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SMALL ICING WIND TUNNEL BASED AT THE KHRISTIANOVICH INSTITUTE OF THEORETICAL AND APPLIED MECHANICS OF THE SIBERIAN BRANCH OF THE RUSSIAN ACADEMY OF SCIENCES.
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- Journal of Applied Mechanics & Technical Physics, 2023, v. 64, n. 6, p. 1015, doi. 10.1134/S0021894423060111
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INVESTIGATIONS OF HIGH-SPEED BOUNDARY LAYER STABILIZATION BY USING POROUS COATINGS (REVIEW).
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- Journal of Applied Mechanics & Technical Physics, 2023, v. 64, n. 4, p. 575, doi. 10.1134/S002189442304003X
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Numerical design of multimodal axisymmetric hypersonic nozzles for wind tunnels.
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- Journal of Applied Mechanics & Technical Physics, 2010, v. 51, n. 2, p. 218, doi. 10.1007/s10808-010-0031-0
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Generation and registration of disturbances in a gas flow. 2. Experiments with arrays of tubular microheaters and microsensors.
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- Journal of Applied Mechanics & Technical Physics, 2009, v. 50, n. 3, p. 454, doi. 10.1007/s10808-009-0060-8
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Effect of Porous Coatings on Stability of Hypersonic Boundary Layers.
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- Journal of Applied Mechanics & Technical Physics, 2004, v. 45, n. 2, p. 286, doi. 10.1023/B:JAMT.0000017593.33499.c4
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Nonlinear Mechanisms of the Initial Stage of the Laminar–Turbulent Transition at Hypersonic Velocities.
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- Journal of Applied Mechanics & Technical Physics, 2003, v. 44, n. 5, p. 654, doi. 10.1023/A:1025500219183
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Optimal Method for Heat‐Flow Registration.
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- Journal of Applied Mechanics & Technical Physics, 2003, v. 44, n. 4, p. 596, doi. 10.1023/A:1024269612511
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Experimental and Numerical Study of a Hypersonic Separated Flow in the Vicinity of a Cone‐Flare Model.
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- Journal of Applied Mechanics & Technical Physics, 2002, v. 43, n. 6, p. 867, doi. 10.1023/A:1020716621104
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Relaminarization of a turbulent boundary layer with a mach number M∞=4.
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- Journal of Applied Mechanics & Technical Physics, 2002, v. 43, n. 1, p. 76, doi. 10.1023/A:1013914212127
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Experimental Investigation of Stability of a Hypersonic Boundary Layer on a Cone–Flare Model.
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- Journal of Applied Mechanics & Technical Physics, 2001, v. 42, n. 4, p. 589, doi. 10.1023/A:1019239327496
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Development of Natural Disturbances in a Hypersonic Boundary Layer on a Sharp Cone.
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- Journal of Applied Mechanics & Technical Physics, 2001, v. 42, n. 1, p. 57, doi. 10.1023/A:1018852410488
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Stabilization of a Hypersonic Boundary Layer by Ultrasound-Absorbing Coatings with a Regular Microstructure.
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- Doklady Physics, 2004, v. 49, n. 12, p. 763, doi. 10.1134/1.1848635
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Stabilization of a Hypersonic Boundary Layer by Ultrasound-Absorbing Coatings.
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- Doklady Physics, 2002, v. 47, n. 5, p. 401, doi. 10.1134/1.1484415
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Stability of a Hypersonic Boundary Layer with a Pressure Gradient.
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- Doklady Physics, 2000, v. 45, n. 4, p. 179, doi. 10.1134/1.171736
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Leading-edge receptivity of a hypersonic boundary layer on a flat plate.
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- Journal of Fluid Mechanics, 2001, v. 426, p. 73, doi. 10.1017/s0022112000002147
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Wind Tunnel Testing of a Detonation Ramjet Model at Approach Air Stream Mach Number 5.7 and a Stagnation Temperature of 1500 K.
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- Doklady Physical Chemistry, 2018, v. 481, n. 1, p. 100, doi. 10.1134/S0012501618070035
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Growth and breakdown of wave packets in a high-speed boundary layer.
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- Journal of Fluid Mechanics, 2016, v. 806, p. 1, doi. 10.1017/jfm.2016.524
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- Article