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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 2009, Volume 50, Issue 2, Pages 98–108 (Mi pmtf1721)  
Modeling of supersonic flows near flying vehicle elements

V. M. Kovenya, A. Yu. Slyunyaev

Institute of Computational Technologies, Siberian Division, Russian Academy of Sciences, Novosibirsk, 630090, Russia
Full-text PDF (567 kB)
Abstract: Supersonic flows near flying vehicle elements are calculated in the approximation of the full Navier–Stokes equations for a viscous compressible heat-conducting gas with different values of free-stream. Mach and Reynolds numbers and angles of attack. The main laws of the flow near the lifting surface. and in the inlet are obtained.
Keywords: Navier–Stokes equations, difference scheme, supersonic flow, separation, shock waves.
Received: 29.09.2008
English version:
Journal of Applied Mechanics and Technical Physics, 2009, Volume 50, Issue 2, Pages 251–260
DOI: https://doi.org/10.1007/s10808-009-0034-x
Bibliographic databases:
Document Type: Article
UDC: 533.6
Language: Russian
Citation: V. M. Kovenya, A. Yu. Slyunyaev, “Modeling of supersonic flows near flying vehicle elements”, Prikl. Mekh. Tekh. Fiz., 50:2 (2009), 98–108; J. Appl. Mech. Tech. Phys., 50:2 (2009), 251–260
Citation in format AMSBIB
\Bibitem{KovSly09}
\by V.~M.~Kovenya, A.~Yu.~Slyunyaev
\paper Modeling of supersonic flows near flying vehicle elements
\jour Prikl. Mekh. Tekh. Fiz.
\yr 2009
\vol 50
\issue 2
\pages 98--108
\mathnet{http://mi.mathnet.ru/pmtf1721}
\elib{https://elibrary.ru/item.asp?id=11839333}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 2009
\vol 50
\issue 2
\pages 251--260
\crossref{https://doi.org/10.1007/s10808-009-0034-x}
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