Preprints of the Keldysh Institute of Applied Mathematics
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


Keldysh Institute preprints:
Year:
Volume:
Issue:
Page:
Find




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

Preprints of the Keldysh Institute of Applied Mathematics, 2018, 050, 19 pp.
DOI: https://doi.org/10.20948/prepr-2018-50 (Mi ipmp2412) 		 
This article is cited in 1 scientific paper (total in 1 paper)

Simulation of supersonic flow in the wake behind a wing at $M=2$–$4$

V. E. Borisov, A. A. Davydov, T. V. Konstantinovskaya, A. E. Lutsky, A. M. Shevchenko, A. S. Shmakov
Full-text PDF (1404 kB) Citations (1)
References:
PDF
HTML
DOI: https://doi.org/10.20948/prepr-2018-50
Abstract: The structure of a supersonic vortex and its features depending on the Mach number $M$ are described in this paper. The investigations are performed both in the near and far regions. Numerical and experimental data are compared. Numerical simulations were carried out in Keldysh Institute of Applied Mathematics RAS using parallel algorithms for turbulent flows simulating. The experimental part was carried out in Khristianovich Institute of Theoretical and Applied Mechanics SB RAS.
Keywords: wingtip vortex, vortex wake, supersonic flow, numerical simulation, experimental investigation, URANS, LES.
Funding agency Grant number
Russian Foundation for Basic Research 16-01-00764_а
17-08-00909_а
Bibliographic databases:
Document Type: Preprint
Language: Russian
Citation: V. E. Borisov, A. A. Davydov, T. V. Konstantinovskaya, A. E. Lutsky, A. M. Shevchenko, A. S. Shmakov, “Simulation of supersonic flow in the wake behind a wing at $M=2$–$4$”, Keldysh Institute preprints, 2018, 050, 19 pp.
Citation in format AMSBIB
\Bibitem{BorDavKon18}
\by V.~E.~Borisov, A.~A.~Davydov, T.~V.~Konstantinovskaya, A.~E.~Lutsky, A.~M.~Shevchenko, A.~S.~Shmakov
\paper Simulation of supersonic flow in the wake behind a wing at $M=2$--$4$
\jour Keldysh Institute preprints
\yr 2018
\papernumber 050
\totalpages 19
\mathnet{http://mi.mathnet.ru/ipmp2412}
\crossref{https://doi.org/10.20948/prepr-2018-50}
\elib{https://elibrary.ru/item.asp?id=32809182}
Linking options:
  • https://www.mathnet.ru/eng/ipmp2412
  • https://www.mathnet.ru/eng/ipmp/y2018/p50
    • This publication is cited in the following 1 articles:
    Citing articles in Google Scholar: Russian citations, English citations
    Related articles in Google Scholar: Russian articles, English articles
    		Препринты Института прикладной математики им. М. В. Келдыша РАН
     
      Contact us:
    		  Terms of Use  Registration to the website  Logotypes © Steklov Mathematical Institute RAS, 2024