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
Ашихмина, Т. В.
Issue
Section
Title
File
Vol 5, No 1 (2006)
TECHNICAL SCIENCES
Peculiarities of setting up a problem of calculating processes fora general-purpose gas cylinder as anon-classical two-phase system and estimation of its temperature condition
(Rus)
Vol 6, No 2 (2007): Special Issue
TECHNICAL SCIENCES
Numerical modeling of physical processes in fuel tank refueled by cryogen conventional gas with undrainaged storage
(Rus)
Vol 6, No 2 (2007): Special Issue
TECHNICAL SCIENCES
Numerical modeling of physical processes in fuel tank refueled by cryogen conventional gas with undrainaged storage
(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)
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