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Numerical simulation of the transonic flow past the blunted wedge in the diverging channel. / Ryabinin, Anatoly.

In: AIP Conference Proceedings, Vol. 1959, No. 050026, 02.05.2018, p. 1-5.

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Ryabinin, Anatoly. / Numerical simulation of the transonic flow past the blunted wedge in the diverging channel. In: AIP Conference Proceedings. 2018 ; Vol. 1959, No. 050026. pp. 1-5.

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@article{51f4213e9dba49b0a0a58d73360193b1,
title = "Numerical simulation of the transonic flow past the blunted wedge in the diverging channel",
abstract = "Positions of shock waves in the 2D channel with a blunted wedge are studied numerically. Solutions of the Euler equations are obtained with finite-volume solver SU2 for 15 variants of channel geometry. Numerical simulations reveal a considerable hysteresis in the shock wave position versus the supersonic Mach number given at the inlet. In the certain range of inlet Mach number, there are asymmetrical solutions of the equations. Small change in the geometry of the channel leads to shift of boundaries of the hysteresis range.",
keywords = "SHOCK-WAVE BIFURCATION",
author = "Anatoly Ryabinin",
year = "2018",
month = may,
day = "2",
doi = "10.1063/1.5034654",
language = "English",
volume = "1959",
pages = "1--5",
journal = "AIP Conference Proceedings",
issn = "0094-243X",
publisher = "American Institute of Physics",
number = "050026",
note = "International Scientific Conference on Mechanics - Eighth Polyakhov's Reading : 8th Polyakhov's Reading ; Conference date: 29-01-2018 Through 02-02-2018",
url = "https://events.spbu.ru/events/polyakhov_readings, http://nanomat.spbu.ru/en/node/175, http://nanomat.spbu.ru/ru/node/192, http://spbu.ru/news-events/calendar/viii-polyahovskie-chteniya",

}

RIS

TY - JOUR

T1 - Numerical simulation of the transonic flow past the blunted wedge in the diverging channel

AU - Ryabinin, Anatoly

N1 - Conference code: 8

PY - 2018/5/2

Y1 - 2018/5/2

N2 - Positions of shock waves in the 2D channel with a blunted wedge are studied numerically. Solutions of the Euler equations are obtained with finite-volume solver SU2 for 15 variants of channel geometry. Numerical simulations reveal a considerable hysteresis in the shock wave position versus the supersonic Mach number given at the inlet. In the certain range of inlet Mach number, there are asymmetrical solutions of the equations. Small change in the geometry of the channel leads to shift of boundaries of the hysteresis range.

AB - Positions of shock waves in the 2D channel with a blunted wedge are studied numerically. Solutions of the Euler equations are obtained with finite-volume solver SU2 for 15 variants of channel geometry. Numerical simulations reveal a considerable hysteresis in the shock wave position versus the supersonic Mach number given at the inlet. In the certain range of inlet Mach number, there are asymmetrical solutions of the equations. Small change in the geometry of the channel leads to shift of boundaries of the hysteresis range.

KW - SHOCK-WAVE BIFURCATION

UR - http://www.scopus.com/inward/record.url?scp=85047208980&partnerID=8YFLogxK

U2 - 10.1063/1.5034654

DO - 10.1063/1.5034654

M3 - Conference article

VL - 1959

SP - 1

EP - 5

JO - AIP Conference Proceedings

JF - AIP Conference Proceedings

SN - 0094-243X

IS - 050026

T2 - International Scientific Conference on Mechanics - Eighth Polyakhov's Reading

Y2 - 29 January 2018 through 2 February 2018

ER -

ID: 33823649