Author Details
Юрина, А. Ю., ОАО “НПО “Сатурн”, г. Рыбинск, Russian Federation
| Issue | Section | Title | File |
| Vol 5, No 1 (2006) | AIRCRAFT AND SPACE ROCKET ENGINEERING | Parametric CFD designing of combustion chamber elements |
 (Rus) |
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
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
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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