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
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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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
Абрашкин, В. Ю.
Issue
Section
Title
File
Vol 12, No 3-1 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Correlation and regression model for the assessment of circular non-uniformity of the gas temperature field at the outlet of small gas turbine engine combustion chambers
(Rus)
Vol 12, No 3-1 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Mathematical model for calculating radial non-uniformity of the gas temperature field at the exit of small gas turbine engine combustion chambers
(Rus)
Vol 12, No 3-1 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Development of an algorithm of design calculation of a combustion chamber for microturbine electric power plants
(Rus)
Vol 10, No 5 (2011)
ISSUE WITHOUT SECTION
Modeling of propane combustion processes in case of converting a GTE combustion chamber to gaseous fuel
(Rus)
Vol 10, No 5 (2011)
ISSUE WITHOUT SECTION
Simulation of aerodynamic structure of the flow in the combustion chamber of a small-size gas turbine engine with the help of CAE–systems
(Rus)
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