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
Колмакова, Д. А.
Issue
Section
Title
File
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Simulation of aircraft multistage axial turbine working processes taking into account over-shroud leakage flows and blading inflows
(Rus)
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Investigation of effects of multistage compressor final stage blading shape on compressor performance and flow pattern
(Rus)
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Optimization of aircraft seven stage compressor first stages parameters
(Rus)
Vol 11, No 3-2 (2012): Special Issue
CONFERENCE MATERIALS
The results of gas dynamic and strength improvement of turbocharger TK-32 axial turbine
(Rus)
Vol 11, No 3-3 (2012): Special Issue
CONFERENCE MATERIALS
Approaches to parametric models of blade machines formation
(Rus)
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