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All articles by "Aleksandrov V.Yu."
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 |
Numerical Simulation of Heat Transfer and Determination of Thermal and Hydraulic Characteristics in a Coiled Test Bench Heat Exchanger
Authors: Aleksandrov V.Yu., Koroleva A.P., Kukshinov N.V., Frantsuzov M.S. | Published: 23.11.2017 |
Published in issue: #11(692)/2017 | |
Category: Aviation, Rocket and Technology | |
Keywords: coiled heat exchanger, thermal and hydraulic characteristics, heat exchange surface, conjugate problem, numerical simulation |
An Experimental Study of Electrophysical Characteristics of Gas Flow when Bench Testing Elements of Flow Ducts in Ramjets
Authors: Rudinskiy A.V., Aleksandrov V.Yu., Yagodnikov D.A. | Published: 18.04.2017 |
Published in issue: #4(685)/2017 | |
Category: Technology and Process Machines | |
Keywords: ramjet engine, fire tests, electrophysical diagnostics, gas flow magnetometer, magnetic field strength |
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 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 |
Numerical analysis of a gas veil cooling system for high-aspect-ratio transonic cylindrical channels
Authors: Voronetskiy A.V., Aleksandrov V.Yu., Arefyev K.Yu. | Published: 21.03.2014 |
Published in issue: #3(648)/2014 | |
Category: Calculation and Design of Machinery | |
Keywords: gas generator, veil cooling, transonic flow, mathematical modeling. |