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Wednesday, October 5, 2016

Bernoulli’s Theorem

Statement:

When an incompressible and non-viscous liquid (or gas) flows in streamlined motion from one place to another, then at every point of its path the total energy per unit volume is constant.

That is
(Pressure energy/volume + Kinetic energy/volume + Potential energy/volume) = constant.

P + ½ ρv2 + ρgh = constant

Thus, Bernoulli’s theorem is in one way the principle of conservation of energy for a flowing liquid (or gas).

Bernoulli’s Equation:

Let us focus our attention on the motion of the shaded region. This is our “system”. The lower cylindrical element of fluid of length Δl1 A1 is at height y1 which moves with speed v1After some time, the leading section of our system fills the upper cylinder of fluid of length Δl2 and area A2 at height y2, and is then moving with speed v2.
A pressure force F1 acts on the lower part of the cylindrical tube towards right and pressure force F2 acts on the upper part of the cylindrical tube towards left. The net work done on the system F1 and F2 is

W = F1 Δl1 – F2 Δl2 = P1A1Δl1 – P2 A2Δl2 = (P1 – P2) ΔV

Where we have used the relations F = PA and ΔV = A1Δl1 – A2Δl2 the net effect of the motion of the system is to raise the height of the lower cylinder of mass and to change its speed. The changes in the potential and kinetic energies are

ΔU = Δmg (y2 – y1)

ΔK = ½ Δm (v22 – v21)

W = ΔU + ΔK

(P1 – P2) ΔV = Δmg (y2 – y1) + ½ Δm (v22 – v21)

 Since the density is
ρ = Δm/ΔV,
We have
P1 + ρgy1 + ½ ρv21 = P2 + ρgy2 + ½ ρv22

Since the points 1 and 2 can be chosen arbitrarily, we can express this result as Bernoulli’s Equation
P + ρgy + ½ ρv2 = constant]

It is applied to all points along a streamline in a nonviscous, incompressible and irrotational fluid.

Example:

Figure shows a liquid of density 1200 kg/m3 flowing steadily in a tube of varying cross-section. The cross-section at a point A is 1.0 cm2 and that at B is 20 mm2, the points A and B are in the same horizontal plane. The speed of the liquid at A is 10 cm/s. Calculate the difference in pressures at A and B.
Solution:

From equation of continuity, the speed V2 at B is given by,

A1V1 = A2V2 

(1.0 cm2) (10 cm/s) = (20mm2) V2

V2 = 1.0 cm2/20mm2 x 10cm/s = 50cm/s

By Bernoulli’s equation,

P1 + ρgh1 + ½ ρv21 = P2 + ρgh2 + ½ ρv22

Here h1 = h2. Thus,

P1 - P2 = ½ ρv22 - ½ ρv21

= ½ x (1200 kg/m3) (2500 cm2/s2 - 100 cm2/s2)

= 600 kg/m3 x 2400 cm2/s2 = 144 Pa

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