Teplofizika vysokikh temperatur
RUS  ENG    JOURNALS   PEOPLE   ORGANISATIONS   CONFERENCES   SEMINARS   VIDEO LIBRARY   PACKAGE AMSBIB  
General information
Latest issue
Forthcoming papers
Archive
Impact factor
Guidelines for authors
Submit a manuscript

Search papers
Search references

RSS
Latest issue
Current issues
Archive issues
What is RSS


TVT:
Year:
Volume:
Issue:
Page:
Find




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

Teplofizika vysokikh temperatur, 2020, Volume 58, Issue 6, paper published in the English version journal (Mi tvt11302)  
This article is cited in 4 scientific papers (total in 4 papers)

Papers published in the English version of the journal
Heat and Mass Transfer and Physical Gasdynamics

Experimental research of gasdynamic liquid drops breakup in the supersonic flow with an oblique shock wave

K. J. Arefyevabc, O. V. Gus'kovab, A. N. Prokhorovab, A. S. Savel'evad, E. E. Sonad, K. Gauthame, D. Same, K. T. Sonue, T. M. Muruganandame

a Moscow Institute of Physics and Technology
b Central Institute of Aviation Motors, State Scientific Center of Russian Federation, Moscow
c Bauman Moscow State Technical University
d Joint Institute for High Temperatures, Russian Academy of Sciences, Moscow
e Indian Institute of Technology Madras
Citations (4)
Abstract: This paper is devoted to understanding gasdynamic liquid drops breakup in a supersonic flow with presence of an oblique shock wave. An experimental facility, diagnostic tools and an experimental methodology are presented as well as numerical simulations results. Computations and experiments were used to get flow parameters in the duct with supersonic flow at Mach numbers $2.0$, $2.5$, and $3.0$. The droplets were made to interact with a single oblique shock wave generated by a wedge in the test section. Experimental data are obtained for the change in diameter of the droplets and the change in speed of droplets in a supersonic flow at the three Mach numbers. The data are presented for an initial Weber number over the range of $16$–$115$. It is shown that the mass loss rate of droplets are quadratically related to the Weber number, irrespective of the presence of oblique shock.
Funding agency Grant number
Russian Science Foundation 19-49-02031
Department of Science and Technology, India DST/INT/RUS/RSF/P-37
Research was performed at the expense of the grant of the Russian scientific fund (project no. 19-49-02031) and DST funding sanction no. DST/INT/RUS/RSF/P-37.
Received: 03.12.2019
Revised: 05.03.2020
Accepted: 10.03.2020
English version:
High Temperature, 2020, Volume 58, Issue 6, Pages 884–892
DOI: https://doi.org/10.1134/S0018151X20060036
Bibliographic databases:
Document Type: Article
Language: English
Citation: K. J. Arefyev, O. V. Gus'kov, A. N. Prokhorov, A. S. Savel'ev, E. E. Son, K. Gautham, D. Sam, K. T. Sonu, T. M. Muruganandam, “Experimental research of gasdynamic liquid drops breakup in the supersonic flow with an oblique shock wave”, High Temperature, 58:6 (2020), 884–892
Citation in format AMSBIB
\Bibitem{AreGusPro20}
\by K.~J.~Arefyev, O.~V.~Gus'kov, A.~N.~Prokhorov, A.~S.~Savel'ev, E.~E.~Son, K. Gautham, D. Sam, K. T. Sonu, T. M. Muruganandam
\paper Experimental research of gasdynamic liquid drops breakup in the supersonic flow with an oblique shock wave
\jour High Temperature
\yr 2020
\vol 58
\issue 6
\pages 884--892
\mathnet{http://mi.mathnet.ru/tvt11302}
\crossref{https://doi.org/10.1134/S0018151X20060036}
\isi{https://gateway.webofknowledge.com/gateway/Gateway.cgi?GWVersion=2&SrcApp=Publons&SrcAuth=Publons_CEL&DestLinkType=FullRecord&DestApp=WOS_CPL&KeyUT=000599785600001}
\elib{https://elibrary.ru/item.asp?id=45081951}
\scopus{https://www.scopus.com/record/display.url?origin=inward&eid=2-s2.0-85097678516}
Linking options:
  • https://www.mathnet.ru/eng/tvt11302
    • This publication is cited in the following 4 articles:
    Citing articles in Google Scholar: Russian citations, English citations
    Related articles in Google Scholar: Russian articles, English articles
    		Teplofizika vysokikh temperatur Teplofizika vysokikh temperatur
    Statistics & downloads:
    Abstract page:100
     
      Contact us:
    		  Terms of Use  Registration to the website  Logotypes © Steklov Mathematical Institute RAS, 2024