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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 1983, Volume 24, Issue 3, Pages 108–113 (Mi pmtf5669)  
This article is cited in 1 scientific paper (total in 1 paper)

Flow in the hypersonic boundary layer on a finite triangular wing in the presence of an angle of attack

G. N. Dudin

Moscow
Full-text PDF (625 kB) Citations (1)
Received: 14.05.1982
English version:
Journal of Applied Mechanics and Technical Physics, 1983, Volume 24, Issue 3, Pages 383–388
DOI: https://doi.org/10.1007/BF00909759
Document Type: Article
UDC: 533.6.011.55
Language: Russian
Citation: G. N. Dudin, “Flow in the hypersonic boundary layer on a finite triangular wing in the presence of an angle of attack”, Prikl. Mekh. Tekh. Fiz., 24:3 (1983), 108–113; J. Appl. Mech. Tech. Phys., 24:3 (1983), 383–388
Citation in format AMSBIB
\Bibitem{Dud83}
\by G.~N.~Dudin
\paper Flow in the hypersonic boundary layer on a finite triangular wing in the presence of an angle of attack
\jour Prikl. Mekh. Tekh. Fiz.
\yr 1983
\vol 24
\issue 3
\pages 108--113
\mathnet{http://mi.mathnet.ru/pmtf5669}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 1983
\vol 24
\issue 3
\pages 383--388
\crossref{https://doi.org/10.1007/BF00909759}
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  • https://www.mathnet.ru/eng/pmtf5669
  • https://www.mathnet.ru/eng/pmtf/v24/i3/p108
    • This publication is cited in the following 1 articles:
    Citing articles in Google Scholar: Russian citations, English citations
    Related articles in Google Scholar: Russian articles, English articles
    		Prikladnaya Mekhanika i Tekhnicheskaya Fizika Prikladnaya Mekhanika i Tekhnicheskaya Fizika
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