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
simulation
structure
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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
Сармин, Д. В.
Issue
Section
Title
File
Vol 12, No 3-1 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Comparison of mass properties of high- pressure cylinders with cryogenic fill for a throttle cooling system
(Rus)
Vol 12, No 3-1 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Evaluating the possibility of using low-temperature thermal energy in liquefied natural gas complexes
(Rus)
Vol 8, No 3-2 (2009): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
The analyze of work of throttle cooling system’s microheat exchanger, wich uses nitrogen with nearly critical parameters
(Rus)
Vol 10, No 5 (2011)
ISSUE WITHOUT SECTION
Using a high-pressure vessel with cryogenic refuelling as a storage regasifier for autonomous complexes of gas supplyng and railway transport
(Rus)
Vol 10, No 3-4 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Preliminary tests of tank with cryogenic charging for onboard throttle system of cooling
(Rus)
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