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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Spacecraft
algorithm
blade
combustion chamber
deformation
design
efficiency
endurance limit
experiment
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gas turbine engine
mathematical model
modeling
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residual stresses
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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
Тюгашев, А. А.
Issue
Section
Title
File
Vol 3, No 1 (2004)
CYBERNETICS AND INFORMATION SCIENCE
Method of designing reliable real-time control algorithms for spacecraft
(Rus)
Vol 6, No 1 (2007)
CYBERNETICS AND INFORMATION SCIENCE
Computer-aided specification, verification and synshesis of control programmes on the basis of logical and algebraic approaches
(Rus)
Vol 9, No 2 (2010): Special Issue
CONTROL, COMPUTER SCIENCE AND INFORMATION SCIENCE
Usage of the graphical languages in lifecycle of embedded software for spacecrafts
(Rus)
Vol 10, No 2 (2011)
CONTROL, COMPUTER SCIENCE AND INFORMATION SCIENCE
Constructing the specification for the on-board realtime control algorithm
(Rus)
Vol 11, No 1 (2012)
CONTROL, COMPUTER SCIENCE AND INFORMATION SCIENCE
Visual approach to verifictaion of real-time control software
(Rus)
Vol 11, No 7 (2012)
ISSUE WITHOUT SECTION
Real-time control algorithms requirements verification mathematical model implementation in visual design computer-aided system
(Rus)
Vol 14, No 2 (2015)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Computational algorithm of forming program motion in a scheduled turn of small spacecraft
(Rus)
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