MainCatalogAviation and Rocket-Space EngineeringThermal, Electric Jet Engines, and Power Plants of Aircrafts
Possibilities of Studying the Process of the Metallized Energy Condensed Systems Combustion by the Microwave Radiation Method
| Authors: Yagodnikov D.A., Sukhov A.V., Sergeev A.V., Kozichev V.V., Shostov A.K. | Published: 20.09.2023 |
| Published in issue: #3(146)/2023 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: electromagnetic wave, gasification rate, Rayleigh scattering, secondary radiation, complex reflection coefficient, metal particles | |
Experimental Study of the Carbon Deposits Accumulation in the Oxygen-Methane Model Gas Path
| Authors: Fedorov S.A., Slesarev D.F., Isakov D.V. | Published: 27.03.2023 |
| Published in issue: #1(144)/2023 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: liquid propellant rocket engine, reducing generator gas, carbon deposits, soot | |
Estimation of the Rejection Boundaries of the Spacecraft Schematic Layout by Thermal and Erosive Effects Level of the Electric Rocket Engines Plasma Jets
| Authors: Nadiradze А.B., Dudunov А.А. | Published: 27.03.2023 |
| Published in issue: #1(144)/2023 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: electric rocket engine, plasma jet, thermal effect, erosive effect, allowable effect level, rejection boundary | |
Recuperation of Aircraft Gas Turbine Engines to Solve Problems Land Transport and Energy
| Authors: Benmunach A., Zanabili G., Govorkov A.S. | Published: 11.12.2022 |
| Published in issue: #4(143)/2022 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: gas turbine engines, recuperation, compressor, combustion chamber, turbine, output device | |
Special Aspects of Designing High Temperature Plate Heat Exchangers for Small Gas Turbine Engines
| Authors: Remchukov S.S., Lomazov V.S., Lebedinskiy R.N., Demidyuk I.V., Ptitsyn I.S. | Published: 13.09.2022 |
| Published in issue: #3(142)/2022 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: small-sized gas turbine engine, turboshaft engine, modular plate heat exchanger, turbopropeller engine | |
Numerical Investigation of Work Cycle Characteristics in the Combustion Chamber of a Lox/Methane Liquid-Propellant Rocket Engine Featuring Reductant Power Gas Combustion
| Authors: Sidlerov D.A., Fedorov S.A. | Published: 29.06.2022 |
| Published in issue: #2(141)/2022 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: liquid rocket engine, numerical simulation of combustion, lox/methane fuel | |
Development of Tools for Thermodynamic Calculation of Rocket Engine Characteristics using the Julia Programming Language
| Authors: Belov G.V. | Published: 20.12.2021 |
| Published in issue: #4(139)/2021 | |
| DOI: | |
| Category: Power Engineering | Chapter: Heat Engines | |
| Keywords: combustion products, rocket fuel, thermodynamic modeling | |
Soot Formation Numerical Simulation in Reducing Gas Generators of Oxygen-Methane Liquid Rocket Engines
| Authors: Sidlerov D.A., Fedorov S.A. | Published: 19.12.2021 |
| Published in issue: #4(139)/2021 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: liquid rocket engine, gas generator, numerical simulation, soot formation | |
Heat Exchange and Friction Analysis in Noble Gas Mixtures for Closed Gas Turbines
| Authors: Egorov K.S., Stepanova L.V. | Published: 19.12.2021 |
| Published in issue: #4(139)/2021 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: close gas turbine, noble gases, heat transfer, Prandtl number, mixture of gases | |
Numerical Computation of Specific Impulse and Internal Flow Parameters in Solid Fuel Rocket Motors with Two-Phase Сombustion Products
| Authors: Sultanov T.S., Glebov G.A. | Published: 08.09.2021 |
| Published in issue: #3(138)/2021 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: solid propellant rocket engines, numerical methods, two-phase flows, specific impulse, supersonic nozzle | |