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| Issue |
Title |
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| Vol 19, No 4 (2024) |
About Some Features of the Equilibrium Conditions of Formation and Dissociation of Liquefied Gases Hydrates |
Abstract
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N. A. Shostak, M. A. Samarin |
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| Vol 19, No 4 (2024) |
Review of Research on Scenarios of Diffusion Combustion of Hydrogen Microjets During Their Interaction with Each Other |
Abstract
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A. S. Tambovtsev |
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| Vol 19, No 4 (2024) |
Comparison of Airflow Around the Windward and Leeward Sides of an Aircraft Wing with a Straight Leading Edge |
Abstract
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N. S. Alpatskiy, A. M. Pavlenko, B. Yu. Zanin, I. A. Bondarev |
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| Vol 19, No 4 (2024) |
Experimental Study of the Influence of Weak Shock Waves on the Laminar-Turbulent Transition in the Swept Wing Boundary Layer at Mach Number 2.5 |
Abstract
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L. V. Afanasyev, Yu. G. Yermolaev, A. D. Kosinov, N. V. Semionov, A. V. Shmakova, A. A. Yatskikh |
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| Vol 19, No 2 (2024) |
Experimental Study of the Wave Train Development in a Longitudinal Trace in the Fat Plate Boundary Layer at Mach 2.5 |
Abstract
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M. V. Piterimova, A. D. Kosinov, N. V. Semionov, A. A. Yatskikh, A. V. Shmakova, Yu. G. Yermolaev, B. V. Smorodsky |
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| Vol 19, No 1 (2024) |
Towards Flow Visualization in the Region of Air Blowing through the Perforated Section of a Body of Revolution |
Abstract
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V. I. Kornilov, A. A. Pivovarov, A. N. Popkov |
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| Vol 18, No 2 (2023) |
Experimental Study of the Interaction of Controlled Disturbances from Two Sources in the Supersonic Boundary Layer of a Swept Wing |
Abstract
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G. L. Kolosov, A. D. Kosinov, N. V. Semionov, A. A. Yatskikh |
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| Vol 18, No 2 (2023) |
Stability of Supersonic Boundary Layer with Internal Heat Supply and Injection of Homogeneous Gas through a Porous Wall |
Abstract
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S. A. Gaponov |
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| Vol 18, No 1 (2023) |
Study of Self-Excited Pitch Oscillations of Conical-Spherical Body at Mach Number M = 1.75 and Two Moments of Inertia |
Abstract
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N. A. Mishchenko, E. A. Chasovnikov |
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| Vol 17, No 4 (2022) |
Investigation of the Formation and Further Development of Longitudinal Disturbances and Their Secondary Instability on the Flying Wing Model |
Abstract
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V. S. Kaprilevskaya |
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| Vol 17, No 4 (2022) |
On the Methodology for Estimating the Relationship of Disturbances Using Digital Signal Processing in Relation to Measurements in Supersonic Flows |
Abstract
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L. V. Afanasiev, A. D. Kosinov, A. A. Yatskikh, S. A. Shipul, N. V. Semenov |
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| Vol 17, No 4 (2022) |
Features of the Flow Structure in the Boundary Layer on the Flying Wing Model |
Abstract
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A. M. Pavlenko, B. Yu. Zanin, N. S. Alpatskiy, E. A. Melnik |
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| Vol 17, No 3 (2022) |
Study of the Regimes of Diffusive Combustion of a Hydrogen Microjet |
Abstract
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V. V. Kozlov, M. V. Litvinenko, Yu. А. Litvinenko, A. S. Tambovtsev, A. G. Shmakov |
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| Vol 17, No 3 (2022) |
Application of Accelerometers for Measuring Aerodynamic Forces in Short-Term Facilities |
Abstract
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A. A. Maslov, A. V. Starov, I. S. Tsyryulnikov |
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| Vol 17, No 2 (2022) |
Effect of injection of gas with high specific heat capacity on supersonic boundary-layer stability to controlled disturbances |
Abstract
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V. I. Lysenko, B. V. Smorodsky, A. D. Kosinov |
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| Vol 17, No 2 (2022) |
Two-stage carbon condensation model during detonation of high explosives |
Abstract
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I. A. Rubtsov |
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| Vol 17, No 2 (2022) |
Experimental study of effect of a pair of weak shock waves on laminar-turbulent transition in the boundary layer of flat plate at Mach number 2 |
Abstract
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M. V. Piterimova, А. D. Kosinov, N. V. Semionov, A. A. Yatskikh, V. L. Kocharin, Yu. G. Yermolaev |
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| Vol 17, No 1 (2022) |
About the Dynamic Damping Coefficients of a Segmental-Cone Model at Mach M = 2.3. |
Abstract
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N. P. Adamov, N. A. Mishchenko, E. A. Chasovnikov |
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| Vol 17, No 1 (2022) |
Flow of Ethanol into a Medium with Varying Degrees of Rarefaction |
Abstract
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A. S. Yaskin, A. E. Zarvin, V. V. Kalyada, K. A. Dubrovin, V. E. Khudozhitkov |
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| Vol 17, No 1 (2022) |
Optimization of Parameters of Laser Cladding of the Powder Based on Nickel-Aluminium System |
Abstract
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M. A. Gulov |
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