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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 2015, Volume 56, Issue 5, Pages 111–118
DOI: https://doi.org/10.15372/PMTF20150509 (Mi pmtf902) 		 
This article is cited in 5 scientific papers (total in 5 papers)

Gas-dynamic design of an axisymmetric tunnel air inlet with isentropic compression

V. M. Galkina, D. A. Vnuchkovb, V. I. Zvegintsevb

a Tomsk Polytechnical University, Tomsk, 634050, Russia
b Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch of the Russian Academy of Sciences, Novosibirsk, 630090, Russia
Full-text PDF (572 kB) Citations (5)
DOI: https://doi.org/10.15372/PMTF20150509
Abstract: A method of designing a supersonic axisymmetric tunnel air inlet based on the problem of an inverted flow in an annular nozzle with isentropic expansion is considered. The nozzle contour is constructed by the method of characteristics. Parameters of one inlet for viscous and inviscid gas flows are calculated.
Keywords: supersonic flow, axisymmetric tunnel air inlet, Euler equations, method of characteristics, isentropic expansion, viscous flow.
Received: 19.12.2014
Revised: 01.06.2015
English version:
Journal of Applied Mechanics and Technical Physics, 2015, Volume 56, Issue 5, Pages 831–837
DOI: https://doi.org/10.1134/S0021894415050090
Bibliographic databases:
Document Type: Article
UDC: 519.63 + 533.697.246
Language: Russian
Citation: V. M. Galkin, D. A. Vnuchkov, V. I. Zvegintsev, “Gas-dynamic design of an axisymmetric tunnel air inlet with isentropic compression”, Prikl. Mekh. Tekh. Fiz., 56:5 (2015), 111–118; J. Appl. Mech. Tech. Phys., 56:5 (2015), 831–837
Citation in format AMSBIB
\Bibitem{GalVnuZve15}
\by V.~M.~Galkin, D.~A.~Vnuchkov, V.~I.~Zvegintsev
\paper Gas-dynamic design of an axisymmetric tunnel air inlet with isentropic compression
\jour Prikl. Mekh. Tekh. Fiz.
\yr 2015
\vol 56
\issue 5
\pages 111--118
\mathnet{http://mi.mathnet.ru/pmtf902}
\crossref{https://doi.org/10.15372/PMTF20150509}
\elib{https://elibrary.ru/item.asp?id=25454204}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 2015
\vol 56
\issue 5
\pages 831--837
\crossref{https://doi.org/10.1134/S0021894415050090}
Linking options:
  • https://www.mathnet.ru/eng/pmtf902
  • https://www.mathnet.ru/eng/pmtf/v56/i5/p111
    • This publication is cited in the following 5 articles:
    1. Yue Ma, Mingming Guo, Ye Tian, Jialing Le, “Recent advances and prospects in hypersonic inlet design and intelligent optimization”, Aerospace Science and Technology, 146 (2024), 108953  crossref
    2. O.G. Glotov, “Screening of metal fuels for use in composite propellants for ramjets”, Progress in Aerospace Sciences, 143 (2023), 100954  crossref
    3. Yu.V. Tunik, V.O. Mayorov, “Busemann diffuser for supersonic ramjet engine with detonation combustion of hydrogen-air mixture”, International Journal of Hydrogen Energy, 47:51 (2022), 21828  crossref
    4. D. A. Vnuchkov, V. M. Galkin, V. M. Fomin, V. I. Zvegintsev, INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH (ICMAR 2020), 2351, INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH (ICMAR 2020), 2021, 030061  crossref
    5. V. M. Galkin, V. I. Zvegintsev, D. A. Vnuchkov, “Investigation of annular supersonic inlets with isentropic compression”, Thermophys. Aeromech., 23:5 (2016), 645  crossref
    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
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