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Zhurnal Vychislitel'noi Matematiki i Matematicheskoi Fiziki, 1996, Volume 36, Number 9, Pages 134–154 (Mi zvmmf9212)  
The use of transonic slender-body theory to calculate the spatial flow over a wing–fuselage configuration

V. V. Negoda, K. G. Sayadyan

Moscow
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Received: 07.03.1995
Revised: 27.06.1995
Bibliographic databases:
Document Type: Article
UDC: 519.6:533.7
Language: Russian
Citation: V. V. Negoda, K. G. Sayadyan, “The use of transonic slender-body theory to calculate the spatial flow over a wing–fuselage configuration”, Zh. Vychisl. Mat. Mat. Fiz., 36:9 (1996), 134–154; Comput. Math. Math. Phys., 36:9 (1996), 1277–1293
Citation in format AMSBIB
\Bibitem{NegSay96}
\by V.~V.~Negoda, K.~G.~Sayadyan
\paper The use of transonic slender-body theory to calculate the spatial flow over a wing--fuselage configuration
\jour Zh. Vychisl. Mat. Mat. Fiz.
\yr 1996
\vol 36
\issue 9
\pages 134--154
\mathnet{http://mi.mathnet.ru/zvmmf9212}
\zmath{https://zbmath.org/?q=an:0913.76043}
\transl
\jour Comput. Math. Math. Phys.
\yr 1996
\vol 36
\issue 9
\pages 1277--1293
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