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
Маркушин, А. Н.
Issue
Section
Title
File
Vol 12, No 3-1 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Test benches for researching the processes and operational development of low emission gas turbine engine combustion chambers
(Rus)
Vol 12, No 3-1 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Analyzing the quality of preparing fuel-air mixture and its influence on NOx in a low emission gas turbine engine combustion chamber
(Rus)
Vol 8, No 3-1 (2009): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Technical solutions of NOx decrease in traditional combustion chamber of GTE NK-16ST
(Rus)
Vol 10, No 3-1 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
The influence of burner design on the characteristics of the combustion chamber with gaseous fuels
(Rus)
Vol 12, No 3-2 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Emission characteristics and temperature non-uniformity at the outlet of the gas turbine engine combustion chamber
(Rus)
Vol 10, No 5 (2011)
ISSUE WITHOUT SECTION
Development and research of a low-toxic combustion chamber of a stationary GTE
(Rus)
Vol 15, No 3 (2016)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Investigation of the gas turbine engine combustion chamber workflow
(Rus)
Vol 15, No 3 (2016)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Influence of the burner form on the combustion chamber outlet temperature field ripple for different modes of operation of gas turbine engines
(Rus)
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