The atmospheric pressure is \( 1 \, \text{bar} \), and the vacuum pressure is \( 50 \, \text{mm of Hg} \). The absolute pressure is calculated as:
Absolute pressure = Atmospheric pressure – Vacuum pressure
\( = 1 \, \text{bar} - \frac{50 \, \text{mm of Hg}}{760 \, \text{mm of Hg}} \times 1 \, \text{bar} = 0.92 \, \text{bar}. \)
| LIST I | LIST II |
| A. Reynold’s Number | III. Inertia force to viscous force |
| B. Mach Number | I. Inertia force to elastic force |
| C. Froude’s Number | II. Inertia force to gravity force |
| D. Weber’s Number | IV. Inertia force to surface tension force |
| LIST I | LIST II |
| A. Reynold’s Number | III. Inertia force to viscous force |
| B. Mach Number | I. Inertia force to elastic force |
| C. Froude’s Number | II. Inertia force to gravity force |
| D. Weber’s Number | IV. Inertia force to surface tension force |