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Continuity and Bernoulli's Principle

conceptmedium~45 min study8 MCQ

For steady incompressible flow, Av = constant, and P + ρ v2/2 + ρ g h = constant along a streamline.

What is Continuity and Bernoulli's Principle?

For steady incompressible flow, Av = constant, and P + ρ v2/2 + ρ g h = constant along a streamline.

Key formula / rule: Continuity: A1 v1 = A2 v2.

Key points

  • Derive Bernoulli's equation from work-energy considerations.
  • Apply continuity and Bernoulli to pipe and efflux problems.

Common exam trap

Applying Bernoulli's equation across turbulent or viscous flow.

Definitions

Term

Continuity and Bernoulli's Principle

Meaning

For steady incompressible flow, Av = constant, and P + ρ v2/2 + ρ g h = constant along a streamline.

Term

Continuity and Bernoulli's Principle — explanation

Meaning

Bernoulli's principle is energy conservation per unit volume for an ideal fluid, and explains why a faster stream has lower pressure. It applies to steady, non-viscous, incompressible, streamline flow only.

Learning objectives

  • Derive Bernoulli's equation from work-energy considerations.

  • Apply continuity and Bernoulli to pipe and efflux problems.

Formulae

Key point

Continuity: A1 v1 = A2 v2.

Key point

Bernoulli assumes steady, non-viscous, incompressible, streamline flow.

Key point

Speed rises where the cross-section narrows, so pressure falls.

Prerequisites

  • PHY-U3-MPM-T2-S1-C1

  • PHY-U1-WEP-T1-S2-C2

Common mistakes

  • Applying Bernoulli's equation across turbulent or viscous flow.

  • Comparing points that do not lie on the same streamline.

Keywords

  • Continuity

  • Bernoulli

  • Principle

Practice preview

  • Water flows horizontally through a pipe of non-uniform cross-section. At a point where the diameter is 2 cm, the velocity is 1 m/s and the pressure is 8750 Pa. What is the pressure at a point where the diameter is 1 cm?

    medium

  • A Venturi meter has a pipe diameter of 10 cm and a throat diameter of 5 cm. If the velocity of water in the pipe is 1 m/s, what is the pressure difference between the pipe and the throat? (Density of water = 1000 kg/m^3)

    medium

  • An airplane wing is designed such that the speed of air above the wing is 120 m/s and below the wing is 90 m/s. If the density of air is 1.2 kg/m^3, what is the pressure difference between the lower and upper surfaces of

    hard