Mechanical properties of fluids (Class 11): pressure, flow and viscosity in 3D

Fluids chapter questions come from a few ideas: pressure grows with depth, the flow of a liquid must be continuous, and speed and pressure trade off along a streamline. These labs turn each idea into something you can change and measure.

NCERT Class 11 Physics, Chapter 9 (Mechanical Properties of Fluids). Every lab below runs in 3D in your browser or on a phone, in English and Hindi.

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Pressure and the barometer

Pressure at depth h in a liquid of density ρ is P = P₀ + ρ g h. A mercury barometer is a tube closed at the top and upturned in a dish. The mercury column is held up by the atmosphere, so P₀ = ρ g H. At 101.3 kPa the height is 760 mm of mercury, but with water the column would be about 10.3 m, which is why mercury is used.

In an open U-tube manometer the difference of levels h gives the gauge pressure of the gas, P − P₀ = ρ g h. Change the liquid and the height changes in inverse proportion to its density.

  • P = P₀ + ρ g h
  • H = P₀ / (ρ g)
  • 1 atm = 760 mm Hg = 101.3 kPa

Equation of continuity: why a tap stream thins

For a steady flow of an incompressible liquid, the volume flowing past every cross-section in a second is the same: A v = constant. Water falling from a tap speeds up under gravity, v² = v₀² + 2 g y, so its cross-section must shrink. That is why the stream gets thinner as it falls.

  • A₁ v₁ = A₂ v₂
  • v = √(v₀² + 2 g y)

Bernoulli's principle and the lift on a wing

Along a streamline P + ½ ρ v² + ρ g h is constant. The air above a curved wing travels faster than the air below, so the pressure above is lower and the net upward force is the lift. The aerofoil lab shows the speeds above and below and the lift for a chosen angle of attack.

  • P + ½ ρ v² + ρ g h = constant
  • lift ≈ ½ ρ (v_top² − v_bottom²) × wing area

Viscosity and Reynolds number

Whether a flow is smooth (laminar) or irregular (turbulent) depends on the Reynolds number Re = ρ v d / η. Below about 2000 the flow is laminar, above about 4000 it is turbulent, and in between it is unstable. In the dye experiment a thin thread of dye stays straight in laminar flow and breaks into eddies when the speed is raised.

  • Re = ρ v d / η
  • Re < 2000 laminar, Re > 4000 turbulent
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Frequently asked questions

Why is mercury used in a barometer and not water?

Mercury is 13.6 times denser than water, so the column is only 76 cm tall. A water barometer would need a tube more than 10 m long.

What does the equation of continuity say?

For a steady flow of an incompressible fluid, A v is the same at every cross-section. A narrow section therefore has a faster flow.

Why does water from a tap become thinner as it falls?

Gravity increases its speed, and since A v must stay constant the cross-sectional area has to decrease.

What is the Reynolds number and what are its limits?

Re = ρ v d / η, a ratio of inertial to viscous effects. Flow in a pipe is laminar below about 2000 and turbulent above about 4000.

How does an aeroplane wing produce lift?

The shape and angle of the wing make air move faster above it. By Bernoulli's principle the pressure is lower there, so the pressure below pushes the wing up.

How do I find gas pressure with a manometer?

Measure the difference h between the two levels. The gauge pressure is ρ g h, and the absolute pressure is P₀ + ρ g h if the gas side is lower.

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