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This document discusses different types of nozzles used in propulsion. It describes converging nozzles, which are used to accelerate subsonic flows. Converging-diverging nozzles, also known as de Laval nozzles, are needed to produce supersonic flows and were a key innovation. Real nozzle flows depart slightly from ideal models due to non-adiabatic effects and viscous dissipation. The document outlines the parameters and equations needed to model ideal nozzle flow and determine exit conditions.

Author

alim

Language

EN