A numerical study on the characteristics of hot flows in a Thrust Optimized Parabolic (TOP) nozzle is conducted. the effects of high temperature on the nozzle performance will be investigated for the Vulcain nozzle in over-expanded conditions. Particular attention is given to the Restricted Shock Separation (RSS) condition, in which recirculation and supersonic annular jets inside the nozzle can be observed. The influence of temperature and gas composition are accounted for through their effect on the thermophysical properties of the mixture, and finally through fully unsteady simulations of a chemically reacting mixture. The obtained results highlight the importance of the modeling approach for the prediction of the separation point. The value of the thrust coefficient has non-negligible variations when considering the least and most accurate models, however it may not be needed to employ a combustion model in order to obtain sufficiently accurate predictions of the thrust coefficient.

Influence of Hot Flow Conditions on Nozzle Performances / Resta, Emanuele; Marsilio, Roberto; Ferlauto, Michele. - ELETTRONICO. - (2023). (Intervento presentato al convegno AIAA SCITECH 2023 Forum tenutosi a National Harbor, MD nel 23-27 January 2023) [10.2514/6.2023-0714].

Influence of Hot Flow Conditions on Nozzle Performances

Resta, Emanuele;Marsilio, Roberto;Ferlauto, Michele
2023

Abstract

A numerical study on the characteristics of hot flows in a Thrust Optimized Parabolic (TOP) nozzle is conducted. the effects of high temperature on the nozzle performance will be investigated for the Vulcain nozzle in over-expanded conditions. Particular attention is given to the Restricted Shock Separation (RSS) condition, in which recirculation and supersonic annular jets inside the nozzle can be observed. The influence of temperature and gas composition are accounted for through their effect on the thermophysical properties of the mixture, and finally through fully unsteady simulations of a chemically reacting mixture. The obtained results highlight the importance of the modeling approach for the prediction of the separation point. The value of the thrust coefficient has non-negligible variations when considering the least and most accurate models, however it may not be needed to employ a combustion model in order to obtain sufficiently accurate predictions of the thrust coefficient.
2023
978-1-62410-699-6
File in questo prodotto:
File Dimensione Formato  
scitech2023.pdf

accesso riservato

Descrizione: postprint
Tipologia: 2. Post-print / Author's Accepted Manuscript
Licenza: Non Pubblico - Accesso privato/ristretto
Dimensione 7.05 MB
Formato Adobe PDF
7.05 MB Adobe PDF   Visualizza/Apri   Richiedi una copia
Pubblicazioni consigliate

I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.

Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11583/2975042