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, 2007, Volume 48, Issue 2, Pages 39–47 (Mi pmtf2010)  
This article is cited in 3 scientific papers (total in 3 papers)

Numerical simulation of stabilization of the boundary layer on a surface with a porous coating in a supersonic separated flow

I. V. Egorova, A. V. Novikovb, A. V. Fedorovb

a Joukowski Central Aerohydrodynamic Institute, Moscow Region, Zhukovskii, 140180
b Moscow Institute of Physics and Technology, Moscow Region, Zhukovskii, 140180
Full-text PDF (332 kB) Citations (3)
Abstract: Stability of a supersonic (M∞=5.373)(M∞=5.373) boundary layer with local separation in a compression corner with a passive porous coating partly absorbing flow perturbations is considered by solving two-dimensional Navier–Stokes equations numerically. The second mode of disturbances of a supersonic boundary layer is demonstrated to be the most important one behind the boundary-layer reattachment point. The possibility of effective stabilization of these disturbances behind the reattachment point with the use of porous coatings is confirmed.
Keywords: Navier–Stokes equations, supersonic flows, boundary layer, stability, numerical simulation, porous coatings.
Received: 07.02.2006
Accepted: 15.05.2006
English version:
Journal of Applied Mechanics and Technical Physics, 2007, Volume 48, Issue 2, Pages 176–183
DOI: https://doi.org/10.1007/s10808-007-0023-x
Bibliographic databases:
Document Type: Article
UDC: 532.526:533.6.011.5
Language: Russian
Citation: I. V. Egorov, A. V. Novikov, A. V. Fedorov, “Numerical simulation of stabilization of the boundary layer on a surface with a porous coating in a supersonic separated flow”, Prikl. Mekh. Tekh. Fiz., 48:2 (2007), 39–47; J. Appl. Mech. Tech. Phys., 48:2 (2007), 176–183
Citation in format AMSBIB
\Bibitem{EgoNovFed07}
\by I.~V.~Egorov, A.~V.~Novikov, A.~V.~Fedorov
\paper Numerical simulation of stabilization of the boundary layer on a surface with a porous coating in a supersonic separated flow
\jour Prikl. Mekh. Tekh. Fiz.
\yr 2007
\vol 48
\issue 2
\pages 39--47
\mathnet{http://mi.mathnet.ru/pmtf2010}
\elib{https://elibrary.ru/item.asp?id=17249414}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 2007
\vol 48
\issue 2
\pages 176--183
\crossref{https://doi.org/10.1007/s10808-007-0023-x}
Linking options:
  • https://www.mathnet.ru/eng/pmtf2010
  • https://www.mathnet.ru/eng/pmtf/v48/i2/p39
    • This publication is cited in the following 3 articles:
    1. S. V. Lukashevich, S. O. Morozov, A. N. Shiplyuk, “Investigations of high-speed boundary layer stabilization by using porous coatings (review)”, J. Appl. Mech. Tech. Phys., 64:4 (2023), 575–590  mathnet  crossref  crossref  elib
    2. I. V. Egorov, A. V. Novikov, A. V. Fedorov, “Direct numerical simulation of the laminar-turbulent transition at hypersonic flow speeds on a supercomputer”, Comput. Math. Math. Phys., 57:8 (2017), 1335–1359  mathnet  mathnet  crossref  crossref  isi  scopus
    3. I. V. Egorov, A. V. Novikov, “Direct numerical simulation of laminar-turbulent flow over a flat plate at hypersonic flow speeds”, Comput. Math. Math. Phys., 56:6 (2016), 1048–1064  mathnet  mathnet  crossref  crossref  isi  scopus
    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:58
    Full-text PDF :20
     
      Contact us:
    math-net2025_04@mi-ras.ru     		 Terms of Use  Registration to the website  Logotypes © Steklov Mathematical Institute RAS, 2025