Vardaan Learning Institute
Mechanical Properties of Fluids
References
Compiled from: NCERT Physics Part-2 (Mechanical Properties of
Fluids) • H.C. Verma — Concepts of Physics Vol-1 (Ch. 13: Fluid Mechanics, Ch. 14: Some
Mechanical Properties of Matter) • D.C. Pandey — Understanding Physics: Properties of Matter
• Pradeep's Fundamental Physics XI • S.L. Arora • Cengage (B.M. Sharma) • Errorless
Physics. Target exams: Boards • JEE Main • JEE Advanced • NEET •
NDA.
1. Fluid Pressure & its Variation with Depth
A fluid (liquid or gas) cannot resist shear — it flows. At rest it exerts force only
perpendicular to any surface. Density ρ = m/V (kg/m³); relative density
(specific gravity) = ρ_substance/ρ_water (dimensionless); ρ_water = 1000 kg/m³; ρ_mercury = 13.6 × 10³
kg/m³.
Key Facts
- Pressure at a point in a static fluid is the same in all directions (that's why it
is a scalar).
- Pressure is the same at all points at the same horizontal level in a connected
fluid — the basis of every U-tube problem (hydrostatic paradox: shape/amount of vessel doesn't
matter, only depth).
- Barometer (Torricelli): P_atm = ρ_Hg g h, with h = 76 cm; the space above mercury
is a near-vacuum (Torricellian vacuum). Water barometer would need ≈ 10.3 m!
- Manometer: measures gauge pressure of a gas via the height difference of liquid
columns: P_gas = P₀ ± ρgh.
- U-tube with two liquids: equate pressures at the common interface level:
ρ₁h₁ = ρ₂h₂.
Image Placeholder — Fig. 1
Pressure vs depth, barometer, and the two-liquid U-tube (Landscape •
Background #ffffff)
AI IMAGE PROMPT: Create a three-panel physics textbook diagram in a row, LANDSCAPE
orientation (16:9), pure white background (#ffffff). PANEL 1 titled "P = P₀ + ρgh": a tall open beaker
drawn as a thin black outline filled with light blue (#e3f2fd) liquid up to a surface line labelled "P₀
(atmosphere)"; a dashed vertical dimension arrow from the surface down to a marked point labelled "depth
h"; at that point a small dot with four short red (#d32f2f) arrows pointing in all four directions,
caption "pressure same in all directions"; boxed formula "P = P₀ + ρgh (depends only on depth, not on
shape)". PANEL 2 titled "Mercury barometer": a dish of mercury (grey liquid) with an inverted closed
glass tube standing in it; mercury column risen inside the tube with the empty top region labelled
"Torricellian vacuum"; a dimension arrow along the column labelled "h = 76 cm"; equation below "P_atm =
ρ_Hg g h = 1.013 × 10⁵ Pa". PANEL 3 titled "U-tube, two liquids": a U-shaped thin black tube; the left
arm contains a taller column of light blue liquid labelled "ρ₁, height h₁" above the interface, the
right arm a shorter column of orange (#fff1e8 fill with #d9480f outline) liquid labelled "ρ₂, height
h₂"; a dashed horizontal line through the interface level labelled "same level ⟹ same pressure"; boxed
relation "ρ₁h₁ = ρ₂h₂". Style: flat minimalist vector textbook figure, thin black outlines, light-blue
and orange liquids exactly as specified, dashed reference lines, clean sans-serif labels, no gradients,
no shadows, pure white background.
Three instruments of hydrostatics — the source of every
Board's "define/derive/describe" question in this part.
Q. Find the absolute and gauge pressure at the bottom of a 10 m deep water tank. (P₀ =
1.01 × 10⁵ Pa, ρ = 1000 kg/m³, g = 10 m/s²)
Gauge: $\rho gh = 1000\times10\times10 = \mathbf{10^5 \text{
Pa}}$ (≈ 1 atm — every 10 m of water adds one atmosphere!)
Absolute: $P = 1.01\times10^5 + 10^5 = \mathbf{2.01\times10^5
\text{ Pa}}$
Q. Water is poured into one arm of a U-tube containing mercury. What height of water
column balances a 2 mm rise of mercury level difference? (Rel. density of Hg = 13.6)
Balance at interface: $\rho_wh_w = \rho_{Hg}h_{Hg} \Rightarrow
h_w = 13.6\times2 = \mathbf{27.2 \text{ mm}}$
2. Pascal's Law & Hydraulic Machines
Pascal's Law
Statement: Pressure applied to an enclosed fluid is
transmitted undiminished to every point of the fluid and to the walls of the
container.
Hydraulic lift (force multiplier): pistons of areas a (small) and A (large):
$$\frac{f}{a} = \frac{F}{A} \;\Rightarrow\; F = f\cdot\frac{A}{a}$$
Force is multiplied by A/a, but the small piston moves farther in the same
ratio ($a\,d_1 = A\,d_2$, volume conserved) — work is NOT multiplied (energy
conservation). Same principle: hydraulic brakes (equal braking effort transmitted to all wheels),
hydraulic press/jack.
Image Placeholder — Fig. 2
Hydraulic lift — force multiplication with volume balance (Landscape •
Background #ffffff)
AI IMAGE PROMPT: Create a professional physics textbook diagram, LANDSCAPE orientation
(16:9), pure white background (#ffffff). Draw a U-shaped connected vessel (thin black outline) filled
with light blue (#e3f2fd) liquid; the LEFT arm is NARROW with a small piston on top labelled "area a =
10 cm²", pushed down by a red (#d32f2f) downward arrow labelled "f = 100 N"; a small dashed
double-headed arrow beside it labelled "moves down d₁"; the RIGHT arm is WIDE with a large piston
carrying a simple car silhouette on a platform, pushed up by a green (#43a047) upward arrow labelled
"F = f·A/a = 5000 N", area labelled "A = 500 cm²", with a shorter dashed double-headed arrow "moves up
d₂ (a·d₁ = A·d₂)". Inside the liquid draw several small grey arrows along the tube pointing from the
small piston toward the large piston labelled once "pressure transmitted undiminished (Pascal's law)".
A dashed horizontal line connects the two liquid levels labelled "same pressure at same level: f/a =
F/A". BOTTOM caption: "Force multiplied ×50, distance divided ÷50 — work is conserved". Style: flat
minimalist vector textbook figure, thin black outlines, light-blue liquid, red input and green output
arrows sized very differently, dashed guides, clean sans-serif labels, no gradients, no shadows, pure
white background.
Numbers (10 cm², 500 cm², 100 N → 5000 N) form a ready
worked example.
Q. In a hydraulic lift the piston areas are 5 cm² and 500 cm². What force on the small
piston lifts a 1500 kg car? How far must it move to raise the car by 1 cm? (g = 10 m/s²)
Force: $f = F\cdot\dfrac{a}{A} = 15000\times\dfrac{5}{500} =
\mathbf{150 \text{ N}}$
Distance: $d_1 = d_2\cdot\dfrac{A}{a} = 1\times100 =
\mathbf{100 \text{ cm} = 1 \text{ m}}$ — the price of force multiplication.
3. Buoyancy, Archimedes' Principle & Floatation
Archimedes' Principle
A body wholly or partly immersed in a fluid experiences an upward
buoyant force equal to the weight of the fluid displaced: $F_B = \rho_{fluid}\,
V_{displaced}\,g$, acting through the centre of buoyancy (COM of displaced fluid). Cause: pressure is
greater on the lower surface than the upper.
- Ice floating in water melts → level UNCHANGED (it becomes exactly the water it
displaced).
- Ice containing a stone melts → level FALLS (the sunken stone
displaces only its own small volume afterwards).
- Ice containing a trapped air bubble melts → level unchanged.
- A boat carrying stones: stones thrown into the water → lake level falls (same
reasoning).
- Body floats if ρ_body ≤ ρ_fluid; a ship of steel floats because its average density
(hollow hull) is less than water's.
- Buoyant force is the same at every depth (for an incompressible fluid) — it depends on V and ρ_fl,
not on how deep the body is.
Image Placeholder — Fig. 3
Archimedes' principle: sinking, suspended and floating bodies (Landscape •
Background #ffffff)
AI IMAGE PROMPT: Create a three-panel physics textbook diagram in a row, LANDSCAPE
orientation (16:9), pure white background (#ffffff). Each panel is a beaker (thin black outline) of
light blue (#e3f2fd) water with a grey block, plus an FBD beside it with a red (#d32f2f) downward arrow
"W = ρ_body V g" and a green (#43a047) upward arrow "F_B = ρ_fl V_disp g". PANEL 1 titled "Sinks
(ρ_body > ρ_fl)": block resting at the bottom, red W arrow LONGER than green F_B; caption "apparent
weight = W − F_B > 0". PANEL 2 titled "Just suspended (ρ_body = ρ_fl)": block fully submerged floating
mid-water, arrows EQUAL; caption "W = F_B, apparent weight = 0". PANEL 3 titled "Floats (ρ_body <
ρ_fl)": block floating at the surface with a fraction below the waterline; a dashed waterline through
the block with dimension labels "submerged fraction = ρ_body/ρ_fl"; equal-length arrows W and F_B;
small iceberg note: "ice in water: 92% submerged". Style: flat minimalist vector textbook figure, thin
black outlines, light-blue water, grey blocks, red/green FBD arrows with lengths encoding the
comparison, dashed waterlines, clean sans-serif labels, no gradients, no shadows, pure white
background.
Arrow lengths = the entire sink/suspend/float logic.
Q. A block floats in water with 4/5 of its volume submerged. Find its density. In a liquid
it floats with 2/3 submerged — find that liquid's density.
Water: $\rho_{body} = \dfrac45\times1000 = \mathbf{800 \text{
kg/m}^3}$
Liquid: $\dfrac{\rho_{body}}{\rho_{liq}} = \dfrac23 \Rightarrow
\rho_{liq} = \dfrac{3}{2}\times800 = \mathbf{1200 \text{ kg/m}^3}$
Q. A metal piece weighs 210 g in air and 180 g in water. Find its relative density and the
density of a liquid in which it weighs 186 g.
RD: $\dfrac{210}{210-180} = \dfrac{210}{30} = \mathbf{7}$
Liquid: loss in liquid/loss in water = $\dfrac{24}{30} = 0.8$ →
$\rho_{liq} = \mathbf{800 \text{ kg/m}^3}$
4. Fluid Flow — Continuity Equation & Bernoulli's
Theorem
4.1 Streamline vs Turbulent Flow
- Streamline (laminar) flow: every particle passing a point follows the same path and
velocity as its predecessor; streamlines never cross (two crossing lines would mean two velocities at
one point — impossible). Speed below the critical velocity.
- Turbulent flow: above critical velocity — eddies and whorls, energy dissipated.
- Ideal fluid (for Bernoulli): incompressible, non-viscous, streamline, irrotational.
4.2 Equation of Continuity (Mass Conservation)
4.3 Bernoulli's Theorem (Full Derivation)
Statement: For streamline flow of an ideal fluid, the total energy per unit volume —
pressure + kinetic + potential — is constant along a streamline.
Derivation (work–energy on a fluid element flowing from end 1 to end 2): net work by
pressure forces = $P_1A_1v_1\Delta t - P_2A_2v_2\Delta t = (P_1 - P_2)\Delta V$. This equals the gain
in KE + PE of the transferred mass $\Delta m = \rho\Delta V$:
$$(P_1-P_2)\Delta V = \tfrac12\rho\Delta V(v_2^2 - v_1^2) + \rho\Delta V g(h_2 - h_1)$$
4.4 Applications — the Full Exam List
| Application |
Explanation in one line |
| Venturimeter |
Flow speed from the pressure drop at a constriction: $v_1 =
A_2\sqrt{\dfrac{2(P_1-P_2)}{\rho(A_1^2-A_2^2)}}$ — measures flow rate in pipes |
| Atomizer / sprayer / Bunsen burner |
Fast air over the tube lowers pressure → liquid/gas is pushed up and dragged along |
| Aerofoil (aeroplane lift) |
Air moves faster over the curved top → lower pressure above → net upward lift |
| Magnus effect (spinning ball swings) |
Spin makes air faster on one side → pressure difference curves the flight |
| Blowing over a paper / two boats colliding |
Fast stream between/above → low pressure → paper rises, boats drift together |
| Roofs blown off in storms |
Fast wind above the roof lowers pressure; higher pressure inside pushes the roof UP |
4.5 Torricelli's Theorem — Speed of Efflux
Hole at depth h below the free surface of an open tank: apply Bernoulli between surface
(v ≈ 0) and hole (both at P₀):
$$\boxed{v = \sqrt{2gh}}\ \text{— same as free fall from height h.}$$
Range of the jet (hole at height y from the ground, depth h
from surface, tank on the ground of total head H = h + y): $R = 2\sqrt{hy}$; R is
maximum = H when the hole is at the middle (h = y = H/2). Two holes at depths h and
H − h give the same range — a JEE favourite pair.
Image Placeholder — Fig. 4
Continuity + Bernoulli tube + Torricelli efflux in one master figure (Landscape
• Background #ffffff)
AI IMAGE PROMPT: Create a two-panel physics textbook diagram side by side, LANDSCAPE
orientation (16:9), pure white background (#ffffff). LEFT PANEL titled "Continuity + Bernoulli": draw a
pipe flowing left to right that starts WIDE at a lower level, rises, and becomes NARROW at a higher
level (smooth taper), outlined in black and filled light blue (#e3f2fd); at the wide inlet mark "A₁,
v₁, P₁, height h₁" with a short green (#43a047) flow arrow, at the narrow outlet mark "A₂, v₂, P₂,
height h₂" with a LONGER green flow arrow labelled "narrower ⟹ faster (A₁v₁ = A₂v₂)"; draw thin grey
streamlines inside the pipe that squeeze together in the narrow part; two small vertical pressure-gauge
tubes on the pipe with liquid columns — TALLER column on the wide section, SHORTER on the narrow one,
labelled "faster flow ⟹ lower pressure"; boxed equation below: "P + ½ρv² + ρgh = constant". RIGHT PANEL
titled "Torricelli's efflux": a tall open tank of light blue water; free surface labelled "P₀, v ≈ 0";
a small hole in the side wall at depth marked "h below surface" and height "y above ground"; from the
hole a blue parabolic jet curving to the ground with an initial horizontal green arrow labelled "v =
√(2gh)"; ground distance dimension arrow labelled "R = 2√(hy), max when hole at mid-height"; a faint
dashed second jet from the mirror depth labelled "hole at H − h: same range". Style: flat minimalist
vector textbook figure, thin black outlines, light-blue fluid, grey streamlines, green velocity arrows
with proportional lengths, dashed comparison jet, clean sans-serif labels, no gradients, no shadows,
pure white background.
Squeezed streamlines + gauge columns encode both laws; the
twin-jet shows the equal-range pair.
Q. Water flows at 2 m/s through a horizontal pipe of cross-section 8 cm², which narrows to
2 cm². Find the speed in the narrow part and the pressure drop. (ρ = 1000 kg/m³)
Continuity: $v_2 = \dfrac{A_1v_1}{A_2} = \dfrac{8\times2}{2} =
\mathbf{8 \text{ m/s}}$
Bernoulli (horizontal): $\Delta P = \tfrac12\rho(v_2^2 - v_1^2)
= 500(64-4) = \mathbf{3\times10^4 \text{ Pa}}$
Q. A tank filled to height 5 m stands on the ground. A small hole is punched 1.25 m above
the base. Find the efflux speed and the horizontal range of the jet. (g = 10 m/s²)
Depth of hole: $h = 5 - 1.25 = 3.75$ m → $v = \sqrt{2gh} =
\sqrt{75} \approx \mathbf{8.66 \text{ m/s}}$
Range: $R = 2\sqrt{hy} = 2\sqrt{3.75\times1.25} =
2\sqrt{4.6875} \approx \mathbf{4.33 \text{ m}}$
5. Viscosity — Internal Friction of Fluids
Definition
Viscosity is the property by which a fluid opposes relative
motion between its layers (internal friction). A layer drags its slower neighbour forward and is dragged
backward by it. Newton's law of viscous flow:
5.1 Stokes' Law & Terminal Velocity (Full Derivation)
Stokes' law: viscous drag on a sphere of radius r moving slowly at speed v through a
fluid of viscosity η:
$$F = 6\pi\eta rv$$
Terminal velocity: a sphere falling in a fluid accelerates until weight = buoyancy +
drag; thereafter it falls at constant $v_t$:
$$\tfrac43\pi r^3\rho g = \tfrac43\pi r^3\sigma g + 6\pi\eta rv_t$$
$$\boxed{\,v_t = \frac{2r^{2}(\rho - \sigma)g}{9\eta}\,}$$
ρ = sphere density, σ = fluid density. Note $v_t \propto r^2$ — big raindrops
fall faster; tiny cloud droplets practically float. If σ > ρ (air bubble in water), v_t is negative
— the bubble rises at terminal speed. Applications: parachute descent, millikan's
oil-drop experiment, rain reaching ground at safe speed.
5.2 Poiseuille's Formula & Reynolds Number
- Poiseuille (laminar flow through a tube): volume flow rate $Q =
\dfrac{\pi P r^{4}}{8\eta L}$ — the fierce r⁴ dependence (halve the radius → 1/16 the flow; why
slightly narrowed arteries matter so much).
- Reynolds number: $R_e = \dfrac{\rho vD}{\eta}$ (dimensionless). $R_e \lesssim 1000$:
laminar; $\gtrsim 2000$: turbulent; between: unstable. Critical velocity $v_c =
\dfrac{R_e\eta}{\rho D}$.
Image Placeholder — Fig. 5
Terminal velocity: force balance and the v–t growth curve (Landscape •
Background #ffffff)
AI IMAGE PROMPT: Create a two-panel physics textbook diagram side by side, LANDSCAPE
orientation (16:9), pure white background (#ffffff). LEFT PANEL titled "Force balance at terminal
velocity": a tall cylinder (thin black outline) filled with light blue (#e3f2fd) viscous liquid; a
small grey sphere midway down with a short black downward arrow beside it labelled "falls at constant
v_t"; FBD on the sphere: one red (#d32f2f) downward arrow "W = 4/3 πr³ρg" balanced by TWO upward
arrows stacked — a blue (#1e88e5) arrow "F_B = 4/3 πr³σg (buoyancy)" and a green (#43a047) arrow
"F_v = 6πηr v_t (Stokes drag)"; boxed result "W = F_B + F_v ⟹ v_t = 2r²(ρ − σ)g / 9η"; small note
"v_t ∝ r² — bigger drops fall faster". RIGHT PANEL titled "Approach to terminal velocity": a
first-quadrant graph, x-axis "time t", y-axis "speed v"; a blue curve rising steeply from the origin
and smoothly flattening to a horizontal dashed asymptote labelled "v_t (terminal velocity)"; annotate
the early part "a ≈ g initially" and the flat part "a = 0, net force zero". Style: flat minimalist
vector textbook figure, thin black outlines, light-blue liquid, red/blue/green FBD arrows with the two
upward arrows together matching the downward arrow's length, dashed asymptote, clean sans-serif labels,
no gradients, no shadows, pure white background.
The saturation curve is itself an exam question: "sketch v
vs t for a sphere dropped in a viscous liquid."
Q. A raindrop of radius r falls with terminal velocity 5 cm/s. Find the terminal velocity
of a drop of radius 2r. If eight such small drops coalesce into one, what is the big drop's terminal
velocity?
v_t ∝ r²: radius 2r → $v = 4\times5 = \mathbf{20 \text{
cm/s}}$
Coalescence: $8\cdot\tfrac43\pi r^3 = \tfrac43\pi R^3
\Rightarrow R = 2r$ → again $\mathbf{20 \text{ cm/s}}$ (i.e., $v \propto n^{2/3}v_0$ with n = 8).
6. Surface Tension — Complete Theory
6.1 Definition & Surface Energy
- Temperature: S decreases with rising temperature (zero at critical temperature). Hot
soup tastes better — lower S spreads it over the tongue.
- Impurities: detergents/soap lower S of water (better wetting/cleaning);
highly soluble salts raise it slightly. Camphor dances on water: it dissolves unevenly, lowering S
locally — stronger S elsewhere tugs it around.
- Examples: needle floats on water; insects walk on ponds; hair of a paintbrush cling together when
wet.
| Pair |
Angle of contact θ |
Behaviour |
| Water–clean glass |
≈ 0° (acute) |
Wets the surface; meniscus concave; liquid RISES in capillary |
| Mercury–glass |
≈ 135–140° (obtuse) |
Does not wet; meniscus convex; liquid FALLS in capillary |
| Water–waxy/lotus leaf |
Obtuse |
Water beads up (does not wet) |
θ depends only on the pair of materials (and temperature/impurities) — not on the tube's
radius or inclination. Detergents work by making θ small (better wetting); waterproofing agents make θ
large.
6.3 Excess Pressure Inside Drops & Bubbles
6.4 Capillarity (Full Derivation of the Ascent Formula)
Derivation (pressure method): in a tube of radius r, the concave meniscus has radius
$R = r/\cos\theta$. Just below the meniscus the pressure is lower than atmospheric by $2S/R$. Liquid
rises height h until $\rho gh$ restores the balance:
$$\rho gh = \frac{2S\cos\theta}{r}$$
Image Placeholder — Fig. 6
Excess pressure family + capillary rise and fall (Landscape • Background
#ffffff)
AI IMAGE PROMPT: Create a two-panel physics textbook diagram side by side, LANDSCAPE
orientation (16:9), pure white background (#ffffff). LEFT PANEL titled "Excess pressure ΔP =
2S/R or 4S/R": three circles in a row — (1) a filled light-blue circle labelled "liquid drop: 1
surface, ΔP = 2S/R"; (2) a white circle with a light-blue ring outline inside a light-blue rectangle
background labelled "air bubble in liquid: 1 surface, ΔP = 2S/R"; (3) a circle drawn with a DOUBLE
outline (two concentric close circles) labelled "soap bubble in air: 2 surfaces, ΔP = 4S/R"; below
them a small sketch of a SMALL and a LARGE soap bubble connected by a thin tube with a grey arrow
inside the tube pointing from small to large, captioned "air flows small → large (smaller bubble has
higher pressure)". RIGHT PANEL titled "Capillarity": a wide dish of light-blue water with TWO thin
vertical glass tubes standing in it — the LEFT tube shows water RISEN above the dish level with a
CONCAVE meniscus, a dimension arrow labelled "h = 2S cos θ / (rρg)" and a small angle mark at the wall
labelled "θ ≈ 0° (wets)"; the RIGHT tube stands in a separate small dish of grey mercury with the
level DEPRESSED below the dish level and a CONVEX meniscus, labelled "mercury: θ obtuse ⟹ depression";
caption below "thinner tube → higher rise (h ∝ 1/r)". Style: flat minimalist vector textbook figure,
thin black outlines, light-blue water and grey mercury, double-outline soap bubble, correct
concave/convex menisci, dimension arrows, clean sans-serif labels, no gradients, no shadows, pure
white background.
The 1-surface vs 2-surface distinction and the two menisci
are exactly what examiners check.
Q. Find the excess pressure inside (a) a water drop of radius 1 mm (S = 0.072 N/m), (b) a
soap bubble of radius 1 cm (S_soap = 0.025 N/m).
(a) Drop: $\Delta P = \dfrac{2S}{R} =
\dfrac{2\times0.072}{10^{-3}} = \mathbf{144 \text{ Pa}}$
(b) Soap bubble: $\Delta P = \dfrac{4S}{R} =
\dfrac{4\times0.025}{10^{-2}} = \mathbf{10 \text{ Pa}}$
Q. Water rises 6 cm in a capillary tube. How high will it rise in a tube of half the
radius? What happens in the original tube on the Moon (g/6)?
h ∝ 1/r: half radius → $h = \mathbf{12 \text{ cm}}$
h ∝ 1/g: on the Moon → $6\times6 = \mathbf{36 \text{ cm}}$ (if
the tube is long enough; else the meniscus flattens at the top without overflowing).
7. Solved Examples — Every Question Type in the Chapter
One worked model of each distinct question type asked from this chapter, tagged by exam.
Attempt each yourself first, then check.
Q. State and prove Bernoulli's theorem (5 marks). / Derive the terminal velocity formula
(3 marks). / Derive the capillary ascent formula (3 marks). / State Pascal's law and explain the
hydraulic lift (3 marks).
Where to answer from: Section 4.3 (work–energy derivation with
Fig. 4), Section 5.1 (three-force balance with Fig. 5), Section 6.4 (pressure method with Fig. 6),
Section 2 with Fig. 2. Always state assumptions (ideal fluid, streamline flow) for full marks.
Q. Find the net horizontal thrust on a dam wall of width w holding water to depth H.
Average gauge pressure: $\bar{P} = \dfrac{0 + \rho gH}{2}$
(linear variation).
Thrust: $F = \bar{P}\times(wH) = \mathbf{\tfrac12\rho gH^2w}$,
acting at H/3 above the base (centroid of the pressure triangle) — why dams are thick at the
bottom.
Q. A cube of density 800 kg/m³ floats at the interface of water (below) and oil of density
600 kg/m³ (above), fully submerged. What fraction of its volume is in water?
Weight = total buoyancy: $800V = 1000V_w + 600(V - V_w)$
$200V = 400V_w \Rightarrow \dfrac{V_w}{V} = \mathbf{\dfrac12}$ — half in water,
half in oil.
Q. Equal masses of two liquids of densities 2 g/cc and 3 g/cc are mixed. Find the density
of the mixture. What if equal volumes are mixed instead?
Equal masses (harmonic-type): $\rho =
\dfrac{2\rho_1\rho_2}{\rho_1+\rho_2} = \dfrac{2\times6}{5} = \mathbf{2.4 \text{ g/cc}}$
Equal volumes (arithmetic): $\rho =
\dfrac{\rho_1+\rho_2}{2} = \mathbf{2.5 \text{ g/cc}}$ — mirror of the average-speed rules!
Q. Air (ρ = 1.3 kg/m³) flows at 60 m/s over the top of a wing of area 25 m² and at 45 m/s
below it. Find the lift.
Bernoulli: $\Delta P = \tfrac12\rho(v_t^2 - v_b^2) =
0.65(3600-2025) = 1024$ Pa
Lift: $F = \Delta P\times A = 1024\times25 \approx
\mathbf{2.56\times10^4 \text{ N}}$
Q. A tank of head H = 4 m has two holes, at depths 1 m and 3 m below the surface. Compare
their jet ranges on the ground.
R = 2√(hy): hole 1: $2\sqrt{1\times3} = 2\sqrt3$; hole 2:
$2\sqrt{3\times1} = 2\sqrt3$ — equal ranges (depths h and H − h always pair up).
Max range would need the hole at 2 m: R = H = 4 m.
Q. A water drop of radius 3 mm is split into 27 identical droplets. Find the work done. (S
= 0.072 N/m)
Small radius: $r = R/n^{1/3} = 3/3 = 1$ mm.
Work = SΔA: $W = 4\pi S(27r^2 - R^2) = 4\pi(0.072)(27 -
9)\times10^{-6} = 4\pi(0.072)(18\times10^{-6}) \approx \mathbf{1.63\times10^{-5} \text{ J}}$
Q. Two soap bubbles of radii 3 cm and 4 cm coalesce in vacuum isothermally into one bubble.
Find its radius.
In vacuum, surface energy area is conserved via air content — the neat
result: $R^2 = r_1^2 + r_2^2 = 9 + 16 = 25$
R = 5 cm. (With outside pressure, use $P_0(V_1+V_2) + \ldots$ —
the vacuum case is the standard MCQ.)
Q. The radius of a tube is reduced to half while the pressure head and length stay the
same. How does the volume flow rate change?
Q ∝ r⁴: new rate $= \left(\tfrac12\right)^4 =
\mathbf{\dfrac{1}{16}}$ of the original — the r⁴ law.
Q. Water rises to height h in a capillary of radius r. Show that the surface-tension force
does work 2× the PE gained by the risen column. Where does the rest go?
Work by ST force: upward pull $2\pi rS\cos\theta$ acts through
height h: $W = 2\pi rS\cos\theta\,h = \pi r^2\rho g h^2$ (using the ascent formula).
PE gained: mass $\pi r^2h\rho$ rises to CM height h/2: $U =
\tfrac12\pi r^2\rho gh^2$ — exactly half of W.
The other half is dissipated as heat (viscous losses during the
rise) — a beautiful energy audit asked in JEE Advanced.
8. Common Mistakes & Misconceptions — Final Checklist
Night Before Exam
Read this the night before the exam:
- Pressure depends only on depth (and ρ, g) — never on the vessel's shape or the amount of liquid
(hydrostatic paradox).
- Gauge = ρgh; absolute = P₀ + ρgh. Manometers and most gauges read GAUGE pressure.
- Hydraulic machines multiply force, never work — the small piston must travel proportionally
farther.
- Buoyant force = weight of DISPLACED fluid, not of the body; it is independent of depth.
- Floating fraction = ρ_body/ρ_fluid; floating ice melting leaves the level unchanged (stone inside →
level falls).
- Continuity: narrower ⟹ faster. Bernoulli: faster ⟹ lower pressure. Chain them in that order.
- Bernoulli needs an ideal fluid along a streamline — don't apply it across turbulent or viscous
regions.
- Torricelli speed √(2gh) uses depth below the FREE SURFACE, not height above the ground; holes at h
and H − h have equal ranges.
- Terminal velocity ∝ r²; coalescing n drops: v → n^(2/3)·v.
- η of liquids falls on heating, of gases RISES — opposite behaviours.
- Poiseuille's Q ∝ r⁴ — tiny radius changes cause huge flow changes.
- Soap bubble has TWO surfaces: ΔP = 4S/R (drop: 2S/R); smaller bubble has HIGHER inside pressure —
air flows small → big.
- Capillary rise h ∝ 1/r and ∝ 1/g; a too-short tube does NOT overflow — the meniscus flattens.
- Angle of contact depends on the material pair, not on tube radius or tilt.
- Surface tension DECREASES with temperature; detergents lower it (that's the cleaning mechanism).
| Concept |
Formula |
Condition / Note |
| Pressure at depth |
$P = P_0 + \rho gh$ |
1 atm = 1.013×10⁵ Pa = 76 cm Hg |
| U-tube balance |
$\rho_1h_1 = \rho_2h_2$ |
Equate P at the same level |
| Hydraulic lift |
$F = f\,A/a$ |
$a\,d_1 = A\,d_2$ (work conserved) |
| Buoyant force |
$F_B = \rho_{fl}V_{disp}g$ |
Apparent wt = W − F_B |
| Floating fraction |
$\frac{V_{sub}}{V} = \frac{\rho_{body}}{\rho_{fl}}$ |
RD = W_air/(W_air − W_water) |
| Continuity |
$A_1v_1 = A_2v_2$ |
Falling tap stream narrows |
| Bernoulli |
$P + \tfrac12\rho v^2 + \rho gh = $ const |
Ideal fluid, along a streamline |
| Venturimeter |
$v_1 = A_2\sqrt{\frac{2\Delta P}{\rho(A_1^2-A_2^2)}}$ |
Flow-rate meter |
| Torricelli |
$v = \sqrt{2gh}$ |
Range $R = 2\sqrt{hy}$, max = H at mid-depth |
| Force on a dam |
$F = \tfrac12\rho gH^2w$ |
Acts at H/3 from the base |
| Viscous force |
$F = -\eta A\,dv/dx$ |
η: Pa·s = 10 poise |
| Stokes' law |
$F = 6\pi\eta rv$ |
Small sphere, laminar |
| Terminal velocity |
$v_t = \frac{2r^2(\rho-\sigma)g}{9\eta}$ |
∝ r²; n drops coalesce → n^{2/3}v |
| Poiseuille |
$Q = \frac{\pi Pr^4}{8\eta L}$ |
Q ∝ r⁴ |
| Reynolds number |
$R_e = \rho vD/\eta$ |
<1000 laminar, >2000 turbulent |
| Surface tension |
$S = F/L = W/\Delta A$ |
Bubble blow work = 8πR²S |
| Excess pressure |
Drop: $2S/R$; soap bubble: $4S/R$ |
Smaller bubble → higher P |
| Drop splitting |
$W = 4\pi S(nr^2 - R^2)$ |
$R = n^{1/3}r$; coalescing releases heat |
| Capillary rise |
$h = \frac{2S\cos\theta}{r\rho g}$ |
h ∝ 1/r, 1/g; short tube: meniscus flattens |
Study Plan
How to use these notes: Day 1: Sections 1–3
(pressure, Pascal, Archimedes) + Figs 1–3; drill the ice-melting cases aloud. Day 2:
Section 4 (continuity + Bernoulli + Torricelli) + Fig 4; write the Bernoulli derivation and all six
applications from memory. Day 3: Section 5 (viscosity) + Fig 5; derive v_t unaided.
Day 4: Section 6 (surface tension) + Fig 6, then all ten Types of Section 7 without
looking, followed by the mistakes checklist. Finish every session by writing the formula sheet from
memory.