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Supersonic Nozzle Performance Analysis by djeffal mohammed amine is a document available to read on EtoBox.

This document summarizes a research study that analyzed the influence of convergent section length and angle on the performance of supersonic nozzles through computational fluid dynamics simulations. The study found that a convergent inlet angle of 28.5 degrees produced the best results and maximum thrust force. The flow behavior inside the nozzle was complex in nature. Variations in the convergent section geometry significantly impacted pressure, velocity, and turbulent characteristics within the nozzle. O

Author

djeffal mohammed amine

Language

EN