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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| Hauptverfasser: | , , , , , |
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| Format: | Artigo |
| Sprache: | Inglês |
| Veröffentlicht: |
MDPI AG
2026-02-01
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| Schriftenreihe: | Aerospace |
| Schlagworte: | |
| Online-Zugang: | https://www.mdpi.com/2226-4310/13/2/143 |
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