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All articles by "Sidlerov D.A."

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:

DOI: 10.18698/0236-3941-2022-2-43-53

  
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

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:

DOI: 10.18698/0236-3941-2021-4-19-31

  
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

Investigating the Specifics of Work Cycle Evolution in the Combustion Chamber of an Oxygen/Kerosene Liquid Rocket Engine

Authors: Mosolov S.V., Sidlerov D.A. Published: 22.04.2019
Published in issue: #2(125)/2019  
DOI:

DOI: 10.18698/0236-3941-2019-2-34-46

  
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts  
Keywords: liquid rocket engine, combustion chamber, numerical simulation, kerosene combustion

Investigation of Antipulsation Partitions Influence on the Working Process Development in Oxygen-Kerosene LRE Combustion Chamber with Jet-Centrifugal Injectors by Numerical Simulation

Authors: Mosolov S.V., Sidlerov D.A. Published: 12.04.2017
Published in issue: #2(113)/2017  
DOI:

DOI: 10.18698/0236-3941-2017-2-44-53

  
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts  
Keywords: liquid rocket engine, combustion chamber, numerical simulation, fuel burning

Analysis of the characteristic features of operational process in liquid rocket engine combustion chamber with jet-centrifugal and centrifugal-centrifugal injectors

Authors: Mosolov S.V., Sidlerov D.A. Published: 29.03.2016
Published in issue: #2(107)/2016  
DOI:

DOI: 10.18698/0236-3941-2016-2-60-71

  
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts  
Keywords: liquid rocket engine, combustion chamber, numerical simulation, fuel burning
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