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// Prikladnaya Mekhanika i Tekhnicheskaya Fizika
// Archive
Prikl. Mekh. Tekh. Fiz.,
1993
Volume 34,
Issue 5,
Pages
88–94
(Mi pmtf3983)
This article is cited in
1
paper
Numerical calculation of a three-dimensional laminar compressible boundary layer on profiled triangular wings with supersonic front edges
V. N. Vetlutskii
,
T. V. Poplavskaya
Novosibirsk
UDC:
532.526
Received:
03.02.1992
Accepted:
01.10.1992
Fulltext:
PDF file (669 kB)
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English version:
Journal of Applied Mechanics and Technical Physics, 1993,
34
:5,
677–682
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Steklov Math. Inst. of RAS
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