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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 1973, Volume 14, Issue 6, Pages 76–81 (Mi pmtf7393)  
Numerical solution of the problem of the flow of a supersonic gas stream over the upper surface of a delta wing in the expansion region

G. P. Voskresenskii

Moscow
Full-text PDF (1183 kB)
Received: 24.05.1973
English version:
Journal of Applied Mechanics and Technical Physics, 1973, Volume 14, Issue 6, Pages 798–802
DOI: https://doi.org/10.1007/BF00853194
Document Type: Article
UDC: 533.6.011:51
Language: Russian
Citation: G. P. Voskresenskii, “Numerical solution of the problem of the flow of a supersonic gas stream over the upper surface of a delta wing in the expansion region”, Prikl. Mekh. Tekh. Fiz., 14:6 (1973), 76–81; J. Appl. Mech. Tech. Phys., 14:6 (1973), 798–802
Citation in format AMSBIB
\Bibitem{Vos73}
\by G.~P.~Voskresenskii
\paper Numerical solution of the problem of the flow of a supersonic gas stream over the upper surface of a delta wing in the expansion region
\jour Prikl. Mekh. Tekh. Fiz.
\yr 1973
\vol 14
\issue 6
\pages 76--81
\mathnet{http://mi.mathnet.ru/pmtf7393}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 1973
\vol 14
\issue 6
\pages 798--802
\crossref{https://doi.org/10.1007/BF00853194}
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