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Zh. Vychisl. Mat. Mat. Fiz., 1984, Volume 24, Number 6, Pages 900–915 (Mi zvmmf4374)  

A numerical method of calculation of supersonic flow around aircraft wings

G. P. Voskresenskii


Full text: PDF file (2208 kB)

English version:
USSR Computational Mathematics and Mathematical Physics, 1984, 24:3, 174–183

Bibliographic databases:

UDC: 519.6:533.7
Received: 26.08.1982
Revised: 23.12.1982

Citation: G. P. Voskresenskii, “A numerical method of calculation of supersonic flow around aircraft wings”, Zh. Vychisl. Mat. Mat. Fiz., 24:6 (1984), 900–915; U.S.S.R. Comput. Math. Math. Phys., 24:3 (1984), 174–183

Citation in format AMSBIB
\Bibitem{Vos84}
\by G.~P.~Voskresenskii
\paper A numerical method of calculation of supersonic flow around aircraft wings
\jour Zh. Vychisl. Mat. Mat. Fiz.
\yr 1984
\vol 24
\issue 6
\pages 900--915
\mathnet{http://mi.mathnet.ru/zvmmf4374}
\mathscinet{http://www.ams.org/mathscinet-getitem?mr=750100}
\zmath{https://zbmath.org/?q=an:0599.76079}
\transl
\jour U.S.S.R. Comput. Math. Math. Phys.
\yr 1984
\vol 24
\issue 3
\pages 174--183
\crossref{https://doi.org/10.1016/0041-5553(84)90067-3}


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