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Publications in Math-Net.Ru
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Specific features of wave train development in a streamwise disturbance of a supersonic boundary layer
Prikl. Mekh. Tekh. Fiz., 65:4 (2024), 63–82
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Experimental investigation of the evolution of controlled perturbations in a longitudinal vortex generated in a boundary layer on a flat plate at a Mach number $\mathrm{M}=2$
Prikl. Mekh. Tekh. Fiz., 64:4 (2023), 118–129
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An investigation of the influence of the parameters of a pulse discharge on localized disturbances generated in a supersonic boundary layer
Pisma v Zhurnal Tekhnicheskoi Fiziki, 45:5 (2019), 59–62
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Experimental study of nonlinear processes in a swept-wing boundary layer at the Mach number $\mathrm{M}= 2$
Prikl. Mekh. Tekh. Fiz., 55:5 (2014), 45–54
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Evolution of disturbances in a laminarized supersonic boundary layer on a swept wing
Prikl. Mekh. Tekh. Fiz., 49:2 (2008), 40–46
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Experimental study of evolution of disturbances in a supersonic boundary layer on a swept-wing model under controlled conditions
Prikl. Mekh. Tekh. Fiz., 41:1 (2000), 50–56
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“Anomalous” nonlinear wave phenomena in a supersonic boundary layer
Prikl. Mekh. Tekh. Fiz., 40:5 (1999), 91–98
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An experimental study of the nonlinear evolution of instability waves on a flat plate for mach number $\mathrm{M}=3$
Prikl. Mekh. Tekh. Fiz., 38:2 (1997), 107–114
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Instability of a three-dimensional supersonic boundary layer
Prikl. Mekh. Tekh. Fiz., 36:6 (1995), 50–54
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