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
Leonovich, G. I.
Issue
Section
Title
File
Vol 13, No 2 (2014)
ISSUE WITHOUT SECTION
Airborne LIDAR in ensuring gliding UAV flight mode
(Rus)
Vol 11, No 7 (2012)
ISSUE WITHOUT SECTION
Network digital fiber-optic displacement sensors with closed opticaletwork digital fiber-optic displacement sensors with closet optical chanel
(Rus)
Vol 10, No 5 (2011)
ISSUE WITHOUT SECTION
Heat meter for ASECM, integrated into TP management information system of an industrial enterprise
(Rus)
Vol 10, No 5 (2011)
ISSUE WITHOUT SECTION
Fiber-optical pressure transducer for the UA engine control system
(Rus)
Vol 10, No 7 (2011)
ISSUE WITHOUT SECTION
The fiber-optical multitouch pressure transducer
(Rus)
Vol 16, No 2 (2017)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Some issues of research and development in aviation industry
(Rus)
Vol 10, No 3-3 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Heat meter for AKSUE, integrated into management information system TP of the industrial enterprise
(Rus)
Vol 10, No 3-3 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
The fiber-optical gauge of pressure for the control system of engine BPLA
(Rus)
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