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Shock waves in a channel with a central body. / Ryabinin, A.N.

In: ARPN Journal of Engineering and Applied Sciences, Vol. 12, No. 11, 2017, p. 3532-3536.

Research output: Contribution to journal › Article

Harvard

Ryabinin, AN 2017, 'Shock waves in a channel with a central body', ARPN Journal of Engineering and Applied Sciences, vol. 12, no. 11, pp. 3532-3536. <http://www.arpnjournals.org/jeas/research_papers/rp_2017/jeas_0617_6086.pdf>

APA

Ryabinin, A. N. (2017). Shock waves in a channel with a central body. ARPN Journal of Engineering and Applied Sciences, 12(11), 3532-3536. http://www.arpnjournals.org/jeas/research_papers/rp_2017/jeas_0617_6086.pdf

Vancouver

Ryabinin AN. Shock waves in a channel with a central body. ARPN Journal of Engineering and Applied Sciences. 2017;12(11):3532-3536.

Author

Ryabinin, A.N. / Shock waves in a channel with a central body. In: ARPN Journal of Engineering and Applied Sciences. 2017 ; Vol. 12, No. 11. pp. 3532-3536.

BibTeX

@article{9baa417d5d1e4ed0a3696a87a1ff3e84,
title = "Shock waves in a channel with a central body",
abstract = "Positions of shock waves in the 2D channel with a central body are studied numerically. Solutions of the Euler equations and Reynolds-averaged Navier–Stokes equations are obtained with finite-volume solvers. Numerical simulations reveal a considerable hysteresis in the shock wave position versus the supersonic Mach number given at the inlet for inviscid gas and for viscous gas. 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 the hysteresis range.",
keywords = "shock wave position, computational fluid dynamics, hysteresis",
author = "A.N. Ryabinin",
year = "2017",
language = "не определен",
volume = "12",
pages = "3532--3536",
journal = "ARPN Journal of Engineering and Applied Sciences",
issn = "1819-6608",
publisher = "Asian Research Publishing Network (ARPN)",
number = "11",

}

RIS

TY - JOUR

T1 - Shock waves in a channel with a central body

AU - Ryabinin, A.N.

PY - 2017

Y1 - 2017

N2 - Positions of shock waves in the 2D channel with a central body are studied numerically. Solutions of the Euler equations and Reynolds-averaged Navier–Stokes equations are obtained with finite-volume solvers. Numerical simulations reveal a considerable hysteresis in the shock wave position versus the supersonic Mach number given at the inlet for inviscid gas and for viscous gas. 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 the hysteresis range.

AB - Positions of shock waves in the 2D channel with a central body are studied numerically. Solutions of the Euler equations and Reynolds-averaged Navier–Stokes equations are obtained with finite-volume solvers. Numerical simulations reveal a considerable hysteresis in the shock wave position versus the supersonic Mach number given at the inlet for inviscid gas and for viscous gas. 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 the hysteresis range.

KW - shock wave position

KW - computational fluid dynamics

KW - hysteresis

M3 - статья

VL - 12

SP - 3532

EP - 3536

JO - ARPN Journal of Engineering and Applied Sciences

JF - ARPN Journal of Engineering and Applied Sciences

SN - 1819-6608

IS - 11

ER -

ID: 7751487