Abstract:
In this paper we present a wingtip vortex numerical study in the supersonic regime at a wide distance from the wing with the Mach number M=3M=3. The wing incidence is 10∘10∘. Reynolds's averaged Navier–Stokes equations with the Spalart–Allmaras turbulence model were used to describe the flow. Numerical simulations were made in Keldysh Institute of Applied Mathematics Russian Academy of Sciences. A parallel implementation of algorithms for simulating turbulent flows on multiprocessor computer systems was used.
Citation:
A. A. Davydov, T. V. Konstantinovskaya, A. E. Lutsky, “Numerical simulation of a vortex wake behind a wing at a wide distance from the wing in supersonic flow”, Keldysh Institute preprints, 2017, 095, 15 pp.
\Bibitem{DavKonLut17}
\by A.~A.~Davydov, T.~V.~Konstantinovskaya, A.~E.~Lutsky
\paper Numerical simulation of a vortex wake behind a wing at a wide distance from the wing in supersonic flow
\jour Keldysh Institute preprints
\yr 2017
\papernumber 095
\totalpages 15
\mathnet{http://mi.mathnet.ru/ipmp2311}
\crossref{https://doi.org/10.20948/prepr-2017-95}
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https://www.mathnet.ru/eng/ipmp/y2017/p95
This publication is cited in the following 1 articles:
V. E. Borisov, A. A. Davydov, T. V. Konstantinovskaya, A. E. Lutskii, A. M. Shevchenko, A. S. Shmakov, “Modelirovanie sverkhzvukovogo techeniya v slede za krylom pri M=2M=2–44”, Preprinty IPM im. M. V. Keldysha, 2018, 050, 19 pp.
Citation in format AMSBIB
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