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Cited article:

A two-dimensional boundary layer model for combustion chamber simulation

Erykson M. S. Costa, Marcio T. Mendonca, Fernando S. Costa and Cesar A. V. Salvador
Journal of the Brazilian Society of Mechanical Sciences and Engineering 46 (5) (2024)
https://doi.org/10.1007/s40430-024-04843-9

Numerical Investigation of Work Cycle Characteristics in the Combustion Chamber of a Lox/Methane Liquid-Propellant Rocket Engine Featuring Reductant Power Gas Combustion

D.A. Sidlerov and S.A. Fedorov
Herald of the Bauman Moscow State Technical University. Series Mechanical Engineering (2 (141)) 43 (2022)
https://doi.org/10.18698/0236-3941-2022-2-43-53

State of the art in the theoretical study of the high-frequency stability of working processes in liquid-propellant rocket combustion chambers

O.V. Pylypenko, O.D. Nikolayev, I.D. Bashliy, N.V. Khoriak and S.I. Dolgopolov
Technical mechanics 2 (2) 5 (2020)
https://doi.org/10.15407/itm2020.02.005

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

S.V. Mosolov and D.A. Sidlerov
Herald of the Bauman Moscow State Technical University. Series Mechanical Engineering (2 (125)) 34 (2019)
https://doi.org/10.18698/0236-3941-2019-2-34-46