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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 2017, Volume 58, Issue 6, Pages 23–40
DOI: https://doi.org/10.15372/PMTF20170603
(Mi pmtf636)
 

This article is cited in 52 scientific papers (total in 52 papers)

Effect of small bluntness on the formation of Görtler vortices in a supersonic flow around a compression corner

P. V. Chuvakhovab, V. Ya. Borovoya, I. V. Egorovab, V. N. Radchenkoa, H. Olivierc, A. Rogeliac

a Central Aerohydrodynamic Institute
b Moscow Institute of Physics and Technology, Dolgoprudnyi, 141700, Russia
c Rhenish-Westphalian Technical University, Aachen, 52056, Germany
Abstract: The influence of small cylindrical bluntness of the leading edge of a flat plate on the formation of spatial structures in a nominally two-dimensional supersonic flow in a compression corner at the Mach number M8 and a laminar state of the undisturbed boundary layer is studied by the method of temperature-sensitive paints. Streamwise vortices are found in the region of reattachment of the separated flow in a wide range of Reynolds numbers (0.151062.55106) for various angles of flow deflection and plate lengths. It is demonstrated that the existence of these vortices induces transverse oscillations of the heat transfer coefficient; the amplitude of these oscillations may reach 30%. The maximum Stanton numbers reaching 80% are observed in the case with significant roughness of the leading edge of the flat plate. Both the maximum Stanton numbers in the reattachment region and the amplitude of transverse oscillations of the Stanton number induced by streamwise vortices are found to decrease significantly in the case of small bluntness of the leading edge. Solutions of three-dimensional Navier–Stokes equations are derived for some test conditions. The computed results are in good agreement with experimental data, which testifies to a significant stabilizing effect of small bluntness on the intensity of streamwise vortices.
Keywords: small bluntness, high-entropy layer, boundary layer, compression corner, Görtler vortices, supersonic flow, flow separation, flow reattachment.
Funding agency Grant number
Russian Foundation for Basic Research 14-01-91332
Received: 23.09.2016
Revised: 02.11.2016
English version:
Journal of Applied Mechanics and Technical Physics, 2017, Volume 58, Issue 6, Pages 975–989
DOI: https://doi.org/10.1134/S0021894417060037
Bibliographic databases:
Document Type: Article
UDC: 533.6.011
Language: Russian
Citation: P. V. Chuvakhov, V. Ya. Borovoy, I. V. Egorov, V. N. Radchenko, H. Olivier, A. Rogelia, “Effect of small bluntness on the formation of Görtler vortices in a supersonic flow around a compression corner”, Prikl. Mekh. Tekh. Fiz., 58:6 (2017), 23–40; J. Appl. Mech. Tech. Phys., 58:6 (2017), 975–989
Citation in format AMSBIB
\Bibitem{ChuBorEgo17}
\by P.~V.~Chuvakhov, V.~Ya.~Borovoy, I.~V.~Egorov, V.~N.~Radchenko, H.~Olivier, A.~Rogelia
\paper Effect of small bluntness on the formation of G\"ortler vortices in a supersonic flow around a compression corner
\jour Prikl. Mekh. Tekh. Fiz.
\yr 2017
\vol 58
\issue 6
\pages 23--40
\mathnet{http://mi.mathnet.ru/pmtf636}
\crossref{https://doi.org/10.15372/PMTF20170603}
\elib{https://elibrary.ru/item.asp?id=30676157}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 2017
\vol 58
\issue 6
\pages 975--989
\crossref{https://doi.org/10.1134/S0021894417060037}
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  • https://www.mathnet.ru/eng/pmtf/v58/i6/p23
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