A Hybrid Real/Ideal Gas Mixture Computational Framework to Capture Wave Propagation in Liquid Rocket Combustion Chamber Conditions

The present work focuses on the development of new mathematical and numerical tools to deal with wave propagation problems in a realistic liquid rocket chamber environment. A simplified real fluid equation of state is here derived, starting from the literature. An approximate Riemann solver is then...

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Bibliographic Details
Main Authors: Simone D’Alessandro, Marco Pizzarelli, Francesco Nasuti
Format: Article
Language:English
Published: MDPI AG 2021-09-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/8/9/250