MainCatalogAviation and Rocket-Space EngineeringThermal, Electric Jet Engines, and Power Plants of Aircrafts
Influence of the Droplet Spray Torch Initial Configuration Behind the Aerodynamic Spraying System on Fuel Distribution Uniformity in the Direct-Flow Combustion Chamber
| Authors: Voronetskiy A.V., Batenin I.A. | Published: 10.01.2026 |
| Published in issue: #4(155)/2025 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: aerodynamic spraying system, droplet spray torch, numerical simulation, flow rate intensity, combustion chamber, mean square deviation, distribution uniformity | |
Modernization of the AI-25 Bypass Turbofan Engine Combustion Chamber Module using the Astra CAE-System
| Authors: Aleksentsev A.A., Pelevin V.S., Zubrilin I.A., Filinov E.P. | Published: 10.01.2026 |
| Published in issue: #4(155)/2025 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: сombustion chamber, temperature unevenness, combustion efficiency, hydraulic losses, preliminary design | |
Methodology for Assessing the Abrasive Particles Separation Effect in Axial Compressors on the Aviation Gas Turbine Engine Characteristics: Simulating Separation and Results
| Authors: Popov S.S., Cherkasov A.N., Klepikov D.S. | Published: 16.10.2025 |
| Published in issue: #3(154)/2025 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: compressor, gas turbine engine, separator, setup, CAD, ANSYS, CFD, Fluent | |
Influence of Injecting the Gasification Products of the Thermal Protection Coating of the SRE Nozzle Recessed Part on the Specific Impulse Losses
| Authors: Shaydullin R.A., Sabirzyanov A.N. | Published: 09.04.2025 |
| Published in issue: #1(152)/2025 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: combustion, ammonium perchlorate, polybutadiene rubber, simulation, decomposition, thermal protection coating, decomposition products injection, losses, chemical nonequi-librium, non-stationary ideal mixing reactor, flow reactor | |
Methodology for Assessing Abrasive Particles Separation in the Axial Compressors Influencing Characteristics of the Aerial Vehicle Gas Turbine Engines: Dynamics Simulation in an Axial
| Authors: Popov S.S., Cherkasov A.N., Klepikov D.S. | Published: 08.04.2025 |
| Published in issue: #1(152)/2025 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: erosion, wear, compressor, gas turbine engine, separator, CAD, ANSYS, CFD, CFX | |
Conceptual Design of a Small-Sized Heat Recovery Turboshaft Engine
| Authors: Mikhailov A.E., Mikhailova A.B., Eremenko V.V., Goryukhin M.О., Krasnoperov D.G. | Published: 22.01.2025 |
| Published in issue: #4(151)/2024 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: small-sized gas-turbine engine, heat recovery, recuperator, plate heat exchanger | |
Mathematical Simulation of the Contactless Process in Charging a Multicopter Battery From the External Electromagnetic Field
| Authors: Kim K.K., Koroleva E.B., Vataev A.S., Mikhailov M.V., Soloviev A.S. | Published: 22.01.2025 |
| Published in issue: #4(151)/2024 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: unmanned aerial vehicle, winding, charge, battery, contact wire | |
Numerical Simulation of the NK-38ST Gas Turbine Engine Combustion Chamber CO Emission Depending on the Ambient Temperature
| Authors: Tikhonov O.A., Sabirzyanov A.N., Baklanov A.V. | Published: 18.09.2024 |
| Published in issue: #3(150)/2024 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: gas turbine unit, combustion chamber, mathematical model, numerical simulation, kinetic mechanism, emission | |
Algorithm for Computing the Solid Propellant Rocket Engine with Ballistic Charge in the Aerospace Technology Track Testing
| Authors: Astahov S.A., Kataev A.V., Sizov G.A. | Published: 07.07.2024 |
| Published in issue: #2(149)/2024 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: rocket track, ballistic solid propellant, specific impulse, strength, stiffness, mass limitations | |
Parametric Calculation of the Limiting Characteristics of Electrization of Structural Elements of the Solid Propellant Rocket Engine Exhaust Duct
| Authors: Fedotova K.V., Yagodnikov D.A. | Published: 17.04.2024 |
| Published in issue: #1(148)/2024 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: weakly ionized plasma, electrization, power condensed system, floating potential, double electric layer | |