Author Details
Еремина, В. В.
| Issue | Section | Title | File |
| Vol 22, No 4 (2023) | AIRCRAFT AND SPACE ROCKET ENGINEERING | Features of the use of directional fixed antennas of a high-speed radio link on a small spacecraft AIST-2T |
 (Rus) |
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
User
Keywords
Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine
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User
Keywords
Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine