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
Каюков, С. С.
Issue
Section
Title
File
Vol 12, No 3-1 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Modeling direct fuel injection by a multipin nozzle into the ice combustion chamber using CAE/CAD-systems
(Rus)
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Construction and calculation of three-dimensional model threedimensional model of ice combustion chamber for dynamic calculation of heat processes in ANSYS Fluent
(Rus)
Vol 11, No 3-3 (2012): Special Issue
CONFERENCE MATERIALS
Main results of use CAE/CAD-systems in the process of design and calculation of the working processes in internal combustion engine
(Rus)
Vol 14, No 2 (2015)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Strength analysis of internal combustion engine elements by using ANSYS with taking into account heat processes in the combustion chamber
(Rus)
Vol 14, No 2 (2015)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Analysis of the possibility of improving performance characteristics of a solenoid injector for the CommonRail system
(Rus)
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