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// Prikladnaya Mekhanika i Tekhnicheskaya Fizika
// Archive
Prikl. Mekh. Tekh. Fiz.,
1994
Volume 35,
Issue 1,
Pages
68–74
(Mi pmtf3752)
Computational analysis of a spatial compressed turbulent boundary layer on the upwind side of delta wings under supersonic flow
V. N. Vetlutskii
,
T. V. Poplavskaya
Novosibirsk
UDC:
532.526
Received:
18.02.1993
Fulltext:
PDF file (700 kB)
English version:
Journal of Applied Mechanics and Technical Physics, 1994,
35
:1,
69–74
©
Steklov Math. Inst. of RAS
, 2025