VESTNIK of Samara University.
Aerospace and Mechanical Engineering
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
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Combustion chamber
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algorithm
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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
Stadnik, D. M.
Issue
Section
Title
File
Vol 12, No 1 (2013)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Test rig for a hydraulic drive under switched inertance control
(Rus)
Vol 11, No 3-2 (2012): Special Issue
CONFERENCE MATERIALS
Switched-reactance control of pressure and flow as a way to increase energy efficiency of hydraulic drives – a state-of the-art review
(Rus)
Vol 11, No 4 (2012)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Stabilization of a pilot-operated gas pressure control valve by placing a throttle at the inlet
(Rus)
Vol 14, No 1 (2015)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Study of characteristics of the launch vehicle fuel line gas damper
(Rus)
Vol 15, No 4 (2016)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Procedure of designing a pilot operated gas pressure regulator for launch vehicle fuel tanks
(Rus)
Vol 18, No 1 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Imitation models of aircraft hydraulic units with account for typical faults
(Rus)
Vol 19, No 2 (2020)
MECHANICAL ENGINEERING
Calculating the dynamic error in measurement of electrohydromechanical system parameters, taking into account the operating speed of sensors
(Rus)
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