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
Mingazov, B. G.
Issue
Section
Title
File
Vol 12, No 3-1 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
The influence of engineering changes on NOx emission in a gas-turbine endine combustion chamber
(Rus)
Vol 8, No 3-1 (2009): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Features of the new gas turbine aviation engines theory course
(Rus)
Vol 10, No 5 (2011)
ISSUE WITHOUT SECTION
Research of toxic substances emission during water injection into a combustion chamber
(Rus)
Vol 10, No 5 (2011)
ISSUE WITHOUT SECTION
Analysis of combustion models applicability for designing combustion chamber with a large number of nozzles
(Rus)
Vol 10, No 3-2 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Simulation of turbulent flow in simple and complex diffuser channels
(Rus)
Vol 20, No 3 (2021)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Design and development of combustion chambers for gas turbine engines based on calculations of various levels of complexity
(Rus)
Vol 23, No 1 (2024)
MECHANICAL ENGINEERING
Determination of completeness of combustion, temperature and emission characteristics in a swirl flow based on the theory of turbulent combustion
(Rus)
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