TY - GEN
T1 - Fully conservative scheme for multi-component flows satisfying pressure equilibrium
AU - Fujiwara, Yuji
AU - Tamaki, Yoshiharu
AU - Kawai, Soshi
N1 - Funding Information:
This work was supported in part by Japan Society for the Promotion of Science (JSPS) KAKENHI Grant Number JP19K21927.
Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc.. All rights reserved.
PY - 2022
Y1 - 2022
N2 - 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.
AB - 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.
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U2 - 10.2514/6.2022-1052
DO - 10.2514/6.2022-1052
M3 - Conference contribution
AN - SCOPUS:85123383333
SN - 9781624106316
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
BT - AIAA SciTech Forum 2022
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Y2 - 3 January 2022 through 7 January 2022
ER -