The smallest section of a nozzle is known as the:
throat
A nozzle is a device that controls the direction or characteristics of a fluid flow, especially to increase its velocity as it exits the nozzle. Nozzles are used in various applications, including jet engines, rocket engines, and garden hoses.
A typical nozzle designed to accelerate fluid flow consists of different sections. These sections have varying cross-sectional areas to manage the fluid's pressure and velocity.
A common type of nozzle, particularly for compressible flow designed for acceleration (like in rockets), has three main parts:
Looking at the structure, the throat is specifically defined as the section with the smallest cross-sectional area in a nozzle that accelerates flow. The question asks for the smallest section, which directly corresponds to the definition of the throat.
The other options represent different parts:
Therefore, the smallest section of a nozzle is known as the throat.
In supersonic section of nozzle of accelerating flow the area along flow direction
In a nozzle, steam is flowing. If the back pressure is equal to the critical pressure, the mass flow rate of steam is :
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?