Standard

Transonic flow simulation in a bent channel using SU2 software. / Ryabinin, Anatoly; Kuzmin, Alexander.

Proceedings - 2020 Ivannikov Ispras Open Conference, ISPRAS 2020. ed. / A Avetisyan. Institute of Electrical and Electronics Engineers Inc., 2021. p. 175-178 9394139 (Proceedings - 2020 Ivannikov Ispras Open Conference, ISPRAS 2020).

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

Harvard

Ryabinin, A & Kuzmin, A 2021, Transonic flow simulation in a bent channel using SU2 software. in A Avetisyan (ed.), Proceedings - 2020 Ivannikov Ispras Open Conference, ISPRAS 2020., 9394139, Proceedings - 2020 Ivannikov Ispras Open Conference, ISPRAS 2020, Institute of Electrical and Electronics Engineers Inc., pp. 175-178, 2020 Ivannikov Ispras Open Conference, ISPRAS 2020, Moscow, Russian Federation, 10/12/20. https://doi.org/10.1109/ispras51486.2020.00034

APA

Ryabinin, A., & Kuzmin, A. (2021). Transonic flow simulation in a bent channel using SU2 software. In A. Avetisyan (Ed.), Proceedings - 2020 Ivannikov Ispras Open Conference, ISPRAS 2020 (pp. 175-178). [9394139] (Proceedings - 2020 Ivannikov Ispras Open Conference, ISPRAS 2020). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ispras51486.2020.00034

Vancouver

Ryabinin A, Kuzmin A. Transonic flow simulation in a bent channel using SU2 software. In Avetisyan A, editor, Proceedings - 2020 Ivannikov Ispras Open Conference, ISPRAS 2020. Institute of Electrical and Electronics Engineers Inc. 2021. p. 175-178. 9394139. (Proceedings - 2020 Ivannikov Ispras Open Conference, ISPRAS 2020). https://doi.org/10.1109/ispras51486.2020.00034

Author

Ryabinin, Anatoly ; Kuzmin, Alexander. / Transonic flow simulation in a bent channel using SU2 software. Proceedings - 2020 Ivannikov Ispras Open Conference, ISPRAS 2020. editor / A Avetisyan. Institute of Electrical and Electronics Engineers Inc., 2021. pp. 175-178 (Proceedings - 2020 Ivannikov Ispras Open Conference, ISPRAS 2020).

BibTeX

@inproceedings{61f012ade381446c8da5cab7a30d84fc,
title = "Transonic flow simulation in a bent channel using SU2 software",
abstract = "Turbulent 2D airflow in a bent convergent-divergent channel is studied numerically. The free stream is supersonic and parallel to the lower wall of channel. Solutions of the unsteady Reynolds-averaged Navier-Stokes equations are obtained with an open-source finite-volume solver SU2. The solutions demonstrate an expulsion/swallowing of the shock waves with variation of the free-stream Mach number Flow topology in the channel and in front of its entrance is discussed. The hysteresis of shock wave positions with variation of is determined. ",
keywords = "hysteresis, instability, shock waves, supersonic intake",
author = "Anatoly Ryabinin and Alexander Kuzmin",
note = "Publisher Copyright: {\textcopyright} 2020 IEEE. Copyright: Copyright 2021 Elsevier B.V., All rights reserved.; 2020 Ivannikov Ispras Open Conference, ISPRAS 2020 ; Conference date: 10-12-2020 Through 11-12-2020",
year = "2021",
month = apr,
doi = "10.1109/ispras51486.2020.00034",
language = "English",
series = "Proceedings - 2020 Ivannikov Ispras Open Conference, ISPRAS 2020",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "175--178",
editor = "A Avetisyan",
booktitle = "Proceedings - 2020 Ivannikov Ispras Open Conference, ISPRAS 2020",
address = "United States",

}

RIS

TY - GEN

T1 - Transonic flow simulation in a bent channel using SU2 software

AU - Ryabinin, Anatoly

AU - Kuzmin, Alexander

N1 - Publisher Copyright: © 2020 IEEE. Copyright: Copyright 2021 Elsevier B.V., All rights reserved.

PY - 2021/4

Y1 - 2021/4

N2 - Turbulent 2D airflow in a bent convergent-divergent channel is studied numerically. The free stream is supersonic and parallel to the lower wall of channel. Solutions of the unsteady Reynolds-averaged Navier-Stokes equations are obtained with an open-source finite-volume solver SU2. The solutions demonstrate an expulsion/swallowing of the shock waves with variation of the free-stream Mach number Flow topology in the channel and in front of its entrance is discussed. The hysteresis of shock wave positions with variation of is determined.

AB - Turbulent 2D airflow in a bent convergent-divergent channel is studied numerically. The free stream is supersonic and parallel to the lower wall of channel. Solutions of the unsteady Reynolds-averaged Navier-Stokes equations are obtained with an open-source finite-volume solver SU2. The solutions demonstrate an expulsion/swallowing of the shock waves with variation of the free-stream Mach number Flow topology in the channel and in front of its entrance is discussed. The hysteresis of shock wave positions with variation of is determined.

KW - hysteresis

KW - instability

KW - shock waves

KW - supersonic intake

UR - http://www.scopus.com/inward/record.url?scp=85104580651&partnerID=8YFLogxK

UR - https://www.mendeley.com/catalogue/b37091a4-ce62-332f-9bff-0ca378c3a583/

U2 - 10.1109/ispras51486.2020.00034

DO - 10.1109/ispras51486.2020.00034

M3 - Conference contribution

AN - SCOPUS:85104580651

T3 - Proceedings - 2020 Ivannikov Ispras Open Conference, ISPRAS 2020

SP - 175

EP - 178

BT - Proceedings - 2020 Ivannikov Ispras Open Conference, ISPRAS 2020

A2 - Avetisyan, A

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2020 Ivannikov Ispras Open Conference, ISPRAS 2020

Y2 - 10 December 2020 through 11 December 2020

ER -

ID: 77910853