Formation of a method of choosing rational values of ultralow power turbine parameters in a turbine drive system - PDF (Russian)
Copyright (c)
Copyright (c)
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
User
Article Tools
Email this article (Login required)
Email the author (Login required)
Email this article (Login required)
Email the author (Login required)
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
×
User
Article Tools
Email this article (Login required)
Email the author (Login required)
Email this article (Login required)
Email the author (Login required)
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
Copyright (c)