Flow-Mach-number-variation-induced hysteresis in steady shock wave reflections

M. S. Ivanov, G. Ben-Dor, T. Elperin, A. N. Kudryavtsev, D. V. Khotyanovsky

Research output: Contribution to journalArticlepeer-review

35 Scopus citations

Abstract

Flow-mach-number-variation-induced hysteresis was studied in steady shock wave reflections. The flow between two symmetrically spaced wedges was simulated using a shock-capturing total variation diminishing (TVD) scheme. It was shown that a flow Mach number variation-induced hysteresis is possible in two-dimensional steady flows.

Original languageEnglish
Pages (from-to)972-974
Number of pages3
JournalAIAA Journal
Volume39
Issue number5
DOIs
StatePublished - 1 Jan 2001

ASJC Scopus subject areas

  • Aerospace Engineering

Fingerprint

Dive into the research topics of 'Flow-Mach-number-variation-induced hysteresis in steady shock wave reflections'. Together they form a unique fingerprint.

Cite this