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Matematicheskoe modelirovanie, 2008, Volume 20, Number 6, Pages 23–34 (Mi mm2436)  

This article is cited in 4 scientific papers (total in 4 papers)

The aerodynamics of hypersonic flight vehicles under a surface mass transfer

N. I. Sidnyaev

N. E. Bauman Moscow State Technical University
Full-text PDF (413 kB) Citations (4)
References:
Abstract: In the article the results of researches of aerodynamic properties of the pattern of a high-speed flight vehicle are presented, which body is executed in the form of a body of revolution by the way of different combinations of conical bodies, for example, with the blunt permeable conical nose if there is an active thermal shield, central cylindrical or poorly conical plot and conical tailplane. The structures of pressure distribution on a surface of a body are received at different attack angles permitting to receive the information on dynamic characteristics of a flight vehicle and reactance.
Received: 28.07.2006
English version:
Mathematical Models and Computer Simulations, 2009, Volume 1, Issue 3, Pages 343–352
DOI: https://doi.org/10.1134/S2070048209030016
Bibliographic databases:
Language: Russian
Citation: N. I. Sidnyaev, “The aerodynamics of hypersonic flight vehicles under a surface mass transfer”, Mat. Model., 20:6 (2008), 23–34; Math. Models Comput. Simul., 1:3 (2009), 343–352
Citation in format AMSBIB
\Bibitem{Sid08}
\by N.~I.~Sidnyaev
\paper The aerodynamics of hypersonic flight vehicles under a surface mass transfer
\jour Mat. Model.
\yr 2008
\vol 20
\issue 6
\pages 23--34
\mathnet{http://mi.mathnet.ru/mm2436}
\zmath{https://zbmath.org/?q=an:1150.76432}
\transl
\jour Math. Models Comput. Simul.
\yr 2009
\vol 1
\issue 3
\pages 343--352
\crossref{https://doi.org/10.1134/S2070048209030016}
\scopus{https://www.scopus.com/record/display.url?origin=inward&eid=2-s2.0-84923838523}
Linking options:
  • https://www.mathnet.ru/eng/mm2436
  • https://www.mathnet.ru/eng/mm/v20/i6/p23
  • This publication is cited in the following 4 articles:
    1. Cong Zh., Chen R., He Z., “Numerical Modeling of Em Scattering From Plasma Sheath: a Review”, Eng. Anal. Bound. Elem., 135 (2022), 73–92  crossref  mathscinet  isi
    2. N. I. Sidnyaev, “Methods for Calculating the Influence of the Electrodynamic Field in the Ionosphere on a Spacecraft”, Cosmic Res, 60:3 (2022), 165  crossref
    3. N. I. Sidnyaev, N. M. Gordeeva, “The asymptotic theory of flows for the near wake of an axisymmetric body”, J. Appl. Industr. Math., 9:1 (2015), 110–118  mathnet  mathnet  crossref
    4. Fomin V.M., Zapryagaev V.I., Lokotko A.V., Volkov V.F., “Effect of distributed gas injection on aerodynamic characteristics of a body of revolution in a supersonic flow”, J. Appl. Mech. Tech. Phys., 53:3 (2012), 333–339  crossref  adsnasa  isi  elib  elib  scopus
    Citing articles in Google Scholar: Russian citations, English citations
    Related articles in Google Scholar: Russian articles, English articles
    Математическое моделирование
    Statistics & downloads:
    Abstract page:735
    Full-text PDF :340
    References:83
    First page:19
     
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