Standard

Measurement of the distribution of pressure pulsations along the axis of the supersonic nozzle. / Lukashevich, Sergey; Morozov, Sergey; Shiplyuk, Aleksandr.

в: AIP Conference Proceedings, Том 2504, 030032, 16.02.2023.

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

Harvard

Lukashevich, S, Morozov, S & Shiplyuk, A 2023, 'Measurement of the distribution of pressure pulsations along the axis of the supersonic nozzle', AIP Conference Proceedings, Том. 2504, 030032. https://doi.org/10.1063/5.0132273

APA

Lukashevich, S., Morozov, S., & Shiplyuk, A. (2023). Measurement of the distribution of pressure pulsations along the axis of the supersonic nozzle. AIP Conference Proceedings, 2504, [030032]. https://doi.org/10.1063/5.0132273

Vancouver

Lukashevich S, Morozov S, Shiplyuk A. Measurement of the distribution of pressure pulsations along the axis of the supersonic nozzle. AIP Conference Proceedings. 2023 февр. 16;2504:030032. doi: 10.1063/5.0132273

Author

Lukashevich, Sergey ; Morozov, Sergey ; Shiplyuk, Aleksandr. / Measurement of the distribution of pressure pulsations along the axis of the supersonic nozzle. в: AIP Conference Proceedings. 2023 ; Том 2504.

BibTeX

@article{7e755d23928d4a02a7ab0795e9156568,
title = "Measurement of the distribution of pressure pulsations along the axis of the supersonic nozzle",
abstract = "The distributions of pressure pulsations along the axis of the supersonic nozzle are obtained experimentally. Measurements of pressure pulsations behind the normal shock along the nozzle axis of the Tranzit-M short-term wind tunnel have been carried out. The experiments were carried out at three values of the stagnation pressure P0=2.1; 3.7; 13.9 bar in configurations with and without honeycomb. The values of pulsations in the subsonic part of the nozzle without a honeycomb 1.3% with a honeycomb 0.7% were obtained. The maximum pressure pulsations in the supersonic part of the nozzle were 2.2% without honeycomb and 1.5% without honeycomb.",
author = "Sergey Lukashevich and Sergey Morozov and Aleksandr Shiplyuk",
note = "The research was carried out within the state assignment of Ministry of Science and Higher Education of the Russian Federation (project No. 121030500154-2).; 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",
year = "2023",
month = feb,
day = "16",
doi = "10.1063/5.0132273",
language = "English",
volume = "2504",
journal = "AIP Conference Proceedings",
issn = "0094-243X",
publisher = "American Institute of Physics",

}

RIS

TY - JOUR

T1 - Measurement of the distribution of pressure pulsations along the axis of the supersonic nozzle

AU - Lukashevich, Sergey

AU - Morozov, Sergey

AU - Shiplyuk, Aleksandr

N1 - The research was carried out within the state assignment of Ministry of Science and Higher Education of the Russian Federation (project No. 121030500154-2).

PY - 2023/2/16

Y1 - 2023/2/16

N2 - The distributions of pressure pulsations along the axis of the supersonic nozzle are obtained experimentally. Measurements of pressure pulsations behind the normal shock along the nozzle axis of the Tranzit-M short-term wind tunnel have been carried out. The experiments were carried out at three values of the stagnation pressure P0=2.1; 3.7; 13.9 bar in configurations with and without honeycomb. The values of pulsations in the subsonic part of the nozzle without a honeycomb 1.3% with a honeycomb 0.7% were obtained. The maximum pressure pulsations in the supersonic part of the nozzle were 2.2% without honeycomb and 1.5% without honeycomb.

AB - The distributions of pressure pulsations along the axis of the supersonic nozzle are obtained experimentally. Measurements of pressure pulsations behind the normal shock along the nozzle axis of the Tranzit-M short-term wind tunnel have been carried out. The experiments were carried out at three values of the stagnation pressure P0=2.1; 3.7; 13.9 bar in configurations with and without honeycomb. The values of pulsations in the subsonic part of the nozzle without a honeycomb 1.3% with a honeycomb 0.7% were obtained. The maximum pressure pulsations in the supersonic part of the nozzle were 2.2% without honeycomb and 1.5% without honeycomb.

UR - https://www.scopus.com/record/display.uri?eid=2-s2.0-85149697958&origin=inward&txGid=0a726c3ead6c1cbe91a2503881cd5b94

UR - https://www.mendeley.com/catalogue/0d20dd9d-5ee2-31e2-a6c1-e52f4c19684e/

U2 - 10.1063/5.0132273

DO - 10.1063/5.0132273

M3 - Conference article

VL - 2504

JO - AIP Conference Proceedings

JF - AIP Conference Proceedings

SN - 0094-243X

M1 - 030032

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

Y2 - 20 September 2021 through 24 September 2021

ER -

ID: 59505299