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Analysis of the Variable Cross-Section Duct and Straightening Device Geometry Effects on the Hydrogen Combustion Process
| Authors: Guskov O.V., Zakharov V.S., Minko A.V. | Published: 11.06.2021 |
| Published in issue: #7(736)/2021 | |
| Category: Aviation, Rocket and Technology | Chapter: Aerodynamics and Heat Transfer Processes in Aircraft | |
| Keywords: transition channel, combustion chamber, straightening device, hydrogen combustion process, combustion efficiency, numerical simulation |
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 |
Laser Ignition of Liquid-Oxygen–Gaseous-Hydrogen Fuel in a Large-Scale Combustion Chamber
| Authors: Rebrov S.G., Golubev V.A., Kosmachev Y.P., Kosmacheva V.P. | Published: 16.12.2019 |
| Published in issue: #12(717)/2019 | |
| Category: Aviation, Rocket and Technology | Chapter: Inspection and Testing of Aircraft and Aircraft Systems | |
| Keywords: laser ignition, rocket engine, combustion chamber, liquid-oxygen–gaseous-hydrogen, optical breakdown |
Laser Ignition of Oxygen-Hydrocarbon Fuels in Rocket Engines
| Authors: Rebrov S.G., Golubev V.A., Golikov A.N. | Published: 30.07.2018 |
| Published in issue: #7(700)/2018 | |
| Category: Aviation, Rocket and Technology | Chapter: Inspection and Testing of Aircraft and Aircraft Systems | |
| Keywords: laser ignition, rocket fuel, oxygen-kerosene, oxygen-methane, optical breakdown, combustion chamber |
Stoichiometric Gas Turbine Engines
| Authors: Pismennyi V.L. | Published: 26.06.2018 |
| Published in issue: #6(699)/2018 | |
| Category: Aviation, Rocket and Technology | Chapter: Aerodynamics and Heat Transfer Processes in Aircraft | |
| Keywords: gas turbine engines, heat exchanger, stoichiometric GTE, supersonic speed, hypersonic speed, combustion chamber |
Trial Test Results on Intake Manifold Mounting Elements of the Combustion Chamber of the NK-38ST Gas Turbine Engine
| Authors: Baklanov A.V., Neumoin S.P., Vakhitov A.R. | Published: 28.04.2018 |
| Published in issue: #4(697)/2018 | |
| Category: Energy and Electrical Engineering | Chapter: Turbomachines and Combination Turbine Plants | |
| Keywords: fuel manifold, mounting system, combustion chamber, gas turbine engine, fuel pipe strain-gaging |
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 Study of the Workpiece Heating Process during Gas Forming with Back-Pressure
| Authors: Botashev A.Y., Malsugenov R.S., Bisilov N.U., Bayramukov R.A. | Published: 10.08.2016 |
| Published in issue: #8(677)/2016 | |
| Category: Technology and Process Machines | |
| Keywords: gas forming, combustion chamber, fuel mixture, workpiece heating |
The Application of Cyclic Symmetry and the Substructure Method in the Thermal Stress Analysis of the Combustion Chamber of the Liquid-Propellant Rocket Engine with LOX Cooling
| Authors: Korotkaya O.V., Gavryushin S.S. | Published: 20.01.2016 |
| Published in issue: #1(670)/2016 | |
| Category: Technology and Process Machines | |
| Keywords: mathematical modeling, finite element method, substructure, cyclic symmetry, stress-strain state, nozzle, combustion chamber, liquid-propellant rocket engine, cooling channels, LOX-cooling |
Comparing the integral thrust-economic characteristics of ramjets in a wide range of speeds and flight levels
| Authors: Serebryakov D.I., Sidorov R.S., Styazhkin R.V. | Published: 13.11.2014 |
| Published in issue: #11(656)/2014 | |
| Category: Calculation and Design of Machinery | |
| Keywords: ramjet, combustion chamber, thrust, specific impulse, numerical simulation. |