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// Zhurnal Vychislitel'noi Matematiki i Matematicheskoi Fiziki
// Archive
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
UDC:
519.6:533.7
Received:
26.08.1982
Revised:
23.12.1982
Fulltext:
PDF file (2208 kB)
English version:
USSR Computational Mathematics and Mathematical Physics, 1984,
24
:3,
174–183
Bibliographic databases:
©
Steklov Math. Inst. of RAS
, 2025
Fulltext:
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