In a nozzle, steam is flowing. If the back pressure is equal to the critical pressure, the mass flow rate of steam is :
maximum
When steam flows through a nozzle, its velocity increases as the cross-sectional area changes, converting thermal energy into kinetic energy. The flow rate depends on the pressure difference between the inlet and the exit (back pressure).
For a given nozzle geometry and inlet steam conditions, there is a specific back pressure known as the critical pressure. The critical pressure is reached when the velocity of the fluid flow at the narrowest part of the nozzle (the throat, if it's a converging-diverging nozzle, or the exit for a converging nozzle) reaches the speed of sound (sonic velocity) for the local conditions.
As the back pressure downstream of the nozzle is gradually reduced from the inlet pressure, the pressure ratio across the nozzle increases, and the mass flow rate of steam through the nozzle also increases. This continues until the back pressure reaches the critical pressure.
Therefore, the mass flow rate of steam through a nozzle is limited by the sonic velocity condition at the throat (or exit). This limiting condition occurs when the back pressure is equal to the critical pressure. Any further reduction in back pressure does not increase the mass flow rate.
This means that the mass flow rate achieves its highest possible value when the back pressure is exactly equal to the critical pressure.
Thus, if the back pressure is equal to the critical pressure, the mass flow rate of steam is maximum.
In supersonic section of nozzle of accelerating flow the area along flow direction
The smallest section of a nozzle is known as the:
Supersaturated expansion of steam through the nozzle results in:
Mach number greater than unity implies that the flow is
Which of the following will be the result after the application of nozzle?