\delta v)^2\).

If δv is much smaller than v, neglect the squared term and use \(Mg=\Delta P A\). This gives the fractional increase \(\delta v/v\approx Mg/(\rho Av^2)\). Here δv is the speed difference in m/s, v is the lower speed in m/s, ρ is air density in kg/m³ and A is effective wing area in m². For Test-05 Q23, 900 km/h = 250 m/s, so the fraction is 0.064, about 6.4%. Without the small-difference approximation, solve \(\delta v/v=\sqrt{1+2Mg/(\rho Av^2)}-1\), which gives about 6.2%.

Storm roofs, atomisers and useful limits

If air inside a building is approximately at rest while air rushes across its roof, outside pressure can fall below inside pressure. The estimated upward force is \(F=\tfrac12\rho v^2A\). If the wind speed doubles, this ideal estimate grows fourfold.

An atomiser uses a fast stream to lower pressure near a tube opening. Higher pressure over the liquid reservoir then pushes liquid up the tube. We often say the liquid is “sucked up”, but the pressure difference is what moves it.

Worked example · Wing

Air of density 1.2 kg/m³ moves at 70 m/s above a wing and 60 m/s below it. For an effective area of 20 m², estimate lift.

Show solution
  1. \(\Delta P=\tfrac12(1.2)(70^2-60^2)=780\) Pa.
  2. \(F=780\times20=15600\) N upward.
  3. For level flight in this simplified model, this balances a weight of 15600 N; it is not a prediction of lift for every wing of that area.

15.6 kN upward

Worked example · Roof

A wind of 20 m/s blows over a 50 m² roof. Air inside is nearly still, and air density is 1.2 kg/m³. Estimate the upward force.

Show solution
  1. \(\Delta P=\tfrac12(1.2)(20^2)=240\) Pa.
  2. \(F=240\times50=12000\) N, upward because the indoor pressure is greater.

12 kN upward

From your Test-05

★ Coaching extra

Liquids in accelerating containers

Water in a bus rises at the rear when the bus accelerates forward. The liquid is at rest relative to the bus after settling, but the bus frame is accelerating. In that frame include an inertial force opposite the acceleration: the effective gravity is \(\boldsymbol g_\text{eff}=\boldsymbol g-\boldsymbol a\).

The pressure increases in the direction of effective gravity. The free surface is perpendicular to it, since points on that surface are at the same atmospheric pressure. For horizontal acceleration, the surface is no longer horizontal.

Horizontal acceleration
\[\tan\theta=\frac{|a|}{g},\qquad |\Delta h|=\frac{|a|\ell}{g}\]
θ is the tilt from horizontal; ℓ is the horizontal tank length. The rear side is higher, assuming enough liquid and no spilling.
Symbols and assumptions: a = signed horizontal tank acceleration (m/s²); g = gravitational acceleration (m/s²); θ = free-surface tilt from horizontal; ℓ = horizontal tank length (m); Δh = surface-height difference across that length (m). Absolute values give magnitudes.
Vertical acceleration
\[P-P_0=\rho(g+a)h,\qquad F_B=\rho_\ell V_\text{sub}(g+a)\]
Here a is signed positive upward. For downward acceleration of magnitude a, replace g+a with g−a.
Symbols and assumptions: P = absolute pressure at depth h (Pa); P₀ = surface pressure (Pa); ρ or ρ_l = liquid density (kg/m³); g = gravitational acceleration (m/s²); a = signed lift acceleration, positive upward (m/s²); h = vertical depth (m); F_B = buoyancy (N); V_sub = submerged volume (m³).
Interactive

Effective gravity and the free surface

Surface tilt–
Rise difference across 1 m–

Positive horizontal acceleration means right; positive vertical acceleration means up. The surface drawing is schematic. In vertical free fall (a = −9.8 m/s²), the gravity-driven pressure gradient and buoyancy vanish; the model omits surface-tension effects.

Floating fraction and free fall

For nonzero effective gravity, both weight and buoyancy scale by the same factor, so \(V_\text{sub}/V=\rho_\text{body}/\rho_\ell\) stays unchanged in a vertical lift. At free fall both become zero: the equation becomes 0 = 0 and no longer selects a floating fraction. Do not cancel zero and claim ordinary floating equilibrium.

Worked example · Bus tank

A 1 m long tank accelerates horizontally at 4.9 m/s². Find the surface tilt and the level difference, taking g = 9.8 m/s².

Show solution
  1. \(\tan\theta=4.9/9.8=0.5\), hence \(\theta\approx26.6^\circ\).
  2. \(\Delta h=a\ell/g=0.5\) m; the rear level is higher.

26.6°; 50 cm

Check your understanding

★ Exam

Problem patterns and shortcuts

1 · Pressure and connected liquids

Begin at a surface of known pressure. Going down adds ρgΔh; going up subtracts it. At a horizontal level in the same connected liquid, match pressures. Use gauge pressure for a net force when atmospheric pressure acts on both sides.

2 · Floating and a change in water level

For floating, displaced liquid weight equals body weight. A floating object's displacement is m/ρₗ; a fully submerged object's is its own volume. Compare displaced volumes before and after moving an object; do not compare its weight with its volume.

3 · A hydraulic machine

Use F₁/A₁ = F₂/A₂, then A₁x₁ = A₂x₂. Diameter ratio d₂/d₁ must be squared to get the force ratio. Force is multiplied at the cost of distance; an ideal lift does not multiply work.

4 · Pipes, branches and pressure

Find speeds from mass conservation first: ρAv is constant, or Av for an incompressible fluid. Then apply Bernoulli between two chosen points. Keep height and speed changes separate; a narrower section is not automatically at lower pressure if its height or pump input also changes.

5 · Efflux, flight time and range

Distinguish depth h below the liquid surface from hole height y above the landing plane. For an open tank with surface height H: v = √(2gh), t = √(2y/g), R = 2√(hy), h + y = H. Maximum R is H for h = y = H/2. Equal-range holes are symmetric about the midpoint.

6 · Venturimeter and Pitot tube

A venturimeter combines continuity with the static-pressure difference. For two open piezometer tubes carrying the same liquid, ΔP = ρgΔh. A Pitot tube instead measures stagnation minus static pressure, ΔP = ½ρv². With a different manometer liquid, derive its pressure balance before substituting a height.

7 · Lift, wind and jets

Wing or roof: F = ΔPA, with ΔP from the squared speed difference in the stated ideal model. Jet stopping normally on a wall: force = mass flow rate × speed = ρAv². The jet formula comes from momentum conservation; it is not the same pressure calculation.

8 · An accelerating vessel

Use the vessel frame and gₑff = g − a as vectors. For a horizontal acceleration, tan θ = |a|/g. For a lift, replace g by g+a or g−a in pressure and buoyancy. Treat free fall separately.

Worked example · Jet thrust

A water jet of cross-section 2 cm² hits a fixed flat wall normally at 10 m/s and flows sideways afterwards. Find the force on the wall (ρ = 1000 kg/m³).

Show solution
  1. \(A=2\times10^{-4}\) m² and \(\dot m=\rho Av=2\) kg/s.
  2. The normal speed changes from 10 m/s to zero: \(F=\dot m\,v=20\) N.
  3. If the jet were reversed completely at the same speed, the normal momentum change would double; here it merely loses its normal component.

20 N

★ Exam

Night-before checklist

  • Pressure: P = P₀ + ρgh; it depends on depth and density, not container shape. Gauge pressure is P−P₀.
  • Manometer: walk through the columns, adding pressure downward and subtracting upward. Heights belong to their own liquid densities.
  • Pascal: F/A is transmitted; diameter ratio squared gives force ratio. A₁x₁ = A₂x₂.
  • Buoyancy: Fᵦ = ρₗVsubg; for floating, Vsub/V = ρbody/ρₗ. An object's whole volume is not always displaced.
  • Continuity conserves mass: ρAv; for incompressible flow Av is constant. Halving diameter makes speed four times larger.
  • Bernoulli conserves mechanical energy in ideal steady flow: P + ½ρv² + ρgh. Each term is in Pa.
  • Along one streamline, irrotational flow is not required; irrotational flow permits the same Bernoulli constant across different streamlines. Real viscous flow loses mechanical energy.
  • Efflux: v = √(2gh) only for the stated open-tank approximation. Both surfaces are at atmospheric pressure; h is depth below the surface.
  • Range uses the hole's height above the landing plane. For an open tank, Rmax = H at half-depth; complementary depths give equal range.
  • Venturimeter: derive speed from continuity and static-pressure difference. Pitot: stagnation−static = ½ρv².
  • Lift: faster upper air can mean lower upper pressure; F = ΔPA. Opposite spin reverses the Magnus effect.
  • Acceleration: use effective gravity; the rear surface rises during forward acceleration. In free fall, gravity-driven buoyancy vanishes.

Quick formula reference

QuantityFormulaCondition / unit
Hydrostatic pressure\(P-P_0=\rho gh\)Constant density; Pa
Buoyancy\(F_B=\rho_\ell V_\text{sub}g\)N
Volume flow rate\(Q=Av\)m³/s; v is mean speed
Bernoulli\(P+\tfrac12\rho v^2+\rho gz=\text{const}\)Pa; along a streamline
Efflux speed\(v=\sqrt{2gh+2\Delta P/\rho}\)Large reservoir; m/s
Jet range, open tank\(R=2\sqrt{h(H-h)}\)Landing at base level; m
Time to drain an open tank\(t=(A/a)\sqrt{2H/g}\)Constant tank area A, small hole a; s
Lift estimate\(F=\tfrac12\rho(v_t^2-v_b^2)A\)N; effective uniform pressure
Jet stopped by a wall\(F=\rho Av^2\)N; normal incidence

Practise the complete Fluids I set · Review formulas