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
Лавров, В. Н.
Issue
Section
Title
File
Vol 1, No 2 (2002): Special Issue
ISSUE WITHOUT SECTION
Experience of design and lines of further improvement of gas turbine engine low-emission combustion chambers
(Rus)
Vol 6, No 2 (2007): Special Issue
TECHNICAL SCIENCES
Numerical simulation of working process in afterburner chamber of vapour gas machine with NK-37 engine
(Rus)
Vol 6, No 2 (2007): Special Issue
TECHNICAL SCIENCES
Developing of low emission fuel burning system in gas turbine engines
(Rus)
Vol 12, No 3-2 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Results of primary operation of NK-37 engine low emission combustion system
(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)
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