Fully conservative scheme for multi-component flows satisfying pressure equilibrium

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

In compressible flows with a non-constant ratio of specific heats (i.e., multi-component or supercritical flows), it is well-known that numerical simulation with general conservative equations generates spurious pressure oscillations. This study proposes a fully conservative scheme that satisfies the pressure equilibrium for compressible multi-component flows. The idea is the spatial discretization describes the transport of the specific heats with only the conservative governing equations and without additional equations. In contrast to the previous studies that solve non-conservative or overspecified equations, the proposed scheme preserves pressure equilibrium by solving only conservation equations for mass, momentum, total energy, and mass of species.

Original languageEnglish
Title of host publicationAIAA SciTech Forum 2022
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624106316
DOIs
Publication statusPublished - 2022
EventAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 - San Diego, United States
Duration: 2022 Jan 32022 Jan 7

Publication series

NameAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022

Conference

ConferenceAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Country/TerritoryUnited States
CitySan Diego
Period22/1/322/1/7

ASJC Scopus subject areas

  • Aerospace Engineering

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