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
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algorithm
blade
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deformation
design
efficiency
endurance limit
experiment
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gas turbine engine
mathematical model
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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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Author Details
Author Details
Sundukov, E. V.
Issue
Section
Title
File
Vol 8, No 3-1 (2009): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Influence of width of the filter on characteristics of discrete components of the spectrum of vibration of gas turbine engine
(Rus)
Vol 8, No 3-1 (2009): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
The analysis of influence of parameters of the spectrum of maxima on efficiency of allocation modulating components of vibration of gas turbine engine
(Rus)
Vol 8, No 3-1 (2009): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Vibration diagnosis not centered shafts connected by gear gearing
(Rus)
Vol 17, No 3 (2018)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Refining methods of vibration diagnostics of wear of turbo-prop engine differential speed reduction unit gear teeth
(Rus)
Vol 18, No 4 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Simulation model of oscillations of the “sun gear – satellites” pair of turboprop engine planetary reduction gearbox in the presence of defects of tooth flanks
(Rus)
Vol 19, No 1 (2020)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Using signals from the gas-turbine engine shaft speed sensor in the diagnosis of the technical condition of its reduction gearbox
(Rus)
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