Bernoulli’s Theorem

In streamline flow, the energy of a fluid particle remains constant.
Suppose that, in a tube of flow a fluid enters the cross-section A1 with velocity v1 and leave the cross-section A2 with a velocity v2. Let the pressures at A1 and A2 be P1 and P2 respectively.

Consider an element ABCD of the incompressible fluid entering the tube. In time Δt, the fluid element ABB’A’ enters the tube. The expelled fluid emerges from the tube at the other end and is denoted by DCC’D’.

Δm = ρA1v1 Δt = ρ A2v2 Δt

Work done by fluid pressure at 1 = (P1A1) v1Δt = P1 Δm/ρ

Work done by fluid pressure at 2 = − (P2A2) v2 Δt = −P2 Δm/ρ

Work done by gravity = -Δm.g. (h2 – h1)

Change in kinetic energy = $ \displaystyle \frac{1}{2}\Delta m [v_2^2 -v_1^2 ] $

Using work energy theorem, W = ΔK

$ \displaystyle P_1\frac{\Delta m}{\rho}-P_2\frac{\Delta m}{\rho} -\Delta m(h_2-h_1) = \frac{1}{2}\Delta m(v_2^2 – v_1^2)$

$ \displaystyle \frac{P_1}{\rho}+gh_1 + \frac{v_1^2}{2}= \frac{P_2}{\rho} + gh_2 + \frac{v_2^2}{2} $

$ \displaystyle P_1 + \rho gh_1 + \frac{1}{2}\rho v_1^2 = P_2 + \rho gh_2 + \frac{1}{2}\rho v_2^2 $

$ \displaystyle P + \rho gh + \frac{1}{2}\rho v^2 = Constant $

where, P = Pressure energy per unit volume = Pressure at a cross-section.

ρgh = potential energy per unit volume and

(1/2) ρv2 = kinetic energy per unit volume.

The above equation is known as Bernoulli’s equation.

Solved Example : Water flows through a tunnel from the reservoir of a dam towards the turbine installed in its power plant. The power plant is situated h m below the reservoir. If the ratio of the cross-sectional areas of the tunnel at the reservoir and power station end is η , find the speed of the water entering into the turbine.

Solution: Applying Bernoulli’s theorem at reservoir and power plant for the flowing water, we obtain,

$ \displaystyle P_0 + \rho gh_1 + \frac{1}{2}\rho v_1^2 = P_0 + \rho gh_2 + \frac{1}{2}\rho v_2^2 $

$ \displaystyle \rho gh_1 + \frac{1}{2}\rho v_1^2 = \rho gh_2 + \frac{1}{2}\rho v_2^2 $

$ \displaystyle v_2^2 = v_1^2 + 2 g(h_1 -h_2 ) $

Putting (h1 – h2) = h, we obtain

$ \displaystyle v_2 = \sqrt{ v_1^2 + 2 g h} $       …….(1)

Equation of continuity yields A1v1 = A2v2              …….(2)

Eliminating v1 from above equations , we obtain

$ \displaystyle v_2^2 = (\frac{A_2}{A_1}v_2)^2 + 2 g h $

$ \displaystyle v_2^2(1-(\frac{A_2}{A_1})^2) = 2gh $

$ \displaystyle v_2 = \sqrt{\frac{2 g h}{1-(\frac{A_2}{A_1})^2}} $

$\large \frac{A_1}{A_2} = \eta $

$ \displaystyle v_2 = \sqrt{\frac{2 g h}{1-(\frac{1}{\eta})^2}} $

$\large v_2 = \eta \sqrt{\frac{2gh}{\eta^2 – 1}}$

Also Read:

Nature of Flow
Principle of Continuity
Applications Of Bernoulli’s Theorem : Venturimeter
Velocity of Efflux
Surface Tension
Surface Energy
Excess Pressure inside a soap bubble
Angle of contact
Capillarity & Ascent Formula
Viscosity , Stoke’s Law & Terminal Velocity
Poiseuille’s formula

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