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
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gas turbine engine
mathematical model
modeling
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residual stresses
simulation
structure
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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
Васильев, А. Ю.
Issue
Section
Title
File
Vol 1, No 2 (2002): Special Issue
ISSUE WITHOUT SECTION
Investigation of fuel spraying and mixing in the head of nk-type engine combustor
pdf
(Rus)
Vol 1, No 2 (2002): Special Issue
ISSUE WITHOUT SECTION
Experimental determination of characteristics of pneumatic atomizers and their correlation with calculation results
(Rus)
Vol 5, No 2-2 (2006): Special Issue
TECHNICAL SCIENCES
Design and experimental investigation of combustors atomizing device
(Rus)
Vol 6, No 2 (2007): Special Issue
TECHNICAL SCIENCES
Diagnostics of quality mixing in spray of the fuel nozzles by optical methods
(Rus)
Vol 6, No 2 (2007): Special Issue
TECHNICAL SCIENCES
Comparisons of performances of various injector types used air flow
(Rus)
Vol 12, No 3-2 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Development of pneumatic- type starting nozzles for a full-scale low emission combustion chamber
(Rus)
Vol 12, No 3-2 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Peculiarities of application of biofuel mixture in combustion chambers of modern gas turbine engines
(Rus)
Vol 10, No 5 (2011)
ISSUE WITHOUT SECTION
Experimental investigations of fluid atomization by model frontal devices of combustion chambers
(Rus)
Vol 10, No 5 (2011)
ISSUE WITHOUT SECTION
Design and investigation of a pneumatic atomizer as applied to a low emission combustion chamber of a promising gas-turbine engine
(Rus)
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