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Determination of the position of the laminar-turbulent transition on the surface of a supersonic nozzle. / Lukashevich, Sergey; Morozov, Sergey; Shiplyuk, Aleksandr.

в: AIP Conference Proceedings, Том 2504, № 1, 030091, 16.02.2023.

Результаты исследований: Научные публикации в периодических изданиях › статья по материалам конференции › Рецензирование

Harvard

Lukashevich, S, Morozov, S & Shiplyuk, A 2023, 'Determination of the position of the laminar-turbulent transition on the surface of a supersonic nozzle', AIP Conference Proceedings, Том. 2504, № 1, 030091. https://doi.org/10.1063/5.0133158

APA

Lukashevich, S., Morozov, S., & Shiplyuk, A. (2023). Determination of the position of the laminar-turbulent transition on the surface of a supersonic nozzle. AIP Conference Proceedings, 2504(1), [030091]. https://doi.org/10.1063/5.0133158

Vancouver

Lukashevich S, Morozov S, Shiplyuk A. Determination of the position of the laminar-turbulent transition on the surface of a supersonic nozzle. AIP Conference Proceedings. 2023 февр. 16;2504(1):030091. doi: 10.1063/5.0133158

Author

Lukashevich, Sergey ; Morozov, Sergey ; Shiplyuk, Aleksandr. / Determination of the position of the laminar-turbulent transition on the surface of a supersonic nozzle. в: AIP Conference Proceedings. 2023 ; Том 2504, № 1.

BibTeX

@article{46195d2072104c1cae55b6e669160c30,
title = "Determination of the position of the laminar-turbulent transition on the surface of a supersonic nozzle",
abstract = "The experimental results on determining the position of the laminar-turbulent transition of a supersonic boundary layer on the axisymmetric nozzle surface are presented. Measurements of pressure disturbances behind the normal shock wave along the nozzle axis of the Tranzit-M short-duration wind tunnel have been carried out. The launches were carried out in a configuration without a prechamber (from the atmosphere). It is shown that the transition begins at a distance of 0.14 m from the nozzle throat, and the maximum level of disturbances at the nozzle exit reaches 1.8%.",
author = "Sergey Lukashevich and Sergey Morozov and Aleksandr Shiplyuk",
year = "2023",
month = feb,
day = "16",
doi = "10.1063/5.0133158",
language = "English",
volume = "2504",
journal = "AIP Conference Proceedings",
issn = "0094-243X",
publisher = "American Institute of Physics",
number = "1",
note = "2021 Actual Problems of Continuum Mechanics: Experiment, Theory, and Applications : XXVIII Всероссийская конференция с международным участием «Высокоэнергетические процессы в механике сплошной среды», посвященная 100-летию со дня рождения Н.Н. Яненко ; Conference date: 20-09-2021 Through 24-09-2021",

}

RIS

TY - JOUR

T1 - Determination of the position of the laminar-turbulent transition on the surface of a supersonic nozzle

AU - Lukashevich, Sergey

AU - Morozov, Sergey

AU - Shiplyuk, Aleksandr

PY - 2023/2/16

Y1 - 2023/2/16

N2 - The experimental results on determining the position of the laminar-turbulent transition of a supersonic boundary layer on the axisymmetric nozzle surface are presented. Measurements of pressure disturbances behind the normal shock wave along the nozzle axis of the Tranzit-M short-duration wind tunnel have been carried out. The launches were carried out in a configuration without a prechamber (from the atmosphere). It is shown that the transition begins at a distance of 0.14 m from the nozzle throat, and the maximum level of disturbances at the nozzle exit reaches 1.8%.

AB - The experimental results on determining the position of the laminar-turbulent transition of a supersonic boundary layer on the axisymmetric nozzle surface are presented. Measurements of pressure disturbances behind the normal shock wave along the nozzle axis of the Tranzit-M short-duration wind tunnel have been carried out. The launches were carried out in a configuration without a prechamber (from the atmosphere). It is shown that the transition begins at a distance of 0.14 m from the nozzle throat, and the maximum level of disturbances at the nozzle exit reaches 1.8%.

UR - https://www.scopus.com/record/display.uri?eid=2-s2.0-85149627986&origin=inward&txGid=a1aa20e7aac0054edd8980a6e7b825aa

UR - https://www.mendeley.com/catalogue/4a10202b-c645-3971-8551-459e6b23db2c/

U2 - 10.1063/5.0133158

DO - 10.1063/5.0133158

M3 - Conference article

VL - 2504

JO - AIP Conference Proceedings

JF - AIP Conference Proceedings

SN - 0094-243X

IS - 1

M1 - 030091

T2 - 2021 Actual Problems of Continuum Mechanics: Experiment, Theory, and Applications

Y2 - 20 September 2021 through 24 September 2021

ER -

ID: 59659882