The discharge through a converging - diverging nozzle reaches its maxi...
Convergent - Divergent nozzles are used to increase the flow of gas to supersonic speeds (as in the case of rockets). Their cross - sectional area first decreases and then increases. The area where the diameter is minimum is called the throat.
As the gas enters the converging section, its velocity increases, considering the mass flow rate to be constant. As the gas passes through the throat, it attains sonic velocity (mach number = 1). As the gas passes through the divergent nozzle, the velocity increases to supersonic (mach number >1)
The flow rate is maximum for a given nozzle if flow is sonic at the throat. This condition is achieved by managing the back pressure.
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The discharge through a converging - diverging nozzle reaches its maxi...
Explanation:
A converging-diverging nozzle is a device that converts the energy of a fluid into kinetic energy by accelerating it to high velocities. This device consists of two sections, a converging section where the cross-sectional area decreases and a diverging section where the cross-sectional area increases.
The velocity of the fluid increases in the converging section due to the reduction in the cross-sectional area. As the fluid reaches the throat, the cross-sectional area is at its minimum and the velocity is at its maximum, according to the principle of continuity. The fluid then expands in the diverging section, which causes a decrease in velocity and an increase in pressure.
The maximum discharge through a converging-diverging nozzle occurs when the flow is sonic at the throat. This means that the velocity of the fluid at the throat is equal to the speed of sound in the fluid. When the flow is sonic at the throat, the pressure at the exit is equal to the ambient pressure, which is the pressure outside the nozzle.
The reason for this is that the pressure at the exit is determined by the velocity of the fluid, which in turn is determined by the pressure and temperature at the throat. If the pressure at the exit is higher than the ambient pressure, the fluid will be slowed down and compressed, which reduces the mass flow rate. If the pressure at the exit is lower than the ambient pressure, the fluid will expand and create a shock wave, which also reduces the mass flow rate. Therefore, the maximum discharge occurs when the pressure at the exit is equal to the ambient pressure.
In conclusion, the maximum discharge through a converging-diverging nozzle occurs when the flow is sonic at the throat because it ensures that the pressure at the exit is equal to the ambient pressure.
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