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Fizika Goreniya i Vzryva, 2014, Volume 50, Issue 2, Pages 24–30 (Mi fgv111)  
This article is cited in 5 scientific papers (total in 5 papers)

Comparison of methods of flight simulation using a combustion heated facility

V. Yu. Alexandrov, D. S. Moseev

Baranov Central Institute of Aviation Motor Development, Moscow, 111116, Russia
Full-text PDF (149 kB) Citations (5)
Abstract: This paper gives the results of a comparative analysis of methods of simulating airflow for specified flight conditions at the inlet of a high-speed scramjet engine using test facilities with combustion heating of the working fluid. Conditions of the adequacy of the compared heating methods were determined from the obtained values of the engine thrust.
Keywords: facility, heating, similarity criterion, combustion products.
Received: 13.02.2013
Revised: 20.05.2013
English version:
Combustion, Explosion and Shock Waves, 2014, Volume 50, Issue 2, Pages 144–149
DOI: https://doi.org/10.1134/S001050821402004X
Bibliographic databases:
Document Type: Article
UDC: 621.452.226.018.2
Language: Russian
Citation: V. Yu. Alexandrov, D. S. Moseev, “Comparison of methods of flight simulation using a combustion heated facility”, Fizika Goreniya i Vzryva, 50:2 (2014), 24–30; Combustion, Explosion and Shock Waves, 50:2 (2014), 144–149
Citation in format AMSBIB
\Bibitem{AleMos14}
\by V.~Yu.~Alexandrov, D.~S.~Moseev
\paper Comparison of methods of flight simulation using a combustion heated facility
\jour Fizika Goreniya i Vzryva
\yr 2014
\vol 50
\issue 2
\pages 24--30
\mathnet{http://mi.mathnet.ru/fgv111}
\elib{https://elibrary.ru/item.asp?id=21937182}
\transl
\jour Combustion, Explosion and Shock Waves
\yr 2014
\vol 50
\issue 2
\pages 144--149
\crossref{https://doi.org/10.1134/S001050821402004X}
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  • https://www.mathnet.ru/eng/fgv/v50/i2/p24
    • This publication is cited in the following 5 articles:
    Citing articles in Google Scholar: Russian citations, English citations
    Related articles in Google Scholar: Russian articles, English articles
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