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

doi:10.2514/2.1406

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

Department of Mechanical Engineering

Research output: Contribution to journal › Article › peer-review

38 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 language	English
Pages (from-to)	972-974
Number of pages	3
Journal	AIAA Journal
Volume	39
Issue number	5
DOIs	https://doi.org/10.2514/2.1406
State	Published - 1 Jan 2001

ASJC Scopus subject areas

Aerospace Engineering

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title = "Flow-Mach-number-variation-induced hysteresis in steady shock wave reflections",

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.",

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AU - Ivanov, M. S.

AU - Ben-Dor, G.

AU - Elperin, T.

AU - Kudryavtsev, A. N.

AU - Khotyanovsky, D. V.

PY - 2001/1/1

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AB - 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.

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

Abstract

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