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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 1996, Volume 37, Issue 1, Pages 114–118 (Mi pmtf3491)  
Calculation of pressure distribution near the leading edge of an airfoil using the discrete-vortex method

D. N. Gorelov

Institute of Information Technologies and Applied Mathematics, Siberian Division, Russian Academy of Sciences, Omsk 644077
Full-text PDF (369 kB)
Received: 28.11.1994
Accepted: 04.01.1995
English version:
Journal of Applied Mechanics and Technical Physics, 1996, Volume 37, Issue 1, Pages 96–100
DOI: https://doi.org/10.1007/BF02369407
Document Type: Article
UDC: 518.12:533.6
Language: Russian
Citation: D. N. Gorelov, “Calculation of pressure distribution near the leading edge of an airfoil using the discrete-vortex method”, Prikl. Mekh. Tekh. Fiz., 37:1 (1996), 114–118; J. Appl. Mech. Tech. Phys., 37:1 (1996), 96–100
Citation in format AMSBIB
\Bibitem{Gor96}
\by D.~N.~Gorelov
\paper Calculation of pressure distribution near the leading edge of an airfoil using the discrete-vortex method
\jour Prikl. Mekh. Tekh. Fiz.
\yr 1996
\vol 37
\issue 1
\pages 114--118
\mathnet{http://mi.mathnet.ru/pmtf3491}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 1996
\vol 37
\issue 1
\pages 96--100
\crossref{https://doi.org/10.1007/BF02369407}
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