Implicit-explicit flux vector splitting scheme for hypersonic thermochemical nonequilibrium flows

Satoru Yamamoto, Hideo Nagatomo, Hisaaki Daiguji

Research output: Contribution to journalArticlepeer-review

3 Citations (Scopus)

Abstract

Hypersonic flows associated with chemical and thermal nonequilibrium flows must be calculated using not only ordinary mass, momentum, and energy conservation equations based on Navier-Stokes equations but also mass equations of chemical species related to chemical reactions. In this paper, an implicit-explicit flux vector splitting scheme that can be used in both explicit and implicit calculations is proposed and applied to a hypersonic thermochemical nonequilibrium flow problem. The numerical algorithm of the splitting scheme is explained, and some calculated results are shown.

Original languageEnglish
Pages (from-to)314-319
Number of pages6
JournalUnknown Journal
Issue number453
Publication statusPublished - 1995 Dec 1
EventProceedings of the 14th International Conference on Numerical Methods in Fluid Dynamics - Bangalore, India
Duration: 1994 Jul 111994 Jul 15

ASJC Scopus subject areas

  • Physics and Astronomy (miscellaneous)

Fingerprint Dive into the research topics of 'Implicit-explicit flux vector splitting scheme for hypersonic thermochemical nonequilibrium flows'. Together they form a unique fingerprint.

Cite this