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Bifurcations of transonic flow in the channels of various shapes. / Ryabinin, Anatoly.

International Conference on the Methods of Aerophysical Research, ICMAR 2020. ed. / Vasily M. Fomin; Alexander Shiplyuk. American Institute of Physics, 2021. 030017 (AIP Conference Proceedings; Vol. 2351).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Harvard

Ryabinin, A 2021, Bifurcations of transonic flow in the channels of various shapes. in VM Fomin & A Shiplyuk (eds), International Conference on the Methods of Aerophysical Research, ICMAR 2020., 030017, AIP Conference Proceedings, vol. 2351, American Institute of Physics, 20th International Conference on the Methods of Aerophysical Research, ICMAR 2020, Akademgorodok, Novosibirsk, Russian Federation, 1/11/20. https://doi.org/10.1063/5.0051708

APA

Ryabinin, A. (2021). Bifurcations of transonic flow in the channels of various shapes. In V. M. Fomin, & A. Shiplyuk (Eds.), International Conference on the Methods of Aerophysical Research, ICMAR 2020 [030017] (AIP Conference Proceedings; Vol. 2351). American Institute of Physics. https://doi.org/10.1063/5.0051708

Vancouver

Ryabinin A. Bifurcations of transonic flow in the channels of various shapes. In Fomin VM, Shiplyuk A, editors, International Conference on the Methods of Aerophysical Research, ICMAR 2020. American Institute of Physics. 2021. 030017. (AIP Conference Proceedings). https://doi.org/10.1063/5.0051708

Author

Ryabinin, Anatoly. / Bifurcations of transonic flow in the channels of various shapes. International Conference on the Methods of Aerophysical Research, ICMAR 2020. editor / Vasily M. Fomin ; Alexander Shiplyuk. American Institute of Physics, 2021. (AIP Conference Proceedings).

BibTeX

@inproceedings{e3007f15f2e84e94b19ff193948485cd,
title = "Bifurcations of transonic flow in the channels of various shapes",
abstract = "The flow in 2D channels of variable cross-section was studied numerically. The channels contain bodies that split the channels into narrow ones. Solutions of Euler's equations are obtained using the finite-volume solver of the Ansys CFX software package. A set of solutions is found. These solutions depend on the input Mach number and on the initial condition. Numerical simulations show a significant hysteresis in the drag coefficient of bodies in the channel relative to the supersonic Mach number set at the inlet. In a certain range of the inlet Mach number, there are asymmetric solutions of the equations.",
author = "Anatoly Ryabinin",
note = "Publisher Copyright: {\textcopyright} 2021 Author(s).; 20th International Conference on the Methods of Aerophysical Research, ICMAR 2020 ; Conference date: 01-11-2020 Through 07-11-2020",
year = "2021",
month = may,
day = "24",
doi = "10.1063/5.0051708",
language = "English",
series = "AIP Conference Proceedings",
publisher = "American Institute of Physics",
editor = "Fomin, {Vasily M.} and Alexander Shiplyuk",
booktitle = "International Conference on the Methods of Aerophysical Research, ICMAR 2020",
address = "United States",

}

RIS

TY - GEN

T1 - Bifurcations of transonic flow in the channels of various shapes

AU - Ryabinin, Anatoly

N1 - Publisher Copyright: © 2021 Author(s).

PY - 2021/5/24

Y1 - 2021/5/24

N2 - The flow in 2D channels of variable cross-section was studied numerically. The channels contain bodies that split the channels into narrow ones. Solutions of Euler's equations are obtained using the finite-volume solver of the Ansys CFX software package. A set of solutions is found. These solutions depend on the input Mach number and on the initial condition. Numerical simulations show a significant hysteresis in the drag coefficient of bodies in the channel relative to the supersonic Mach number set at the inlet. In a certain range of the inlet Mach number, there are asymmetric solutions of the equations.

AB - The flow in 2D channels of variable cross-section was studied numerically. The channels contain bodies that split the channels into narrow ones. Solutions of Euler's equations are obtained using the finite-volume solver of the Ansys CFX software package. A set of solutions is found. These solutions depend on the input Mach number and on the initial condition. Numerical simulations show a significant hysteresis in the drag coefficient of bodies in the channel relative to the supersonic Mach number set at the inlet. In a certain range of the inlet Mach number, there are asymmetric solutions of the equations.

UR - http://www.scopus.com/inward/record.url?scp=85107185827&partnerID=8YFLogxK

UR - https://www.mendeley.com/catalogue/8f321dc6-ba3a-313d-9a35-40b659c1b361/

U2 - 10.1063/5.0051708

DO - 10.1063/5.0051708

M3 - Conference contribution

AN - SCOPUS:85107185827

T3 - AIP Conference Proceedings

BT - International Conference on the Methods of Aerophysical Research, ICMAR 2020

A2 - Fomin, Vasily M.

A2 - Shiplyuk, Alexander

PB - American Institute of Physics

T2 - 20th International Conference on the Methods of Aerophysical Research, ICMAR 2020

Y2 - 1 November 2020 through 7 November 2020

ER -

ID: 84643110