Step 1: Use the continuity equation.
The continuity equation for an incompressible flow is given by:
\[
A_1 v_1 = A_2 v_2
\]
Where:
- \( A_1 = \frac{\pi d_1^2}{4} \) is the cross-sectional area at the entrance,
- \( A_2 = \frac{\pi d_2^2}{4} \) is the cross-sectional area at the exit,
- \( v_1 = 3 \, \text{m/s} \) is the velocity at the entrance,
- \( d_1 = 0.25 \, \text{m} \) and \( d_2 = 0.20 \, \text{m} \) are the diameters at the entrance and exit, respectively.
Step 2: Solve for \( v_2 \).
Rearranging the continuity equation to solve for \( v_2 \):
\[
v_2 = v_1 \times \frac{A_1}{A_2} = 3 \times \frac{\left( \frac{\pi (0.25)^2}{4} \right)}{\left( \frac{\pi (0.20)^2}{4} \right)} = 3 \times \left(\frac{0.25^2}{0.20^2}\right) = 3 \times \left(\frac{0.0625}{0.04}\right) = 4.68 \, \text{m/s}
\]
Final Answer: \[ \boxed{4.68 \, \text{m/s}} \]
Which of the following statements are true?
A. The same Bernoulli's equation is applicable to all the points in the flow field if the flow is irrotational.
B. The value of "Constant in the Bernoulli's equation" is different for different streamlines if the flow is rotational.
C. When a nozzle is fitted at the end of a long pipeline, the discharge increases.
D. The velocity of flow at the nozzle end is more than that in the case of a pipe without a nozzle, the head in both cases being the same.
Choose the most appropriate answer from the options given below:
Match List-I with List-II and choose the correct answer:
Match List-I with List-II:
Who said this sentence –
Match List-I with List-II and choose the correct answer:
Match List-I with List-II and choose the correct answer: