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
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
mathematical modeling
modeling
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spacecraft
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Keywords
Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
mathematical modeling
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine
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Author Details
Author Details
Зубрилин, И. А., Самарский государственный аэрокосмический университет имени академика С.П. Королёва (национальный исследовательский университет), Russian Federation
Issue
Section
Title
File
Vol 12, No 3-1 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Influence of the turbine ignition, flame tube suspension and nozzles on the combustion chamber characteristics
(Rus)
Vol 12, No 3-1 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Effect of non-uniform compressor flow parameters on the characteristics of a gas turbine engine combustion chamber
(Rus)
Vol 13, No 1 (2014)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Calculation of hydrodynamic noise in the diffuser of a pulsation damper flow channel
(Rus)
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Vortical gaz-wind-energy plant
(Rus)
Vol 11, No 2 (2012)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Multisprayer low-emission combustion chamber of modern turbojet engines – N. D. Kuznetsov’s creative heritage
(Rus)
Vol 11, No 5-2 (2012): Special Issue
CONFERENCE MATERIALS
Problems and solutions of using computer technologies in designing of combustion chambers GTE
(Rus)
Vol 14, No 2 (2015)
MECHANICAL ENGINEERING AND POWER ENGINEERING
The effect of the way of setting boundary conditions on the results of modeling a flow at the flameholder outlet
(Rus)
Vol 14, No 2 (2015)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Determination of thermal state and modification of the flame tube cooling system with the help of three-dimensional modeling methods
(Rus)
Vol 10, No 5 (2011)
ISSUE WITHOUT SECTION
Vortex gas wind-driven power plant for supplying compressor stations with electrical energy
(Rus)
Vol 10, No 5 (2011)
ISSUE WITHOUT SECTION
Specifying the dimensions of the reverse current area of a 3-D gas-turbine engine combustion chamber model using the ANSYS FLUENT software
(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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