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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 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
Full-text PDF (700 kB)
Received: 18.02.1993
English version:
Journal of Applied Mechanics and Technical Physics, 1994, Volume 35, Issue 1, Pages 69–74
DOI: https://doi.org/10.1007/BF02369753
Document Type: Article
UDC: 532.526
Language: Russian
Citation: V. N. Vetlutskii, T. V. Poplavskaya, “Computational analysis of a spatial compressed turbulent boundary layer on the upwind side of delta wings under supersonic flow”, Prikl. Mekh. Tekh. Fiz., 35:1 (1994), 68–74; J. Appl. Mech. Tech. Phys., 35:1 (1994), 69–74
Citation in format AMSBIB
\Bibitem{VetPop94}
\by V.~N.~Vetlutskii, T.~V.~Poplavskaya
\paper Computational analysis of a spatial compressed turbulent boundary layer on the upwind side of delta wings under supersonic flow
\jour Prikl. Mekh. Tekh. Fiz.
\yr 1994
\vol 35
\issue 1
\pages 68--74
\mathnet{http://mi.mathnet.ru/pmtf3752}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 1994
\vol 35
\issue 1
\pages 69--74
\crossref{https://doi.org/10.1007/BF02369753}
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