Russian Aeronautics
ISSN 1068-7998 (Print)
ISSN 1934-7901 (Online)
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Keywords
aircraft
blade
combustion chamber
composite materials
finite element method
gas turbine engine
heat transfer
helicopter
main rotor
mathematical model
mathematical modeling
measurement
numerical modeling
optimization
rocket engine
rotor
spacecraft
stress-strain state
system
unmanned aerial vehicle
wind tunnel
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Keywords
aircraft
blade
combustion chamber
composite materials
finite element method
gas turbine engine
heat transfer
helicopter
main rotor
mathematical model
mathematical modeling
measurement
numerical modeling
optimization
rocket engine
rotor
spacecraft
stress-strain state
system
unmanned aerial vehicle
wind tunnel
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Author Details
Author Details
Khaliulin, R. R.
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Vol 61, No 1 (2018)
Aircraft and Rocket Engine Design and Development
Development of the Technique for Calculating the Ejectors with Low Entrainment Ratios
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