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
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine
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Keywords
Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine
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Лукачёв, С. В.
Issue
Section
Title
File
Vol 12, No 3-1 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Correlation and regression model for the assessment of circular non-uniformity of the gas temperature field at the outlet of small gas turbine engine combustion chambers
(Rus)
Vol 12, No 3-1 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Mathematical model for calculating radial non-uniformity of the gas temperature field at the exit of small gas turbine engine combustion chambers
(Rus)
Vol 9, No 1 (2010)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Compulsory ignition of fuel-air mixture in small-sized gas turbine engine combustion chambers
(Rus)
Vol 9, No 1 (2010)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Peculiarities of gas temperature field formation at the exit of small-sized gas turbine engine combustion chambers
(Rus)
Vol 16, No 2 (2017)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Some issues of research and development in aviation industry
(Rus)
Vol 1, No 1 (2002)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Choice of optimum parameters for operation process and the approach to thermal calculation of aircraft piston engines technique in the aircraft system
(Rus)
Vol 20, No 2 (2021)
JUBILEES OF SCIENTISTS
Professor A.P. Merkulov’ role in the process of research and development of the vortex effect
(Rus)
Vol 21, No 3 (2022)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Kinetic model and kerosene surrogate for calculating gas turbine engine emission of carcinogenic hydrocarbons
(Rus)
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