Subsonic-Supersonic Supersonic-?

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SUMMARY

The discussion centers on the function of nozzles in transitioning from subsonic to supersonic flow, specifically in the context of Laval nozzles. Participants confirm that even in supersonic conditions, a nozzle remains beneficial for further expansion and acceleration of the flow. The optimal nozzle length is crucial, and some nozzles are designed to be extendable for varying mission profiles. Additionally, the choice of nozzle is dependent on the altitude at which the operation occurs.

PREREQUISITES
  • Understanding of fluid dynamics principles, particularly compressible flow.
  • Familiarity with Laval nozzle design and its applications.
  • Knowledge of supersonic flow characteristics and behavior.
  • Awareness of aerospace mission profiles and altitude effects on propulsion systems.
NEXT STEPS
  • Research the design and function of extendable nozzles in aerospace applications.
  • Study the impact of altitude on nozzle performance and selection for different missions.
  • Explore the principles of compressible flow in fluid dynamics.
  • Learn about the optimization of nozzle length for various flight regimes.
USEFUL FOR

Aerospace engineers, propulsion specialists, and students studying fluid dynamics or aerospace engineering who are interested in nozzle design and its implications for supersonic flight.

H_man
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Subsonic-Supersonic... Supersonic--?

Hi all,

I was just wondering.. in the case of the Laval nozzle you go from subsonic to supersonic. But once your flow is already supersonic is there any sense in having a physical nozzle (as surely there is still some divergence to the exhaust) or would it just impede flow? I am thinking about use above the atmosphere.

Cheers,

Harry
 
Engineering news on Phys.org
Thanks, that's a great website.

I now see you need different nozzles for different missions depending on the altitude.
 

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