(a) State Bernoulli’s Principle. (b) Figure below shows a liquid of density 1200kgm-3 flowing steadily in a tube of varying cross-sections. The cross- section at point A is 1.0 cm² and that at B is 20 mm², points A and B are in the same horizontal plane. The speed of the liquid at A is 10 cm/s. Calculate (i) the speed at B. (ii) the difference in pressure at A and B.

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Question:

(a) State Bernoulli’s Principle.

(b) Figure below shows a liquid of density 1200kgm-3 flowing steadily in a tube of varying cross-sections. The cross- section at point A is 1.0 cm² and that at B is 20 mm², points A and B are in the same horizontal plane. The speed of the liquid at A is 10 cm/s. Calculate:

  1. the speed at B.
  2. the difference in pressure at A and B.

Figure below shows a liquid of density 1200kgm-3 flowing steadily in a tube of varying cross-sections. The cross- section at point A is 1.0 cm² and that at B is 20 mm², points A and B are in the same horizontal plane. The speed of the liquid at A is 10 cm/s. Calculate:

Question collected form Telegram Group.

Solution:

(a) According to Bernoulli's principle, the total mechanical energy of the moving fluid, which includes gravitational potential energy of elevation, fluid pressure energy, and kinetic energy of fluid motion, remains constant.

(b) Given:

A1=1cm2

A2 = 20mm2=$\frac{1}{5}$cm2

V1=10cm/s

(i) From Equation of Contunity:

A1 V1= A2 V2

10 × 1 =$\frac{1}{5}$ × V2

Or, V2 = 50cm/s.

Thus speed at B = 50cm/s.

(ii) The difference in pressure between points A and B can be calculated using Bernoulli's equation:

$$p_1 + \frac{1}{2} \rho_1 v_1^2 = p_2 + \frac{1}{2} \rho_2 v_2^2$$

We know that $\rho_1 = \rho_2 = 1200 \text{ kg/m}^3$, $v_1 = 10 \text{ cm/s}$, and $v_2 = 50 \text{ cm/s}$. Substituting these values into Bernoulli's equation, we get:

$$p_1 + \frac{1}{2} \times 1200 \text{ kg/m}^3 \times 10 \text{ cm/s}^2 = p_2 + \frac{1}{2} \times 1200 \text{ kg/m}^3 \times 50 \text{ cm/s}^2$$

Solving for $p_2$, we get:

$$p_2 = p_1 - \frac{1}{2} \times 1200 \text{ kg/m}^3 \times (50 \text{ cm/s})^2 - \frac{1}{2} \times 1200 \text{ kg/m}^3 \times (10 \text{ cm/s})^2 = -144 \text{ Pa}$$

Therefore, the pressure at point B is 144 Pa lower than the pressure at point A.

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