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
Ильинский, С. А.
Issue
Section
Title
File
Vol 5, No 2-1 (2006): Special Issue
TECHNICAL SCIENCES
About measurement of pulsations of pressure in flowing part GTE
(Rus)
Vol 8, No 3-3 (2009): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Dynamic tests of probes for measurement of pulsations pressure at the raised average pressure
(Rus)
Vol 13, No 1 (2014)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Development of a small-sized acoustic probe for the measurement of pressure pulsations in the gasdynamic duct of gas turbine engines
(Rus)
Vol 10, No 3-1 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
About the probes for measuring pulsations of pressure in the flowing part gas turbine engines
(Rus)
Vol 11, No 1 (2012)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Approximate correlative-spectral analysis of temperature patterns of combustion chambers
(Rus)
Vol 11, No 3-2 (2012): Special Issue
CONFERENCE MATERIALS
On the development of probes for measuring pressure pulsations in the gas-dynamic channel gas generator
(Rus)
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