Author Details
Berns, V. A.
| Issue | Section | Title | File |
| Vol 15, No 1 (2016) | AIRCRAFT AND SPACE ROCKET ENGINEERING | Influence of the suspension system on the accuracy of the aircraft modal testing results |
 (Rus) |
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
User
Keywords
Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
deformation
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
structure
turbine
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User
Keywords
Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
deformation
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
structure
turbine