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All articles by "Arefyev K.Yu."
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 |
The Method of Experimental Research into the Efficiency of the Working Process in High Speed Solid Fuel Ramjet Engines
| Authors: Aleksandrov V.Yu., Arefyev K.Yu., Prokhorov A.N., Fedotova K.V., Sharov M.S., Yanovskiy L.S. | Published: 11.02.2016 |
| Published in issue: #2(671)/2016 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: ramjet engine, afterburner, experimental study, combustion efficiency, specific impulse |