VESTNIK of Samara University.
Aerospace and Mechanical Engineering
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
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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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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
Куценко, Ю. Г.
Issue
Section
Title
File
Vol 1, No 2 (2002): Special Issue
ISSUE WITHOUT SECTION
Using computational gas dynamics methods for the simulation of multicomponent gas flow, combustion and heat exchange in a gas turbine combustion chamber
(Rus)
Vol 5, No 1 (2006)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Application of gas dynamics numerical methods for the analysis of nitrogen oxide formation process and choosing low emission combustor design
(Rus)
Vol 6, No 2 (2007): Special Issue
TECHNICAL SCIENCES
Simulation of lean blow out process inside gas turbine combustor
(Rus)
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