Mise en evidence experimentale et numerique d'un phenomene d'hysteresis lors de la transition reflexion de Mach-reflexion reguliere

A. Chpoun; D. Passerel; J. C. Lengrand; Li Haidong Li; G. Ben-Dor

Mise en evidence experimentale et numerique d'un phenomene d'hysteresis lors de la transition reflexion de Mach-reflexion reguliere

Translated title of the contribution: Numerical and experimental confirmation of a hysteresis phenomenon in the regular reflection-Mach reflection transition

A. Chpoun, D. Passerel, J. C. Lengrand, Li Haidong Li, G. Ben-Dor

Department of Mechanical Engineering

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

18 Scopus citations

Abstract

The reflection of shock waves over straight reflecting surfaces in steady flows was investigated experimentally using the hypersonic wind tunnel of Laboratoire d'Aerothermique du CNRS at Meudon in France. The results for M"SUB 0" =4.96 contradict the state of the art regarding the regular left and right arrows Mach reflection transition in steady flows. Not only was a hysteresis found to be existing in this transition, but also, unlike previous reports, regular reflection configurations were found to be stable in the dual-solution domain in which theoretically both regular and Mach reflection are possible. (from English summary)

Translated title of the contribution	Numerical and experimental confirmation of a hysteresis phenomenon in the regular reflection-Mach reflection transition
Original language	French
Pages (from-to)	1447-1453
Number of pages	7
Journal	Comptes Rendus de l Academie des Sciences Serie Il Fascicule B - Mecanique PH
Volume	319
Issue number	12
State	Published - 1 Jan 1994

ASJC Scopus subject areas

General Materials Science
General Environmental Science
General Engineering
General Earth and Planetary Sciences

Cite this

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title = "Mise en evidence experimentale et numerique d'un phenomene d'hysteresis lors de la transition reflexion de Mach-reflexion reguliere",

abstract = "The reflection of shock waves over straight reflecting surfaces in steady flows was investigated experimentally using the hypersonic wind tunnel of Laboratoire d'Aerothermique du CNRS at Meudon in France. The results for M{"}SUB 0{"} =4.96 contradict the state of the art regarding the regular left and right arrows Mach reflection transition in steady flows. Not only was a hysteresis found to be existing in this transition, but also, unlike previous reports, regular reflection configurations were found to be stable in the dual-solution domain in which theoretically both regular and Mach reflection are possible. (from English summary)",

author = "A. Chpoun and D. Passerel and Lengrand, {J. C.} and {Haidong Li}, Li and G. Ben-Dor",

year = "1994",

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Mise en evidence experimentale et numerique d'un phenomene d'hysteresis lors de la transition reflexion de Mach-reflexion reguliere. / Chpoun, A.; Passerel, D.; Lengrand, J. C. et al.
In: Comptes Rendus de l Academie des Sciences Serie Il Fascicule B - Mecanique PH, Vol. 319, No. 12, 01.01.1994, p. 1447-1453.

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

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T1 - Mise en evidence experimentale et numerique d'un phenomene d'hysteresis lors de la transition reflexion de Mach-reflexion reguliere

AU - Chpoun, A.

AU - Passerel, D.

AU - Lengrand, J. C.

AU - Haidong Li, Li

AU - Ben-Dor, G.

PY - 1994/1/1

Y1 - 1994/1/1

N2 - The reflection of shock waves over straight reflecting surfaces in steady flows was investigated experimentally using the hypersonic wind tunnel of Laboratoire d'Aerothermique du CNRS at Meudon in France. The results for M"SUB 0" =4.96 contradict the state of the art regarding the regular left and right arrows Mach reflection transition in steady flows. Not only was a hysteresis found to be existing in this transition, but also, unlike previous reports, regular reflection configurations were found to be stable in the dual-solution domain in which theoretically both regular and Mach reflection are possible. (from English summary)

AB - The reflection of shock waves over straight reflecting surfaces in steady flows was investigated experimentally using the hypersonic wind tunnel of Laboratoire d'Aerothermique du CNRS at Meudon in France. The results for M"SUB 0" =4.96 contradict the state of the art regarding the regular left and right arrows Mach reflection transition in steady flows. Not only was a hysteresis found to be existing in this transition, but also, unlike previous reports, regular reflection configurations were found to be stable in the dual-solution domain in which theoretically both regular and Mach reflection are possible. (from English summary)

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Mise en evidence experimentale et numerique d'un phenomene d'hysteresis lors de la transition reflexion de Mach-reflexion reguliere

Abstract

ASJC Scopus subject areas

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