Prikladnaya Mekhanika i Tekhnicheskaya Fizika
RUS  ENG    JOURNALS   PEOPLE   ORGANISATIONS   CONFERENCES   SEMINARS   VIDEO LIBRARY   PACKAGE AMSBIB  
General information
Latest issue
Archive

Search papers
Search references

RSS
Latest issue
Current issues
Archive issues
What is RSS



Prikl. Mekh. Tekh. Fiz.:
Year:
Volume:
Issue:
Page:
Find






Personal entry:
Login:
Password:
Save password
Enter
Forgotten password?
Register


Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 2016, Volume 57, Issue 2, Pages 64–75
DOI: https://doi.org/10.15372/PMTF20160207
(Mi pmtf856)
 

This article is cited in 3 scientific papers (total in 3 papers)

Linear stability of the Couette flow of a vibrationally excited gas. 2. Viscous problem

Yu. N. Grigor'evab, I. V. Ershova

a Institute of Computational Technologies, Siberian Branch of the Russian Academy of Sciences, Novosibirsk, 630090, Russia
b Novosibirsk State University, Novosibirsk, 630090, Russia
Full-text PDF (388 kB) Citations (3)
Abstract: Based on the linear theory, stability of viscous disturbances in a supersonic plane Couette flow of a vibrationally excited gas described by a system of linearized equations of two-temperature gas dynamics including shear and bulk viscosity is studied. It is demonstrated that two sets are identified in the spectrum of the problem of stability of plane waves, similar to the case of a perfect gas. One set consists of viscous acoustic modes, which asymptotically converge to even and odd inviscid acoustic modes at high Reynolds numbers. The eigenvalues from the other set have no asymptotic relationship with the inviscid problem and are characterized by large damping decrements. Two most unstable viscous acoustic modes (I and II) are identified; the limits of these modes were considered previously in the inviscid approximation. It is shown that there are domains in the space of parameters for both modes, where the presence of viscosity induces appreciable destabilization of the flow. Moreover, the growth rates of disturbances are appreciably greater than the corresponding values for the inviscid flow, while thermal excitation in the entire considered range of parameters increases the stability of the viscous flow. For a vibrationally excited gas, the critical Reynolds number as a function of the thermal nonequilibrium degree is found to be greater by 12% than for a perfect gas.
Keywords: linear stability theory, vibrational relaxation, two-temperature aerodynamics, disturbance modes.
Funding agency Grant number
Russian Foundation for Basic Research 14-01-00274а
Received: 17.11.2014
English version:
Journal of Applied Mechanics and Technical Physics, 2016, Volume 57, Issue 2, Pages 247–257
DOI: https://doi.org/10.1134/S0021894416020073
Bibliographic databases:
Document Type: Article
UDC: 532.5:532.517.4
Language: Russian
Citation: Yu. N. Grigor'ev, I. V. Ershov, “Linear stability of the Couette flow of a vibrationally excited gas. 2. Viscous problem”, Prikl. Mekh. Tekh. Fiz., 57:2 (2016), 64–75; J. Appl. Mech. Tech. Phys., 57:2 (2016), 247–257
Citation in format AMSBIB
\Bibitem{GriErs16}
\by Yu.~N.~Grigor'ev, I.~V.~Ershov
\paper Linear stability of the Couette flow of a vibrationally excited gas. 2. Viscous problem
\jour Prikl. Mekh. Tekh. Fiz.
\yr 2016
\vol 57
\issue 2
\pages 64--75
\mathnet{http://mi.mathnet.ru/pmtf856}
\crossref{https://doi.org/10.15372/PMTF20160207}
\elib{https://elibrary.ru/item.asp?id=26040222}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 2016
\vol 57
\issue 2
\pages 247--257
\crossref{https://doi.org/10.1134/S0021894416020073}
Linking options:
  • https://www.mathnet.ru/eng/pmtf856
  • https://www.mathnet.ru/eng/pmtf/v57/i2/p64
    Cycle of papers
    This publication is cited in the following 3 articles:
    Citing articles in Google Scholar: Russian citations, English citations
    Related articles in Google Scholar: Russian articles, English articles
    Prikladnaya Mekhanika i Tekhnicheskaya Fizika Prikladnaya Mekhanika i Tekhnicheskaya Fizika
    Statistics & downloads:
    Abstract page:26
    Full-text PDF :5
     
      Contact us:
     Terms of Use  Registration to the website  Logotypes © Steklov Mathematical Institute RAS, 2024