Stability of the laminar boundary layer on the surface of the Mach-6 contoured nozzle

Standard

Stability of the laminar boundary layer on the surface of the Mach-6 contoured nozzle. / Morozov, S. O.; Shiplyuk, A. N.

In: Journal of Physics: Conference Series, Vol. 1404, No. 1, 012089, 06.12.2019.

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

Harvard

Morozov, SO & Shiplyuk, AN 2019, 'Stability of the laminar boundary layer on the surface of the Mach-6 contoured nozzle', Journal of Physics: Conference Series, vol. 1404, no. 1, 012089. https://doi.org/10.1088/1742-6596/1404/1/012089

APA

Morozov, S. O., & Shiplyuk, A. N. (2019). Stability of the laminar boundary layer on the surface of the Mach-6 contoured nozzle. Journal of Physics: Conference Series, 1404(1), [012089]. https://doi.org/10.1088/1742-6596/1404/1/012089

Vancouver

Morozov SO, Shiplyuk AN. Stability of the laminar boundary layer on the surface of the Mach-6 contoured nozzle. Journal of Physics: Conference Series. 2019 Dec 6;1404(1):012089. doi: 10.1088/1742-6596/1404/1/012089

Author

Morozov, S. O. ; Shiplyuk, A. N. / Stability of the laminar boundary layer on the surface of the Mach-6 contoured nozzle. In: Journal of Physics: Conference Series. 2019 ; Vol. 1404, No. 1.

BibTeX

@article{01143f94feb949bb8482cf4168a1af6f,

title = "Stability of the laminar boundary layer on the surface of the Mach-6 contoured nozzle",

abstract = "The stability of the laminar boundary layer on the surface of the Mach 6 contoured nozzle designed for short-duration wind tunnel Transit-M is investigated. The numerical simulation of the laminar flow inside the nozzle is performed using Ansys Fluent software. The obtained boundary layers profiles on the nozzle surface are used to calculate the growth rate of the first and second Mack mode and G{\"o}rtler vortices in the framework of the linear stability theory. It has been shown that, for the Mach 6 nozzle, the G{\"o}rtler vortices grow most rapidly, the first Mack mode grows slower, and the second mode is insignificant.",

author = "Morozov, {S. O.} and Shiplyuk, {A. N.}",

note = "Publisher Copyright: {\textcopyright} 2019 IOP Publishing Ltd. Copyright: Copyright 2020 Elsevier B.V., All rights reserved.; 16th All-Russian Seminar with International Participation on Dynamics of Multiphase Media, DMM 2019 ; Conference date: 30-09-2019 Through 05-10-2019",

year = "2019",

month = dec,

day = "6",

doi = "10.1088/1742-6596/1404/1/012089",

language = "English",

volume = "1404",

journal = "Journal of Physics: Conference Series",

issn = "1742-6588",

publisher = "IOP Publishing Ltd.",

number = "1",

}

RIS

TY - JOUR

T1 - Stability of the laminar boundary layer on the surface of the Mach-6 contoured nozzle

AU - Morozov, S. O.

AU - Shiplyuk, A. N.

PY - 2019/12/6

Y1 - 2019/12/6

N2 - The stability of the laminar boundary layer on the surface of the Mach 6 contoured nozzle designed for short-duration wind tunnel Transit-M is investigated. The numerical simulation of the laminar flow inside the nozzle is performed using Ansys Fluent software. The obtained boundary layers profiles on the nozzle surface are used to calculate the growth rate of the first and second Mack mode and Görtler vortices in the framework of the linear stability theory. It has been shown that, for the Mach 6 nozzle, the Görtler vortices grow most rapidly, the first Mack mode grows slower, and the second mode is insignificant.

AB - The stability of the laminar boundary layer on the surface of the Mach 6 contoured nozzle designed for short-duration wind tunnel Transit-M is investigated. The numerical simulation of the laminar flow inside the nozzle is performed using Ansys Fluent software. The obtained boundary layers profiles on the nozzle surface are used to calculate the growth rate of the first and second Mack mode and Görtler vortices in the framework of the linear stability theory. It has been shown that, for the Mach 6 nozzle, the Görtler vortices grow most rapidly, the first Mack mode grows slower, and the second mode is insignificant.

UR - http://www.scopus.com/inward/record.url?scp=85077813937&partnerID=8YFLogxK

U2 - 10.1088/1742-6596/1404/1/012089

DO - 10.1088/1742-6596/1404/1/012089

M3 - Conference article

AN - SCOPUS:85077813937

VL - 1404

JO - Journal of Physics: Conference Series

JF - Journal of Physics: Conference Series

SN - 1742-6588

IS - 1

M1 - 012089

T2 - 16th All-Russian Seminar with International Participation on Dynamics of Multiphase Media, DMM 2019

Y2 - 30 September 2019 through 5 October 2019

ER -

ID: 23123017