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
Пегин, И. В.
Issue
Section
Title
File
Vol 11, No 3-1 (2012): Special Issue
CONFERENCE MATERIALS
Investigation of the possibility of the creation LREST by thrust 400 N with a baffle - centrifugal scheme of NT and NDMG mixing
(Rus)
Vol 13, No 5-1 (2014): Special Issue
ISSUE WITHOUT SECTION
50 n thrust correction engine for the "Luna-resurs" lunar module descent engine
(Rus)
Vol 13, No 5-1 (2014): Special Issue
ISSUE WITHOUT SECTION
Research of the influence of design parameters of a 400 N-thrust low-thrust liquid rocket engine on its energy efficiency
(Rus)
Vol 13, No 5-3 (2014): Special Issue
ISSUE WITHOUT SECTION
Results of experimental studies of parameters of low-thrust rocket engines operating on gaseous oxygen-hydrogen fuel
(Rus)
Vol 13, No 5-3 (2014): Special Issue
ISSUE WITHOUT SECTION
Verification of energy efficiency of a low-thrust liquid-propellant engine with the deflector-centrifugal injecting pattern
(Rus)
This website uses cookies
You consent to our cookies if you continue to use our website.
About Cookies
TOP