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Tesi etd-06092013-111023


Thesis type
Tesi di laurea specialistica
Author
BERTUCCELLI, ALESSIA, GIULIA
URN
etd-06092013-111023
Title
NUMERICAL METHODS FOR MULTICOMPONENT FLOW SIMULATIONS OF SOLID ROCKET MOTOR IGNITION
Struttura
INGEGNERIA CIVILE E INDUSTRIALE
Corso di studi
INGEGNERIA AEROSPAZIALE
Commissione
relatore Prof. Salvetti, Maria Vittoria
relatore Dott. Beux, François
Parole chiave
  • NUMERICAL METHODS
Data inizio appello
09/07/2013;
Consultabilità
parziale
Data di rilascio
09/07/2053
Riassunto analitico
In this work of thesis, the Solid Propellant Rocket Motor ignition transient simulation has been investigated. In particular, a physical model, which considered a mean gas in the combustion chamber has been modified, to introduce and consider the presence of a calorically perfect gaseous species mixture.The aim of the work has been to developed new numerical approach for the integration of conservation equations. In particular, new Roe's schemes have been developed.
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