Step 1: Understanding the Power-Flow Rate Relationship
- Power \( P \) required to maintain the flow of an incompressible fluid is given by: \[ P \propto Q^3 \] where \( Q \) is the volumetric flow rate.
Step 2: Effect of Doubling Flow Rate
- If the flow rate is doubled: \[ Q' = 2Q \] - New power required: \[ P' = (2Q)^3 = 8P \]
Step 3: Increase in Power
\[ \text{Increase in power} = P' - P = 8P - P = 7P \] \[ \text{Percentage increase} = \frac{7P}{P} \times 100 = 700\% \]
Step 4: Conclusion
Since the power increase is 700\%, Option (3) 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?