Investigation of gas flow influence on acoustic waves, propagating downstream and upstream through gas flow in a cylindrical duct; Russian Physics Journal; Vol. 68, iss. 2

Bibliografiske detaljer
Parent link:Russian Physics Journal=Известия вузов. Физика.— .— Basel: Springer Nature Switzerland AG
Vol. 68, iss. 2.— 2025.— P. 300-307
Andre forfattere: Yamkin A. V. Aleksandr Vladimirovich, Chukhareva N. V. Natalia Vyacheslavovna, Bubenchikov M. A. Mikhail Alekseevich, Yamkin M. A. Maksim Aleksandrovich
Summary:Title screen
The physical and mechanical principles governing aeroacoustic vibrations within a cylindrical channel have been established through a series of numerical experiments aimed at investigating the impact of multidirectional turbulent gas flow on the propagation of these vibrations. The developed physical and mathematical model has demonstrated its efficacy, as verification processes confirmed a strong correspondence between the results of numerical simulations, experimental findings, and existing literature data. This validation allows us to assert the reliability of the model and its potential for further research endeavors. The outcomes of the numerical experiments distinctly reveal that the amplitude of waves propagating upstream surpassed that of downstream and non-flow waves at equal distances from the acoustic source within the cylindrical channel. The results obtained were corroborated through comparison with experimental and relevant literature data. The identified influence of flow can be practically applied in cross-correlation analyses of the amplitude of aeroacoustic vibrations resulting from leaks in gas pipelines, thereby enhancing the accuracy of leak detection systems
Текстовый файл
AM_Agreement
Sprog:engelsk
Udgivet: 2025
Fag:
Online adgang:https://doi.org/10.1007/s11182-025-03433-z
Format: Electronisk Book Chapter
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=683592

MARC

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330 |a The physical and mechanical principles governing aeroacoustic vibrations within a cylindrical channel have been established through a series of numerical experiments aimed at investigating the impact of multidirectional turbulent gas flow on the propagation of these vibrations. The developed physical and mathematical model has demonstrated its efficacy, as verification processes confirmed a strong correspondence between the results of numerical simulations, experimental findings, and existing literature data. This validation allows us to assert the reliability of the model and its potential for further research endeavors. The outcomes of the numerical experiments distinctly reveal that the amplitude of waves propagating upstream surpassed that of downstream and non-flow waves at equal distances from the acoustic source within the cylindrical channel. The results obtained were corroborated through comparison with experimental and relevant literature data. The identified influence of flow can be practically applied in cross-correlation analyses of the amplitude of aeroacoustic vibrations resulting from leaks in gas pipelines, thereby enhancing the accuracy of leak detection systems 
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461 1 |t Russian Physics Journal  |l Известия вузов. Физика  |c Basel  |n Springer Nature Switzerland AG 
463 1 |t Vol. 68, iss. 2  |v P. 300-307  |d 2025 
610 1 |a Characteristics of aeroacoustic vibrations 
610 1 |a Physical and mathematical model 
610 1 |a Acoustic waves 
610 1 |a Gas flow 
610 1 |a Acoustic pressure 
610 1 |a Acoustics 
610 1 |a Gas pipeline 
610 1 |a электронный ресурс 
610 1 |a труды учёных ТПУ 
701 1 |a Yamkin  |b A. V.  |g Aleksandr Vladimirovich 
701 1 |a Chukhareva  |b N. V.  |c specialist in the field of oil and gas business  |c associate Professor, Tomsk Polytechnic University, candidate of chemical Sciences  |f 1967-  |g Natalia Vyacheslavovna  |9 14933 
701 1 |a Bubenchikov  |b M. A.  |g Mikhail Alekseevich 
701 1 |a Yamkin  |b M. A.  |g Maksim Aleksandrovich 
801 0 |a RU  |b 63413507  |c 20251203  |g RCR 
856 4 |u https://doi.org/10.1007/s11182-025-03433-z  |z https://doi.org/10.1007/s11182-025-03433-z 
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