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All articles by "Chernov G.I."
Analysis of the influence of the choice of refrigerating agent on the energy characteristics of a rotary-plate compressor operating in the field of wet steam of an air conditioning system
| Authors: Sadvakasov D.Kh., Raykovskiy N.A., Chernov G.I., Zhukova E.A., Zhukov A.O. | Published: 03.03.2026 |
| Published in issue: #3(792)/2026 | |
| Category: Mechanical Engineering and Machine Science | Chapter: Hydraulic Machines, Vacuum, Compressor Technology, Hydraulic and Pneumatic Systems | |
| Keywords: refrigerant, wet steam, rotary-plate compressor, refrigeration cycle, flow coefficient, cooling capacity |
Development of a mathematical model of the unlubricated compressor stage of the rotary-vane type with a new tribological configuration
| Authors: Raykovskiy N.A., Kalashnikov A.M., Sadvakasov D.Kh., Chernov G.I., Evdokimov V.S., Kudentsov V.Y. | Published: 13.10.2024 |
| Published in issue: #10(775)/2024 | |
| Category: Mechanical Engineering and Machine Science | Chapter: Hydraulic Machines, Vacuum, Compressor Technology, Hydraulic and Pneumatic Systems | |
| Keywords: compressor stage, rotary-vane compressor, sealing plate, mathematical model |
Theoretical Assessment of the Impact of Cooling and Recovery Systems on Energy Efficiency of Compressor Units Based on Long Stroke Piston Stages
| Authors: Yusha V.L., Busarov S.S., Chernov G.I. | Published: 10.02.2020 |
| Published in issue: #2(719)/2020 | |
| Category: Energy and Electrical Engineering | Chapter: Vacuum and Compressor Technology and Pneumatic Systems | |
| Keywords: low-capacity compressor units, piston long stroke stages, recovery systems, Rankine cycle, dead volume, quasi-isothermal workflow |
Design of a Heat Transfer Intensification System for Hydrocarbon Fuel in the Cooling Channels of the Liquid Rocket Engine
| Authors: Yusha V.L., Chernov G.I., Shcherban K.V. | Published: 06.09.2018 |
| Published in issue: #8(701)/2018 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: liquid rocket engine, strength analysis, thermal analysis, hypersonic aircraft, cooling system, heat transfer intensification systems |