Step 1: Mach number definition.
\(M=\dfrac{V}{a}\), with speed of sound \(a=\sqrt{\gamma R T}\).
Step 2: Evaluate each day.
Day 1: \(M_1=\dfrac{V_1}{\sqrt{\gamma R T_1}}\).
Day 2: \(a_2=\sqrt{\gamma R (1.2T_1)}=\sqrt{1.2}\,a_1\), and \(V_2=\sqrt{1.2}\,V_1\). Therefore \[ M_2=\frac{V_2}{a_2} =\frac{\sqrt{1.2}\,V_1}{\sqrt{1.2}\,a_1} =\frac{V_1}{a_1} =M_1. \] \[\boxed{M_2=M_1}\]
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?
