Step 1: The pressure at the closed end of the tube is given by: \[ P = \text{atmospheric pressure} + \text{pressure due to mercury column} \]
Step 2: When the tube is held vertically, the pressure at the closed end is \( 75 \, \text{cm} \) of mercury.
Step 3: When the tube is held horizontally, the length of the air column changes due to the balance of pressures. The total length of the column is \( L = 28 \, \text{cm} \).
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?