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
Первышин, А. Н.
Issue
Section
Title
File
Vol 5, No 2-2 (2006): Special Issue
TECHNICAL SCIENCES
Impulse & energetic characteristics of insufficiently expanded two-phase combustion-gas stream
(Rus)
Vol 7, No 3 (2008): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Model of varigrained particle stream moving by hypersonic combustion materials investigation
(Rus)
Vol 7, No 3 (2008): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
A model of motion of monodispersible gas-liquid stream is in transzvukovoy of part of rocket chamber
(Rus)
Vol 10, No 1 (2011)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Forming of the structure and properties of titanium alloys according to mechanical properties in the processes of plastic working of metals
(Rus)
Vol 10, No 3-4 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Test bench for investigation of thrusters intra-chamber working processes
(Rus)
Vol 10, No 3-4 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Working process of gaseous fuel metallizator
(Rus)
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