Standard

Choice of boundary conditions at the unsteady modeling of jets flowing into the supersonic flow. / Zamuraev, V. P.; Kalinina, A. P.; Popova, D. S. et al.

In: Journal of Physics: Conference Series, Vol. 1268, No. 1, 012024, 16.07.2019.

Research output: Contribution to journal › Conference article › peer-review

Harvard

Zamuraev, VP, Kalinina, AP, Popova, DS, Fedorova, DV & Ivanova, ON 2019, 'Choice of boundary conditions at the unsteady modeling of jets flowing into the supersonic flow', Journal of Physics: Conference Series, vol. 1268, no. 1, 012024. https://doi.org/10.1088/1742-6596/1268/1/012024

APA

Zamuraev, V. P., Kalinina, A. P., Popova, D. S., Fedorova, D. V., & Ivanova, O. N. (2019). Choice of boundary conditions at the unsteady modeling of jets flowing into the supersonic flow. Journal of Physics: Conference Series, 1268(1), [012024]. https://doi.org/10.1088/1742-6596/1268/1/012024

Vancouver

Zamuraev VP, Kalinina AP, Popova DS, Fedorova DV, Ivanova ON. Choice of boundary conditions at the unsteady modeling of jets flowing into the supersonic flow. Journal of Physics: Conference Series. 2019 Jul 16;1268(1):012024. doi: 10.1088/1742-6596/1268/1/012024

Author

Zamuraev, V. P. ; Kalinina, A. P. ; Popova, D. S. et al. / Choice of boundary conditions at the unsteady modeling of jets flowing into the supersonic flow. In: Journal of Physics: Conference Series. 2019 ; Vol. 1268, No. 1.

BibTeX

@article{d993c7b8a209423b8cc4a5855c34b2ca,
title = "Choice of boundary conditions at the unsteady modeling of jets flowing into the supersonic flow",
abstract = "Numerical simulation of ignition of the gas mixture not mixed previously in the supersonic flow localized in a channel was performed. The ignition is initiated by the shock wave from the throttling jet, which results in significant changing of pressure difference between the main flow and the gas generator of the throttling jet. It is shown that applying boundary conditions similar to the breakdown of arbitrary discontinuity conditions, makes it possible to obtain the transonic mode observed in the experiment. The near-wall and axisymmetric supply of the gaseous fuel was considered.",
author = "Zamuraev, {V. P.} and Kalinina, {A. P.} and Popova, {D. S.} and Fedorova, {D. V.} and Ivanova, {O. N.}",
year = "2019",
month = jul,
day = "16",
doi = "10.1088/1742-6596/1268/1/012024",
language = "English",
volume = "1268",
journal = "Journal of Physics: Conference Series",
issn = "1742-6588",
publisher = "IOP Publishing Ltd.",
number = "1",
note = "All-Russian Conference and School for Young Scientists, devoted to 100th Anniversary of Academician L.V. Ovsiannikov on Mathematical Problems of Continuum Mechanics, MPCM 2019 ; Conference date: 13-05-2019 Through 17-05-2019",

}

RIS

TY - JOUR

T1 - Choice of boundary conditions at the unsteady modeling of jets flowing into the supersonic flow

AU - Zamuraev, V. P.

AU - Kalinina, A. P.

AU - Popova, D. S.

AU - Fedorova, D. V.

AU - Ivanova, O. N.

PY - 2019/7/16

Y1 - 2019/7/16

N2 - Numerical simulation of ignition of the gas mixture not mixed previously in the supersonic flow localized in a channel was performed. The ignition is initiated by the shock wave from the throttling jet, which results in significant changing of pressure difference between the main flow and the gas generator of the throttling jet. It is shown that applying boundary conditions similar to the breakdown of arbitrary discontinuity conditions, makes it possible to obtain the transonic mode observed in the experiment. The near-wall and axisymmetric supply of the gaseous fuel was considered.

AB - Numerical simulation of ignition of the gas mixture not mixed previously in the supersonic flow localized in a channel was performed. The ignition is initiated by the shock wave from the throttling jet, which results in significant changing of pressure difference between the main flow and the gas generator of the throttling jet. It is shown that applying boundary conditions similar to the breakdown of arbitrary discontinuity conditions, makes it possible to obtain the transonic mode observed in the experiment. The near-wall and axisymmetric supply of the gaseous fuel was considered.

UR - http://www.scopus.com/inward/record.url?scp=85073900752&partnerID=8YFLogxK

U2 - 10.1088/1742-6596/1268/1/012024

DO - 10.1088/1742-6596/1268/1/012024

M3 - Conference article

AN - SCOPUS:85073900752

VL - 1268

JO - Journal of Physics: Conference Series

JF - Journal of Physics: Conference Series

SN - 1742-6588

IS - 1

M1 - 012024

T2 - All-Russian Conference and School for Young Scientists, devoted to 100th Anniversary of Academician L.V. Ovsiannikov on Mathematical Problems of Continuum Mechanics, MPCM 2019

Y2 - 13 May 2019 through 17 May 2019

ER -

ID: 21997555