Author Details
Wang, Ch.
| Issue | Section | Title | File |
| Vol 16, No 2 (2017) | AIRCRAFT AND SPACE ROCKET ENGINEERING | Control over the deployment of an orbital tether system of great length |
 (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
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
design
efficiency
experiment
finite element method
gas turbine engine
mathematical model
mathematical modeling
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine