VESTNIK of Samara University.
Aerospace and Mechanical Engineering
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
Menu
Archives
Home
About the Journal
Editorial Team
Editorial Policies
Author Guidelines
About the Journal
Issues
Search
Current
Articles in press
Retracted articles
Archives
Contact
Subscriptions
All Journals
User
Username
Password
Remember me
Forgot password?
Register
Search
Search
Search Scope
All
Authors
Title
Abstract
Index terms
Full Text
Browse
By Issue
By Author
By Title
By Sections
Other Journals
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
×
User
Username
Password
Remember me
Forgot password?
Register
Search
Search
Search Scope
All
Authors
Title
Abstract
Index terms
Full Text
Browse
By Issue
By Author
By Title
By Sections
Other Journals
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
Home
>
Search
>
Author Details
Author Details
Букатый, А. С., Рыбинская государственная авиационная технологическая академия имени П.А. Соловьева, Russian Federation
Issue
Section
Title
File
Vol 5, No 2-2 (2006): Special Issue
TECHNICAL SCIENCES
Prognostication of the technological residual deformations of slim disks after strengthening by means of superficial plastic straining
(Rus)
Vol 5, No 2-2 (2006): Special Issue
TECHNICAL SCIENCES
Automatical system for determination the residual tensions in the segments of complex forms
(Rus)
Vol 8, No 3-2 (2009): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
The determination of the efficient parameters of surface strenghtening the thin-walled and the small-hard parts of gas turbine engines based on deformation tolerance
(Rus)
This website uses cookies
You consent to our cookies if you continue to use our website.
About Cookies
TOP