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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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
Еленев, В. Д.
Issue
Section
Title
File
Vol 3, No 1 (2004)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Simulation of spacecraft functioning processes with regard to accumulated failures of opboard system elements
(Rus)
Vol 5, No 1 (2006)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Estimation of technogenetic substance flow density distribution in time and spacewith regard to local breakages of space vehicle compartments
(Rus)
Vol 5, No 1 (2006)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Method of choosing parameters of space observation system orbital structure
(Rus)
Vol 10, No 2 (2011)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Determination of mass-power propertions for parametric range of launch vehicle modifications
(Rus)
Vol 11, No 2 (2012)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Principles of constructing systems and objects of a middle-class space rocket complex with increased load-carrying capacity
(Rus)
Vol 13, No 4 (2014)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Accuracy control method for space complex products at the stage of design engineering
(Rus)
Vol 14, No 1 (2015)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Research of small spacecraft dynamiсs taking into account the influence of elastic vibrations of asjacent solar panels and aerodynamic moment
(Rus)
Vol 19, No 1 (2020)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Control over maintaining accuracy of integrity of reference surfaces of spacecraft components in their joint functioning at various stages of design
(Rus)
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