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
Tkachenko, A. Yu.
Issue
Section
Title
File
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Methods and means of aircraft gas turbine engine conceptual design underlying the CAE system «ASTRA»
(Rus)
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Problem formulation of bypass engine parameters optimization with a preselected gas generator
(Rus)
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Influence of the initial design data uncertainty on the choice of optimal working process parameters of gas turbine engine
(Rus)
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Use of the dynamic programming method for solving tasks of GTE management optimization using the aircraft efficiency criteria
(Rus)
Vol 11, No 3-2 (2012): Special Issue
CONFERENCE MATERIALS
Development of a virtual prototype of gasturbine engine at the stage of conceptual thermogasdynamic designusing the CAE-system «ASTRA»
(Rus)
Vol 11, No 3-3 (2012): Special Issue
CONFERENCE MATERIALS
Fulfilment of initial design level of gas turbine engine using the methods of «ASTRA» CAE system
(Rus)
Vol 13, No 5-3 (2014): Special Issue
ISSUE WITHOUT SECTION
Computer-aided system of virtual gas turbine engine testing
(Rus)
Vol 15, No 4 (2016)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Development of an exhaust air turbine engine
(Rus)
Vol 15, No 4 (2016)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Peculiarities of computer modeling of the working process in small gas turbine engines
(Rus)
Vol 18, No 3 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Mathematical model for calculating the mass of a heat exchanger in problems of optimizing the parameters of the working process of aircraft gas turbine engines
(Rus)
Vol 19, No 3 (2020)
MECHANICAL ENGINEERING
Improving the efficiency of aviation turbofan engines by using an intercooler and a recuperative heat exchanger
(Rus)
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