Investigations of Chemical Nonequilibrium Two-Phase Flow in Solid Rocket Motor Nozzles

In this study, a calculation method for two-phase nonequilibrium flow in solid rocket motor nozzles is established, and an in-depth investigation into the nonequilibrium flow within the nozzle is conducted. Based on NEPE high-energy propellant, a simplified reaction mechanism model is established an...

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Autors principals:	Tianhao Feng, Wei Zhao, Yan Ba, Yanchao Zhu, Yiwen Guan, Wenjing Yang
Format:	Artigo
Idioma:	Inglês
Publicat:	MDPI AG 2026-02-01
Col·lecció:	Aerospace
Matèries:	solid rocket motor non-equilibrium flow simplified mechanism two-phase flow
Accés en línia:	https://www.mdpi.com/2226-4310/13/2/143
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