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Publications in Math-Net.Ru
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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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Aerogasdynamic investigations at the Institute of Theoretical and Applied Mechanics in the last decade
Prikl. Mekh. Tekh. Fiz., 38:4 (1997), 46–76
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Instability of a three-dimensional boundary layer on a swept wing
Prikl. Mekh. Tekh. Fiz., 38:3 (1997), 32–38
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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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Resonance flow randomization in the K-regime of boundary-layer transition
Prikl. Mekh. Tekh. Fiz., 31:2 (1990), 83–94
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Progress of aerodynamic research at the Institute of Theoretical and Applied Mechanics, Siberian Branch, Academy of Sciences of the USSR
Prikl. Mekh. Tekh. Fiz., 28:4 (1987), 86–106
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Barrier cooling with multislit and lattice injection in a turbulent boundary layer
Prikl. Mekh. Tekh. Fiz., 7:3 (1966), 149–153
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Heat transfer with tangential fluid injection
Prikl. Mekh. Tekh. Fiz., 7:2 (1966), 135–137
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The effectiveness of a gaseous film on a tubular surface
Prikl. Mekh. Tekh. Fiz., 7:1 (1966), 115–120
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Effectiveness of gas film cooling for a turbulent boundary layer
Prikl. Mekh. Tekh. Fiz., 6:5 (1965), 142–146
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