Standard

Frequency response of the flow in a radial swirler. / Litvinov, Ivan; Gorelikov, Evgeny; Shtork, Sergey.

в: Journal of Mechanical Science and Technology, Том 36, № 5, 05.2022, стр. 2397-2402.

Результаты исследований: Научные публикации в периодических изданияхстатьяРецензирование

Harvard

Litvinov, I, Gorelikov, E & Shtork, S 2022, 'Frequency response of the flow in a radial swirler', Journal of Mechanical Science and Technology, Том. 36, № 5, стр. 2397-2402. https://doi.org/10.1007/s12206-022-0422-1

APA

Litvinov, I., Gorelikov, E., & Shtork, S. (2022). Frequency response of the flow in a radial swirler. Journal of Mechanical Science and Technology, 36(5), 2397-2402. https://doi.org/10.1007/s12206-022-0422-1

Vancouver

Litvinov I, Gorelikov E, Shtork S. Frequency response of the flow in a radial swirler. Journal of Mechanical Science and Technology. 2022 май;36(5):2397-2402. doi: 10.1007/s12206-022-0422-1

Author

Litvinov, Ivan ; Gorelikov, Evgeny ; Shtork, Sergey. / Frequency response of the flow in a radial swirler. в: Journal of Mechanical Science and Technology. 2022 ; Том 36, № 5. стр. 2397-2402.

BibTeX

@article{b356e6a497e44519b5db24c04d63a993,
title = "Frequency response of the flow in a radial swirler",
abstract = "We report the results of an experimental study on flow with a precessing vortex core in an isothermal radial swirler burner model. It was shown for the first time that in radial swirler flow, the Strouhal number (the dimensionless precession frequency of the vortex core) is inversely related to the swirl number in the range 0.5 < S < 0.8. A minimum occurs in the precessing vortex core frequency due to the reduced velocity of the helical vortex structure in the axial flow direction and the axial stretching of the helical vortex structure. This finding emphasizes the importance of accounting for the helical geometry of the precessing vortex when predicting the frequency response of burner installations.",
keywords = "LDA, Microphones, Precessing vortex core, Swirl flow, Swirler",
author = "Ivan Litvinov and Evgeny Gorelikov and Sergey Shtork",
note = "Funding Information: This study was supported by the Russian Science Foundation (Grant No. 21-19-00769). Publisher Copyright: {\textcopyright} 2022, The Korean Society of Mechanical Engineers and Springer-Verlag GmbH Germany, part of Springer Nature.",
year = "2022",
month = may,
doi = "10.1007/s12206-022-0422-1",
language = "English",
volume = "36",
pages = "2397--2402",
journal = "Journal of Mechanical Science and Technology",
issn = "1738-494X",
publisher = "Korean Society of Mechanical Engineers",
number = "5",

}

RIS

TY - JOUR

T1 - Frequency response of the flow in a radial swirler

AU - Litvinov, Ivan

AU - Gorelikov, Evgeny

AU - Shtork, Sergey

N1 - Funding Information: This study was supported by the Russian Science Foundation (Grant No. 21-19-00769). Publisher Copyright: © 2022, The Korean Society of Mechanical Engineers and Springer-Verlag GmbH Germany, part of Springer Nature.

PY - 2022/5

Y1 - 2022/5

N2 - We report the results of an experimental study on flow with a precessing vortex core in an isothermal radial swirler burner model. It was shown for the first time that in radial swirler flow, the Strouhal number (the dimensionless precession frequency of the vortex core) is inversely related to the swirl number in the range 0.5 < S < 0.8. A minimum occurs in the precessing vortex core frequency due to the reduced velocity of the helical vortex structure in the axial flow direction and the axial stretching of the helical vortex structure. This finding emphasizes the importance of accounting for the helical geometry of the precessing vortex when predicting the frequency response of burner installations.

AB - We report the results of an experimental study on flow with a precessing vortex core in an isothermal radial swirler burner model. It was shown for the first time that in radial swirler flow, the Strouhal number (the dimensionless precession frequency of the vortex core) is inversely related to the swirl number in the range 0.5 < S < 0.8. A minimum occurs in the precessing vortex core frequency due to the reduced velocity of the helical vortex structure in the axial flow direction and the axial stretching of the helical vortex structure. This finding emphasizes the importance of accounting for the helical geometry of the precessing vortex when predicting the frequency response of burner installations.

KW - LDA

KW - Microphones

KW - Precessing vortex core

KW - Swirl flow

KW - Swirler

UR - http://www.scopus.com/inward/record.url?scp=85129120452&partnerID=8YFLogxK

UR - https://www.mendeley.com/catalogue/33cc3496-1d2f-3717-9e08-ba4fc44009c8/

U2 - 10.1007/s12206-022-0422-1

DO - 10.1007/s12206-022-0422-1

M3 - Article

AN - SCOPUS:85129120452

VL - 36

SP - 2397

EP - 2402

JO - Journal of Mechanical Science and Technology

JF - Journal of Mechanical Science and Technology

SN - 1738-494X

IS - 5

ER -

ID: 36036709