When Mach number is less than unity, the flow is called-
Sub-sonic flow
Therefore, when the Mach number is less than unity, the flow is called Sub-sonic flow. Mach Number (M) Flow Type Characteristics M < 1 Sub-sonic Speed less than sound; pressure waves move upstream M = 1 Sonic Speed equals sound; critical condition 1 < M < \approx 5 Super-sonic Speed greater than sound; shock waves form M > \approx 5 Hyper-sonic Very high speed; significant heating effects Conclusion Based on the definition and classification of flow regimes by Mach number, a flow with a Mach number less than unity (M < 1) is known as Sub-sonic flow.
Match the following and select the correct answer from the codes given below the lists
List I | List II | ||
A. | Steam Nozzle | 1. | Mach number |
B. | Compressible flow | 2. | Reaction turbine |
C. | Surface Tension | 3. | Biot number |
D. | Heat conduction | 4. | Nusselt number |
5. | Supersaturation | ||
6. | Weber number | ||
The Reynold’s number, used for critical velocity for turbulent flow of fluids, is given by the relation
Reynolds number for non - circular cross-section is:
[V = mean velocity, ν = kinematic viscosity, P = ratio of cross-sectional area to the wetted perimeter]
A) \(V.\frac{{4P}}{v}\)
B) \(\frac{{V.P}}{v}\)
C) \(\frac{{V.2P}}{{4v}}\)
D) \(\frac{{V.P}}{{4v}}\)
When the Mach number is less than unity, the flow is
The only possible dimensionless group that combines velocity ‘V’, body size ‘L’, fluid density ‘ρ’ & surface tension ‘σ’