Abstract:
Large-scale streamwise vortices in the vicinity of a perforated wall in the supersonic part of the nozzle are studied. The governing effect of gas inflow through a perforated wall on origination and parameters of streamwise vortices is experimentally established.
Keywords:
large-scale streamwise vortices, supersonic flow, nozzle, porous wall, gas inflow and outflow.
Citation:
V. N. Zaikovskii, S. P. Kiselev, V. P. Kiselev, “Large-scale streamwise vortices in the supersonic part of a permeable nozzle”, Prikl. Mekh. Tekh. Fiz., 46:5 (2005), 68–75; J. Appl. Mech. Tech. Phys., 46:5 (2005), 670–676
\Bibitem{ZaiKisKis05}
\by V.~N.~Zaikovskii, S.~P.~Kiselev, V.~P.~Kiselev
\paper Large-scale streamwise vortices in the supersonic part of a permeable nozzle
\jour Prikl. Mekh. Tekh. Fiz.
\yr 2005
\vol 46
\issue 5
\pages 68--75
\mathnet{http://mi.mathnet.ru/pmtf2302}
\elib{https://elibrary.ru/item.asp?id=15175966}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 2005
\vol 46
\issue 5
\pages 670--676
\crossref{https://doi.org/10.1007/s10808-005-0122-5}
Linking options:
https://www.mathnet.ru/eng/pmtf2302
https://www.mathnet.ru/eng/pmtf/v46/i5/p68
This publication is cited in the following 5 articles:
V. N. Zaikovskii, V. P. Kiselev, S. P. Kiselev, O. V. Belai, G. V. Trubacheev, “Vortex structures in supersonic jets exhausting into a submerged space”, J. Appl. Mech. Tech. Phys., 65:3 (2024), 439–450
Sergey Denisikhin, Vladislav Emelyanov, Konstantin Volkov, “Fluid Dynamics of Thrust Vectorable Submerged Nozzle”, Fluids, 6:8 (2021), 278
Erwin Franquet, Vincent Perrier, Stéphane Gibout, Pascal Bruel, “Free underexpanded jets in a quiescent medium: A review”, Progress in Aerospace Sciences, 77 (2015), 25
V. N. Zaikovskii, S. V. Klinkov, V. F. Kosarev, B. M. Melamed, G. V. Trubacheev, “Control of spray spot shape in cold spray technology. Part 2. Spraying process”, Thermophys. Aeromech., 21:2 (2014), 223
V. N. Zaikovskii, S. V. Klinkov, V. F. Kosarev, B. M. Melamed, G. V. Trubacheev, “Control of spray spot in cold spray technology. Part 1. Gas dynamic aspects”, Thermophys. Aeromech., 21:1 (2014), 105
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