Abstract:
Results of an experimental study of density-wave characteristics in the shock layer are presented for the case of a hypersonic nitrogen flow around a model with a two-dimensional compression surface, which is an arc of a circle, and a sharp leading edge. Controlled periodic disturbances developed on the streaky structure are registered by the electron-beam fluorescence technique. The streaky structure of the type of two vortices rotating in the opposite directions is generated in the shock layer by an oblique gas-dynamic whistle.
Citation:
V. M. Aniskin, S. G. Mironov, “Evolution of controlled disturbances in the shock layer on the compression surface”, Prikl. Mekh. Tekh. Fiz., 44:5 (2003), 30–38; J. Appl. Mech. Tech. Phys., 44:5 (2003), 626–633
\Bibitem{AniMir03}
\by V.~M.~Aniskin, S.~G.~Mironov
\paper Evolution of controlled disturbances in the shock layer on the compression surface
\jour Prikl. Mekh. Tekh. Fiz.
\yr 2003
\vol 44
\issue 5
\pages 30--38
\mathnet{http://mi.mathnet.ru/pmtf2534}
\elib{https://elibrary.ru/item.asp?id=17274826}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 2003
\vol 44
\issue 5
\pages 626--633
\crossref{https://doi.org/10.1023/A:1025591917366}
Linking options:
https://www.mathnet.ru/eng/pmtf2534
https://www.mathnet.ru/eng/pmtf/v44/i5/p30
This publication is cited in the following 2 articles:
A. N. Kudryavtsev, S. G. Mironov, T. V. Poplavskaya, I. S. Tsyryulnikov, “Experimental study and direct numerical simulation of the evolution of disturbances in a viscous shock layer on a flat plate”, J. Appl. Mech. Tech. Phys., 47:5 (2006), 617–627
Sergey G. Mironov, Vladimir M. Aniskin, “Experimental study of a hypersonic shock layer stability on a circular surface of compression”, Comptes Rendus. Mécanique, 332:9 (2004), 701
Citation in format AMSBIB
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