VESTNIK of Samara University.
Aerospace and Mechanical Engineering
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
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Combustion chamber
Gas turbine engine
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Spacecraft
algorithm
blade
combustion chamber
deformation
design
efficiency
endurance limit
experiment
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gas turbine engine
mathematical model
modeling
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Keywords
Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
deformation
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
structure
turbine
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Author Details
Author Details
Салич, В. Л.
Issue
Section
Title
File
Vol 8, No 3-3 (2009): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Development of advanced low thrust rocket engines with ecologically friendly propellants
(Rus)
Vol 13, No 5-4 (2014): Special Issue
ISSUE WITHOUT SECTION
Development of thruster chamber operating on oxygen-hydrogen fuel
(Rus)
Vol 13, No 5-4 (2014): Special Issue
ISSUE WITHOUT SECTION
Modeling of intrachamber processes in an oxygen-hydrogen thruster
(Rus)
Vol 15, No 4 (2016)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Mathematical modelling of the working process of a hot gas pressure feed system
(Rus)
Vol 17, No 4 (2018)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Experimental research on the development of an “oxygen (gas) + kerosene” – fueled thruster
(Rus)
Vol 18, No 1 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Development of the active gas generator for high altitude firing test benches
(Rus)
Vol 10, No 3-2 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Mixing processe research in 10…15 N thrusters
(Rus)
Vol 10, No 3-2 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
The numerical modelling of processes in combustion chambers of low thrust rocket engines
(Rus)
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