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Fluid Dynamics

Fluid dynamics studies how liquids and gases flow under the action of forces. The PMDC MDCAT 2026 syllabus expects you to understand the equation of continuity, Bernoulli's principle, viscosity-driven drag, terminal velocity, and the difference between laminar and turbulent flow. Expect 1-2 MCQs from this chapter.

PMC Table of Specifications. This chapter covers five PMDC subtopics — Bernoulli's Equation, Equation of Continuity, Fluid Drag, Fluid Flow (Laminar & Turbulent), and Terminal Velocity. Each is treated below in textbook style.

Equation of Continuity

For an incompressible, non-viscous fluid flowing steadily through a pipe of varying cross-section, the mass flowing per second past every point is the same. Mathematically:

A1v1 = A2v2    (Av = constant)

Where A is the cross-sectional area and v is the speed of the fluid. This is a direct consequence of conservation of mass. Wherever the pipe narrows, the fluid must speed up; wherever it widens, the fluid slows down. The product Av is called the volume flow rate (m³/s).

Worked example

Water flows through a pipe whose radius narrows from 4 cm to 2 cm. If v1 = 2 m/s, then v2 = (A1/A2)v1 = (16/4)(2) = 8 m/s. Speed quadruples because area scales with r².

Bernoulli's Equation

For an ideal (incompressible, non-viscous, streamline) fluid, the sum of pressure energy, kinetic energy and potential energy per unit volume is constant along a streamline:

P + ½ρv² + ρgh = constant

P
Static pressure of the fluid (Pa).
½ρv²
Dynamic pressure due to fluid motion.
ρgh
Hydrostatic pressure due to height h above a reference level.

Direct consequence: where speed is high, pressure is low. This single statement explains aeroplane lift, the lift of a roof in a storm, the action of an atomiser/spray gun, the carburettor, and the Venturi meter.

Memory aid. "Faster flow → lower pressure." Aeroplane wings are shaped so that air on the upper surface travels faster than on the lower surface, producing a net upward lift.

Applications

Fluid Flow (Laminar, Turbulent)

Two distinct flow regimes occur in real fluids:

Laminar (streamline) vs Turbulent flow
PropertyLaminar / streamlineTurbulent
MotionSmooth, parallel layersChaotic, eddies and vortices
Velocity at a pointConstant in timeFluctuates rapidly
Mixing between layersNoneStrong
Energy lossLowHigh (dissipated as heat)
Reynolds number Re = ρvd/η< 1000 (transition 1000–2000)> 2000
Bernoulli applies?Yes (along a streamline)No
ExamplesSlow flow in narrow tubes, blood in capillariesSmoke from chimney, water from open tap, blood in aorta
Common trap. Bernoulli's equation strictly applies only to steady, non-viscous, incompressible, streamline (laminar) flow. Apply it to turbulent flow and your numerical answer will be wrong.

Fluid Drag

When a body moves through a fluid, it experiences a retarding force called drag. For a small spherical object moving slowly through a viscous fluid, Stokes' law gives the drag:

F = 6πηrv

where η is the coefficient of viscosity (Pa·s), r is the radius of the sphere, and v is its speed relative to the fluid. Drag rises linearly with speed at low Re, but for fast/large objects (turbulent regime) drag rises with v².

Coefficient of viscosity (η)

Viscosity is the internal friction of a fluid — resistance to shear. SI unit: Pa·s (or N·s/m²). For liquids viscosity decreases with temperature (e.g. honey thins on heating); for gases it increases with temperature.

Terminal Velocity

A body falling through a viscous fluid eventually reaches a constant speed when the net force on it is zero. At this point the weight is balanced by buoyancy plus the viscous drag. For a sphere of radius r, density ρ in a fluid of density σ:

vt = 2r²(ρ − σ)g / (9η)

Key features:

Why raindrops do not kill you

A raindrop reaches terminal velocity within metres of falling. For a 2 mm drop, vt ≈ 6–9 m/s. Without air drag a raindrop falling from 1 km would strike at >140 m/s.

Worked MCQs

Five MCQs that capture the high-yield testing patterns for this chapter.

Q1. Water flows through a pipe whose radius reduces from 4 cm to 2 cm. If the speed in the wider section is 1 m/s, the speed in the narrow section is:

  • 2 m/s
  • 4 m/s
  • 8 m/s
  • 16 m/s

By continuity A1v1 = A2v2. Areas scale with r², so A1/A2 = (4/2)² = 4, giving v2 = 4 × 1 = 4 m/s.

Q2. Bernoulli's equation is a statement of conservation of:

  • Mass
  • Momentum
  • Energy
  • Charge

P + ½ρv² + ρgh = constant expresses conservation of mechanical energy per unit volume of an ideal fluid along a streamline. Continuity, by contrast, is conservation of mass.

Q3. Stokes' drag on a small sphere of radius r moving slowly with speed v through a fluid of viscosity η is:

  • F = 4πηrv
  • F = 6πηrv
  • F = 6πηr²v
  • F = ηrv

Stokes' law: F = 6πηrv. Linear in radius and in speed; valid only at low Reynolds numbers (laminar regime).

Q4. The terminal velocity of a sphere falling through a viscous medium is doubled if:

  • Its radius is doubled
  • Its radius is increased by √2 times
  • Its mass is doubled
  • Viscosity is halved keeping radius constant only doubles it once

vt ∝ r². To double vt we need r² to double, i.e. r becomes √2 times its original value.

Q5. Which condition is NOT required for Bernoulli's equation to be applied?

  • Steady flow
  • Incompressible fluid
  • Non-viscous fluid
  • Turbulent flow

Bernoulli's equation requires laminar (streamline) flow, not turbulent. The other three conditions are essential assumptions of the derivation.

Quick Recap

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