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
deformation
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
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
deformation
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
structure
turbine
Home
>
Search
>
Author Details
Author Details
Туманов, Н. В.
Issue
Section
Title
File
Vol 8, No 3-1 (2009): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Modeling stable growth of fatigue cracks in aero engine turbine discs under simple and complex loading cycles
(Rus)
Vol 9, No 4 (2010)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Multi-scale complex failure analysis of aero engine compressor disks
(Rus)
Vol 13, No 5-1 (2014): Special Issue
ISSUE WITHOUT SECTION
Conception of cycle life additivity and its application for determining the resource of aero engine disks
(Rus)
Vol 13, No 5-1 (2014): Special Issue
ISSUE WITHOUT SECTION
Kinetic equation of stable growth for low cycle fatigue cracks
(Rus)
Vol 14, No 3-1 (2015): Special Issue
ISSUE WITHOUT SECTION
Application of the cyclic life additivity concept for the determination of service life of aero engine disks made from powder alloys
(Rus)
Vol 10, No 3-2 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Study of mechanisms of low cycle fatigue crack propagation in aero engine disks under operating conditions and disk residual life estimation
(Rus)
Vol 10, No 3-2 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Complex failure analysis of aero engine compressor blades
(Rus)
This website uses cookies
You consent to our cookies if you continue to use our website.
About Cookies
TOP