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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 2023, Volume 64, Issue 4, Pages 118–129
DOI: https://doi.org/10.15372/PMTF202215232
(Mi pmtf1679)
 

This article is cited in 2 scientific papers (total in 2 papers)

Experimental investigation of the evolution of controlled perturbations in a longitudinal vortex generated in a boundary layer on a flat plate at a Mach number $\mathrm{M}=2$

A. D. Kosinov, M. V. Piterimova, A. V. Shmakova, N. V. Semenov, Yu. G. Ermolaev

Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch of the Russian Academy of Sciences, Novosibirsk, Russia
References:
Abstract: Using the results of experimental studies, a comparison is made of the space-time distributions of the amplitude of controlled pulsations in the linear and weakly nonlinear phases of the development of a wave train in homogeneous and inhomogeneous boundary layers on a flat plate at a Mach number $\mathrm{M}=2$. (The inhomogeneity of the flow is caused by a longitudinal stationary perturbation generated by a pair of weak shock waves. Controlled perturbations were generated locally from the surface at a fixed power of the high-frequency glow discharge inside the model.) It is established that the inhomogeneity of the flow changes the mechanism of interaction of subharmonic perturbations. It is shown that in the center of the wave train there is a violation of the spatial synchronism of pulsations of subharmonic frequency.
Keywords: supersonic flow, flat plate, boundary layer, weak shock waves, controlled disturbances.
Funding agency Grant number
Russian Science Foundation 22-19-00666
Received: 23.11.2022
Revised: 17.02.2023
Accepted: 27.02.2023
English version:
Journal of Applied Mechanics and Technical Physics, 2023, Volume 64, Issue 4, Pages 656–666
DOI: https://doi.org/10.1134/S0021894423040119
Bibliographic databases:
Document Type: Article
UDC: 532.526
Language: Russian
Citation: A. D. Kosinov, M. V. Piterimova, A. V. Shmakova, N. V. Semenov, Yu. G. Ermolaev, “Experimental investigation of the evolution of controlled perturbations in a longitudinal vortex generated in a boundary layer on a flat plate at a Mach number $\mathrm{M}=2$”, Prikl. Mekh. Tekh. Fiz., 64:4 (2023), 118–129; J. Appl. Mech. Tech. Phys., 64:4 (2023), 656–666
Citation in format AMSBIB
\Bibitem{KosPitShm23}
\by A.~D.~Kosinov, M.~V.~Piterimova, A.~V.~Shmakova, N.~V.~Semenov, Yu.~G.~Ermolaev
\paper Experimental investigation of the evolution of controlled perturbations in a longitudinal vortex generated in a boundary layer on a flat plate at a Mach number $\mathrm{M}=2$
\jour Prikl. Mekh. Tekh. Fiz.
\yr 2023
\vol 64
\issue 4
\pages 118--129
\mathnet{http://mi.mathnet.ru/pmtf1679}
\crossref{https://doi.org/10.15372/PMTF202215232}
\elib{https://elibrary.ru/item.asp?id=54283717}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 2023
\vol 64
\issue 4
\pages 656--666
\crossref{https://doi.org/10.1134/S0021894423040119}
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  • https://www.mathnet.ru/eng/pmtf/v64/i4/p118
  • This publication is cited in the following 2 articles:
    Citing articles in Google Scholar: Russian citations, English citations
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    Prikladnaya Mekhanika i Tekhnicheskaya Fizika Prikladnaya Mekhanika i Tekhnicheskaya Fizika
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    References:16
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