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
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
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structure
turbine
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Keywords
Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine
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Author Details
Author Details
Пегин, И. В.
Issue
Section
Title
File
Vol 11, No 3-1 (2012): Special Issue
CONFERENCE MATERIALS
Investigation of the possibility of the creation LREST by thrust 400 N with a baffle - centrifugal scheme of NT and NDMG mixing
(Rus)
Vol 13, No 5-1 (2014): Special Issue
ISSUE WITHOUT SECTION
50 n thrust correction engine for the "Luna-resurs" lunar module descent engine
(Rus)
Vol 13, No 5-1 (2014): Special Issue
ISSUE WITHOUT SECTION
Research of the influence of design parameters of a 400 N-thrust low-thrust liquid rocket engine on its energy efficiency
(Rus)
Vol 13, No 5-3 (2014): Special Issue
ISSUE WITHOUT SECTION
Results of experimental studies of parameters of low-thrust rocket engines operating on gaseous oxygen-hydrogen fuel
(Rus)
Vol 13, No 5-3 (2014): Special Issue
ISSUE WITHOUT SECTION
Verification of energy efficiency of a low-thrust liquid-propellant engine with the deflector-centrifugal injecting pattern
(Rus)
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