Author Details
Borisoglebskij, A. V.
| Issue | Section | Title | File |
| Vol 5, No 2-2 (2006): Special Issue | TECHNICAL SCIENCES | A performance analysis of the pulsejet intended for aircraft acceleration up to mach number 0,9…1,2 |
 (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
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
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
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine