Author Details
Tolpegin, O. A.
| Issue | Section | Title | File |
| Vol 14, No 1 (2015) | AIRCRAFT AND SPACE ROCKET ENGINEERING | Missile control on the basis of construction of attainability domains |
 (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
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
mathematical modeling
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
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
mathematical modeling
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine