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// Prikladnaya Mekhanika i Tekhnicheskaya Fizika
// Archive
Prikl. Mekh. Tekh. Fiz.,
1985
Volume 26,
Issue 5,
Pages
23–29
(Mi pmtf5346)
This article is cited in
3
papers
Compressible laminar boundary layer on a delta wing with attached shock wave
V. N. Vetlutskii
,
T. V. Poplavskaya
Novosibirsk
UDC:
532.526
Received:
12.07.1984
Fulltext:
PDF file (704 kB)
Cited by
English version:
Journal of Applied Mechanics and Technical Physics, 1985,
26
:5,
624–629
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Steklov Math. Inst. of RAS
, 2025