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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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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Falaleev, S. V.
Issue
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Vol 10, No 2 (2011)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Construction of a promising face gas-dynamic seal of the aircraft engine
(Rus)
Vol 10, No 3-1 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Modelling of an ejector for turbine aeroengines for application in performance synthesis tools
(Rus)
Vol 10, No 3-1 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Problems and prospect of microgasturbines development for unmanned aerial vehicle propulsion
(Rus)
Vol 11, No 3-2 (2012): Special Issue
CONFERENCE MATERIALS
Designing of the aviation engine's hydrodynamic bearing
(Rus)
Vol 11, No 3-3 (2012): Special Issue
CONFERENCE MATERIALS
Building a diagnosis face gas dynamic seals
(Rus)
Vol 14, No 3-2 (2015): Special Issue
ISSUE WITHOUT SECTION
Improving the reliability of radial face seals of aircraft engine rotor supports
(Rus)
Vol 10, No 3-3 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Unification of the design of gasdynamic seal
(Rus)
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