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All articles by "Arefyev K.Yu."
On the issue of increasing the efficiency of the workflow in the combustion chamber of the evaporative type of aviation gas turbine engines when operating on fuel with an anti-turbulent additive
| Authors: Yanovskiy L.S., Arefyev K.Yu., Popov I.M., Abramov M.A., Borovik I.N., Ezhov V.M. | Published: 14.04.2026 |
| Published in issue: #4(793)/2026 | |
| Category: Energy and Electrical Engineering | Chapter: Turbomachines and Piston Engines | |
| Keywords: aircraft engine, kerosene TC-1, polyisobutylene, ignition induction period, combustion coefficient, combustion chamber of an aircraft engine |
A Thermal Strength State Analysis of a Cylindrical Combustion Chamber Manufactured Using Additive Technologies
| Authors: Ushakova E.S., Arefyev K.Yu., Zaikin S.V., Polyanskiy A.R., Isakov V.V. | Published: 10.02.2020 |
| Published in issue: #2(719)/2020 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: additive technologies, stress-strain state, factor of safety, specific heat flux, cooler heating, combustion chamber |
Methodological Aspects of Determining Thrust of Irrotational Air-Breathing Jet Engines in Bench and Flight Tests
| Authors: Semenov V.L., Aleksandrov V.Yu., Prokhorov A.N., Arefyev K.Yu., Kruchkov S.V. | Published: 26.11.2019 |
| Published in issue: #11(716)/2019 | |
| Category: Aviation, Rocket and Technology | Chapter: Inspection and Testing of Aircraft and Aircraft Systems | |
| Keywords: irrotational air-breathing jet engine, high-speed aircraft, engine thrust, specific impulse, pressure loading, numerical model |
The Determination of the Flow Acoustic Characteristics in a Duct with Variable Cross-Section of a Laboratory Unit
| Authors: Arefyev K.Yu., Ilchenko M.A. | Published: 08.10.2018 |
| Published in issue: #9(702)/2018 | |
| Category: Aviation, Rocket and Technology | Chapter: Aerodynamics and Heat Transfer Processes in Aircraft | |
| Keywords: resonant frequencies, velocity oscillations, isentropic acoustic vibrations, thermal anemometer, spectral characteristics |
Modeling Heat Strength Characteristics of Structural Elements of a Solid Propellant Rocket Engine Manufactured Using Prototyping
| Authors: Ushakova E.S., Arefyev K.Yu., Polyanskiy A.R. | Published: 28.04.2018 |
| Published in issue: #4(697)/2018 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: powder prototyping technology, safety factor, temperature conditions of the structure, convective heat transfer, nozzle block |
An Experimental Study of the Influence of Unpredictable Changes in the Form of the Resonant Cavity Leading Edge on the Operating Capacity of the Gas-Dynamic Ignition System
| Authors: Aleksandrov V.Yu., Arefyev K.Yu., Ilchenko M.A. | Published: 24.03.2017 |
| Published in issue: #3(684)/2017 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: gas-dynamic ignition system, pulsation process, heat release intensity, change of form, resonant cavity |
Detonation of Air-Methane Mixture in a Supersonic Crossflow
| Authors: Aleksandrov V.Yu., Arefyev K.Yu., Baskakov A.A., Ilchenko M.A. | Published: 20.02.2017 |
| Published in issue: #2(683)/2017 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: detonation combustion, pressure pulsation, turbulent combustion, experimental study, propagation velocity of detonation wave front, degeneration of detonation |
The Study of Cylindrical Duct Cooling by Solid Hydrocarbon Fuel Gasification Products
| Authors: Arefyev K.Yu., Fedotova K.V., Yanovskiy L.S., Averkov I.S., Baykov A.V. | Published: 27.01.2017 |
| Published in issue: #1(682)/2017 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: one-dimensional mathematical model, thermal state modeling of combustion chamber walls, axisymmetric ramjet duct, combustion chamber, solid hydrocarbon fuel, cooling capacity of gasification products |
The Analysis of Influence of the Nozzle Structure and Fluid Injection Path on the Efficiency of Two-Phase Mixing in a Constant Cross Section Channel
| Authors: Arefyev K.Yu., Voronetskiy A.V., Prokhorov A.N., Suchkov S.A., Filimonov L.A. | Published: 30.06.2016 |
| Published in issue: #7(676)/2016 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: mathematical modeling, fuel injection, droplet fragmentation, droplet evaporation, constant section channel |
Numerical Analysis of the Thermal State of the Resonator in a Gas-Dynamic Ignition System with Two-Phase Fuel Composition
| Authors: Vorozheeva O.A., Arefyev K.Yu. | Published: 11.05.2016 |
| Published in issue: #5(674)/2016 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: thermal state, gas-dynamic ignition system, two-phase fuel composition, mathematical modeling, ethanol, temperature field, resonator, pulsed mode |