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
Горшкалев, А. А.
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 12, No 3-1 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Method of calculation and analysis of gas flow aerodynamic indices in a vortex wind power plant
(Rus)
Vol 12, No 3-1 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Formation of microvortex gas flows in channels of a block catalyst with coplanar channels
(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
Formation in the channels of the block catalyst the micro vortex gas flows with intense twist
(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 10, No 3-4 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Application CAD/CAE-systems for calculation on durability of details crank rod mechanism of internal combustion engine
(Rus)
Vol 10, No 3-4 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Experienceof CAE/CAD-systems using at designing of internal combustion engine
(Rus)
Vol 20, No 3 (2021)
MECHANICAL ENGINEERING
Development of a methodology for calculating the working process of a small-size two-stroke internal combustion engine
(Rus)
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