SONIC condition. Incoming flow initially has subsonic speed which is increased by convergent section. At throat, flow reaches the sonic speed and as it PROGRESSES further in the divergent section it further EXPANDS to SUPERSONIC speeds.

"> SONIC condition. Incoming flow initially has subsonic speed which is increased by convergent section. At throat, flow reaches the sonic speed and as it PROGRESSES further in the divergent section it further EXPANDS to SUPERSONIC speeds.

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For supersonic jet, C D nozzle is used for the acceleration of exhaust.

Aircraft Design Propulsion Jet-Engine Thrust Considerations and Turbojet Installed Thrust in Aircraft Design 3 weeks ago

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A Typical C D nozzle consists of convergent section as well as divergent section. Apart from those it also includes a throat section at where flow is in SONIC condition. Incoming flow initially has subsonic speed which is increased by convergent section. At throat, flow reaches the sonic speed and as it PROGRESSES further in the divergent section it further EXPANDS to SUPERSONIC speeds.

Posted on 26 Jun 2025, this text provides information on Aircraft Design related to Propulsion Jet-Engine Thrust Considerations and Turbojet Installed Thrust in Aircraft Design. Please note that while accuracy is prioritized, the data presented might not be entirely correct or up-to-date. This information is offered for general knowledge and informational purposes only, and should not be considered as a substitute for professional advice.

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