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, 2003, Volume 44, Issue 2, Pages 72–82 (Mi pmtf2481)  
This article is cited in 7 scientific papers (total in 7 papers)

Stability and transition on a swept cylinder in a supersonic flow

A. I. Semisynova, A. V. Fedorovb, V. E. Novikova, N. V. Semenova, A. D. Kosinova

a Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, Novosibirsk, 630090
b Moscow Physicotechnical Institute, Zhukovskii, Moscow Region, 140160
Full-text PDF (324 kB) Citations (7)
Abstract: Results of experimental investigations of the evolution of natural disturbances and laminar–turbulent transition in a supersonic boundary layer on the attachment line of a circular cylinder with a sweep angle of $68^\circ$ and a free-stream Mach number $\mathrm{M}=2$ are presented. The experimental studies are supplemented by calculations of the mean flow and stability characteristics. Flow regimes in the boundary layer on the attachment line are determined by a hot-wire technique as functions of the Reynolds number and height of two-dimensional roughness elements. The results are compared with NASA (Ames) experiments.
Keywords: boundary layer, transition, stability, attachment line on a swept wing.
Received: 27.05.2002
Accepted: 14.10.2002
English version:
Journal of Applied Mechanics and Technical Physics, 2003, Volume 44, Issue 2, Pages 212–220
DOI: https://doi.org/10.1023/A:1022544410399
Bibliographic databases:
Document Type: Article
UDC: 532.526
Language: Russian
Citation: A. I. Semisynov, A. V. Fedorov, V. E. Novikov, N. V. Semenov, A. D. Kosinov, “Stability and transition on a swept cylinder in a supersonic flow”, Prikl. Mekh. Tekh. Fiz., 44:2 (2003), 72–82; J. Appl. Mech. Tech. Phys., 44:2 (2003), 212–220
Citation in format AMSBIB
\Bibitem{SemFedNov03}
\by A.~I.~Semisynov, A.~V.~Fedorov, V.~E.~Novikov, N.~V.~Semenov, A.~D.~Kosinov
\paper Stability and transition on a swept cylinder in a supersonic flow
\jour Prikl. Mekh. Tekh. Fiz.
\yr 2003
\vol 44
\issue 2
\pages 72--82
\mathnet{http://mi.mathnet.ru/pmtf2481}
\elib{https://elibrary.ru/item.asp?id=17274773}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 2003
\vol 44
\issue 2
\pages 212--220
\crossref{https://doi.org/10.1023/A:1022544410399}
Linking options:
  • https://www.mathnet.ru/eng/pmtf2481
  • https://www.mathnet.ru/eng/pmtf/v44/i2/p72
    • This publication is cited in the following 7 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:37
    Full-text PDF :5
     
      Contact us:
    		  Terms of Use  Registration to the website  Logotypes © Steklov Mathematical Institute RAS, 2024