Water flows with a flow rate of 0.5 cumecs through a pipe AB of length 12 m having a uniform cross-section. The end B of the pipe is above the end A and the pipe makes an angle of 30° to the horizontal. For a pressure of 20 kN / m2 at the end B, the corresponding pressure at the end A (in kN / m2 units) is:
78.9
This question involves calculating the pressure at the lower end (A) of an inclined pipe, given the pressure at the upper end (B), the pipe's dimensions, and the flow rate of water. We can solve this using the principles of fluid mechanics, specifically Bernoulli's equation.
Bernoulli's equation relates pressure, velocity, and elevation between two points in a flowing fluid. For points A and B, it states:
$$P_A + \frac{1}{2}\rho v_A^2 + \rho g z_A = P_B + \frac{1}{2}\rho v_B^2 + \rho g z_B$$Where:
The problem states the pipe has a uniform cross-section. This means the cross-sectional area ($A$) is constant throughout the pipe. Since the flow rate ($Q = A \times v$) is also constant, the velocity ($v$) must be the same at both ends ($v_A = v_B = v$). Therefore, the kinetic energy terms ($\frac{1}{2}\rho v^2$) cancel out:
$$P_A + \rho g z_A = P_B + \rho g z_B$$Rearranging to solve for $P_A$:
$$P_A = P_B + \rho g (z_B - z_A)$$We need to find the difference in elevation ($z_B - z_A$) between points B and A. Let's set the datum at point A, so $z_A = 0$. Point B is above A, and the pipe length is 12 m at an angle of 30° to the horizontal. The vertical height difference ($h = z_B - z_A$) is:
$$h = L \sin(\theta)$$Substituting the values:
$$h = 12 \text{ m} \times \sin(30^\circ)$$Since $\sin(30^\circ) = 0.5$:
$$h = 12 \text{ m} \times 0.5 = 6 \text{ m}$$So, the elevation difference $h$ is 6 meters.
Now, we can plug the values into the simplified Bernoulli's equation. We'll use the standard density for water, $\rho = 1000$ kg/m³, and $g = 9.81$ m/s².
First, calculate the pressure difference due to the elevation head ($\rho g h$):
$$\rho g h = (1000 \text{ kg/m³}) \times (9.81 \text{ m/s²}) \times (6 \text{ m})$$ $$\rho g h = 58860 \text{ N/m²}$$Convert this to kN/m² by dividing by 1000:
$$\rho g h = \frac{58860}{1000} \text{ kN/m²} = 58.86 \text{ kN/m²}$$Now, calculate $P_A$:
$$P_A = P_B + \rho g h$$ $$P_A = 20 \text{ kN/m²} + 58.86 \text{ kN/m²}$$ $$P_A = 78.86 \text{ kN/m²}$$The calculated pressure at end A is approximately 78.86 kN/m², which rounds to 78.9 kN/m². This matches one of the given options.
Bernoulli’s theorem applies to _________ flow.
Bernoulli's theorem deals with the principle of conservation of-
In Bernoulli’s equation \(\frac{p}{{\rho g}} + \frac{{{v^2}}}{{2g}} + z\) , each term represents:
The mathematical expression in terms of velocity (V) and acceleration due to gravity (g) for the Kinetic Head is given by ________.
Bernoulli’s theorem is applicable for