Step 1: Condition for closed streamline.
In source/sink flow superimposed with uniform stream, a closed streamline exists if net source strength = 0.
Step 2: Sum of given sources.
\[
q_{total} = \frac{\pi}{2} - \frac{\pi}{3} + \frac{\pi}{4} - \frac{\pi}{5}
\]
Step 3: Simplify.
Common denominator $60$:
\[
= \frac{30\pi - 20\pi + 15\pi - 12\pi}{60} = \frac{13\pi}{60}
\]
Step 4: Required additional source.
\[
q_{5} = - \frac{13\pi}{60} \approx -0.681
\]
Wait — but statement asks positive magnitude such that streamline closes. If sign convention preserved, answer = $-0.68$. Magnitude = $0.68$.
\[
\boxed{-0.68 \;\; (\text{sink})}
\]
In a low-speed airplane, a venturimeter with a 1.3:1 area ratio is used for airspeed measurement. The airplane’s maximum speed at sea level is 90 m/s. If the density of air at sea level is 1.225 kg/m³, the maximum pressure difference between the inlet and the throat of the venturimeter is __________ kPa (rounded off to two decimal places).
In a fluid flow, Mach number is an estimate of _________.
Consider a pair of point vortices with clockwise circulation \( \Gamma \) each. The distance between their centers is \( a \), as shown in the figure. Assume two-dimensional, incompressible, inviscid flow. Which one of the following options is correct?

In a low-speed airplane, a venturimeter with a 1.3:1 area ratio is used for airspeed measurement. The airplane’s maximum speed at sea level is 90 m/s. If the density of air at sea level is 1.225 kg/m³, the maximum pressure difference between the inlet and the throat of the venturimeter is __________ kPa (rounded off to two decimal places).
In a fluid flow, Mach number is an estimate of _________.
Consider a pair of point vortices with clockwise circulation \( \Gamma \) each. The distance between their centers is \( a \), as shown in the figure. Assume two-dimensional, incompressible, inviscid flow. Which one of the following options is correct?
