Author Details
Kalev, V. I.
| Issue | Section | Title | File |
| Vol 18, No 4 (2019) | AIRCRAFT AND SPACE ROCKET ENGINEERING | Solving the problem of minimax closed-loop control of liquid-propellant launch vehicle fuel consumption control |
 (Rus) |
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
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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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User
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